AD 72-11-05

Airworthiness directive · Auxiliary Fuel Cell Leaks · Cessna 411, 411A, 421 and 3 more

Effective
June 2, 1972
Models
411, 411A, 421, 421A, 421B, 421C
Data sheet
TCDSA7CE
Registered aircraft
779 matched by model
Product
Aircraft · Small airplane
Amendment
39-1454

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 May 30, 2024.

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The airworthiness directive

72-11-05 CESSNA: Amdt. 39-1454. Applies to Models 411 and 421 series airplanes.

Compliance: Required as indicated, unless already accomplished.

In order to detect auxiliary fuel cell leakage that could result in possible fire and explosion hazards from fuel vapor ignition, accomplish the following:

A) On Model 411 (Serial Numbers 411-0001 thru 411-0200) airplanes:

1) Within 10 hours' time in service after the effective date of this AD, and thereafter prior to the first flight of each day, visually inspect the lower surface of the wings in the area of the auxiliary fuel cells for fuel stains and leakage. If auxiliary fuel cell leakage is observed, prior to further flight, replace the auxiliary fuel cells with improved auxiliary fuel cells in accordance with Cessna Service Letter ME72-8, dated April 21, 1972, or any equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

2) The repetitive inspections required prior to the first flight of each day may be performed by the pilot, including pilots of aircraft engaged in air taxi 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.

3) On or before January 1, 1973, replace all auxiliary fuel cells with the improved auxiliary fuel cells specified in Cessna Service Letter ME72-8, dated April 21, 1972.

4) The repetitive inspections required in Paragraph A(1) may be discontinued when the improved auxiliary fuel cells are installed.

B) On Model 411 (Serial Numbers 411-0201 thru 411-0300) airplanes and on Model 421 (Serial Numbers 421-0001 thru 421B0048) airplanes, within 10 hours' time in service after the effective date of this AD and thereafter at intervals not to exceed 100 hours' time in service from the date of the last inspection, visually inspect the lower surface of the wings in the area of the auxiliary fuel cells for stains or leakage. If auxiliary fuel cell leakage is observed, prior to further flight, replace the auxiliary fuel cells with improved auxiliary fuel cells in accordance with Cessna Service Letter ME72-8, dated April 21, 1972, or any equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region. The repetitive inspections required in this paragraph may be discontinued when the improved auxiliary fuel cells are installed.

This amendment becomes effective June 2, 1972.

Affected TCDS · 1

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

Registered aircraft · 779

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
  • Cessna779 aircraft
By year built
19651993
Registered aircraft by year built: 514 aircraft
19653
19662
19673
196827
19699
19706
19716
197219
197350
197457
197554
197653
197751
197837
197936
198033
198136
198218
19832
19848
19853
19931

265 with no year recorded

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Aircraft

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