TCDS E00089EN

Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E00089EN) and ot her 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: CFM International, S.A. 2 Boulevard du Général Martial Valin 75724 Paris Cedex 15 France I. MODELS LEAP-1A35AX LEAP-1A33X LEAP-1A33B2X LEAP-1A32X TYPE High bypass turbofan engine, with: coaxial front fan/booster driven by a multi-stage low pressure turbine; a multi-stage compressor; two-stage high pressure turbine; annular pre swirl combustor, and a full authority digital engine control (FADEC). RATINGS See Note 1. Static Thrust at Sea Level lb (daN) • Takeoff (5 min.) • Maximum continuous Flat Rating Ambient Temperature °F (°C) • Takeoff • Maximum continuous 32,160 (14,305) 24,850 (11,054) 86 (30) 77 (25) - - - - - - - - - - - - - - - - - - - - - - - - COMPONENTS Part Number Full Authority Digital Control (FADEC) • Electronic control unit • Software • Identification plug 2500M34 2590M00 and 2590M01 - - - - - - - - - - - - - - - - - - Refer to the latest revision of CFM Service Bulletin LEAP-1A SB 72-0136 for a list of Data Entry Plug part numbers PAGE 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 REV. 11 10 10 10 11 10 11 10 11 10 11 11 11 11 11 11 11 11 11 11 11 11 11 11 11 11 11 11 U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET E00089EN TCDS NUMBER E00089EN REVISION: Revision 11 DATE: May 12, 2026 CFM INTERNATIONAL, S.A. MODELS: LEAP-1A35A LEAP-1C30 LEAP-1A33S LEAP-1A33RS LEAP-1A33 LEAP-1C30B1 LEAP-1A32S LEAP-1A32RS LEAP-1A33B2 LEAP-1C28 LEAP-1A30S LEAP-1A30RS LEAP-1A32 LEAP-1A29 LEAP-1A26S LEAP-1A26E2 LEAP-1A30 LEAP-1A29CJ LEAP-1A26E1S LEAP-1A26 LEAP-1A26CJ LEAP-1A35AR LEAP-1A26E1 LEAP-1A35AX LEAP-1A33R LEAP-1A24 LEAP-1A33X LEAP-1A33B2R LEAP-1A24E1 LEAP-1A33B2X LEAP-1A32R LEAP-1A23 LEAP-1A32X LEAP-1A30R LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" "---" NOT APPLICABLE NOTE: SIGNIFICANT CHANGES ARE BLACK-LINED IN THE LEFT MARGIN. E00089EN 2 of 28 I. MODELS (Cont.) LEAP-1A35AX LEAP-1A33X LEAP-1A33B2X LEAP-1A32X FUEL • Approved fuel conforming to GE Specification D50TF2, Classes A, C, D, and E. Primary fuel is D50TF2 Class-A (Jet A) with other fuels listed being acceptable alternates. No fuel control adjustment is required when changing from primary to alternate fuels. Use of aviation gasoline and D50TF2 Class-B, Wide-Cut Distillate (Jet B or JP-4) is not authorized. • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 73-0001 for a list of fuels specifically approved for LEAP-1A engine. OIL • Approved oils are synthetic type conforming to SAE AS5780 specification, grade SPC (Standard Performance Capability) or HPC (High performance Capability). • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 79-0001 for a list of oil specifically approved for the LEAP-1A engine. PHYSICAL CHARACTERISTICS LEAP-1A G01 PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) 100.1 (2543) 93.2 (2368) - - - - - - - - - - - - - - - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, Including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6591 (2990) - - - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400.0) 99.0 (2514.6) 97.8 (2484.1) - - - - - - - - - - - - - - - - - - PHYSICAL CHARACTERISTICS LEAP-1A All other Gyy (see Note 5) PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) 99.7 (2533) 93.0 (2362) - - - - - - - - - - - - - - - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6632 (3008) - - - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400) 99.0 (2514.6) 97.8 (2484.1) - - - - - - - - - - - - - - - - - - E00089EN 3 of 28 II. MODELS LEAP-1A35A LEAP-1A33 LEAP-1A33B2 LEAP-1A32 TYPE High bypass turbofan engine, with: coaxial front fan/booster driven by a multi-stage