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2016-25-25 |
BAE SYSTEMS (OPERATIONS) LIMITED AIRPLANES:
(
c o r r e c t i o n )
Amendment 39-18751; Docket No. FAA-2016-0457; Directorate Identifier 2015-NM-084-AD. |
TDATA NOTE: The Product Identification line of the regulatory text con-
tained an error, incorrectly identifying Bombardier as the
product manufacturer, but should have identified BAE Systems
(Operations) Limited. Tdata made the correction upon the
initial release.
(a) EFFECTIVE DATE
This AD is effective February 7, 2017.
(b) AFFECTED ADS
This AD replaces AD 2012-11-15, Amendment 39-17079 (77 FR 36127, June
18, 2012) ("AD 2012-11-15").
(c) APPLICABILITY
This AD applies to BAE (Operations) Limited Model 4101 airplanes,
certificated in any category, all models and all serial numbers.
(d) SUBJECT
Air Transport Association (ATA) of America Code 57, Wings.
(e) REASON
This AD was prompted by new reports of cracking found in the wing rear
spar and technical analysis results, which confirmed that the crack
initiation and propagation are due to fatigue, with no indication of
any other crack initiation mechanism (e.g., stress corrosion). We are
issuing this AD to detect and correct cracking in the wing rear spar,
which could propagate to a critical length, possibly affecting the
structural integrity of the area and resulting in a fuel tank rupture,
with consequent damage to the airplane and possible injury to its
occupants.
(f) COMPLIANCE
Comply with this AD within the compliance times specified, unless al-
ready done.
(g) REPETITIVE INSPECTIONS AND REPAIR
Within 30 days after the effective date of this AD, or within 1,600
flight cycles since the most recent detailed inspection was done as
specified in BAE Systems Alert Service Bulletin J41-A57-029, whichever
occurs later: Do a detailed inspection for cracks, corrosion, and
other defects (defects include scratches, dents, holes, damage to
fastener holes, or damage to surface protection and finish) of the
rear face of the wing rear spars, in accordance with the
Accomplishment Instructions of BAE Systems Alert Service Bulletin J41
-A57-029, Revision 3, dated April 8, 2014. Repeat the inspection
thereafter at intervals not to exceed 1,600 flight cycles.
(1) If any cracking, corrosion, or other defect is found within the
criteria defined in Chapter 57, Wings, of the Jetstream Series 4100
Structural Repair Manual (SRM), Volume 1, Publication Ref. No.
(Transmittal No.) SA 4-4100/SRM/400, Revision 32, dated October 15,
2014 ("Chapter 57 of the SRM"): Before further flight, repair the
affected area, in accordance with the repair instructions of Chapter
57 of the SRM.
(2) If any cracking, corrosion, or other defect is found exceeding the
criteria defined in Chapter 57 of the SRM: Before further flight,
repair using a method approved by the Manager, International Branch,
ANM-116, Transport Airplane Directorate, FAA; or the European Aviation
Safety Agency (EASA); or BAE Systems (Operations) Limited's EASA
Design Organization Approval (DOA).
(h) REPAIR DOES NOT CONSTITUTE TERMINATING ACTION EXCEPT FOR CERTAIN RE-
PAIRS
Accomplishment of a repair as required by paragraphs (g)(1) and (g)(2)
of this AD, does not constitute terminating action for the repetitive
inspections required by paragraph (g) of this AD, unless the approved
repair required by paragraph (g)(2) of this AD states otherwise (e.g.,
the approved repair states the repair terminates the inspections for
the repaired area only).
(i) OTHER FAA AD PROVISIONS
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, International
Branch, ANM-116, Transport Airplane Directorate, 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 International Branch, send it to ATTN: Todd Thompson,
Aerospace Engineer, International Branch, ANM-116, Transport Airplane
Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356;
telephone 425-227-1175; fax 425-227-1149. Information may be emailed
to: 9-ANM-116-AMOC-REQUESTS@faa.gov. 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. The AMOC approval letter
must specifically reference this AD.
(2) Contacting the Manufacturer: As of the effective date of this AD, for
any requirement in this AD to obtain corrective actions from a
manufacturer, the action must be accomplished using a method approved
by the Manager, International Branch, ANM-116, Transport Airplane
Directorate, FAA; or the EASA; or BAE Systems (Operations) Limited's
EASA DOA. If approved by the DOA, the approval must include the DOA
-authorized signature.
(j) RELATED INFORMATION
Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA
Airworthiness Directive 2015-0100, dated June 3, 2015, for related
information. This MCAI may be found in the AD docket on the Internet
at http://www.regulations.gov by searching for and locating Docket No.
FAA-2016-0457.
(k) 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 this AD specifies otherwise.
(i) BAE Systems Alert Service Bulletin J41-A57-029, Revision 3 dated April
8, 2014.
(ii) Chapter 57, Wings, of the BAE Systems (Operations) Limited Jetstream
Series 4100 Structural Repair Manual, Volume 1, Publication Ref. No.
(Transmittal No.) SA 4-4100/SRM/400, Revision 32, dated October 15,
2014.
(3) For service information identified in this AD, contact BAE Systems
(Operations) Limited, Customer Information Department, Prestwick
International Airport, Ayrshire, KA9 2RW, Scotland, United Kingdom;
telephone +44 1292 675207; fax +44 1292 675704; email RApublications@
baesystems.com; Internet http://www.baesystems.com/Businesses/Regional
Aircraft/index.htm.
(4) You may view this service information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the
availability of this material at the FAA, call 425-227-1221.
(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 Renton, Washington, on January 23, 2017. Dionne Palermo, Acting
Manager, Transport Airplane Directorate, Aircraft Certification Service.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer, Inter-
national Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind
Avenue SW, Renton, WA 98057-3356; telephone 425-227-1175; fax 425-227-1149
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