81 FR 145 - Airworthiness Directives; Piper Aircraft, Inc.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 2 (January 5, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 2 (January 5, 2016)
| Page Range | 145-147 | |
| FR Document | 2015-32907 |
[Federal Register Volume 81, Number 2 (Tuesday, January 5, 2016)] [Rules and Regulations] [Pages 145-147] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-32907] ======================================================================== Rules and Regulations Federal Register ________________________________________________________________________ This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510. The Code of Federal Regulations is sold by the Superintendent of Documents. Prices of new books are listed in the first FEDERAL REGISTER issue of each week. ======================================================================== Federal Register / Vol. 81, No. 2 / Tuesday, January 5, 2016 / Rules and Regulations [[Page 145]] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-8311; Directorate Identifier 2015-CE-039-AD; Amendment 39-18356; AD 2015-26-08] RIN 2120-AA64 Airworthiness Directives; Piper Aircraft, Inc. AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain Piper Aircraft, Inc. Model PA-44-180 and PA-44-180T airplanes. This AD requires an inspection and, if necessary, modification of the emergency gear extension cable. This AD was prompted by a report of a misrouted emergency gear extension cable. We are issuing this AD to correct the unsafe condition on these products. DATES: This AD is effective January 20, 2016. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 20, 2016. We must receive comments on this AD by February 19, 2016. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. Fax: 202-493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. Hand Delivery: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this final rule, contact Piper Aircraft, Inc., Customer Service, 2926 Piper Drive, Vero Beach, Florida 32960; telephone: (877) 879-0275; fax: none; email: [email protected]; Internet: www.piper.com. You may review the referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. It is also available on the Internet at http://www.regulations.gov by searching for locating Docket No. FAA-2015-4085. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015- 8311; or in person at the Docket Management Facility 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 Office (phone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Hector Hernandez, Aerospace Engineer, FAA, Atlanta Aircraft Certification Office, 1701 Columbia Avenue, College Park, Georgia 30337; telephone: (404) 474-5587; fax: (404) 474- 5606; email: [email protected]. SUPPLEMENTARY INFORMATION: Discussion The FAA has received recent reports of misrouted emergency gear extension cables on Piper Models PA-44-180 and PA-44-180T airplanes. This condition spans many years beginning in 2007 where one of the airplanes experienced the left-side copilot rudder pedal snagging on the emergency landing gear extension cable during taxi maneuvers. Piper Modification Kit 884333 (Piper Service Bulletin No. 1188, dated April 14, 2008) provides the parts and instructions to reroute the cable away from the pedal for airplanes in service and a production change was made to duplicate the kit configuration. In 2009, there was a quality escape on the production aircraft (after issuance of SB 1188), which was addressed with Piper Service Bulletin No. 1213, dated March 24, 2010. Recently, there has been another quality escape reported of the cable being routed incorrectly, resulting in the issuance of Piper Service Bulletin 1213A, dated October 23, 2015 to more fully address the incorrect routing of the emergency gear extension cables. Although the incidents occurred on the ground, the airworthiness concern is the potential for this rudder restriction to occur in flight at high angles of rudder deflection. The FAA believes that a majority of the airplanes have already incorporated Service Bulletin 1188 and Service Bulletin 1213. However, the only way to mandate its incorporation is through AD action. In addition, the FAA believes that a large percentage of the airplanes that were manufactured after SB 1213 was issued could have the emergency gear extension cable routed incorrectly because the P-clamp that secures the cable could be installed on the inboard bolt just as easily as the outboard bolt (the type design configuration). Piper is establishing a very robust assembly/inspection procedure going forward to ensure that the quality escape issue does not reoccur. The FAA has determined that this condition can be addressed by requiring: The modification in Service Bulletin 1188 for all Models PA-44-180 and PA-44-180T airplanes manufactured prior to April 14, 2008 (the date of SB 1188); and The inspection of the emergency gear inspection cable for correct routing of all Model PA-44-180 airplanes manufactured after April 14, 2008 (the date of SB 1188) following