low pressure turbine; a multi-stage compressor; two-stage high pressure turbine; annular pre swirl combustor, and a full authority digital engine control (FADEC). RATINGS See Note 1. Static Thrust at Sea Level lb (daN) • Takeoff (5 min.) • Maximum continuous Flat Rating Ambient Temperature °F (°C) • Takeoff • Maximum continuous 32,160 (14,305) 31,690 (14,096) 86 (30) 77 (25) - - - - - - - - - - - - - - - - - - - - - - - - COMPONENTS Part Number Full Authority Digital Control (FADEC) • Electronic control unit • Software • Identification plug 2500M34 2590M00 and 2590M01 - - - - - - - - - - - - - - - - - - Refer to the latest revision of CFM Service Bulletin LEAP-1A SB 72-0136 for a list of Data Entry Plug part numbers FUEL • Approved fuel conforming to GE Specification D50TF2, Classes A, C, D, and E. Primary fuel is D50TF2 Class-A (Jet A) with other fuels listed being acceptable alternates. No fuel control adjustment is required when changing from primary to alternate fuels. Use of aviation gasoline and D50TF2 Class-B, Wide-Cut Distillate (Jet B or JP-4) is not authorized. • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 73-0001 for a list of fuels specifically approved for LEAP-1A engine. OIL • Approved oils are synthetic type conforming to SAE AS5780 specification, grade SPC (Standard Performance Capability) or HPC (High performance Capability). • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 79-0001 for a list of oil specifically approved for the LEAP-1A engine. PHYSICAL CHARACTERISTICS LEAP-1A G01 PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) 100.1 (2543) 93.2 (2368) - - - - - - - - - - - - - - - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, Including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6591 (2990) - - - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400.0) 99.0 (2514.6) 97.8 (2484.1) - - - - - - - - - - - - - - - - - - E00089EN 4 of 28 II. MODELS (Cont.) LEAP-1A35A LEAP-1A33 LEAP-1A33B2 LEAP-1A32 PHYSICAL CHARACTERISTICS LEAP-1A All other Gyy (see Note 5) PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) 99.7 (2533) 93.0 (2362) - - - - - - - - - - - - - - - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6632 (3008) - - - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400) 99.0 (2514.6) 97.8 (2484.1) - - - - - - - - - - - - - - - - - - THIS SPACE INTENTIALLY LEFT BLANK E00089EN 5 of 28 III. MODELS LEAP-1A30 LEAP-1A29 LEAP-1A29CJ TYPE High bypass turbofan engine, with: coaxial front fan/booster driven by a multi-stage low pressure turbine; a multi-stage compressor; two-stage high pressure turbine; twin annular pre swirl combustors; and a full authority digital engine control (FADEC). RATINGS See Note 1. Static Thrust at Sea Level lb (daN) • Takeoff (5 min.) 32,160 (14,305) 29,290 (13,029) - - • Maximum continuous 31,690 (14,096) 26,680 (11,868) - - Flat Rating Ambient Temperature °F (°C) • Takeoff • Maximum continuous 86 (30) 77 (25) 97 (36) - - - - - - COMPONENTS Part Number Full Authority Digital Control (FADEC) • Electronic control unit • Software • Identification plug 2500M34 2590M00 and 2590M01 - - - - and - - - - - - and - - Refer to the latest revision of CFM Service Bulletin LEAP-1A SB 72-0136 for a list of Data Entry Plug part numbers FUEL • Approved fuel conforming to GE Specification D50TF2, Classes A, C, D, and E. Primary fuel is D50TF2 Class-A (Jet A) with other fuels listed being acceptable alternates. No fuel control adjustment is required when changing from primary to alternate fuels. Use of aviation gasoline and D50TF2 Class-B, Wide-Cut Distillate (Jet B or JP-4) is not authorized. • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 73-0001 for a list of fuels