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AD 85-02-03 ACTIVE

Autopilot Accessory Units Mod.
Key Information
AD Number 85-02-03 Status Active
Effective Date March 01, 1985 Issue Date Not specified
Docket Number Unknown Amendment 39-4985
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) The Boeing Company
Model(s) 737-200 Series
Regulatory Text

85-02-03 BOEING: Amendment 39-4985. Applies to all Boeing Model 737-200 series airplanes equipped with Boeing Autopilot Accessory Units, part numbers 65-52812-201, -203, - 206, -207, -210, -211, -214, and -216 certificated in all categories. Compliance required as indicated, unless previously accomplished. \n\n\tTo preclude the potential of a hard landing due to runaway stabilizer trim, accomplish the following: \n\n\tA.\tPrior to July 31, 1985, modify the Autopilot Accessory Units listed above in accordance with Boeing Service Bulletin 737-22-1062 dated September 16, 1983. \n\n\tB.\tAlternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, Seattle, Washington. \n\n\tThis amendment becomes effective March 1, 1985.