pilot determines
                                                                                that the attitude
                                                                                is becoming
                                                                                uncontrollably
                                                                                divergent.
--------------------------------------------------------------------------------------------------------------------------------------------------------
2.d.3.c..................  Adverse/Proverse Yaw  Correct Trend,       Cruise or Climb.     Record the time         X      X      X
                                                  2[deg]   Augmentation On      history of initial
                                                  transient sideslip   and Off.             entry into cyclic
                                                  angle.                                    only turns, using
                                                                                only a moderate
                                                                                rate for cyclic
                                                                                input. Results
                                                                                must be recorded
                                                                                for turns in both
                                                                                directions.
--------------------------------------------------------------------------------------------------------------------------------------------------------
3. Reserved
--------------------------------------------------------------------------------------------------------------------------------------------------------
4. Visual System
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.a. Visual System Response Time: (Choose either test 4.a.1. or 4.a.2. to satisfy test 4.a., Visual System Response Time Test. This test is also
 sufficient for flight deck instrument response timing.)
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.a.1....................  Latency.............
--------------------------------------------------------------------------------------------------------------------------------------------------------
                                                 150 ms (or less)     Takeoff, climb, and  One test is                           X
                                                  after helicopter     descent.             required in each
                                                  response.                                 axis (pitch, roll
                                                                                and yaw) for each
                                                                                of the three
                                                                                conditions (take-
                                                                                off, cruise, and
                                                                                approach or
                                                                                landing).
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.a.2....................  Transport Delay.....
--------------------------------------------------------------------------------------------------------------------------------------------------------
                                                 150 ms (or less)     N/A................  A separate test is                    X
                                                  after controller                          required in each
                                                  movement.                                 axis (pitch, roll,
                                                                                and yaw).
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.b. Field of View
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.b.1....................  Reserved............
--------------------------------------------------------------------------------------------------------------------------------------------------------

4.b.2....................  Continuous visual     Minimum continuous   N/A................  An SOC is required                    X   Horizontal field of
                            field of view.        field of view                             and must explain                          view is centered
                                                  providing 146[deg]                        the geometry of                           on the zero degree
                                                  horizontal and                            the installation.                         azimuth line
                                                  36[deg] vertical                          Horizontal field                          relative to the
                                                  field of view for                         of view must not                          aircraft fuselage.
                                                  each pilot                                be less than a
                                                  simultaneously and                        total of 146[deg]
                                                  any geometric                             (including not
                                                  error between the                         less than 73[deg]
                                                  Image Generator                           measured either
                                                  eye point and the                         side of the center
                                                  pilot eye point is                        of the design eye
                                                  8[deg] or less.                           point). Additional
                                                                                horizontal field
                                                                                of view capability
                                                                                may be added at
                                                                                the sponsor's
                                                                                discretion
                                                                                provided the
                                                                                minimum field of
                                                                                view is retained.
                                                                                Vertical field of
                                                                                view: Not less
                                                                                than a total of
                                                                                36[deg] measured
                                                                                from the pilot's
                                                                                and co-pilot's eye
                                                                                point.
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.b.3....................  Reserved............
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.c......................  Surface contrast      Not less than 5:1..  N/A................  The ratio is                          X   Measurements may be
                            ratio.                                                          calculated by                             made using a
                                                                                dividing the                              1[deg] spot
                                                                                brightness level                          photometer and a
                                                                                of the center,                            raster drawn test
                                                                                bright square                             pattern filling
                                                                                (providing at                             the entire visual
                                                                                least 2 foot-                             scene (all
                                                                                lamberts or 7 cd/                         channels) with a
                                                                                m\2\) by the                              test pattern of
                                                                                brightness level                          black and white
                                                                                of any adjacent                           squares, 5 per
                                                                                dark square.                              square, with a
                                                                                white square in
                                                                                the center of each
                                                                                channel. During
                                                                                contrast ratio
                                                                                testing, simulator
                                                                                aft-cab and flight
                                                                                deck ambient light
                                                                                levels should be
                                                                                zero.
--------------------------------------------------------------------------------------------------------------------------------------------------------

4.d......................  Highlight brightness  Not less than three  N/A................  Measure the                           X   Measurements may be
                                                  (3) foot-lamberts                         brightness of the                         made using a
                                                  (10 cd/m\2\).                             center white                              1[deg] spot
                                                                                square while                              photometer and a
                                                                                superimposing a                           raster drawn test
                                                                                highlight on that                         pattern filling
                                                                                white square. The                         the entire visual
                                                                                use of                                    scene (all
                                                                                calligraphic                              channels) with a
                                                                                capabilities to                           test pattern of
                                                                                enhance the raster                        black and white
                                                                                brightness is                             squares, 5 per
                                                                                acceptable, but                           square, with a
                                                                                measuring light                           white square in
                                                                                points is not                             the center of each
                                                                                acceptable.                               channel.
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.e......................  Surface resolution..  Not greater than     N/A................  An SOC is required                    X   The eye will
                                                  two (2) arc                               and must include                          subtend two (2)
                                                  minutes.                                  the relevant                              arc minutes when
                                                                                calculations.                             positioned on a
                                                                                3[deg] glide
                                                                                slope, 6,876 ft
                                                                                slant range from
                                                                                the centrally
                                                                                located threshold
                                                                                of a black runway
                                                                                surface painted
                                                                                with white
                                                                                threshold bars
                                                                                that are 16 ft
                                                                                wide with 4-foot
                                                                                gaps between the
                                                                                bars. This
                                                                                requirement is the
                                                                                same as 4 arc
                                                                                minutes per
                                                                                optical line pair.
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.f......................  Light point size....  Not greater than     N/A................  An SOC is required                    X   Light point size
                                                  five (5) arc-                             and must include                          may be measured
                                                  minutes.                                  the relevant                              using a test
                                                                                calculations.                             pattern consisting
                                                                                of a centrally
                                                                                located single row
                                                                                of light points
                                                                                reduced in length
                                                                                until modulation
                                                                                is just
                                                                                discernible in
                                                                                each visual
                                                                                channel. A row of
                                                                                48 lights will
                                                                                form a 4[deg]
                                                                                angle or less.
--------------------------------------------------------------------------------------------------------------------------------------------------------

4.g......................  Light point contrast                                                                                A 1[deg] spot
                            ratio.                                                                                photometer may be
                                                                                used to measure a
                                                                                square of at least
                                                                                1[deg] filled with
                                                                                light points
                                                                                (where light point
                                                                                modulation is just
                                                                                discernible) and
                                                                                compare the
                                                                                results to the
                                                                                measured adjacent
                                                                                background. During
                                                                                contrast ratio
                                                                                testing, simulator
                                                                                aft-cab and flight
                                                                                deck ambient light
                                                                                levels should be
                                                                                zero.
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.g.1....................  Reserved............
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.g.2....................                        Not less than 25:1.  N/A................  An SOC is required                    X
                                                                                and must include
                                                                                the relevant
                                                                                calculations.
--------------------------------------------------------------------------------------------------------------------------------------------------------
4.h. Visual ground segment
--------------------------------------------------------------------------------------------------------------------------------------------------------
                                                 The visible segment  Landing              The QTG must                          X   Pre-position for
                                                  in the simulator     configuration,       contain relevant                          this test is
                                                  must be within 20%   trimmed for          calculations and a                        encouraged, but
                                                  of the segment       appropriate          drawing showing                           may be achieved
                                                  computed to be       airspeed, at 100     the data used to                          via manual or
                                                  visible from the     ft (30 m) above      establish the                             autopilot control
                                                  helicopter flight    the touchdown        helicopter                                to the desired
                                                  deck. The            zone, on glide       location and the                          position.
                                                  tolerance(s) may     slope with an RVR    segment of the
                                                  be applied at        value set at 1,200   ground that is
                                                  either end or at     ft (350 m).          visible
                                                  both ends of the                          considering design
                                                  displayed segment.                        eyepoint,
                                                  However, lights                           helicopter
                                                  and ground objects                        attitude, flight
                                                  computed to be                            deck cut-off
                                                  visible from the                          angle, and a
                                                  helicopter flight                         visibility of 1200
                                                  deck at the near                          ft (350 m) RVR.
                                                  end of the visible                        Simulator
                                                  segment must be                           performance must
                                                  visible in the                            be measured
                                                  simulator.                                against the QTG
                                                                                calculations. The
                                                                                data submitted
                                                                                must include at
                                                                                least the
                                                                                following:

