AD 65-17-01

Active

Thrust Reverser

Key Information
65-17-01
Active
August 23, 1965
Not specified
Unknown
39-108
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
727-100 Series 727-100C Series 727-200 Series 727-200F Series 727 Series 727C Series
Regulatory Text

65-17-01\tBOEING: Amdt. 39-108 Part 39 Federal Register July 24, 1965. Applies to Model 727 Series Airplanes. \n\n\tCompliance required within the next 600 hours' time in service after the effective date of this AD unless already accomplished. \n\n\tTo prevent inadvertent thrust reversing from failure to the locking pin, replace the thrust reverser lockout actuator piston, P/N 65-37853-2, on each engine, with actuator piston, P/N 65- 37853-3, in accordance with Boeing Alert Service Bulletin No. 78-18, or later FAA-approved revision, or an equivalent approved by the Chief, Aircraft Engineering Division, FAA Western Region. \n\n\tThis directive effective August 23, 1965.

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References
This information is not available.
--- - Part 39
FAA Documents