# TCDS E1GL: Rolls-Royce Corporation - Type: Type certificate data sheet - Status: Current - Holder: Rolls-Royce Corporation - Revision: 32 - Revised: November 1, 2019 - Product: Engine - Certification basis: Part 27, Part 29, Part 33 - Registered aircraft: 1,456, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/5e/4a/5e4ad71fee5726835fbdbcb369c62542828c57ee34090ba4a05677e0297a13b4 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9BEDE563533F0B28862584B1004D18E5.0001 - Page: https://openairdocs.org/tcds/E1GL ## Models (23) As the data sheet lists them. - 250-C30 - 250-C30R (T703-AD-700) ((T703-AD-700)) - 250-C47M - 250-C30R/1 (T703-AD-700B) ((T703-AD-700B)) - 250-C28 - 250-C30U - 250-C30R/3M - 250-C30R/3 - 250-C30S - 250-C30G - 250-C30P - 250-C30M - 250-C28C - 250-C40B - 250-C47B - 250-C28B - 250-C30G/2 - 250-C47B/8 - 250-C47E - 250-C30R/3D - 250-C47E/1 - 250-C47E/4 - 250-C30R/3M7 ## ADs (36, in force first) - [AD 2018-13-01](https://openairdocs.org/ad/2018-13-01): Turbine Governor · Rolls-Royce 250-C10 (T63-A-5), 250-C18, 250-C18A and 24 more. Effective Aug 16, 2018 - [AD 2006-20-07](https://openairdocs.org/ad/2006-20-07): Adds an additional life limit for third- and fourth-stage turbine wheels · Rolls-Royce 250-C30, 250-C30G, 250-C30G/2 and 11 more. Effective Nov 2, 2006 - [AD 2006-16-04](https://openairdocs.org/ad/2006-16-04): Inspection of the fuel nozzle screen · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 43 more. Effective Sep 7, 2006 - [AD 2005-20-11](https://openairdocs.org/ad/2005-20-11): Airfoils at the hub and shroud of third-stage turbine wheels · Rolls-Royce 250-C28, 250-C28B and 250-C28C. Effective Oct 18, 2005 - [AD 2004-24-04](https://openairdocs.org/ad/2004-24-04): Hydromechanical unit (HMU) Power Lever Angle (PLA) potentiometer · Rolls-Royce 250-C30R/3, 250-C30R/3M, 250-C47B and 1 more. Effective Jan 3, 2005 - [AD 2004-14-02](https://openairdocs.org/ad/2004-14-02): SN third-stage turbine wheels · Rolls-Royce 250-C28, 250-C28B and 250-C28C. Effective Jul 26, 2004 - [AD 2002-06-08](https://openairdocs.org/ad/2002-06-08): Third Stage Turbine Wheels · Rolls-Royce 250-C28, 250-C28B and 250-C28C. Effective Apr 26, 2002 - [AD 98-24-28](https://openairdocs.org/ad/98-24-28): Main Fuel Control Bellows · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 36 more. Effective Jan 7, 1999 - [AD 98-10-03](https://openairdocs.org/ad/98-10-03): Hydromechanical Unit · Rolls-Royce 250-C47B. Effective May 26, 1998 - [AD 97-25-09](https://openairdocs.org/ad/97-25-09): Helical Power Takeoff Gearshaft Assembly · Rolls-Royce 250-C40B. Effective Dec 23, 1997 - [AD 96-19-01](https://openairdocs.org/ad/96-19-01): Superior Air Parts Manufacture Approval (PMA) Bearings · Rolls-Royce 250-B15G, 250-B17F, 250-B17F/1 and 17 more. Effective Sep 26, 1996 - [AD 89-23-12](https://openairdocs.org/ad/89-23-12): Turbine Nozzle Assembly · Rolls-Royce 250-C28B and 250-C28C. Effective Oct 29, 1989 - [AD 88-17-01](https://openairdocs.org/ad/88-17-01): Fuel