# TCDS E38NE: CFM International S.A. - Type: Type certificate data sheet - Status: Current - Holder: CFM International S.A. - Revision: 15 - Revised: January 15, 2026 - Product: Engine - Certification basis: Part 33 - Data sheet PDF: https://openairdocs.org/files/sha256/54/d9/54d92d33a47f65536f720f46b71363963236b6bc7b7e2b3c5ee71d933bfe9b7f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107866946420260115154148.0001 - Page: https://openairdocs.org/tcds/E38NE ## Models (52) As the data sheet lists them. - CFM56-5B1/2P - CFM56-5B4/2P - CFM56-5C2/F - CFM56-5C3/G4 - CFM56-5B6/P - CFM56-5C2/P - CFM56-5C2/G4 - CFM56-5C3/P - CFM56-5B4/3B1 - CFM56-5B9/3 - CFM56-5B4/P - CFM56-5C2/F4 - CFM56-5B4/P1 - CFM56-5C2/4 - CFM56-5B7 - CFM56-5C2 - CFM56-5B1/3 - CFM56-5B2/2P - CFM56-5B9/P - CFM56-5B4 - CFM56-5B5/P - CFM56-5B3/P - CFM56-5B9/2P - CFM56-5B2 - CFM56-5C4/1P - CFM56-5B4/2P1 - CFM56-5B1 - CFM56-5C4/P - CFM56-5B2/P - CFM56-5C4/1 - CFM56-5B3/2P1 - CFM56-5B3/2P - CFM56-5B1/P - CFM56-5B4/3 - CFM56-5B7/3 - CFM56-5B8/P - CFM56-5B7/P - CFM56-5B3/P1 - CFM56-5B5/3 - CFM56-5C2/G - CFM56-5C3/F4 - CFM56-5B6/3 - CFM56-5B6/2P - CFM56-5B6 - CFM56-5B3/3 - CFM56-5C3/F - CFM56-5B3/3B1 - CFM56-5C3/G - CFM56-5B2/3 - CFM56-5B5 - CFM56-5B8/3 - CFM56-5C4 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET E38NE TCDS NUMBER E38NE REVISION: 15* DATE: January 15th, 2026 CFM INTERNATIONAL, S.A. MODELS: CFM56-5B1 CFM56-5B1/P CFM56-5B1/2P CFM56-5B2 CFM56-5B1/3 CFM56-5B2/3 CFM56-5B3/3 CFM56-5B3/3B1 CFM56-5B2/P CFM56-5B2/2P CFM56-5B3/P CFM56-5B3/P1 CFM56-5B4/3 CFM56-5B4/3B1 CFM56-5B5/3 CFM56-5B6/3 CFM56-5B3/2P CFM56-5B3/2P1 CFM56-5B4 CFM56-5B4/P CFM56-5B4/P1 CFM56-5B4/2P CFM56-5B4/2P1 CFM56-5B5 CFM56-5B5/P CFM56-5B6 CFM56-5B6/P CFM56-5B6/2P CFM56-5B7 CFM56-5B7/P CFM56-5B8/P CFM56-5B9/P CFM56-5B7/3 CFM56-5B8/3 CFM56-5B9/3 CFM56-5B9/2P CFM56-5C2 CFM56-5C2/4 CFM56-5C2/F CFM56-5C2/F4 CFM56-5C2/G CFM56-5C2/G4 CFM56-5C2/P CFM56-5C3/F CFM56-5C3/F4 CFM56-5C3/G CFM56-5C3/G4 CFM56-5C3/P CFM56-5C4 CFM56-5C4/P CFM56-5C4/1 CFM56-5C4/1P Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E38NE) 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: CFM International, S.A. 2 Boulevard du General Martial Valin 75015 Paris, France I. MODELS CFM56-5B1 CFM56-5B1/P CFM56-5B1/2P CFM56-5B1/3 TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. CFM56-5B/2P & -5B/2P1 SERIES ONLY: Double Annular Combustor RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 30,000/ 13,345 daN 29,090/ 12,940 daN - - - - - - - - - - - - - - - - - - - - - - - - Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 86oF / 30oC 77oF / 25oC - - - - - - - - - - - - FUEL SYSTEM See NOTE 7 for approved fuels * 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. 15 13 13 13 10 13 13 11 13 13 13 13 11 11 11 11 11 11 11 11 12 11 13 15 11 15 13 14 LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" "---" NOT APPLICABLE NOTE: SIGNIFICANT CHANGES ARE BLACK-LINED IN THE LEFT MARGIN. E37NE 2 of 28 I. MODELS (CONT.) CFM56-5B1 CFM56-5B1/P CFM56-5B1/2P CFM56-5B1/3 Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit (GE Part Number) 301-797-402-0 301-785-503-0 1348M79 - - --- - - - - --- - - - - --- - - Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 1820M36 1820M89 2042M13 2042M14 2123M55 2123M56 --- --- --- --- 338-046-002-0 338-046-004-0 338-046-006-0 - - - - - - - - - - - - 2121M47 2121M48 2447M39 2458M04 338-046-004-0 338-125-301-0 338-125-305-0 1820M87 1820M88 - - - - - - - - --- --- --- --- - - 338-046-090-0 338-046-095-0 338-122-801-0 338-122-805-0 338-125-301-0 338-125-305-0 --- --- --- --- - - - - --- --- 2447M39 2458M04 - - --- --- --- --- --- --- OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5B 79-0001 list approved brand oils. IGNITION SYSTEM GE PART NUMBER Ignition unit Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 102.3 / 2599.7 75.12 / 1908 82.87 / 2105 - - - - - - - - - - - - - - - - - - WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation. Pounds Kilograms 5412.9 2455.2 - - - - 5512.9 2500.6 5412.9 2455.2 CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 204.8 ± 1 5202 ± 25 - - - - - - - - - - - - E37NE 3 of 28 II. MODELS CFM56-5B2 CFM56-5B2/P CFM56-5B2/2P CFM56-5B2/3 TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. CFM56-5B/2P & -5B/2P1 SERIES ONLY: Double Annular Combustor RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 31,000/ 13,789 daN 29,090/ 12,940 daN - - - - - - - - - - - - - - - - - - - - - - - - Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 86oF / 30oC 77oF / 25oC - - - - - - - - - - - - FUEL SYSTEM See NOTE 7 for approved fuels Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit (GE Part Number) 301-797-402-0 301-785-503-0 1348M79 - - --- - - - - --- - - - - --- - - Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 1820M36 1820M89 2042M13 2042M14 2123M55 2123M56 --- --- --- --- 338-046-021-0 338-046-023-0 338-046-026-0 - - - - - - - - - - - - 2447M39 2458M04 2121M47 2121M48 338-046-023-0 338-122-720-0 338-122-725-0 338-128-660-0 338-128-665-0 1820M87 1820M88 - - - - - - - - --- --- --- --- - - 338-046-080-0 338-122-820-0 338-122-825-0 338-125-320-0 338-125-325-0 338-127-400-0 338-127-405-0 --- --- --- --- - - - - 2447M39 2458M04 --- --- - - --- --- --- --- --- --- --- OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5B 79-0001 list approved brand oils. IGNITION SYSTEM GE PART NUMBER Ignition unit Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 102.3 / 2599.7 75.12 / 1908 82.8 / 2105 - - - - - - - - - - - - - - - - - - E37NE 4 of 28 II. MODELS (CONT.) CFM56-5B2 CFM56-5B2/P CFM56-5B2/2P CFM56-5B2/3 WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation. Pounds Kilograms 5412.9 2455.2 - - - - 5512.9 2500.6 5412.9 2455.2 CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 204.8 ± 1 5202 ± 25 - - - - - - - - - - - - III. MODELS CFM56-5B3/P CFM56-5B3/P1 CFM56-5B3/2P CFM56-5B3/2P1 TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. CFM56-5B/2P & -5B/2P1 SERIES ONLY: Double Annular Combustor RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 32,000/ 14,234 daN 29,090/ 12,940 daN - - - - - - - - - - - - - - - - - - - - - - - - Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 86oF / 30oC 77oF / 25oC - - - - - - - - - - - - FUEL SYSTEM See NOTE 7 for approved fuels Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) 301-797-402-0 - - - - - - Hydromechanical unit (GE Part Number) 1348M79 - - - - - - Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 1820M36 --- 1820M87 --- 1820M89 --- 1820M88 --- 2042M13 - - - - - - 2042M14 - - - - - - 2123M55 - - - - - - 2123M56 - - - - - - 2121M47 - - --- --- 2121M48 - - --- --- 2447M39 - - --- --- 2458M04 - - --- --- 338-122-730-0 338-122-733-0 338-122-732-0 338-122-733-0 338-122-732-0 --- 338-122-830-0 --- 338-122-735-0 --- 338-122-835-0 --- 338-128-670-0 --- 338-128-300-0 --- 338-128-675-0 --- 338-128-305-0 --- 338-128-310-0 --- 338-128-315-0 --- 338-128-320-0 --- 338-128-325-0 --- OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5B 79-0001 list approved brand oils. E37NE 5 of 28 III. MODELS (CONT.) CFM56-5B3/P CFM56-5B3/P1 CFM56-5B3/2P CFM56-5B3/2P1 IGNITION SYSTEM GE PART NUMBER Ignition unit Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 102.3 / 2599.7 75.12 / 1908 82.87 / 2105 - - - - - - - - - - - - - - - - - - WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation Pounds Kilograms 5412.9 2455.2 - - - - 5512.9 2500.6 - - - - CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 204.8 ± 1 5202 ± 25 - - - - - - - - - - - - IV. MODELS CFM56-5B4 CFM56-5B4/P CFM56-5B4/P1 CFM56-5B4/2P TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. CFM56-5B/2P & -5B/2P1 SERIES ONLY: Double Annular Combustor RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 27,000/ 12,010 daN 24,370/ 10,840 daN - - - - - - - - - - - - - - - - - - - - - - - - Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 113oF / 45oC 77oF / 25oC - - - - 122oF / 50oC - - 113oF / 45oC - - FUEL SYSTEM See NOTE 7 for approved fuels Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit (GE Part Number) 301-797-402-0 301-785-503-0 1348M79 - - --- - - - - --- - - - - --- - - E37NE 6 of 28 IV. MODELS (CONT.) CFM56-5B4 CFM56-5B4/P CFM56-5B4/P1 CFM56-5B4/2P Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 1820M36 1820M89 2042M13 2042M14 2123M55 2123M56 --- --- --- --- 338-046-041-0 338-046-043-0 338-046-046-0 - - - - - - - - - - - - 2121M47 2121M48 2447M39 2458M04 338-046-043-0 338-122-740-0 338-122-745-0 338-128-680-0 338-128-685-0 --- --- - - - - - - - - - - - - - - - - 338-046-044-0 --- --- --- --- 1820M87 1820M88 - - - - - - - - --- --- --- --- 338-046-043-0 338-122-840-0 338-122-845-0 338-125-340-0 338-125-345-0 338-128-410-0 338-128-415-0 OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5B 79-0001 list approved brand oils. IGNITION SYSTEM GE PART NUMBER Ignition unit Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 102.3 / 2599.7 75.12 / 1908 82.87 / 2105 - - - - - - - - - - - - - - - - - - WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation Pounds Kilograms 5412.9 2455.2 - - - - - - - - 5512.9 2500.6 CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 204.8 ± 1 5202 ± 25 - - - - - - - - - - - - V. MODELS CFM56-5B3/3 CFM56-5B3/3B1 CFM56-5B4/3B1 CFM56-5B4/3 TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. CFM56-5B/2P & -5B/2P1 SERIES ONLY: Double Annular Combustor RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 32,000/ 14,234 daN 29,090/ 12,940 daN - - - - - - - - 27,000/ 12,010 daN 24,370/ 10,840 daN - - - - - - - - E37NE 7 of 28 V. MODELS (CONT.) CFM56-5B3/3 CFM56-5B3/3B1 CFM56-5B4/3B1 CFM56-5B4/3 Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 86oF / 30oC 77oF / 25oC - - - - 122oF / 50oC - - 113oF / 45oC - - FUEL SYSTEM See NOTE 7 for approved fuels Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit (GE Part Number) 301-797-402-0 1348M79 - - - - - - - - - - - - Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 2123M55 2123M56 2447M39 2458M04 338-122-732-0 - - - - - - - - 338-122-733-0 - - - - - - - - 338-046-044-0 - - - - - - - - 338-046-043-0 OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5B 79-0001 list approved brand oils. IGNITION SYSTEM GE PART NUMBER Ignition unit Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 102.3 / 2599.7 75.12 / 1908 82.87 / 2105 - - - - - - - - - - - - - - - - - - WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation Pounds Kilograms 5412.9 2455.2 - - - - - - - - - - - - CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 204.8 ± 1 5202 ± 25 - - - - - - - - - - - - VI. MODELS CFM56-5B4/2P1 CFM56-5B5 CFM56-5B5/P CFM56-5B5/3 TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. CFM56-5B/2P & -5B/2P1 SERIES ONLY: Double Annular Combustor E37NE 8 of 28 RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 27,000/ 12,010 daN 24,370/ 10,840 daN 22,000/ 9,786 daN 20,250/ 9,008 daN - - - - - - - - - - - - - - - - E37NE 9 of 28 VI. MODELS (CONT.) CFM56-5B4/2P1 CFM56-5B5 CFM56-5B5/P CFM56-5B5/3 Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 122oF / 50oC 77oF / 25oC 113oF / 45oC - - - - - - - - - - FUEL SYSTEM See NOTE 7 for approved fuels Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit (GE Part Number) 301-797-402-0 1348M79 - - 301-785-503-0 - - - - --- - - - - --- - - Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) --- --- 2042M13 2042M14 2123M55 2123M56 --- --- --- --- 338-046-044-0 1820M36 1820M89 - - - - - - - - --- --- --- --- 338-046-050-0 338-046-052-0 338-046-055-0 - - - - - - - - - - - - 2121M47 2121M48 2447M39 2458M04 338-046-052-0 338-122-750-0 338-122-755-0 338-128-690-0 338-128-695-0 --- --- --- --- - - - - --- --- - - - - - - --- --- --- --- OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5B 79-0001 list approved brand oils. IGNITION SYSTEM GE PART NUMBER Ignition unit Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 