[Federal Register: September 15, 2008 (Volume 73, Number 179)]
[Rules and Regulations]
[Page 53105-53113]
[DOCID:fr15se08-1]

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Rules and Regulations
                                                Federal Register
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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-0052; Directorate Identifier 2008-NE-01-AD;
Amendment 39-15672; AD 2008-19-05]
RIN 2120-AA64

Airworthiness Directives; Engine Components, Inc. (ECi)
Reciprocating Engine Cylinder Assemblies

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
Lycoming Engines (formerly Textron Lycoming) models 320, 360, and 540
series, ``Parallel Valve'' reciprocating engines, with certain Engine
Components, Inc. (ECi) cylinder assemblies, part number (P/N) AEL65102
series ``Titan'', installed. This AD requires initial and repetitive
visual inspections and compression tests to detect cracks at the head-
to-barrel interface, replacement of cylinder assemblies found cracked,
and replacement of certain cylinder assemblies, at new reduced times-
in-service. This AD results from reports of 45 failures with head
separations of ECi cylinder assemblies. We are issuing this AD to
prevent loss of engine power due to cracks at the head-to-barrel
interface in the cylinder assemblies and possible engine failure caused
by separation of a cylinder head, which could result in loss of control
of the aircraft.

DATES: This AD becomes effective October 20, 2008.

ADDRESSES: You can get the service information identified in this AD
from Engine Components, Inc., 9503 Middlex, San Antonio, TX 78217;
Phone<PHONE_NUMBER>; fax<PHONE_NUMBER>; http://www.eci2fly.com.
    The Docket Operations office is located at Docket Management
Facility, U.S. Department of Transportation, 1200 New Jersey Avenue,
SE., West Building Ground Floor, Room W12-140, Washington, DC 20590-
0001.

FOR FURTHER INFORMATION CONTACT: Peter W. Hakala, Aerospace Engineer,
Special Certification Office, FAA, Rotorcraft Directorate, 2601 Meacham
Blvd., Fort Worth, TX 76193; e-mail<EMAIL_ADDRESS>telephone
(817) 222-5145; fax<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39
with a proposed AD. The proposed AD applies to Lycoming Engines
(formerly Textron Lycoming) models 320, 360, and 540 series, ``Parallel
Valve'' reciprocating engines, with certain Engine Components Inc.
(ECi) cylinder assemblies, part number (P/N) AEL65102 series ``Titan'',
installed. We published the proposed AD in the Federal Register on May
19, 2008 (73 FR 28756). That action proposed to require initial and
repetitive visual inspections and compression tests to detect cracks at
the head-to-barrel interface, replacement of cylinder assemblies found
cracked, and replacement of certain cylinder assemblies, at new reduced
times-in-service.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://
www.regulations.gov; or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Operations office (telephone<PHONE_NUMBER>) is provided in
the ADDRESSES section. Comments will be available in the AD docket
shortly after receipt.

Comments

    We provided the public the opportunity to participate in the
development of this AD. We have considered the comments received.

Request To Reduce the Economic Impact

    One commenter, the Aircraft Owners and Pilots Association, states
that the 50-hour inspection interval should be increased to 100 hours,
to reduce the economic impact of the cylinder assembly inspections.
Another commenter, a private citizen, states that the cost of the 50-
hour inspections was not considered in the NPRM economic estimate.
    We do not agree. We selected the 50-hour inspection interval so
that aluminum cylinder cracks could be detected before a head
separation occurred. By removing leaking cylinder heads discovered
during the periodic 50-hour inspections, the probability of having an
in flight head separation is greatly reduced. Also, the 50-hour
inspection interval coincides with the scheduled maintenance for normal
engine oil and filter changes. Also, the costs of compliance in the
NPRM did include costs for the additional cylinder assembly
inspections. We did not change the AD.

Retiring Cylinder Assemblies at Time-Between-Overhaul Is Too Expensive

    One commenter, a private citizen, states that it is too expensive
to retire all the subject cylinder assemblies at the normal overhaul
time. Another commenter, a private citizen, states that it is
unreasonable for general aviation airplane owners, in Part 91 use, to
be required to retire cylinder assemblies at the time-between-overhaul
or at normal engine overhaul time.
    We do not agree. The subject cylinder assemblies can be safely run
to the normal TBO with the required 50-hour inspections, with
compression tests. Because of metallurgical analysis results of the
fatigue cracks in the aluminum alloy cylinder heads, and also the
history of the head separation hours-in-service, the probability of a
head separation is greater with the subject cylinder assemblies running
past the time-between-overhaul time. Therefore, we do not consider the
cylinder assemblies to be airworthy past the normal engine overhaul
time. We did not change the AD.

Cylinder Assembly Serial Number Range Is Different in the ECi Mandatory
Service Bulletin

    One commenter, ECi., states that the cylinder assembly serial
number range in the proposed AD for the Group ``B'' cylinders is
slightly different from the serial numbers listed in the ECi Mandatory
service Bulletin No. 08-1. The commenter states that several additional
cylinder serial numbers should be included in Group ``B''.
    We do not agree. We researched the cylinder assembly serial numbers
in the proposed AD and they are correct. The Group ``A'' cylinder
assemblies go up to serial number 35171-22. The Group ``B'' cylinder
assemblies start at serial number 35239-01. We discussed the serial
number comment with ECi. They agree that the serial number range in the
proposed AD is correct. ECi states that they have revised the serial
numbers in ECi. Mandatory Service Bulletin (MSB) No. 08-1 to match the
serial numbers in the AD, and issued MSB No. 08-1, Revision 3, dated
August 19, 2008. We now reference this MSB Revision 3 in the AD.

Conclusion

    We have carefully reviewed the available data, including the
comments received, and determined that air safety and the public
interest require adopting the AD as proposed. We have determined that
these changes will neither increase the economic burden on any operator
nor increase the scope of the AD.

Costs of Compliance

    We estimate that this AD will affect 13,000 ECi cylinder assemblies
installed in aircraft of U.S. registry. The visual inspection and
compression tests will take about 4 work-hours for each engine. An
individual cylinder replacement will require $1,100 for parts and 6
work-hours. Lycoming engines with a set of 4 ECi cylinders will require
12 work-hours for the cylinder replacement. Lycoming engines with a set
of 6 ECi cylinders will require 16 work-hours for the cylinder
replacement. We estimate 18 percent of the affected population of
cylinders will be replaced. We estimate the total cost of the AD to
U.S. operators to be $7,952,000. Our estimate is exclusive of any
possible warranty coverage.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, Section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more detail the scope of the Agency's authority.
    We are issuing this rulemaking under the authority described in
subtitle VII, part A, subpart III, section 44701, ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.

Regulatory Findings

    We have determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the national government and the States, or on the distribution of power
and responsibilities among the various levels of government.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive
Order 12866;
    (2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and
    (3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
    We prepared a summary of the costs to comply with this AD and
placed it in the AD Docket. You may get a copy of this summary at the
address listed under ADDRESSES.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Safety.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator,
the Federal Aviation Administration amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness
directive:

2008-19-05 Engine Components, Inc. (ECi): Amendment 39-15672. Docket
No. FAA-2008-0052; Directorate Identifier 2008-NE-01-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective October
20, 2008.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to the Lycoming Engines (formerly Textron
Lycoming) models 320, 360, and 540 series, ``Parallel Valve'',
reciprocating engines listed in Table 1 of this AD, with ECi
cylinder assembly, part number (P/N) AEL65102 series ``Titan'', and
with cylinder head, P/N AEL85099, installed.
    (1) The applicable cylinder assembly serial numbers (SNs) are SN
1138-02 through SN 35171-22, (referred to in this AD as Group ``A''
cylinder assemblies); and
    (2) SN 35239-01 through SN 37016-28 (referred to in this AD as
Group ``B'' cylinder assemblies).
    (3) Note that the cylinder assembly P/N is at the crankcase end
of the cylinder assembly, and might be difficult to see. As a guide
in determining if your cylinder assemblies are affected, all
affected cylinder assemblies have cylinder head P/N AEL85099. The
cylinder head P/N is at the top of the cylinder head, near the
intake and exhaust valve springs, and is easier to locate than the
cylinder assembly P/N.
    (4) Note that the set of numbers appearing on the cylinder,
above and to the left of the SN, in the form of ``123456'' is not
used for determining applicability.

                         Table 1--Engine Models
------------------------------------------------------------------------
 Cylinder assembly part No.:          Installed on engine models:
------------------------------------------------------------------------
AEL65102-NST04...............  O-320-A1B, A2B, A2C, A2D, A3A, A3B, B2B,
                                B2C, B2D, B2E, B3B, B3C, C2B, C2C, C3B,
                                C3C, D1A, D1AD, D1B, D1C, D1D, D1F, D2A,
                                D2B, D2C, D2F, D2G, D2H, D2J, D3G, E1A,
                                E1B, E1C, E1F, E1J, E2A, E2B, E2C, E2D,
                                E2E, E2F, E2G, E2H, E3D, E3H
                               IO-320-A1A, A2A, B1A, B1B, B1C, B1D, B1E,
                                B2A, D1A, D1AD, D1B, D1C, E1A, E1B, E2A,
                                E2B
                               AEIO-320-D1B, D2B, E1A, E1B, E2A, E2B
                               AIO-320-A1A, A1B, A2A, A2B, B1B, C1B

