AD 72-11-01

Airworthiness directive · Possible Fire From Fuel Vapor · Piper PA-23-235, PA-23-250 (Navy UO-1) and PA-E23-250 with STC SA179CE or SA867SW

Effective
May 19, 1972
Published
May 13, 1972
Issued
May 5, 1972
Models
PA-23-235, PA-23-250 (Navy UO-1), PA-E23-250
Data sheet
TCDS1A10
Registered aircraft
924 matched by model
Product
Aircraft · Small airplane
Amendment
39-1448

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

72-11-01 PIPER AIRCRAFT: Amdt. 39-1448. Applies to PA-23-235, PA-23-250, and PA-E23-250 series airplanes Serial Numbers 27-1 through 27-4765 inclusive, equipped with non-supercharged engines, including airplanes modified in accordance with STC SA179CE and STC SA867SW and certificated in all categories.

Compliance required as indicated.

In order to prevent possible explosion and fire resulting from fuel vapor ignition during engine starting, accomplish the following:

a. Serial Numbers 27-1 through 27-2504 inclusive: Prior to first flight of each day, visually check the lower surface of the wings in the areas of the fuel cells and aft nacelle for fuel stains and any odor of fuel vapor. If fuel stains or any other sign of fuel leakage are observed, the source of leakage must be determined and repairs or replacements accomplished prior to further flight, in accordance with Section IX of Piper Service Manual No. 753464 or an equivalent repair approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region.

b. Serial Numbers 27-2505 through 27-4765 inclusive: Inspect in accordance with paragraph (a) above within 50 hours' time in service after the effective date of this AD or since the last inspection and every 50 hours thereafter.

c. The checks required by paragraphs (a) and (b) above may be performed by the pilot, including pilots of aircraft engaged in Air Carrier operations. A chronological listing of compliance with this AD must be made in the airplane's permanent maintenance log in accordance with FAR 91.173.

d. When the instruction paragraph contained in Piper Service Letter No. 606 is complied with or equivalent inspections and alterations approved by the Chief, Engineering and Manufacturing Branch, FAA Eastern Region, further compliance with this AD is not required.

(Piper Service Letters Nos. 449 and 449A refer to this subject.)

This AD supersedes AD 70-03-08.

This amendment is effective May19, 1972.

Affected TCDS · 1

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

Registered aircraft · 924

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
  • Piper924 aircraft
By year built
19531995
Registered aircraft by year built: 744 aircraft
19531
196033
196113
196224
196331
196428
196545
196660
196731
196839
196949
197019
197124
197227
197344
197449
197536
197652
197735
197836
197946
198011
198110
19951

180 with no year recorded

By model

Aircraft

See all 924 aircraft

NTSB investigations that cite this AD · 1

Their narratives or probable cause name AD 72-11-01, often to say whether the aircraft complied with it.