# TCDS E00076EN: Rolls-Royce Deutschland Ltd & Co KG - Type: Type certificate data sheet - Status: Current - Holder: Rolls-Royce Deutschland Ltd & Co KG - Revision: 24 - Revised: September 22, 2026 - Product: Engine - Certification basis: Part 33, Part 21 - Registered aircraft: 56, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/52/8b/528b4ae770b5916c68b748361c9169a145fa52a91cd7330bd3ae37a1abcc8f62 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166430261920260929181626.0001 - Page: https://openairdocs.org/tcds/E00076EN ## Models (34) As the data sheet lists them. - Trent 1000-AE2 - Trent 1000-K2 - Trent 1000-A2 - Trent 1000-C2 - Trent 1000-CE3 - Trent 1000-R3 - Trent 1000-G3 - Trent7000-72 - Trent 1000-H2 - Trent 1000-D3 - Trent 1000-D - Trent 1000-G2 - Trent 1000-E2 - Trent 1000-M3 - Trent 1000-AE - Trent 1000-G - Trent 1000-D2 - Trent 1000-H3 - Trent 1000-C - Trent 1000-Q3 - Trent 1000-K3 - Trent 1000-J2 - Trent 1000-E - Trent 1000-N3 - Trent 1000-L3 - Trent 1000-H - Trent 1000-L2 - Trent 1000-CE2 - Trent7000-72C - Trent 1000-AE3 - Trent 1000-CE - Trent 1000-P3 - Trent 1000-A - Trent 1000-J3 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text TCDS NUMBER E00076EN U.S. DEPARTMENT OF TRANSPORTATION DATE: September 22, 2026 Revision 24 ROLLS-ROYCE DEUTSCHLAND LTD & CO KG FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET E00076EN MODELS: Trent 1000-A Trent 1000-D2 Trent 1000-J3 Trent 1000-AE Trent 1000-E2 Trent 1000-K3 Trent 1000-C Trent 1000-G2 Trent 1000-L3 Trent 1000-CE Trent 1000-H2 Trent 1000-M3 Trent 1000-D Trent 1000-J2 Trent 1000-N3 Trent 1000-E Trent 1000-K2 Trent 1000-P3 Trent 1000-G Trent 1000-L2 Trent 1000-Q3 Trent 1000-H Trent 1000-AE3 Trent 1000-R3 Trent 1000-A2 Trent 1000-CE3 Trent 7000-72 Trent 1000-AE2 Trent 1000-D3 Trent 7000-72C Trent 1000-C2 Trent 1000-G3 Trent 1000-CE2 Trent 1000-H3 Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E00076EN) and other approved data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance with pertinent aircraft data sheets and applicable portions of the Federal Aviation Regulations, provided they are installed, operated, and maintained as prescribed by the approved manufacturer's manuals and other approved instructions. TYPE CERTIFICATE (TC) HOLDER: Rolls-Royce Deutschland Ltd & Co KG Eschenweg 11. 15827 Blankenfelde-Mahlow, Germany TYPE CERTIFICATE (TC) RECORD: Rolls-Royce plc transferred TC E00076EN to Rolls-Royce Deutschland on February 21, 2019 TYPE The engine is a three shaft high bypass ratio, axia l flow, turbofan with low pressure, intermediate pressure and high pressure compressors driven by separate turbines through coaxial shafts. The LP compressor fan diameter is 112 inches with a swept fan blade and outlet guide vanes. The combustion system consists of a single annular combustor with 18 fuel spray nozzles. The LP and IP assemblies rotate independently in a counter clockwise direction; the HP assembly rotates clockwise, when viewed from back of the engine looking forward. The compressor and turbine have the following features: Compressor Turbine LP - single stage LP - 6 stage IP - 8 stage IP - single stage HP - 6 stage HP - single stage The engine control system utilizes an electronic engine controller (EEC) which has an airframe interface for digital bus communications. An engi ne monitoring unit (EMU) is fitted to provide vibration signals to the aircraft. LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" "---" INDICATES “NOT APPLICABLE" PAGE 1 2 3 4 5 6 7 8 9 REV. 2 4 13 13 13 1 4 13 22 22 2 0 PAGE 1 0 11 12 13 1 4 15 1 6 17 18 REV. 22 13 13 13 2 0 1 4 21 22 13 PAGE 19 2 0 21 22 23 REV. 17 13 2 4 23 23 TCDS E00076EN P age 2 of 24 I . MODELS Trent 1000-A Trent 1000-AE Trent 1000-C Trent 1000-CE Trent 1000-E Trent 1000-E2 Trent 1000-G Trent 1000-G2 Trent 1000-H Trent 1000-H2 Trent 1000-A2 Trent 1000-C2 Trent 1000-G3 Trent 1000-H3 Trent 1000-AE2 Trent 1000-CE2 Trent 1000-AE3 Trent 1000-CE3 Trent 1000-D Trent 1000-D2 Trent 1000-D3 Trent 1000-L2 Trent 1000-L3 Trent 1000-P3 RATINGS (See NOTE 1) Takeoff (5 min) Thrust, (net) - lbf (See NOTE 13) 69,194 74,511 59,631 72,066 63,897 Maximum continuous Thrust, (net) - lbf 64,722 69,523 58,866 64,722 58,866 PRINCIPAL DIMENSIONS, inches Length - tip of spinner to rear of cold nozzle 187.8 - - - - - - - - Radius – from centerline not including drain mast 74.8 - - - - - - - - CENTER OF GRAVITY, Wet, inches Trent 1000 Without Service Bulletin 72-G319 or Modification 72-G319 Offset from the center of front engine mount (power plant station 3000mm). Offset from Horizontal Centerline Offset from Vertical Centerline 31.0 (A) 0.7 (A) -3.3 (A) 31.0 (C,D) 0.7 (C,D) -3.3 (C,D) 31.0 (E) 0.7 (E) -3.3 (E) 31.0 (G) 0.7 (G) -3.3 (G) 31.0 (H) 0.7 (H) -3.3 (H) TCDS E00076EN P age 3 of 24 I . MODELS Trent 1000-A Trent 1000-AE Trent 1000-C Trent 1000-CE Trent 1000-E Trent 1000-E2 Trent 1000-G Trent 1000-G2 Trent 1000-H Trent 1000-H2 Trent 1000-A2 Trent 1000-C2 Trent 1000-G3 Trent 1000-H3 Trent 1000-AE2 Trent 1000-CE2 Trent 1000-AE3 Trent 1000-CE3 Trent 1000-D Trent 1000-D2 Trent 1000-D3 Trent 1000-L2 Trent 1000-L3 Trent 1000-P3 Offset from the center of front engine mount (power plant station 3000mm). 31.7 (A, AE) 31.6 (A2, AE2) 31.9 (AE3) 31.7 (C, CE, D) 31.6 (C2, CE2, D2, L2) 31.9 (CE3, D3, 31.7 (E) 31.6 (E2) 31.7 (G) 31.6 (G2) 31.9 (G3) 31.7 (H) 31.6 (H2) 31.9 (H3) L3, P3) Offset from Horizontal 0.6 (A, AE) 0.6 (C, CE, D) 0.6 (E) 0.6 (G) 0.6 (H) Centerline 0.7 (A2, AE2) 0.7 (C2, CE2, 0.7 (E2) 0.7 (G2) 0.7 (H2) 0.8 (AE3) D2, L2) 0.8 (G3) 0.8 (H3) 0.8 (CE3, D3, L3, P3) Offset from Vertical -3.4 (A,AE) -3.4 (C, CE, D) -3.4 (E) -3.4 (G) -3.4 (H) Centerline -3.1 (A2,AE2) -3.1 (C2, CE2, -3.1 (E2) -3.1 (G2) -3.1 (H2) -2.9 (AE3) D2, L2) -2.9 (G3) -2.9 (H3) -2.9 (CE3, D3, L3, P3) WEIGHT Dry with nacelle engine build-up items (lbs) Trent 1000- A, -C, -D, -E, -G, and –H 13,087 (A) 13,087 (C, D) 13,087 (E) 13,087 (G) 13,087 (H) Without Service Bulletin 72-G319 or Modification 72-G319 Trent 1000- 13,300 (A, AE) 13,111 (A2, AE2) 13,479 (AE3) 13,300 (C, CE, D) 13,111 (C2, CE2, D2, L2) 13,300 (E) 13,111 (E2) 13,300 (G) 13,111 (G2) 13,479 (G3) 13,300 (H) 13,111 (H2) 13,479 (H3) 13,479 (CE3 , D3, L3, P3) TCDS E00076EN P age 4 of 24 I . MODELS Trent 1000-A Trent 1000-AE Trent 1000-C Trent 1000-CE Trent 1000-E Trent 1000-E2 Trent 1000-G Trent 1000-G2 Trent 1000-H Trent 1000-H2 Trent 1000-A2 Trent 1000-C2 Trent 1000-G3 Trent 1000-H3 Trent 1000-AE2 Trent 1000-CE2 Trent 1000-AE3 Trent 1000-CE3 Trent 1000-D Trent 1000-D2 Trent 1000-D3 Trent 1000-L2 Trent 1000-L3 Trent 1000-P3 ENGINE BUILD STANDARD Trent 1000-A 2286 Issue 3 Trent 1000-C 2287 Issue 3 Trent 1000-E 2289 Issue 3 Trent 1000-G 2291 Issue 3 Trent 1000-H 2292 Issue 3 Rolls-Royce Drawing Introduction Sheet (DIS) Trent 1000-AE 2374 Issue 2 Trent 1000-CE 2375 Issue 3 Trent 1000-E2 2330 Issue 3 Trent 1000-G2 2331 Issue 3 Trent 1000-H2 2332 Issue 3 Trent 1000-A2 2327 Issue 3 Trent 1000-C2 2328 Issue 3 Trent 1000-G3 2360 Issue 3 Trent 1000-H3 2361 Issue 3 Trent 1000-AE2 2376 Issue 2 Trent 1000-CE2 2377Issue 2 Trent 1000-AE3 2372 Issue 3 Trent 1000-CE3 2373 Issue 3 Trent 1000-D 2288 Issue 3 Trent 1000-D2 2329 Issue 3 Trent 1000-D3 2357 Issue 3 Trent 1000-L2 2335 Issue 3 Trent 1000-L3 2364 Issue 3 Trent 1000-P3 2368 Issue 3 I. MODELS Trent 1000-J2 Trent 1000-J3 Trent 1000-K2 Trent 1000-K3 Trent 1000-Q3 Trent 1000-M3 Trent 1000-N3 Trent 1000-R3 Trent7000-72 Trent7000-72C RATINGS (See NOTE 1) Takeoff (5 min) Thrust, (net) - lbf (See NOTE 13) 78,129 79,728 81,028 72,834 Maximum continuous Thrust, (net) - lbf 71,818 72,691 72,691 65,005 TCDS E00076EN P age 5 of 24 I. MODELS Trent 1000-J2 Trent 1000-J3 Trent 1000-K2 Trent 1000-K3 Trent 1000-Q3 Trent 1000-M3 Trent 1000-N3 Trent 1000-R3 Trent 7000-72 Trent7000-72C PRINCIPAL DIMENSIONS, inches Length - tip of spinner to rear of cold nozzle