AD 82-04-08

Airworthiness directive · Landing Gear Retraction · Piper PA-34-220T

Effective
February 25, 1982
Published
February 25, 1982
Issued
February 10, 1982
Model
PA-34-220T
Data sheet
TCDSA7SO
Registered aircraft
256 matched by model
Product
Aircraft · Small airplane
Amendment
39-4323

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

82-04-08 PIPER AIRCRAFT CORPORATION: Amendment 39-4323. Applies to Piper Model PA-34-220T (Serial Numbers 34-8133001 through 34-8233020) airplanes certificated in any category.

Compliance: Required as indicated unless already accomplished.

To prevent a potentially hazardous condition during landing and ground operation due to the inadvertent retraction of the landing gear, accomplish the following:

A) Within the next 50 hours time-in-service after the effective date of this AD, inspect and modify the landing gear selector and squat switches in accordance with the Instructions Section contained in Piper Service Bulletin No. 732, dated November 11, 1981.

B) Any equivalent method of compliance may be approved by the Chief, Atlanta Aircraft Certification Office, FAA, Southern Region, Room 275, 3400 Norman Berry Drive, East Point, Georgia 30344.

This amendment becomes effective February 25, 1982.

Affected TCDS · 1

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

Registered aircraft · 256

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
  • Piper248 aircraft
  • New Piper8 aircraft
By year built
19782024
Registered aircraft by year built: 207 aircraft
19781
198173
198221
198310
198411
19855
19892
19902
19933
19946
19964
19978
199811
199913
20007
20014
200210
20034
20043
20051
20072
20121
20131
20143
20241

49 with no year recorded

By model

Aircraft

See all 256 aircraft