                               LIO-320-B1A
------------------------------------------------------------------------
AEL65102-NST05...............  IO-320-C1A, C1B, C1F, F1A
                               LIO-320-C1A
------------------------------------------------------------------------
AEL65102-NST06...............  O-320-A1A, A2A, A2B, A2C, A3A, A3B, A3C,
                                E1A, E1B, E2A, E2C, (also, an O-320
                                model with no suffix)
                               IO-320-A1A, A2A
------------------------------------------------------------------------
AEL65102-NST07...............  IO-320-B1A, B1B
                               LIO-320-B1A
------------------------------------------------------------------------
AEL65102-NST08...............  O-320-B1A, B1B, B2A, B2B, B3A, B3B, B3C,
                                C1A, C1B, C2A, C2B, C3A, C3B, C3C, D1A,
                                D1B, D2A, D2B, D2C
------------------------------------------------------------------------
AEL65102-NST10...............  O-360-A1A, A1C, A1D, A2A, A2E, A3A, A3D,
                                A4A, B1A, B1B, B2A, B2B, C1A, C1C, C1G,
                                C2A, C2B, C2C, C2D, D1A, D2A, D2B
                               IO-360-B1A, B1B, B1C
                               HO-360-A1A, B1A, B1B
                               HIO-360-B1A, B1B
                               AEIO-360-B1B
                               O-540-A1A, A1A5, A1B5, A1C5, A1D, A1D5,
                                A2B, A3D5, A4A5, A4B5, A4C5, A4D5, B1A5,
                                B1B5, B1D5, B2A5, B2B5, B2C5, B2C5D,
                                B4A5, B4B5, B4B5D, D1A5, E1A, E4A5,
                                E4B5, E4C5, F1A5, F1B5, G1A5, G2A5
                               IO-540-C1B5, C1C5, C2C, C4B5, C4B5D,
                                C4C5, D4A5, D4B5, N1A5, N1A5D
------------------------------------------------------------------------
AEL65102-NST12...............  O-360-A1A, A1AD, A1D, A1F, A1F6, A1F6D,
                                A1G, A1G6, A1G6D, A1H, A1H6, A1J, A1LD,
                                A1P, A2A, A2D, A2F, A2G, A2H, A3A, A3AD,
                                A3D, A4A, A4AD, A4D, A4G, A4J, A4JD,
                                A4K, A4M, A4N, A4P, A5AD, B1A, B2C, C1A,
                                C1C, C1E, C1F, C1G, C2A, C2B, C2C, C2D,
                                C2E, C4F, C4P, D2A, F1A6, G1A6
                               HO-360-C1A
                               LO-360-A1G6D, A1H6
                               HIO-360-B1A, B1B, G1A
                               LTO-360-A1A6D
                               TO-360-A1A6D
                               IO-360-B1B, B1BD, B1D, B1E, B1F, B1F6,
                                B1G6, B2E, B2F, B2F6, B4A, E1A, L2A,
                                M1A, M1B
                               AEIO-360-B1B, B1D, B1E, B1F, B1F6, B1G6,
                                B1H, B2F, B2F6, B4A, H1A, H1B
                               O-540-A4D5, B2B5, B2C5, B2C5D, B4B5,
                                B4B5D, E4A5, E4B5, E4B5D, E4C5, G1A5,
                                G1A5D, G2A5, H1A5, H1A5D, H1B5, H1B5D,
                                H2A5, H2A5D, H2B5D
                               IO-540-C4B5, C4B5D, C4D5, C4D5D, D4A5,
                                D4B5, D4C5, N1A5, N1A5D, T4A5D, T4B5,
                                T4B5D, T4C5D, V4A5, V4A5D
                               AEIO-540-D4A5, D4B5, D4C5, D4D5
------------------------------------------------------------------------
AEL65102-NST26...............  IO-540-J4A5, R1A5
                               TIO-540-C1A, E1A, G1A, H1A
------------------------------------------------------------------------
AEL65102-NST38...............  IO-360-F1A
                               TIO-540-AA1AD, AB1AD, AB1BD, AF1A, AG1A,
                                AK1A, C1A, C1AD, K1AD
                               LTIO-540-K1AD
------------------------------------------------------------------------
AEL65102-NST43...............  O-360-J2A
                               O-540-F1B5, J1A5D, J1B5D, J1C5D, J1D5D,
                                J2A5D, J2B5D, J2C5D, J2D5D, J3A5, J3A5D,
                                J3C5D
                               IO-540-AB1A5, W1A5, W1A5D, W3A5D
------------------------------------------------------------------------
AEL65102-NST44...............  O-540-L3C5D
------------------------------------------------------------------------

    For information, the Lycoming Engines (formerly Textron
Lycoming) models 320, 360, and 540 series, ``Parallel Valve'',
reciprocating engines are installed on, but not limited to, the
aircraft listed in the following Table 2:

            Table 2--Engines Installed On, But Not Limited To
------------------------------------------------------------------------
        Engine models:             Installed on, but not limited to:
------------------------------------------------------------------------
O-320-A1A....................  Piper Aircraft: Tri-Pacer (PA-22 ``150'',
                                PA-22S ``150''), Apache (PA-23), Pawnee
                                (PA-25).
                               Doyn Aircraft: Doyn-Cessna (170, 170A,
                                170B).
                               Mooney Aircraft: Mark (20A).
                               Dinfia: Ranquel (1A-46).
                               Simmering-Graz Pauker: Flamingo (SGP-M-
                                222).
                               Aviamilano: Scricciolo (P-19).
                               Vos Helicopter Co.: Spring Bok.
O-320-A1B....................  Piper Aircraft: Tri-Pacer (PA-22 ``150'',
                                PA-22S ``150''), Apache (PA-23).
                               Doyn Aircraft: Doyn-Cessna (170, 170A,
                                170B).
                               S.O.C.A.T.A.: Horizon (Gardan).

O-320-A2A....................  Piper Aircraft: Tri-Pacer (PA-22 ``150'',
                                PA-22S ``150''), Agriculture (PA-18A
                                ``150'') Super Cub (PA-18 ``150''),
                                Caribbean (PA-22 ``150''), Pawnee (PA-
                                25).
                               Intermountain Mfg. Co.: Call Air Texas (A-
                                5, A-5T).
                               Lake Aircraft: Colonial (C-1).
                               Rawdon Bros.: Rawdon (T-1, T-15, T-15D).
                               Shinn Engineering: Shinn (2150-A).
                               Dinfia: Ranquel ((1A)46).
                               Neiva: (1PD-5802).
                               Sud: Gardan-Horizon (GY-80).
                               LaVerda: Falco (F8L Series II, America).
                               Malmo: Vipan (MF1-10).
                               Kingsford Smith: Autocrat (SCRM-153).
                               Aero Commander: 100.
O-320-A2B....................  Piper Aircraft: Tri-Pacer (PA-22 ``150'',
                                PA-22S ``150''), Cherokee (PA-28
                                ``150''), Super Cub (PA-18 ``150'').
                               Champion Aircraft: Challenger (7GCA,
                                7GCB, 7KC), Citabria (7GCAA, 7GCRC),
                                Agriculture (7GCBA).
                               Beagle: Pup (150).
                               Artic: Interstate S1B2.
                               Robinson: R-22.
                               Varga: Kachina 2150A.
O-320-A2C....................  Robinson: R-22.
                               Cicare: Cicare AG.
                               Bellanca Aircraft: Citabria 150 (7GCAA),
                                Citabria 150S (7GCBC).
O-320-A2D....................  Piper Aircraft: Apache (PA-23).
O-320-A3A....................  Doyn Aircraft: Doyn-Cessna (170, 170A,
                                170B).
                               Corben-Fettes: Globe Special (Globe GC-
                                1B).
O-320-A3B....................  Piper Aircraft: Apache (PA-23).
                               Doyn Aircraft: Doyn-Cessna (170, 170A,
                                170B).
                               Teal II: TSC (1A2).
O-320-B1A....................  Piper Aircraft: Apache (PA-23 ``160'').
                               Doyn Aircraft: Doyn-Cessna (170, 170A,
                                170B).
                               Malmo: Vipan (MF1-10).
O-320-B1B....................  Piper Aircraft: Apache (PA-23 ``160'').
                               Doyn Aircraft: Doyn-Cessna (170, 170A,
                                170B).
O-320-B2A....................  Piper Aircraft: Tri-Pacer (PA-22 ``160'',
                                PA-22S ``160'').
O-320-B2B....................  Piper Aircraft: Tri-Pacer (PA-22 ``160'',
                                PA-22S ``160'').
                               Beagle: Airedale (D5-160).
                               Fuji-Heavy Industries: Fuji (F-200).
                               Uirapuru: Aerotec 122.
O-320-B2C....................  Robinson: R-22.
O-320-B2D....................  Maule: MX-7-160.
O-320-B2E....................  Lycon.
O-320-B3A....................  Piper Aircraft: Apache (PA-23 ``160'').
                               Doyn Aircraft: Doyn-Cessna (170, 170A,
                                170B).
O-320-B3B....................  Piper Aircraft: Apache (PA-23 ``160'').
                               Doyn Aircraft: Doyn-Cessna (170, 170A,
                                170B).
                               Sud: Gardan (GY80-160).
O-320-C1A....................  Piper Aircraft: Apache (PA-23 ``160'').
                               Riley Aircraft: Rayjay (Apache).
O-320-C1B....................  Piper Aircraft: Apache (PA-23 ``160'').
O-320-C3A....................  Piper Aircraft: Apache (PA-23 ``160'').
O-320-C3B....................  Piper Aircraft: Apache (PA-23 ``160'').
O-320-D1A....................  Sud: Gardan (GY-80).
                               Gyroflug: Speed Cancard.
                               Grob: G115.
O-320-D1F....................  Slingsby: T67 Firefly.
O-320-D2A....................  Piper Aircraft: Cherokee (PA-28S
                                ``160'').
                               Robin: Major (DR400-140B), Chevalier (DR-
                                360), (R-3140).
                               S.O.C.A.T.A.: Tampico TB9.
                               Slingsby: T67C Firefly.
                               Daetwyler: MD-3-160.
                               Nash Aircraft Ltd.: Petrel.
                               Aviolight: P66D Delta.
                               General Avia: Pinguino.
O-320-D2B....................  Beech Aircraft: Musketeer (M-23).
                               Piper Aircraft: Cherokee (PA-28 ``160'').
O-320-D2J....................  Cessna Aircraft: Skyhawk 172.
O-320-D3G....................  Piper Aircraft: Warrior II, Cadet (PA-28-
                                161).
O-320-E1A....................  Grob: G115.
O-320-E1C....................  M.B.B. (Messerschmitt-Boelkow-Blohm):
                                Monsun (BO-209-B).
O-320-E1F....................  M.B.B.: Monsun (BO-209-B).
O-320-E2A....................  Piper Aircraft: Cherokee (PA-28 ``140'',
                                PA-28 ``150'').
                               Robin: Major (DR-340), Sitar, Bagheera
                                (GY-100-135).