Radius – from centerline not including drain mast 187.8 74.8 - - - - - - - - 188.0 72.3 CENTER OF GRAVITY, Wet, inches Offset from the center of front engine mount (power plant station 3000mm). Offset from Horizontal Centerline Offset from Vertical Centerline 31.6 (J2, K2) 31.9 (J3, K3, Q3) 0.7 (J2, K2) 0.8 (J3, K3, Q3) -3.1 (J2, K2) -2.9 (J3, K3, Q3) 31.9 0.8 -2.9 31.9 0.8 -2.9 30.1 1.3 -3.4 WEIGHT Dry with nacelle engine build-up items (lbs) 13,111 (J2, K2) 13,479 (J3, K3, Q3) 13,479 13,479 14,200 ENGINE BUILD Trent 1000-J2 Trent 1000-M3 Trent 1000-R3 Trent 7000-72 STANDARD 2333 Issue 3 2365 Issue 3 2369 Issue 3 2379 Issue 2 Rolls-Royce Drawing + Introduction Sheet (DIS) Trent 1000-J3 Trent 1000-N3 MB 73-K233 2362 Issue 3 2367 Issue 3 MB 72-K200 MB 72-K150 Trent 1000-K2 2334 Issue 3 Trent7000-72C 2378 Issue 1 Trent 1000-K3 + 2363 Issue 3 MB 73-K233 MB 72-K200 Trent 1000-Q3 MB 72-K150 2370 Issue 3 TCDS E00076EN P age 6 of 24 APPROVED FUELS See Engine Operating Instructions for approved fuels and additives. See Engine Operating Instructions for approved oils. APPROVED OILS All engine models except the Trent7000-72 and Trent7000-72C Maximum 0.63 U.S. Quarts per hour. Trent7000-72, Trent7000-72C Maximum 0.48 U.S. Quarts per hour. OIL CONSUMPTION For details of equipment included in the type design definition refer to the Installation manual. For details of equipment supplied by the Airframe TC holder, refer to the installation manual. A thrust reverser unit is not part of the engine type design and is certified as part of the aircraft type design. The engine is approved for operation with a thrust reverser unit. EQUIPMENT TCDS E00076EN P age 7 of 24 CERTIFICATION BASIS Trent 1000-A, -C, -D, -E, -G, and -H Airworthiness Standards: 14 CFR part 33 effective February 1, 1965, as amended by 33-1 through 33-21. Without Service Bulletin Emissions Standards: 14 CFR part 34, Amendmen t 5A, effective October 23, 2013. In addition, 72-G319 or Modification the engine meets ICAO environmental standards defined in Annex 16, amendment 7, dated 72-G319 November 17, 2011. See NOTE 11 fo r a detailed summary of the certification basis for fuel venting and exhaust emissions. Pursuant to 14 CFR § 21.29(a)(1)(ii), the Type Certificate was issued in validation of the European Aviation Safety Agency (EASA) Certification Standards CS-E, original issue dated October 24, 2003, which were found to provide a level of safety equivalent to that provided by 14 CFR Part 33 effective February 1, 1965, as amended by 33-1 through 33-21. Trent 1000-A, -C, -D, -E, -G, and –H Airworthiness Standards: 14 CFR part 33 effective February 1, 1965, as amended by 33-1 through 33-21. With an Exemption to § 33.27(c)(2)(v), amendment 33-10, No. 17864 dated June 13, 2018. With Service Bulletin 72-G319 or Modification 72-G319 Emissions Standards: 14 CFR part 34, Amendmen t 5A, effective October 23, 2013. In addition, the engine meets ICAO environmental standards defined in Annex 16, amendment 7, dated November 17, 2011. See NOTE 11 for a detailed summary of the certification basis for fuel venting and exhaust emissions. Pursuant to 14 CFR § 21.29(a)(1)(ii), the Type Certificate was issued in validation of the European Aviation Safety Agency (EASA) Certification Standards CS-E, original issue dated October 24, 2003, and CS-E 1030 and CS-E 1040 amendment 3, which were found to provide a level of safety equivalent to that provided by 14 CFR Part 33 effective February 1, 1965, as amended by 33-1 through 33-21. Trent 1000-A2, -C2, -D2, -E2, -G2, -H2, -J2, -K2, and –L2 Airworthiness Standards: 14 CFR part 33, effectiv e February 1, 1965, as amended by 33-1 through 33- 21 and amendment 31 § 33.27. With an Exempti on to § 33.27(f)(6), amendment 33-31, No. 17413 dated July 28, 2017. Emissions Standards: 14 CFR part 34, Amendmen t 5A, effective October 23, 2013. In addition, the engine meets ICAO environmental standards defined in Annex 16, amendment 7, dated November 17, 2011. See NOTE 11 fo r a detailed summary of the certification basis for fuel venting and exhaust emissions. Trent 1000-AE3, -CE3, -D3, Airworthiness Standards: 14 CFR part 33, effectiv e February 1, 1965, as amended by 33-1 through 33- -G3, -H3, -J3, -K3, -L3, -M3, 21 and amendmen t 31 § 33.27. With an Exemption to § 33.27(f)(6), amendmen t 33-31, No. 17413 -N3, -P3, -Q3, and -R3 dated July 28, 2017 and an Exemption to §§ 33.14, amendment 33-10; and 33.83(d), amendment 33-17; No. 18082A dated June 11, 2021. Emissions Standards: 14 CFR pa rt 34, Amendment 7A, effective May 24,2024. See NOTE 11 for a detailed summary of the certification basis for fuel venting and exhaust emissions. Equivalent level of Safety (ELOS) Findings:  ELOS No. AT03561EN-E-P-9 to 14 CFR 33.78(a)(1)  ELOS No. AT03561EN-E-P-16 to 14 CFR 33.83(a), (b) and (c)  ELOS No. AT03561EN-E-P-19 to 14 CFR 33.27(d)  ELOS No. AT03561EN-E-P-21 to 14 CFR 33.201(c) and (e). Pursuant to 14 CFR § 21.29(a)(1)(ii), the Type Certificate was issued in validation of the European Aviation Safety Agency (EASA) Certification Standards CS-E, original issue dated October 24, 2003, and CS-E 1030 and CS-E 1040 amendment 3, which were found to provide a level of safety equivalent to that provided by 14 CFR Part 33 effective February 1, 1965, as amended by 33-1 through 33-31. Airworthiness Standards: 14 CFR part 33, effectiv e February 1, 1965, as amended by 33-1 through 33- 21 and amendment 31 § 33.27. With an Exemption to § 33.27(f)(6), amendmen t 33-31, No. 17413 Trent 1000-AE,-CE,-AE2,- dated July 28, 2017. CE2 Emissions Standards: 14 CFR part 34, Amendmen t 5A, effective October 23, 2013. In addition, the engine meets ICAO environmental standards defined in Annex 16, amendment 7, dated November 17, 2011. See NOTE 11 fo r a detailed summary of the certification basis for fuel venting and exhaust emissions. Equivalent level of Safety (ELOS) Findings:  ELOS No. AT03561EN-E-P-19 to 14 CFR 33.27(d) TCDS E00076EN P age 8 of 24 Trent7000-72, -72C Airworthiness Standards: 14 CFR part 33, effective February 1, 1965, as amended by 33-1 through 33- 21, amendment 26 §33.28 and amendment 31 § 33.27. With an Exemption to § 33.27(f)(6), amendment 33-31, No. 17413 dated July 28, 2017 and a Time Limited Exemption to §§ 33.14, amendment 33-10; and 33.83(d), amendment 33-17; No. 18082A dated June 11, 2021. Emissions Standards: 14 CFR part 34, Amendmen t 7A, effective May 24, 2024. See NOTE 11 for a detailed summary of the certification basis for fuel venting and exhaust emissions. Equivalent level of Safety (ELOS) Findings:  ELOS No. AT03561EN-E-P-9 to 14 CFR 33.78(a)(1)  ELOS No. AT03561EN-E-P-16 to 14 CFR 33.83(a), (b) and (c)  ELOS No. AT03561EN-E-P-19 to 14 CFR 33.27(d)  ELOS No. AT03491EN-E-P-13 to 14 CFR 33.27(b)(3)  ELOS No. AT03591EN-E-P-21 to 14 CFR 33.93(a)(2) Pursuant to 14 CFR § 21.29(a)(1)(ii), the Type Certificate was issued in validation of the European Aviation Safety Agency (EASA) Certification Standards CS-E, original issue dated October 24, 2003, and CS-E 1030 and CS-E 1040 amendment 3, which were found to provide a level of safety equivalent to that provided by 14 CFR Part 33 effective February 1, 1965, as amended by 33-1 through 33-31. APPLICATION MODEL DATE ISSUED DELETED Trent 1000-A December 10, 2004 August 7, 2007 Trent 1000-AE July 28, 2014 December 20, 2018 Trent 1000-C December 10, 2004 August 7, 2007 Trent 1000-CE July 28, 2014 December 20, 2018 Trent 1000-D December 10, 2004 August 7, 2007 Trent 1000-E December 10, 2004 August 7, 2007 Trent 1000-G December 10, 2004 August 7, 2007 Trent 1000-H December 10, 2004 August 7, 2007 Trent 1000-A2 June 11, 2 012 May 9, 2014 Trent 1000-AE2 July 28, 2014 December 20, 2018 Trent 1000-C2 June 11, 2 012 May 9, 2014 Trent 1000-CE2 July 28, 2014 December 20, 2018 Trent 1000-D2 June 11, 2 012 May 9, 2014 Trent 1000-E2 June 11, 2 012 