- 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.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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| FAA DRS HTML | 25 KB | afbdf8dd…99cde06 | FAA DRS (API key needed) |
On this page
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.
| 1965 | 3 |
|---|---|
| 1966 | 2 |
| 1967 | 3 |
| 1968 | 27 |
| 1969 | 9 |
| 1970 | 6 |
| 1971 | 6 |
| 1972 | 19 |
| 1973 | 50 |
| 1974 | 57 |
| 1975 | 54 |
| 1976 | 53 |
| 1977 | 51 |
| 1978 | 37 |
| 1979 | 36 |
| 1980 | 33 |
| 1981 | 36 |
| 1982 | 18 |
| 1983 | 2 |
| 1984 | 8 |
| 1985 | 3 |
| 1993 | 1 |
265 with no year recorded