Fill and Sign the Service Agreement and Duplicate Gsa Form

TCDS NUMBER E00056EN REVISION: 9* DATE: July 27, 2011 CFM INTERNATIONAL, S.A. U.S. DEPARTMENT OF TRANSPORTATION MODELS: CFM56-7B20 CFM56-7B20/2 CFM56-7B20E CFM56-7B22 CFM56-7B22/B1 CFM56-7B22/3 CFM56-7B22E CFM56-7B22E/B1 CFM56-7B24/2 CFM56-7B24/B1 CFM56-7B24/3B1 CFM56-7B24E CFM56-7B26/3 CFM56-7B26 CFM56-7B26/B1 CFM56-7B26/3B1 CFM56-7B26/3F CFM56-7B26/B2 CFM56-7B26E/B1 CFM56-7B26E/B2 CFM56-7B26E/F CFM56-7B27 CFM56-7B27AE CFM56-7B27/3 CFM56-7B26/3B2 CFM56-7B27/B1 CFM56-7B27/2 CFM56-7B27/3B1 CFM56-7B27A/3 CFM56-7B27E/B1 CFM56-7B27E/B3 CFM56-7B27E CFM56-7B27E/B1F FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET E00056EN CFM56-7B20/3 CFM56-7B22/2 CFM56-7B22/3B1 CFM56-7B24 CFM56-7B24/3 CFM56-7B24E/B1 CFM56-7B26/2 CFM56-7B26/3B2F CFM56-7B26E CFM56-7B26E/B2F CFM56-7B27A CFM56-7B27/3F CFM56-7B27/B3 CFM56-7B27/3B3 CFM56-7B27/3B1F CFM56-7B27E/F Engines of models described herein conforming with this data sheet (which is part of Type Certificate Number E00056EN) 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 TYPE CFM56-7B20 CFM56-7B22 CFM56-7B24 High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE and 7BE/F series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) 22,700/ 10,097 daN 24,200/ 10,765 daN 22,300/ 19,400/ 9,920 daN 8,630 daN AMBIENT TEMPERATURE 86oF / 30oC -77oF / 25oC -- 22,800/ 10,142 daN 20,600/ 9,163 daN Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. Flat rating Takeoff Maximum continuous --- * PAGE REV. 1 9 2 8 3 8 4 8 5 8 6 8 7 8 8 8 9 8 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 8 8 8 8 8 8 8 8 8 8 8 8 8 9 9 9 LEGEND: "- -" INDICATES "SAME AS PRECEDING MODEL" "---" NOT APPLICABLE NOTE: SIGNIFICANT CHANGES ARE BLACK-LINED IN THE LEFT MARGIN. E00056EN I. MODELS (CONT.) FUEL SYSTEM Fuel pump / SNECMA part number (P/N) (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N OIL IGNITION SYSTEM Two ignition units Unison Simmonds Two igniter plugs Unison Champion PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters 2 of 25 CFM56-7B20 CFM56-7B22 See NOTE 7 for approved fuels. CFM56-7B24 340-402-104 340-402-105 --- --- 1853M56 -- -- 1851M50 1853M33 2042M67 2044M16 ----- ----- 1853M78 2044M25 --- --- 340-131-732 340-131-721 340-131-712 340-131-737 340-131-726 340-131-717 340-203-401 340-203-301 340-203-201 340-200-050 340-199-250 340-198-850 340-200-150 340-199-350 340-198-950 Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFMService Bulletin CFM56-7B 79-001 list approved brand oils. GE P/N 9238M66 1538M69 1374M12 1374M13 INCHES / MILLIMETERS 98.7/2507.5 83.4/2118.0 72.0/1829.0 --- --- --- --- -- -- --- --- Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5260.0 --2385.9 --STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4+ 1.0 5269+ 25 --- --- E00056EN II. MODELS TYPE 3 of 25 CFM56-7B26 CFM56-7B27 CFM56-7B27A CFM56-7B20/2 CFM56-7B22/2 High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multistage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE and 7BE/F series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. 26,300/ 11,699 daN 27,300/ 12,143 daN --- 20,600/ 9,163 daN 22,700/ 10,097 daN Maximum continuous, sea level static thrust, lb. 25,900/ 11,521 daN 25,900/ 11,521 daN --- 19,400/ 8,630 daN 22,300/ 9,920 daN --- --- --- Flat rating Takeoff Maximum continuous FUEL SYSTEM Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N OIL IGNITION SYSTEM Two ignition units Unison Simmonds Two igniter plugs Unison Champion PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) AMBIENT TEMPERATURE 86oF / 30oC -77oF / 25oC -See NOTE 7 for approved fuels. 340-402-104 340-402-105 --- --- --- --- 1853M56 -- -- -- -- 1851M50 1853M33 2042M67 2044M16 ----- ------ 1851M50 ---- ----- 1853M78 2044M25 --- --- --- --- 340-138-710 340-203-701 340-131-752 340-131-742 340-138-715 --340-131-757 340-131-747 340-203-201 --340-203-601 340-203-501 ----340-201-450 340-200-850 ----340-201-550 340-200-950 Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. GE P/N 340-138-720 340-138-725 340-203-301 ----- --- --- --- --- -1374M12 -1374M13 INCHES / MILLIMETERS -98.7/2507.5 --- --- --- -- -- -- --- --- --- --- 9238M66 1538M69 83.4/2118.0 72.0/1829.0 E00056EN II. MODELS (CONT.) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters III. MODELS TYPE 4 of 25 CFM56-7B26 CFM56-7B27 CFM56-7B27A CFM56-7B20/2 CFM56-7B22/2 Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5260 -5282 5360 -2385.9 -2395.9 2431.3 -STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4 + 1.0 5269 + 25 --- --- --- --- CFM56-7B24/2 CFM56-7B26/2 CFM56-7B27/2 CFM56-7B26/B1 High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE and 7BE/F series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. Flat rating Takeoff Maximum continuous FUEL SYSTEM Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N 26,300/ 11,699 daN 27,300/ 12,143 daN 26,300/ 11,699 daN 25,900/ 22,800/ 11,521 daN 10,142 daN AMBIENT TEMPERATURE 86oF / 30oC -77oF / 25oC -See NOTE 7 for approved fuels 25,900/ 11,521 daN 25,900/ 11,521 daN --- --- 24,200/ 10,765 daN 340-402-104 340-402-105 --- --- --- 1853M56 -- -- -- 1851M50 1853M33 2042M67 2044M16 ----- ----- ----- 1853M78 2044M25 --- --- --- 340-138-730 340-138-735 340-203-401 340-138-740 340-138-745 340-203-501 340-138-750 340-138-755 340-203-601 340-203-511 340-143-201 340-143-301 340-201-050 340-201-150 E00056EN III. MODELS (CONT.) OIL IGNITION SYSTEM Two ignition units Unison Simmonds Two igniter plugs Unison Champion PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters IV. MODELS TYPE 5 of 25 CFM56-7B24/2 CFM56-7B26/2 CFM56-7B27/2 CFM56-7B26/B1 Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. GE P/N 9238M66 1538M69 1374M12 1374M13 INCHES / MILLIMETERS 98.7/2507.5 83.4/2118.0 72.0/1829.0 --- --- --- --- --- --- -- -- -- --- --- --- Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5360 --5260 2431.3 --2385.9 STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4 + 1.0 5269 + 25 --- --- --- CFM56-7B27/B1 CFM56-7B27/B3 CFM56-7B22/B1 CFM56-7B24/B1 High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multistage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE and 7BE/F series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. Flat rating Takeoff Maximum continuous FUEL SYSTEM Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N -- 22,700/ 10,097 daN 24,200/ 10,765 daN -25,900/ 11,521 daN AMBIENT TEMPERATURE 86oF / 30oC -77oF / 25oC -See NOTE 7 for approved fuels. 22,300/ 9,920 daN 22,800/ 10,142 daN 96.8oF / 36oC -- 105.8oF / 41oC -- 27,300/ 12,143 daN 340-402-104 340-402-105 --- --- --- 1853M56 -- -- -- E00056EN IV. MODELS (CONT.) Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N OIL IGNITION SYSTEM Two ignition units Unison Simmonds Two igniter plugs Unison Champion PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters 6 of 25 CFM56-7B27/B1 CFM56-7B27/B3 CFM56-7B22/B1 CFM56-7B24/B1 1851M50 1853M33 2042M67 2044M16 ----- ----- ----- 1853M78 2044M25 --- --- --- 340-142-001 340-143-441 340-142-801 340-142-101 340-143-451 340-142-901 340-203-311 340-203-631 340-203-611 340-199-450 340-202-050 340-201-650 340-199-550 340-202-150 340-201-750 Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. GE P/N 9238M66 1538M69 1374M12 1374M13 INCHES / MILLIMETERS 98.7/2507.5 83.4/2118.0 72.0/1829.0 340-142-201 340-142-301 340-203-411 340-200-250 340-200-350 --- --- --- --- --- --- -- -- -- --- --- --- Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5260 ---2385.9 ---STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4 + 1.0 5269 + 25 --- --- --- E00056EN V. MODELS TYPE 7 of 25 CFM56-7B26/B2 CFM56-7B26/3B2 High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multistage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE and 7BE/F series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) Takeoff (5 min. See NOTE 13), sea level, static thrust, lb. 26,300/ 11,699 daN 26,300/ 11,699 daN Maximum continuous, sea level static thrust, lb. 22,800/ 10,142 daN 22,800/ 10,142 daN Flat rating Takeoff Maximum continuous FUEL SYSTEM Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N OIL IGNITION SYSTEM Two ignition units Unison Simmonds Two igniter plugs Unison Champion PRINCIPLE DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter AMBIENT TEMPERATURE 95F / 35C 77F / 25C See NOTE 7 for approved fuels. --- 340-402-104 340-402-105 340-402-105 1853M56 -- 1851M50 1853M33 2042M67 2044M16 ----- 1853M78 2044M25 --- 340-203-521 340-203-521 Synthetic type conforming to GE Specification D50TFI, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. GE P/N 9238M66 1538M69 1374M12 1374M13 INCHES / MILLIMETERS 98.7 / 2507.5 83.4 / 2118.0 72.0 / 1829.0 ------ --- E00056EN V. MODELS (CONT.) WEIGHT (dry) 8 of 25 CFM56-7B26/B2 CFM56-7B26/3B2 Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters 5260 2385.9 --- STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) VI. MODELS TYPE 207.4 + 1.0 5269 + 25 --- CFM56-7B20/3 CFM56-7B22/3 CFM56-7B24/3 High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE and 7BE/F series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. 