102.3 / 2599.7 75.12 / 1908 82.87 / 2105 - - - - - - - - - - - - - - - - - - WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation. Pounds Kilograms 5512.9 2500.6 5412.9 2455.2 - - - - - - - - CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 204.8 ± 1 5202 ± 25 - - - - - - - - - - - - E37NE 10 of 28 VII. MODELS CFM56-5B6 CFM56-5B6/P CFM56-5B6/3 CFM56-5B6/2P TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. CFM56-5B/2P & -5B/2P1 SERIES ONLY: Double Annular Combustor RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 23,500/ 10,453 daN 20,250/ 9,008 daN - - - - - - - - - - - - - - - - - - - - - - - - Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 113oF / 45oC 77oF / 25oC - - - - - - - - - - - - FUEL SYSTEM See NOTE 7 for approved fuels Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit (GE Part Number) 301-797-402-0 301-785-503-0 1348M79 - - --- - - - - --- - - - - --- - - Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 1820M36 1820M89 2042M13 2042M14 2123M55 2123M56 --- --- --- --- 338-046-060-0 338-046-062-0 338-046-065-0 - - - - - - - - - - - - 2121M47 2121M48 2447M39 2458M04 338-046-062-0 338-122-760-0 338-122-765-0 338-129-700-0 338-129-705-0 --- --- --- --- - - - - --- --- - - - - - - --- --- --- --- 1820M87 1820M88 2042M13 2042M14 - - - - --- --- --- --- - - 338-122-860-0 338-122-865-0 338-125-360-0 338-125-365-0 338-128-430-0 338-128-435-0 OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5B 79-0001 list approved brand oils. IGNITION SYSTEM GE PART NUMBER Two ignition units Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward Flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 102.3 / 2599.7 75.12 / 1908 82.87 / 2105 - - - - - - - - - - - - - - - - - - E37NE 11 of 28 VII. MODELS (CONT.) CFM56-5B6 CFM56-5B6/P CFM56-5B6/3 CFM56-5B6/2P WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation. Pounds Kilograms 5412.9 2455.2 - - - - - - - - 5512.9 2500.6 CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 204.8 ± 1 5202 ± 25 - - - - - - - - - - - - VIII. MODELS CFM56-5B7 CFM56-5B7/P CFM56-5B7/3 CFM56-5B8/P TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. CFM56-5B/2P & -5B/2P1 SERIES ONLY: Double Annular Combustor RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 27,000/ 12,010 daN 24,370/ 10,840 daN - - - - - - - - - - - - - - - - 21,600/ 9,608 daN 19,060/ 8,478 daN Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 113oF / 45oC 77oF / 25oC - - - - - - - - - - - - FUEL SYSTEM See NOTE 7 for approved fuels Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit (GE Part Number) 301-797-402-0 1348M79 - - - - - - - - - - - - Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 1820M36 1820M89 2042M13 2042M14 2123M55 2123M56 --- --- --- --- 338-126-941-0 338-128-440-0 338-128-445-0 - - - - - - - - - - - - 2121M47 2121M48 2447M39 2458M04 - - 338-128-450-0 338-128-455-0 338-128-470-0 338-128-475-0 --- --- --- --- - - - - --- --- - - - - - - --- --- --- --- --- --- 2042M13 2042M14 - - - - 2121M47 2121M48 - - - - 338-130-001-0 --- --- --- --- OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5B 79-0001 list approved brand oils. IGNITION SYSTEM GE PART NUMBER Ignition unit Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - E37NE 12 of 28 VIII. MODELS (CONT.) CFM56-5B7 CFM56-5B7/P CFM56-5B7/3 CFM56-5B8/P PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 102.3 / 2599.7 75.12 / 1908 82.87 / 2105 - - - - - - - - - - - - - - - - - - WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation. Pounds Kilograms 5412.9 2455.2 - - - - - - - - - - - - CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 204.8 ± 1 5202 ± 25 - - - - - - - - - - - - IX. MODELS CFM56-5B8/3 CFM56-5B9/P CFM56-5B9/2P CFM56-5B9/3 TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. CFM56-5B/2P & -5B/2P1 SERIES ONLY: Double Annular Combustor. RATINGS (See NOTE 4) Takeoff (5 min., see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 21,600/ 9,608 daN 19,060/ 8,478 daN 23,300/ 10,364 daN 20,250/ 9,008 daN - - - - - - - - - - - - - - - - Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 113°F / 45°C 77°F / 25°C - - - - - - - - - - - - FUEL SYSTEM See NOTE 7 for approved fuels Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit (GE Part Number) 301-797-402-0 1348M79 - - - - - - - - - - - - Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 2123M55 2123M56 --- --- 2447M39 2458M04 --- --- 338-130-001-0 - - - - 2042M13 2042M14 - - - - 2121M47 2121M48 338-130-010-0 - - - - - - - - --- --- --- --- - - - - - - --- --- 2447M39 2458M04 --- --- - - OIL Synthetic type conforming to GE Specification D50TF1, Type 1 and Type 11. CFM Service Bulletin CFM56-5B 79-0001 lists approved brand oils. IGNITION SYSTEM GE PART NUMBER E37NE 13 of 28 Ignition unit Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - E37NE 14 of 28 IX.MODELS (CONT.) CFM56-5B8/3 CFM56-5B9/P CFM56-5B9/2P CFM56-5B9/3 PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 102.3 / 2599.7 75.12 / 1908 82.87 / 2105 - - - - - - - - - - - - - - - - - - WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation. Pounds Kilograms 5412.9 2455.2 - - - - 5512.9 2500.6 5412.9 2455.2 CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 204.8 ± 1 5202 ± 25 - - - - - - - - - - - - X. MODELS CFM56-5C2 CFM56-5C2/4 CFM56-5C2/F CFM56-5C2/F4 TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. Long duct mixed flow exhaust system. Thrust reverser. RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 31,200/ 13,878 daN 28,300/ 12,588 daN - - - - - - - - - - - - - - - - - - - - - - - - Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 86oF / 30oC 77oF / 25oC - - - - - - - - - - - - FUEL SYSTEM See NOTE 7 for approved fuels Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit (GE Part Number) 301-785-503-0 301-797-402-0 1348M79 - - - - - - - - - - - - - - - - - - Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 1754M93 1799M97 1799M98 1851M41 1851M42 1851M43 