specifically approved for LEAP-1A engine. OIL • Approved oils are synthetic type conforming to SAE AS5780 specification, grade SPC (Standard Performance Capability) or HPC (High performance Capability). • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 79-0001 for a list of oil specifically approved for the LEAP-1A engine. PHYSICAL CHARACTERISTICS LEAP-1A G01 PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) - - - - 100.1 (2543) - - - - 93.2 (2368) - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6591 (2990) - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400) - - - - 99.0 (2514.6) - - - - 97.8 (2484.1) - - - - E00089EN 6 of 28 III. MODELS LEAP-1A30 LEAP-1A29 LEAP-1A29CJ PHYSICAL CHARACTERISTICS LEAP-1A All other Gyy (see Note 5) PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) - - - - 99.7 (2533) - - - - 93.0 (2362) - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6632 (3008) - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400) - - - - 99.0 (2514.6) - - - - 97.8 (2484.1) - - - - THIS SPACE INTENTIONALLY LEFT BLANK E00089EN 7 of 28 IV. MODELS LEAP-1A26 LEAP-1A26CJ LEAP-1A26E1 TYPE High bypass turbofan engine, with: coaxial front fan/booster driven by a multi-stage low pressure turbine; a multi-stage compressor; two-stage high pressure turbine; twin annular pre swirl combustors; and a full authority digital engine control (FADEC). RATINGS See Note 1. Static Thrust at Sea Level lb (daN) • Takeoff (5 min.) 27,120 (12,064) - - - - • Maximum continuous 26,680 (11,868) - - - - Flat Rating Ambient Temperature °F (°C) • Takeoff • Maximum continuous 111 (44) 77 (25) - - - - 120 (49) - - COMPONENTS Part Number Full Authority Digital Control (FADEC) • Electronic control unit • Software • Identification plug 2500M34 2590M00 and 2590M01 - - - - and - - - - - - and - - Refer to the latest revision of CFM Service Bulletin LEAP-1A SB 72-0136 for a list of Data Entry Plug part numbers FUEL • Approved fuel conforming to GE Specification D50TF2, Classes A, C, D, and E. Primary fuel is D50TF2 Class-A (Jet A) with other fuels listed being acceptable alternates. No fuel control adjustment is required when changing from primary to alternate fuels. Use of aviation gasoline and D50TF2 Class-B, Wide-Cut Distillate (Jet B or JP-4) is not authorized. • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 73-0001 for a list of fuels specifically approved for LEAP-1A engine. OIL • Approved oils are synthetic type conforming to SAE AS5780 specification, grade SPC (Standard Performance Capability) or HPC (High performance Capability). • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 79-0001 for a list of oil specifically approved for the LEAP-1A engine. PHYSICAL CHARACTERISTICS LEAP-1A G01 PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) - - - - 100.1 (2543) - - - - 93.2 (2368) - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6591 (2990) - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400) - - - - 99.0 (2514.6) - - - - 97.8 (2484.1) - - - - E00089EN 8 of 28 IV. MODELS LEAP-1A26 LEAP-1A26CJ LEAP-1A26E1 PHYSICAL CHARACTERISTICS LEAP-1A All other Gyy (see Note 5) PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) - - - - 99.7 (2533) - - - - 93.0 (2362) - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6632 (3008) - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400) - - - - 99.0 (2514.6) - - - - 97.8 (2484.1) - - - - THIS SPACE INTENTIONALLY LEFT BLANK E00089EN 9 of 28 V. MODELS LEAP-1A24 LEAP-1A24E1 LEAP-1A23 TYPE High bypass turbofan engine, with: coaxial front fan/booster driven by a multi-stage low pressure turbine; a multi-stage compressor; two-stage high pressure turbine; twin annular pre-swirl