May 9, 2014 Trent 1000-G2 June 11, 2 012 May 9, 2014 Trent 1000-H2 June 11, 2 012 May 9, 2014 Trent 1000-J2 June 11, 2 012 May 9, 2014 Trent 1000-K2 June 11, 2 012 May 9, 2014 Trent 1000-L2 June 11, 2 012 May 9, 2014 Trent 1000-AE3 July 30, 2 014 October 20, 2017 Trent 1000-CE3 July 30, 2 014 October 20, 2017 Trent 1000-D3 July 30, 2 014 October 20, 2017 Trent 1000-G3 July 30, 2 014 October 20, 2017 Trent 1000-H3 July 30, 2 014 October 20, 2017 Trent 1000-J3 July 30, 2 014 October 20, 2017 Trent 1000-K3 July 30, 2 014 October 20, 2017 Trent 1000-L3 July 30, 2 014 October 20, 2017 Trent 1000-M3 July 30, 2 014 October 20, 2017 Trent 1000-N3 July 30, 2 014 October 20, 2017 Trent 1000-P3 July 30, 2 014 October 20, 2017 Trent 1000-Q3 July 30, 2 014 October 20, 2017 Trent 1000-R3 July 30, 2 014 October 20, 2017 Trent7000-72 December 3, 2014 December 20, 2018 Trent7000-72C December 3, 2014 December 20, 2018 TCDS E00076EN P age 9 of 24 NOTE 1. ENGINE RATINGS: The engine ratings are based on sea-level static, International Standard Atmosphere (ISA) conditions. No power take-offs are assumed. All engine models are flat rated to ISA + 15oC except the Trent 1000-D, –D2, - D3 and – L2 which are flat rated to ISA +20oC, the Trent 1000-K2 and –K3, which are flat rated to ISA+18oC, the Trent 1000-L3, which is flat rated to ISA +20oC, the Trent 1000-P3, which is flat rated ISA+25.3oC, the Trent 1000- Q3, which is flat rated to ISA+20.6oC, the Trent 1000-R3, which is flat rated to ISA+10oC and the Trent7000-72 and -72C , which are flat rated to ISA+22oC. NOTE 2. TEMPERATURE LIMITS: TURBINE GAS TEMPERATURE (TGT) – trimmed/indicated °C (see Note 11) Measured at the 1st stage Nozzle Guide Vane of the LP Turbine. Trent 1000-A, -C, -D, -E, -G, and -H with or without Service Bulletin 72 G319 or Modification 72-G319 and without Service Bulletin 73-H646, Trent1000-AE, -CE without Service Bulletin 73-H646 Maximum Ground Starting and Shutdown 700 Maximum Inflight Relights 900 Maximum Takeoff (5 min., see NOTE 13) 900 Maximum Continuous (unrestricted duration) 850 Maximum Exhaust Gas Overtemperature (see NOTE 13) 920 Trent 1000-A, -C, -D, -E, -G, -H with Service Bulletin 72 G319 or Modification 72-G319 and with Service Bulletin 73-H646, Trent 1000-AE, -CE with Service Bulle tin 73-H646, Trent 1000-A2, -AE2, -C2, -CE2, -D2, -E2, -G2, -H2, -J2, -K2, -L2, Trent 1000-AE3, -CE3, -D3, -G3, -H3, -J3, -K3,-L3, -M3, -N3, -P3, -Q3, -R3, Trent7000-72, -72C Maximum Ground Starting and Shutdown 700 Maximum Inflight Relights 900 Maximum Takeoff (5 min., see NOTE 13.) 900 Maximum Takeoff (2 min. out of a total of 5 minutes, see NOTE 13) 900 Maximum Continuous (unrestricted duration) 850 Maximum Exhaust Gas Overtemperature (see NOTE 13) 920 FUEL oC Measured at the inlet to the engine. Trent 1000-A, -C, -D, -E, -G, -H, Trent 1000-AE -CE, Trent 1000-A2, -AE2, -C2, -CE2, -D2, -E2, -G2, -H2, -J2, -K2, -L2 Minimum Fuel Temperature Before Start -45 Maximum Fuel Temperature 65 Trent 1000-AE3, -CE3, -D3, -G3, -H3, -J3, -K3,-L3, -M3, -N3, -P3, -Q3, -R3 Minimum Fuel Temperature Before Start -54 Minimum Fuel Temperature For Engine Acceleration -45 Maximum Fuel Temperature 65 Trent7000-72, Trent7000-72C Minimum fuel temperature: (at, or below 14,600ft) -44 Minimum fuel temperature: (above 14,600 ft) -54 Maximum fuel temperature: 55 NOTES TCDS E00076EN P age 10 of 24 NOTE 2. continued OIL oC Combined oil scavenge temperature Trent 1000-A, Trent 1000-C, Trent 1000-D, Trent 1000-E, Trent 1000-G, and Trent 1000-H Without Service Bulletin 72-G319 or With Service Bulletin 72-G319 or Modification 72-G319 Incorporated Modification 72-G319 Incorporated Minimum for starting: -40 Minimum for starting: -40 Minimum for acceleration to power, for Minimum for acceleration to power, for fuel inlet temperature -23°C and higher: 40 fuel inlet temperature -23°C and higher: 40 Minimum for acceleration to power, for Minimum for acceleration to power, for fuel inlet temperature from -45°C to -23°C: fu el inlet temperature from -45°C to -23°C: Varies linearly from 40 to 77 Varies linearly from 40 to 77 Maximum for unrestricted use: 196 Maximum for unrestricted use: 193 Transient limit (15 minutes) : 205 Transient limit (15 minutes) : 201 Trent 1000-AE, Trent 1000-CE Minimum for starting: -40 Minimum for acceleration to power, for fuel inlet temperature -23°C and higher: 40 Minimum for acceleration to power, for fuel inlet temperature from -45°C to -23°C: Varies linearly from 40 to 77 Maximum for unrestricted use: 193 Transient limit (15 minutes) : 201 Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, and Trent 1000-L2 Minimum for starting: -40 Minimum for acceleration to power, for fuel inlet temperature -23°C and higher: 40 Minimum for acceleration to power, for fuel inlet temperature from -45°C to -23°C: Varies linearly from 40 to 77 Maximum for unrestricted use: 193 Transient limit (15 minutes) : 201 Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000 K3, Trent 1000-L3, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3, Trent 1000-R3 Minimum for starting: -40 Minimum for acceleration to power, for fuel inlet temperature -23°C and higher: 40 Minimum for acceleration to power, for fuel inlet temperature from -45°C to -23°C: Varies linearly from 40 to 90 Maximum for unrestricted use: 196 Transient limit (15 minutes) : 201 Trent7000-72, Trent7000-72C Minimum for starting: -40 Minimum for acceleration to power, for fuel inlet temperature -11°C and higher: 40 Minimum for acceleration to power, for fuel inlet temperature between -11°C and -54°C: Varies linearly from 40 to 106 Maximum for unrestricted use: 191.8 Transient limit (15 minutes) : 197.3 TCDS E00076EN P age 11 of 24 NOTE 3. PRESSURE LIMITS: FUEL All engine models except the Trent7000-72 and Trent7000-72C Minimum absolute pressure at engine inlet: 5 psi + Vapor Pressure Transient conditions with engine running (2 seconds): 2 psi + Vapor Pressure For engine operation with the aircraft boost pumps inoperative the engine minimum fuel pressure limit is reduced down to 3.4 psi at altitudes of up to 35000 feet for up to 600 minutes. Refer to the Installation Manual for additional information. Maximum absolute pressure at the pylon interface: Steady state conditions with engine running: 70 psi Transient conditions with engine running (2 seconds) 140 psi Static after engine shutdown 170 psi Trent7000-72, Trent7000-72C Minimum absolute pressure at engine inlet: 5 psi + Vapor Pressure Refer to the Installation Manual for additional information. Maximum absolute pressure at the pylon interface: Steady state conditions with engine running: 40 psi Transient conditions with engine running (2 seconds) 100 psi Static after engine shutdown 100 psi OIL Trent 1000-A, Trent 1000-C, Trent 1000-D, Trent 1000-E, Trent 1000-G, and Trent 1000-H Without Service Bulletin 72-G319 or With Service Bulletin 72-G319 or Modification 72-G319 Incorporated Modification 72-G319 Incorporated Minimum Ground idle to 74% IP rpm: 30 psi Minimum Ground idle to 74% IP rpm: 30 psi Minimum between 74% and 100% IP rpm: Minimum between 74% and 100% IP rpm: Varies linearly from 30 to 75 psi Varies linearly from 30 to 90 psi Minimum Above 100% IP rpm: 75 psi Minimum Above 100% IP rpm: 90 psi Trent 1000-AE, Trent 1000-CE Minimum Ground idle to 74% IP rpm: 30 psi Minimum between 74% and 100% IP rpm: Varies linearly from 30 to 90 psi Minimum Above 100% IP rpm: 90 psi Trent 1000-A2, Trent –AE2, Trent 1000-C2, Trent-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, Trent 1000-L2 and Trent7000-72 and Trent7000-72C. Minimum Ground idle to 74% IP rpm: 30 psi Minimum between 74% and 100% IP rpm: Varies linearly from 30 to 90 psi Minimum Above 100% IP rpm: 90 psi Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000 K3, Trent 1000-L3, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3, Trent 