2010-18-13: Blade
FAA order 2010-18-13 is an airworthiness directive in force since October 18, 2010. The FAA's subject line: Blade. It names the Pratt & Whitney PW4052, Pratt & Whitney PW4056, Pratt & Whitney PW4060, Pratt & Whitney PW4062, Pratt & Whitney PW4062A, Pratt & Whitney PW4090, Pratt & Whitney PW4158, Pratt & Whitney PW4168A, Pratt & Whitney PW4460, Pratt & Whitney PW4462 engines: about 145 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: engine.
What it applies to as the FAA lists it
- Kind of product
- Engine
- Makes
- Pratt & Whitney Division
- Models
- PW4052, PW4056, PW4060, PW4062, PW4062A, PW4074, PW4077, PW4077D, PW4084D, PW4090, PW4090-3, PW4152, PW4156A, PW4158, PW4164, PW4168, PW4168A, PW4460, PW4462
- Engine series
- Pratt & Whitney PW4052 1 aircraft
Pratt & Whitney PW4056 25 aircraft
Pratt & Whitney PW4060 14 aircraft
Pratt & Whitney PW4062 6 aircraft
Pratt & Whitney PW4062A 2 aircraft
Pratt & Whitney PW4090 2 aircraft
Pratt & Whitney PW4158 65 aircraft
Pratt & Whitney PW4168A 12 aircraft
Pratt & Whitney PW4460 10 aircraft
Pratt & Whitney PW4462 8 aircraft
Dates and paperwork
- In force since
- October 18, 2010
- Published
- September 13, 2010 (signed August 26, 2010)
- Docket
- FAA-2010-0217
- Replaced by
- 2012-18-17
- Status
- Historical
- The FAA's document
- Read the order on the FAA's site
The FAA's summary their words, unchanged
The FAA is adopting a new airworthiness directive (AD) for PW PW4052, PW4056, PW4060, PW4062, PW4062A, PW4074, PW4077, PW4077D, PW4084D, PW4090, PW4090-3, PW4152, PW4156A, PW4158, PW4164, PW4168, PW4168A, PW4460, and PW4462 turbofan engines. This AD requires initial and repetitive fluorescent penetrant inspections (FPI) for cracks in the blade locking and loading slots of the high-pressure compressor (HPC) drum rotor disk assembly. This AD results from reports of cracked locking and loading slots in the HPC drum rotor disk assembly. We are issuing this AD to detect cracks in the locking and loading slots in the HPC drum rotor disk assemblies, which could result in rupture of the HPC drum rotor disk assembly and damage to the airplane.
The order itself the regulatory text, as published
Show the full text (4,143 characters)
Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 7, 2026. Connections as data: /graph/directive/2010-18-13.json · aircraft systems.