combustors; and a full authority digital engine control (FADEC). RATINGS See NOTE 1. Static Thrust at Sea Level lb (daN) • Takeoff (5 min.) 24,010 (10,680) - - - - • Maximum continuous 24,000 (10,676) - - 23,510 (10,458) Flat Rating Ambient Temperature °F (°C) • Takeoff (5 min.) • Maximum continuous 113 (45) 77 (25) 130 (55) - - 113 (45) - - COMPONENTS Part Number Full Authority Digital Control (FADEC) • Electronic control unit • Software • Identification plug 2500M34 2590M00 and 2590M01 - - - - and - - - - - - and - - Refer to the latest revision of CFM Service Bulletin LEAP-1A SB 72-0136 for a list of Data Entry Plug part numbers FUEL • Approved fuel conforming to GE Specification D50TF2, Classes A, C, D, and E. Primary fuel is D50TF2 Class-A (Jet A) with other fuels listed being acceptable alternates. No fuel control adjustment is required when changing from primary to alternate fuels. Use of aviation gasoline and D50TF2 Class-B, Wide-Cut Distillate (Jet B or JP-4) is not authorized. • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 73-0001 for a list of fuels specifically approved for LEAP-1A engine. OIL • Approved oils are synthetic type conforming to SAE AS5780 specification, grade SPC (Standard Performance Capability) or HPC (High performance Capability). • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 79-0001 for a list of oil specifically approved for the LEAP-1A engine. PHYSICAL CHARACTERISTICS LEAP-1A G01 PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) - - - - 100.1 (2543) - - - - 93.2 (2368) - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6591 (2990) - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400) - - - - 99.0 (2514.6) - - - - 97.8 (2484.1) - - - - E00089EN 10 of 28 V. MODELS (Cont.) LEAP-1A24 LEAP-1A24E1 LEAP-1A23 PHYSICAL CHARACTERISTICS LEAP-1A All other Gyy (see Note 5) PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) - - - - 99.7 (2533) - - - - 93.0 (2362) - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6632 (3008) - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400) - - - - 99.0 (2514.6) - - - - 97.8 (2484.1) - - - - THIS SPACE INTENTIONALLY LEFT BLANK E00089EN 11 of 28 VII. MODELS LEAP-1A35AR LEAP-1A33R LEAP-1A33B2R LEAP-1A32R LEAP-1A30R TYPE High bypass turbofan engine, with: coaxial front fan/booster driven by a multi-stage low pressure turbine; a multi-stage compressor; two-stage high pressure turbine; annular pre swirl combustor, and a full authority digital engine control (FADEC). RATINGS See Note 1. Static Thrust at Sea Level lb (daN) • Takeoff (5 min.) • Maximum continuous Flat Rating Ambient Temperature °F (°C) • Takeoff • Maximum continuous 32,160 (14,305) 24,850 (11,054) 86 (30) 77 (25) - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - COMPONENTS Full Authority Digital Control (FADEC) • Electronic control unit • Software • Identification plug Part Number 2500M34 2590M00 and 2590M01 - - - - - - - - - - - - - - - - - - - - - - - - Refer to the latest revision of CFM Service Bulletin LEAP-1A SB 72-0136 for a list of Data Entry Plug part numbers FUEL • Approved fuel conforming to GE Specification D50TF2, Classes A, C, D, and E. Primary fuel is D50TF2 Class-A (Jet A) with other fuels listed being acceptable alternates. No fuel control adjustment is required when changing from primary to alternate fuels. Use of aviation gasoline and D50TF2 Class-B, Wide-Cut Distillate (Jet B or JP-4) is not authorized. • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 73-0001 for a list of fuels specifically approved for LEAP-1A engine. OIL • Approved oils are synthetic type conforming to SAE AS5780 specification, grade SPC (Standard Performance Capability) or HPC (High performance