SB 1213A, dated October 23, 2015. This condition, if not corrected, could result in restriction of the rudder movement at high angles of rudder deflection with consequent loss of control. We are issuing this AD to correct the unsafe condition on these products. [[Page 146]] Related Service Information Under 1 CFR Part 51 We reviewed Piper Aircraft, Inc. Service Bulletin No. 1213A, dated October 23, 2015. The service information describes procedures for inspection of the routing and security of the emergency gear extension cable and, if necessary, instructions to reroute the emergency gear extension cable. Piper considers compliance with this service bulletin mandatory. We reviewed Piper Aircraft, Inc. Service Bulletin No. 1188, dated April 14, 2008. The service information describes procedures to reroute and restrain the emergency gear extension cable. Piper considers compliance with this service bulletin mandatory. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section. FAA's Determination We are issuing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the same type design. AD Requirements This AD requires accomplishing the actions specified in the service information described previously. FAA's Justification and Determination of the Effective Date An unsafe condition exists that requires the immediate adoption of this AD. The FAA has found that the risk to the flying public justifies waiving notice and comment prior to adoption of this rule because if the emergency gear extension cable is left routed incorrectly, it could allow the copilot's left rudder pedal to become entangled with the cable, resulting in a restriction of rudder movement at high angles of rudder deflection with consequent loss of control. Therefore, we find that notice and opportunity for prior public comment are impracticable and that good cause exists for making this amendment effective in less than 30 days. Comments Invited This AD is a final rule that involves requirements affecting flight safety and was not preceded by notice and an opportunity for public comment. However, we invite you to send any written data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include the docket number FAA-2015-8311 and Directorate Identifier 2015-CE-039-AD at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this AD because of those comments. We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD. Costs of Compliance We estimate that this AD affects 415 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Inspect the emergency gear .5 work-hour x $85 Not applicable..... $42.50 (Estimated 35 extension cable for proper per hour = $42.50. airplanes) routing. $1,487.75. Install Piper emergency gear 2 work-hours x $85 $21................ $191 (Estimated 380 extension modification kit. per hour = $170. airplanes) $72,580. ---------------------------------------------------------------------------------------------------------------- We estimate the following costs to do any necessary replacements that would be required based on the either the results of the inspection or other requirements. We have no way of determining the number of aircraft that might need this replacement: On-Condition Costs ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- Reroute the emergency gear extension cable... 2 work-hours x $85 per hour = $21 $191 $170. ---------------------------------------------------------------------------------------------------------------- According to the manufacturer, some of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected individuals. We do not control warranty coverage for affected individuals. As a result, we have included all costs in our cost estimate. 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 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 [[Page 147]] 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), (3) Will not affect intrastate aviation in Alaska, and (4) 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. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA 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 (AD): 2015-26-08: Amendment 39-18356; Docket No. FAA-2015-8311; Directorate Identifier 2015-CE-039-AD. (a) Effective Date This AD is effective January 20, 2016. (b) Affected ADs None. (c) Applicability This AD applies to Piper Aircraft, Inc. Model PA-44-180 Seminole airplanes, serial numbers (S/Ns) 44-7995001 through 44-8195026, 4495001 through 4496377, 4496379, 4496380, and 4496384 through 4496386; and Piper Aircraft, Inc. Model PA-44-180T Seminole airplanes, S/Ns 44-8107001 through 44-8207020, certificated in any category. (d) Subject Joint Aircraft System Component (JASC)/Air Transport Association (ATA) of America Code 2720, Rudder Control System. (e) Unsafe Condition This AD was prompted by a report of a misrouted emergency gear extension cable. We are issuing this AD to require an inspection and, if necessary, modification of the emergency gear extension cable. We are issuing this AD to correct the unsafe condition on these