78-23-01: Fuel Drain Assembly
FAA order 78-23-01 is an airworthiness directive in force since November 3, 1978. The FAA's subject line: Fuel Drain Assembly. It names Piper PA-28 Cherokee, Warrior, Archer and Arrow, Piper PA-32 Cherokee Six, Lance and Saratoga: about 22,550 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- Piper Aircraft Inc.
- Models
- PA-28-235, PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32S-300
- On this site
- Piper PA-28 Cherokee, Warrior, Archer and Arrow 18,633 registered
Piper PA-32 Cherokee Six, Lance and Saratoga 3,917 registered
Dates and paperwork
- In force since
- November 3, 1978
- Published
- November 2, 1978 (signed October 20, 1978)
- Docket
- Unknown
- Status
- Current
- The FAA's document
- Read the order on the FAA's site
The order itself the regulatory text, as published
Show the full text (2,439 characters)
78-23-01 PIPER AIRCRAFT CORPORATION: Amendment 39-3330. Applies to Models PA-28-235, PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300 and PA- 32RT-300T airplanes, certificated in all categories.
Compliance is required as indicated.
To prevent inadvertent fuel drain lever actuation, accomplish the following:
(a) On Model PA-28-235 serial numbers 28-10003 through 28-10660, accomplish the following:
(1) Within the next 50 hours time in service after the effective date of this AD, unless already accomplished, remove the fuel drain lever cover assembly Piper Part Number 65196-05, -06, or -07.
(2) Remove snap studs from spar box if installed.
(3) Using existing stud holes in spar box, install new drain cover assembly, Piper Kit 763 883V.
(4) Actuate fuel drain valve handle and insure adequate clearance between the handle and cover assembly.
(5) Make appropriate maintenance record entry.
(b) On Models PA-28-235, PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300, and PA-32RT-300T, all serial numbers, accomplish the following:
(1) For airplanes with 300 hours or more time in service, within the next 50 hours time in service from the effective date of this AD, and at intervals not to exceed 100 hours time in service from the last check, check the fuel drain lever cover assembly door to determine whether the door freely opens and closes freely without manual assistance and prevents actuation of the lever when the door is in the closed position.
(2) If the door does not open and close freely or if the door does not prevent access to the lever when it is in the closed position, replace the fuel drain lever cover assembly with a serviceable assembly, and make the appropriate maintenance record entry.
(3) If the door opens and closes freely and prevents access to the lever when it is in the closed position, make the appropriate maintenance record entry.
(c) An alternate method of compliance may be approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region.
The checks in this AD may be accomplished by the pilot and appropriate maintenance record entries made in accordance with FAR 91.173. Replacement must be accomplished by a person authorized by FAR 43.3.
(Piper Service Letter 856 dated September 15, 1978, pertains to paragraph (a).)
This amendment becomes effective November 3, 1978.
Related safety bulletins advice on the same designs, not orders
2022-10-192022-20 · Wing Spar
2021-06-29AIR-21-10 · Wing, Attach Fittings (JASC 5740)
2021-03-30AIR-21-07 · WING SPAR, Verification of Correct Washers used with Wing Spar Attach Bolts
2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2018-08-30CE-18-25 · Powerplant; Air Intake
Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 7, 2026. Connections as data: /graph/directive/78-23-01.json · aircraft systems.
