- Models
- 47B, 47B3, 47D, 47D1, 47E, 47G
- Data sheet
- TCDSH-1
- Registered aircraft
- 114 matched by model
- Product
- Aircraft · Rotorcraft
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 | 18 KB | 45e6ae80…72ac2bc | FAA DRS (API key needed) |
On this page
The airworthiness directive
54-24-01 BELL: Applies to All Models 47B, 47B3, 47D, 47D1, 47E, 47G Except 47G Serial Numbers 1286, 1287, 1294, 1295, and 1299 and Subsequent.
Compliance required no later than next 25-hour inspection.
In order to preclude improper installation of antitorque pedal assembly for dual controls, install two stop assemblies, P/N 47-722-165-1.
(Bell Mandatory Service Bulletin No. 98 dated October 29, 1954, covers this same subject and outlines the details for the installation.)
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 114
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1946 | 1 |
|---|---|
| 1947 | 10 |
| 1948 | 3 |
| 1949 | 3 |
| 1950 | 2 |
| 1951 | 6 |
| 1952 | 8 |
| 1953 | 7 |
| 1954 | 8 |
| 1955 | 4 |
| 1956 | 7 |
| 1957 | 3 |
| 1958 | 1 |
| 1959 | 3 |
| 1960 | 2 |
| 1963 | 6 |
| 1964 | 1 |
| 1965 | 3 |
| 1966 | 1 |
| 1967 | 2 |
| 1969 | 1 |
| 1972 | 1 |
| 1979 | 1 |
30 with no year recorded