products. (f) Compliance Comply with paragraphs (g)(1) through (g)(2) including all subparagraph's of this AD within the compliance times specified, unless already done. (g) Actions (1) For Piper Model PA-44-180 Seminole airplanes serial numbers (S/N) 4496245 through 4496377, 4496379, 4496380, and 4496384 through 4496386: Within 30 days after January 20, 2016 (the effective date of this AD), inspect the emergency gear extension cable for proper routing and appropriate attachment of the cable to the rudder pedal assembly following the Part 1 instructions in Piper Aircraft, Inc. Service Bulletin (SB) No. 1213A, dated October 23, 2015. (i) If the inspection required in paragraph (g)(1) of this AD reveals a misrouted cable, before further flight, correct the emergency gear extension cable following the Part 2 instructions in Piper Aircraft, Inc. SB No. 1213A, dated October 23, 2015. (ii) If the inspection required in paragraph (g)(1) of this AD reveals a correct installation following the Part 1 instructions in Piper Aircraft, Inc. SB No. 1213A, dated October 23, 2015, no further action is required. (2) For Piper Model PA-44-180 Seminole airplanes SNs 44-7995001 through 44-8195026, 4495001 through 4496244; and Piper Model PA-44- 180T Seminole airplanes, SNs 44-8107001 through 44-8207020: Within 30 days after January 20, 2016 (the effective date of this AD), install the Piper emergency gear extension cable modification kit, part number 88433-002, following the instructions in Piper Aircraft, Inc. SB No. 1188, dated April 14, 2008. (h) Alternative Methods of Compliance (AMOCs) (1) The Manager, Atlanta ACO, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the ACO, send it to the attention of the person identified in paragraph (k) of this AD. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (i) Related Information For more information about this AD, contact Hector Hernandez, Aerospace Engineer, FAA, Atlanta Aircraft Certification Office, 1701 Columbia Avenue, College Park, Georgia 30337; telephone: (404) 474- 5587; fax: (404) 474-5606; email: [email protected]. (j) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) Piper Aircraft, Inc. Service Bulletin No. 1188, dated April 14, 2008. (ii) Piper Aircraft, Inc. Service Bulletin No. 1213A, dated October 23, 2015. (3) For Piper Aircraft, Inc. service information identified in this AD, contact Piper Aircraft, Inc., Customer Service, 2926 Piper Drive, Vero Beach, Florida 32960; telephone: (877) 879-0275; fax: none; email: [email protected]; Internet: www.piper.com. (4) You may review the referenced service information at the FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Kansas City, Missouri, on December 23, 2015. Pat Mullen, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-32907 Filed 1-4-16; 8:45 am] BILLING CODE 4910-13-P
![145
Rules and Regulations Federal Register
Vol. 81, No. 2
Tuesday, January 5, 2016
This section of the FEDERAL REGISTER • Hand Delivery: U.S. Department of instructions to reroute the cable away
contains regulatory documents having general Transportation, Docket Operations, M– from the pedal for airplanes in service
applicability and legal effect, most of which 30, West Building Ground Floor, Room and a production change was made to
are keyed to and codified in the Code of W12–140, 1200 New Jersey Avenue SE., duplicate the kit configuration.
Federal Regulations, which is published under Washington, DC 20590, between 9 a.m.
50 titles pursuant to 44 U.S.C. 1510. In 2009, there was a quality escape on
and 5 p.m., Monday through Friday, the production aircraft (after issuance of
The Code of Federal Regulations is sold by except Federal holidays. SB 1188), which was addressed with
the Superintendent of Documents. Prices of For service information identified in
Piper Service Bulletin No. 1213, dated
new books are listed in the first FEDERAL this final rule, contact Piper Aircraft,
March 24, 2010. Recently, there has
REGISTER issue of each week. Inc., Customer Service, 2926 Piper
been another quality escape reported of
Drive, Vero Beach, Florida 32960;
the cable being routed incorrectly,
telephone: (877) 879–0275; fax: none;
DEPARTMENT OF TRANSPORTATION email: customer.service@piper.com; resulting in the issuance of Piper
Internet: www.piper.com. You may Service Bulletin 1213A, dated October
Federal Aviation Administration review the referenced service 23, 2015 to more fully address the
information at the FAA, Small Airplane incorrect routing of the emergency gear
14 CFR Part 39 Directorate, 901 Locust, Kansas City, extension cables.
[Docket No. FAA–2015–8311; Directorate Missouri 64106. For information on the Although the incidents occurred on
Identifier 2015–CE–039–AD; Amendment availability of this material at the FAA, the ground, the airworthiness concern is
39–18356; AD 2015–26–08] call (816) 329–4148. It is also available the potential for this rudder restriction
RIN 2120–AA64 on the Internet at http:// to occur in flight at high angles of
www.regulations.gov by searching for rudder deflection.