Capability). • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 79-0001 for a list of oil specifically approved for the LEAP-1A engine. PHYSICAL CHARACTERISTICS LEAP-1A G01 PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) 100.1 (2543) 93.2 (2368) - - - - - - - - - - - - - - - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, Including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6591 (2990) - - - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400.0) 99.0 (2514.6) 97.8 (2484.1) - - - - - - - - - - - - - - - - - - E00089EN 12 of 28 VII. MODELS (Cont.) LEAP-1A35AR LEAP-1A33R LEAP-1A33B2R LEAP-1A32R LEAP-1A30R PHYSICAL CHARACTERISTICS LEAP-1A All other Gyy (see Note 5) PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) 99.7 (2533) 93.0 (2362) - - - - - - - - - - - - - - - - - - - - - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6632 (3008) - - - - - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400) 99.0 (2514.6) 97.8 (2484.1) - - - - - - - - - - - - - - - - - - - - - - - - THIS SPACE INTENTIONALLY LEFT BLANK E00089EN 13 of 28 VII. MODELS LEAP-1A33S LEAP-1A32S LEAP-1A30S LEAP-1A26S LEAP-1A26E1S TYPE High bypass turbofan engine, with: coaxial front fan/booster driven by a multi-stage low pressure turbine; a multi-stage compressor; two-stage high pressure turbine; annular pre swirl combustor, and a full authority digital engine control (FADEC). RATINGS See Note 1. Static Thrust at Sea Level lb (daN) • Takeoff (5 min.) • Maximum continuous Flat Rating Ambient Temperature °F (°C) • Takeoff • Maximum continuous 32,160 (14,305) 24,850 (11,054) 86 (30) 77 (25) - - - - - - - - - - - - - - - - 27,120 (12,064) 26,680 (11,868) 111 (44) 77 (25) - - - - - - - - COMPONENTS Part Number Full Authority Digital Control (FADEC) • Electronic control unit • Software • Identification plug 2500M34 2590M00 and 2590M01 - - - - - - - - - - - - - - - - - - - - - - - - Refer to the latest revision of CFM Service Bulletin LEAP-1A SB 72-0136 for a list of Data Entry Plug part numbers FUEL • Approved fuel conforming to GE Specification D50TF2, Classes A, C, D, and E. Primary fuel is D50TF2 Class-A (Jet A) with other fuels listed being acceptable alternates. No fuel control adjustment is required when changing from primary to alternate fuels. Use of aviation gasoline and D50TF2 Class-B, Wide-Cut Distillate (Jet B or JP-4) is not authorized. • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 73-0001 for a list of fuels specifically approved for LEAP-1A engine. OIL • Approved oils are synthetic type conforming to SAE AS5780 specification, grade SPC (Standard Performance Capability) or HPC (High performance Capability). • Refer to the latest revision of CFM Service Bulletin LEAP-1A S/B 79-0001 for a list of oil specifically approved for the LEAP-1A engine. PHYSICAL CHARACTERISTICS LEAP-1A G01 PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) 100.1 (2543) 93.2 (2368) - - - - - - - - - - - - - - - - - - WEIGHT Not to Exceed The engine weight is defined as the weight of the basic engine, Including basic engine accessories and fluids weight (oil and fuel). lb (kg) 6591 (2990) - - - - - - CENTER OF GRAVITY LOCATION Engine Only, Nominal Weight Station (axial) HPC case fwd flange = 200 in (5080 mm) Waterline Buttline in (mm) 212.6 (5400.0) 99.0 (2514.6) 97.8 (2484.1) - - - - - - - - - - - - - - - - - - E00089EN 14 of 28 VII. MODELS (Cont.) LEAP-1A33S LEAP-1A32S LEAP-1A30S LEAP-1A26S LEAP-1A26E1S PHYSICAL CHARACTERISTICS LEAP-1A All other Gyy (see Note 5) PRINCIPLE DIMENSIONS Length Fwd. fan case flange to TRF aft flange Width Maximum Envelope Height Maximum Envelope in (mm) 131.0 (3328) 99.7 (2533) 93.0 (2362) - - - - - - - - - - - - - - - -