| AD Number | 69-04-03 | Status | Active |
| Effective Date | March 22, 1969 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-724 |
| Product Type | ["Aircraft"] | Product Subtype | ["Rotorcraft"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Schweizer Aircraft Corporation |
| Model(s) | 269A 269A-1 269B |
69-04-03 HUGHES: Amdt. 39-724. Applies to Model 269A, 269A-1, 269A-2, and 269B helicopters with P/N 269A6035 low tip speed tail rotor blade installed.
To insure continued airworthiness of the low tip speed tail rotor blade, prior to accumulation of 5000 hours' time in service, remove tail rotor blade, P/N 269A6035, marking it permanently and conspicuously to avoid its inadvertent return to service, and replace with a new or serviceable tail rotor blade, P/N 269A6035, having less than 5000 hours' time in service.
This amendment becomes effective March 22, 1969.