Airworthiness Directives; Piper locating Docket No. FAA–2015–4085. The FAA believes that a majority of
Aircraft, Inc. Examining the AD Docket the airplanes have already incorporated
AGENCY: Federal Aviation Service Bulletin 1188 and Service
You may examine the AD docket on
Administration (FAA), DOT. the Internet at http:// Bulletin 1213. However, the only way to
www.regulations.gov by searching for mandate its incorporation is through AD
ACTION: Final rule; request for
and locating Docket No. FAA–2015– action. In addition, the FAA believes
comments.
8311; or in person at the Docket that a large percentage of the airplanes
SUMMARY: We are adopting a new Management Facility between 9 a.m. that were manufactured after SB 1213
airworthiness directive (AD) for certain and 5 p.m., Monday through Friday, was issued could have the emergency
Piper Aircraft, Inc. Model PA–44–180 except Federal holidays. The AD docket gear extension cable routed incorrectly
and PA–44–180T airplanes. This AD contains this AD, the regulatory because the P-clamp that secures the
requires an inspection and, if necessary, evaluation, any comments received, and cable could be installed on the inboard
modification of the emergency gear other information. The street address for bolt just as easily as the outboard bolt
extension cable. This AD was prompted the Docket Office (phone: 800–647– (the type design configuration).
by a report of a misrouted emergency 5527) is in the ADDRESSES section. Piper is establishing a very robust
gear extension cable. We are issuing this Comments will be available in the AD assembly/inspection procedure going
AD to correct the unsafe condition on docket shortly after receipt. forward to ensure that the quality
these products. FOR FURTHER INFORMATION CONTACT: escape issue does not reoccur. The FAA
DATES: This AD is effective January 20, Hector Hernandez, Aerospace Engineer, has determined that this condition can
2016. FAA, Atlanta Aircraft Certification be addressed by requiring:
The Director of the Federal Register Office, 1701 Columbia Avenue, College • The modification in Service
approved the incorporation by reference Park, Georgia 30337; telephone: (404) Bulletin 1188 for all Models PA–44–180
of a certain publication listed in this AD 474–5587; fax: (404) 474–5606; email: and PA–44–180T airplanes
as of January 20, 2016. hector.hernandez@faa.gov. manufactured prior to April 14, 2008
We must receive comments on this SUPPLEMENTARY INFORMATION: (the date of SB 1188); and
AD by February 19, 2016.
ADDRESSES: You may send comments, Discussion • The inspection of the emergency
using the procedures found in 14 CFR The FAA has received recent reports gear inspection cable for correct routing
11.43 and 11.45, by any of the following of misrouted emergency gear extension of all Model PA–44–180 airplanes
methods: cables on Piper Models PA–44–180 and manufactured after April 14, 2008 (the
• Federal eRulemaking Portal: Go to PA–44–180T airplanes. This condition date of SB 1188) following SB 1213A,
dated October 23, 2015.
asabaliauskas on DSK5VPTVN1PROD with RULES
http://www.regulations.gov. Follow the spans many years beginning in 2007
instructions for submitting comments. where one of the airplanes experienced This condition, if not corrected, could
• Fax: 202–493–2251. the left-side copilot rudder pedal result in restriction of the rudder
• Mail: U.S. Department of snagging on the emergency landing gear movement at high angles of rudder
Transportation, Docket Operations, M– extension cable during taxi maneuvers. deflection with consequent loss of
30, West Building Ground Floor, Room Piper Modification Kit 884333 (Piper control. We are issuing this AD to
W12–140, 1200 New Jersey Avenue SE., Service Bulletin No. 1188, dated April correct the unsafe condition on these
Washington, DC 20590. 14, 2008) provides the parts and products.
