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2010-09-23
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Airworthiness Directives; Raytheon Aircraft Company, Model 390, Premier 1 Airplanes
Rules and Regulations
D09002ee1bde4aba5
D09002ee1bde4ac41
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
The FAA adopts a new airworthiness directive (AD) for certain Raytheon Aircraft Company, Model 390, Premier 1 airplanes. This AD requires you to inspect the routing and security of the left and right main landing gear (MLG) squat switch wire harness installations for damage, repair any damage or replace components, and reinstall the squat switch wire harness. We are issuing this AD to prevent damage to the wire harnesses, which could result in loss of pressurization, loss of transponder responses to interrogations, and failure of other systems utilizing air/ground status signals. This failure could lead to loss of control of the airplane.
69 FR 75223
https://www.govinfo.gov/app/details/FR-2004-12-16/04-27195
04-27195
fr16de04-1
RIN 2120-AA64
4910-13-P
Docket No. FAA 2004-19119
Directorate Identifier 2004-CE-26-AD
Amendment 39-13903
AD 2004-25-15
https://www.govinfo.gov/app/details/FR-2004-12-16/04-27195
https://www.govinfo.gov/content/pkg/FR-2004-12-16/html/04-27195.htm
https://www.govinfo.gov/content/pkg/FR-2004-12-16/pdf/04-27195.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
75223
75225
69 FR 75223
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, Premier 1 Airplanes; Federal Register Vol. 69, Issue
RULE
04-27195
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2005-01-18
Docket No. FAA 2004-19119
Directorate Identifier 2004-CE-26-AD
Amendment 39-13903
AD 2004-25-15
4910-13-P
04-27195
Final rule.
The FAA adopts a new airworthiness directive (AD) for certain Raytheon Aircraft Company, Model 390, Premier 1 airplanes. This AD requires you to inspect the routing and security of the left and right main landing gear (MLG) squat switch wire harness installations for damage, repair any damage or replace components, and reinstall the squat switch wire harness. We are issuing this AD to prevent damage to the wire harnesses, which could result in loss of pressurization, loss of transponder responses to interrogations, and failure of other systems utilizing air/ground status signals. This failure could lead to loss of control of the airplane.
This AD becomes effective on January 18, 2005.
Philip Petty, Aerospace Engineer, ACE- 119W, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-4139; facsimile: (316) 946-4107.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness directives:
Raytheon,
http://dms.dot.gov
http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
Federal Register
Vol. 69, no. 241
Office of the Federal Register, National Archives and Records Administration
2004-12-16
continuing
daily
deposited
born digital
240 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2004-12-16
P0b002ee180977e00
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr16de04
https://www.govinfo.gov/app/details/FR-2004-12-16
https://www.govinfo.gov/content/pkg/FR-2004-12-16/pdf/FR-2004-12-16.pdf
https://www.govinfo.gov/content/pkg/FR-2004-12-16/xml/FR-2004-12-16.xml
fdlp
75223
75450
DGPO
2010-09-23
2023-05-03
FR-2004-12-16
machine generated
eng
FR
FR-2004-12-16
69
241