82 FR 14601 - Airworthiness Directives; BAE Systems (Operations) Limited Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 82, Issue 54 (March 22, 2017)

Page Range		14601-14602
FR Document		2017-05163

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to all BAE Systems (Operations) Limited Model 4101 airplanes. As published, the Product Identification line of the regulatory text contains an error. This document corrects that error. In all other respects, the original document remains the same.

Federal Register, Volume 82 Issue 54 (Wednesday, March 22, 2017)

[Federal Register Volume 82, Number 54 (Wednesday, March 22, 2017)]
[Rules and Regulations]
[Pages 14601-14602]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2017-05163]



========================================================================
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. 

========================================================================


Federal Register / Vol. 82, No. 54 / Wednesday, March 22, 2017 / 
Rules and Regulations

[[Page 14601]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-0457; Directorate Identifier 2015-NM-084-AD; 
Amendment 39-18751; AD 2016-25-25]
RIN 2120-AA64


Airworthiness Directives; BAE Systems (Operations) Limited 
Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

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

SUMMARY: The FAA is correcting an airworthiness directive (AD) that 
published in the Federal Register. That AD applies to all BAE Systems 
(Operations) Limited Model 4101 airplanes. As published, the Product 
Identification line of the regulatory text contains an error. This 
document corrects that error. In all other respects, the original 
document remains the same.

DATES: This correction is effective March 22, 2017.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of February 7, 
2017 (82 FR 7, January 3, 2017).

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov; 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 address for the 
Docket Office (phone: 800-647-5527) is Docket Management Facility, U.S. 
Department of Transportation, Docket Operations, M-30, West Building 
Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 
20590.

FOR FURTHER INFORMATION CONTACT: 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.

SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 2016-25-25, 
Amendment 39-18751 (82 FR 7, January 3, 2017) (``AD 2016-25-25''), 
currently requires repetitive detailed inspections for cracks, 
corrosion, and other defects of the rear face of the wing rear spar, 
and repair if necessary, for all BAE Systems (Operations) Limited Model 
4101 airplanes.
    As published, the Product Identification line of the regulatory 
text contains an error. The Product Identification line incorrectly 
identifies Bombardier as the product manufacturer, but should have 
identified BAE Systems (Operations) Limited. All other references to 
the product manufacturer appear correctly as BAE Systems (Operations) 
Limited throughout the preamble and regulatory text of AD 2016-25-25.
    No other part of the preamble or regulatory information has been 
changed; therefore, only the changed portion of the final rule is being 
published in the Federal Register.
    The effective date of this AD remains February 7, 2017.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Correction

    Accordingly, pursuant to the authority delegated to me by the 
Administrator, the Federal Aviation Administration amends part 39 of 
the Federal Aviation Regulations (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  [Corrected]

0
2. The FAA amends Sec.  39.13 by removing Amendment 39-17079 (77 FR 
36127, June 18, 2012), and adding the following new airworthiness 
directive (AD):

2016-25-25 BAE Systems (Operations) Limited: Amendment 39-18751; 
Docket No. FAA-2016-0457; Directorate Identifier 2015-NM-084-AD.

(a) Effective Date

    This airworthiness directive (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 Systems (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 already done.

(g) Repetitive Inspections and Repair

    Within 30 days after February 7, 2017 (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.

[[Page 14602]]

    (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 
Repairs

    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: [email protected]. 
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 February 7, 2017 (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 
[email protected]; Internet http://www.baesystems.com/Businesses/RegionalAircraft/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.
[FR Doc. 2017-05163 Filed 3-21-17; 8:45 am]
 BILLING CODE 4910-13-P