                                                                                (1) Static
                                                                                helicopter
                                                                                dimensions as
                                                                                follows: (i)
                                                                                Horizontal and
                                                                                vertical distance
                                                                                from main landing
                                                                                gear (MLG) to
                                                                                glideslope
                                                                                reception antenna.
                                                                                (ii) Horizontal
                                                                                and vertical
                                                                                distance from MLG
                                                                                to pilot's
                                                                                eyepoint. (iii)
                                                                                Static flight deck
                                                                                cutoff angle.
                                                                                (2) Approach data
                                                                                as follows: (i)
                                                                                Identification of
                                                                                runway. (ii)
                                                                                Horizontal
                                                                                distance from
                                                                                runway threshold
                                                                                to glideslope
                                                                                intercept with
                                                                                runway. (iii)
                                                                                Glideslope angle.
                                                                                (iv) Helicopter
                                                                                pitch angle on
                                                                                approach.
                                                                                (3) Helicopter data
                                                                                for manual
                                                                                testing: (i) Gross
                                                                                weight. (ii)
                                                                                Helicopter
                                                                                configuration.
                                                                                (iii) Approach
                                                                                airspeed. If non-
                                                                                homogenous fog is
                                                                                used to obscure
                                                                                visibility, the
                                                                                vertical variation
                                                                                in horizontal
                                                                                visibility must be
                                                                                described and be
                                                                                included in the
                                                                                slant range
                                                                                visibility
                                                                                calculation used
                                                                                in the
                                                                                computations.
--------------------------------------------------------------------------------------------------------------------------------------------------------
5. Reserved
--------------------------------------------------------------------------------------------------------------------------------------------------------

-----------------------------------------------------------------------

Begin Information

3. Control Dynamics

    a. The characteristics of a helicopter flight control system
have a major effect on the handling qualities. A significant
consideration in pilot acceptability of a helicopter is the ``feel''
provided through the flight deck controls. Considerable effort is
expended on helicopter feel system design in order to deliver a
system with which pilots will be comfortable and consider the
helicopter desirable to fly. In order for an FTD to be
representative, it too must present the pilot with the proper feel;
that of the respective helicopter.
    (1) Recordings such as free response to an impulse or step
function are classically used to estimate the dynamic properties of
electromechanical systems. It is only possible to estimate the
dynamic properties as a result of only being able to estimate true
inputs and responses. Therefore, it is imperative that the best
possible data be collected since close matching of the FTD control
loading system to the helicopter systems is essential. Control feel
dynamic tests are described in the Table of Objective Tests in this
appendix. Where accomplished, the free response is measured after a
step or pulse input is used to excite the system.
    (2) For initial and upgrade evaluations, it is required that
control dynamic characteristics be measured at and recorded directly
from the flight deck controls. This procedure is usually
accomplished by measuring the free response of the controls using a
step or pulse input to excite the system. The procedure must be
accomplished in hover, climb, cruise, and autorotation. For
helicopters with irreversible control systems, measurements may be
obtained on the ground. Proper pitot-static inputs (if appropriate)
must be provided to represent airspeeds typical of those encountered
in flight.
    (3) It may be shown that for some helicopters, climb, cruise,
and autorotation have like effects. Thus, some tests for one may
suffice for some tests for another. If either or both considerations
apply, engineering validation or helicopter manufacturer rationale
must be submitted as justification for ground tests or for
eliminating a configuration. For FTDs requiring static and dynamic
tests at the controls, special test fixtures will not be required
during initial and upgrade evaluations if the sponsor's QTG shows
both test fixture results and the results of an alternative
approach, such as computer plots which were produced concurrently
and show satisfactory agreement. Repeat of the alternative method
during the initial evaluation would then satisfy this test
requirement.
    b. Control Dynamics Evaluations. The dynamic properties of
control systems are often stated in terms of frequency, damping, and
a number of other classical measurements which can be found in texts
on control systems. In order to establish a consistent means of
validating test results for FTD control loading, criteria are needed
that will clearly define the interpretation of the measurements and
the tolerances to be applied. Criteria are needed for both the
underdamped system and the overdamped system, including the
critically damped case. In the case of an underdamped system with
very light damping, the system may be quantified in terms of
frequency and damping. In critically damped or overdamped systems,
the frequency and damping is not readily measured from a response
time history. Therefore, some other measurement must be used.
    (1) Tests to verify that control feel dynamics represent the
helicopter must show that the dynamic damping cycles (free response
of the control) match that of the helicopter within specified
tolerances. The method of evaluating the response and the tolerance
to be applied are described below for the underdamped and critically
damped cases.
    (a) Underdamped Response. Two measurements are required for the
period, the time to first zero crossing (in case a rate limit is
present) and the subsequent frequency of oscillation. It is
necessary to measure cycles on an individual basis in case there are
nonuniform periods in the response. Each period will be
independently compared to the respective period of the helicopter
control system and, consequently, will enjoy the full tolerance
specified for that period.
    (b) The damping tolerance will be applied to overshoots on an
individual basis. Care must be taken when applying the tolerance to
small overshoots since the significance of such overshoots becomes
questionable. Only those overshoots larger than 5 percent of the
total initial displacement will be considered significant. The
residual band, labeled T(Ad) on Figure 1 of this
attachment is 5 percent of the initial displacement
amplitude, Ad, from the steady state value of the
oscillation. Oscillations within the residual band are considered
insignificant. When comparing simulator data to helicopter data, the
process would begin by overlaying or aligning the simulator and
helicopter steady state values and then comparing amplitudes of
oscillation peaks, the time of the first zero crossing, and
individual periods of oscillation. To be satisfactory, the simulator
must show the same number of significant overshoots to within one
when compared against the helicopter data. The procedure for
evaluating the response is illustrated in Figure 1 of this
attachment.
    (c) Critically Damped and Overdamped Response. Due to the nature
of critically damped responses (no overshoots), the time to reach 90
percent of the steady state (neutral point) value must be the same
as the helicopter within 10 percent. The simulator
response must be critically damped also. Figure 2 of this attachment
illustrates the procedure.
    (d) Special considerations. Control systems that exhibit
characteristics other than classical overdamped or underdamped
responses should meet specified tolerances. In addition, special
consideration should be given to ensure that significant trends are
maintained.
    (2) Tolerances.
    (a) The following summarizes the tolerances, ``T'' for
underdamped systems, and ``n'' is the sequential period of a full
cycle of oscillation. See Figure D2A of this attachment for an
illustration of the referenced measurements.

T(P0).................................  10% of P0
T(P1).................................  20% of P1
T(P2).................................  30% of P2
T(Pn).................................  10(n+1)% of Pn
T(An).................................  10% of A1
T(Ad).................................  5% of Ad = residual
                                         band
Significant overshoots................  First overshoot and < plus-
                                         minus>1 subsequent overshoots

    (b) The following tolerance applies to critically damped and
overdamped systems only. See Figure D2B for an illustration of the
reference measurements:

T(P0).................................  10% of P0

BILLING CODE 4910-13-P

[GRAPHIC] [TIFF OMITTED] TP22OC07.050

End Information

-----------------------------------------------------------------------

Begin QPS Requirement

BILLING CODE 4910-13-C
    c. Alternative method for control dynamics evaluation.
    (1) An alternative means for validating control dynamics for
aircraft with hydraulically powered flight controls and artificial
feel systems is by the measurement of control force and rate of
movement. For each axis of pitch, roll, and yaw, the control must be
forced to its maximum extreme position for the following distinct
rates. These tests are conducted at under normal flight and ground
conditions.
    (a) Static test--Slowly move the control so that a full sweep is
achieved within 95-105 seconds. A full sweep is defined as movement
of the controller from neutral to the stop, usually aft or right
stop, then to the opposite stop, then to the neutral position.
    (b) Slow dynamic test--Achieve a full sweep within 8-12 seconds.
    (c) Fast dynamic test--Achieve a full sweep within 3-5 seconds.

    Note: Dynamic sweeps may be limited to forces not exceeding 100
lbs. (44.5 daN).

    (d) Tolerances
    (i) Static test; see Table D2A, Flight Training Device (FTD)
Objective Tests, Items 2.a.1., 2.a.2., and 2.a.3.
    (ii) Dynamic test--2 lbs (0.9 daN) or 10% on dynamic increment above static test.

End QPS Requirement

-----------------------------------------------------------------------

Begin Information

    d. The FAA is open to alternative means that are justified and
appropriate to the application. For example, the method described
here may not apply to all manufacturers' systems and certainly not
to aircraft with reversible control systems. Each

case is considered on its own merit on an ad hoc basis. If the FAA
finds that alternative methods do not result in satisfactory
performance, more conventionally accepted methods will have to be
used.

4. For Additional Information on the Following Topics, Please Refer to
Appendix C, Attachment 2, and the Indicated Paragraph Within That
Attachment

     Additional Information About Flight Simulator
Qualification for New or Derivative Helicopters, paragraph 8.
     Engineering Simulator Validation Data, paragraph 9.
     Validation Test Tolerances, paragraph 11.
     Validation Data Road Map, paragraph 12.
     Acceptance Guidelines for Alternative Avionics,
paragraph 13.
     Transport Delay Testing, paragraph 14.
     Continuing Qualification Evaluation Validation Data
Presentation, paragraph 15.

