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2010-09-23
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Airworthiness Directives; Raytheon Aircraft Company Model 390 Airplanes
Rules and Regulations
D09002ee1bded3329
D09002ee1bded3388
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
This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Model 390 airplanes. This AD requires you to replace the inboard fuel probe mounting brackets with ones of improved design. This AD is the result of reports of a design problem with the fuel probe assembly brackets. The actions specified by this AD are intended to correct the required air gap clearance between the fuel probe and the adjacent wing fuel tank access panel, which could result in arcing between the two conductive materials in the event of a lightning strike. This could serve as an ignition source inside the fuel tank and result in fire or explosion.
67 FR 59775
https://www.govinfo.gov/app/details/FR-2002-09-24/02-23880
02-23880
fr24se02-4
RIN 2120-AA64
4910-13-U
Docket No. 2002-CE-37-AD
Amendment 39-12884
AD 2002-19-04
https://www.govinfo.gov/app/details/FR-2002-09-24/02-23880
https://www.govinfo.gov/content/pkg/FR-2002-09-24/html/02-23880.htm
https://www.govinfo.gov/content/pkg/FR-2002-09-24/pdf/02-23880.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
59775
59777
67 FR 59775
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Raytheon Aircraft Company Model 390 Airplanes; Federal Register Vol. 67, Issue
RULE
02-23880
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2002-10-04
Docket No. 2002-CE-37-AD
Amendment 39-12884
AD 2002-19-04
4910-13-U
02-23880
Final rule; request for comments.
This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Model 390 airplanes. This AD requires you to replace the inboard fuel probe mounting brackets with ones of improved design. This AD is the result of reports of a design problem with the fuel probe assembly brackets. The actions specified by this AD are intended to correct the required air gap clearance between the fuel probe and the adjacent wing fuel tank access panel, which could result in arcing between the two conductive materials in the event of a lightning strike. This could serve as an ignition source inside the fuel tank and result in fire or explosion.
This AD becomes effective on October 4, 2002.
James P. Galstad, Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-4135; facsimile: (316) 946-4407.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Raytheon,
9-ACE-7-Docket@faa.gov
Federal Register
Vol. 67, no. 185
Office of the Federal Register, National Archives and Records Administration
2002-09-24
continuing
daily
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339 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2002-09-24
P0b002ee1809dca9f
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr24se02
https://www.govinfo.gov/app/details/FR-2002-09-24
https://www.govinfo.gov/content/pkg/FR-2002-09-24/pdf/FR-2002-09-24.pdf
https://www.govinfo.gov/content/pkg/FR-2002-09-24/xml/FR-2002-09-24.xml
fdlp
59769
60098
DGPO
2010-09-23
2023-05-04
FR-2002-09-24
machine generated
eng
FR
FR-2002-09-24
67
185