1960M55 1960M56 1960M82 1960M83 337-151-901-0 337-151-905-0 - - - - - - - - - - - - - - - - - - - - 337-151-941-0 337-151-951-0 - - - - - - - - - - - - - - - - - - - - 337-180-401-0 337-180-411-0 - - - - - - - - - - - - - - - - - - - - 337-180-441-0 337-180-451-0 E37NE 15 of 28 X. MODELS (CONT.) CFM56-5C2 CFM56-5C2/4 CFM56-5C2/F CFM56-5C2/F4 OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5C 79-0001 list approved brand oils. IGNITION SYSTEM GE PART NUMBER Ignition unit Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 103.2 / 2622 76.61 / 1946 88.58 / 2250 - - - - - - - - - - - - - - - - - - WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation Pounds Kilograms 5830 2644.4 - - - - - - - - - - - - CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 206.0 ± 1.0 5232.4 ± 25.4 - - - - - - - - - - - - XI. MODELS CFM56-5C2/G CFM56-5C2/G4 CFM56-5C2/P CFM56-5C3/F TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. Long duct mixed flow exhaust system. Thrust reverser. RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 31,200/ 13,878 daN 28,300/ 12,588 daN - - - - - - - - - - - - - - - - 32,500/ 14,457 daN 29,400/ 13,078daN Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 86oF / 30oC 77oF / 25oC - - - - - - - - - - - - FUEL SYSTEM See NOTE 7 for approved fuels Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit (GE Part Number) 301-785-503-0 301-797-402-0 1348M79 - - - - - - --- - - - - 301-785-503-0 - - - - E37NE 16 of 28 XI. MODELS (CONT.) CFM56-5C2/G CFM56-5C2/G4 CFM56-5C2/P CFM56-5C3/F Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 1754M93 1799M97 1799M98 1851M41 1851M42 1851M43 1960M55 1960M56 1960M82 1960M83 337-183-601-0 337-183-611-0 - - - - - - - - - - - - - - - - - - - - 337-183-641-0 337-183-651-0 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 337-180-421-0 337-180-431-0 OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5C 79-0001 list approved brand oils. IGNITION SYSTEM GE PART NUMBER Two ignition units Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 103.2 / 2622 76.61 / 1946 88.58 / 2250 - - - - - - - - - - - - - - - - - - WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation. Pounds Kilograms 5830 2644.4 - - - - - - - - - - - - CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 206.0 ± 1.0 5232.4 ± 25.4 - - - - - - - - - - - - XII. MODELS CFM56-5C3/F4 CFM56-5C3/G CFM56-5C3/G4 CFM56-5C3/P TYPE High bypass turbofan; coaxial front/fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. Long duct mixed flow exhaust system. Thrust reverser. RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 32,500/ 14,457 daN 29,400/ 13,078 daN - - - - - - - - - - - - - - - - - - - - - - - - Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 86oF / 30oC 77oF / 25oC - - - - - - - - - - - - FUEL SYSTEM See NOTE 7 for approved fuels E37NE 17 of 28 XII. MODELS (CONT.) CFM56-5C3/F4 CFM56-5C3/G CFM56-5C3/G4 CFM56-5C3/P Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit (GE Part Number) 301-785-503-0 301-797-402-0 1348M79 - - - - - - - - - - - - --- - - - - Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 1754M93 1799M97 1799M98 1851M41 1851M42 1851M43 1960M82 1960M83 1960M55 1960M56 337-180-461-0 337-180-471-0 - - - - - - - - - - - - - - - - - - - - 337-183-621-0 337-183-631-0 - - - - - - - - - - - - - - - - - - - - 337-183-661-0 337-183-671-0 - - - - - - - - - - - - - - - - - - - - - - - - OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5C 79-0001 list approved brand oils. IGNITION SYSTEM GE PART NUMBER Two ignition units Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 103.2 / 2622 76.61 / 1946 88.58 / 2250 - - - - - - - - - - - - - - - - - - WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation. Pounds Kilograms 5830 2644.4 - - - - - - - - - - - - CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches Millimeters 206.0 ± 1.0 5232.4 ± 25.4 - - - - - - - - - - - - XIII. MODELS CFM56-5C4 CFM56-5C4/P CFM56-5C4/1 CFM56-5C4/1P TYPE High bypass turbofan; coaxial front/fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine and annular combustor. Long duct mixed flow exhaust system. Thrust reverser. RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 16), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. 34,000/ 15,124 daN 30,060/ 13,371 daN - - - - - - - - - - - - - - - - - - - - - - - - E37NE 18 of 28 XIII. MODELS (CONT.) CFM56-5C4 CFM56-5C4/P CFM56-5C4/1 CFM56-5C4/1P Flat rating AMBIENT TEMPERATURE Takeoff Maximum continuous 86oF / 30oC 77oF / 25oC - - - - - - - - - - - - FUEL SYSTEM See NOTE 7 for approved fuels Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) 301-797-402-0 - - - - - - Hydromechanical unit (GE Part Number) 1348M79 - - - - - - Electronic control unit (GE Part Number) Identification plugs (SNECMA Part Number) 1754M93 1799M97 1799M98 1851M41 1851M42 1851M43 1960M55 1960M56 1960M82 1960M83 337-183-801-0 337-183-811-0 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 337-183-821-0 337-183-831-0 - - - - - - - - - - - - - - - - - - - - - - - - OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-5C 79-0001 list approved brand oils. IGNITION SYSTEM GE PART NUMBER Two ignition units Unison Two igniter plugs Unison Champion 9238M66 1374M12 1374M13 - - - - - - - - - - - - - - - - - - PRINCIPAL DIMENSIONS INCHES / MILLIMETERS Length, (fan case forward flange to LPT frame aft flange) Width, (fan casing forward flange diameter) Height, (bottom of accessory gearbox to top of fan casing forward flange) 103.2 / 2622 76.61 / 1946 88.58 / 2250 - - - - - - - - - - - - - - - - - - WEIGHT (dry) Includes basic engine accessories and optional equipment as listed in manufacturers specification, and engine-mounted portions of the condition monitoring instrumentation. Pounds 5830 - - - - - - Kilograms 2644.4 - - - - - - CENTER OF GRAVITY LOCATIONS STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) Inches 206.0 ± 1.0 - - - - - - Millimeters 5232.4 ± 25.4 - - - - - - E37NE 19 of 28 CERTIFICATION BASIS 1. 