AD 96-15-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | Pratt & Whitney Division | JT8D-209 | PRATT & WHITNEY Model JT8D-200 Series Engines |
| engine | Pratt & Whitney Division | JT8D-217 | PRATT & WHITNEY Model JT8D-200 Series Engines |
| engine | Pratt & Whitney Division | JT8D-217A | PRATT & WHITNEY Model JT8D-200 Series Engines |
| engine | Pratt & Whitney Division | JT8D-217C | PRATT & WHITNEY Model JT8D-200 Series Engines |
| engine | Pratt & Whitney Division | JT8D-219 | PRATT & WHITNEY Model JT8D-200 Series Engines |
Unsafe Condition
Fatigue crack initiation and propagation in the first stage fan hubs, Part Number 5000501-01, leading to fan hub fracture and potential uncontained engine failure and damage to the aircraft.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Remove from service affected first stage fan hubs with specified serial numbers (T50693, T50823, T50827, R32926, R32960, P66756) and replace with serviceable parts. Alternative methods of compliance may be approved by the Manager, Engine Certification Office.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Pratt & Whitney JT8D-209, JT8D-217, JT8D-217A, JT8D-217C, JT8D-219 engines with first stage fan hubs, Part Number 5000501-01, serial numbers T50693, T50823, T50827, R32926, R32960, P66756. These engines are installed on but not limited to McDonnell Douglas MD-80 series aircraft.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.