1000-R3 Minimum Ground idle to 74% IP rpm: Trimmed/ indicated 30 psi Minimum between 74% and 100% IP rpm: Trimmed/ indicated varies linearly from 30 to 90 psi Minimum Above 100% IP rpm: Trimmed/ indicated 90 psi TCDS E00076EN P age 12 of 24 NOTE 4. ACCESSORY DRIVE MOUNTING PROVISIONS: Trent 1000 The Trent 1000 engine’s accessory gearbox may be fitted with two, Variable Frequency Starter Generators (VFSG) and one Hydraulic Pump to provide electrical and hydraulic power to the aircraft. These units are part of the airframe, and certified under Aircraft Airworthiness Standards. The Engine Installation Manual details installation and operational requirements, including torque and power limitations. Trent7000 The Trent7000 engines’s accessory gearbox may be fitted with one Intergrated Drive Generator (IDG) and two hydraulic pump’s to provide electrical and hydraulic power to the aircraft. These units are part of the Airframe, and certified under Airfcraft Airworthiness Standards. The Engine Installation Manual details installation and operational requirements, including torque and power limitations. Trent 1000-A, -C, -D, -E, -G and –H with or without SB 72-G319 or modification 72-G319 and –AE,- CE,–A2, -AE2, -C2, -CE2 -D2, -E2, -G2, -H2, -J2, -K2, -L2: Drive and mounting provisions Accessory VFSG Hydraulic Pump Drive identification Rear face of the EGB, left and right side of lower bevel box Front face of the right side of the EGB Speed ratio 1.658 IP speed 0.6538 IP speed Direction of rotation (looking at drive pad) Counter Clockwise Counter Clockwise Maximum power Maximum torque* 500 kVA 750 kVA (5 second transient) 51 hp 1496 lbf-ft 3715 lbf-in Overhung moment 1718.3 lbf-in (wet including QAD) 140 lbf-in (wet) *Maximum shear neck value Trent 1000-AE3, -CE3, -D3, -G3, -H3, -J3, -K3, -L3, -M3, -N3, -P3, -Q3, and -R3: Drive and mounting provisions Accessory VFSG Hydraulic Pump Drive identification Rear face of the EGB, left and right side of lower bevel box Front face of the right side of the EGB Speed ratio 1.6666 IP speed 0.6545 IP speed Direction of rotation (looking at drive pad) Counter Clockwise Counter Clockwise Maximum power Maximum torque* 500 kVA 750 kVA (5 second transient) 51 hp 1496 lbf-ft 3715 lbf-in Overhung moment 1718.3 lbf-in (wet including QAD) 140 lbf-in (wet) *Maximum shear neck value TCDS E00076EN P age 13 of 24 *Maximum shear neck value ACCESSORY DRIVE MOUNTING PROVISIONS: (cont.) Trent7000-72, -72C NOTE 4. continued Drive and mounting provisions Accessory Integrated Drive Generator (IDG) Hydraulic Pump Drive identification Rear face, Port side of the External Gearbox (2-off) Front face, Starboard side of the External Gearbox Speed ratio 0.987 IP speed 0.488 IP Speed Direction of rotation (looking at drive pad) Counter Clockwise Counter Clockwise Maximum power Maximum torque* 115kVA (continuous max) 180kVA (5 sec transient overload) 66 kW (88HP) 882.8 lbf.ft 368.8 lbf-ft Overhung moment 1165 lbf-in 160 lbf-in TCDS E00076EN P age 14 of 24 NOTE 5. MODEL DESCRIPTION: Trent 1000-A Basic model. Trent 1000-C Same as basic model except for increased thrust rating. Trent 1000-D Same as Trent 1000-C except flat rated to ISA +20 oC with a takeoff thrust increase (varying from 0.2 to 1.4 percent) scaled in as a function of the takeoff roll Mach number. Trent 1000-E Same as basic model except for decreased thrust ratings. Trent 1000-G Same as basic model except for increased Take-off thrust ratings. Trent 1000-H Same as Trent 1000-E except for increased Take-off thrust ratings. Trent 1000-A2 Same as Trent 1000-A/01 with increase d flight load capability, increased turbine entry temperature, a two-minute transient overtemperature limit, and a takeoff thrust increase (varying from 0.2 to 1.4 percent) scaled in as a function of the takeoff roll Mach number. Trent 1000-C2 Same as Trent 1000-A2 except for increased thrust ratings. Trent 1000-D2 Same as Trent 1000-C2 except flat rated to ISA +20 oC. Trent 1000-E2 Same as Trent 1000-A2 except for decreased thrust ratings. Trent 1000-G2 Same as Trent 1000-A2 except for increased Take-off thrust ratings. Trent 1000-H2 Same as Trent 1000-E2 except for increased Take of Thrust ratings Trent 1000-J2 Same as Trent 1000-A2 except for increased thrust ratings. Trent 1000-K2 Same as Trent 1000-J2 except flat rated to ISA +18 oC. Trent 1000-L2 Same as Trent 1000-C2 except flat rated to ISA +20 oC. Trent 1000-AE3 Same as Trent 1000-A/ 01 with increased flight load capability, decreased turbine entry temperature, a two-minute transient overtemperature limit, and a takeoff thrust increase (varying from 0.2 to 1.4 percent) scaled in as a function of the takeoff roll Mach number.. Trent 1000-CE3 Same as Trent 1000-AE3 except for increased thrust ratings Trent 1000-D3 Same as Trent 1000-CE3 except flat rated to ISA +20 oC Trent 1000-G3 Same as Trent 1000-AE3 except for increased Take-off thrust ratings. Trent 1000-H3 Same as Trent 1000-G3 except for decreased thrust ratings. Trent 1000-J3 Same as Trent 1000-AE3 except for increased thrust ratings. Trent 1000-K3 Same as Trent 1000-J3 except flat rated to ISA +18 oC. Trent 1000-L3 Same as Trent 1000-D3 except flat rated to ISA +20 oC. Trent 1000-M3 Same as Trent 1000-J3 except for increased thrust ratings. Trent 1000-N3 Same as Trent 1000-R3 except for decreased Take-off thrust ratings flat rated to ISA+15oC. Trent 1000-P3 Same as Trent 1000-CE3 except flat rated to ISA+25.3 oC. Trent 1000-Q3 Same as Trent 1000-J3 except flat rated to ISA +20.6 oC. Trent 1000-R3 Same as Trent 1000-AE3 except for incr eased thrust ratings flat rated to ISA +10oC. Trent7000-72 Basic model for us e on the Airbus A330 airframe. Similar thrusts as the Trent 1000-G, and flat rated to ISA+22°C Trent7000-72C Same as Trent 7000-72 except for increased Take-off thrust ratings at high altitude. Trent 1000-AE Same as Trent 1000-A/01 with a takeoff thrust increase (varying from 0.2 to 1.4 percent) scaled in as a function of the takeoff roll Mach number. Trent 1000-CE Same as Trent 1000-AE except for increased thrust rating. Trent 1000-AE2 Same as Trent 1000-A2. Trent 1000-CE2 Same as Trent 1000-C2. Trent 1000-A, -C, -D, -E, -G, and -H Engines incorporating Service Bulletin 72-G319 or Modification 72-G319 are identified on the engine name plate by “/01” in the Build Standard block. Engines incorporating deactivation of the fuel return to tank system are identified by the modification Service Bulletin 72-G893. In addition, these engines are identified on the engine name plate by “/01A” in the Build Standard block. NOTE 6. ACCESSORIES, COMPONENTS, OR SYSTEM ASSEMBLIES PROVIDED AS PART OF ENGINE TYPE DESIGN: Not Applicable NOTE 7. ACCESSORIES, COMPONENTS, OR SYSTEM ASSEMBLIES NOT PROVIDED AS PART OF ENGINE TYPE DESIGN: Not Applicable TCDS E00076EN P age 15 of 24 NOTE 8. SPECIAL ANTI-ICING OR DE-ICING REQUIREMENTS: All engine models except the Trent7000-72 and Trent7000-72C (See NOTE 21) do not supply compressor air for airframe ventilation (Cabin Bleed). All engine models supply compressor air for preventing ice build-up on the engine nacelle (Cowl Thermal Anti- Ice (CTAI)). Nacelle thermal anti-icing flow demand (HP3) is modulated via a regulating valve. Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE, Trent 1000-D, Trent 1000-E, Trent 1000-G, Trent 1000-H, Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, Trent 1000-L2. Engine Power Setting Maximum Cowl Thermal Anti Ice Flow TET (K) % Core Mass Flow (W26) Idle to 1430 2.67 1430 to 1785 2.67 to 1.25 varying linearly 1785 to 1820 1.25 to 0.54 varying linearly 1820 and above 0.54 Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000- K3, Trent 1000-L3, Trent 1000-M3,Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3, Trent 1000-R3. Engine Power Setting Maximum Cowl Thermal Anti Ice Flow TET (K) % Core Mass Flow (W26) Idle to 1015 2.9 1015 to 1765 2.9 to 2.1 varying linearly 1765 to 1810 2.1 to 0.5 varying linearly Above 1810 0.5 Trent7000-72, Trent7000-72C Engine Power Setting Maximum Cowl Thermal Anti Ice Flow TET (K) % Core Mass Flow (W26) Idle to 1175 0.86 1175 to 1725 0.86 to 0.82 varying linearly 1725 to 1750 0.82 to 0.54 varying linearly 1750 to 1830 0.54 to 0.39 varying linearly Above 1830 0.39 W26 represents the air mass-flow through the core of the engine. NOTE 9. ENGINE MOUNT SYSTEM PROVISIONS: The engine mount points are on the Fancase, Intercase and Tail Bearing Housing and are defined in the Engine Installation Manual NOTE 10. POWER BOOST, INJECTION OR AUGMENTATION SYSTEMS: Not Applicable NOTE 11. SPECIAL INSTALLATION REQUIREMENTS: ETOPS: These engine models have demonstrated eligibility for ETOPS under 14 CFR §33.201 for a maximum diversion time of 330 minutes. The Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE, Trent 1000- D, Trent 1000-E, Trent 1000-G, Trent 1000-H, Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000- CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, Trent 1000-L2, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3, Trent 1000-R3 engine models have complied with the requirements of §§ 33.4 (A33.3(c)), 33.71(c)(4) and 33.201, and are therefore eligible for installation on Extended Operations (ETOPS) and Early ETOPS approved airplanes. The demonstrated diversion time is 330 minutes at MCT plus 15 minutes at hold power. Note, that ETOPS eligibility does not constitute airplane or operational level approvals necessary to conduct ETOPS flights. TCDS E00076EN P age 16 of 24 NOTE 11. continued ETOPS cont.: The Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000-K3 and Trent 1000-L3 engine models have demonstrated eligibility for ETOPS under 14 CFR §33.201 for a maximum diversion time of 330 minutes except engines fitted with IPC Rotor 1 blades P/N KH28129 that have accumulated more than 500 cycles since new or since refurbishment as applicable, or fitted with IPC Rotor 2 blades P/N KH28131 that have accumulated more than 900 cycles since new or since refurbishment as applicable, for which ETOPS capability in accordance with §33.201 is approved for a maximum diversion time of 180 minutes plus 15 minutes at hold power. These engi ne models have complied with the requirements of §§ 33.4 (A33.3(c)), 33.71(c)(4) and 33.201, and are therefore eligible for installation on Extended Operations (ETOPS) and Early ETOPS approved airplanes. Note, that ETOPS eligibility does not constitute airplane or operational level approvals necessary to conduct ETOPS flights. The Trent7000-72 and Trent7000-72C engine models have complied with the requirements of §§ 33.4 (A33.3(c)), 33.71(c)(4) and 33.201, and are therefore eligible for installation on Extended Operations (ETOPS) and Early ETOPS approved airplanes. The demonstrated diversion time is 330 minutes at MCT plus 15 minutes at hold power. ETOPS is restricted to engines in corporating MB72-K203 and NMSB Trent 1000 72-AK269. Note, that ETOPS eligibility does not constitute airplane or operational level approvals necessary to conduct ETOPS flights. The Trent7000-72 and Tren t7000-72C engine models have demonstrated eligibility for ETOPS under 14 CFR §33.201 for a maximum diversion time of 330 minutes except engines fitted with IPC Rotor 1 blades P/N KH28129 that have accumulated more than 500 cycles since new or since refurbishment as applicable, for which ETOPS capability in accordance with §33.201 is approved for a maximum diversion time of 180 minutes plus 15 minutes at hold power. These engine models have complied with the requirements of §§ 33.4 (A33.3(c)), 33.71(c)(4) and 33.201, and are therefore eligible for installation on Extended Operations (ETOPS) and Early ETOPS approved airplanes. Note, that ETOPS eligibility does not constitute airplane or operational level approvals necessary to conduct ETOPS flights. IPC Rotor 1 blades P/N KH28129 and IPC Rotor 2 blades P/N KH28131 are to be replaced no later than June 30, 2023 by modified blade standards that are expected to restore a maximum approved diversion time of 330 minutes plus 15 minutes at hold power. THRUST REVERSER: These engines are approved for use in thrust reverse operation with thrust reverser units that conform to the following drawings: Trent 1000 Drawing Name Drawing Number Thrust Reverser Left Wing Outboard 725Z3030 Thrust Reverser Left Wing Inboard 725Z3040 Thrust Reverser Right Wing Inboard 725Z3050 Thrust Reverser Right Wing Outboard 725Z3060 Trent7000 Drawing Name Drawing Number Thrust Reverser Left Wing Outboard BKL0011-07-0 Thrust Reverser Left Wing Inboard BKL0051-07-0 Thrust Reverser Right Wing Inboard BKL0011-07-0 Thrust Reverser Right Wing Outboard BKL0051-07-0 TCDS E00076EN P age 17 of 24 NOTE 11 continued EMISSIONS STANDARDS: The following emissions standards promulgated in 14 CFR Part 34, Amendment 5A, effective October 23, 2013 and 40 CFR Part 87, effective July 18, 2012 have been complied with for the Trent 1000-A, Trent 1000-C, Trent 1000-D, Trent 1000-E, Trent 1000-G, Trent 1000-H, Trent 1000-A2, Trent 1000-C2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2 and Trent 1000-L2. The Trent 1000-AE, Trent 1000-CE, Trent 1000-AE2, and Trent 1000-CE2 engine models:  Fuel Venting Emission Standards: 14 CFR §§ 34. 10(a) and 34.11, and 40 CFR §§ 87.10(a) and 87.11  Smoke Number (SN) Emission Standards: 14 CFR §34.21(e)(2) and 40 CFR § 87.23(c)(1)  Carbon Monoxide (CO) Emission Standards: 14 CFR § 34.21(d)(1)(ii) and 40 CFR § 87.23(c)(1)  Hydrocarbons (HC) Emission Standards: 14 CF R § 34.21(d)(1)(i) and 40 CFR § 87.23(c)(1)  Oxides of Nitrogen (NOx) Emission Standards: 14 CFR § 34.23(b)(1) and 40 CFR § 87.23(c)(3) In addition to the FAA’s finding of compliance based on the certification requirements defined in this TCDS, Rolls-Royce has declared that the ICAO emissions standards identified in Annex 16, Volume II, Third Edition, Part III, Chapter 2, Section 2.2.2 for SN, Section 2.3.2 for CO and HC, Section 2.3.2.e.3 for NOx (also known as CAEP/8), and Part II Chapter 2 for fuel venting have been demonstrated. The following emissions standards promulgated in 14 CFR part 34, amendment 7A, effective May 24, 2024, and 40 CFR part 1031, effective December 23, 2022, have been complied with for the Trent 1000-AE3, Trent 1000- CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000-K3, Trent 1000-L3, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3, Trent 1000-R3, Trent7000-72, and Trent7000-72C engine models:  Fuel Venting Emission Standards: 14 CFR 34.10(a) and 34.11, and 40 CFR 1031.30(b)  Smoke Number (SN) Emission Standards: 14 CFR 34.21(e) and 40 CFR 1031.60(a)(5)  Carbon Monoxide (CO) Emission Standards: 14 CFR 34.21(d)(1)(ii) and 40 CFR 1031.60(d)  Hydrocarbons (HC) Emission Standards: 14 CFR 34.21(d)(1)(i) and 40 CFR 1031.60(c)  Oxides of Nitrogen (NOx) Emission Standards: 14 CFR 34.23(b)(1) and 40 CFR 1031.60(e)(5) (Tier 8 new type)  non-volatile Particulate Matter (nvPM) Mass Concentration Emission Standards: 14 CFR 34.25(a)(1) and 40 CFR 1031.60(a)(6) (Tier 10)  nvPM Mass and Number Emission Standards: 14 CFR 34.25(a)(2) and 40 CFR 1031.60(b)(2) (Tier 11 in-production) In addition to the FAA’s finding of compliance based on the certification requirements defined in this TCDS, Rolls-Royce has declared that the ICAO emissions standards identified in Annex 16, Volume II, Fourth Edition, Part II, Chapter 2 for fuel venting, Part III, Chapter 2, Section 2.2.2 for SN, Section 2.3.2 for CO and HC, Section 2.3.2.e for NOx (CAEP/8), Chapter 4, Section 4.2.2.1 for nvPM Mass Concentration (CAEP/10), and Section 4.2.2.2 for nvPM Mass and Number (CAEP/11), have been demonstrated. TIME LIMITED DISPATCH: Trent 1000 and Trent7000 The engine models are approved for Time Limited