14 CFR Part 33, effective February 1, 1965, with Amendments 33-1 through 33-11 thereto. 2. See NOTE 21 for emissions certification basis. NOTE: CFM56-5B1/2, -5B2/2, -5B4/2, and -5B6/2 have been removed from this type data sheet since they have been either converted to another CFM56 model rating or are out of service. MODEL APPLICATION DATE TYPE CERTIFICATE ISSUED/AMENDED TYPE CERTIFICATE WITHDRAWN CFM56-5C2 12/15/88 12/31/91 CFM56-5C3 12/15/88 12/31/91 05/24/93 CFM56-5C2/F 04/03/92 03/01/93 CFM56-5C3/F 04/03/92 03/01/93 CFM56-5B2 08/30/90 05/28/93 CFM56-5B1 08/30/90 02/02/94 CFM56-5B4 06/08/92 02/02/94 CFM56-5B1/2 12/01/92 07/27/94 07/25/02 CFM56-5B2/2 12/01/92 07/27/94 07/25/02 CFM56-5B4/2 12/01/92 07/27/94 07/25/02 CFM56-5C2/G 02/26/93 10/27/94 CFM56-5C3/G 02/26/93 10/27/94 CFM56-5C4 02/26/93 10/27/94 CFM56-5B6/2 04/19/94 10/30/95 07/25/02 CFM56-5B5 04/19/94 03/11/96 CFM56-5B6 04/19/94 03/11/96 CFM56-5C2/4 06/14/95 04/17/96 CFM56-5C2/F4 06/14/95 04/17/96 CFM56-5C2/G4 06/14/95 04/17/96 CFM56-5C3/F4 06/14/95 04/17/96 CFM56-5C3/G4 06/14/95 04/17/96 CFM56-5C4/1 06/21/95 04/17/96 CFM56-5B1/P 02/21/95 06/20/96 CFM56-5B1/2P 02/21/95 06/20/96 CFM56-5B2/P 02/21/95 06/20/96 CFM56-5B2/2P 02/21/95 06/20/96 CFM56-5B3/2P 02/21/95 06/20/96 CFM56-5B4/P 02/21/95 06/20/96 CFM56-5B4/2P 02/21/95 06/20/96 CFM56-5B5/P 02/21/95 06/20/96 CFM56-5B6/P 02/21/95 06/20/96 CFM56-5B6/2P 02/21/95 06/20/96 CFM56-5B3/P 02/21/95 09/10/96 CFM56-5B7 12/03/97 06/07/99 CFM56-5B7/P 12/03/97 11/03/99 CFM56-5B8/P 04/23/01 07/25/02 CFM56-5B9/P 04/23/01 07/25/02 CFM56-5B9/2P 04/23/01 07/25/02 CFM56-5C2/P 12/14/00 08/06/03 CFM56-5C3/P 12/14/00 08/06/03 CFM56-5C4/P 12/14/00 08/06/03 CFM56-5C4/1P 12/14/00 08/06/03 CFM56-5B3/P1 01/25/02 10/25/04 CFM56-5B3/2P1 01/25/02 10/25/04 CFM56-5B4/P1 01/25/02 10/25/04 CFM56-5B4/2P1 01/25/02 10/25/04 CFM56-5B1/3 04/23/05 09/15/06 CFM56-5B2/3 04/23/05 09/15/06 CFM56-5B3/3 04/23/05 09/15/06 CFM56-5B3/3B1 04/23/05 09/15/06 CFM56-5B4/3 04/23/05 09/15/06 CFM56-5B4/3B1 04/23/05 09/15/06 CFM56-5B5/3 04/23/05 09/15/06 E37NE 20 of 28 CERTIFICATION BASIS (CONT.) APPLICATION TYPE CERTIFICATE TYPE CERTIFICATE MODEL DATE ISSUED/AMENDED WITHDRAWN CFM56-5B6/3 04/23/05 09/15/06 CFM56-5B7/3 04/23/05 09/15/06 CFM56-5B8/3 04/23/05 09/15/06 CFM56-5B9/3 04/23/05 09/15/06 The Direction Generale de L'Aviation Civile (DGAC) originally type certificated these engine models under DGAC Certifcate de Type Moteur M17. The FAA validated these products under Type Certificate Number E38NE. Effective September 28, 2003, the European Aviation Safety Agency (EASA) began oversight of these products on behalf of France. EASA Type Certificate Number EASA.E.003 was issued on October 24, 2004. PRODUCTION BASIS IMPORT REQUIREMENTS The original production basis was "Agreement de Production" Numbers F.G.007 or P03 issued by the DGAC for engines produced in France by Snecma under license from CFM International, S.A. Effective September 28, 2004, these engine models were produced under EASA Production Certificate FR.21G.0007. (See NOTE 10) To be considered for installation on aircraft registered in the United States, each individually imported engine must be accompanied by an EASA airworthiness approval certificate (EASA Form 1 – Authorized Release Certificate) or JAA Form 1 issued by Snecma on behalf of EASA under EASA Production Certificate FR.21G.0007. The EASA Form 1 – Authorized Release Certificate, or JAA Form 1, should contain the following statement: ‘The engine covered by this certificate has been examined, tested, and found to conform to U.S. Type Certificate No. E38NE and is in a condition for safe operation.’ E37NE 21 of 28 NOTES NOTE 1. MAXIMUM PERMISSIBLE TEMPERATURES CFM56-5B SAC COMBUSTOR SERIES CFM56-5B/2P AND - 5B/2P1 SERIES ALL CFM56-5C ENGINE MODELS TURBINE EXHAUST GAS (T495) (See NOTE 17) As measured by a harness of nine thermocouples located at the second stage low pressure turbine vane: Takeoff (5 min.) Maximum continuous Starting CFM56-5B/2 In-flight Time temperature envelope Refer to model's S.O.I. 950°C 915°C 725°C --- CFM-TP.0I.13 - - - - - - 850°C - - - - - - - - --- CFM-TP.OI.12 FUEL PUMP INLET REFER TO THE APPROPRIATE INSTALLATION MANUAL OIL SUPPLY Continuous operation Transient (15 minutes) 140°C/284°F 155°C/311°F - - - - - - - - NOTE 2. FUEL AND OIL PRESSURE LIMITS Fuel limits Oil limits Operation and air/ground starting pressure limits with the aircraft boost pump operative extend from a minimum fuel pressure of not less than 5.5 psia (37.9 kPa absolute) above the true fuel vapor pressure to a maximum of 50 psig (344.8 kPa gauge), relative to atmosphere, with vapor/liquid ratio of zero at all conditions. See Installation Manual, Part A, Section 5, Figures A2 and A4. For limits with the aircraft boost pump inoperative, see Installation Manual, Part A, Section 5, Figures A3 and A5. The minimum pressure limit at idle is 13 psid (89.6 kPa differential) and varies up to 45 psid (310.2 kPa differential) at cruise thrust. The maximum pressure limit during cold starts is 300 psid (2069 kPa differential), limited by a pressure-relief valve. See NOTE 13. NOTE 3. ACCESSORY DRIVE PROVISIONS CFM56-5B ENGINE MODELS CFM56-5C ENGINE MODELS ELECTRICAL Rotation (1) Speed ratio to core Pad Rating (kW) Shear Torque (in-lb) Maximum overhung moment (in-lb) CCW 0.5947 135 9,492 1,000 - - - - - - - - - - HYDRAULIC PUMP Rotation (1) Speed ratio to core Pad Rating (in-lb) Shear Torque (in-lb) Maximum overhung moment (in-lb) CCW 0.256 1,500 4,400 160 - - - - - - - - 183 (1) CW = CLOCKWISE / CCW = COUNTERCLOCKWISE E37NE 22 of 28 NOTE 4. Engine ratings are based on calibrated stand performance under the following conditions: Takeoff thrust is nominally independent of ambient temperature (flat rated) up to ambient temperature of: Std + 15°C (30°C, 86°F): CFM56-5B1, -5B1/P, -5B1/2P, -5B1/3, -5B2, -5B2/P, -5B2/2P, -5B2/3, -5B3/3, -5B3/3B1, -5B3/P, -5B3/P1, -5B3/2P, -5B3/2P1, -5C2, -5C2/4, -5C2/F, -5C2/F4, -5C2/G, -5C2/G4, -5C2/P, -5C3/F, -5C3/F4, -5C3/G, -5C3/G4, -5C3/P, -5C4, -5C4/P, -5C4/1, -5C4/1P. Std + 30°C (45°C, 113°F): CFM56-5B4, -5B4/P, -5B4/2P, -5B4/3, -5B5, -5B5/P, -5B5/3, -5B6, -5B6/P, -5B6/2P, -5B6/3, -5B7, -5B7/P, -5B7/3, -5B8/P, -5B8/3, -5B9/P, -5B9/2P, -5B9/3. Std + 35°C (50°C, 122°F): CFM56-5B4/P1, -5B4/2P1, -5B4/3B1. Maximum continuous is nominally independent of ambient temperature (flat rated) up to ambient temperature of Std. + 10°C (25°C, 77°F) for all models. Zero customer bleed and horsepower extraction. No scrubbing drags. 