- Effective
- January 18, 1962
- Published
- January 18, 1962
- Model
- PA-25
- Registered aircraft
- 59 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 May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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On this page
The airworthiness directive
62-02-06 PIPER: Amdt. 387 Part 507 Federal Register January 18, 1962. Applies to Model PA-25 Aircraft, Serial Numbers 25-1 to 25-619 Inclusive, 25-622, 25-623, 25-625, and 25-626.
Compliance required as indicated.
As a result of inspections performed on the aluminum front spar wing-to-fuselage attachment fittings, Piper P/N's 61111-00 and 61111-01, it has been determined that the following action is necessary. Within the next 25 hours' time in service after the effective date of this AD, but not later than February 15, 1962, unless already accomplished, replace the aluminum front spar wing-to-fuselage attachment fittings, Piper P/N's 61111-00 and 61111-01, with steel forgings, Piper P/N's 60113-00 and 60113-01, or equivalent parts approved by the FAA Eastern Region, Engineering and Manufacturing Branch. The steel forgings have 1/8 inch raised digits "60112" or "60112-1" on the parts.
The replacement shall be accomplished in accordance with Piper Service BulletinNo. 206, dated August 24, 1961, or FAA approved equivalent.
(Piper Service Bulletin No. 206, dated August 24, 1961, pertains to this subject.)
This supersedes AD 61-13-02.
This directive effective January 18, 1962.
Registered aircraft · 59
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1959 | 6 |
|---|---|
| 1960 | 32 |
| 1961 | 7 |
| 1962 | 3 |
| 1963 | 1 |
10 with no year recorded