AD 81-10-04

Active

Aileron Modification

Key Information
81-10-04
Active
April 30, 1981
April 15, 1981
Unknown
39-4094
Applicability
["Aircraft"]
["Small Airplane"]
Piper Aircraft Inc.
PA-44-180
Regulatory Text

81-10-04 PIPER AIRCRAFT CORPORATION: Amendment 39-4094. Applies to Model PA-44-180 (Seminole), serial numbers 44-7995001 through 44-8095006, airplanes certificated in all categories.

Compliance is required within the next 50 hours time in service after the effective date of the AD, unless already accomplished. To reduce aileron spar deflection and cracking which could result in loss of aileron control, accomplish the following:

a. Modify the ailerons in accordance with Piper Aircraft Corporation Service Bulletin No. 702, dated December 4, 1980, and Piper Rework Kit P/N 764 088V.

b. Make appropriate maintenance record entry.

An equivalent method of compliance may be approved by the Chief, Engineering and Manufacturing Branch, FAA, Southern Region.

This amendment becomes effective April 30, 1981.

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References
This information is not available.
--- - Part 39
--- - _EMPTY_
Issuing Office
["AIR-720: Operational Safety Branch"]
FAA Documents