| AD Number | 76-06-06 | Status | Active |
| Effective Date | March 25, 1976 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2547 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | FS 2003 Corp. |
| Model(s) | PA-12 PA-12S |
76-06-06 PIPER AIRCRAFT CORPORATION: Amendment 39-2547. Applies to Piper Model PA-12 airplanes certificated in all categories equipped with Piper Model PA-14 wing flaps in accordance with STC No. SA231AL.
NOTE: STC No. SA231AL incorporates Rodney E. Schaeffer Drawing PA-12-1001, Revision "A", dated September 15, 1975.
Compliance is required within the next 50 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent a loss of flap control, inspect the flap control system to ensure that six flap control pulley guards are installed in accordance with the Rodney E. Schaeffer Drawing PA-12- 1001, Revision "A", dated September 15, 1975, or an FAA approved equivalent. Install those pulley guards which are found to be missing.
NOTE: Copies of the Rodney E. Schaeffer Drawing PA-12-1001, Revision "A", dated September 15, 1975, may be obtained from Rodney E. Schaeffer, 1253 Cramer, Wichita, Kansas, 67212. This drawing may also be examined at the FAA Alaska Region, 632 Sixth Avenue, Anchorage, Alaska 99501, and at FAA Headquarters, 800 Independence Avenue, S.W., Washington, D.C. 20591.
This amendment becomes effective on March 25, 1976.