[Federal Register Volume 81, Number 2 (Tuesday, January 5, 2016)]
[Rules and Regulations]
[Pages 145-147]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[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