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2018-02-16
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Airworthiness Directives; Fokker Services B.V. Airplanes
Proposed Rules
D09002ee1bdc35630
D09002ee1bdc356de
United States
Department of Transportation
originator
org
United States Government Agency or Subagency
United States
Federal Aviation Administration
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org
United States Government Agency or Subagency
We propose to adopt a new airworthiness directive (AD) for all Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. This proposed AD was prompted by reports that cracks can occur in a frame of the tail section on certain airplanes. This proposed AD would require a one-time detailed inspection of the oblique frame 67-2 for any cracking, and repair if necessary. We are proposing this AD to detect and correct such cracking, which could lead to failure of the oblique frame 67-2, and consequent loss of the structural integrity of the tail section.
80 FR 3500
https://www.govinfo.gov/app/details/FR-2015-01-23/2015-00959
2015-00959
fr23ja15-13
RIN 2120-AA64
4910-13-P
Docket No. FAA-2014-1048
Directorate Identifier 2014-NM-055-AD
https://www.govinfo.gov/app/details/FR-2015-01-23/2015-00959
https://www.govinfo.gov/content/pkg/FR-2015-01-23/html/2015-00959.htm
https://www.govinfo.gov/content/pkg/FR-2015-01-23/pdf/2015-00959.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
3500
3502
80 FR 3500
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Fokker Services B.V. Airplanes; Federal Register Vol. 80, Issue
PRORULE
2015-00959
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2015-03-09
Docket No. FAA-2014-1048
Directorate Identifier 2014-NM-055-AD
4910-13-P
2015-00959
Notice of proposed rulemaking (NPRM).
We propose to adopt a new airworthiness directive (AD) for all Fokker Services B.V. Model F.28 Mark 0070 and 0100 airplanes. This proposed AD was prompted by reports that cracks can occur in a frame of the tail section on certain airplanes. This proposed AD would require a one-time detailed inspection of the oblique frame 67-2 for any cracking, and repair if necessary. We are proposing this AD to detect and correct such cracking, which could lead to failure of the oblique frame 67-2, and consequent loss of the structural integrity of the tail section.
We must receive comments on this proposed AD by March 9, 2015.
Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington WA 98057-3356; telephone (425) 227-1137; fax (425) 227-1149.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
Fokker Services B.V. Airplanes
,
9-ANM-116-AMOC-REQUESTS@faa.gov
technicalservices@fokker.com
http://www.myfokkerfleet.com
http://www.regulations.gov
Federal Register
Vol. 80, no. 15
Office of the Federal Register, National Archives and Records Administration
2015-01-23
continuing
daily
deposited
born digital
411 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2015-01-23
P0b002ee1987a7ff4
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr23ja15
https://www.govinfo.gov/app/details/FR-2015-01-23
https://www.govinfo.gov/content/pkg/FR-2015-01-23/pdf/FR-2015-01-23.pdf
https://www.govinfo.gov/content/pkg/FR-2015-01-23/xml/FR-2015-01-23.xml
fdlp
3463
3864
DGPO
2018-02-16
2023-04-29
FR-2015-01-23
machine generated
eng
FR
FR-2015-01-23
80
15