TCDS E00076EN

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