- Holder
- Rolls-Royce Corporation
- Revision
- 32
- Revised
- November 1, 2019
- Status
- Current
- Product
- Engine
- Certification basis
- Part 27, Part 29, Part 33
- Models
- 23
- Registered
- 1,456 aircraft
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 23
| Model | Also known as | Note |
|---|---|---|
| 250-C30 | Formerly Detroit Diesel Allison of General Motors, then Allison Gas Turbine Division of General Motors, then Allison Engine Company, Inc., then Rolls-Royce Corporation (Indiana) | |
| 250-C30R (T703-AD-700) | (T703-AD-700) | Formerly Detroit Diesel Allison of General Motors, then Allison Gas Turbine Division of General Motors, then Allison Engine Company, then Inc. |
| 250-C47M | Formerly Rolls-Royce Corporation (Indiana) |
Airworthiness directives · 36
ADs whose products are models on this data sheet, matched by model and maker.
AD 2018-13-01Turbine GovernorAD 2006-20-07Adds an additional life limit for third- and fourth-stage turbine wheelsAD 2006-16-04Inspection of the fuel nozzle screen
See all 36 ADsRegistered aircraft
Registry models that point at this data sheet, with their registered aircraft.
Rolls-Royce 250-C47B537 registered aircraftAllison 250-C30 series224 registered aircraftRolls-Royce 250-C47E/4182 registered aircraft
See all 39 registry modelsSTCs approved under this data sheet · 6
STC SE00057ATInstallation of Aeronautical Accessories, Inc., Pc Safety Valve KitSTC SE00014ENInstallation of the Pratt & Whitney Engine Services, Inc. CrossCheck Engine Monitor Kit P/N HUMS-K-071-1, Rev. A on the specified PT6A engine models and kit P/N HUMS-K-071-2 on the specified A250 engine models.STC SE00026ENInstallation of Pratt & Whitney Engine Services Inc. IntelliStart Plus Electronic Control Unit (ECU), P/N DPU-K-010 on specified 250 engine models.STC SE578GLInstallation of a fuel flow transducer.STC ST00037ATUnison igniter plugs, P/N 9044400-1.STC SQ00338ATUnison igniter leads, P/N9048222-101, 102, 103, 104, 105, 106.