Dispatch. The maximum rectification period for each dispatchable state is specified in the Engine Installation Manual. ENGINE GAS TEMPERATURE: The measured Engine Gas Temperature (EGT) is modified by trimming for the purposes of the cockpit display. Trimming of EGT is done to provide consistent cockpit displayed levels of maximum allowable EGT, across engine models irrespective of the maximum allowable levels of un-trimmed EGT. EGT trims are programmed into the Data Entry Plug (DEP) which is fitted to the Electronic Engine Controller (EEC). The EEC processes the EGT and calculates the indicated EGT. Indicated redline values and corresponding EGT pull-down trims are provided in the following tables. Trent 1000-A, -C, -D, -E, -G, and –H without Service Bulletin 72-G319 or Modification 72-G319 Redline Value EGT Indicated [°C] EGT Trim [°C] Maximum Continuous 850 -105 Take-off 900 -83 20 second Over Temperature 920 -64.5 TCDS E00076EN P age 18 of 24 Trent 1000-AE and -CE EGT Indicated [°C] EGT Trim [°C] Redline Value -63.5 -59.5 900 Take-off -83 -82.5 Maximum Continuous With SB 73-K153 ENGINE GAS TEMPERATURE: (cont.) NOTE 11 continued -63.5 -54.5 850 20 sec Over Temperature -70.5 Not Applicable Take-off (2 minute transient) 920 Trent 1000-A, -C, -D, -E, -G, and –H with Service Bulletin 72-G319 or Modification 72-G319 Redline Value EGT Indicated [°C] EGT Trim [°C] With SB 73-H389 With SB 72-G893 and SB 73-H646 With SB 73-K153 Maximum Continuous 850 -82.5 -85 -85 -83 Take-off 900 -59.5 -65.5 -65.5 -63.5 Take-off (2 minute transient) Not Applicable Not Applicable -72.5 -70.5 20 sec Over Temperature 920 -54.5 -66 -66 -63.5 Trent 1000-A2,-AE2, -C2, –CE2, -D2, -E2, -G2, -H2, -J2, -K2, and –L2 Trent 1000-AE3, -CE3, -D3, -G3, -H3, -J3, -K3, -L3, -M3, -N3, -P3, -Q3, -R3 Trent7000-72, -72C Redline Value EGT Indicated [°C] EGT Trim [°C] EGT Indicated [°C] EGT Trim [°C] With SB 73- K177 Max Continuous 850 -101.5 -97.5 850 -84 Take-off 900 -74.5 -69.5 900 -53.5 Take-off (2 minute transient) -81 -77.5 -55 20 sec Over Temperature 920 -72 -68 920 -52.5 NOTE 12. MANUFACTURER’S SERVICE BULLETINS OR OTHER INSTRUCTIONS COVERING MATTERS OF INTEREST: Service bulletins, structural repair manuals, vendor manuals, and engine maintenance manuals, which contain a statement that the document is approved by the European Aviation Safety Agency, are accepted by the FAA and are considered FAA approved. These appr ovals pertain to the design data only. TCDS E00076EN P age 19 of 24 NOTE 13. SPECIAL OPERATING PROCEDURES: The take-off rating and its associated operating limitations may be used for up to 10 minutes in the event of engine out contingency, but their use is otherwise limited to not more than 5 minutes. Some engine models are approved for 2-minute transient overtemperature within 5-minute time limit associated with the take-off rating when engine is accelerated to take-off from a cold state. See note 11. The engine is approved for a maximum exhaust gas overtemperature of 920oC for inadvertent use due to abnormal operation for periods up to 20 seconds without requiring rejection of the engine from service or maintenance action other than to correct the cause. The cause of the overtem perature must be investigated and corrected. NOTE 14. SPECIAL REPAIR OR OVERHAUL LIMITATIONS Not Applicable NOTE 15. APPLICABLE INSTALLATION, MAINTENANCE AND OVERHAUL MANUALS. Trent 1000 and Trent7000 manuals submitted under EASA requirements and accepted as equivalent to 14 CFR § 33.4 and 14 CFR § 33.5 requirements are: Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE , Trent 1000-D, Trent 1000-E, Trent 1000-G, and Trent 1000-H OPERATING INSTRUCTIONS INSTALLATION MANUAL ENGINE MANUAL TIME LIMITS MANUAL For engines without Service Bulletin 72-G319 or Modification 72- G319 OI-Trent 1000- B787 DNS 130613 E-Trent-10RR Incorporated in T-Trent-10RR For engines with Service Bulletin 72-G319 or Modification 72- G319 OI-Trent 1000- B787 DNS 130613 E-Trent-10RR Incorporated in T-Trent-10RRB Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, and Trent 1000-L2 Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000- K3, Trent 1000-L3, Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3, Trent 1000-R3 OPERATING INSTRUCTIONS INSTALLATION MANUAL ENGINE MANUAL TIME LMITS MANUAL OI-Trent 1000-B787C1 DNS 193530 E-Trent-10RC T-Trent-10RRC OPERATING INSTRUCTIONS INSTALLATION MANUAL ENGINE MANUAL TIME LMITS MANUAL OI-Trent 1000-TEN-B787 EDNS01000566257 E-Trent-10RRT T-Trent-10RRT Cleaning, Inspection, and Repair Manual (CIR) Check and Rectify Manual (CRM) Standard Practices Manual (SPM) Overhaul Processes Manual (OPM) CIR-TRENT-10RRT CR-TRENT-10 RRT RR-CAEL-SPM TSD594-J TCDS E00076EN P age 20 of 24 NOTE 15 continued Trent7000-72, Trent7000-72C Maintenance Manual Airbus A330 Customer Aircraft Maintenance Manual (AMM) The Engine Maintenance Section submitted in compliance to 14 CFR § 33.4 and Appendix A 33.3(a) resides in Chapter 70 of the respective Aircraft Maintenance Manual for all of the above models. NOTE 16. IMPORT REQUIREMENTS: To be considered eligible for installation on U.S. registered aircraft, each new engine to be exported to the United States with UK CAA or EASA airworthiness approval shall have a Joint Aviation Authorities (JAA) or EASA Form 1, Authorized Release Certificate. The JAA or EASA Form 1 should state that the engine conforms to the type design approved under the U.S. Type Certificate E00076EN, is in a condition for safe operation and has undergone a final operational check. Reference 14 CFR Section 21.500, which provides for the airworthiness acceptance of aircraft engines manufactured outside of the U.S. and for which a U.S. type certificate has been issued. Additional guidance is contained in FAA Advisory Circular 21-23, "Airworthiness Certification of Civil Aircraft, Engines, Propellers, and Related Products Imported into the United States." NOTE 17. LIFE LIMITED PART INFORMATION: Life-limited parts are identified in Time Limits Manuals identified in Note 15. The Trent 1000 and Trent7000 cyclic life limits are based on a commercial mission cycle, which consists of a start, takeoff, climb, cruise, descent, and landing. Us e (or non-use) of a fan reverser for braking during landing does not affect cycle counts. Each of the following constitutes one cycle: (1) a flight consisting of a takeoff and landing, (2) a touch-and-go landing or simulated touch-and-go landing (no weight on wheels) for pilot training. NOTE 18. MILITARY MODEL INFORMATION: Not applicable. OPERATING INSTRUCTIONS INSTALLATION MANUAL ENGINE MANUAL TIME LMITS MANUAL EDNS01000696186 (OI-TRENT-A330) EDNS01000696188 E-T7000-1RR T-7000-1RR Cleaning, Inspection, and Repair Manual (CIR) Check and Rectify Manual (CRM) Standard Practices Manual (SPM) Overhaul Processes Manual (OPM) CIR-T7000-1RR CR-T7000-1RR RR-CAEL-SPM TSD594-J TCDS E00076EN P age 21 of 24 NOTE 19. MAXIMUM PERMISSIBLE ENGINE ROTOR SPEEDS (%) 100% HP = 13,391 rpm; 100% IP = 8,937 rpm; 100% LP = 2,683 rpm When maintenance running is performed above idle thrust with the aircraft static, the control system automatically applies a temperature dependent LP speed limit (Keep Out Zone). Refe r to the Aircraft Maintenance Manual for details. The Maximum Continuous speeds are not displayed as limitations on the aircraft flight deck. Trent 1000-A, Trent 1000-C, Trent 1000-D, Trent 1000-E, Trent 1000-G, and Trent 1000-H Without Service Bulletin 72-G319 or With Service Bulletin 72-G319 or Modification 72-G319 Incorporated Modification 72-G319 Incorporated Takeoff (5 minutes, see NOTE 13) Takeoff (5 minutes, see NOTE 13) HP 98.6% HP 100.2% IP 100.8% IP 103.5% LP 101.4% LP 101.5% Maximum Continuous Maximum Continuous HP 97.8% HP 99.2% IP 99.5% IP 100.8% LP 101.4% LP 101.5% For engines without SB 72-G319 or Modification 72-G319, LP speed must not exceed 