                               S.O.C.A.T.A.: Super Rallye (MS-886),
                                Rallye Commodore (MS-892).
                               Siai-Marchetti: (S-202).
                               F.F.A.: Bravo (AS-202/15).
                               Partenavia: Oscar (P66B), Bucker (131
                                APM).
                               Aeromot: Paulistina P-56.
                               Pezetel: Koliber 150.
O-320-E2C....................  Beech Aircraft: Musketeer III (M-23III).
                               M.B.B.: Monsun (BO-209-B).
O-320-E2D....................  Cessna Aircraft: Cardinal (172-I, 177).
O-320-E2F....................  M.B.B.: Monsun (BO-209-B), Wassmer
                                Pacific (WA-51).
O-320-E2G....................  American Aviation Corp.: Traveler.
O-320-E3D....................  Piper Aircraft: Cherokee (140).
                               Beech Aircraft: Sport.
IO-320-B2A...................  Piper Aircraft: Twin Comanche (PA-30).
IO-320-B1C...................  Hi. Shear: Wing.
IO-320-B1D...................  Ted Smith Aircraft: Aerostar.
IO-320-C1A...................  Piper Aircraft: Twin Comanche (PA-30
                                Turbo).
IO-320-D1A...................  M.B.B.: Monsun (BO-209-C).
IO-320-D1B...................  M.B.B.: Monsun (BO-209-C).
IO-320-E1A...................  M.B.B.: Monsun (BO-209-C).
IO-320-E1B...................  Bellanca Aircraft.
IO-320-E2A...................  Champion Aircraft: Citabria.
IO-320-E2B...................  Bellanca Aircraft.
IO-320-F1A...................  CAAR Engineering: Carr Midget.
LIO-320-B1A..................  Piper Aircraft: Twin Comanche (PA-39).
LIO-320-C1A..................  Piper Aircraft: Twin Comanche (PA-39).
AIO-320-B1B..................  M.B.B.: Monsun (BO-209-C).
AEIO-320-D1B.................  Slingsby: T67M Firefly.
AEIO-320-D2B.................  Hundustan Aeronautics Ltd.: HT-2.
AEIO-320-E1A.................  Bellanca Aircraft.
                               Champion Aircraft.
AEIO-320-E1B.................  Bellanca Aircraft.
                               Champion Aircraft: Decathalon (8KCAB-CS).
AEIO-320-E2B.................  Bellanca Aircraft.
                               Champion Aircraft: Decathalon (8KCAB).
O-320-A1A....................  Riley Aircraft: Riley Twin.
O-360-A1A....................  Beech Aircraft: Travel Air (95, B-95).
                               Piper Aircraft: Comanche (PA-24).
                               Intermountain Mfg. Co.: Call Air (A-6).
                               Lake Aircraft: Colonial (C-2, LA-4, 4A or
                                4P).
                               Doyn Aircraft: Doyn-Cessna (170B, 172,
                                172A, 172B).
                               Mooney Aircraft: Mark ``20B'' (M-20B).
                               Earl Horton: Pawnee (Piper PA-25).
                               Dinfia: Ranquel (1A-51).
                               Neiva: (1PD-5901).
                               Regente: (N-591).
                               Wassmer: Super 4 (WA-50A), Sancy (WA-40),
                                Baladou (WA-40), Pariou (WA-40).
                               Sud: Gardan (GY-180).
                               Bolkow: (207).
                               Partenavia: Oscar (P-66).
                               Siai-Marchetti: (S-205).
                               Procaer: Picchio (F-15-A).
                               S.A.A.B.: Safir (91-D).
                               Malmo: Vipan (MF-10B).
                               Aero Boero: AB-180.
                               Beagle: Airedale (A-109).
                               DeHavilland: Drover (DHA-3MK3).
                               Kingsford-Smith: Bushmaster (J5-6).
                               Aero Engine Service Ltd.: Victa (R-2).
O-360-A1AD...................  S.O.C.A.T.A.: Tabago TB-10.
O-360-A1D....................  Piper Aircraft: Comanche (PA-24).
                               Lake Aircraft: Colonial (LA-4, 4A or 4P).
                               Doyn Aircraft: Doyn-Beech (Beech 95).
                               Mooney Aircraft: Master ``21'' (M-20E),
                                Mark ``20B'', ``20D'', (M20B, M20C),
                                Mooney Statesman (M-20G).
                               Dinfia: Querandi (1A-45).
                               Wassmer: (WA-50).
                               Malmo: Vipan (MF1-10).
                               Cessna Aircraft: Skyhawk.
                               Doyn Aircraft: Doyn-Piper (PA-23
                                ``160'').
O-360-A1F6...................  Cessna Aircraft: Cardinal.
O-360-A1F6D..................  Cessna Aircraft: Cardinal 177.
                               Teal III: TSC (1A3).

O-360-A1G6...................  Aero Commander.
O-360-A1G6D..................  Beech Aircraft: Duchess 76.
O-360-A1H6...................  Piper Aircraft: Seminole (PA-44).
O-360-A1LD...................  Wassmer: Europa WA-52.
O-360-A1P....................  Aviat: Husky.
O-360-A2A....................  Center Est Aeronautique: Regente (DR-
                                253).
                               S.O.C.A.T.A.: Rallye Commodore (MS-893).
                               Societe Aeronautique Normande:
                                Mousquetaire (D-140).
                               Bolkow: Klemm (K1-107C).
                               Partenavia: Oscar (P-66).
                               Beagle: Husky (D5-180) (J1-U).
O-360-A2D....................  Piper Aircraft: Comanche (PA-24),
                                Cherokee ``C'' (PA-28 ``180'').
                               Mooney Aircraft: Master ``21'' (M-20D),
                                Mark ``21'' (M-20E).
O-360-A2E....................  Std. Helicopter.
O-360-A2F....................  Aero Commander: Lark (100).
                               Cessna Aircraft: Cardinal.
O-360-A2G....................  Beech Aircraft: Sport.
O-360-A3A....................  C.A.A.R.P.S.A.N.: (M-23III).
                               Societe Aeronautique Normande: Jodel (D-
                                140C).
                               Robin: Regent (DR400/180), Remorqueur
                                (DR400/180R). R-3170.
                               S.O.C.A.T.A.: Rallye 180GT, Sportavia
                                Sportsman (RS-180).
                               Norman Aeroplace Co.: NAC-1 Freelance.
                               Nash Aircraft Ltd.: Petrel.
O-360-A3AD...................  S.O.C.A.T.A.: TB-10.
                               Robin: Aiglon (R-1180T).
O-360-A4A....................  Piper Aircraft: Cherokee ``D'' (PA-28
                                ``180'').
O-360-A4D....................  Varga: Kachina.
O-360-A4G....................  Beech Aircraft: Musketeer Custom III.
O-360-A4K....................  Grumman American: Tiger.
                               Beech Aircraft: Sundowner 180.
O-360-A4M....................  Piper Aircraft: Archer II (PA-28 ``18'').
                               Valmet: PIK-23.
O-360-A4N....................  Cessna Aircraft: 172 (Optional).
O-360-A4P....................  Penn Yan: Super Cub Conversion.
O-360-A5AD...................  C. Itoh and Co.: Fuji FA-200.
O-360-B2C....................  Seabird Aviation: SB7L.
O-360-C1A....................  Intermountain Mfg. Co.: Call Air (A-6).
O-360-C1E....................  Bellanca Aircraft: Scout (8GCBC-CS).
O-360-C1F....................  Maule: Star Rocket MX-7-180.
O-360-C1G....................  Christen: Husky (A-1).
O-360-C2B....................  Hughes Tool Co.:HIO-360-B1A (269A).
O-360-C2D....................  Hughes Tool Co.: (269A).
O-360-C2E....................  Hughes Tool Co.: (YHO-2HU) Military.
                               Bellanca Aircraft: Scout (8GCBC FP).
O-360-C4F....................  Maule: MX-7-180A.
O-360-C4P....................  Penn Yan: Super Cub Conversion.
O-360-F1A6...................  Cessna Aircraft: Cutlass RG.
O-360-J2A....................  Robinson: R22.
IO-360-B1A...................  Beech Aircraft: Travel-Air (B-95A).
                               Doyn Aircraft: Doyn-Piper (PA-23
                                ``200'').
IO-360-B1B...................  Beech Aircraft: Travel-Air (B-95B).
                               Doyn Aircraft: Doyn-Piper (PA-23
                                ``200'').
                               Fuji: (FA-200).
IO-360-B1D...................  United Consultants: See-Bee.
IO-360-B1E...................  Piper Aircraft: Arrow (PA-28 ``180R'').
IO-360-B1F...................  Utva: 75.
IO-360-B2E...................  C.A.A.R.P.C.A.P. (10).
IO-360-B1F6..................  Great Lakes: Trainer.
IO-360-B1G6..................  American Blimp: Spector 42.
IO-360-B2F6..................  Great Lakes: Trainer.
LO-360-A1G6D.................  Beech Aircraft: Duchess.
LO-360-A1H6..................  Piper Aircraft: Seminole (PA-44).
IO-360-E1A...................  T.R. Smith Aircraft: Aerostar.
IO-360-L2A...................  Cessna Aircraft: Skyhawk C-172.
IO-360-M1A...................  Diamond Aircraft: DA-40.
IO-360-M1B...................  Vans Aircraft: RV6, RV7, RV8.
                               Lancair: 360.
AEIO-360-B1F.................  F.F.A.: Bravo (200).
                               Grob: G115/Sport-Acro.
AEIO-360-B1G6................  Great Lakes.
AEIO-360-B2F.................  Mundry: CAP-10.
AEIO-360-B4A.................  Pitts: S-1S.