20,600/ 9,163 daN 22,700/ 10,097 daN 24,200/ 10,765 daN Maximum continuous, sea level static thrust, lb. 19,400/ 8,630 daN 22,300/ 9,920 daN 22,800/ 10,142 daN Flat rating Takeoff Maximum continuous FUEL SYSTEM Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) AMBIENT TEMPERATURE 86oF / 30oC -77oF / 25oC -See NOTE 7 for approved fuels. --- -- -- -- -- 1851M50 1853M33 2042M67 2044M16 ----- ----- 1853M78 2044M25 --- --- 340-203-201 340-203-301 340-203-401 340-402-105 1853M56 Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N E00056EN 9 of 25 VI. MODELS (CONT.) OIL CFM56-7B20/3 CFM56-7B22/3 CFM56-7B24/3 Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. IGNITION SYSTEM GE P/N Two ignition units Unison Simmonds 9238M66 1538M69 --- --- Two igniter plugs Unison Champion 1374M12 1374M13 --- --- -- -- --- --- PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters INCHES / MILLIMETERS 98.7/2507.5 83.4/2118.0 72.0/1829.0 Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5260.0 --2385.9 --STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4+ 1.0 5269+ 25 --- CFM56-7B27/3 --- VII. MODELS CFM56-7B26/3 TYPE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE and 7BE/F series: improved HPC diffuser, HPT and LPT performance CFM56-7B26/3B1 CFM56-7B27A/3 RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. Flat rating Takeoff Maximum continuous 27,300/ 12,143 daN 26,300/ 11,699 daN 27,300/ 12,143 daN 25,900/ 25,900/ 11,521 daN 11,521 daN AMBIENT TEMPERATURE 86oF / 30oC -77oF / 25oC -- 25,900/ 11,521 daN 25,900/ 11,521 daN --- --- 26,300/ 11,699 daN E00056EN VII. MODELS (CONT.) FUEL SYSTEM Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N OIL IGNITION SYSTEM Two ignition units Unison Simmonds Two igniter plugs Unison Champion PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters 10 of 25 CFM56-7B26/3 CFM56-7B27/3 See NOTE 7 for approved fuels. CFM56-7B26/3B1 CFM56-7B27A/3 340-402-105 -- -- -- 1853M56 -- -- -- 1851M50 1853M33 2042M67 2044M16 ----- ----- ----- 1853M78 2044M25 --- --- --- 340-203-501 340-203-601 340-203-511 340-203-701 Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. GE P/N 9238M66 1538M69 1374M12 1374M13 INCHES / MILLIMETERS 98.7/2507.5 83.4/2118.0 72.0/1829.0 --- --- --- --- --- --- -- -- -- --- --- --- Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5260 --5282 2385.9 --2395.9 STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4 + 1.0 5269 + 25 --- --- --- E00056EN VIII. MODELS TYPE 11 of 25 CFM56-7B27/3F CFM56-7B27/3B1F CFM56-7B26/3F CFM56-7B26/3B2F High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE and 7BE/F series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. Flat rating Takeoff Maximum continuous FUEL SYSTEM Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N OIL IGNITION SYSTEM Two ignition units Unison Simmonds Two igniter plugs Unison Champion PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) --- 26,300/ 11,699 daN --- --- 25,900/ 11,521 daN 22,800/ 10,142 daN --- --- --- 340-402-105 -- -- -- 1853M56 -- -- -- 1851M50 1853M33 2042M67 2044M16 ----- ----- ----- 1853M78 2044M25 --- --- --- 340-205-001 340-205-111 340-205-101 340-205-021 27,300/ 12,143 daN 25,900/ 11,521 daN AMBIENT TEMPERATURE 86oF / 30oC 77oF / 25oC See NOTE 7 for approved fuels. Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. GE P/N 9238M66 1538M69 1374M12 1374M13 INCHES / MILLIMETERS 98.7/2507.5 83.4/2118.0 72.0/1829.0 --- --- --- --- --- --- -- -- -- --- --- --- E00056EN VIII. MODELS (CONT.) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters IX. MODELS TYPE 12 of 25 CFM56-7B27/3F CFM56-7B27/3B1F CFM56-7B26/3F CFM56-7B26/3B1F Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5260 ---2385.9 ---STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4 + 1.0 5269 + 25 --- --- --- CFM56-7B27/3B1 CFM56-7B27/3B3 CFM56-7B22/3B1 CFM56-7B24/3B1 High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multistage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE and 7BE/F series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. Flat rating Takeoff Maximum continuous FUEL SYSTEM Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N OIL IGNITION SYSTEM -- 22,700/ 10,097 daN 24,200/ 10,765 daN -25,900/ 11,521 daN AMBIENT TEMPERATURE 86oF / 30oC -77oF / 25oC -See NOTE 7 for approved fuels. 22,300/ 9,920 daN 22,800/ 10,142 daN 96.8oF / 36oC -- 105.8oF / 41oC -- 27,300/ 12,143 daN 340-402-105 -- -- -- 1853M56 -- -- -- 1851M50 1853M33 2042M67 2044M16 ----- ----- ----- 1853M78 2044M25 --- --- --- 340-203-611 340-203-631 340-203-311 340-203-411 Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. GE P/N Two ignition units Unison Simmonds 9238M66 1538M69 --- --- --- Two igniter plugs Unison Champion 1374M12 1374M13 --- --- --- E00056EN IX. MODELS (CONT.) PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters X. MODELS TYPE 13 of 25 CFM56-7B27/3B1 CFM56-7B27/3B3 INCHES / MILLIMETERS -98.7/2507.5 --- 83.4/2118.0 72.0/1829.0 CFM56-7B22/3B1 CFM56-7B24/3B1 -- -- --- --- Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5260 ---2385.9 ---STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4 + 1.0 5269 + 25 --- --- --- CFM56-7B20E CFM56-7B22E CFM56-7B24E CFM56-7B24E/B1 High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) 22,700/ 10,097 daN 24,200/ 10,765 daN 24,200/ 10,765 daN Maximum continuous, sea level static thrust, lb. Flat rating Takeoff Maximum continuous 22,300/ 19,400/ 9,920 daN 8,630 daN AMBIENT TEMPERATURE 86 oF / 30oC -77oF / 25oC -- 22,800/ 10,142 daN 22,800/ 10,142 daN --- 105.8 oF / 41oC -- FUEL SYSTEM See NOTE 7 for approved fuels. Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. 20,600/ 9,163 daN 340-402-105 --- --- -- 1853M56 -- -- -- 1851M50 1853M33 2042M67 2044M16 ----- ----- ----- 1853M78 2044M25 --- --- --- Identification plugs / SNECMA P/N 340-203-201 340-203-301 340-203-401 340-203-411 X. MODELS(CONT) CFM56-7B20E CFM56-7B22E CFM56-7B24E Fuel pump / SNECMA part number (P/N) (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software CFM56-7B24E/B1 E00056EN 14 of 25 OIL Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. IGNITION SYSTEM GE P/N Two ignition units Unison Simmonds Two igniter plugs Unison Champion PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters XI. MODELS TYPE 9238M66 1538M69 1374M12 1374M13 INCHES / MILLIMETERS 98.7/2507.5 83.4/2118.0 72.0/1829.0 --- --- --- --- --- --- -- -- -- --- --- --- Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5280 ---2395 ---STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4+ 1.0 5269+ 25 --- --- --- CFM56-7B26E CFM56-7B27E CFM56-7B26E/B1 CFM56-7B27AE High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. Flat rating Takeoff Maximum continuous 27,300/ 12,143 daN 26,300/ 11,699 daN 27,300/ 12,143 daN 25,900/ 25,900/ 11,521 daN 11,521 daN AMBIENT TEMPERATURE 86oF / 30oC -77oF / 25oC -- 25,900/ 11,521 daN 25,900/ 11,521 daN --- --- 26,300/ 11,699 daN E00056EN XI. MODELS (CONT.) FUEL SYSTEM Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N OIL IGNITION SYSTEM Two ignition units Unison Simmonds Two igniter plugs Unison Champion PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters 15 of 25 CFM56-7B26E CFM56-7B27E See NOTE 7 for approved fuels. CFM56-7B26E/B1 CFM56-7B27AE 340-402-105 -- -- -- 1853M56 -- -- -- 1851M50 1853M33 2042M67 2044M16 ----- ----- ----- 1853M78 2044M25 --- --- --- 340-203-501 340-203-601 340-203-511 340-203-701 Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. GE P/N 9238M66 1538M69 1374M12 1374M13 INCHES / MILLIMETERS 98.7/2507.5 83.4/2118.0 72.0/1829.0 --- --- --- --- --- --- -- -- -- --- --- --- Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5280 --5302 2395 --2405 STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4 + 1.0 5269 + 25 --- --- --- E00056EN XII. MODELS TYPE 16 of 25 CFM56-7B27E/F CFM56-7B27E/B1F CFM56-7B26E/F CFM56-7B26E/B2F High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multi-stage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. Flat rating Takeoff Maximum continuous FUEL SYSTEM Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N OIL IGNITION SYSTEM Two ignition units Unison Simmonds Two igniter plugs Unison Champion PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) --- 26,300/ 11,699 daN --- --- 25,900/ 11,521 daN 22,800/ 10,142 daN --- --- 95.oF / 35oC -- 340-402-105 -- -- -- 1853M56 -- -- -- 1851M50 1853M33 2042M67 2044M16 ----- ----- ----- 1853M78 2044M25 --- --- --- 340-205-001 340--111 340-205-101 340-205-021 27,300/ 12,143 daN 25,900/ 11,521 daN AMBIENT TEMPERATURE 86oF / 30oC 77oF / 25oC See NOTE 7 for approved fuels. Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. GE P/N 9238M66 1538M69 1374M12 1374M13 INCHES / MILLIMETERS 98.7/2507.5 83.4/2118.0 72.0/1829.0 --- --- --- --- --- --- -- -- -- --- --- --- E00056EN XII. MODELS (CONT.) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters XIII. MODELS TYPE 17 of 25 CFM56-7B27E/F CFM56-7B27E/B1F CFM56-7B26E/F CFM56-7B26E/B2F Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5280 ---2395 ---STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4 + 1.0 5269 + 25 --- --- --- CFM56-7B27E/B1 CFM56-7B27E/B3 CFM56-7B22E/B1 CFM56-7B26E/B2 High bypass turbofan; coaxial front fan/booster driven by multi-stage low pressure turbine, multistage compressor with one-stage high pressure turbine CFM56-7B series: single annular combustor CFM56-7B/2 series: double annular combustor CFM56-7B/3 series: improved emissions single annular combustor CFM56-7B/3F series: improved emissions single annular combustor and increased EGT CFM56-7BE series: improved HPC diffuser, HPT and LPT performance RATINGS (See NOTE 4) Takeoff (5 min. see NOTE 13), sea level, static thrust, lb. Maximum continuous, sea level static thrust, lb. Flat rating Takeoff Maximum continuous FUEL SYSTEM Fuel pump / SNECMA P/N (Combined boost and single element gear-type pump) Hydromechanical unit / GE P/N Electronic control unit / GE P/N - Hardware - Software Identification plugs / SNECMA P/N -- 22,700/ 10,097 daN 26,300/ 10,699 daN -25,900/ 11,521 daN AMBIENT TEMPERATURE 86oF / 30oC -77oF / 25oC -See NOTE 7 for approved fuels. 