AD 87-07-03

Active

Airstair Exit Handle

Key Information
87-07-03
Active
April 13, 1987
Not specified
Unknown
39-5577
Applicability
["Aircraft"]
["Large Airplane"]
The Boeing Company
737-100 Series 737-200 Series 737-200C Series 737-300 Series 737-400 Series 737-500 Series 737-600 Series 737-700 Series 737-800 Series
Regulatory Text

87-07-03 BOEING: Amendment 39-5577. Applies to Boeing Model 737 airplanes, equipped with an aft airstair on which the detent plate modification described in Boeing Service Bulletin 737-52-1083, dated June 4, 1982, or later revisions, has been incorporated; certificated in any category. Compliance is required within one year after the effective date of this AD. \n\n\tTo ensure usability of the aft airstair exit in the event of an emergency evacuation, accomplish the following, unless previously accomplished: \n\n\tA.\tRemove the aft airstair operating handle detent plate which has been modified in accordance with Boeing Service Bulletin 737-52-1083, and install an unmodified Boeing P/N 65- 60510-1 aft airstair operating handle detent plate. \n\n\tB.\tAn alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. \n\n\tC.\tSpecial flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of the requirements of this AD.\n \n\tAll persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to the Boeing Commercial Airplane Company, P.O. Box 3707, Seattle, Washington 98124-2207. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington.\n \n\tThis amendment becomes effective April 13, 1987.

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