AD 65-06-06

Airworthiness directive · Fuel Quantity Gauge Sender Units · Piper PA-28-140, PA-28-150, PA-28-160 and 2 more

Effective
March 12, 1965
Published
March 12, 1965
Issued
March 4, 1965
Models
PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235
Data sheet
TCDS2A13
Registered aircraft
8,998 matched by model
Product
Aircraft · Small airplane
Amendment
39-46

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

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.

Affected TCDS · 1

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

Registered aircraft · 8,998

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
  • Piper8,997 aircraft
  • Piper/Valdes-Ervin1 aircraft
By year built
19412001
Registered aircraft by year built: 7,703 aircraft
19411
196154
1962213
1963316
1964606
1965732
1966928
1967965
1968877
1969705
1970260
1971426
1972459
1973526
1974264
1975185
1976132
197752
19811
20011

1,295 with no year recorded

By model

Aircraft

See all 8,998 aircraft