AD 77-12-01

final rule
Data completeness: 70%

Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, and PA-32S-300 Airplanes

AD Number
77-12-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-28-235 Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, and PA-32S-300 Airplanes
aircraft Piper Aircraft Inc. PA-32-260 Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, and PA-32S-300 Airplanes
aircraft Piper Aircraft Inc. PA-32-300 Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, and PA-32S-300 Airplanes
aircraft Piper Aircraft Inc. PA-32S-300 Airworthiness Directives; Piper Models PA-28-235, PA-32-260, PA-32-300, and PA-32S-300 Airplanes

Unsafe Condition

Fuel system malfunction and possible power interruption due to internal leaking fuel selector valves, improper fuel tank fill caps, unmodified fuel selector control systems, misaligned fuel tank vent tubes, and improperly installed fuel hose assemblies.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect fuel selector valve and perform drain checks, replace non-compliant fuel tank fill caps with Piper Part Number 66817-00, modify fuel selector control system per Service Bulletin 376, rework vent tubes to specified angles and install new vent assemblies, and inspect/replace twisted fuel hose assemblies. Actions must be repeated at intervals not exceeding 50 hours time in service.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

within the next five hours time in service after the effective date of this A.D. and thereafter before the first flight of each day until (b), (c), (d) and (e) are accomplished and thereafter at intervals not to exceed 50 hours time in service from the last check

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Piper Models PA-28-235, PA-32-260, PA-32-300, and PA-32S-300 with specified serial ranges, equipped with Airborne Model 1H10, 1H16-1, 1H26-2, 1H26-3, or 1H26-4 fuel selector valves or without Piper fuel valve kits 757 148V or 760 895V.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.