AD 78-01-11

Active

Emergency Exit Release Handle

Key Information
78-01-11
Active
February 13, 1978
Not specified
Unknown
39-3116
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
DC-9-11 DC-9-12 DC-9-13 DC-9-14 DC-9-15 DC-9-15F DC-9-21 DC-9-31 DC-9-32 DC-9-32 (VC-9C) DC-9-32F DC-9-32F (C-9A) DC-9-32F (C-9B) DC-9-33F DC-9-34 DC-9-34F DC-9-41 DC-9-51 DC-9-81 (MD-81) DC-9-82 (MD-82) DC-9-83 (MD-83) DC-9-87 (MD-87)
Regulatory Text

78-01-11 MCDONNELL DOUGLAS: Amendment 39-3116. Applies to all passenger and passenger/cargo Model DC-9 airplanes certificated in all categories, including C-9A, C-9B and VC-9C. \n\n\tCompliance required within 180 days from the effective date of this AD, unless already accomplished. \n\n\tTo identify the location and operation of the tail cone emergency exit release handle, accomplish the following: \n\n\tModify the tail cone emergency exit release handle locating and operating markings in accordance with McDonnell Douglas Service Bulletin 53-134, Revision 1, dated December 16, 1977 or later FAA approved revision, or an equivalent modification approved by the Chief, Aircraft Engineering Division, FAA Western Region. \n\n\tThis Amendment becomes effective February 13, 1978.

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