| AD Number | 82-04-08 | Status | Active |
| Effective Date | February 25, 1982 | Issue Date | February 10, 1982 |
| Docket Number | Unknown | Amendment | 39-4323 |
| 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-34-220T |
82-04-08 PIPER AIRCRAFT CORPORATION: Amendment 39-4323. Applies to Piper Model PA-34-220T (Serial Numbers 34-8133001 through 34-8233020) airplanes certificated in any category.
Compliance: Required as indicated unless already accomplished.
To prevent a potentially hazardous condition during landing and ground operation due to the inadvertent retraction of the landing gear, accomplish the following:
A) Within the next 50 hours time-in-service after the effective date of this AD, inspect and modify the landing gear selector and squat switches in accordance with the Instructions Section contained in Piper Service Bulletin No. 732, dated November 11, 1981.
B) Any equivalent method of compliance may be approved by the Chief, Atlanta Aircraft Certification Office, FAA, Southern Region, Room 275, 3400 Norman Berry Drive, East Point, Georgia 30344.
This amendment becomes effective February 25, 1982.