VerDate Sep<11>2014 18:31 Jan 04, 2016 Jkt 238001 PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 E:\FR\FM\05JAR1.SGM 05JAR1](https://thefederalregister.org/doc/81_FR_147/page/1.svg)
![Federal Register / Vol. 81, No. 2 / Tuesday, January 5, 2016 / Rules and Regulations 147
responsibilities among the various (f) Compliance (2) You must use this service information
levels of government. Comply with paragraphs (g)(1) through as applicable to do the actions required by
For the reasons discussed above, I (g)(2) including all subparagraph’s of this AD this AD, unless the AD specifies otherwise.
certify that this AD: within the compliance times specified, (i) Piper Aircraft, Inc. Service Bulletin No.
(1) Is not a ‘‘significant regulatory 1188, dated April 14, 2008.
unless already done.
(ii) Piper Aircraft, Inc. Service Bulletin No.
action’’ under Executive Order 12866, 1213A, dated October 23, 2015.
(g) Actions
(2) Is not a ‘‘significant rule’’ under (3) For Piper Aircraft, Inc. service
DOT Regulatory Policies and Procedures (1) For Piper Model PA–44–180 Seminole
airplanes serial numbers (S/N) 4496245 information identified in this AD, contact
(44 FR 11034, February 26, 1979), Piper Aircraft, Inc., Customer Service, 2926
(3) Will not affect intrastate aviation through 4496377, 4496379, 4496380, and
Piper Drive, Vero Beach, Florida 32960;
4496384 through 4496386: Within 30 days
in Alaska, and telephone: (877) 879–0275; fax: none; email:
after January 20, 2016 (the effective date of
(4) Will not have a significant customer.service@piper.com; Internet:
this AD), inspect the emergency gear
economic impact, positive or negative, extension cable for proper routing and
www.piper.com.
on a substantial number of small entities (4) You may review the referenced service
appropriate attachment of the cable to the
under the criteria of the Regulatory information at the FAA, Small Airplane
rudder pedal assembly following the Part 1
Flexibility Act. Directorate, 901 Locust, Kansas City,
instructions in Piper Aircraft, Inc. Service
Missouri 64106. For information on the
Bulletin (SB) No. 1213A, dated October 23,
List of Subjects in 14 CFR Part 39 availability of this material at the FAA, call
2015. (816) 329–4148.
Air transportation, Aircraft, Aviation (i) If the inspection required in paragraph (5) You may view this service information
safety, Incorporation by reference, (g)(1) of this AD reveals a misrouted cable, that is incorporated by reference at the
Safety. before further flight, correct the emergency National Archives and Records
gear extension cable following the Part 2 Administration (NARA). For information on
Adoption of the Amendment instructions in Piper Aircraft, Inc. SB No. the availability of this material at NARA, call
Accordingly, under the authority 1213A, dated October 23, 2015. 202–741–6030, or go to: http://
delegated to me by the Administrator, (ii) If the inspection required in paragraph www.archives.gov/federal-register/cfr/ibr-
the FAA amends 14 CFR part 39 as (g)(1) of this AD reveals a correct installation locations.html.
following the Part 1 instructions in Piper
follows: Aircraft, Inc. SB No. 1213A, dated October Issued in Kansas City, Missouri, on
23, 2015, no further action is required. December 23, 2015.
PART 39—AIRWORTHINESS
(2) For Piper Model PA–44–180 Seminole Pat Mullen,
DIRECTIVES airplanes SNs 44–7995001 through 44– Acting Manager, Small Airplane Directorate,
8195026, 4495001 through 4496244; and Aircraft Certification Service.
