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.

Rules and Regulations Federal Register

14601 

Vol. 82, No. 54 

Wednesday, March 22, 2017 

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 

■ 1. The authority citation for part 39 

continues to read as follows: 

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

§ 39.13 [Corrected] 

■ 2. The FAA amends § 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. 


jstallworth on DSK7TPTVN1PROD with RULES
14602 Federal Register / Vol. 82, No. 54 / Wednesday, March 22, 2017 / Rules and Regulations 

(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: 9-ANM116-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 

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 RApublications@

baesystems.com; 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/ibrlocations.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 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2016–9302; Directorate 

Identifier 2016–NM–037–AD; Amendment 

39–18826; AD 2017–06–02] 

RIN 2120–AA64 

Airworthiness Directives; Fokker 

Services B.V. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for Fokker 

Services B.V. Model F28 Mark 0100 

airplanes equipped with Rolls-Royce 

TAY 650–15 engines. This AD was 

prompted by reports of uncontained 

engine fan blade failures in Rolls-Royce 

TAY 650–15 engines. This AD requires 

installation of a caution placard in the 

flight compartment. We are issuing this 

AD to address the unsafe condition on 

these products. 

DATES: This AD is effective April 26, 

2017. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of April 26, 2017. 

ADDRESSES: For service information 

identified in this final rule, contact 

Fokker Services B.V., Technical 

Services Dept., P.O. Box 1357, 2130 EL 

Hoofddorp, the Netherlands; telephone: 

+31 (0)88–6280–350; fax: +31 (0)88– 

6280–111; email: technicalservices@

fokker.com; Internet http://

www.myfokkerfleet.com. You may view 

this referenced 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. It is also available 

on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2016– 

9302. 

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–2016– 

9302; 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 (telephone 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: Tom 

Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue SW., Renton, WA 

98057–3356; telephone 425–227–1137; 

fax 425–227–1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to Fokker Services B.V. Model 

F28 Mark 0100 airplanes equipped with 

Rolls-Royce TAY 650–15 engines. The 

NPRM published in the Federal 

Register on November 1, 2016 (81 FR 

75759) (‘‘the NPRM’’). The NPRM was 

prompted by reports of uncontained 

engine fan blade failures in Rolls-Royce 


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