22,300/ 9,920 daN 22,800/ 10,142 daN 96.8oF / 36oC -- 95.oF / 35oC -- 27,300/ 12,143 daN 340-402-105 -- -- -- 1853M56 -- -- -- 1851M50 1853M33 2042M67 2044M16 ----- ----- ----- 1853M78 2044M25 --- --- --- 340-203-611 340-203-631 340-203-311 340-203-521 E00056EN 18 of 25 CFM56-7B27E/B1 OIL IGNITION SYSTEM CFM56-7B27E/B3 CFM56-7B22E/B1 CFM56-7B26E/B2 Synthetic type conforming to GE Specification D50TF1, Type I and Type II. CFM Service Bulletin CFM56-7B 79-001 list approved brand oils. GE P/N Two ignition units Unison Simmonds 9238M66 1538M69 --- --- --- Two igniter plugs Unison Champion 1374M12 1374M13 --- --- --- -- -- -- --- --- --- PRINCIPAL DIMENSIONS Length (fan case forward flange to LPT frame aft flange) Width (maximum envelope) Height (fan case forward flange outer diameter) WEIGHT (dry) Pounds Kilograms CENTER OF GRAVITY LOCATIONS Inches Millimeters CERTIFICATION BASIS INCHES / MILLIMETERS 98.7/2507.5 83.4/2118.0 72.0/1829.0 Includes basic engine accessories and optional equipment as listed in manufacturer’s engine specification, including engine mounted portions of the condition monitoring instrumentation. 5280 ---2395 ---STATION, ENGINE ONLY (REFER TO INSTALLATION DRAWING) 207.4 + 1.0 5269 + 25 --- --- --- 1. 14 CFR Part 33 effective February 1, 1965, with Amendments 33-1 through 33-15 thereto. 2. See NOTE 22 for emissions certification basis. MODEL CFM56-7B18 CFM56-7B20 CFM56-7B22 CFM56-7B24 CFM56-7B26 CFM56-7B27 CFM56-7B20/2 CFM56-7B22/2 CFM56-7B24/2 CFM56-7B26/2 CFM56-7B27/2 CFM56-7B26/B1 CFM56-7B27/B1 CFM56-7B27/B3 CFM56-7B22/B1 CFM56-7B24/B1 CFM56-7B27A CFM56-7B22/B2 CFM56-7B26/B2 CFM56-7B18/3 CFM56-7B20/3 CFM56-7B22/3 CFM56-7B22/3B1 APPLICATION DATE NOV 28, 1995 NOV 28, 1995 NOV 28, 1995 NOV 28, 1995 NOV 28, 1995 NOV 28, 1995 NOV 28, 1995 NOV 28, 1995 NOV 28, 1995 NOV 28, 1995 NOV 28, 1995 MAR 4, 1998 MAR 4, 1998 JUL 30, 1998 JUN 11, 1997 JUN 11, 1997 SEPT 8, 1999 AUG 20, 2001 AUG 20, 2001 APR 23, 2004 APR 23, 2004 APR 23, 2004 APR 23, 2004 TYPE CERTIFICATE ISSUED/AMENDED DEC 17, 1996 DEC 17, 1996 DEC 17, 1996 DEC 17, 1996 DEC 17, 1996 DEC 17, 1996 NOV 14, 1997 NOV 14, 1997 NOV 14, 1997 NOV 14, 1997 NOV 14, 1997 OCT 30, 1998 OCT 30, 1998 OCT 30, 1998 MAY 9, 2000 MAY 9, 2000 APR 27, 2001 APR 25, 2003 APR 25, 2003 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 TYPE CERTIFICATE WITHDRAWN OCT 17, 2008 (*) OCT 17, 2008(*) OCT 17, 2008(*) E00056EN CERTIFICATION BASIS (cont) 19 of 25 CFM56-7B22/3B2 CFM56-7B24/3 CFM56-7B24/3B1 CFM56-7B26/3 CFM56-7B26/3B1 CFM56-7B26/3B2 CFM56-7B26/3F CFM56-7B26/3B2F CFM56-7B27/3 CFM56-7B27/3B1 CFM56-7B27/3B3 CFM56-7B27/3F CFM56-7B27/3B1F CFM56-7B27A/3 CFM56-7B20E CFM56-7B22E CFM56-7B22E/B1 CFM56-7B24E CFM56-7B24E/B1 CFM56-7B26E CFM56-7B26E/B1 CFM56-7B26E/B2 CFM56-7B26E/F CFM56-7B26E/B2F CFM56-7B27E CFM56-7B27E/B1 CFM56-7B27E/B3 CFM56-7B27E/F CFM56-7B27E/B1F CFM56-7B27AE APR 23, 2004 APR 23, 2004 APR 23, 2004 APR 23, 2004 APR 23, 2004 APR 23, 2004 DEC 15, 2005 DEC 15, 2005 APR 23, 2004 APR 23, 2004 APR 23, 2004 APR 23, 2004 APR 23, 2004 APR 23, 2004 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 AUG 28, 2008 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 JUN 14, 2006 OCT 17, 2008 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 JUL 30, 2010 OCT 17, 2008(*) (*) Effective October 17, 2008 the models designation CFM56-7B18, CFM56-7B22/B2, CFM56-7B18/3, CFM56-7B22/3B2 were withdrawn at the request of the manufacturer. None of these models were released to revenue service. The Direction Generale de L'Aviation Civile (DGAC) originally type certificated these engine models under DGAC Certificate de Type Moteur M21. The FAA validated these products under Type Certificate Number E00056EN. 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.004 was issued June 14, 2006. The original production basis was French “Agreement de Production” No. F.G.007 or P03 issued by Direction Generale de L’Aviation Civile (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 European Aviation Safety Agency (EASA) Production Certificate FR.21G.0007. (See NOTE 10). IMPORT REQUIREMENTS 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 E00056EN and is in a condition for safe operation.’ NOTES E00056EN 20 of 25 NOTE 1. MAXIMUM PERMISSIBLE TEMPERATURES (ALL MODELS) TURBINE EXHAUST GAS (T495) (See NOTE 14) Takeoff (5 min.) Maximum continuous Starting As measured by a harness of eight thermocouples located at the second stage low pressure turbine vane: 950oC 925oC 725oC Time temperature envelope Refer to model’s S.O.I. FUEL PUMP INLET OIL SUPPLY (See NOTE 18) Continuous operation Transient (45 minutes) NOTE 2. Fuel limits CFMI-TP.01.14 REFER TO THE APPROPRIATE INSTALLATION MANUAL. 