96.5% during any aircraft operation with an apparent tailwind, i.e., tailwind greater than aircraft forward speed. This limitation does not apply to an engine with SB 72-G319 or Modification 72-G319. Trent 1000-AE and Trent 1000-CE Takeoff (5 minutes, see NOTE 13) HP 100.2% IP 103.5% LP 101.5% Maximum Continuous HP 99.2% IP 100.8% LP 101.5% Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000-G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, and Trent 1000-L2 Takeoff (5 minutes, see NOTE 13) HP 101.0% IP 103.5% LP 101.5% Maximum Continuous HP 99.5% IP 100.8% LP 101.5% Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3, Trent 1000-R3, Trent7000-72 and Trent7000- 72C Takeoff (5 minutes, see NOTE 13) HP 101.5% IP 103.5% LP 101.5% Maximum Continuous HP 99.5% IP 100.8% LP 101.5% Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000-K3, Trent 1000-L3 Takeoff (5 minutes, see NOTE 13) HP 101.5% IP 103.6% LP 101.5% Maximum Continuous HP 99.5% TCDS E00076EN P age 22 of 24 IP 100.8% LP 101.5% Maximum Transient (30 second limit. The transient IP limit is applicable for take-off and go-around maneuvers only and lasts for 30 seconds, before reverting to the steady-state limit). HP N/A IP 103.9% LP N/A NOTE 20. OUTPUT/PROPELLER SHAFT TORQUE LIMITS Not Applicable NOTE 21. BLEED AIR EXTRACTION PROVISIONS: See Note 8 for information regarding Bleed Air Extraction related to Anti-Icing facilities. All engine models except the Trent7000-72 and Trent7000-72C do not supply compressor air for airframe ventilation (Cabin Bleed). The Trent Trent7000-72 and Trent7000-72C engines supply compressor air for airframe ventilation (Cabin Bleed). Airframe ventilation (Cabin Bleed) is modulated via a regulating valve from either HPC stage 6 or IPC stage 8 source as shown). Trent7000-72 and Trent7000-72C Engine Power Setting Maximum Normal Cabin Air Bleed Turbine Entry Temperature (TET (K)) % Core Mass Flow (W26) 1000 15.8 (HPC 6) 1260 15.8 (HPC 6) 1600 5.6 (HPC 6 or IPC 8) 1708 4.3 (IPC 8) 1740 3.2 (IPC 8) 1835 and above 2.35 (IPC 8) Engine Power Setting Maximu m Abnormal Cabin Air Bleed TET (K) % Core Mass Flow (W26) 1000 16.9 (HPC 6) 1500 16.9 (HPC 6) 1655 11.3 (HPC 6/IPC 8) 1708 9.5 (IPC 8) 1725 7.2 (IPC 8) 1835 and above 4.95 (IPC 8) NOTE 22. ROTOR DISK INTEGRITY AND ROTOR BLADE CONTAINMENT See the following for applicable conditions and limitations: Exemption to § 33.27(f)(6), No. 17413 dated July 28, 2017 Exemption to § 33.27(c)(2)(v), No. 17864dated June 13, 2018 Exemption to §§ 33.14 and 33.83(d), No. 18082A dated June 11,2021 TCDS E00076EN P age 23 of 24 NOTE 23. All engine models except the Trent7000-72 and Trent7000-72C These engines are fitted with a Digital Electronic Engine Fuel Control system in which the software is designated as follows according to EUROCAE ED-12B/RTCA DO178B: • EEC: Level “A”. • EMU: Level “E”, except that the flight deck vibration display is Level “C”. Trent7000-72, Trent7000-72C These engines are fitted with a Digital Electronic Engine Fuel Control system in which the software is designated as follows: • EEC is designated EUROCAE ED-12B/RTCA DO178B Level “A”. • Pre SB 77-L241: EMU is designated EUROCAE ED-12C/RTCA DO178C Level “C”. • Post SB 77-L241: EMU is designated EUROCAE ED-12C/RTCA DO178C Level “E”, except that the flight deck vibration display is Level “C”. TCDS E00076EN P age 24 of 24 NOTE 24. The measured TGT is modified by trimming to provide consistent cockpit maximum trimmed TGT indications across all engine models. The TGT trim profile is programmed into the Data Entry Plug (DEP), which is fitted to the Engine Electronic Controller (EEC). The EEC processes the measured TGT and calculates the indicated TGT. The maximum TGT pull-down is the maximum value permitted, which corresponds to the maximum cleared turbine temperature. Trent 1000-A, Trent 1000-AE, Trent 1000-C, Trent 1000-CE, Trent 1000-D, Trent 1000-E, Trent 1000-G, Trent 1000-H Take-Off Max Max Exhaust Gas Overtemperature TGT Trim Profile (2 minute / 5 minute) Continuous (20 sec onds) Original Cert- DIS issue 2 (Profile 1) N/A / -57K -88K -50.5K DIS issue 3 (Profile 8) N/A / -83K -105K -64.5K SB73-G537 (Profile 11) N/A / -52.5K -79K -46K Trent 1000-A/01, Trent 1000-AE/01, Trent 1000-C/01, Trent 1000-CE/01, Trent 1000-D/01, Trent 1000-E/01, Trent 1000-G/01, Trent 1000-H/01 Take-Off Max Max Exhaust Gas Overtemperature TGT Trim Profile (2 minute / 5 minute) Continuous (20 sec onds) Basic (Profile 11) N/A / -52.5K -79K -46K SB73-H016 (Profile 12) N/A / -59.5K -82.5K -54.5K SB73-H389 (Profile 13) N/A / -65.5K -85K -66K SB73-H646 (Profile 14) -72.5K / -65.5K -85K -66K SB73-K153 (Profile 19) -70.5K / -63.5K -83K -63.5K Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2, Trent 1000-CE2, Trent 1000-D2, Trent 1000-E2, Trent 1000- G2, Trent 1000-H2, Trent 1000-J2, Trent 1000-K2, Trent 1000-L2 Take-Off Max Max Exhaust Gas Overtemperature TGT Trim Profile (2 minute / 5 minute) Continuous (20 sec onds) Basic (Profile 15) -81K / -74.5K -101.5K -72K SB73-K177 (Profile 16) -77.5K / -69.5K -97.5K -68K Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3, Trent 1000-G3, Trent 1000-H3, Trent 1000-J3, Trent 1000- K3, Trent 1000-L3 Take-Off Max Max Exhaust Gas Overtemperature TGT Trim Profile (2 minute / 5 minute) Continuous (20 sec onds) Basic (Profile 17) -55K / -53.5K -84K -52.5K SB 73-K827 (Profile 20) -58.5K / -54.5K -84.5K -53K SB 73-L276 (Profile 24) -76.5K /-68.5K -112.5K -67.5K Trent 1000-M3, Trent 1000-N3, Trent 1000-P3, Trent 1000-Q3, Trent 1000-R3 Take-Off Max Max Exhaust Gas Overtemperature TGT Trim Profile (2 minute / 5 minute) Continuous (20 sec onds) Basic (Profile 17) -55K / -53.5K -84K -52.5K Trent7000-72, Trent7000-72C Take-Off Max Max Exhaust Gas Overtemperature TGT Trim Profile (2 minute / 5 minute) Continuous (20 sec onds) Basic (Profile 17) -55K / -53.5K -84K -52.5K SB72-K336 (Profile 22) -84K / -72.5 - 101.5 -76.5K SB73-L176 (Profile 23) -78K / -70K - 105.5K -69.5K ----END---- ``` ## ADs (49, in force first) - [AD 2026-20-02](https://openairdocs.org/ad/2026-20-02): Air · Boeing 787-8, 787-9, Trent 1000-A and 17 more. Effective Oct 14, 2026 - [AD 2026-17-06](https://openairdocs.org/ad/2026-17-06): Turbine Engine Oil System · Rolls-Royce Deutschland Trent7000-72 and Trent7000-72C. Effective Oct 2, 2026 - [AD 2026-16-08](https://openairdocs.org/ad/2026-16-08): Turbine Engine Compressor Section · Rolls-Royce Deutschland Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2 and 8 more. Effective Sep 18, 2026 - [AD 2026-10-21](https://openairdocs.org/ad/2026-10-21): Engine Bleed Air System · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 10 more. Effective Jul 9, 2026 - [AD 2026-12-06](https://openairdocs.org/ad/2026-12-06): Turbine Section · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 10 more. Effective Jun 30, 2026 - [AD 2026-04-13](https://openairdocs.org/ad/2026-04-13): Engine Bleed Air System · Rolls-Royce Deutschland Trent7000-72 and Trent7000-72C. Effective Apr 10, 2026 - [AD 2025-26-03](https://openairdocs.org/ad/2025-26-03): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland Trent 1000-A, Trent 1000-AE, Trent 1000-C and 5 more. Effective Jan 27, 2026 - [AD 2025-23-10](https://openairdocs.org/ad/2025-23-10): Turbine Engine Compressor Section · Rolls-Royce Deutschland Trent 1000-A, Trent 1000-AE, Trent 1000-C and 15 more. Effective Dec 8, 2025 - [AD 2025-05-03](https://openairdocs.org/ad/2025-05-03): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland Trent7000-72 and Trent7000-72C. Effective Apr 17, 2025 - [AD 2025-02-14](https://openairdocs.org/ad/2025-02-14): Turbine Engine Compressor Section · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 12 more. Effective Apr 1, 2025 - [AD 2024-21-03](https://openairdocs.org/ad/2024-21-03): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 10 more. Effective Jan 