- Effective
- August 4, 1970
- Published
- July 30, 1970
- Issued
- July 13, 1970
- Model
- PA-30
- Data sheet
- TCDSA1EA
- Registered aircraft
- 878 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-1044
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 | 19 KB | f6f53715…70744e1 | FAA DRS (API key needed) |
On this page
The airworthiness directive
70-15-17 PIPER AIRCRAFT: Amdt. 39-1044. Applies to Piper PA-30 type airplanes, serial numbers 30-1 through 30-852 and 30-854 through 30-901, certificated in all categories.
Before further flight, attach the following operating limitation placard to the airspeed indicator in full view of the pilot:
"DO NOT EXCEED 230 MPH CAS."
This amendment is effective August 4, 1970 and was effective for all recipients of the airmail notice, dated 2 July 1970, which contained this amendment.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 878
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1957 | 1 |
|---|---|
| 1963 | 82 |
| 1964 | 158 |
| 1965 | 101 |
| 1966 | 172 |
| 1967 | 103 |
| 1968 | 36 |
| 1969 | 102 |
123 with no year recorded