- Effective
- February 1, 1976
- Models
- 204B, 205A-1, 212
- Registered aircraft
- 125 matched by model
- Product
- Aircraft · Rotorcraft
- Amendment
- 39-2502
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 | 19 KB | ec45d9f1…68262d6 | FAA DRS (API key needed) |
On this page
The airworthiness directive
76-02-06 BELL: Amendment 39-2502. Applies to Bell Models 212, 204B, and 205A-1 helicopters certificated in all categories.
Compliance required as indicated after receipt of this AD.
Prior to next flight, remove the main rotor blades having the following Serial Numbers: A2-28211, A2-29920, A2-29325, A2-28198, A2-27872, A2-28195, A2-29315, A2-29919, A2- 29334, A2-29915, A2-28016, A2-27961, A2-27982, A2-27963, A2-28023, A2-28015, A2-28019, A2-27968, A2-27967, A2-28020, A2-03642, A2-03646, and A2-03643.
This supersedes airmail letter dated December 24, 1975, and Amendment 39-2488 (41 F.R. 1738), AD 76-01-05.
This amendment is effective February 1, 1976, and was effective upon receipt for all recipients of the letter dated January 8, 1976, which contained this amendment.
Affected TCDS · 2
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 125
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1965 | 1 |
|---|---|
| 1966 | 1 |
| 1967 | 1 |
| 1968 | 5 |
| 1969 | 3 |
| 1970 | 2 |
| 1971 | 3 |
| 1972 | 5 |
| 1973 | 7 |
| 1974 | 11 |
| 1975 | 9 |
| 1976 | 5 |
| 1977 | 5 |
| 1978 | 3 |
| 1979 | 14 |
| 1980 | 12 |
| 1981 | 4 |
| 1982 | 4 |
| 1984 | 1 |
| 1991 | 1 |
| 1993 | 2 |
| 1995 | 1 |
25 with no year recorded