6, 2025 - [AD 2024-23-04](https://openairdocs.org/ad/2024-23-04): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland Trent 1000-A, Trent 1000-AE, Trent 1000-C and 5 more. Effective Jan 6, 2025 - [AD 2024-10-14](https://openairdocs.org/ad/2024-10-14): Turbine Section · Rolls-Royce Deutschland Trent 1000-A, Trent 1000-AE, Trent 1000-C and 5 more. Effective Aug 13, 2024 - [AD 2024-08-06](https://openairdocs.org/ad/2024-08-06): Engine Fuel and Control · Rolls-Royce Deutschland Trent 1000-A, Trent 1000-A2, Trent 1000-AE and 16 more. Effective Jun 10, 2024 - [AD 2024-05-12](https://openairdocs.org/ad/2024-05-12): Engine Fuel and Control · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 10 more. Effective May 22, 2024 - [AD 2023-22-04](https://openairdocs.org/ad/2023-22-04): Turbine Section · Rolls-Royce Deutschland Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2 and 8 more. Effective Dec 26, 2023 - [AD 2023-12-16](https://openairdocs.org/ad/2023-12-16): Turbine Engine Combustion Section · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 10 more. Effective Aug 15, 2023 - [AD 2023-12-21](https://openairdocs.org/ad/2023-12-21): Engine · Rolls-Royce Deutschland Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2 and 8 more. Effective Aug 15, 2023 - [AD 2022-11-15](https://openairdocs.org/ad/2022-11-15): Turbine Section · Rolls-Royce Deutschland Trent7000-72 and Trent7000-72C. Effective Jul 13, 2022 - [AD 2022-08-16](https://openairdocs.org/ad/2022-08-16): Turbine Engine Compressor Section · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-G3 and 11 more. Effective May 31, 2022 - [AD 2022-04-02](https://openairdocs.org/ad/2022-04-02): Turbine Section · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 10 more. Effective Mar 29, 2022 - [AD 2021-18-05](https://openairdocs.org/ad/2021-18-05): Turbine Engine Compressor Section · Rolls-Royce Deutschland Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2 and 8 more. Effective Oct 21, 2021 - [AD 2021-17-12](https://openairdocs.org/ad/2021-17-12): Engine Fuel Pump · Rolls-Royce Deutschland Trent 1000-A, Trent 1000-A2, Trent 1000-AE and 14 more. Effective Oct 13, 2021 - [AD 2021-07-11](https://openairdocs.org/ad/2021-07-11): Turbine Section · Rolls-Royce Deutschland Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2 and 8 more. Effective May 11, 2021 - [AD 2020-15-08](https://openairdocs.org/ad/2020-15-08): Turbine Engine Compressor Section · Rolls-Royce Deutschland Trent 1000-A, Trent 1000-A2, Trent 1000-AE and 16 more. Effective Aug 31, 2020 - [AD 2020-14-04](https://openairdocs.org/ad/2020-14-04): Turbine Engine Compressor Section · Rolls-Royce Deutschland Trent 1000-A, Trent 1000-AE, Trent 1000-C and 5 more. Effective Jul 23, 2020 - [AD 2019-20-05](https://openairdocs.org/ad/2019-20-05): Turbine Engine, Turbine Section · Rolls-Royce Deutschland Trent 1000-A, Trent 1000-A2, Trent 1000-AE and 29 more. Effective Oct 30, 2019 - [AD 2019-16-14](https://openairdocs.org/ad/2019-16-14): Turbine Engine Compressor Section · Rolls-Royce Deutschland Trent 1000-A, Trent 1000-AE, Trent 1000-C and 5 more. Effective Sep 11, 2019 - [AD 2019-15-05](https://openairdocs.org/ad/2019-15-05): Turbine Section · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-D3, Trent 1000-G3 and 9 more. Effective Aug 16, 2019 - [AD 2019-07-09](https://openairdocs.org/ad/2019-07-09): Turbine Engine Compressor Section · Rolls-Royce Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2 and 8 more. Effective May 28, 2019 - [AD 2017-10-19](https://openairdocs.org/ad/2017-10-19): Turbine Engine, Compressor Section · Rolls-Royce Trent 1000-A2, Trent 1000-C2, Trent 1000-D2 and 6 more. Effective Jul 20, 2017 - [AD 2017-02-01](https://openairdocs.org/ad/2017-02-01): Turbine/Turboprop Engine/Turbine Section · Rolls-Royce Trent 1000-A, Trent 1000-C, Trent 1000-D and 3 more. Effective Mar 14, 2017 - [AD 2014-22-02](https://openairdocs.org/ad/2014-22-02): Engine electronic controller (EEC) software · Rolls-Royce Trent 1000-A, Trent 1000-C, Trent 1000-D and 3 more. Effective Nov 14, 2014 - [AD 2024-06-06](https://openairdocs.org/ad/2024-06-06) (historical): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland Trent7000-72 and Trent7000-72C. Effective May 21, 2024 - [AD 2023-26-04](https://openairdocs.org/ad/2023-26-04) (historical): Engine Bleed Air System · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 10 more. Effective Feb 7, 2024 - [AD 2023-24-06](https://openairdocs.org/ad/2023-24-06) (historical): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 10 more. Effective Jan 31, 2024 - [AD 2023-21-08](https://openairdocs.org/ad/2023-21-08) (historical): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland Trent 1000-A, Trent 1000-AE, Trent 1000-C and 5 more. Effective Dec 19, 2023 - [AD 2021-26-13](https://openairdocs.org/ad/2021-26-13) (historical): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2 and 8 more. Effective Jan 27, 2022 - [AD 2021-25-03](https://openairdocs.org/ad/2021-25-03) (historical): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland Trent7000-72 and Trent7000-72C. Effective Jan 19, 2022 - [AD 2021-25-04](https://openairdocs.org/ad/2021-25-04) (historical): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 10 more. Effective Jan 19, 2022 - [AD 2021-21-13](https://openairdocs.org/ad/2021-21-13) (historical): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland Trent 1000-AE, Trent 1000-A, Trent 1000-C and 5 more. Effective Dec 2, 2021 - [AD 2020-20-07](https://openairdocs.org/ad/2020-20-07) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 12 more. Effective Nov 10, 2020 - [AD 2020-15-12](https://openairdocs.org/ad/2020-15-12) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland Trent 1000-A2, Trent 1000-AE2, Trent 1000-C2 and 8 more. Effective Aug 31, 2020 - [AD 2020-13-07](https://openairdocs.org/ad/2020-13-07) (historical): Engine Fuel Pump · Rolls-Royce Deutschland Trent 1000-D2, Trent 1000-J2 and Trent 1000-K2. Effective Jul 13, 2020 - [AD 2020-05-01](https://openairdocs.org/ad/2020-05-01) (historical): Turbine Section · Rolls-Royce Deutschland Trent 1000-AE3, Trent 1000-CE3, Trent 1000-D3 and 10 more. Effective Mar 25, 2020 - [AD 2018-25-01](https://openairdocs.org/ad/2018-25-01) (historical): Turbine Engine Compressor Section · Rolls-Royce Trent 1000-A, Trent 1000-C, Trent 1000-D and 3 more. Effective Dec 21, 2018 - [AD 2018-13-07](https://openairdocs.org/ad/2018-13-07) (historical): Turbine Engine Compressor Section · Rolls-Royce Trent 1000-A, Trent 1000-C, Trent 1000-D and 3 more. Effective Aug 7, 2018 - [AD 2018-15-01](https://openairdocs.org/ad/2018-15-01) (historical): Turbine Engine, Turbine Section · Rolls-Royce Trent 1000-A, Trent 1000-A2, Trent 1000-C and 12 more. Effective Aug 7, 2018 - [AD 2018-08-02](https://openairdocs.org/ad/2018-08-02) (historical): Turbine Engine Compressor Section · Rolls-Royce Trent 1000-A2, Trent 1000-C2, Trent 1000-D2 and 8 more. Effective Apr 24, 2018 ## Registered aircraft by registry model (OpenAirDocs) - [Rolls-Roy TRENT-7000-72](https://openairdocs.org/engine/rolls-roy-trent-7000-72): 37 aircraft (registry code 54605) - [Rolls-Royce TRENT-1000](https://openairdocs.org/engine/rolls-royce-trent-1000-series): 14 aircraft (registry code 54544) - [Rolls-Royce TRENT-1000-D2](https://openairdocs.org/engine/rolls-royce-trent-1000-d2): 3 aircraft (registry code 54547) - [Rolls-Royce Deutschland TRENT-1000-K3](https://openairdocs.org/engine/rolls-royce-deutschland-trent-1000-k3): 1 aircraft (registry code 54566) - [Rolls-Royce TRENT-1000-D3](https://openairdocs.org/engine/rolls-royce-trent-1000-d3): 1 aircraft (registry code 54538) - [Rolls-Royce TRENT-1000-A2](https://openairdocs.org/engine/rolls-royce-trent-1000-a2): 0 aircraft (registry code 54545) --- 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.