140oC/284oF 155oC/311oF FUEL AND OIL PRESSURE LIMITS Fuel system pressure limits required to meet all engine operating conditions extend from a minimum fuel pressure of not less than 5 psia (0.35 bar absolute) above the true fuel vapor pressure to a maximum fuel pressure of 148 psia (10.2 bar absolute) with a fuel vapor/liquid ratio < 0.45 at all conditions. For specific installation limits, see Installation Manual, CFM7B01, Part A, Section 5, Figures A2 and A3. Oil limits NOTE 3. The minimum pressure limit is 13 psid (90 kPa differential). The maximum pressure limit during cold starts is 305 psid (2102 kPa differential), limited by a pressure-relief valve. See NOTE 12. ACCESSORY DRIVE PROVISIONS ALL MODELS -7B27A,-7B27A/3 & -7B27AE *(3) EXCEPT -7B27A, -7B27A/3 & -7B27AE ELECTRICAL Rotation (1) Speed ratio to core (2) Pad Rating (kW) Shear Torque (in-lb) Maximum overhung moment (in-lb) CW 0.565 135 9,000 950 CW .565 239.4*(3) 17,500 1,540 HYDRAULIC PUMP Rotation (1) Speed ratio to core (2) Pad Rating (in-lb) Shear Torque (in-lb) Maximum overhung moment (in-lb) CW 0.256 1,550 4,400 166 CW 0.256 1,550 4,400 166 (1) (2) *(3) CW = CLOCKWISE FACING PAD / CCW = COUNTERCLOCKWISE FACING PAD 100% CORE ENGINE SPEED = 14,460 RPM FOR 7B27A, 7B27A/3 & 7B27AE, UNDER CERTAIN BLEED CONDITIONS, MAXMUM PAD RATING IS NOT AVAILABLE. REFER TO INSTALLATION MANUAL CFM-7B01 FOR MAX PERMISSIBLE EXTRACTION LOADS UNDER THESE CONDITIONS. E00056EN NOTE 4. 21 of 25 Engine ratings are based on calibrated stand performance (sea level static) under the following conditions: Takeoff thrust is nominally independent of ambient temperature (flat rated) up to ambient temperature of: o o o o o o o o o  Std + 15 C (30 C, 86 F) for all models except as noted below o  Std + 21 C (36 C, 96.8 F) for 7B22/B1, 7B22/3B1 and 7B22/B1 o  Std + 26 C (41 C, 105.8 F) for 7B24/B1, 7B24/3B1 and 7B24E/B1 o  Std + 20 C (35 C, 95 F) for 7B26/B2, 7B26/3B2, 7B26/3B2F, 7B26E/B2 and 7B26E/B2F Maximum continuous is nominally independent of ambient temperature (flat rated) up to o o o ambient temperature of Std. + 10 C (25 C, 77 F) for all models. Zero customer bleed and horsepower extraction. 100% inlet recovery. NOTE 5. Low pressure rotor (N1) High pressure rotor (N2) NOTE 6. LOCATION Fan Discharge HPC Stage 5 only Compressor discharge only Based on the production flight exhaust system. MAXIMUM PERMISSIBLE ENGINE ROTOR SPEEDS (ALL MODELS) RPM % 5,382 104 15,183 105 100% N1 = 5,175 RPM, 100% N2= 14,460 RPM MAXIMUM PERMISSIBLE AIR BLEED EXTRACTION (ALL MODELS)* FAN CORRECTED SPEED FLOW LIMIT 2% fan airflow All speeds above minimum idle All speeds above minimum idle 10% core airflow Minimum idle to 61% N1K 61% to 82.5% N1K Above 82.5% N1K 12% core airflow Linear variation from 12% to 7% core airflow 7% core airflow 13% core airflow Minimum idle to 61% N1K Linear variation from 13% to 10% core airflow 61% to 82.5% N1K 10% core airflow Above 82.5% N1K * FOR THE 7B27A, 7B27A/3 & 7B27AE ENGINES, UNDER CERTAIN GEARBOX LOAD CONDITIONS, THIS BLEED SCHEDULE WILL NOT BE AVAILABLE. FOR PERMITTED BLEED SCHEDULES UNDER THESE CONDITIONS, REFER TO CFM56-7B INSTALLATION MANUAL CFM7B01. HPC Stage 5 and compressor discharge combined 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 GE 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, CFMI-TP.01.14, Section 3, for additive usage. NOTE 8. Life limits established for critical rotating components are published in Chapter 5 of the CFM56-7B Engine Shop Manual, CFM-TP.SM.10. NOTE 9. Power setting, power checks and control of engine thrust output in all operations is to be based on CFM engine charts referring to fan speed. Fan speed sensors are included in the engine assembly for this purpose. E00056EN NOTE 10. 22 of 25 The type certificate holder, CFM International, S.A., is a company established and jointly owned by Societe Nationale l’Etude et de Construction de Moteurs d’Aviation (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 under EASA Type Certificate E.004. Engines of the same model designation produced in the United States under Type Certificate No. E00055EN are identical to and fully interchangeable with engines produced under this type certificate. Similarly, modules, assemblies, or parts produced in the United States under Production Certificate No. 108 are eligible for use in engines produced under this type certificate These engines, when produced by General Electric under Production Certificate No.108, are identified by an even numbered serial number prefix ( Reference CFM56-7B Service Bulletin 72-0747 for a list of approved prefixes). All engines identified by