| AD Number | 65-14-01 | Status | Active |
| Effective Date | June 26, 1965 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-96 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | Federal Register: June 26, 1965 | ||
| Manufacturer(s) | Textron Aviation Inc. |
| Model(s) | 35-33 H35 J35 K35 |
65-14-01 BEECH: Amdt. 39-96 Part 39 Federal Register June 26, 1965. Applies to Models H35, J35, K35, and 35-33 Series Aircraft Equipped with Ellingsworth Products Co., Inc. Alternator Kit Number 195860 Installed Under STC SA1-377.
Compliance required within the next 25 hours' time in service after the effective date of this AD, and thereafter at intervals not to exceed 50 hours' time in service from the last inspection.
To prevent further failures of the alternator support bracket, accomplish the following:
(a) Remove alternator supporting brackets, P/N's 195814, 195820, 195836, 195838, 195840 and 626131, thoroughly clean and inspect for elongated bolt holes.
(b) Inspect brackets not having elongated bolt holes, for cracks using dye penetrant or magnetic particle method or FAA-approved equivalent.
(c) Replace brackets having elongated bolt holes or cracks with unused parts of the same part number or FAA-approved equivalent before further flight.
(d) Upon request of the operator, and FAA maintenance inspector, subject to prior approval of the Chief, Engineering and Manufacturing Branch, FAA Eastern Region, may adjust the repetitive inspection intervals specified in this AD to permit compliance at an established inspection period of the operator if the request contains substantiating data to justify the increase for such operator.
This directive effective June 26, 1965.