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2010-09-24
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Airworthiness Directives; Airbus Model A300-600 and A310 Series Airplanes Equipped With General Electric Model CF6-80 Engines
Rules and Regulations
D09002ee1be02faff
D09002ee1be02fb8d
United States
Department of Transportation
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United States Government Agency or Subagency
This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A300-600 and A310 series airplanes, that requires an inspection to detect defects of the directional pilot valves (DPV); and replacement of any defective DPV with a new DPV, or deactivation of the thrust reverser system, if necessary. This amendment is prompted by a report indicating that, during a maintenance check, an uncommanded deployment and stowage of the thrust reverser occurred due to improperly modified DPV's. The actions specified by this AD are intended to prevent uncommanded deployment and stowage of the thrust reverser during maintenance activities, as a result of improperly modified DPV's, which could result in injury to maintenance personnel or other people on the ground.
61 FR 46541
https://www.govinfo.gov/app/details/FR-1996-09-04/96-22260
96-22260
fr04se96-6
RIN 2120-AA64
4910-13-U
Docket No. 95-NM-175-AD
Amendment 39-9734
AD 96-18-10
https://www.govinfo.gov/app/details/FR-1996-09-04/96-22260
https://www.govinfo.gov/content/pkg/FR-1996-09-04/html/96-22260.htm
https://www.govinfo.gov/content/pkg/FR-1996-09-04/pdf/96-22260.pdf
2 p.
46541
46542
61 FR 46541
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Airbus Model A300-600 and A310 Series Airplanes Equipped With General Electric Model CF6-80 Engines; Federal Register Vol. 61, Issue
RULE
96-22260
DEPARTMENT OF TRANSPORTATION
1996-10-09
Docket No. 95-NM-175-AD
Amendment 39-9734
AD 96-18-10
4910-13-U
96-22260
Final rule.
This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A300-600 and A310 series airplanes, that requires an inspection to detect defects of the directional pilot valves (DPV); and replacement of any defective DPV with a new DPV, or deactivation of the thrust reverser system, if necessary. This amendment is prompted by a report indicating that, during a maintenance check, an uncommanded deployment and stowage of the thrust reverser occurred due to improperly modified DPV's. The actions specified by this AD are intended to prevent uncommanded deployment and stowage of the thrust reverser during maintenance activities, as a result of improperly modified DPV's, which could result in injury to maintenance personnel or other people on the ground.
Effective October 9, 1996.
Charles Huber, Aerospace Engineer, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (206) 227-2589; fax (206) 227-1149.
Federal Register
Vol. 61, no. 172
Office of the Federal Register, National Archives and Records Administration
1996-09-04
continuing
daily
deposited
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178 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-1996-09-04
P0b002ee180a20143
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr04se96
https://www.govinfo.gov/app/details/FR-1996-09-04
https://www.govinfo.gov/content/pkg/FR-1996-09-04/pdf/FR-1996-09-04.pdf
fdlp
46529
46698
DGPO
2010-09-24
2023-05-06
FR-1996-09-04
machine generated
eng
FR
FR-1996-09-04
61
172