| AD Number | 78-22-07 | Status | Active |
| Effective Date | November 15, 1978 | Issue Date | October 23, 1978 |
| Docket Number | Unknown | Amendment | 39-3332 |
| 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-32RT-300 PA-32RT-300T |
78-22-07 PIPER AIRCRAFT CORPORATION: Amendment 39-3332. Applies to the following model PA-32RT-300 and PA-32RT-300T aircraft, certificated in all categories:
PA-32RT-300 Lance II
32R-7885001 to 32R-7885216 Inclusive
32R-7885218 to 32R-7885253 Inclusive
32R-7885255, 32R-7885257 to 32R-7885260 Inclusive
PA-32RT-300T Turbo Lance II
32R-7887001 to 32R-7887110 Inclusive
32R-7887112 to 32R-7887173 Inclusive
32R-7887175 to 32R-7887182 Inclusive
32R-7887184 to 32R-7887196 Inclusive
32R-7887198 to 32R-7887201 Inclusive
32R-7887203 to 32R-7887205 Inclusive
32R-7887207, 32R-7887208, 32R-7887210,
32R-7887212 to 32R-7887215 Inclusive
32R-7887217, 32R-7887218, 32R-7887220,
32R-7887222, 32R-7887224 and 32R-7887226.
Compliance required within the next 10 hours of operation, or at the next regularly scheduled or annual inspection, whichever occurs first.
To insure full travel of the control column, replace the control column stop sleeve and checkcontrol column travel and stabilator travel in accordance with the instructions contained in Piper Service Bulletin 619 (and Control Column Stop Modification Kit Number 763 895V) or later revision approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region, or in an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region.
This amendment becomes effective November 15, 1978.