| AD Number | 76-02-06 | Status | Active |
| Effective Date | February 01, 1976 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2502 |
| Product Type | ["Aircraft"] | Product Subtype | ["Rotorcraft"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Bell Helicopter Textron, Inc. |
| Model(s) | 204B 205A-1 212 |
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.