AD 81-10-04

Airworthiness directive · Aileron Modification · Piper PA-44-180

Effective
April 30, 1981
Published
April 27, 1981
Issued
April 15, 1981
Model
PA-44-180
Data sheet
TCDSA19SO
Registered aircraft
562 matched by model
Product
Aircraft · Small airplane
Amendment
39-4094

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed November 21, 2025.

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The airworthiness directive

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.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 562

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Piper558 aircraft
  • New Piper4 aircraft
By year built
19782026
Registered aircraft by year built: 525 aircraft
197845
197943
19803
19812
19896
19901
19931
19952
19961
19974
19981
19995
20009
200143
200239
20036
20048
200510
20069
20077
200816
20094
20106
20111
201212
201311
20149
20158
20166
201711
201828
201930
202016
202113
202218
202315
202426
202528
202622

37 with no year recorded

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Aircraft

See all 562 aircraft