- Effective
- June 13, 1996
- Published
- May 9, 1996 · 61 FR 21071–21073
- Model
- 76E Series
- Data sheet
- TCDSP4EA
- Product
- Propeller
- Amendment
- 39-9583
- Docket
- 95-ANE-03
- Issued as
- Final rule
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| Official PDF | 126 KB | 0a1076c4…0cd21ed | 96-11257.pdf on govinfo.gov |
| FAA DRS HTML | 34 KB | 946fad86…f4937df | FAA DRS (API key needed) |
| Federal Register text | 13 KB | b3b03699…b0de57c | 96-11257.txt on federalregister.gov |
On this page
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft
No registered aircraft matched this AD’s modelsForeign aircraft aren’t included, and ADs on propellers and appliances aren’t matched by model.
NTSB investigations that cite this AD · 5
Their narratives or probable cause name AD 69-09-03, often to say whether the aircraft complied with it.
NTSB CEN11LA555Accident · No injuriesLimited investigationFinal reportPiper PA-28-180 · Millsap, TXA sudden loss of engine thrust due to the separation of a propeller blade in cruise flight due to high cycle fatigue.NTSB CEN09LA132Accident · No injuriesLimited investigationFinal reportGrumman American Avn. AA-5B · Milford, INA loss of engine thrust due to the separation of a section of one of the propeller blades as a result of fatigue failure of the propeller because of corrosion. Contributing to the accident was the failure of the mechanic to detect and address the propeller…NTSB DFW08LA094Accident · No injuriesLimited investigationFinal reportPiper PA-28-180 · Paducah, TXFatigue failure and separation of the propeller during cruise flight. Contributing to the accident was the owner's failure to comply with a long standing Airworthiness Directive.NTSB BFO96LA015Accident · No injuriesLimited investigationFinal reportPiper PA-28-180 · Lebanon, VAfailure of the propeller blade due to fatigue cracking originating from corrosion damage. A related factor was the soft terrain encountered during the forced landing.NTSB ANC95LA160Accident · Serious injuriesLimited investigationFinal reportCessna 172N · Glennallen, AKImproper planning/decision by the pilot, which resulted in fuel exhaustion, due to an inadequate supply of fuel. A factor relating to the accident was: the lack of suitable terrain for an emergency landing.