End Information

-----------------------------------------------------------------------

Attachment 3 to Appendix D to Part 60--Flight Training Device (FTD)
Subjective Evaluation

-----------------------------------------------------------------------

Begin QPS Requirements

1. Requirements

    a. Except for special use visual scenes and airport models
described below, all visual scenes and airport models required by
this part must be representations of real-world, operational
airports or representations of fictional airports and must meet the
requirements set out in Tables D3B and D3C of this attachment, as
appropriate.
    b. If fictional airports are used, the sponsor must ensure that
navigational aids and all appropriate maps, charts, and other
navigational reference material for the fictional airports (and
surrounding areas as necessary) are compatible, complete, and
accurate with respect to the visual presentation and scene content
of the visual model of this fictional airport. An SOC must be
submitted that addresses navigation aid installation and performance
and other criteria (including obstruction clearance protection) for
all instrument approaches to the fictional airports that are
available in the simulator. The SOC must reference and account for
information in the terminal instrument procedures manual and the
construction and availability of the required maps, charts, and
other navigational material. This material must be clearly marked
``for training purposes only.''
    c. When the simulator is being used by an instructor or
evaluator for purposes of training, checking, or testing under this
chapter, only visual scenes and airport models classified as Class
I, Class II, or Class III may be available to the instructor or
evaluator. The classifications are as follows:
    (1) Class I (whether modeling real world airports or fictional
airports), for those visual scenes and airport models used for FTD
qualification at a specified level. These visual scenes and airport
models must meet the minimum requirements in Table D3B of this
attachment, be evaluated by the NSPM, be listed on the Statement of
Qualification(SOQ), and be available for use at the FTD IOS.
    (2) Class II (whether modeling real world airports or fictional
airports), for those visual scenes and airport models that are in
excess of those used for FTD qualification at a specified level.
These visual scenes and airport models must meet the minimum
requirements set out in Table C3C of this attachment. These visual
scenes and airport models may be made available on the FTD IOS
without further involvement of the NSPM or the TPAA.
    (3) For an interim period ending (2 years after date of
publication of the final rule in the Federal Register), Class III
visual scenes and airport models (whether modeling real world
airports, generic airports, or fictional airports) may be approved
for specific purposes by the TPAA or a foreign regulatory authority
for a foreign user of the device. Examples of approved activities
include specific airport or runway qualification, very low
visibility operations training, including Surface Movement Guidance
System (SMGS) operations, or use of a specific airport visual model
aligned with an instrument procedure for another airport for
instrument training. At the end of the interim period, all Class III
visual scenes and airport models must be classified as either a
Class I or a Class II visual scene or airport model or be removed
from availability at the simulator IOS. However, Class III visual
scenes and airport models may continue to be used after the end of
the interim period if they are part of a training program
specifically approved by the TPAA or other regulatory authority that
uses a task and capability analysis as the basis for approval of
this specific media element, (i.e., the specific scene or model
selected for use in that program).
    d. When a person sponsors an FSTD maintained by a person other
than a U.S. certificate holder, the sponsor is accountable for that
FSTD originally meeting, and continuing to meet, the criteria under
which it was originally qualified and the appropriate Part 60
criteria, including the visual scenes and airport models that may be
used by instructors or evaluators for purposes of training,
checking, or testing under this chapter.
    e. Neither Class II nor Class III airport visual models are
required to appear on the SOQ. However, the sponsor is accountable
that the FSTD originally meets, and continues to meet, the visual
scene and airport model requirements for Class II or Class III
visual scenes and airport models that may be used by instructors or
evaluators for training, checking, or testing under this chapter.
    f. When the visual scenes and airport models represent real
world airports and a permanent change is made to that real world
airport (e.g., a new runway, an extended taxiway, a new lighting
system, a runway closure) without a written extension grant from the
NSPM (described below), an update to that visual scene or airport
model must be made in accordance with the following time limits:
    (1) For a new airport runway, a runway extension, a new airport
taxiway, a taxiway extension, or a runway/taxiway closure--within 60
days of the opening for use of the new airport runway, runway
extension, new airport taxiway, or taxiway extension; or within 60
days of the closure of the runway or taxiway.
    (2) For a new or modified approach light system--within 30 days
of the activation of the new or modified approach light system.
    (3) For other facility or structural changes on the airport
(e.g., new terminal, relocation of Air Traffic Control Tower)--
within 6 months of the opening of the new or changed facility or
structure.
    g. If a sponsor desires an extension to the time limit for an
update to a visual scene or airport model, the sponsor must provide
a written extension request to the POI/TCPM stating the reason for
the update delay and a proposed completion date. A copy of this
request must also be sent to the NSPM. The sponsor will forward a
copy of the POI/TCPM's response to the NSPM. If the POI/TCPM has
granted an extension, the NSPM will issue an extension
authorization, not to exceed an additional 12 months.

End QPS Requirements

-----------------------------------------------------------------------

Begin Information

2. Discussion

    a. The subjective tests and the examination of functions provide
a basis for evaluating the capability of the FTD to perform over a
typical utilization period; determining that the FTD satisfactorily
meets the appropriate training/testing/checking objectives and
competently simulates each required maneuver, procedure, or task;
and verifying correct operation of the FTD controls, instruments,
and systems. The items in the list of operations tasks are for FTD
evaluation purposes only. They must not be used to limit or exceed
the authorizations for use of a given level of FTD as found in the
Practical Test Standards or as may be approved by the TPAA. All
items in the following paragraphs are subject to an examination of
function.
    b. The List of Operations Tasks addressing pilot functions and
maneuvers is divided by flight phases. All simulated helicopter
systems functions will be assessed for normal and, where
appropriate, alternate operations. Normal, abnormal, and emergency
operations associated with a flight phase will be assessed during
the evaluation of maneuvers or events within that flight phase.
    c. Systems to be evaluated are listed separately under ``Any
Flight Phase'' to ensure appropriate attention to systems checks.
Operational navigation systems (including inertial navigation
systems, global positioning systems, or other long-range systems)
and the associated electronic display systems will be evaluated if
installed. The NSP pilot will include in his report to the TPAA, the
effect of the system operation and any system limitation.
    d. At the request of the TPAA, the NSP Pilot may assess the FTD
for a special aspect of a sponsor's training program during the
functions and subjective portion of an evaluation. Such an
assessment may include a portion of a specific operation (e.g., a
Line Oriented Flight Training (LOFT) scenario) or

special emphasis items in the sponsor's training program. Unless
directly related to a requirement for the qualification level, the
results of such an evaluation would not necessarily affect the
qualification of the FTD.
    e. The FAA intends to allow the use of Class III visual scenes
and airport models on a limited basis when the sponsor provides the
TPAA (or other regulatory authority) an appropriate analysis of the
skills, knowledge, and abilities (SKAs) necessary for competent
performance of the tasks in which this particular media element is
used. The analysis should describe the ability of the FSTD/visual
media to provide an adequate environment in which the required SKAs
may be satisfactorily performed and learned. The analysis should
also include the specific media element, such as the visual scene or
airport model. Additional sources of information on the conduct of
task and capability analysis may be found on the FAA's Advanced
Qualification Program (AQP) Web site at: http://www.faa.gov/education_research/training/aqp/
.