Controls · Rolls-Royce 250-B17, 250-B17B, 250-B17C and 26 more. Effective Mar 1, 1989 - [AD 88-07-06](https://openairdocs.org/ad/88-07-06): Gas Producer Support Pressure Oil Tube Assembly · Rolls-Royce 250-C30, 250-C30M, 250-C30P and 2 more. Effective Mar 30, 1988 - [AD 86-20-13](https://openairdocs.org/ad/86-20-13): External Splines · Rolls-Royce 250-C28B, 250-C28C, 250-C30 and 9 more. Effective Dec 3, 1986 - [AD 86-19-12](https://openairdocs.org/ad/86-19-12): Gas Producer Turbine Rotor · Rolls-Royce 250-C30, 250-C30G, 250-C30G/2 and 7 more. Effective Oct 3, 1986 - [AD 85-25-07 R1](https://openairdocs.org/ad/85-25-07-R1): Outer Combustion Case Assembly · Rolls-Royce 250-C28, 250-C28B, 250-C28C and 10 more. Effective Aug 15, 1986 - [AD 86-16-03](https://openairdocs.org/ad/86-16-03): Scavenge Line Air/Oil Centrifugal Separator Assembly · Rolls-Royce 250-C28B and 250-C28C. Effective Aug 13, 1986 - [AD 84-24-54 R2](https://openairdocs.org/ad/84-24-54-R2): Gas Producer Turbine Rotor · Rolls-Royce 250-C30, 250-C30P, 250-C30R (T703-AD-700) and 1 more. Effective Jan 6, 1986 - [AD 85-25-08](https://openairdocs.org/ad/85-25-08): Compressor Mount Assembly · Rolls-Royce 250-C28B, 250-C28C, 250-C30 and 2 more. Effective Jan 6, 1986 - [AD 85-25-09](https://openairdocs.org/ad/85-25-09): Turbine Shafts And Couplings · Rolls-Royce 250-C28B and 250-C28C. Effective Jan 6, 1986 - [AD 85-25-12](https://openairdocs.org/ad/85-25-12): Turbine-To-Compressor-Coupling · Rolls-Royce 250-C28B and 250-C28C. Effective Jan 6, 1986 - [AD 85-06-51](https://openairdocs.org/ad/85-06-51): Magnetic Plugs · Rolls-Royce 250-C30 and 250-C30S. Effective May 10, 1985 - [AD 84-17-51](https://openairdocs.org/ad/84-17-51): Turbine Rotor Assembly · Rolls-Royce 250-C30 and 250-C30S. Effective Dec 26, 1984 - [AD 81-13-12 R1](https://openairdocs.org/ad/81-13-12-R1): 4th Stage Turbine Nozzle Assembly · Rolls-Royce 250-C30, 250-C30P and 250-C30S. Effective Sep 26, 1983 - [AD 83-01-04](https://openairdocs.org/ad/83-01-04): Turbine Assemblies · Rolls-Royce 250-C28B and 250-C28C. Effective Jan 24, 1983 - [AD 82-24-05](https://openairdocs.org/ad/82-24-05): Control Assembly and Power Turbine Governor Assembly · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 43 more. Effective Nov 26, 1982 - [AD 82-03-02](https://openairdocs.org/ad/82-03-02): N2 (Electronic) Overspeed Control System · Rolls-Royce 250-C28B. Effective Feb 4, 1982 - [AD 79-16-06](https://openairdocs.org/ad/79-16-06): Accessory Drive Gearbox · Rolls-Royce 250-C28, 250-C28B, 250-C28C and 10 more. Effective Jan 11, 1980 - [AD 79-18-13](https://openairdocs.org/ad/79-18-13): Third Stage Turbine Wheel · Rolls-Royce 250-C28B and 250-C28C. Effective Sep 6, 1979 - [AD 79-06-05](https://openairdocs.org/ad/79-06-05): Overspeed Control System · Rolls-Royce 250-C28B and 250-C30. Effective Mar 26, 1979 - [AD 78-26-01](https://openairdocs.org/ad/78-26-01): Engine Electrical System · Rolls-Royce 250-C28B. Effective Nov 3, 1978 - [AD 