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2010-09-24
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Airworthiness Directives; British Aerospace Jetstream Model 3201 Airplanes
Proposed Rules
D09002ee1bdfe98e8
D09002ee1bdfead5f
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 document proposes to adopt a new airworthiness directive (AD) that would apply to certain British Aerospace Jetstream Model 3201 airplanes. The proposed AD would require replacing the nose landing gear downlock actuator, the flap actuator, the steering selector valve, the hydraulic reservoir, and the emergency selector valve. The proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified by the proposed AD are intended to prevent internal corrosion of the hydraulic components on airplanes where these components were exposed to water contamination, which could result in reduced or loss of control of the airplane.
63 FR 67633
https://www.govinfo.gov/app/details/FR-1998-12-08/98-32471
98-32471
fr08de98-22
RIN 2120-AA64
4910-13-U
Docket No. 98-CE-91-AD
https://www.govinfo.gov/app/details/FR-1998-12-08/98-32471
https://www.govinfo.gov/content/pkg/FR-1998-12-08/html/98-32471.htm
https://www.govinfo.gov/content/pkg/FR-1998-12-08/pdf/98-32471.pdf
2 p.
67633
67634
63 FR 67633
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; British Aerospace Jetstream Model 3201 Airplanes; Federal Register Vol. 63, Issue
PRORULE
98-32471
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
1999-01-11
Docket No. 98-CE-91-AD
4910-13-U
98-32471
Notice of proposed rulemaking (NPRM).
This document proposes to adopt a new airworthiness directive (AD) that would apply to certain British Aerospace Jetstream Model 3201 airplanes. The proposed AD would require replacing the nose landing gear downlock actuator, the flap actuator, the steering selector valve, the hydraulic reservoir, and the emergency selector valve. The proposed AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified by the proposed AD are intended to prevent internal corrosion of the hydraulic components on airplanes where these components were exposed to water contamination, which could result in reduced or loss of control of the airplane.
Comments must be received on or before January 11, 1999.
Mr. S.M. Nagarajan, Aerospace Engineer, FAA, Small Airplane Directorate, 1201 Walnut, suite 900, Kansas City, Missouri 64106; telephone: (816) 426-6932; facsimile: (816) 426-2169.
Federal Register
Vol. 63, no. 235
Office of the Federal Register, National Archives and Records Administration
1998-12-08
continuing
daily
deposited
born digital
202 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-1998-12-08
P0b002ee180a54774
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr08de98
https://www.govinfo.gov/app/details/FR-1998-12-08
https://www.govinfo.gov/content/pkg/FR-1998-12-08/pdf/FR-1998-12-08.pdf
fdlp
67573
67763
DGPO
2010-09-24
2023-05-05
FR-1998-12-08
machine generated
eng
FR
FR-1998-12-08
63
235