100% inlet recovery. Based on CFM International referee separate flow exhaust system with primary (core) exhaust nozzle and fan nozzle for all CFM56-5B engine models. Based on CFM International long duct mixed flow flight exhaust system for all CFM56-5C engine models. NOTE 5. MAXIMUM PERMISSIBLE ENGINE ROTOR SPEEDS (See NOTE 18) CFM56-5C2, -5C2/F, -5C3/F, -5C2/G, -5C3/G, -5C2/4, -5C2/F4, -5C2/G4, -5C3/F4, -5C3/G4 ALL CFM56-5B ENGINE MODELS CFM56-5C4, -5C4/1, -5C2/P, -5C3/P, -5C4/P, -5C4/1P RPM % RPM % RPM % Low pressure rotor (N1) High pressure rotor (N2) 4,800 15,183 100.3 105.0 5,200 - - 104.0 - - 4,985 - - 104.2 - - NOTE 6. MAXIMUM PERMISSIBLE AIR BLEED EXTRACTION (ALL MODELS) LOCATION FAN CORRECTED SPEED FLOW LIMIT Fan Discharge HPC Stage 5 only Compressor discharge only HPC Stage 5 and compressor discharge combined All speeds above minimum idle All speeds above minimum idle Minimum idle to 61% N1K 61% to 82.5% N1K Above 82.5% N1K Minimum idle to 61% N1K 61% to 82.5% N1K Above 82.5% N1K 2% fan airflow 10% core airflow 14% core airflow Linear variation from 14% to 7% core airflow 7% core airflow 14% core airflow Linear variation from 14% to 10% core airflow 10% core airflow NOTE 7. Approved fuel conforming to GE Specification D50TF2. MIL-T-5624, Grades JP-4 or JP-5, ASTM D 1655, Jet A, A1 and B are consistent with this General Electric Specification. Primary fuel is 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 is not authorized. Consult Specific Operating Instructions for additive usage. E37NE 23 of 28 NOTE 8. Life limits established for critical rotating and static components are published in Chapter 5 of the CFM56-5B Shop Manual, CFMI-TP-SM.9, for the CFM56-5B engine models, and the CFM56-5C Shop Manual, CFMI-TP.SM.8, for the CFM56-5C engine models. NOTE 9. Power setting, power checks and control of engine thrust output in all operations are to be based on CFM International engine charts referring to fan speed. Fan speed sensors are included in the engine assembly for this purpose. NOTE 10. The type certificate holder, CFM International, S.A., is a company established and jointly owned by Snecma of France and the General Electric Company for the certification, sale, and support of CFM56 series engines. With respect to the benefits of type certification for production, General Electric and Snecma function as licensees of CFM International, S.A. This type certificate applies only to engines produced in France to EASA Type Certificate No. EASA.E.003. Engines of the same model designation produced in the United States to Type Certificate No. E37NE are identical to and fully interchangeable with engines produced to this type certificate. Modules, assemblies, or parts produced in the United States under Production Certificate No. 108 are eligible for use in engines produced to this type certificate. CFM56-5B Engine Models: CFM56-5B Engine Models: The engine assembly line is identified by a 3 digit prefix in the engine serial number. Refer to CFM56-5B Service Bulletin 72-0781 for a list of the applicable serial numbers. French “Agreement de Production“ No. P03 was the original Snecma Production Basis. Beginning on February 17, 1998, all engines produced by Snecma were produced under Production Certificate No. F.G.007. Engine serial number 779-374 was the first CFM56-5B engine produced by Snecma under Production Certificate No. F.G.007. Effective September 28, 2004, engines produced by Snecma were produced under EASA Production Certificate FR.21G.0007. Engine serial number 577-150 was the first CFM56-5B/P engine produced by Snecma under the EASA Production Certificate. Engine serial number 577-933 was the first CFM56-5B/2P engine produced by Snecma under the EASA Production Certificate. CFM56-5C Engine Models: CFM56-5C Engine Models: The engine assembly line is identified by a 3 digit prefix in the engine serial number. Refer to CFM56-5C Service Bulletin 72-0697 for a list of the applicable serial numbers. French “Agreement de Production“ No. P03 was the original Snecma Production Basis. Beginning on February 5, 1998, all engines produced by Snecma were produced under Production Certificate No. F.G.007. Engine serial number 741-737 was the first CFM56-5C engine produced by Snecma under Production Certificate No. F.G.007. Effective September 28, 2004, engines produced by Snecma were produced under EASA Production Certificate FR.21G.0007. Engine serial number 567-281 was the first CFM56-5C series engine produced by Snecma under the EASA Production Certificate. NOTE 11. The engine manufacturer supplies the nacelle system and attachment fittings NS-CFM56-5G01, the total exhaust system ES-CFM56-5G01, and the engine-assembled EBU 736L699, which have been approved for installation on all CFM56-5C engine models in accordance with 14 CFR § 33. NOTE 12. The minimum permissible idle in flight corresponds to N2=58.8% (8,500 rpm) which is a non-adjustable limit, preset into the ECU Control schedule. NOTE 13. During negative -g operation only, it is permissible to operate below minimum oil pressure (13 psid) for a maximum of 10 seconds. See Specific Operating Instruction, Section 6. E37NE 24 of 28 NOTE 14. The models shown on this TCDS have the following general characteristics: MODEL CHARACTERISTICS CFM56-5B1 Similar to CFM56-5C2, except for new fan and booster and CFM56-5 