AD 79-22-02

Airworthiness directive · Fuel Leakage · Piper PA-28-161, PA-28-181, PA-28-201T and 6 more

Effective
October 26, 1979
Published
October 25, 1979
Issued
October 12, 1979
Models
PA-28-161, PA-28-181, PA-28-201T, PA-28-235, PA-28-236, PA-28R-201 and 3 more
Data sheet
TCDS2A13
Registered aircraft
7,661 matched by model
Product
Aircraft · Small airplane
Amendment
39-3595

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

79-22-02 PIPER AIRCRAFT CORPORATION: Amendment 39-3595. Applies to Model PA-28-161, serial numbers 28-7816024 through 28-7916475; Model PA-28-181, serial numbers 28-7890023 through 28-7990493, Model PA-28-201T, serial numbers 28-7921001 through 28-7921068; Model PA-28R-201, serial numbers 28R-7737135 through 28R-7837317; Model PA-28RT-201, serial numbers 28R-7918001 through 28R-7918172; Model PA-28R-201T, serial numbers 28R-7703309 through 28R-7803373; Model PA-28RT-201T, serial numbers 28R-7931001 through 28R-7931222; Model PA-28-235, serial numbers 28-7710079 through 28-7710089; and Model PA-28-236, serial numbers 28-7911001 through 28-7911204 airplanes certificated in all categories.

Compliance required within the next 50 hours' time in service after the effective date of this AD unless already accomplished.

To prevent possible fuel leakage and potential fire hazard, accomplish the following:

a. De-fuel the aircraft in accordance with the Piper Service or Maintenance Manual, for the appropriate model aircraft.

b. Remove the right hand and left hand fuel tanks in accordance with the Piper Service or Maintenance Manual for the appropriate model aircraft.

c. Modify the fuel tank vent system in accordance with the instructions listed in the "Fuel Tank Vent Modification and Vent Hose Replacement" Kit, Piper part number 763 934V.

d. Reinstall the fuel tanks in accordance with instruction in the appropriate Piper Service or Maintenance Manual.

CAUTION

Do not allow lines or hoses to rotate during installation and tightening when attaching the fuel lines to the tank fittings to prevent fuel flow obstruction due to hose twisting.

e. Refuel the aircraft and check for leaks and fuel quantity gauge function.

f. Make an appropriate maintenance record entry.

g. An equivalent method of compliance may be approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region.NOTE: Piper Service Bulletin 646 pertains to this subject.

This amendment is effective October 26, 1979.

Affected TCDS · 1

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

Registered aircraft · 7,661

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
  • Piper7,629 aircraft
  • New Piper31 aircraft
  • Piper/Valdes-Ervin1 aircraft
By year built
19632026
Registered aircraft by year built: 6,655 aircraft
196387
1964135
196544
196661
196785
196881
196947
19708
197115
197248
197364
197424
197583
1976340
1977863
1978733
1979905
1980315
1981279
1982133
198393
1984102
198597
198621
19876
198821
198958
19905
19929
19939
19947
199516
199615
199721
199862
199964
200084
200156
200248
200353
200417
200537
200628
200714
20089
20109
20114
20121
201338
201449
201532
201641
201763
201889
2019139
2020114
2021108
2022126
2023140
2024142
2025162
202696

1,006 with no year recorded

By model

Aircraft

See all 7,661 aircraft