- Models
- GC-1A, GC-1B
- Data sheet
- TCDSA-766
- Registered aircraft
- 541 matched by model
- Product
- Aircraft · Small airplane
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 | 7c8cc569…1435908 | FAA DRS (API key needed) |
On this page
The airworthiness directive
47-06-02 GLOBE: (Was Mandatory Note 5 of AD-766-5.) Applies to Models GC-1A and GC-1B Aircraft Serial Numbers 3 to 408 Inclusive; 1004 to 1319 Inclusive; and 2001 to 2239 Inclusive.
Compliance required prior to April 1, 1947.
Replace the warning placard located at the landing gear emergency extension crank with a revised placard, Globe P/N 11-532-3735, having the added instruction: "Crank back to the full up position before the next retraction of the landing gear". Complete rewinding is necessary to prevent damage to the retraction system.
(Globe Customer Service Maintenance Bulletin No. 6 covers this same subject.)
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 541
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1945 | 1 |
|---|---|
| 1946 | 317 |
| 1947 | 7 |
| 1948 | 80 |
| 1949 | 10 |
| 1950 | 11 |
| 1951 | 3 |
| 1952 | 1 |
| 1953 | 1 |
| 1954 | 1 |
| 1956 | 3 |
| 1957 | 1 |
| 1978 | 1 |
104 with no year recorded