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2013-02-05
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Airworthiness Directives; DASSAULT AVIATION Airplanes
Proposed Rules
D09002ee1bdcaa57c
D09002ee1bdcaa5ff
United States
Department of Transportation
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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 certain DASSAULT AVIATION Model MYSTERE-FALCON 900 and FALCON 900EX airplanes. This proposed AD was prompted by reports of chafing between the tail strobe power supply and a hydraulic line. This proposed AD would require modifying the tail strobe power supply wire routing. We are proposing this AD to prevent chafing between the tail strobe power supply and a hydraulic line, which could result in hydraulic fluid leakage and possible fire due to arcing, and consequent loss of control of the airplane due to structural failure of the tail.
78 FR 8052
https://www.govinfo.gov/app/details/FR-2013-02-05/2013-02450
2013-02450
fr05fe13-16
RIN 2120-AA64
4910-13-P
Docket No. FAA-2012-1322
Directorate Identifier 2012-NM-155-AD
https://www.govinfo.gov/app/details/FR-2013-02-05/2013-02450
https://www.govinfo.gov/content/pkg/FR-2013-02-05/html/2013-02450.htm
https://www.govinfo.gov/content/pkg/FR-2013-02-05/pdf/2013-02450.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
8052
8054
78 FR 8052
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; DASSAULT AVIATION Airplanes; Federal Register Vol. 78, Issue
PRORULE
2013-02450
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2013-03-22
Docket No. FAA-2012-1322
Directorate Identifier 2012-NM-155-AD
4910-13-P
2013-02450
Notice of proposed rulemaking (NPRM).
We propose to adopt a new airworthiness directive (AD) for certain DASSAULT AVIATION Model MYSTERE-FALCON 900 and FALCON 900EX airplanes. This proposed AD was prompted by reports of chafing between the tail strobe power supply and a hydraulic line. This proposed AD would require modifying the tail strobe power supply wire routing. We are proposing this AD to prevent chafing between the tail strobe power supply and a hydraulic line, which could result in hydraulic fluid leakage and possible fire due to arcing, and consequent loss of control of the airplane due to structural failure of the tail.
We must receive comments on this proposed AD by March 22, 2013.
Tom Rodriguez, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425) 227-1137; fax (425) 227-1149.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
DASSAULT AVIATION Airplanes
,
9-ANM-116-AMOC-REQUESTS@faa.gov
http://www.dassaultfalcon.com
http://www.regulations.gov
Federal Register
Vol. 78, no. 24
Office of the Federal Register, National Archives and Records Administration
2013-02-05
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361 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2013-02-05
P0b002ee183c63dbb
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr05fe13
https://www.govinfo.gov/app/details/FR-2013-02-05
https://www.govinfo.gov/content/pkg/FR-2013-02-05/pdf/FR-2013-02-05.pdf
https://www.govinfo.gov/content/pkg/FR-2013-02-05/xml/FR-2013-02-05.xml
fdlp
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DGPO
2013-02-05
2023-04-30
FR-2013-02-05
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FR
FR-2013-02-05
78
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