an odd numbered prefix () will be produced by SNECMA under Production Certificate No.F.G.007. (Reference CFM56-7B Service Bulletin 72-0747 for a list of approved prefixes) Effective September 28, 2004, engines produced by SNECMA were produced under EASA Production Certificate FR.21G.0007. Engine serial number 893-133 was the first engine produced by SNECMA under the EASA Production Certificate NOTE 11. The minimum permissible idle in flight corresponds to N2=64.7% (9,350 rpm) below 25oF. Between 25oF (-3.8oC) and 40oF (4.4oC), the idle speed varies from 64.7% (9,350 rpm) to 58.8% (8,500 rpm). Above 40oF (4.4oC), the minimum permissible idle speed is 58.8% (8,500 rpm). Other EEC schedule limitations, such as minimum fuel flow and minimum PS3 (including Mach No. bias for 7B27A,7B27A/3 & -7B27AE), may result in minimum N2 speed limitations in flight that are higher than the N2 limits listed above. All limits are nonadjustable and are preset into the EEC schedules. NOTE 12. 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 Instructions, CFMI-TP.01.14, Section 6. NOTE 13. The normal 5 minute takeoff rating may be extended to 10 minutes for engine out contingency. NOTE 14 (a). The indicated maximum permissible takeoff exhaust gas temperature (EGT) is 950oC. These indicated takeoff EGT redlines are accomplished via an EGT shunt and an EGT trim in the ECU software as noted below. The effect on EGT (units oC) with respect to the indicated takeoff EGT redline value of 950oC for each of the models is summarized below: NOTE 14 (a) (CONT). Model 7B20, 7B20/3 7B22, 7B22/3 7B22/B1, 7B22/3B1 7B24, 7B24/3 7B24/B1, 7B24/3B1 7B26, 7B26/B1, 7B26/B2, 7B26/2, 7B26/3B1, 7B26/3B2, 7B26/3 7B27, 7B27A, 7B27/B1, 7B27/B3, 7B27/3, 7B27/3B1, 7B27/3B3, 7B27A/3 7B20/2 7B22/2 7B24/2 7B26/2 Actual Measured Takeoff Redline Value Authorized Indicated Takeoff EGT level with 30oC Shunt Only* Maximum EGT Trim Level** Indicated Takeoff EGT Redline 884 886 907 908 920 920 914 916 937 938 950 950 36 34 13 12 0 0 950 950 950 950 950 950 920 950 0 950 894 896 918 930 914 916 938 950 36 34 12 0 950 950 950 950 E00056EN 7B27/2 7B26/3F, 7B26/3B2F, 7B27/3F, 7B27/3B1F 7B20E 7B22E 7B22E/B1 7B24E 7B24E/B1 7B26E/B1, 7B26E/B2, 7B26E 7B27E, 7B27E/B1, 7B27E/B3, 7B27AE 7B26E/F, 7B26E/B2F, 7B27E/F, 7B27E/B1F 23 of 25 930 940 950 950 0 0 950 950 904 906 927 928 940 940 914 916 937 938 950 950 36 34 13 12 0 0 950 950 950 950 950 950 940 950 0 950 928 960 938 950 12 0 950 950 * EGT shunt adds 30oC to actual measured engine EGT on CFM56-7B, 7B/3 and 7BE series engines, 10oC to actual measured engine EGT on CFM56-7B/3F and –7BE/F series engines, and 20oC to the actual measured engine EGT on CFM56-7B/2 series engines to provide an indicated EGT level. This EGT shunt is triggered above 8,500 RPM core speed for all CFM56 series engines. For E series only, there is a 20oC profile EGT shunt (cooler) in addition to the present +30oC or +10oC (E/F series) shunt. This profile shunt (-20oC) will be active above 10400 rpm Physical Core speed (N2) and –10oC Shunt at ground idle conditions. This profile shunt will be active for all flight conditions. ** The EGT trim function adds the values noted above to the indicated EGT levels. This EGT trim is only triggered at mach numbers from 0 to 0.40 and when the core speed is greater than 11,200 RPM. This function is only applicable for the engine models indicated. NOTE 14 (b). The indicated maximum permissible maximum continuous EGT is 925oC. The same trims and shunts described in Note 14(a) for takeoff EGT are applicable to maximum continuous EGT. NOTE 14 (c). All CFM56-7B engines are certified with an indicated maximum permissible takeoff EGT transient allowance of 960oC for 20 seconds. This equates to a 10oC increase above the maximum permissible indicated value of 950oC. NOTE 15. The CFM56-7B27A, CFM56-7B27A/3 and CFM56-7B27AE variants are designed for military application only. The engine serial number of these variants includes 654, 655, 362 or 363 depending on final assembly location. FAA certified engines used in military service are not necessarily operated or maintained in accordance with FAA regulations. Commercial service uses of the CFM56-7B27A, CFM56-7B27A/3 or CFM56-7B27AE variants, and the installation of used CFM56-7B27A, CFM57-7B27A/3 and CFM56-7B27AE parts in another CFM56-7B variant, are subject to prior approval of the FAA (Engine Certification Office, ANE-140). . Note deleted. NOTE 16. NOTE 17. Criteria pertaining to the dispatch and maintenance requirements for the engine control systems are specified in the airworthiness limitation section of the CFM56-7B Engine Shop Manual (CFM-TP.SM.10), which defines the various configurations and maximum operating intervals. NOTE 18. The actual maximum