14601

Rules and Regulations Federal Register
Vol. 82, No. 54

Wednesday, March 22, 2017

This section of the FEDERAL REGISTER FOR FURTHER INFORMATION CONTACT: 2016–25–25 BAE Systems (Operations)
contains regulatory documents having general Todd Thompson, Aerospace Engineer, Limited: Amendment 39–18751; Docket
applicability and legal effect, most of which International Branch, ANM–116, No. FAA–2016–0457; Directorate
are keyed to and codified in the Code of Identifier 2015–NM–084–AD.
Transport Airplane Directorate, FAA,
Federal Regulations, which is published under 1601 Lind Avenue SW., Renton, WA (a) Effective Date
50 titles pursuant to 44 U.S.C. 1510.
98057–3356; telephone 425–227–1175; This airworthiness directive (AD) is
The Code of Federal Regulations is sold by fax 425–227–1149. effective February 7, 2017.
the Superintendent of Documents. SUPPLEMENTARY INFORMATION: (b) Affected ADs
Airworthiness Directive (AD) 2016–25–
This AD replaces AD 2012–11–15,
25, Amendment 39–18751 (82 FR 7, Amendment 39–17079 (77 FR 36127, June
DEPARTMENT OF TRANSPORTATION January 3, 2017) (‘‘AD 2016–25–25’’), 18, 2012) (‘‘AD 2012–11–15’’).
currently requires repetitive detailed
Federal Aviation Administration inspections for cracks, corrosion, and (c) Applicability
other defects of the rear face of the wing This AD applies to BAE Systems
14 CFR Part 39 rear spar, and repair if necessary, for all (Operations) Limited Model 4101 airplanes,
BAE Systems (Operations) Limited certificated in any category, all models and
[Docket No. FAA–2016–0457; Directorate
all serial numbers.
Identifier 2015–NM–084–AD; Amendment Model 4101 airplanes.
39–18751; AD 2016–25–25] As published, the Product (d) Subject
RIN 2120–AA64
Identification line of the regulatory text Air Transport Association (ATA) of
contains an error. The Product America Code 57, Wings.
Airworthiness Directives; BAE Identification line incorrectly identifies (e) Reason
Systems (Operations) Limited Bombardier as the product
manufacturer, but should have This AD was prompted by new reports of
Airplanes cracking found in the wing rear spar and
identified BAE Systems (Operations) technical analysis results, which confirmed
AGENCY: Federal Aviation Limited. All other references to the that the crack initiation and propagation are
Administration (FAA), DOT. product manufacturer appear correctly due to fatigue, with no indication of any
ACTION: Final rule; correction. as BAE Systems (Operations) Limited other crack initiation mechanism (e.g., stress
throughout the preamble and regulatory corrosion). We are issuing this AD to detect
SUMMARY: The FAA is correcting an text of AD 2016–25–25. and correct cracking in the wing rear spar,
airworthiness directive (AD) that No other part of the preamble or which could propagate to a critical length,
published in the Federal Register. That regulatory information has been possibly affecting the structural integrity of
AD applies to all BAE Systems the area and resulting in a fuel tank rupture,
changed; therefore, only the changed with consequent damage to the airplane and
(Operations) Limited Model 4101 portion of the final rule is being possible injury to its occupants.
airplanes. As published, the Product published in the Federal Register.
Identification line of the regulatory text The effective date of this AD remains (f) Compliance
contains an error. This document February 7, 2017. Comply with this AD within the
corrects that error. In all other respects, compliance times specified, unless already
the original document remains the List of Subjects in 14 CFR Part 39 done.
same. Air transportation, Aircraft, Aviation (g) Repetitive Inspections and Repair
DATES: This correction is effective safety, Incorporation by reference, Within 30 days after February 7, 2017 (the
March 22, 2017. Safety. effective date of this AD), or within 1,600
The Director of the Federal Register Adoption of the Correction flight cycles since the most recent detailed
approved the incorporation by reference inspection was done as specified in BAE
Accordingly, pursuant to the Systems Alert Service Bulletin J41–A57–029,
of certain publications listed in this AD
authority delegated to me by the whichever occurs later: Do a detailed
as of February 7, 2017 (82 FR 7, January inspection for cracks, corrosion, and other
Administrator, the Federal Aviation
3, 2017). defects (defects include scratches, dents,
Administration amends part 39 of the
ADDRESSES: You may examine the AD Federal Aviation Regulations (14 CFR holes, damage to fastener holes, or damage to
docket on the Internet at http:// surface protection and finish) of the rear face
part 39) as follows: of the wing rear spars, in accordance with the
www.regulations.gov; or in person at the
Docket Management Facility between 9 Accomplishment Instructions of BAE
PART 39—AIRWORTHINESS Systems Alert Service Bulletin J41–A57–029,
a.m. and 5 p.m., Monday through DIRECTIVES Revision 3, dated April 8, 2014. Repeat the
Friday, except Federal holidays. The AD inspection thereafter at intervals not to
docket contains this AD, the regulatory ■ 1. The authority citation for part 39 exceed 1,600 flight cycles.
evaluation, any comments received, and continues to read as follows: (1) If any cracking, corrosion, or other
other information. The address for the Authority: 49 U.S.C. 106(g), 40113, 44701. defect is found within the criteria defined in
jstallworth on DSK7TPTVN1PROD with RULES

