| AD Number | 80-17-02 | Status | Active |
| Effective Date | August 08, 1980 | Issue Date | July 29, 1980 |
| Docket Number | Unknown | Amendment | 39-3872 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | --- - _EMPTY_ |
| Citation | This information is not available. | ||
| Manufacturer(s) | Piper Aircraft Inc. |
| Model(s) | PA-31 PA-31-325 PA-31-350 |
80-17-02 PIPER AIRCRAFT CORPORATION: Amendment 39-3872. Applies to the following Piper models of airplanes certificated in all categories: PA-31 and PA-31-325, S/N 31-7401201 through 31-8012076, 31-8012078, and 31-8012079; and PA-31-350, S/N 31-7405401 through 31-8052169 and 31-8052172.
Compliance is required within the next 50 hours time in service after the effective date of this AD unless already accomplished. To ensure flutter integrity of the elevator system, accomplish the following:
(a) Inspect the elevator balance weights for correct dimensions, and, if necessary, install correct elevator balance weights in accordance with Piper Aircraft Corporation Service Bulletin No. 690, dated July 7, 1980, or in an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, FAA, Southern Region.
(b) Revise the part numbers on both elevators in accordance with Piper Aircraft Corporation Service Bulletin No. 690, dated July 7, 1980, or in an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, FAA, Southern Region.
(c) Make appropriate maintenance record entry.
This amendment becomes effective August 8, 1980.