| AD Number | 77-24-01 | Status | Active |
| Effective Date | April 17, 1978 | Issue Date | April 03, 1978 |
| Docket Number | Unknown | Amendment | 39-3182 |
| 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 |
77-24-01 PIPER: Amendment 39-3083 as amended by Amendment 39-3182. Applies to the following models: PA-31 and PA-31-325, Serial Nos. 31-465, 31-7712057 thru 31-7712078, 31-7712081 and 31-7712083; PA-31-350 Serial Nos. 31-7752099, 31-7752101, 31-7752103, 31- 7752105 thru 31-7752114, 31-7752117 thru 31-7752131 and 31-7752134 thru 31-7752138, certificated in all categories.
To prevent possible hazards in flight associated with missing horizontal stabilizer and fin skin to stiffener rivet attachments, accomplish the following within the next fifty hours in service from the effective date of this AD unless previously accomplished:
(a) Inspect and, if required, repair the horizontal stabilizer and fin skin to stiffener rivet attachments in accordance with the "Instructions" section of Piper Service Bulletin No. 575 or equivalent procedures which must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
(b) Upon submission of substantiatingdata through an FAA Maintenance Inspector, the compliance time specified in this AD may be increased by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
The affected airplanes may be flown in accordance with FAR 21.197 to a location where the AD compliance procedures can be accomplished.
Amendment 39-3083 was effective November 24, 1977.
This amendment 39-3182 is effective April 17, 1978.