End Information

-----------------------------------------------------------------------

     Table D3A.--Table of Functions and Subjective Tests Level 7 FTD
------------------------------------------------------------------------
                         <<>>
-------------------------------------------------------------------------
         Number                          Operations tasks
------------------------------------------------------------------------
Tasks in this table are subject to evaluation if appropriate for the
 helicopter simulated as indicated in the SOQ Configuration List or a
 Level 7 FTD. Items not installed, not functional on the FTD, and not
 appearing on the SOQ Configuration List, are not required to be listed
 as exceptions on the SOQ.
------------------------------------------------------------------------
1. Preflight Procedures
------------------------------------------------------------------------
1.a....................  Preflight Inspection (Flight Deck Only)
                          switches, indicators, systems, and equipment.
------------------------------------------------------------------------
1.b....................  APU/Engine start and run-up.
------------------------------------------------------------------------
1.b.1..................  Normal start procedures.
------------------------------------------------------------------------
1.b.2..................  Alternate start procedures.
------------------------------------------------------------------------
1.b.3..................  Abnormal starts and shutdowns (hot start, hung
                          start).
------------------------------------------------------------------------
1.b.4..................  Rotor engagement.
------------------------------------------------------------------------
1.b.5..................  System checks.
------------------------------------------------------------------------
1.c....................  Taxiing--Ground.
------------------------------------------------------------------------
1.c.1..................  Power required to taxi.
------------------------------------------------------------------------
1.c.2..................  Brake effectiveness.
------------------------------------------------------------------------
1.c.3..................  Ground handling.
------------------------------------------------------------------------
1.c.4..................  Abnormal/emergency procedures, for example:
------------------------------------------------------------------------
1.c.4.a................  Brake system failure.
------------------------------------------------------------------------
1.c.4.b................  Ground resonance.
------------------------------------------------------------------------
1.c.4.c................  Other (as may be listed on the Statement of
                          Qualification).
------------------------------------------------------------------------
1.d....................  Taxiing--Hover.
------------------------------------------------------------------------
1.d.1..................  Takeoff to a hover.
------------------------------------------------------------------------
1.d.2..................  Instrument response.
------------------------------------------------------------------------
1.d.2.a................  Engine instruments.
------------------------------------------------------------------------
1.d.2.a................  Flight instruments.
------------------------------------------------------------------------
1.d.3..................  Hovering turns.
------------------------------------------------------------------------
1.d.4..................  Hover power checks.
------------------------------------------------------------------------
1.d.4.a................  In ground effect (IGE).
------------------------------------------------------------------------
1.d.4.b................  Out of ground effect (OGE).
------------------------------------------------------------------------
1.d.5..................  Crosswind/tailwind hover.
------------------------------------------------------------------------
1.d.6..................  Abnormal/emergency procedures:
------------------------------------------------------------------------
1.d.6.a................  Engine failure.
------------------------------------------------------------------------

1.d.6.b................  Fuel governing system failure.
------------------------------------------------------------------------
1.d.6.c................  Settling with power (OGE).
------------------------------------------------------------------------
1.d.6.d................  Stability augmentation system failure.
------------------------------------------------------------------------
1.d.6.e................  Directional control malfunction (including Loss
                          of Tail Rotor Effectiveness, LTE).
------------------------------------------------------------------------
1.d.6.f................  Other (as may be listed on the Statement of
                          Qualification).
------------------------------------------------------------------------
1.e....................  Pre-takeoff Checks.
------------------------------------------------------------------------
2. Takeoff and Departure Phase
------------------------------------------------------------------------
2.a....................  Normal and Crosswind Takeoff.
------------------------------------------------------------------------
2.a.1..................  From ground.
------------------------------------------------------------------------
2.a.2..................  From hover.
------------------------------------------------------------------------
2.a.3..................  Running.
------------------------------------------------------------------------
2.a.4..................  Crosswind/tailwind.
------------------------------------------------------------------------
2.a.5..................  Maximum performance.
------------------------------------------------------------------------
2.b....................  Instrument.
------------------------------------------------------------------------
2.c....................  Powerplant Failure During Takeoff.
------------------------------------------------------------------------
2.c.1..................  Takeoff with engine failure after critical
                          decision point (CDP).
------------------------------------------------------------------------
2.d....................  Rejected Takeoff.
------------------------------------------------------------------------
2.e....................  Instrument Departure.
------------------------------------------------------------------------
2.f....................  Other (as may be listed on the Statement of
                          Qualification).
------------------------------------------------------------------------
3. Climb
------------------------------------------------------------------------
3.a....................  Normal.
------------------------------------------------------------------------
3.b....................  Obstacle clearance.
------------------------------------------------------------------------
3.c....................  Vertical.
------------------------------------------------------------------------
3.d....................  One engine inoperative.
------------------------------------------------------------------------
3.e....................  Other (as may be listed on the Statement of
                          Qualification).
------------------------------------------------------------------------
4. Inflight Maneuvers
------------------------------------------------------------------------
4.a....................  Performance.
------------------------------------------------------------------------
4.b....................  Flying qualities.
------------------------------------------------------------------------
4.c....................  Turns.
------------------------------------------------------------------------
4.c.1..................  Timed.
------------------------------------------------------------------------
4.c.2..................  Normal.
------------------------------------------------------------------------
4.c.3..................  Steep.
------------------------------------------------------------------------
4.d....................  Accelerations and decelerations.
------------------------------------------------------------------------
4.e....................  High-speed vibrations.
------------------------------------------------------------------------
4.f....................  Abnormal/emergency procedures, for example:
------------------------------------------------------------------------
4.f.1..................  Engine fire.
------------------------------------------------------------------------

4.f.2..................  Engine failure.
------------------------------------------------------------------------
4.f.2.a................  Powerplant Failure--Multiengine Helicopters.
------------------------------------------------------------------------
4.f.2.b................  Powerplant Failure--Single-Engine Helicopters.
------------------------------------------------------------------------
4.f.3..................  In-flight engine shutdown (and restart, if
                          applicable).
------------------------------------------------------------------------
4.f.4..................  Fuel governing system failures (e.g., FADEC
                          malfunction).
------------------------------------------------------------------------
4.f.5..................  Directional control malfunction.
------------------------------------------------------------------------
4.f.6..................  Hydraulic failure.
------------------------------------------------------------------------
4.f.7..................  Stability augmentation system failure.
------------------------------------------------------------------------
4.f.8..................  Rotor vibrations.
------------------------------------------------------------------------
4.f.9..................  Recovery From Unusual Attitudes.
------------------------------------------------------------------------
4.f.10.................  Settling with Power.
------------------------------------------------------------------------
4.g....................  Other (as may be listed on the Statement of
                          Qualification).
------------------------------------------------------------------------
5. Instrument Procedures
------------------------------------------------------------------------
5.a....................  Instrument Arrival.
------------------------------------------------------------------------
5.b....................  Holding.
------------------------------------------------------------------------
5.c....................  Precision Instrument Approach.
------------------------------------------------------------------------
5.c.1..................  Normal--All engines operating.
------------------------------------------------------------------------
5.c.2..................  Manually controlled--One or more engines
                          inoperative.
------------------------------------------------------------------------
5.c.3..................  Approach procedures:
------------------------------------------------------------------------
5.c.3.a................  PAR.
------------------------------------------------------------------------
5.c.3.b................  GPS.
------------------------------------------------------------------------
5.c.3.c................  ILS.
------------------------------------------------------------------------
5.c.3.c.1..............  Manual (raw data).
------------------------------------------------------------------------
5.c.3.c.2..............  Autopilot* only.
------------------------------------------------------------------------
5.c.3.c.3..............  Flight director only.
------------------------------------------------------------------------
5.c.3.c.4..............  Autopilot* and flight director (if appropriate)
                          coupled.
------------------------------------------------------------------------
5.c.3.d................  Other (as may be listed on the Statement of
                          Qualification).
------------------------------------------------------------------------
5.d....................  Non-precision Instrument Approach.
------------------------------------------------------------------------
5.d.1..................  Normal--All engines operating.
------------------------------------------------------------------------
5.d.2..................  One or more engines inoperative.
------------------------------------------------------------------------
5.d.3..................  Approach procedures:
------------------------------------------------------------------------
5.d.3.a................  NDB.
------------------------------------------------------------------------
5.d.3.b................  VOR, RNAV, TACAN, GPS.
------------------------------------------------------------------------
5.d.3.c................  ASR.
------------------------------------------------------------------------
5.d.3.d................  Circling.
------------------------------------------------------------------------
5.d.3.e................  Helicopter only.
------------------------------------------------------------------------

5.d.3.f................  Other (as may be listed on the Statement of
                          Qualification.
------------------------------------------------------------------------
5.e....................  Missed Approach.
------------------------------------------------------------------------
5.e.1..................  All engines operating.
------------------------------------------------------------------------
5.e.2..................  One or more engines inoperative.
------------------------------------------------------------------------
5.e.3..................  Stability augmentation system failure.
------------------------------------------------------------------------
5.e.4..................  Other (as may be listed on the Statement of
                          Qualification).
------------------------------------------------------------------------
6. Landings and Approaches to Landings
------------------------------------------------------------------------
6.a....................  Visual Approaches.
------------------------------------------------------------------------
6.a.1..................  Normal.
------------------------------------------------------------------------
6.a.2..................  Steep.
------------------------------------------------------------------------
6.a.3..................  Shallow.
------------------------------------------------------------------------
6.a.4..................  Crosswind.
------------------------------------------------------------------------
6.b....................  Landings.
------------------------------------------------------------------------
6.b.1..................  Normal.
------------------------------------------------------------------------
6.b.1.a................  Running.
------------------------------------------------------------------------
6.b.1.b................  From Hover.
------------------------------------------------------------------------
6.b.2..................  Crosswind.
------------------------------------------------------------------------
6.b.3..................  Tailwind.
------------------------------------------------------------------------
6.b.4..................  One or more engines inoperative.
------------------------------------------------------------------------
6.b.5..................  Rejected Landing.
------------------------------------------------------------------------
6.b.6..................  Other (as may be listed on the Statement of
                          Qualification).
------------------------------------------------------------------------
7. Normal and Abnormal Procedures (any phase of flight)
------------------------------------------------------------------------
7.a....................  Helicopter and powerplant systems operation (as
                          applicable).
------------------------------------------------------------------------
7.a.1..................  Anti-icing/deicing systems.
------------------------------------------------------------------------
7.a.2..................  Auxiliary power-plant.
------------------------------------------------------------------------
7.a.3..................  Communications.
------------------------------------------------------------------------
7.a.4..................  Electrical system.
------------------------------------------------------------------------
7.a.5..................  Environmental system.
------------------------------------------------------------------------
7.a.6..................  Fire detection and suppression.
------------------------------------------------------------------------
7.a.7..................  Flight control system.
------------------------------------------------------------------------
7.a.8..................  Fuel system.
------------------------------------------------------------------------
7.a.9..................  Engine oil system.
------------------------------------------------------------------------
7.a.10.................  Hydraulic system.
------------------------------------------------------------------------
7.a.11.................  Landing gear.
------------------------------------------------------------------------
7.a.12.................  Oxygen.
------------------------------------------------------------------------
7.a.13.................  Pneumatic.
------------------------------------------------------------------------

7.a.14.................  Powerplant.
------------------------------------------------------------------------
7.a.15.................  Flight control computers.
------------------------------------------------------------------------
7.a.16.................  Fly-by-wire controls.
------------------------------------------------------------------------
7.a.17.................  Stabilizer.
------------------------------------------------------------------------
7.a.18.................  Stability augmentation and control augmentation
                          system(s).
------------------------------------------------------------------------
7.a.19.................  Other (as may be listed on the Statement of
                          Qualification).
------------------------------------------------------------------------
7.b....................  Flight management and guidance system (as
                          applicable).
------------------------------------------------------------------------
7.b.1..................  Airborne radar.
------------------------------------------------------------------------
7.b.2..................  Automatic landing aids.
------------------------------------------------------------------------
7.b.3..................  Autopilot*.
------------------------------------------------------------------------
7.b.4..................  Collision avoidance system.
------------------------------------------------------------------------
7.b.5..................  Flight data displays.
------------------------------------------------------------------------
7.b.6..................  Flight management computers.
------------------------------------------------------------------------
7.b.7..................  Head-up displays.
------------------------------------------------------------------------
7.b.8..................  Navigation systems.
------------------------------------------------------------------------
7.b.9..................  Other (as may be listed on the Statement of
                          Qualification).
------------------------------------------------------------------------
8. Emergency procedures (as applicable)
------------------------------------------------------------------------
8.a....................  Autorotative Landing.
------------------------------------------------------------------------
8.b....................  Air hazard avoidance.
------------------------------------------------------------------------
8.c....................  Ditching.
------------------------------------------------------------------------
8.d....................  Emergency evacuation.
------------------------------------------------------------------------
8.e....................  Inflight fire and smoke removal.
------------------------------------------------------------------------
8.f....................  Retreating blade stall recovery.
------------------------------------------------------------------------
8.g....................  Mast bumping.
------------------------------------------------------------------------
8.h....................  Loss of tail rotor effectiveness.
------------------------------------------------------------------------
8.i....................  Other (as may be listed on the Statement of
                          Qualification).
------------------------------------------------------------------------
9. Postflight Procedures
------------------------------------------------------------------------
9.a....................  After-Landing Procedures.
------------------------------------------------------------------------
9.b....................  Parking and Securing.
------------------------------------------------------------------------
9.b.1..................  Engine and systems operation.
------------------------------------------------------------------------
9.b.2..................  Parking brake operation.
------------------------------------------------------------------------
9.b.3..................  Rotor brake operation.
------------------------------------------------------------------------
9.b.4..................  Abnormal/emergency procedures.
------------------------------------------------------------------------
10. Instructor Operating Station (IOS), as appropriate
------------------------------------------------------------------------
10.a...................  Power Switch(es).
------------------------------------------------------------------------
10.b...................  Helicopter conditions.
------------------------------------------------------------------------

10.b.1.................  Gross weight, center of gravity, fuel loading
                          and allocation, etc.
------------------------------------------------------------------------
10.b.2.................  Helicopter systems status.
------------------------------------------------------------------------
10.b.3.................  Ground crew functions (e.g., ext. power).
------------------------------------------------------------------------
10.c...................  Airports.
------------------------------------------------------------------------
10.c.1.................  Selection.
------------------------------------------------------------------------
10.c.2.................  Runway selection.
------------------------------------------------------------------------
10.c.3.................  Preset positions (e.g., ramp, over final
                          approach fix).
------------------------------------------------------------------------
10.d...................  Environmental controls.
------------------------------------------------------------------------
10.d.1.................  Temperature.
------------------------------------------------------------------------
10.d.2.................  Climate conditions (e.g., ice, rain).
------------------------------------------------------------------------
10.d.3.................  Wind speed and direction.
------------------------------------------------------------------------
10.e...................  Helicopter system malfunctions.
------------------------------------------------------------------------
10.e.1.................  Insertion/deletion.
------------------------------------------------------------------------
10.e.2.................  Problem clear.
------------------------------------------------------------------------
10.f...................  Locks, Freezes, and Repositioning.
------------------------------------------------------------------------
10.f.1.................  Problem (all) freeze/release.
------------------------------------------------------------------------
10.f.2.................  Position (geographic) freeze/release.
------------------------------------------------------------------------
10.f.3.................  Repositioning (locations, freezes, and
                          releases).
------------------------------------------------------------------------
10.f.4.................  Ground speed control.
------------------------------------------------------------------------
10.g...................  Sound Controls.
------------------------------------------------------------------------
10.g.1.................  On/off/adjustment.
------------------------------------------------------------------------
10.h...................  Control Loading System (as applicable).
------------------------------------------------------------------------
10.h.1.................  On/off/emergency stop.
------------------------------------------------------------------------
10.i...................  Observer Stations.
------------------------------------------------------------------------
10.i.1.................  Position.
------------------------------------------------------------------------
10.i.2.................  Adjustments.
------------------------------------------------------------------------
*``Autopilot'' means attitude retention mode of operation.

     Table D3B.--Table of Functions and Subjective Tests Level 7 FTD
------------------------------------------------------------------------
                         <<>>
-------------------------------------------------------------------------
                              Visual scene content requirements for
         Number                      qualification at Level 7
------------------------------------------------------------------------
This table specifies the minimum airport visual model content and
 functionality to qualify an FTD at the indicated level. This table
 applies only to the airport/helicopter landing area scenes required for
 FTD qualification.
------------------------------------------------------------------------
1......................  Functional test content requirements for Level
                          7 Flight Training Devices.
------------------------------------------------------------------------
                         The following is the minimum airport/landing
                          area model content requirement to satisfy
                          visual capability tests, and provides suitable
                          visual cues to allow completion of all
                          functions and subjective tests described in
                          this attachment for FTDs at Levels 7.
------------------------------------------------------------------------
1.a....................  A minimum of one (1) representative airport and
                          one (1) representative helicopter landing area
                          model.