LP turbine and revised thrust ratings. CFM56-5B1/P Same as CFM56-5B1, except for redesigned high pressure compressor, high pressure turbine, and low pressure turbine. CFM56-5B1/3 Same as CFM56-5B1/P, except for redesigned high pressure compressor, high pressure turbine, and combustor. CFM56-5B1/2P Same as CFM56-5B1/2, except for redesigned high pressure compressor, high pressure turbine, and low pressure turbine. Note, the CFM56-5B1/2 was similar to the CFM56-5B1 except the CFM56-5B1/2 had a dual annual combustor. CFM56-5B2 Same as CFM56-5B1, except for increased thrust ratings. CFM56-5B2/P Same as CFM56-5B2, except for redesigned high pressure compressor, high pressure turbine, and low pressure turbine. CFM56-5B2/3 Same as CFM56-5B2/P, except for redesigned high pressure compressor, high pressure turbine, and combustor. CFM56-5B2/2P Same as CFM56-5B2/2, except for redesigned high pressure compressor, high pressure turbine, and low pressure turbine. Note, the CFM56-5B2/2 was similar to the CFM56-5B1 but with a dual annual combustor and increased thrust rating. CFM56-5B3/P Same as CFM56-5B1, except for increased thrust rating and redesigned high pressure compressor, high pressure turbine, and low pressure turbine. CFM56-5B3/3 Same as CFM56-5B3/P, except for redesigned high pressure compressor, high pressure turbine, and combustor. CFM56-5B3/P1 Same as CFM56-5B3/P, except for a manually-activated takeoff thrust bump (within the certified standard day rating) for ambient temperatures above corner point. CFM56-5B3/3B1 Same as CFM56-5B3/P1, except for redesigned high pressure compressor, high pressure turbine, and combustor. CFM56-5B3/2P Same as CFM56-5B1, except for increased thrust rating and redesigned high pressure compressor, high pressure turbine, and low pressure turbine. CFM56-5B3/2P has a dual annular combustor. CFM56-5B3/2P1 Same as CFM56-5B3/2P, except for a manually-activated takeoff thrust bump (within the certified standard day rating) for ambient temperatures above corner point. CFM56-5B4 Same as CFM56-5B1, except for decreased thrust ratings. CFM56-5B4/P Same as CFM56-5B4, except for redesigned high pressure compressor, high pressure turbine, and low pressure turbine. CFM56-5B4/3 Same as CFM56-5B4/P, except for redesigned high pressure compressor, high pressure turbine, and combustor. E37NE 25 of 28 NOTE 14. (CONT.) CFM56-5B4/P1 Same as CFM56-5B4/P, except for increased flat rating ambient temperature (corner point), and a manually-activated takeoff thrust bump (within the certified standard day rating) for ambient temperatures above corner point. CFM56-5B4/3B1 Same as CFM56-5B4/P1, except for redesigned high pressure compressor, high pressure turbine, and combustor. CFM56-5B4/2P Same as CFM56-5B4/2, except for redesigned high pressure compressor, high pressure turbine, and low pressure turbine. Note, the CFM56-5B4/2 was similar to the CFM56-5B1 but with a dual annual combustor and decreased thrust rating. CFM56-5B4/2P1 Same as CFM56-5B4/2P, except for increased flat rating ambient temperature (corner point), and a manually-activated takeoff thrust bump (within the certified standard day rating) for ambient temperatures above corner point. CFM56-5B5 Same as CFM56-5B1, except for decreased thrust ratings. CFM56-5B5/P Same as CFM56-5B5, except for redesigned high pressure compressor, high pressure turbine, and low pressure turbine. CFM56-5B5/3 Same as CFM56-5B5/P, except for redesigned high pressure compressor, high pressure turbine, and combustor. CFM56-5B6 Same as CFM56-5B1, except for decreased thrust ratings. CFM56-5B6/P Same as CFM56-5B6, except for redesigned high pressure compressor, high pressure turbine, and low pressure turbine. CFM56-5B6/3 Same as CFM56-5B6/P, except for redesigned high pressure compressor, high pressure turbine, and combustor. CFM56-5B6/2P Same as CFM56-5B6/2, except for redesigned high pressure compressor, high pressure turbine, and low pressure turbine. Note, the CFM56-5B6/2 was similar to the CFM56-5B1 but with a dual annual combustor and decreased thrust rating. CFM56-5B7 Same as CFM56-5B1, except for decreased thrust ratings. CFM56-5B7/P Same as CFM56-5B7, except for redesigned high pressure compressor, high pressure turbine, and low pressure turbine. CFM56-5B7/3 Same as CFM56-5B7/P, except for redesigned high pressure compressor, high pressure turbine, and combustor. CFM56-5B8/P Same as CFM56-5B1/P, except for reduced thrust rating. CFM56-5B8/3 Same as CFM56-5B8/P, except for redesigned high pressure compressor, high pressure turbine, and combustor. CFM56-5B9/P Same as CFM56-5B1/P, except for reduced thrust rating. CFM56-5B9/3 Same as CFM56-5B9/P, except for redesigned high pressure compressor, high pressure turbine, and combustor. CFM56-5B9/2P Same as CFM56-5B1/2P, except for reduced thrust rating. E37NE 26 of 28 NOTE 14. (CONT.) CFM56-5C2 Basic model. CFM56-5C2/4 Similar to CFM56-5C2, except for N1 limit increase through introduction of CFM56-5C4 redesigned fan stage airfoils. CFM56-5C2/F Similar to CFM56-5C2, except EGT limit increase through introduction of hot section modifications. CFM56-5C2/F4 Similar to CFM56-5C2/F, except for N1 limit increase through introduction of CFM56-5C4 redesigned fan stage airfoils. CFM56-5C2/G Similar to CFM56-5C2, except EGT limit increase through introduction of hot section modifications. CFM56-5C2/G4 Similar to CFM56-5C2/G, except for N1 limit increase through introduction of CFM56-5C4 redesigned fan stage airfoils. CFM56-5C2/P Same as CFM56-5C2/G4, except for redesigned high pressure compressor and high pressure turbine. CFM56-5C3/F Same as CFM56-5C2/F, except for increased thrust ratings. CFM56-5C3/F4 Similar to CFM56-5C3/F, except for N1 limit increase through introduction of CFM56-5C4 redesigned fan stage airfoils. CFM56-5C3/G Same as CFM56-5C2/G, except for increased thrust ratings CFM56-5C3/G4 Similar to CFM56-5C3/G, except for N1 limit increase through introduction