2004-24-09](https://openairdocs.org/ad/2004-24-09) (historical): Fuel nozzle · Rolls-Royce 250-B15A, 250-B15E, 250-B15G and 40 more. Effective Jan 5, 2005 - [AD 2003-13-10](https://openairdocs.org/ad/2003-13-10) (historical): Hydromechanical unit (HMU) power lever angle (PLA) · 250-C30R/3, 250-C30R/3M, 250-C47B and 1 more. Effective Jul 15, 2003 - [AD 97-21-09](https://openairdocs.org/ad/97-21-09) (historical): Engine Main Electrical Harness Assembly · 250-C47B. Effective Dec 3, 1997 - [AD 96-24-09](https://openairdocs.org/ad/96-24-09) (historical): Engine Main Electrical Harness Assembly · 250-C47B. Effective Nov 25, 1996 ## Registered aircraft by registry model (OpenAirDocs) - [Rolls-Royce 250-C47B](https://openairdocs.org/engine/rolls-royce-250-c47b): 537 aircraft (registry code 54585) - [Allison 250-C30 series](https://openairdocs.org/engine/allison-250-c30-series): 224 aircraft (registry code 03015) - [Rolls-Royce 250-C47E/4](https://openairdocs.org/engine/rolls-royce-250-c47e-4): 182 aircraft (registry code 54236) - [Rolls-Royce 250-C30P](https://openairdocs.org/engine/rolls-royce-250-c30p): 152 aircraft (registry code 54013) - [Allison 250-C47](https://openairdocs.org/engine/allison-250-c47-series): 123 aircraft (registry code 03029) - [Rolls-Royce 250-C30](https://openairdocs.org/engine/rolls-royce-250-c30): 76 aircraft (registry code 54023) - [Allison 250-C28 series](https://openairdocs.org/engine/allison-250-c28-series): 43 aircraft (registry codes 03022, 03021) - [Allison 250-C30P](https://openairdocs.org/engine/allison-250-c30p): 25 aircraft (registry code 03099) - [Rolls-Royce 250-C40B](https://openairdocs.org/engine/rolls-royce-250-c40b): 19 aircraft (registry code 54525) - [Rolls-Royce 250-C47 series](https://openairdocs.org/engine/rolls-royce-250-c47-series): 16 aircraft (registry code 54235) - [Allison 250-C47B](https://openairdocs.org/engine/allison-250-c47b): 15 aircraft (registry code 03109) - [Rolls-Royce 250-C47M](https://openairdocs.org/engine/rolls-royce-250-c47m): 13 aircraft (registry code 54020) - [Allison 250-C28B](https://openairdocs.org/engine/allison-250-c28b): 5 aircraft (registry code 03114) - [Allison 250-C30](https://openairdocs.org/engine/allison-250-c30): 5 aircraft (registry code 03097) - [Allison 250-C47M](https://openairdocs.org/engine/allison-250-c47m): 3 aircraft (registry code 03110) - [Rolls-Royce 250-C28B](https://openairdocs.org/engine/rolls-royce-250-c28b): 3 aircraft (registry code 54010) - [Rolls-Royce 250-C30G](https://openairdocs.org/engine/rolls-royce-250-c30g): 3 aircraft (registry code 54016) - [Rolls-Royce 250-C30G/2](https://openairdocs.org/engine/rolls-royce-250-c30g-2): 3 aircraft (registry code 54018) - [Rolls-Royce 250-C30S](https://openairdocs.org/engine/rolls-royce-250-c30s): 2 aircraft (registry code 54012) - [Allison 250-C30G/2](https://openairdocs.org/engine/allison-250-c30g-2): 1 aircraft (registry code 03105) - [Allison 250-C40B](https://openairdocs.org/engine/allison-250-c40b): 1 aircraft (registry