- Effective
- November 29, 1967
- Models
- 150G, 150H
- Data sheet
- TCDS3A19
- Registered aircraft
- 1,733 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-516
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.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 19 KB | 33aa38c7…e0c38c7 | FAA DRS (API key needed) |
On this page
The airworthiness directive
67-31-04 CESSNA: Amdt. 39-516, Part 39, Federal Register November 29, 1967. Applies to Models 150G and 150H Airplanes, Serial Numbers 15064533 through 15067891.
To prevent loss of longitudinal control, unless already accomplished, prior to further flight, remove the glove compartment from the aircraft.
If after it is removed the glove compartment is modified, the modification must be approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Central Region, before it is reinstalled in the aircraft and the aircraft returned to service.
This amendment effective November 29, 1967, for all persons except those to whom it was made effective by air mail letter dated November 17, 1967.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 1,733
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1966 | 442 |
|---|---|
| 1967 | 588 |
| 1968 | 356 |
| 1971 | 1 |
346 with no year recorded