Docket Office (phone: 800–647–5527) is Chapter 57, Wings, of the Jetstream Series
Docket Management Facility, U.S. § 39.13 [Corrected] 4100 Structural Repair Manual (SRM),
Volume 1, Publication Ref. No. (Transmittal
Department of Transportation, Docket ■ 2. The FAA amends § 39.13 by No.) SA 4–4100/SRM/400, Revision 32, dated
Operations, M–30, West Building removing Amendment 39–17079 (77 FR October 15, 2014 (‘‘Chapter 57 of the SRM’’):
Ground Floor, Room W12–140, 1200 36127, June 18, 2012), and adding the Before further flight, repair the affected area,
New Jersey Avenue SE., Washington, following new airworthiness directive in accordance with the repair instructions of
DC 20590. (AD): Chapter 57 of the SRM.

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14602 Federal Register / Vol. 82, No. 54 / Wednesday, March 22, 2017 / Rules and Regulations

(2) If any cracking, corrosion, or other (2) You must use this service information AD to address the unsafe condition on
defect is found exceeding the criteria defined as applicable to do the actions required by these products.
in Chapter 57 of the SRM: Before further this AD, unless this AD specifies otherwise.
DATES: This AD is effective April 26,
flight, repair using a method approved by the (i) BAE Systems Alert Service Bulletin J41–
Manager, International Branch, ANM–116, A57–029, Revision 3, dated April 8, 2014. 2017.
Transport Airplane Directorate, FAA; or the (ii) Chapter 57, Wings, of the BAE Systems The Director of the Federal Register
European Aviation Safety Agency (EASA); or (Operations) Limited Jetstream Series 4100 approved the incorporation by reference
BAE Systems (Operations) Limited’s EASA Structural Repair Manual, Volume 1, of a certain publication listed in this AD
Design Organization Approval (DOA). Publication Ref. No. (Transmittal No.) SA 4– as of April 26, 2017.
4100/SRM/400, Revision 32, dated October ADDRESSES: For service information
(h) Repair Does Not Constitute Terminating
15, 2014. identified in this final rule, contact
Action Except for Certain Repairs
(3) For service information identified in
Accomplishment of a repair, as required by Fokker Services B.V., Technical
this AD, contact BAE Systems (Operations)
paragraphs (g)(1) and (g)(2) of this AD, does Limited, Customer Information Department, Services Dept., P.O. Box 1357, 2130 EL
not constitute terminating action for the Prestwick International Airport, Ayrshire, Hoofddorp, the Netherlands; telephone:
repetitive inspections required by paragraph KA9 2RW, Scotland, United Kingdom; +31 (0)88–6280–350; fax: +31 (0)88–
(g) of this AD, unless the approved repair telephone +44 1292 675207; fax +44 1292 6280–111; email: technicalservices@
required by paragraph (g)(2) of this AD states 675704; email RApublications@ fokker.com; Internet http://
otherwise (e.g., the approved repair states the baesystems.com; Internet http:// www.myfokkerfleet.com. You may view
repair terminates the inspections for the www.baesystems.com/Businesses/
repaired area only). this referenced service information at
RegionalAircraft/index.htm. the FAA, Transport Airplane
(i) Other FAA AD Provisions (4) You may view this service information
Directorate, 1601 Lind Avenue SW.,
at the FAA, Transport Airplane Directorate,
The following provisions also apply to this 1601 Lind Avenue SW., Renton, WA. For Renton, WA. For information on the
AD: information on the availability of this availability of this material at the FAA,
(1) Alternative Methods of Compliance call 425–227–1221. It is also available
material at the FAA, call 425–227–1221.
(AMOCs): The Manager, International on the Internet at http://
(5) You may view this service information
Branch, ANM–116, Transport Airplane
Directorate, FAA, has the authority to
that is incorporated by reference at the www.regulations.gov by searching for
National Archives and Records and locating Docket No. FAA–2016–
approve AMOCs for this AD, if requested
Administration (NARA). For information on 9302.
using the procedures found in 14 CFR 39.19.
the availability of this material at NARA, call
In accordance with 14 CFR 39.19, send your
202–741–6030, or go to: http:// Examining the AD Docket
request to your principal inspector or local
www.archives.gov/federal-register/cfr/ibr- You may examine the AD docket on
Flight Standards District Office, as
locations.html.
appropriate. If sending information directly the Internet at http://