AEIO-360-H1A.................  Bellanca Aircraft: Super Decathalon
                                (8KCAB-180).
AEIO-360-H1B.................  American Champion: Super Decathalon.
VO-360-A1A...................  Brantly Hynes Helicopter: (B-2).
VO-360-A1B...................  Brantly Hynes Helicopter: (B-2, B2-A).
                                Military (YHO-3BR).
VO-360-B1A...................  Brantly Hynes Helicopter: (B-2, B2-A).
IVO-360-A1A..................  Brantly Hynes Helicopter: (B2-B).
HO-360-B1A...................  Hughes Tool Co.: (269A).
HO-360-B1B...................  Hughes Tool Co.: (269A).
HO-360-C1A...................  Schweizer: (300C).
HIO-360-B1A..................  Hughes Tool Co.: Military (269-A-1) (TH-
                                55A).
HIO-360-B1B..................  Hughes Tool Co.: (269A).
HIO-360-G1A..................  Schweizer: (CB).
O-540-A1A....................  Rhein-Flugzeugbau: (RF-1).
O-540-A1A5...................  Piper Aircraft: Comanche (PA-24 ``180'').
                               Helio: Military (H-250).
                               Yoeman Aviation: (YA-1).
O-540-A1B5...................  Piper Aircraft: Aztec (PA-23 ``250''),
                                Comanche (PA-24 ``250'').
O-540-A1C5...................  Piper Aircraft: Comanche (PA-24 ``250'').
O-540-A1D....................  Found Bros.: (FBA-2C).
                               Dornier: (DO-28-B1).
O-540-A1D5...................  Piper Aircraft: Aztec (PA-23 ``250''),
                                Comanche (PA-24 ``250''), Military Aztec
                                (U-11A).
                               Dornier: (DO-28).
O-540-A2B....................  Aero Commander: (500).
                               Mid-States Mfg. Co.: Twin Courier (H-500)
                                (U-5).
O-540-A3D5...................  Piper Aircraft: Navy Aztec (PA-23
                                ``250'').
O-540-B1A5...................  Piper Aircraft: Apache (PA-23 ``235'').
O-540-B1B5...................  Piper Aircraft: Comanche (PA-24 ``250'').
                               Doyn Aircraft: Doyn-Piper (PA-24
                                ``250'').
O-540-B1D5...................  Wassmer: (WA-421).
O-540-B2B5...................  Piper Aircraft: Pawnee (PA-25 ``235''),
                                Cherokee (PA-28 ``235''), Aztec (PA-23
                                ``235'').
                               Intermountain Mfg. Co.: Call Air (A-9).
                               Rawdon Bros.: Rawdon (T-1).
                               S.O.C.A.T.A.: Rallye 235CA.
O-540-B2C5...................  Piper Aircraft: Pawnee (PA-25 ``235'').
O-540-B4B5...................  Piper Aircraft: Cherokee (PA-28 ``235'').
                               Embraer: Corioca (EMB-710).
                               S.O.C.A.T.A.: Rallye 235GT, Rallye 235C.
                               Maule: Star Rocket (MX-7-235), Super
                                Rocket (M-6-235), Super Std. Rocket (M-7-
                                235).
O-540-E4A5...................  Piper Aircraft: Comanche (PA-24 ``260'').
                               Aviamilano: Flamingo (F-250).
                               Siai-Marchetti: (SF-260) (SF-208).
O-540-E4B5...................  Britten-Norman: (BN-2).
                               Piper Aircraft: Cherokee Six (PA-32
                                ``260'').
O-540-E4C5...................  Pilatus Britten-Norman: Islander (BN-2A-
                                26), Islander (BN-2A-27), Islander II
                                (BN-2B-26), Islander (BN-2A-21),
                                Trislander (BN-2A-Mark III-2).
O-540-F1B5...................  Omega Aircraft: (BS-12D1).
                               Robinson: (R-44).
O-540-G1A5...................  Piper Aircraft: Pawnee (PA-25 ``260'').
O-540-H1B5D..................  Aero Boero: 260.
O-540-H2A5...................  Embraer: Impanema ``AG''.
                               Gippsland: GA-200.
O-540-H2B5D..................  Aero Boero: 260.
O-540-J1A5D..................  Maule: Star Rocket (MX-7-235), Super
                                Rocket (M-6-235), Super Std. Rocket (M-7-
                                235).
O-540-J3A5...................  Robin: R-3000/235.
O-540-J3A5D..................  Piper Aircraft: Dakota (PA-28-236).
O-540-J3C5D..................  Cessna Aircraft: Skylane RG.
O-540-L3C5D..................  Cessna Aircraft: TR-182, Turbo Skylane
                                RG.
IO-540-C1B5..................  Piper Aircraft: Aztec B (PA-23 ``250''),
                                Comanche (PA-24 ``250'').
IO-540-C1C5..................  Riley Aircraft: Turbo-Rocket.
IO-540-C4B5..................  Piper Aircraft: Aztec C (PA-23 ``250''),
                                Aztec F.
                               Wassmer: (WA4-21).
                               Avions Pierre Robin: (HR100/250).
                               Bellanca Aircraft: Aries T-250.
                               Aerofab: Renegade 250.
IO-540-C4D5..................  S.O.C.A.T.A.: TB-20.
IO-540-C4D5D.................  S.O.C.A.T.A.: Trinidad TB-20.
IO-540-D4A5..................  Piper Aircraft: Comanche (PA-24 ``260'').
                               Siai-Marchetti: (SF-260).
IO-540-D4B5..................  Cerva: (CE-43 Guepard).
IO-540-J4A5..................  Piper Aircraft: Aztec (PA-23 ``250'').
IO-540-R1A5..................  Piper Aircraft: Comanche (PA-24).
IO-540-T4A5D.................  General Aviation: Model 114.

IO-540-T4B5..................  Commander: 114B.
IO-540-T4B5D.................  Rockwell: 114.
IO-540-T4C5D.................  Lake Aircraft: Seawolf.
IO-540-V4A5..................  Maule: MT-7-260, M-7-260.
                               Aircraft Manufacturing Factory.
IO-540-V4A5D.................  Brooklands: Scoutmaster.
IO-540-W1A5..................  Maule: MX-7-235, MT-7-235, M7-235.
IO-540-W1A5D.................  Maule: Star Rocket (MX-7-235), Super
                                Rocket (M-6-235), Super Std. Rocket (M-7-
                                235).
IO-540-W3A5D.................  Schweizer: Power Glider.
AEIO-540-D4A5................  Christen: Pitts (S-2S) (S-2B).
                               Siai-Marchetti: SF-260.
                               H.A.L.: HPT-32.
                               Slingsby: Firefly T3A.
AEIO-540-D4B5................  Moravan: Zlin-50L.
                               H.A.L.: HPT-32.
AEIO-540-D4D5................  Burkhart Grob: Grob G, 115T Aero.
TIO-540-C1A..................  Piper Aircraft: Turbo Aztec (PA-23-250).
TIO-540-K1AD.................  Piper Aircraft.
TIO-540-AA1AD................  Aerofab Inc.: Turbo Renegade (270).
TIO-540-AB1AD................  S.O.C.A.T.A.: Trinidad TC TB-21.
TIO-540-AB1BD................  Schweizer.
TIO-540-AF1A.................  Mooney Aircraft: ``TLS'' M20M.
TIO-540-AG1A.................  Commander Aircraft: 114TC.
TIO-540-AK1A.................  Cessna Aircraft: Turbo Skylane T182T.
LTIO-540-K1A.................  Piper Aircraft.
------------------------------------------------------------------------

Unsafe Condition

    (d) This AD results from reports of 45 failures with head
separations of ECi cylinder assemblies. We are issuing this AD to
prevent loss of engine power due to cracks at the head-to-barrel
interface in the cylinder assemblies and possible engine failure
caused by separation of a cylinder head, which could result in loss
of control of the aircraft.

Compliance

    (e) You are responsible for having the actions required by this
AD performed within the compliance times specified unless the
actions have already been done.

Engines Not Overhauled or Cylinder Assemblies Not Replaced Since New

    (f) If your engine has not been overhauled or had any cylinder
assemblies replaced since new, no further action is required.

Engines Overhauled or Cylinder Assemblies Replaced Since New

    (g) If your engine was overhauled or had a cylinder assembly
replaced since new, do the following:
    (1) Before further flight, inspect the maintenance records and
engine logbook to determine if the overhaul or repair facility used
ECi cylinder assemblies, P/N AEL65102, with cylinder head, PN
AEL85099, with a SN 1138-02 through SN 35171-22, or a SN 35239-01
through SN 37016-28, installed.
    (2) If the cylinder assemblies are not ECi, P/N AEL65102, no
further action is required.
    (3) If the cylinder assemblies are ECi, P/N AEL65102, and if the
serial number is not listed in this AD, no further action is
required.
    (4) If the cylinder assemblies are ECi, P/N AEL65102, and if the
serial number is listed in this AD, do the following:

Group ``A'' Cylinder Assemblies

    (i) For Group ``A'' cylinder assemblies:
    (A) Perform an initial visual inspection as specified in
paragraphs (h) through (j) of this AD, and an initial compression
test as specified in paragraphs (k) through (o) of this AD, within
the next 10 operating hours time-in-service (TIS), if the cylinder
assembly has 350 or more operating hours TIS on the effective date
of this AD, but fewer than 2,000 operating hours TIS.
    (B) Perform an initial visual inspection as specified in
paragraphs (h) through (j) of this AD, and an initial compression
test as specified in paragraphs (k) through (o) of this AD, before
exceeding 350 operating hours TIS, if the cylinder assembly has
fewer than 350 operating hours TIS on the effective date of this AD.
    (C) Replace cylinder assemblies installed in helicopter engines
within the next 25 operating hours TIS after the effective date of
this AD if the cylinder assembly has 1,500 operating hours TIS or
more on the effective date of this AD.
    (D) Replace cylinder assemblies installed in airplane engines
within the next 25 operating hours TIS after the effective date of
this AD if the cylinder assembly has 2,000 operating hours TIS or
more on the effective date of this AD.
    (E) Perform repetitive visual inspections as specified in
paragraphs (h) through (j) of this AD, and repetitive compression
tests as specified in paragraphs (k) through (o) of this AD, within
every 50 operating hours TIS.
    (F) Replace cylinder assemblies installed in helicopter engines
that pass the visual inspections and compression tests, no later
than 1,500 operating hours TIS after the effective date of this AD.
    (G) Replace cylinder assemblies installed in airplane engines
that pass the visual inspections and compression tests, no later
than 2,000 operating hours TIS after the effective date of this AD.

Group ``B'' Cylinder Assemblies

    (ii) For Group ``B'' cylinder assemblies:
    (A) Perform an initial visual inspection as specified in
paragraphs (h) through (j) of this AD, and initial compression test
as specified in paragraphs (k) through (o) of this AD, within an
additional 10 operating hours TIS.
    (B) Replace the cylinder assembly within the next 25 operating
hours TIS after the effective date of this AD if the cylinder
assembly has 350 or more operating hours TIS on the effective date
of this AD.
    (C) Replace cylinder assemblies that pass the initial visual
inspections and compression tests, before exceeding 350 operating
hours TIS after the effective date of this AD.

Visual Inspection

    (h) Visually inspect around the exhaust valve side, for cracks
or any signs of black or white residue of combustion leakage from
cracks.
    (i) Replace cracked cylinder assemblies before further flight.
    (j) Information on cylinder assembly visual inspection can be
found in ECi Mandatory Service Bulletin (MSB) No. 08-1, Revision 3,
dated August 19, 2008.

Cylinder Assembly Compression Test

    (k) Compression test the cylinder assembly.
    (l) Information on cylinder assembly compression testing can be
found in ECi MSB No. 08-1, Revision 3, dated August 19, 2008.
    (m) During the compression test, if the cylinder pressure gauge
reads below 70 pounds-per-square-inch, apply a water and

soap solution to the side of the leaking cylinder, near the head-to-
barrel interface.
    (n) Replace the cylinder assembly before further flight, if air
leakage and bubbles are observed on the side of the cylinder
assembly, near the head-to-barrel interface.
    (o) Repair or replace the engine cylinder assembly before
further flight if the cause of the low gauge reading in paragraph
(m) of this AD is from leaking intake or exhaust valves, or from
leaking piston rings.

Prohibition of ECi Cylinder Assemblies Affected by This AD

    (p) After the effective date of this AD, do not install any ECi
cylinder assembly, P/N AEL65102, with cylinder head, P/N AEL85099,
and with SN 1138-02 through SN 35171-22, or SN 35239-01 through SN
37016-28, onto any engine, and do not attempt to repair or reuse
these ECi cylinder assemblies.

Alternative Methods of Compliance

    (q) The Manager, Special Certification Office, has the authority
to approve alternative methods of compliance for this AD if
requested using the procedures found in 14 CFR 39.19.

Special Flight Permits

    (r) Under 14 CFR 39.23, we will not approve special flight
permits for this AD for engines that have failed the visual
inspection or the cylinder assembly compression test required by
this AD.

Related Information

    (s) ECi Mandatory Service Bulletin No. 08-1, Revision 3, dated
August 19, 2008, pertains to the subject of this AD.
    (t) Contact Peter W. Hakala, Aerospace Engineer, Special
Certification Office, FAA, Rotorcraft Directorate, 2601 Meacham
Blvd., Fort Worth, TX 76193; e-mail<EMAIL_ADDRESS>
telephone<PHONE_NUMBER>; fax<PHONE_NUMBER>, for more information
about this AD.

    Issued in Burlington, Massachusetts, on September 5, 2008.
Peter A. White,
Assistant Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. E8-21125 Filed 9-12-08; 8:45 am]

BILLING CODE 4910-13-P


[Federal Register Volume 87, Number 205 (Tuesday, October 25, 2022)]
[Notices]
[Pages 64496-64497]
[FR Doc No: 2022-23152]

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

DEPARTMENT OF HOMELAND SECURITY

Federal Emergency Management Agency

[Internal Agency Docket No. FEMA-4673-DR; Docket ID FEMA-2022-0001]

Florida; Amendment No. 5 to Notice of a Major Disaster
Declaration

AGENCY: Federal Emergency Management Agency, DHS.

ACTION: Notice.

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

SUMMARY: This notice amends the notice of a major disaster declaration
for the State of Florida (FEMA-4673-DR), dated September 29, 2022, and
related determinations.

DATES: This amendment was issued October 5, 2022.

FOR FURTHER INFORMATION CONTACT: Dean Webster, Office of Response and
Recovery, Federal Emergency Management Agency, 500 C Street SW,
Washington, DC 20472,<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: The notice of a major disaster declaration
for the State of Florida is hereby amended to include the following
areas among those areas determined to have been adversely affected by
the event declared a major disaster by the President in his declaration
of September 29, 2022.

    DeSoto, Flagler, Hillsborough, Putnam, Seminole, St. Johns, and
Volusia Counties for permanent work [Categories C-G] (already
designated for Individual Assistance and assistance for debris
removal and emergency protective measures [Categories A and B],
including direct federal assistance, under the Public Assistance
program).
    Indian River and Monroe Counties for debris removal [Category A]
and permanent work [Categories C-G] (already designated for
emergency protective measures [Category B], including direct federal
assistance, under the Public Assistance program).

    The following Catalog of Federal Domestic Assistance Numbers
(CFDA) are to be used for reporting and drawing funds: 97.030,
Community Disaster Loans; 97.031, Cora Brown Fund; 97.032, Crisis
Counseling; 97.033, Disaster Legal Services; 97.034, Disaster
Unemployment Assistance (DUA);

97.046, Fire Management Assistance Grant; 97.048, Disaster Housing
Assistance to Individuals and Households In Presidentially Declared
Disaster Areas; 97.049, Presidentially Declared Disaster
Assistance--Disaster Housing Operations for Individuals and
Households; 97.050, Presidentially Declared Disaster Assistance to
Individuals and Households--Other Needs; 97.036, Disaster Grants--
Public Assistance (Presidentially Declared Disasters); 97.039,
Hazard Mitigation Grant.

Deanne Criswell,
Administrator, Federal Emergency Management Agency.
[FR Doc. 2022-23152 Filed 10-24-22; 8:45 am]
BILLING CODE 9111-23-P


Personnel are qualified and capable of performing set up and field repairs of all sizes of portable generators
                   Composition & Ordering Specifications
Requestor must specify Kilowatt (kW) and voltage of generators needed or existing

Requestor should indicate type of connection provisions in place

Trailer-mounted generators are preferred to skid-mounted

Portable switch-gear preferred

Refueling arrangements must be established

Volts: 480_____ 4160_____
Revolutions Per Minute, (RPM): 540_____ 1100_____

Security requirements should be determined by the requesting agency based upon actual field conditions and/or intelligence. Requesting agency should determine if it will provide security or if the responding team/personnel needs to provide security

                                Resource Types

                                   Component
                               Metric / Measure
                                  Capability
                                    Type I
                                    Type II
                                   Type III
                                    Type IV
                                     Notes
Personnel
Hours of operation per shift

 12 hours
 12 hours

Personnel
Duration of self-contained operation

72 hours
0 hours

Support external to the teams will be needed from the requestor such as security, fuel, recharging for phones, batteries, power for computers, etc.
Personnel
Positions per team

1 Qualified electrician
1 Electrician's assistant
1 Qualified electrician
1 Electrician's assistant

Equipment
Duration of sustained  operation

Up to 14 days
Up to 14 days

Equipment
(Vehicle and Specialized Equipment)
# and kind of per team

1 Truck capable of pulling generator(s) delivered
Necessary tools for generator connection
1 Truck capable of pulling generator(s) delivered
Necessary tools for generator connection

Equipment (Communications)
Quantity and kind based on mission assignments

Cell phones, portable radios, satellite phone
Cell phones, portable radios, satellite phone

Supplies (Logistics)
Quantity and kind based on mission assignments

Water/fluids, food, shelter, sanitation, safety equipment, and personal gear
Safety equipment and personal gear

                                   Comments

                                 Reference(s)

	Description
 - This team may be deployed to assist or relieve local water/wastewater management
Resource Category
Public Works
Resource Kind
Team (with personnel/equipment components)
overall function
This team steps into utility management role to supplement on-site personnel

Team should be multidisciplinary and designed dependent upon incident

May be deployed to staff Emergency Support Function (ESF) 3 desk or relieve/supplement local Water/Wastewater Management Team

                   Composition & Ordering Specifications
Mission-specific to identify supporting resources necessary

Security requirements should be determined by the requesting agency based upon actual field conditions and/or intelligence. Requesting agency should determine if it will provide security or if the responding team/personnel needs to provide security

                                Resource Types

                                   Component
                               Metric / Measure
                                  Capability
                                    Type I
                                    Type II
                                   Type III
                                    Type IV
                                     Notes
Personnel
Hours of operation per shift

 12 hours
 12 hours

Personnel
Duration of self-contained operation

72 hours
0 hours

Support external to the teams will be needed from the requestor such as security, fuel, recharging for phones, batteries, power for computers, etc.
Personnel
Positions per team

2-4 Qualified incident commander and individuals experienced in other National Incident Management System (NIMS) / Incident command System (ICS) roles
2-4 Qualified incident commander and individuals experienced in other National Incident Management System (NIMS) / Incident command System (ICS)roles

Equipment
Duration of sustained  operation

Up to 14 days
Up to 14 days

Equipment
(Vehicle and Specialized Equipment)
# and kind of per team

1-2 Light-duty vehicles preferred. 2-4 laptop computers
1-2 Light-duty vehicles preferred. 2-4 laptop computers

Equipment (Communications)
Quantity and kind based on mission assignments

Cell phones, portable radios, satellite phone
Cell phones, portable radios, satellite phone

Supplies (Logistics)
Quantity and kind based on mission assignments

Water/fluids, food, shelter, sanitation, safety equipment, and personal gear
Safety equipment and personal gear

                                   Comments

                                 Reference(s)


	RCRA REVISION CHECKLIST 240

                     Safe Management of Recalled Airbags
                               83 FR 61552-61563
	November 30, 2018
	(RCRA Cluster XXVII, Non-HSWA)

Name of State:  Virginia

State Statutory Authority: § 10.1-1402 of the Code of Virginia

Title of Regulations:  	Virginia Hazardous Waste Management Regulations, 9VAC20-60

Effective Date:   August 23, 2019 (VA.R. Volume 35, Issue 24, July 22, 2019)

Date Checklist Completed: August 26, 2019

                             FEDERAL REQUIREMENTS

                             FEDERAL RCRA CITATION

                           ANALOGOUS STATE CITATION

                               STATE ANALOG IS:

                                  EQUIV-ALENT

                                     LESS
                                    STRIN-
                                     GENT

                                MORE STRIN-GENT

                               BROADER IN SCOPE

             PART 260 HAZARDOUS WASTE MANAGEMENT SYSTEM:  GENERAL

                             SUBPART B DEFINITIONS

DEFINITIONS

Airbag waste means any hazardous waste airbag modules or hazardous waste airbag inflators.
260.10 "Airbag waste"
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-260A.
                                       X

Airbag waste collection facility means any facility that receives airbag waste from airbag handlers subject to regulation under 261.4(j) of this chapter, and accumulates the waste for more than ten days.
260.10 "Airbag waste collection facility"
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-260A.
                                       X

Airbag waste handler means any person, by site, who generates airbag waste that is subject to regulation under this chapter.
260.10 "Airbag waste handler"
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-260A.
                                       X

            PART 261 IDENTIFICATION AND LISTING OF HAZARDOUS WASTE

                               SUBPART A GENERAL

reserved
261.4(i)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-261A.
                                       X

Airbag waste at the airbag waste handler or during transport to an airbag waste collection facility or designated facility is not subject to regulation under parts 262 through parts 268, 270 or 124 of this chapter, and is not subject to the notification requirements of section 3010 of RCRA provided that:
261.4(j)(1)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-261A.
                                       X

The airbag waste is accumulated in a quantity of no more than 250 airbag modules or airbag inflators, for no longer than 180 days;
261.4(j)(1)(i)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-261A.
                                       X

The airbag waste is packaged in a container designed to address the risk posed by the airbag waste and labeled "Airbag Waste  -  Do Not Reuse;"
261.4(j)(1)(ii)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-261A.
                                       X

The airbag waste is sent directly to either
261.4(j)(1)(iii)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-261A.
                                       X

An airbag waste collection facility in the United States under the control of a vehicle manufacturer or their authorized representative, or under the control of an authorized party administering a remedy program in response to a recall under the National Highway Traffic Safety Administration, or
261.4(j)(1)(iii)(A)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-261A.
                                       X

A designated facility as defined in 40 CFR 260.10;
261.4(j)(1)(iii)(B)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-261A.
                                       X

The transport of the airbag waste complies with all applicable U.S. Department of Transportation regulations in 49 CFR part 171 through 180 during transit;
261.4(j)(1)(iv)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-261A.
                                       X

The airbag waste handler maintains at the handler facility for no less than three (3) years records of all off-site shipments of airbag waste and all confirmations of receipt from the receiving facility. For each shipment, these records must, at a minimum, contain the name of the transporter and date of the shipment; name and address of receiving facility; and the type and quantity of airbag waste (i.e., airbag modules or airbag inflators) in the shipment. Confirmations of receipt must include the name and address of the receiving facility; the type and quantity of the airbag waste (i.e., airbag modules and airbag inflators) received; and the date which it was received. Shipping records and confirmations of receipt must be made available for inspection and may be satisfied by routine business records (e.g., electronic or paper financial records, bills of lading, copies of DOT shipping papers, or electronic confirmations of receipt).
261.4(j)(1)(v)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-261A.
                                       X

Once the airbag waste arrives at an airbag waste collection facility or designated facility, it becomes subject to all applicable hazardous waste regulations, and the facility receiving airbag waste is considered the hazardous waste generator for the purposes of the hazardous waste regulations and must comply with the requirements of 40 CFR part 262.
261.4(j)(2)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-261A.
                                       X

Reuse in vehicles of defective airbag modules or defective airbag inflators subject to a recall under the National Highway Traffic Safety Administration is considered sham recycling and prohibited under 40 CFR 261.2(g).
261.4(j)(3)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-261A.
                                       X

      PART 262  -  STANDARDS APPLICABLE TO GENERATORS OF HAZARDOUS WASTE

                              SUBPART A - GENERAL
                                                                              1
reserved
262.14(a)(5)(ix)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-262A.
                                       X

                                                                              1
reserved
262.14(a)(5)(x)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-262A.
                                       X

                                                                              2
For airbag waste, an airbag waste collection facility or a designated facility subject to the requirements of 261.4(j) of this chapter.
262.14(a)(5)(xi)
9VAC20-60-18.
Incorporated by reference (IBR) in 9VAC20-60-262A.
                                       X

1. 40 CFR 262.14(a)(5)(ix) and (x) are reserved for the insertion of provisions from the Management Standards for Hazardous Waste Pharmaceuticals and Amendment to the P075 Listing for Nicotine rule (citation, Revision Checklist 241).

2. 40 CFR 262.14(a)(5)(xi) is the only provision within 262.14(a) which was added or amended by this rule. The other provisions in this section are either unchanged or reserved and therefore the unchanged provisions are not included in this checklist.


[Federal Register Volume 84, Number 62 (Monday, April 1, 2019)]
[Rules and Regulations]
[Pages 12073-12074]
[FR Doc No: 2019-06261]

=======================================================================
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SECURITIES AND EXCHANGE COMMISSION

17 CFR Part 232

[Release Nos. 33-10615; 34-85296; 39-2525; IC-33398]

Adoption of Updated EDGAR Filer Manual

AGENCY: Securities and Exchange Commission.

ACTION: Final rule.

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

SUMMARY: The Securities and Exchange Commission (the ``Commission'')
adopted revisions to the Electronic Data Gathering, Analysis, and
Retrieval System (``EDGAR'') Filer Manual (``EDGAR Filer Manual'' or
``Filer Manual'') and related rules. The EDGAR system is scheduled to
be upgraded on March 11, 2019.

DATES: Effective April 1, 2019. The incorporation by reference of the
EDGAR Filer Manual is approved by the Director of the Federal Register
as of April 1, 2019.

FOR FURTHER INFORMATION CONTACT: In the Division of Trading and
Markets, for questions concerning Form ATS-N, contact Michael R.
Broderick at<PHONE_NUMBER>. In the Office of Municipal Securities, for
questions regarding Forms MA, MA-A and MA-I, contact Ahmed A. Abonamah
at<PHONE_NUMBER>. In the Division of Corporation Finance, for
questions concerning Forms 1-A and DOS, contact Heather Mackintosh at
(202) 551-8111. In the Division of Investment Management, for question
concerning Form N-PORT XML, contact Heather Fernandez at (202) 551-
6708. In the Division of Economic and Risk Analysis, for questions
concerning Inline XBRL submission requirements, contact Mike Willis at
(202) 551-6627.

SUPPLEMENTARY INFORMATION: We adopted an updated EDGAR Filer Manual,
Volume II. The Filer Manual describes the technical formatting
requirements for the preparation and submission of electronic filings
through the EDGAR system.\1\ It also describes the requirements for
filing using EDGARLink Online and the EDGAR Online Forms website.
---------------------------------------------------------------------------

    \1\ We originally adopted the Filer Manual on April 1, 1993,
with an effective date of April 26, 1993. Release No. 33-6986 (April
1, 1993) [58 FR 18638]. We implemented the most recent update to the
Filer Manual on December 14, 2018. See Release No. 33-10585
(December 14, 2018) [83 FR 66100].
---------------------------------------------------------------------------

    The revisions to the Filer Manual reflect changes within Volume II,
entitled EDGAR Filer Manual, Volume II: ``EDGAR Filing,'' (Version 50)
(March 2019). The updated manual is incorporated by reference into the
Code of Federal Regulations.
    The Filer Manual contains all the technical specifications for
filers to submit filings using the EDGAR system. Filers must comply
with the applicable provisions of the Filer Manual in order to assure
the timely acceptance and processing of filings made in electronic
format.\2\ Filers should consult the Filer Manual in conjunction with
our rules governing mandated electronic filings when preparing
documents for electronic submission.
---------------------------------------------------------------------------

    \2\ See Rule 301 of Regulation S-T (17 CFR 232.301).
---------------------------------------------------------------------------

    The EDGAR System and Filer Manual will be updated in Release 19.1
and reflect the changes described below.
    EDGAR introduces changes associated with the adoption of Inline
eXtensible Business Reporting Language (``Inline XBRL'') requirements
for the submission of operating company financial information and fund
risk/return summaries.\3\ The EDGAR system is updated to implement
changes that expand the submission form types that are permitted to
include Inline XBRL submissions. Accordingly, the following additional
submission form types permit the primary document to be in Inline XBRL
format: S-1, S-1/A, S-1MEF, S-3, S-3/A, S-3ASR, S-3D, S-3DPOS, S-3MEF,
S-4, S-4/A, S-4EF, S-4MEF, S-4 POS, S-11, S-11/A, S-11MEF, F-1, F-1/A,
F-1MEF, F-3, F-3/A, F-3ASR, F-3D, F-3DPOS, F-3MEF, F-4, F-4/A, F-4EF,
F-4MEF, F-4 POS, F-10, F-10/A, F-10EF, F-10POS, N-1A, N-1A/A, 485APOS,
485BPOS, 485BXT, and 497. The EDGAR system also is updated to allow
more than one Inline XBRL file attachment per submission to be pre-
validated, submitted, validated, accepted, rendered, and viewed. In
addition, given the termination of the Voluntary XBRL program, the
EDGAR Filer Manual and the EDGAR system are updated to remove and no
longer permit submissions having EX-100 Voluntary XBRL attachments.
Also, the EDGAR Filer Manual updates instructions regarding the layout
specifications for Risk Return Summary Information submissions tagged
with Inline XBRL. Finally, the revised EDGAR Filer Manual clarifies how
EDGAR processes submissions that contain Inline XBRL presentations that
do not pass validation. Please refer to Chapter 5 (Constructing
Attached Documents and Document Types), Chapter 6 (Interactive Data),
and Appendix E (Automated Conformance Rules for EDGAR Data Fields) of
the EDGAR Filer Manual, Volume II: ``EDGAR Filing.''
---------------------------------------------------------------------------

    \3\ See Release No. 33-10514 (June 28, 2018) [83 FR 40846].
---------------------------------------------------------------------------

    EDGAR Release 19.1 updates Item 2 for submission form types 1-A, 1-
A/A, 1-A POS, DOS, and DOS/A to clarify that filers subject to Section
13 or 15(d) of the Securities Exchange Act of 1934 are no longer
ineligible to use the form. Please refer to Chapter 8 (Preparing and
Transmitting Online Submissions) of the EDGAR Filer Manual, Volume II:
``EDGAR Filing.''
    EDGAR permits the display of Schedule B data in submission form
types MA-A and MA/A, provided that information for Schedule B was
included in the filer's most recent Form MA, MA-A or MA/A filing.
Corresponding changes are reflected in the EDGAR Filer Manual. Please
refer to Chapter 8 (Preparing and Transmitting Online Submissions) of
the EDGAR Filer Manual, Volume II: ``EDGAR Filing.''
    In EDGAR Release 18.4, EDGAR was updated to accept submissions of
Form ATS-N and its related EDGAR submission types. In EDGAR Release
19.1, the EDGAR Filer Manual is revised to provide clarifying
information for filers regarding the processing of Form ATS-N
submissions. Please refer to Chapter 8 (Preparing and Transmitting
Online Submissions) of the EDGAR Filer Manual, Volume II: ``EDGAR
Filing.''
    EDGAR Release 19.1 also introduces changes to the ``EDGAR Form N-
PORT XML Technical Specification'' document, which is available on the
SEC's public website at https://www.sec.gov/info/edgar/tech-specs.
    In EDGAR Release 19.1, the EDGAR system is upgraded to support the
2019 GAAP, 2019 EXCH, 2019 Currency and 2019 SRT Taxonomies. Please see
https://www.sec.gov/info/edgar/edgartaxonomies.shtml for a complete
listing of supported standard taxonomies.

    Along with the adoption of the Filer Manual, we are amending Rule
301 of Regulation S-T to provide for the incorporation by reference
into the Code of Federal Regulations of today's revisions. This
incorporation by reference was approved by the Director of the Federal
Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51.
    The updated EDGAR Filer Manual is available for website viewing and
printing; the address for the Filer Manual is https://www.sec.gov/info/edgar/edmanuals.htm. You may also obtain paper copies of the EDGAR
Filer Manual from the following address: Public Reference Room, U.S.
Securities and Exchange Commission, 100 F Street NE, Washington, DC
20549, on official business days between the hours of 10 a.m. and 3
p.m.
    Since the Filer Manual and the corresponding rule and form
amendments relate solely to agency procedures or practice, publication
for notice and comment is not required under the Administrative
Procedure Act (``APA'').\4\ It follows that the requirements of the
Regulatory Flexibility Act \5\ do not apply.
---------------------------------------------------------------------------

    \4\ 5 U.S.C. 553(b)(A).
    \5\ 5 U.S.C. 601-612.
---------------------------------------------------------------------------

    The effective date for the updated Filer Manual and the related
rule and form amendments is April 1, 2019. In accordance with the
APA,\6\ we find that there is good cause to establish an effective date
less than 30 days after publication of these rules. The Commission
believes that establishing an effective date less than 30 days after
publication of these rules is necessary to coordinate the effectiveness
of the updated Filer Manual with these system upgrades.
---------------------------------------------------------------------------

    \6\ 5 U.S.C. 553(d)(3).
---------------------------------------------------------------------------

Statutory Basis

    We are adopting the amendments to Regulation S-T under the
authority in Sections 6, 7, 8, 10, and 19(a) of the Securities Act of
1933,\7\ Sections 3, 12, 13, 14, 15, 15B, 23, and 35A of the Securities
Exchange Act of 1934,\8\ Section 319 of the Trust Indenture Act of
1939,\9\ and Sections 8, 30, 31, and 38 of the Investment Company Act
of 1940.\10\
---------------------------------------------------------------------------

    \7\ 15 U.S.C. 77f, 77g, 77h, 77j, and 77s(a).
    \8\ 15 U.S.C. 78c, 78l, 78m, 78n, 78o, 78o-4, 78w, and 78ll.
    \9\ 15 U.S.C. 77sss.
    \10\ 15 U.S.C. 80a-8, 80a-29, 80a-30, and 80a-37.
---------------------------------------------------------------------------

List of Subjects in 17 CFR Part 232

    Incorporation by reference, Reporting and recordkeeping
requirements, Securities.

