- Effective
- August 15, 1967
- Models
- 200, 200A, 200B, 200C, 200D
- Data sheet
- TCDS3A18
- Registered aircraft
- 83 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-457
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 | 20 KB | b2318add…ff1aec8 | FAA DRS (API key needed) |
On this page
The airworthiness directive
67-23-01 AERO COMMANDER: Amdt. 39-457, Part 39, Federal Register August 5, 1967. Applies to Aero Commander (Meyers) Model 200 Series Airplanes, Serial Numbers 255, 256, 260, 262, 263, 268, 272, 273, 275, 276, 277, 278, 279, 281, 282, 286, 287, 288, 289, 290, 291, 296, 306, 308, 309, 328, 329, 331, 338, and 353.
Compliance required within the next 25 hours' time in service after effective date of this AD unless already accomplished.
To detect improper rigging of the main landing gear emergency extension and down lock mechanism, accomplish the following:
Inspect and adjust each main landing gear in accordance with Aero Commander, Albany Division, Service Bulletin 2004, dated February 10, 1967, or later FAA approved revision, or in a manner approved by the Chief, Engineering and Manufacturing Branch, FAA Southern Region.
This amendment effective August 15, 1967.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 83
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1959 | 1 |
|---|---|
| 1960 | 2 |
| 1961 | 3 |
| 1962 | 5 |
| 1963 | 4 |
| 1964 | 4 |
| 1965 | 3 |
| 1966 | 37 |
| 1967 | 13 |
11 with no year recorded