| AD Number | 71-24-02 | Status | Active |
| Effective Date | November 24, 1971 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-1334 |
| Product Type | ["Aircraft"] | Product Subtype | ["Rotorcraft"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | FH1100 Manufacturing Corporation |
| Model(s) | 1100 FH-1100 |
71-24-02 FAIRCHILD HILLER ROTORCRAFT: Amdt. 39-1334. Applies to Model 1100 and FH-1100 Type Helicopters certificated in all categories.
Compliance required as indicated.
To preclude fatigue failure of the transmission mount strut, P/N 24-28031, due to internal corrosion, accomplish the following:
Within the next 30 days after the effective date of this AD, unless already accomplished replace P/N 24-28031 left side, lateral, adjustable transmission strut with P/N 24-28031-11 strut in accordance with Section 28 of the FH-1100 Service Manual or an alternate method approved by the Chief, Engineering & Manufacturing Branch, FAA, Eastern Region. Upon installation of MS-21252 fork fitting apply RTV-102 sealant or equivalent to the threads of fitting and under AN316-5R retaining nut.
This amendment is effective November 24, 1971.