Text of the Amendments

    In accordance with the foregoing, title 17, chapter II of the Code
of Federal Regulations is amended as follows:

PART 232 REGULATION S-T--GENERAL RULES AND REGULATIONS FOR
ELECTRONIC FILINGS

0
1. The authority citation for part 232 continues to read in part as
follows:

    Authority:  15 U.S.C. 77c, 77f, 77g, 77h, 77j, 77s(a), 77z-3,
77sss(a), 78c(b), 78l, 78m, 78n, 78o(d), 78w(a), 78ll, 80a-6(c),
80a-8, 80a-29, 80a-30, 80a-37, 7201 et seq.; and 18 U.S.C. 1350,
unless otherwise noted.
* * * * *

0
2. Section 232.301 is revised to read as follows:

Sec.  232.301   EDGAR Filer Manual.

    Filers must prepare electronic filings in the manner prescribed by
the EDGAR Filer Manual, promulgated by the Commission, which sets forth
the technical formatting requirements for electronic submissions. The
requirements for becoming an EDGAR Filer and updating company data are
set forth in the updated EDGAR Filer Manual, Volume I: ``General
Information,'' Version 32 (December 2018). The requirements for filing
on EDGAR are set forth in the updated EDGAR Filer Manual, Volume II:
``EDGAR Filing,'' Version 50 (March 2019). Additional provisions
applicable to Form N-SAR filers are set forth in the EDGAR Filer
Manual, Volume III: ``N-SAR Supplement,'' Version 6 (January 2017). All
of these provisions have been incorporated by reference into the Code
of Federal Regulations, which action was approved by the Director of
the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part
51. You must comply with these requirements in order for documents to
be timely received and accepted. The EDGAR Filer Manual is available
for website viewing and printing; the address for the Filer Manual is
https://www.sec.gov/info/edgar/edmanuals.htm. You can obtain paper
copies of the EDGAR Filer Manual at the following address: Public
Reference Room, U.S. Securities and Exchange Commission, 100 F Street
NE, Washington, DC 20549, on official business days between the hours
of 10:00 a.m. and 3:00 p.m. You can also inspect the document at the
National Archives and Records Administration (NARA). For information on
the availability of this material at NARA, call<PHONE_NUMBER>, or go to:
https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    By the Commission.
    Dated: March 12, 2019.
Eduardo A. Aleman,
Deputy Secretary.
[FR Doc. 2019-06261 Filed 3-29-19; 8:45 am]
 BILLING CODE P


[Federal Register Volume 81, Number 26 (Tuesday, February 9, 2016)]
[Notices]
[Pages 6850-6851]
[FR Doc No: 2016-02495]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

[Docket No. CP16-64-000]

ANR Pipeline Company; Notice of Application

    Take notice that on January 20, 2016, ANR Pipeline Company (ANR),
having its principal place of business at 700 Louisiana Street, Suite
700, Houston, Texas 77002-2700, filed in the above referenced docket an
application pursuant to sections 7(c) of the Natural Gas Act (NGA), and
Part 157 of the Commission's regulations requesting authorization to
install, own and operate its Collierville Expansion Project (Project)
located in Shelby Counties, Tennessee, all as more fully set forth in
the application which is on file with the Commission and open to public
inspection. The filing is available for review at the Commission in the
Public Reference Room or may be viewed on the Commission's Web site at
http://www.ferc.gov using the ``eLibrary'' link. Enter the docket
number excluding the last three digits in the docket number field to
access the document. For assistance, contact FERC at
<EMAIL_ADDRESS>or call toll-free,<PHONE_NUMBER> or TYY,
(202) 502-8659.

    Any questions concerning this application may be directed to Robert
Jackson, Manager, Certificates and Regulatory Administration, ANR
Pipeline Company, 700 Louisiana Street, Suite 700, Houston, Texas
77002-2700; by calling<PHONE_NUMBER>; by faxing<PHONE_NUMBER>; or by
emailing<EMAIL_ADDRESS>    Specifically, the applicant proposes the Project will consist of
modifications to upgrade ANR's existing Collierville Meter Station, and
install one (1) new compressor station consisting of one (1) new,
approximately 4,700 horsepower turbine compressor unit and appurtenant
facilities. Upon completion, ANR avers that the Project will expand the
delivery capability of ANR's existing Collierville Meter Station by an
additional 200 million cubic feet per day (MMcf/d), while maintaining
ANR's current certificated capacity levels. ANR estimates the total
cost of the Project to be $36.7 million.
    Pursuant to section 157.9 of the Commission's rules (18 CFR 157.9),
within 90 days of this Notice, the Commission staff will either:
complete its environmental assessment (EA) and place it into the
Commission's public record (eLibrary) for this proceeding; or issue a
Notice of Schedule for Environmental Review. If a Notice of Schedule
for Environmental Review is issued, it will indicate, among other
milestones, the anticipated date for the Commission staff's issuance of
the final environmental impact statement (FEIS) or EA for this
proposal. The filing of the EA in the Commission's public record for
this proceeding or the issuance of a Notice of Schedule for
Environmental Review will serve to notify federal and state agencies of
the timing for the completion of all necessary reviews, and the
subsequent need to complete all federal authorizations within 90 days
of the date of issuance of the Commission staff's FEIS or EA.
    There are two ways to become involved in the Commission's review of
this project. First, any person wishing to obtain legal status by
becoming a party to the proceedings for this project should, on or
before the comment date stated below file with the Federal Energy
Regulatory Commission, 888 First Street NE., Washington, DC 20426, a
motion to intervene in accordance with the requirements of the
Commission's Rules of Practice and Procedure (18 CFR 385.214 or
385.211) and the Regulations under the NGA (18 CFR 157.10). A person
obtaining party status will be placed on the service list maintained by
the Secretary of the Commission and will receive copies of all
documents filed by the applicant and by all other parties. A party must
submit seven copies of filings made in the proceeding with the
Commission and must mail a copy to the applicant and to every other
party. Only parties to the proceeding can ask for court review of
Commission orders in the proceeding.
    However, a person does not have to intervene in order to have
comments considered. The second way to participate is by filing with
the Secretary of the Commission, as soon as possible, an original and
two copies of comments in support of or in opposition to this project.
The Commission will consider these comments in determining the
appropriate action to be taken, but the filing of a comment alone will
not serve to make the filer a party to the proceeding. The Commission's
rules require that persons filing comments in opposition to the project
provide copies of their protests only to the party or parties directly
involved in the protest.
    Persons who wish to comment only on the environmental review of
this project should submit an original and two copies of their comments
to the Secretary of the Commission. Environmental commentors will be
placed on the Commission's environmental mailing list, will receive
copies of the environmental documents, and will be notified of meetings
associated with the Commission's environmental review process.
Environmental commentors will not be required to serve copies of filed
documents on all other parties. However, the non-party commentors will
not receive copies of all documents filed by other parties or issued by
the Commission (except for the mailing of environmental documents
issued by the Commission) and will not have the right to seek court
review of the Commission's final order.
    The Commission strongly encourages electronic filings of comments,
protests and interventions in lieu of paper using the ``eFiling'' link
at http://www.ferc.gov. Persons unable to file electronically should
submit an original and 7 copies of the protest or intervention to the
Federal Energy Regulatory Commission, 888 First Street NE., Washington,
DC 20426.
    Comment Date: 5:00 p.m. Eastern Time on February 24, 2016.

    Dated: February 3, 2016.
Nathaniel J. Davis, Sr.,
Deputy Secretary.
 [FR Doc. 2016-02495 Filed 2-8-16; 8:45 am]
 BILLING CODE 6717-01-P


[Federal Register Volume 77, Number 149 (Thursday, August 2, 2012)]
[Notices]
[Page 46103]
[FR Doc No: 2012-18853]

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DEPARTMENT OF HOMELAND SECURITY

Federal Emergency Management Agency

[Internal Agency Docket No. FEMA-4069-DR; Docket ID FEMA-2012-0002]

Minnesota; Major Disaster and Related Determinations

AGENCY: Federal Emergency Management Agency, DHS.

ACTION: Notice.

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

SUMMARY: This is a notice of the Presidential declaration of a major
disaster for the State of Minnesota (FEMA-4069-DR), dated July 6, 2012,
and related determinations.

DATES: Effective Date: July 6, 2012.

FOR FURTHER INFORMATION CONTACT: Peggy Miller, Office of Response and
Recovery, Federal Emergency Management Agency, 500 C Street SW.,
Washington, DC 20472,<PHONE_NUMBER>.

SUPPLEMENTARY INFORMATION: Notice is hereby given that, in a letter
dated July 6, 2012, the President issued a major disaster declaration
under the authority of the Robert T. Stafford Disaster Relief and
Emergency Assistance Act, 42 U.S.C. 5121 et seq. (the ``Stafford
Act''), as follows:

    I have determined that the damage in certain areas of the State
of Minnesota resulting from severe storms and flooding during the
period of June 14-21, 2012, is of sufficient severity and magnitude
to warrant a major disaster declaration under the Robert T. Stafford
Disaster Relief and Emergency Assistance Act, 42 U.S.C. 5121 et seq.
(the ``Stafford Act''). Therefore, I declare that such a major
disaster exists in the State of Minnesota.
    In order to provide Federal assistance, you are hereby
authorized to allocate from funds available for these purposes such
amounts as you find necessary for Federal disaster assistance and
administrative expenses.
    You are authorized to provide Public Assistance in the
designated areas and Hazard Mitigation throughout the State.
Consistent with the requirement that Federal assistance is
supplemental, any Federal funds provided under the Stafford Act for
Public Assistance and Hazard Mitigation will be limited to 75
percent of the total eligible costs.
    Further, you are authorized to make changes to this declaration
for the approved assistance to the extent allowable under the
Stafford Act.

    The Federal Emergency Management Agency (FEMA) hereby gives notice
that pursuant to the authority vested in the Administrator, under
Executive Order 12148, as amended, Mark A. Neveau, of FEMA is appointed
to act as the Federal Coordinating Officer for this major disaster.
    The following areas of the State of Minnesota have been designated
as adversely affected by this major disaster:

    Aitkin, Carlton, Cook, Crow Wing, Dakota, Goodhue, Kandiyohi,
Lake, Meeker, Pine, Rice, Sibley, and St. Louis Counties and the
Fond du Lac Band of Lake Superior Chippewa, Grand Portage Band of
Lake Superior Chippewa, and the Mille Lacs Band of Ojibwe for Public
Assistance.
    All counties within the State of Minnesota are eligible to apply
for assistance under the Hazard Mitigation Grant Program.