■ 1. The authority citation for part 39
Piper Model PA–44–180T Seminole
continues to read as follows: airplanes, SNs 44–8107001 through 44–
[FR Doc. 2015–32907 Filed 1–4–16; 8:45 am]
BILLING CODE 4910–13–P
Authority: 49 U.S.C. 106(g), 40113, 44701. 8207020: Within 30 days after January 20,
2016 (the effective date of this AD), install
§ 39.13 [Amended] the Piper emergency gear extension cable
■ 2. The FAA amends § 39.13 by adding modification kit, part number 88433–002, DEPARTMENT OF TRANSPORTATION
the following new airworthiness following the instructions in Piper Aircraft,
Inc. SB No. 1188, dated April 14, 2008. Federal Aviation Administration
directive (AD):
2015–26–08: Amendment 39–18356; Docket (h) Alternative Methods of Compliance 14 CFR Part 39
No. FAA–2015–8311; Directorate (AMOCs)
Identifier 2015–CE–039–AD. (1) The Manager, Atlanta ACO, FAA, has [Docket No. FAA–2014–0335; Directorate
(a) Effective Date the authority to approve AMOCs for this AD, Identifier 2013–SW–021–AD; Amendment
if requested using the procedures found in 14 39–18358; AD 2015–26–10]
This AD is effective January 20, 2016. CFR 39.19. In accordance with 14 CFR 39.19,
(b) Affected ADs send your request to your principal inspector RIN 2120–AA64
or local Flight Standards District Office, as
None. appropriate. If sending information directly Airworthiness Directives; Sikorsky
(c) Applicability to the manager of the ACO, send it to the Aircraft Corporation Helicopters
This AD applies to Piper Aircraft, Inc. attention of the person identified in
Model PA–44–180 Seminole airplanes, serial paragraph (k) of this AD. AGENCY: Federal Aviation
numbers (S/Ns) 44–7995001 through 44– (2) Before using any approved AMOC, Administration (FAA), DOT.
8195026, 4495001 through 4496377, notify your appropriate principal inspector, ACTION: Final rule.
4496379, 4496380, and 4496384 through or lacking a principal inspector, the manager
4496386; and Piper Aircraft, Inc. Model PA– of the local flight standards district office/ SUMMARY: We are adopting a new
44–180T Seminole airplanes, S/Ns 44– certificate holding district office. airworthiness directive (AD) for certain
8107001 through 44–8207020, certificated in (i) Related Information Sikorsky Aircraft Corporation (Sikorsky)
any category. Model S–76A, S–76B, and S–76C
For more information about this AD,
(d) Subject contact Hector Hernandez, Aerospace helicopters. This AD requires inspecting
Joint Aircraft System Component (JASC)/ Engineer, FAA, Atlanta Aircraft Certification the main gearbox (MGB) lower housing
Air Transport Association (ATA) of America Office, 1701 Columbia Avenue, College Park, jet bores for leaks, paint or caulk
Code 2720, Rudder Control System. Georgia 30337; telephone: (404) 474–5587; blistering, and liner protrusion. This AD
asabaliauskas on DSK5VPTVN1PROD with RULES
fax: (404) 474–5606; email: was prompted by several reports of
(e) Unsafe Condition hector.hernandez@faa.gov. MGB low oil pressure warnings which
This AD was prompted by a report of a
(j) Material Incorporated by Reference were determined to be the result of
misrouted emergency gear extension cable.
We are issuing this AD to require an (1) The Director of the Federal Register unsecured jet bore liners that had
inspection and, if necessary, modification of approved the incorporation by reference protruded. The actions are intended to
the emergency gear extension cable. We are (IBR) of the service information listed in this prevent failure of the MGB from loss of
issuing this AD to correct the unsafe paragraph under 5 U.S.C. 552(a) and 1 CFR oil, which could result in subsequent
condition on these products. part 51. loss of control of the helicopter.
VerDate Sep<11>2014 18:31 Jan 04, 2016 Jkt 238001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\05JAR1.SGM 05JAR1](https://thefederalregister.org/doc/81_FR_147/page/3.svg)
Document Created: 2016-01-05 01:46:47
Document Modified: 2016-01-05 01:46:47
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final rule; request for comments. | |
| Dates | This AD is effective January 20, 2016. | |
| Contact | Hector Hernandez, Aerospace Engineer, FAA, Atlanta Aircraft Certification Office, 1701 Columbia Avenue, College Park, Georgia 30337; telephone: (404) 474-5587; fax: (404) 474- 5606; email: [email protected] | |
| FR Citation | 81 FR 145 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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