AD 77-12-02

Airworthiness directive · Elevator Balance Weights · Piper PA-31 and PA-31-300 with STC SA986SW

Effective
June 10, 1977
Published
June 9, 1977
Issued
May 27, 1977
Models
PA-31, PA-31-300
Data sheet
TCDSA20SO
Registered aircraft
29 matched by model
Product
Aircraft · Small airplane
Amendment
39-3161

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.

On this page

The airworthiness directive

77-12-02 PIPER: Amendment 39-2915 as amended by Amendment 39-3161. Applies to Piper Models PA-31 and PA-31-300 airplanes which have wing luggage lockers installed per STC SA986SW certificated in all categories.

Compliance required as indicated.

Within the next 25 hours in service or at the next annual inspection, whichever occurs first, after the effective date unless already accomplished, inspect the elevator balance weights for security of attachment ("rivnut pullup") or remove these weights and check elevator unbalance (108 in-lbs. tail heavy maximum) and repair or rebalance elevator, as necessary, in accordance with Nayak Service Bulletin No. 1, dated May 16, 1977, or later approved revisions or in accordance with an equivalent method approved by the Chief, Engineering and Manufacturing Branch, Flight Standards Division, Southwest Region, Federal Aviation Administration, Fort Worth, Texas.

Amendment 39-2915 became effective June 17, 1977.

This amendment 39-3161 becomes effective April 10, 1978.

Affected TCDS · 1

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

Registered aircraft · 29

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
  • Piper29 aircraft
By year built
19681978
Registered aircraft by year built: 22 aircraft
19686
19691
19703
19711
19721
19732
19741
19772
19785

7 with no year recorded

By model

Aircraft

See all 29 aircraft