The following Catalog of Federal Domestic Assistance Numbers (CFDA)
are to be used for reporting and drawing funds: 97.030, Community
Disaster Loans; 97.031, Cora Brown Fund; 97.032, Crisis Counseling;
97.033, Disaster Legal Services; 97.034, Disaster Unemployment
Assistance (DUA); 97.046, Fire Management Assistance Grant; 97.048,
Disaster Housing Assistance to Individuals and Households In
Presidentially Declared Disaster Areas; 97.049, Presidentially
Declared Disaster Assistance--Disaster Housing Operations for
Individuals and Households; 97.050, Presidentially Declared Disaster
Assistance to Individuals and Households--Other Needs; 97.036,
Disaster Grants--Public Assistance (Presidentially Declared
Disasters); 97.039, Hazard Mitigation Grant.

W. Craig Fugate,
Administrator, Federal Emergency Management Agency.
[FR Doc. 2012-18853 Filed 8-1-12; 8:45 am]
BILLING CODE 9111-23-P


[Federal Register Volume 84, Number 113 (Wednesday, June 12, 2019)]
[Notices]
[Pages 27333-27335]
[FR Doc No: 2019-12316]

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DEPARTMENT OF HEALTH AND HUMAN SERVICES

Food and Drug Administration

[Docket No. FDA-2016-N-2474]

Agency Information Collection Activities; Proposed Collection;
Comment Request; Reporting Associated With Designated New Animal Drugs
for Minor Use and Minor Species

AGENCY: Food and Drug Administration, HHS.

ACTION: Notice.

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SUMMARY: The Food and Drug Administration (FDA or Agency) is announcing
an opportunity for public comment on the proposed collection of certain
information by the Agency. Under the Paperwork Reduction Act of 1995
(PRA), Federal Agencies are required to publish notice in the Federal
Register concerning each proposed collection of information, including
each proposed extension of an existing collection of information, and

to allow 60 days for public comment in response to the notice. This
notice solicits comments on the reporting associated with designation
under the Minor Use and Minor Species Animal Health Act of 2004 (MUMS
Act).

DATES: Submit either electronic or written comments on the collection
of information by August 12, 2019.

ADDRESSES: You may submit comments as follows. Please note that late,
untimely filed comments will not be considered. Electronic comments
must be submitted on or before August 12, 2019. The https://www.regulations.gov electronic filing system will accept comments until
11:59 p.m. Eastern Time at the end of August 12, 2019. Comments
received by mail/hand delivery/courier (for written/paper submissions)
will be considered timely if they are postmarked or the delivery
service acceptance receipt is on or before that date.

Electronic Submissions

    Submit electronic comments in the following way:
     Federal eRulemaking Portal: https://www.regulations.gov.
Follow the instructions for submitting comments. Comments submitted
electronically, including attachments, to https://www.regulations.gov
will be posted to the docket unchanged. Because your comment will be
made public, you are solely responsible for ensuring that your comment
does not include any confidential information that you or a third party
may not wish to be posted, such as medical information, your or anyone
else's Social Security number, or confidential business information,
such as a manufacturing process. Please note that if you include your
name, contact information, or other information that identifies you in
the body of your comments, that information will be posted on https://www.regulations.gov.
     If you want to submit a comment with confidential
information that you do not wish to be made available to the public,
submit the comment as a written/paper submission and in the manner
detailed (see ``Written/Paper Submissions'' and ``Instructions'').

Written/Paper Submissions

    Submit written/paper submissions as follows:
     Mail/Hand Delivery/Courier (for written/paper
submissions): Dockets Management Staff (HFA-305), Food and Drug
Administration, 5630 Fishers Lane, Rm. 1061, Rockville, MD 20852.
     For written/paper comments submitted to the Dockets
Management Staff, FDA will post your comment, as well as any
attachments, except for information submitted, marked and identified,
as confidential, if submitted as detailed in ``Instructions.''
    Instructions: All submissions received must include the Docket No.
FDA-2016-N-2474 for ``Reporting Associated With Designated New Animal
Drugs for Minor Use and Minor Species.'' Received comments, those filed
in a timely manner (see ADDRESSES), will be placed in the docket and,
except for those submitted as ``Confidential Submissions,'' publicly
viewable at https://www.regulations.gov or at the Dockets Management
Staff between 9 a.m. and 4 p.m., Monday through Friday.
     Confidential Submissions--To submit a comment with
confidential information that you do not wish to be made publicly
available, submit your comments only as a written/paper submission. You
should submit two copies total. One copy will include the information
you claim to be confidential with a heading or cover note that states
``THIS DOCUMENT CONTAINS CONFIDENTIAL INFORMATION.'' The Agency will
review this copy, including the claimed confidential information, in
its consideration of comments. The second copy, which will have the
claimed confidential information redacted/blacked out, will be
available for public viewing and posted on https://www.regulations.gov.
Submit both copies to the Dockets Management Staff. If you do not wish
your name and contact information to be made publicly available, you
can provide this information on the cover sheet and not in the body of
your comments and you must identify this information as
``confidential.'' Any information marked as ``confidential'' will not
be disclosed except in accordance with 21 CFR 10.20 and other
applicable disclosure law. For more information about FDA's posting of
comments to public dockets, see 80 FR 56469, September 18, 2015, or
access the information at: https://www.gpo.gov/fdsys/pkg/FR-2015-09-18/pdf/2015-23389.pdf.
    Docket: For access to the docket to read background documents or
the electronic and written/paper comments received, go to https://www.regulations.gov and insert the docket number, found in brackets in
the heading of this document, into the ``Search'' box and follow the
prompts and/or go to the Dockets Management Staff, 5630 Fishers Lane,
Rm. 1061, Rockville, MD 20852.

FOR FURTHER INFORMATION CONTACT: JonnaLynn Capezzuto, Office of
Operations, Food and Drug Administration, Three White Flint North, 10A-
12M, 11601 Landsdown St., North Bethesda, MD 20852,<PHONE_NUMBER>,
<EMAIL_ADDRESS>
SUPPLEMENTARY INFORMATION: Under the PRA (44 U.S.C. 3501-3520), Federal
Agencies must obtain approval from the Office of Management and Budget
(OMB) for each collection of information they conduct or sponsor.
``Collection of information'' is defined in 44 U.S.C. 3502(3) and 5 CFR
1320.3(c) and includes Agency requests or requirements that members of
the public submit reports, keep records, or provide information to a
third party. Section 3506(c)(2)(A) of the PRA (44 U.S.C. 3506(c)(2)(A))
requires Federal Agencies to provide a 60-day notice in the Federal
Register concerning each proposed collection of information, including
each proposed extension of an existing collection of information,
before submitting the collection to OMB for approval. To comply with
this requirement, FDA is publishing notice of the proposed collection
of information set forth in this document.
    With respect to the following collection of information, FDA
invites comments on these topics: (1) Whether the proposed collection
of information is necessary for the proper performance of FDA's
functions, including whether the information will have practical
utility; (2) the accuracy of FDA's estimate of the burden of the
proposed collection of information, including the validity of the
methodology and assumptions used; (3) ways to enhance the quality,
utility, and clarity of the information to be collected; and (4) ways
to minimize the burden of the collection of information on respondents,
including through the use of automated collection techniques, when
appropriate, and other forms of information technology.

Reporting Associated With Designated New Animal Drugs for Minor Use and
Minor Species--21 CFR Part 516

OMB Control Number 0910-0605--Extension

    The MUMS Act (Pub. L. 108-282) amended the Federal Food, Drug, and
Cosmetic Act to authorize FDA to establish new regulatory procedures
intended to make more medications legally available to veterinarians
and animal owners for the treatment of minor animal species as well as
uncommon diseases in major animal species. This legislation provides
incentives designed to help pharmaceutical companies overcome the
financial burdens they face in providing limited-demand animal

drugs. These incentives are only available to sponsors whose drugs are
``MUMS-designated'' by FDA. Minor use drugs are drugs for use in major
species (e.g., cattle, horses, swine, chickens, turkeys, dogs, and
cats) that are needed for diseases that occur in only a small number of
animals either because they occur infrequently or in limited geographic
areas. Minor species are all animals other than the major species
(e.g., zoo animals, ornamental fish, parrots, ferrets, and guinea
pigs). Some animals of agricultural importance are also minor species.
These include animals such as sheep, goats, catfish, and honeybees.
Participation in the MUMS program is completely optional for drug
sponsors, so the associated reporting only applies to those sponsors
who request and are subsequently granted ``MUMS designation.''
    Our regulations in 21 CFR part 516 specify the criteria and
procedures for requesting MUMS designation as well as the annual
reporting requirements for MUMS designees. Section 516.20 provides
requirements on the content and format of a request for MUMS-drug
designation; Sec.  516.26 provides requirements for amending MUMS-drug
designation; Sec.  516.27 provides for change in sponsorship of MUMS-
drug designation; Sec.  516.29 provides for termination of MUMS-drug
designation; Sec.  516.30 contains the requirements for annual reports
from sponsor(s) of MUMS-designated drugs; and Sec.  516.36 sets forth
consequences for insufficient quantities of MUMS-designated drugs.
    Description of Respondents: The respondents to this information
collection are pharmaceutical companies that sponsor new animal drugs.
    FDA estimates the burden of this collection of information as
follows:

                                      Table 1--Estimated Annual Reporting 1
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                                                     Number of
         21 CFR section              Number of     responses per   Total annual   Average burden    Total hours
                                    respondents     respondent       responses     per response
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516.20; content and format of                 15               5              75              16           1,200
 MUMS request...................
516.26; requirements for                       3               1               3               2               6
 amending MUMS designation......
516.27; change in sponsorship...               1               1               1               1               1
516.29; termination of MUMS                    2               1               2               1               2
 designation....................
516.30; requirements of annual                15               5              75               2             150
 reports........................
516.36; insufficient quantities.               1               1               1               3               3
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    Total.......................  ..............  ..............  ..............  ..............           1,362
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\1\ There are no capital costs or operating and maintenance costs associated with this collection of
  information.

    The burden estimate for this reporting requirement was derived in
our Office of Minor Use and Minor Species Animal Drug Development by
extrapolating the investigational new animal drug/new animal drug
application reporting requirements for similar actions by this same
segment of the regulated industry and from previous interactions with
the minor use/minor species community, and has not changed since the
last OMB approval.

    Dated: June 6, 2019.
Lowell J. Schiller,
Principal Associate Commissioner for Policy.
[FR Doc. 2019-12316 Filed 6-11-19; 8:45 am]
 BILLING CODE 4164-01-P