code 03108) - [Rolls-Royce 250-C28](https://openairdocs.org/engine/rolls-royce-250-c28): 1 aircraft (registry code 54009) - [Rolls-Royce 250-C30M](https://openairdocs.org/engine/rolls-royce-250-c30m): 1 aircraft (registry code 54014) - [Rolls-Royce 250-C30R](https://openairdocs.org/engine/rolls-royce-250-c30r): 1 aircraft (registry code 54015) - [Rolls-Royce 250-C30R/3](https://openairdocs.org/engine/rolls-royce-250-c30r-3): 1 aircraft (registry code 54021) - [Rolls-Royce 250-C30R/3M](https://openairdocs.org/engine/rolls-royce-250-c30r-3m): 1 aircraft (registry code 54022) - [Allison 250-C28](https://openairdocs.org/engine/allison-250-c28): 0 aircraft (registry code 03113) - [Allison 250-C28C](https://openairdocs.org/engine/allison-250-c28c): 0 aircraft (registry code 03115) - [Allison 250-C30G](https://openairdocs.org/engine/allison-250-c30g): 0 aircraft (registry code 03103) - [Allison 250-C30M](https://openairdocs.org/engine/allison-250-c30m): 0 aircraft (registry code 03100) - [Allison 250-C30R](https://openairdocs.org/engine/allison-250-c30r): 0 aircraft (registry code 03101) - [Allison 250-C30R/1](https://openairdocs.org/engine/allison-250-c30r-1): 0 aircraft (registry code 03106) - [Allison 250-C30R/3](https://openairdocs.org/engine/allison-250-c30r-3): 0 aircraft (registry code 03111) - [Allison 250-C30R/3M](https://openairdocs.org/engine/allison-250-c30r-3m): 0 aircraft (registry code 03112) - [Allison 250-C30S](https://openairdocs.org/engine/allison-250-c30s): 0 aircraft (registry code 03098) - [Allison 250-C30U](https://openairdocs.org/engine/allison-250-c30u): 0 aircraft (registry code 03104) - [Rolls-Royce 250-C28C](https://openairdocs.org/engine/rolls-royce-250-c28c): 0 aircraft (registry code 54011) - [Rolls-Royce 250-C30R/1](https://openairdocs.org/engine/rolls-royce-250-c30r-1): 0 aircraft (registry code 54019) - [Rolls-Royce 250-C30U](https://openairdocs.org/engine/rolls-royce-250-c30u): 0 aircraft (registry code 54017) ## STCs approved under this data sheet (6) - [STC SE00057AT](https://openairdocs.org/stc/SE00057AT): Installation of Aeronautical Accessories, Inc., Pc Safety Valve Kit. Bell Helicopter Textron Inc. - [STC SE00014EN](https://openairdocs.org/stc/SE00014EN): Installation 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.. Pratt & Whitney Engine Services Inc. - [STC SE00026EN](https://openairdocs.org/stc/SE00026EN): Installation of Pratt & Whitney Engine Services Inc. IntelliStart Plus Electronic Control Unit (ECU), P/N DPU-K-010 on specified 250 engine models.. Pratt & Whitney Engine Services Inc. - [STC SE578GL](https://openairdocs.org/stc/SE578GL): Installation of a fuel flow transducer.. Shadin Avionics - [STC ST00037AT](https://openairdocs.org/stc/ST00037AT): Unison igniter plugs, P/N 9044400-1.. Unison Industries - [STC SQ00338AT](https://openairdocs.org/stc/SQ00338AT): Unison igniter leads, P/N9048222-101, 102, 103, 104, 105, 106.. Unison Industries --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.