                         The airport and the helicopter landing area may
                          be contained within the same visual model. If
                          this option is selected, the approach path to
                          the airport runway(s) and the approach path to
                          the helicopter landing area must be different.
                          The model(s) used to meet the following
                          requirements may be demonstrated at either a
                          fictional or a real-world airport or
                          helicopter landing area, but each must be
                          acceptable to the sponsor's TPAA, selectable
                          from the IOS, and listed on the Statement of
                          Qualification.
------------------------------------------------------------------------
1.b....................  Fidelity of the Visual Scene.
                         The fidelity of the visual scene must be
                          sufficient for the aircrew to visually
                          identify the airport and/or helicopter landing
                          area; determine the position of the simulated
                          helicopter within the visual scene;
                          successfully accomplish take-offs, approaches,
                          and landings; and maneuver around the airport
                          and/or helicopter landing area on the ground,
                          or hover taxi, as necessary.
------------------------------------------------------------------------
1.b.1..................  For each of the airport/helicopter landing
                          areas described in 1.a., the FTD visual system
                          must be able to provide at least the
                          following:
------------------------------------------------------------------------
1.b.1.a................  A night and twilight (dusk) environment.
------------------------------------------------------------------------
1.b.1.b................  A daylight environment.
------------------------------------------------------------------------
1.c....................  Runways:
------------------------------------------------------------------------
1.c.1..................  Visible runway number.
------------------------------------------------------------------------
1.c.2..................  Runway threshold elevations and locations must
                          be modeled to provide sufficient correlation
                          with helicopter systems (e.g., altimeter).
------------------------------------------------------------------------
1.c.3..................  Runway surface and markings.
------------------------------------------------------------------------
1.c.4..................  Lighting for the runway in use including runway
                          edge and centerline.
------------------------------------------------------------------------
1.c.5..................  Lighting, visual approach aid (VASI or PAPI)
                          and approach lighting of appropriate colors.
------------------------------------------------------------------------
1.c.6..................  Taxiway lights.
------------------------------------------------------------------------
1.d....................  Helicopter landing area.
------------------------------------------------------------------------
1.d.1..................  Standard heliport designation (``H'') marking,
                          properly sized and oriented.
------------------------------------------------------------------------
1.d.2..................  Perimeter markings for the Touchdown and Lift-
                          Off Area (TLOF) or the Final Approach and
                          Takeoff Area (FATO), as appropriate.
------------------------------------------------------------------------
1.d.3..................  Perimeter lighting for the TLOF or the FATO
                          areas, as appropriate.
------------------------------------------------------------------------
1.d.4..................  Appropriate markings and lighting to allow
                          movement from the runway or helicopter landing
                          area to another part of the landing facility.
------------------------------------------------------------------------
2......................  Visual scene management.
                         The following is the minimum visual scene
                          management requirements for a Level 7 FTD.
------------------------------------------------------------------------
2.a....................  Runway and helicopter landing area approach
                          lighting must fade into view appropriately in
                          accordance with the environmental conditions
                          set in the FTD.
------------------------------------------------------------------------
2.b....................  The direction of strobe lights, approach
                          lights, runway edge lights, visual landing
                          aids, runway centerline lights, threshold
                          lights, touchdown zone lights, and TLOF or
                          FATO lights must be replicated.
------------------------------------------------------------------------
3......................  Visual feature recognition.
                         The following are the minimum distances at
                          which runway features must be visible.
                          Distances are measured from runway threshold
                          or a helicopter landing area to a helicopter
                          aligned with the runway or helicopter landing
                          area on an extended 3[deg] glide-slope in
                          simulated meteorological conditions. For
                          circling approaches, all tests apply to the
                          runway used for the initial approach and to
                          the runway of intended landing.
------------------------------------------------------------------------
3.a....................  For runways: runway definition, strobe lights,
                          approach lights, and edge lights from 5 sm (8
                          km) of the threshold.
------------------------------------------------------------------------
3.b....................  For runways: centerline lights and taxiway
                          definition from 3 sm (5 km).
------------------------------------------------------------------------
3.c....................  For runways: Visual Approach Aid lights (VASI
                          or PAPI) from 3 sm (5 km) of the threshold.
------------------------------------------------------------------------
3.d....................  For runways: Visual Approach Aid lights (VASI
                          or PAPI) from 5 sm (8 km) of the threshold.
------------------------------------------------------------------------
3.e....................  For runways: runway threshold lights and
                          touchdown zone from 2 sm (3 km).
------------------------------------------------------------------------

3.f....................  For runways and helicopter landing areas:
                          markings within range of landing lights for
                          night/twilight scenes and the surface
                          resolution test on daylight scenes, as
                          required.
------------------------------------------------------------------------
3.g....................  For circling approaches: the runway of intended
                          landing and associated lighting must fade into
                          view in a non-distracting manner.
------------------------------------------------------------------------
3.h....................  For helicopter landing areas: landing direction
                          lights and raised FATO lights from 1 sm (1.5
                          km).
------------------------------------------------------------------------
3.i....................  For helicopter landing areas: Flush mounted
                          FATO lights, TOFL lights, and the lighted
                          windsock from 0.5 sm (750 m).
------------------------------------------------------------------------
4......................  Airport or Helicopter Landing Area Model
                          Content.
                         The following prescribes the minimum
                          requirements for an airport/helicopter landing
                          area visual model and identifies other aspects
                          of the environment that must correspond with
                          that model for a Level 7 FTD. For circling
                          approaches, all tests apply to the runway used
                          for the initial approach and to the runway of
                          intended landing. If all runways or landing
                          areas in a visual model used to meet the
                          requirements of this attachment are not
                          designated as ``in use,'' then the ``in use''
                          runways/landing areas must be listed on the
                          Statement of Qualification (e.g., KORD, Rwys
                          9R, 14L, 22R). Models of airports or
                          helicopter landing areas with more than one
                          runway or landing area must have all
                          significant runways or landing areas not ``in-
                          use'' visually depicted for airport/runway/
                          landing area recognition purposes. The use of
                          white or off white light strings that identify
                          the runway or landing area for twilight and
                          night scenes are acceptable for this
                          requirement; and rectangular surface
                          depictions are acceptable for daylight scenes.
                          A visual system's capabilities must be
                          balanced between providing visual models with
                          an accurate representation of the airport and
                          a realistic representation of the surrounding
                          environment. Each runway or helicopter landing
                          area designated as an ``in-use'' runway or
                          area must include the following detail that is
                          either modeled using airport/heliport
                          pictures, construction drawings and maps, U.S.
                          National Imagery and Mapping Agency data other
                          appropriate data, or modeled in accordance
                          with published regulatory material.
------------------------------------------------------------------------
4.a....................  The surface and markings for each ``in-use''
                          runway or helicopter landing area must include
                          the following:
------------------------------------------------------------------------
4.a.1..................  For airports: runway threshold markings, runway
                          numbers, touchdown zone markings, fixed
                          distance markings, runway edge markings, and
                          runway centerline stripes.
------------------------------------------------------------------------
4.a.2..................  For helicopter landing areas: markings for
                          standard heliport identification (``H'') and
                          TOFL, FATO, and safety areas.
------------------------------------------------------------------------
4.b....................  The lighting for each ``in-use'' runway or
                          helicopter landing area must include the
                          following:
------------------------------------------------------------------------
4.b.1..................  For airports: runway approach, threshold, edge,
                          end, centerline (if applicable), touchdown
                          zone (if applicable), leadoff, and visual
                          landing aid lights or light systems for that
                          runway.
------------------------------------------------------------------------
4.b.2..................  For helicopter landing areas: landing
                          direction, raised and flush FATO, TOFL,
                          windsock lighting.
------------------------------------------------------------------------
4.c....................  The taxiway surface and markings associated
                          with each ``in-use'' runway or helicopter
                          landing area must include the following:
------------------------------------------------------------------------
4.c.1..................  For airports: taxiway edge, centerline (if
                          appropriate), runway hold lines, and ILS
                          critical area(s).
------------------------------------------------------------------------
4.c.2..................  For helicopter landing areas: taxiways, taxi
                          routes, and aprons.
------------------------------------------------------------------------
4.d....................  The taxiway lighting associated with each ``in-
                          use'' runway or helicopter landing area must
                          include the following:
------------------------------------------------------------------------
4.d.1..................  For airports: taxiway edge, centerline (if
                          appropriate), runway hold lines, ILS critical
                          areas.
------------------------------------------------------------------------
4.d.2..................  For helicopter landing areas: taxiways, taxi
                          routes, and aprons.
------------------------------------------------------------------------
4.d.3..................  For airports: taxiway lighting of correct
                          color.
------------------------------------------------------------------------
4.e....................  Airport signage associated with each ``in-use''
                          runway or helicopter landing area must include
                          the following:
------------------------------------------------------------------------
4.e.1..................  For airports: signs for runway distance
                          remaining, intersecting runway with taxiway,
                          and intersecting taxiway with taxiway.
------------------------------------------------------------------------
4.e.2..................  For helicopter landing areas: as may be
                          appropriate for the model used.
------------------------------------------------------------------------
4.f....................  Required visual model correlation with other
                          aspects of the airport or helicopter landing
                          environment simulation:
------------------------------------------------------------------------
4.f.1..................  The airport or helicopter landing area model
                          must be properly aligned with the navigational
                          aids that are associated with operations at
                          the ``in-use'' runway or helicopter landing
                          area.
------------------------------------------------------------------------
4.f.2..................  The simulation of runway or helicopter landing
                          area contaminants must be correlated with the
                          displayed runway surface and lighting, if
                          applicable.
------------------------------------------------------------------------
5......................  Correlation with helicopter and associated
                          equipment.
                         The following are the minimum correlation
                          comparisons that must be made for a Level 7
                          FTD.
------------------------------------------------------------------------
5.a....................  Visual system compatibility with aerodynamic
                          programming.
------------------------------------------------------------------------

