- Effective
- June 7, 1963
- Published
- June 7, 1963
- Issued
- May 31, 1963
- Model
- PA-23
- Data sheet
- TCDS1A10
- Registered aircraft
- 155 matched by model
- Product
- Aircraft · Small airplane
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed November 21, 2025.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 21 KB | d6d3dd19…d6a274b | FAA DRS (API key needed) |
On this page
The airworthiness directive
63-12-02 PIPER: Amdt. 572 Part 507 Federal Register June 7, 1963. Applies to Model PA-23 Aircraft Serial Numbers 23-1 Through 23-1284, and 23-1286.
Compliance required as indicated.
Due to cracks being found in the P/N 17058-3 elevator butt rib and the P/N 17058-20 elevator butt rib doubler plate, which parts are incorporated in the P/N 17058-00 elevator assembly originally installed on the above serial numbered aircraft, the following shall be accomplished:
(a) Within the next 50 hours' time in service after the effective date of this AD, unless already accomplished within the last 50 hours' time in service, and within every 100 hours' time in service thereafter visually inspect for cracks, elevator butt rib, P/N 17058-3 and elevator butt rib plate, P/N 17058-20 on the P/N 17058-00 elevator assembly. Replace cracked parts before further flight.
(b) After P/N 19446 elevator assembly is installed, the inspection specified in (a) is no longer required.
(c) Parts shall be assembled and installed to obtain proper alinement and to prevent distortion and over-torquing of the attachment bolts.
(Piper Service Bulletin No. 146B, dated October 25, 1962, pertains to this same subject.)
This directive effective June 7, 1963.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 155
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1954 | 9 |
|---|---|
| 1955 | 34 |
| 1956 | 34 |
| 1957 | 37 |
| 1958 | 1 |
| 1963 | 1 |
39 with no year recorded