to the International Branch, send it to ATTN: Issued in Renton, Washington, on January www.regulations.gov by searching for
Todd Thompson, Aerospace Engineer, 23, 2017. and locating Docket No. FAA–2016–
International Branch, ANM–116, Transport Dionne Palermo, 9302; or in person at the Docket
Airplane Directorate, FAA, 1601 Lind
Acting Manager, Transport Airplane Management Facility between 9 a.m.
Avenue SW., Renton, WA 98057–3356;
Directorate, Aircraft Certification Service. and 5 p.m., Monday through Friday,
telephone 425–227–1175; fax 425–227–1149.
Information may be emailed to: 9-ANM- [FR Doc. 2017–05163 Filed 3–21–17; 8:45 am] except Federal holidays. The AD docket
116-AMOC-REQUESTS@faa.gov. Before BILLING CODE 4910–13–P contains this AD, the regulatory
using any approved AMOC, notify your evaluation, any comments received, and
appropriate principal inspector, or lacking a other information. The street address for
principal inspector, the manager of the local DEPARTMENT OF TRANSPORTATION the Docket Office (telephone 800–647–
flight standards district office/certificate
5527) is Docket Management Facility,
holding district office. The AMOC approval Federal Aviation Administration
letter must specifically reference this AD. U.S. Department of Transportation,
(2) Contacting the Manufacturer: As of Docket Operations, M–30, West
14 CFR Part 39 Building Ground Floor, Room W12–140,
February 7, 2017 (the effective date of this
AD), for any requirement in this AD to obtain [Docket No. FAA–2016–9302; Directorate 1200 New Jersey Avenue SE.,
corrective actions from a manufacturer, the Identifier 2016–NM–037–AD; Amendment Washington, DC 20590.
action must be accomplished using a method 39–18826; AD 2017–06–02] FOR FURTHER INFORMATION CONTACT: Tom
approved by the Manager, International
Rodriguez, Aerospace Engineer,
Branch, ANM–116, Transport Airplane RIN 2120–AA64
Directorate, FAA; or the EASA; or BAE International Branch, ANM–116,
Systems (Operations) Limited’s EASA DOA. Transport Airplane Directorate, FAA,
Airworthiness Directives; Fokker
If approved by the DOA, the approval must 1601 Lind Avenue SW., Renton, WA
Services B.V. Airplanes
include the DOA-authorized signature. 98057–3356; telephone 425–227–1137;
(j) Related Information AGENCY: Federal Aviation fax 425–227–1149.
Administration (FAA), Department of SUPPLEMENTARY INFORMATION:
Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA
Transportation (DOT).
Discussion
Airworthiness Directive 2015–0100, dated ACTION: Final rule.
June 3, 2015, for related information. This We issued a notice of proposed
MCAI may be found in the AD docket on the SUMMARY: We are adopting a new rulemaking (NPRM) to amend 14 CFR
Internet at http://www.regulations.gov by airworthiness directive (AD) for Fokker part 39 by adding an AD that would
searching for and locating Docket No. FAA– Services B.V. Model F28 Mark 0100 apply to Fokker Services B.V. Model
jstallworth on DSK7TPTVN1PROD with RULES

2016–0457. airplanes equipped with Rolls-Royce F28 Mark 0100 airplanes equipped with
(k) Material Incorporated by Reference TAY 650–15 engines. This AD was Rolls-Royce TAY 650–15 engines. The
(1) The Director of the Federal Register
prompted by reports of uncontained NPRM published in the Federal
approved the incorporation by reference engine fan blade failures in Rolls-Royce Register on November 1, 2016 (81 FR
(IBR) of the service information listed in this TAY 650–15 engines. This AD requires 75759) (‘‘the NPRM’’). The NPRM was
paragraph under 5 U.S.C. 552(a) and 1 CFR installation of a caution placard in the prompted by reports of uncontained
part 51. flight compartment. We are issuing this engine fan blade failures in Rolls-Royce

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Document Created: 2017-03-22 03:58:25
Document Modified: 2017-03-22 03:58:25

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; correction.
Dates		This correction is effective March 22, 2017.
Contact		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.
FR Citation		82 FR 14601
RIN Number		2120-AA64
CFR Associated		Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

82 FR 14601 - Airworthiness Directives; BAE Systems (Operations) Limited Airplanes

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 82, Issue 54 (March 22, 2017)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration