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65-06-06: Fuel Quantity Gauge Sender Units

FAA order 65-06-06 is an airworthiness directive in force since March 12, 1965. The FAA's subject line: Fuel Quantity Gauge Sender Units. It names Piper PA-28 Cherokee, Warrior, Archer and Arrow: about 18,633 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: fuel system.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Piper Aircraft Inc.
Models
PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235
On this site
Piper PA-28 Cherokee, Warrior, Archer and Arrow 18,633 registered

Dates and paperwork

In force since
March 12, 1965
Published
March 12, 1965 (signed March 4, 1965)
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 (2,177 characters)
65-06-06 PIPER: Amdt. 39-46 Part 39 Federal Register March 12, 1965. Applies to Model PA-28-140 Aircraft, Serial Numbers 20551 through 20672; Models PA-28-150, PA-28-160, PA-28-180 Aircraft Serial Numbers 1761 through 2183; and Model PA-28-235 Aircraft Serial Numbers 10003 through 10600. Compliance required as indicated. To prevent further failures of the fuel quantity gauge sender unit terminal connecting wire that could cause electrical arcing in the unit, accomplish the following: (a) Within the next 10 hours' time in service after the effective date of this AD, unless already accomplished, install a placard on the instrument panel adjacent to the fuel gauges that reads: "Do not operate aircraft with non-functioning or erratic fuel gauges". The placard may be removed when all fuel quantity gauge sender units have been modified in accordance with (b) or (c). (b) Before each flight after the placard has been installed, inspect to determine whether the aircraft has non-functioning or erratic fuel gauges. Modify the fuel quantity gauge sender unit, Piper P/N 550613, for any non-functioning or erratic gauge in accordance with Piper Service Bulletin No. 223 or later FAA-approved revision, or an equivalent approved by the Chief, Engineering and Manufacturing Branch, FAA Southern Region, before further flight, except that the aircraft may be flown in accordance with the provisions of FAR 21.197 to a base where the modification can be made. During this flight the electrical lead to the sender unit to be modified shall be disconnected. The inspections required by this paragraph may be discontinued for the gauge of any sender unit modified in accordance with this paragraph. (c) Within the next 100 hours' time in service after the effective date of this AD, unless already accomplished, modify all fuel quantity gauge sender units, Piper P/N 550613, in accordance with Piper Service Bulletin No. 223 or later FAA-approved revision, or an equivalent approved by the Chief, Engineering and Manufacturing Branch, FAA Southern Region. (Piper Service Bulletin No. 223, covers this subject.) This directive effective March 12, 1965.

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/65-06-06.json · aircraft systems.