5.b....................  Visual cues to assess sink rate and depth
                          perception during landings.
------------------------------------------------------------------------
5.c....................  Accurate portrayal of environment relating to
                          FTD attitudes.
------------------------------------------------------------------------
5.d....................  The visual scene must correlate with integrated
                          helicopter systems, where fitted (e.g.,
                          terrain, traffic and weather avoidance systems
                          and Head-up Guidance System (HGS)).
------------------------------------------------------------------------
5.e....................  Representative visual effects for each visible,
                          own-ship, helicopter external light(s).
------------------------------------------------------------------------
5.f....................  The effect of rain removal devices.
------------------------------------------------------------------------
6......................  Scene quality.
                         The following are the minimum scene quality
                          tests that must be conducted for a Level 7
                          FTD.
------------------------------------------------------------------------
6.a....................  System light points should be free from
                          distracting jitter, smearing or streaking.
------------------------------------------------------------------------
6.b....................  Demonstration of occulting through each channel
                          of the system in an operational scene.
------------------------------------------------------------------------
6.c....................  Six discrete light step controls (0-5).
------------------------------------------------------------------------
7......................  Special weather representations, which include
                          visibility and RVR, measured in terms of
                          distance. Visibility/RVR checked at 2,000 ft
                          (600 m) above the airport or helicopter
                          landing area and at two heights below 2,000 ft
                          with at least 500 ft of separation between the
                          measurements. The measurements must be taken
                          within a radius of 10 sm (16 km) from the
                          airport or helicopter landing area.
------------------------------------------------------------------------
7.a....................  Effects of fog on airport lighting such as
                          halos and defocus.
------------------------------------------------------------------------
7.b....................  Effect of own-ship lighting in reduced
                          visibility, such as reflected glare, including
                          landing lights, strobes, and beacons.
------------------------------------------------------------------------
8......................  Instructor control of the following:
                         The following are the minimum instructor
                          controls that must be available in a Level 7
                          FTD.
------------------------------------------------------------------------
8.a....................  Environmental effects: e.g., cloud base, cloud
                          effects, cloud density, visibility in statute
                          miles/kilometers and RVR in feet/meters.
------------------------------------------------------------------------
8.b....................  Airport or helicopter landing area selection.
------------------------------------------------------------------------
8.c....................  Airport or helicopter landing area lighting,
                          including variable intensity.
------------------------------------------------------------------------
8.d....................  Dynamic effects including ground and flight
                          traffic.
------------------------------------------------------------------------
                           End QPS Requirement
------------------------------------------------------------------------
                            Begin Information
------------------------------------------------------------------------
9......................  An example of being able to ``combine two
                          airport models to achieve two ``in-use''
                          runways: One runway designated as the ``in-
                          use'' runway in the first model of the
                          airport, and the second runway designated as
                          the ``in-use'' runway in the second model of
                          the same airport. For example, the clearance
                          is for the ILS approach to Runway 27, Circle
                          to Land on Runway 18 right. Two airport visual
                          models might be used: the first with Runway 27
                          designated as the ``in use'' runway for the
                          approach to runway 27, and the second with
                          Runway 18 Right designated as the ``in use''
                          runway. When the pilot breaks off the ILS
                          approach to runway 27, the instructor may
                          change to the second airport visual model in
                          which runway 18 Right is designated as the
                          ``in use'' runway, and the pilot would make a
                          visual approach and landing. This process is
                          acceptable to the FAA as long as the temporary
                          interruption due to the visual model change is
                          not distracting to the pilot.
------------------------------------------------------------------------
10.....................  Sponsors are not required to provide every
                          detail of a runway, but the detail that is
                          provided should be correct within reasonable
                          limits.
------------------------------------------------------------------------
                             End Information
------------------------------------------------------------------------

     Table D3C.--Table of Functions and Subjective Tests Level 7 FTD
------------------------------------------------------------------------
                         <<>>
-------------------------------------------------------------------------
                           Visual scene content requirements additional
         Number             visual models beyond minimum required for
                                          qualification
------------------------------------------------------------------------
This table specifies the minimum airport or helicopter landing area
 visual model content and functionality necessary to add visual models
 to an FTD's visual model library (i.e., beyond those necessary for
 qualification at the stated level) without the necessity of further
 involvement of the NSPM or TPAA.
------------------------------------------------------------------------
1......................  Visual scene management.
                         The following is the minimum visual scene
                          management requirements.
------------------------------------------------------------------------

1.a....................  The installation and direction of the following
                          lights must be replicated for the ``in-use''
                          surface:
------------------------------------------------------------------------
1.a.1..................  For ``in-use'' runways: strobe lights, approach
                          lights, runway edge lights, visual landing
                          aids, runway centerline lights, threshold
                          lights, and touchdown zone lights.
------------------------------------------------------------------------
1.a.2..................  For ``in-use'' helicopter landing areas: ground
                          level TLOF perimeter lights, elevated TLOF
                          perimeter lights (if applicable), Optional
                          TLOF lights (if applicable), ground FATO
                          perimeter lights, elevated TLOF lights (if
                          applicable), landing direction lights.
------------------------------------------------------------------------
2......................  Visual feature recognition.
                         The following are the minimum distances at
                          which runway or landing area features must be
                          visible. Distances are measured from runway
                          threshold or a helicopter landing area to an
                          aircraft aligned with the runway or helicopter
                          landing area on a 3[deg] glide-slope from the
                          aircraft to the touchdown point, in simulated
                          meteorological conditions. For circling
                          approaches, all tests apply to the runway used
                          for the initial approach and to the runway of
                          intended landing.
------------------------------------------------------------------------
2.a....................  For Runways.
------------------------------------------------------------------------
2.a.1..................  Strobe lights, approach lights, and edge lights
                          from 5 sm (8 km) of the threshold.
------------------------------------------------------------------------
2.a.2..................  Centerline lights and taxiway definition from 3
                          sm (5 km).
------------------------------------------------------------------------
2.a.3..................  Visual Approach Aid lights (VASI or PAPI) from
                          3 sm (5 km) of the threshold.
------------------------------------------------------------------------
2.a.4..................  Visual Approach Aid lights (VASI or PAPI) from
                          5 sm (8 km) of the threshold.
------------------------------------------------------------------------
2.a.5..................  Threshold lights and touchdown zone lights from
                          2 sm (3 km).
------------------------------------------------------------------------
2.a.6..................  Markings within range of landing lights for
                          night/twilight (dusk) scenes and as required
                          by the surface resolution test on daylight
                          scenes.
------------------------------------------------------------------------
2.a.7..................  For circling approaches, the runway of intended
                          landing and associated lighting must fade into
                          view in a non-distracting manner.
------------------------------------------------------------------------
2.b....................  For Helicopter landing areas.
------------------------------------------------------------------------
2.b.1..................  Landing direction lights and raised FATO lights
                          from 2 sm (3 km).
------------------------------------------------------------------------
2.b.2..................  Flush mounted FATO lights, TOFL lights, and the
                          lighted windsock from 1 sm (1500 m).
------------------------------------------------------------------------
2.b.3..................  Hover taxiway lighting (yellow/blue/yellow
                          cylinders) from TOFL area.
------------------------------------------------------------------------
2.b.4..................  Markings within range of landing lights for
                          night/twilight (dusk) scenes and as required
                          by the surface resolution test on daylight
                          scenes.
------------------------------------------------------------------------
3......................  Airport or Helicopter Landing Area Model
                          Content.
                         The following prescribes the minimum
                          requirements for what must be provided in an
                          airport visual model and identifies other
                          aspects of the airport environment that must
                          correspond with that model. The detail must be
                          modeled using airport pictures, construction
                          drawings and maps, U.S. National Imagery and
                          Mapping Agency data or other data, or modeled
                          in accordance with published regulatory
                          material; however, this does not require that
                          airport or helicopter landing area models
                          contain details that are beyond the designed
                          capability of the currently qualified visual
                          system. For circling approaches, all
                          requirements of this section apply to the
                          runway used for the initial approach and to
                          the runway of intended landing.
------------------------------------------------------------------------
3.a....................  The surface and markings for each ``in-use''
                          runway or helicopter landing area must include
                          the following:
------------------------------------------------------------------------
3.a.1..................  For airports: runway threshold markings, runway
                          numbers, touchdown zone markings, fixed
                          distance markings, runway edge markings, and
                          runway centerline stripes.
------------------------------------------------------------------------
3.a.2..................  For helicopter landing areas: Standard heliport
                          marking (``H''), TOFL, FATO, and safety areas.
------------------------------------------------------------------------
3.b....................  The lighting for each ``in-use'' runway or
                          helicopter landing area must include the
                          following:
------------------------------------------------------------------------
3.b.1..................  For airports: runway approach, threshold, edge,
                          end, centerline (if applicable), touchdown
                          zone (if applicable), leadoff, and visual
                          landing aid lights or light systems for that
                          runway.
------------------------------------------------------------------------
3.b.2..................  For helicopter landing areas: landing
                          direction, raised and flush FATO, TOFL,
                          windsock lighting.
------------------------------------------------------------------------
3.c....................  The taxiway surface and markings associated
                          with each ``in-use'' runway or helicopter
                          landing area must include the following:
------------------------------------------------------------------------
3.c.1..................  For airports: taxiway edge, centerline (if
                          appropriate), runway hold lines, and ILS
                          critical area(s),
------------------------------------------------------------------------
3.c.2..................  For helicopter landing areas: taxiways, taxi
                          routes, and aprons.
------------------------------------------------------------------------
3.d....................  The taxiway lighting associated with each ``in-
                          use'' runway or helicopter landing area must
                          include the following:
------------------------------------------------------------------------