of CFM56-5C4 redesigned fan stage airfoils. CFM56-5C3/P Same as CFM56-5C3/G4, except for redesigned high pressure compressor and high pressure turbine. CFM56-5C4 Same as CFM56-5C2/G, except for redesigned fan stage airfoils and increased thrust ratings. CFM56-5C4/P Same as CFM56-5C4, except for redesigned high pressure compressor and high pressure turbine. CFM56-5C4/1 Same as CFM56-5C4, except for introduction of takeoff thrust bump as a function of Mach number. CFM56-5C4/1P Same as CFM56-5C4/1, except for redesigned high pressure compressor and high pressure turbine. E37NE 27 of 28 NOTE 15. All CFM56-5B and CFM56-5C FADEC series engines have been approved to operate with certain faults present in the control system based on satisfaction of 14 CFR § 33 requirements and appropriate engine control system reliability requirements. FAA approved criteria pertaining to dispatch and maintenance requirements for the engine control system are specified in General Electric Document No. GEK 103085 (-5B family) and GEK 100741 (-5C family). These documents define the dispatchable configurations and maximum operating intervals. A control system reliability monitoring program has been established with CFM, as a contingency of the dispatch criteria approval, to ensure that overall engine control system and specific component failure rates do not exceed the maximum values permitted by the reliability analysis. NOTE 16. The normal 5 minute takeoff rating may be extended to 10 minutes for engine out contingency. NOTE 17. For the CFM56-5B/P, -5B/P1, -5B/2P, –5B/2P1, -5B/3 and -5B/3B1 series engines, the actual maximum permissible turbine exhaust gas temperature (EGT) is 10oC lower than the indicated EGT. An indicated EGT of 950oC corresponds to an actual EGT of 940oC, and an indicated EGT of 915oC corresponds to an actual EGT of 905oC. For CFM56-5C2/F, -5C2/F4, -5C3/F, and -5C3/F4 engines, the actual maximum permissible turbine EGT is 15oC higher than the indicated EGT. An indicated EGT of 950oC corresponds to an actual EGT of 965oC, and an indicated EGT of 915oC corresponds to an actual EGT of 930oC. For CFM56-5C2/G, -5C2/G4, -5C2/P, -5C3/G, -5C3/G4, -5C3/P, -5C4, -5C4/P, -5C4/1, and -5C4/1P engines, the actual permissible EGT is 25oC higher than the indicated EGT. An indicated EGT of 950oC corresponds to an actual EGT of 975oC, and an indicated EGT of 915oC corresponds to an actual EGT of 940oC. NOTE 18. For CFM56-5C2/4, -5C2/F4, -5C2/G4, -5C2/P, -5C3/F4, -5C3/G4 and -5C3/P engines, the actual maximum permissible N1 rotor speed is higher than the indicated N1. An indicated N1 of 4,800 RPM (100.3%) corresponds to an actual N1 of 4,985 RPM (104.2%). NOTE 19. CFM56-5B series includes: CFM56-5B1, -5B2, -5B4, -5B5, -5B6, -5B7 CFM56-5B/P series includes: CFM56-5B1/P, -5B2/P, -5B3/P, -5B4/P, -5B5/P, -5B6/P, -5B7/P, -5B8/P, -5B9/P CFM56-5B/3 series includes: CFM56-5B1/3, -5B2/3, -5B3/3, -5B4/3, -5B5/3, -5B6/3, -5B7/3, -5B8/3, -5B9/3 CFM56-5B/2P series includes: CFM56-5B1/2P, -5B2/2P, -5B3/2P, -5B4/2P, -5B6/2P, -5B9/2P CFM56-5B/P1 series includes: CFM56-5B3/P1, -5B4/P1 CFM56-5B/2P1 series includes: CFM56-5B3/2P1, -5B4/2P1 CFM56-5B/3B1 series includes: CFM56-5B3/3B1, -5B4/3B1 NOTE 20. Installation Manuals, Specific Operating Instructions, Service Bulletins, Overhaul and Maintenance Manuals, Repair Manuals, Vendor Manuals, and Design Changes which contain a statement that the document is EASA approved or approved under authority of DOA No. EASA.21J.086 or for approvals made before September 28, 2003 by DGAC are accepted by the FAA and considered FAA approved. Repair data and related instructions are considered FAA approved or accepted as applicable. These approvals pertain to the type design only. E37NE 28 of 28 NOTE 21. EXHAUST EMISSIONS AND FUEL VENTING CFM56-5C2 is in compliance with the emissions requirements of Special Federal Aviation Regulations No. 27-5. All other engine models are in compliance with the emissions requirements in 14 CFR Part 34, effective September 10, 1990, as amended by 34-1 through 34-3, with the exception of the following. 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 following CFM56-5B series engines models: CFM56-5B1/3 CFM56-5B2/3 CFM56-5B3/3 CFM56-5B3/3B1 CFM56-5B4/3 CFM56-5B4/3B1 CFM56-5B5/3 CFM56-5B6/3 CFM56-5B7/3 CFM56-5B8/3 CFM56-5B9/3 Fuel Venting Emission Standards: 14 CFR 34.11; in addition, 40 CFR 1031.30(b) Smoke Number (SN) Emission Standards: 14 CFR 34.21(e); in addition, 40 CFR 1031.60(a)(5) Carbon Monoxide (CO) Emission Standards: 14 CFR 34.21(d)(1)(ii); in addition, 40 CFR 1031.60(d) Hydrocarbons (HC) Emission Standards: 14 CFR 34.21(d)(1)(i); in addition, 40 CFR 1031.60(c) Oxides of Nitrogen (NOx) Emission Standards: 14 CFR 34.23(b)(1); in addition, 40 CFR 1031.60(e)(5) (also known as Tier 8 new type) non-volatile Particulate Matter (nvPM) Mass Concentration Emission Standards: 14 CFR 34.25(a)(1); in addition, 40 CFR 1031.60(a)(6) (also known as Tier 10) nvPM Mass and Number Emission Standards: 14 CFR 34.25(a)(2); in addition, 40 CFR 1031.60(b)(2) (also known as Tier 11 in-production) In addition to the FAA's finding of compliance based on the certification requirements defined in this TCDS, the engine manufacturer has declared that the ICAO emissions standards identified in Annex 16, Volume II, Fourth Edition, Amendment 10, effective July 20, 2020, have also been demonstrated for the following: • Part II, Chapter 2 for Fuel Venting, • Part III, Chapter 2, Section 2.2.2 for Smoke number, • Part III, Chapter 2, Section 2.3.2 for Carbon monoxide and Hydrocarbons, • Part III, Chapter 2, Section 2.3.2.e for Oxides of Nitrogen (also known as CAEP/8), • Part III, Chapter 4, Section 4.2.2.1 for nvPM Mass Concentration (also known as CAEP/10), and • Part III, Chapter 4, Section 4.2.2.2 for nvPM Mass and Number (also known as CAEP/11) ----END---- ``` ## ADs None name its models. --- 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.