AD 71-09-05

Airworthiness directive · Front Seat Belt Attaching Hardware · Piper PA-32-260, PA-32-300 and PA-32S-300

Effective
April 30, 1971
Published
April 29, 1971
Issued
April 30, 1971
Models
PA-32-260, PA-32-300, PA-32S-300
Data sheet
TCDSA3SO
Registered aircraft
1,645 matched by model
Product
Aircraft · Small airplane
Amendment
39-1195

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

71-09-05 PIPER: Amdt. 39-1195. Applies to PA-32-260, Serial Nos. 32-04, 32-1 through 32-14, 32-16 through 32-20, 32-22 through 32-1075, 32-1111 through 32-1194, 32-1251 through 32-1283, 32-1285 through 32-1287, 32-1289, 32-1291 through 32-1295, 32-1297, 32-7100001 through 32-7100005.

PA-32-300, PA-32S-300, Serial Nos. 32-15, 32-21, 32-40000 through 32-40545, 32-40566 through 32-40777, 32-40851 through 32-40956, 32-40959 through 32-40974, 32-7140001 through 32-7140008, 32-7140011, 32-7140012.

Compliance required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished.

(a) On aircraft equipped with seat belts but no shoulder harnesses, remove the front seat inboard seat belt attachment hardware (AN3-5A bolt, AN-960-10 washer, MS 20365-1032C nut, and 63900-43 bushing) and replace with AN3-5A bolt, AN-970-3 washer, 63900-144 bushing, and MS 20365-1032C nut. (Supplied in Piper Kit #760-515V.) The new hardware must be installed as follows: Install the bolt in fuselage seat belt attachment fitting with head facing toward center of aircraft. Install seat belt fitting on outboard side of fuselage fitting. Install bushing in seat belt fitting. Install washer and nut.

(b) On aircraft equipped with seat belts and shoulder harnesses, remove front seat inboard seat belt from fuselage attachment and inspect bushing.

(1) If bushing O.D. measures 5/16 inch, reinstall bolt in fuselage fitting with bolt head facing toward center of aircraft. Install seat belt fitting on outboard side of fuselage fitting. Install bushing in seat belt fitting. Install washer and nut. No further action is required.

(2) If bushing O.D. measures 3/8 inch, replace attachment hardware with new hardware as outlined in paragraph (a).

Piper Service Bulletin No. 329A dated March 25, 1971, pertains to the same subject.

Piper Kit No. 760-515V contains the hardware and instructions necessary to accomplish thismodification. Equivalent replacement parts approved by the Chief, Engineering and Manufacturing Branch, FAA Southern Region, may be used.

This amendment becomes effective April 30, 1971.

Affected TCDS · 1

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

Registered aircraft · 1,645

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
  • Piper1,645 aircraft
By year built
19481980
Registered aircraft by year built: 1,408 aircraft
19481
19641
196585
1966216
1967143
196877
1969125
197041
197167
197274
1973101
197486
197577
197640
197754
1978101
1979118
19801

237 with no year recorded

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