3.d.1..................  For airports: runway edge, centerline (if
                          appropriate), runway hold lines, ILS critical
                          areas.
------------------------------------------------------------------------
3.d.2..................  For helicopter landing areas: taxiways, taxi
                          routes, and aprons.
------------------------------------------------------------------------
4......................  Required visual model correlation with other
                          aspects of the airport environment simulation.
                         The following are the minimum visual model
                          correlation tests that must be conducted for
                          Level 7 FTD.
------------------------------------------------------------------------
4.a....................  The airport model must be properly aligned with
                          the navigational aids that are associated with
                          operations at the ``in-use'' runway.
------------------------------------------------------------------------
4.b....................  Slopes in runways, taxiways, and ramp areas
                          must not cause distracting or unrealistic
                          effects.
------------------------------------------------------------------------
5......................  Correlation with helicopter and associated
                          equipment.
                         The following are the minimum correlation
                          comparisons that must be made.
------------------------------------------------------------------------
5.a....................  Visual system compatibility with aerodynamic
                          programming.
------------------------------------------------------------------------
5.b....................  Accurate portrayal of environment relating to
                          flight simulator attitudes.
------------------------------------------------------------------------
5.c....................  Visual cues to assess sink rate and depth
                          perception during landings.
------------------------------------------------------------------------
6......................  Scene quality.
                         The following are the minimum scene quality
                          tests that must be conducted.
------------------------------------------------------------------------
6.a....................  Light points free from distracting jitter,
                          smearing or streaking.
------------------------------------------------------------------------
6.b....................  Surfaces and textural cues free from apparent
                          quantization (aliasing).
------------------------------------------------------------------------
7......................  Instructor controls of the following.
                         The following are the minimum instructor
                          controls that must be available.
------------------------------------------------------------------------
7.a....................  Environmental effects, e.g., cloud base (if
                          used), cloud effects, cloud density,
                          visibility in statute miles/kilometers and RVR
                          in feet/meters.
------------------------------------------------------------------------
7.b....................  Airport/Heliport selection.
------------------------------------------------------------------------
7.c....................  Airport/Heliport lighting including variable
                          intensity.
------------------------------------------------------------------------
7.d....................  Dynamic effects including ground and flight
                          traffic.
------------------------------------------------------------------------
                          End QPS Requirements
------------------------------------------------------------------------
                            Begin Information
------------------------------------------------------------------------
8......................  Sponsors are not required to provide every
                          detail of a runway or helicopter landing area,
                          but the detail that is provided must be
                          correct within the capabilities of the system.
------------------------------------------------------------------------
                             End Information
------------------------------------------------------------------------

     Table D3D.--Table of Functions and Subjective Tests Level 6 FTD
------------------------------------------------------------------------
                         <<>>
-------------------------------------------------------------------------
         Number                          Operations tasks
------------------------------------------------------------------------
Tasks in this table are subject to evaluation if appropriate for the
 helicopter simulated as indicated in the SOQ Configuration List or for
 a Level 6 FTD. Items not installed or not functional on the FTD and not
 appearing on the SOQ Configuration List, are not required to be listed
 as exceptions on the SOQ.
------------------------------------------------------------------------
1. Preflight Procedures
------------------------------------------------------------------------
1.a....................  Preflight Inspection (Flight Deck Only)
                          switches, indicators, systems, and equipment.
------------------------------------------------------------------------
1.b....................  APU/Engine start and run-up.
------------------------------------------------------------------------
1.b.1..................     Normal start procedures.
------------------------------------------------------------------------
1.b.2..................     Alternate start procedures.
------------------------------------------------------------------------
1.b.3..................     Abnormal starts and shutdowns.
------------------------------------------------------------------------

1.b.4..................     Rotor engagement.
------------------------------------------------------------------------
1.b.5..................     System checks.
------------------------------------------------------------------------
2. Takeoff and Departure Phase
------------------------------------------------------------------------
2.a....................  Instrument.
------------------------------------------------------------------------
2.b....................  Takeoff with engine failure after critical
                          decision point (CDP).
------------------------------------------------------------------------
3. Climb
------------------------------------------------------------------------
3.a....................  Normal.
------------------------------------------------------------------------
3.b....................  One engine inoperative.
------------------------------------------------------------------------
4. Inflight Maneuvers
------------------------------------------------------------------------
4.a....................  Performance.
------------------------------------------------------------------------
4.b....................  Flying qualities.
------------------------------------------------------------------------
4.c....................  Turns.
------------------------------------------------------------------------
4.c.1..................     Timed.
------------------------------------------------------------------------
4.c.2..................     Normal.
------------------------------------------------------------------------
4.c.3..................     Steep.
------------------------------------------------------------------------
4.d....................  Accelerations and decelerations.
------------------------------------------------------------------------
4.e....................  Abnormal/emergency procedures:
------------------------------------------------------------------------
4.e.1..................     Engine fire.
------------------------------------------------------------------------
4.e.2..................     Engine failure.
------------------------------------------------------------------------
4.e.3..................     In-flight engine shutdown (and restart, if
                             applicable).
------------------------------------------------------------------------
4.e.4..................     Fuel governing system failures (e.g., FADEC
                             malfunction).
------------------------------------------------------------------------
4.e.5..................     Directional control malfunction (restricted
                             to the extent that the maneuver may not
                             terminate in a landing).
------------------------------------------------------------------------
4.e.6..................     Hydraulic failure.
------------------------------------------------------------------------
4.e.7..................     Stability augmentation system failure.
------------------------------------------------------------------------
5. Instrument Procedures
------------------------------------------------------------------------
5.a....................  Holding.
------------------------------------------------------------------------
5.b....................  Precision Instrument Approach.
------------------------------------------------------------------------
5.b.1..................     All engines operating.
------------------------------------------------------------------------
5.b.2..................     One or more engines inoperative.
------------------------------------------------------------------------
5.b.3..................     Approach procedures:
------------------------------------------------------------------------
5.b.4..................     PAR.
------------------------------------------------------------------------
5.b.5..................     ILS.
------------------------------------------------------------------------
5.b.6..................     Manual (raw data).
------------------------------------------------------------------------
5.b.7..................     Flight director only.
------------------------------------------------------------------------
5.b.8..................     Autopilot* and flight director (if
                             appropriate) coupled.
------------------------------------------------------------------------
5.c....................  Non-precision Instrument Approach.
------------------------------------------------------------------------

5.c....................     Normal--All engines operating.
------------------------------------------------------------------------
5.c....................     One or more engines inoperative.
------------------------------------------------------------------------
5.c....................     Approach procedures:
------------------------------------------------------------------------
5.c.1..................       NDB.
------------------------------------------------------------------------
5.c.2..................       VOR, RNAV, TACAN, GPS.
------------------------------------------------------------------------
5.c.3..................       ASR.
------------------------------------------------------------------------
5.c.4..................       Helicopter only.
------------------------------------------------------------------------
5.d....................  Missed Approach.
------------------------------------------------------------------------
5.d.1..................     All engines operating.
------------------------------------------------------------------------
5.d.2..................     One or more engines inoperative.
------------------------------------------------------------------------
5.d.3..................     Stability augmentation system failure.
------------------------------------------------------------------------
6. Normal and Abnormal Procedures (any phase of flight)
------------------------------------------------------------------------
6.a....................  Helicopter and powerplant systems operation (as
                          applicable).
------------------------------------------------------------------------
6.a.1..................     Anti-icing/deicing systems.
------------------------------------------------------------------------
6.a.2..................     Auxiliary power-plant.
------------------------------------------------------------------------
6.a.3..................     Communications.
------------------------------------------------------------------------
6.a.4..................     Electrical system.
------------------------------------------------------------------------
6.a.5..................     Environmental system.
------------------------------------------------------------------------
6.a.6..................     Fire detection and suppression.
------------------------------------------------------------------------
6.a.7..................     Flight control system.
------------------------------------------------------------------------
6.a.8..................     Fuel system.
------------------------------------------------------------------------
6.a.9..................     Engine oil system.
------------------------------------------------------------------------
6.a.10.................     Hydraulic system.
------------------------------------------------------------------------
6.a.11.................     Landing gear.
------------------------------------------------------------------------
6.a.12.................     Oxygen.
------------------------------------------------------------------------
6.a.13.................     Pneumatic.
------------------------------------------------------------------------
6.a.14.................     Powerplant.
------------------------------------------------------------------------