- Effective
- August 5, 1977
- Published
- August 1, 1977
- Issued
- July 21, 1977
- Model
- PA-30
- Data sheet
- TCDSA1EA
- Registered aircraft
- 878 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-2991
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 | 8c548361…f1cb346 | FAA DRS (API key needed) |
On this page
The airworthiness directive
69-24-04 PIPER: Amendment 39-878 as amended by amendment 39-896 is further amended by Amendment 39-2991. Applies to Piper PA-30 type airplanes certificated in all categories except aircraft incorporating Piper Kit No. 760 368.
Compliance required before further flight, unless already accomplished, as follows:
Change the existing Vmc placard to state the following:
"Minimum Single Engine Control Speed 90 mph CAS".
(Piper Service Bulletin 301A dated November 25, 1969 pertains to this subject.)
Amendment 39-878 was effective November 27, 1969.
Amendment 39-896 was effective December 26, 1969.
This Amendment 39-2991 is effective August 5, 1977.
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
By model
Aircraft
NTSB investigations that cite this AD · 2
Their narratives or probable cause name AD 69-24-04, often to say whether the aircraft complied with it.