permissible oil temperature for starting and idle conditions is 10oC higher for continuous operation and 5oC higher for transient operation than the corresponding indicated oil temperatures. An indicated oil temperature for continuous operation of 140oC (284oF) corresponds to an actual oil temperature of 150oC (302oF). An indicated oil temperature for transient operation of 155oC (311oF) corresponds to an actual oil temperature of 160oC (320oF). E00056EN 24 of 25 NOTE 19. CFM56-7B series includes: CFM56-7B20, -7B22, -7B22/B1, -7B24, -7B24/B1, -7B26, 7B26/B2, -7B27, -7B27A, -7B26/B1, -7B27/B1 and -7B27/B3 CFM56-7B/2 series includes: CFM56-7B20/2, -7B22/2, -7B24/2, -7B26/2, and -7B27/2 CFM56-7B/3 series includes: CFM56-7B20/3, -7B22/3, -7B22/3B1, -7B22/3B2, -7B24/3, 7B24/3B1, -7B26/3, -7B26/3B1, -7B26/3B2, -7B27/3, -7B27/3B1, -7B27/3B3, and –7B27A/3 CFM56-7B/3F series includes: CFM56-7B26/3F, -7B26/3B2F, -7B27/3F, and -7B27/3B1F. CFM56-7BE series includes: CFM56-7B20E, -7B22E, -7B22E/B1, -7B22E/B2, -7B24E, 7B24E/B1, -7B26E, -7B26E/B1, -7B26E/B2, -7B27E, -7B27E/B1, and -7B27E/B3 CFM56-7BE/F series includes: CFM56-7B26E/F, -7B26E/B2F, -7B27E/F, and -7B27E/B1F. NOTE 20. The models shown on this TCDS have the following general characteristics: MODEL CHARACTERISTICS CFM56-7B18 Base model. (No longer available) CFM56-7B20 Same as CFM56-7B18 except for increased thrust ratings. CFM56-7B22 Same as CFM56-7B18 except for increased thrust ratings. CFM56-7B24 Same as CFM56-7B18 except for increased thrust ratings. CFM56-7B26 Same as CFM56-7B18 except for increased thrust ratings. CFM56-7B27 Same as CFM56-7B18 except for increased thrust ratings. CFM56-7B20/2 Same as CFM56-7B20 except CFM56-7B20/2 has a double annular combustor. CFM56-7B22/2 Same as CFM56-7B22 except CFM56-7B22/2 has a double annular combustor. CFM56-7B24/2 Same as CFM56-7B24 except CFM56-7B24/2 has a double annular combustor. CFM56-7B26/2 Same as CFM56-7B26 except CFM56-7B26/2 has a double annular combustor. CFM56-7B27/2 Same as CFM56-7B27 except CFM56-7B27/2 has a double annular combustor. CFM56-7B27/B1 Same as CFM56-7B27 except CFM56-7B27/B1 has optimized power management at takeoff. CFM56-7B26/B1 Same as CFM56-7B26 except CFM56-7B26/B1 is intended for a business jet application (different mission). CFM56-7B27/B3 Same as CFM56-7B27 except CFM56-7B27/B3 is intended for a business jet application (different mission). CFM56-7B22/B1 Same as CFM56-7B22 except CFM56-7B22/B1 has an extended flat rated temperature for takeoff. CFM56-7B24/B1 Same as CFM56-7B24 except CFM56-7B24/B1 has an extended flat rated temperature for takeoff. CFM56-7B27A Same as CFM56-7B27, except CFM56-7B27A has increased capability for gearbox power extraction. CFM56-7B26/B2 Same as CFM56-7B26, except CFM56-7B26/B2 has an extended high altitude and temperature rating above corner point takeoff. CFM56-7B20/3 Same as CFM56-7B20 except forlow emissions combustor and redesigned compressor and HPT rotor. CFM56-7B22/3 Same as CFM56-7B20 except for increased thrust, low emissions combustor and redesigned compressor and HPT rotor. CFM56-7B24/3 Same as CFM56-7B20 except for increased thrust, low emissions combustor and redesigned compressor and HPT rotor. CFM56-7B26/3 Same as CFM56-7B20 except for increased thrust, low emissions combustor and redesigned compressor and HPT rotor. CFM56-7B27/3 Same as CFM56-7B20xcept for increased thrust, low emissions combustor and redesigned compressor and HPT rotor. CFM56-7B22/3B1 Same as CFM56-7B22/B1 except for low emissions combustor and redesigned compressor and HPT rotor. CFM56-7B24/3B1 Same as CFM56-7B24/B1 except for low emissions combustor and redesigned compressor and HPT rotor. CFM56-7B26/3B1 Same as CFM56-7B26/B1 except for low emissions combustor and redesigned compressor and HPT rotor. CFM56-7B26/3B2 Same as CFM56-7B26/B2 except for low emissions combustor and redesigned compressor and HPT rotor. CFM56-7B27/3B1 Same as CFM56-7B27/B1 except for low emissions combustor and redesigned compressor and HPT rotor. CFM56-7B27/3B3 Same as CFM56-7B27/B3 except for low emissions combustor and redesigned compressor and HPT rotor. E00056EN 25 of 25 NOTE 20. Continued CFM56-7B26/3F CFM56-7B26/3B2F CFM56-7B27/3F CFM56-7B27/3B1F CFM56-7B27A/3 Same as CFM56-7B26/3 except for increased EGT limits Same as CFM56-7B26/3B2 except for increased EGT limits. Same as CFM56-7B27/3 except for increased EGT limits. Same as CFM56-7B27/3B3 except for increased EGT limits. Same as CFM56-7B27A except for low emissions combustor and redesigned compressor and HPT rotor. CFM56-7BE series The E models incorporate, with respect to /3 models, improved HPC diffuser, new HPT , new LPT and new exhaust diffuser (Boeing Part). CFM56-7BE/F series The E/F models incorporate, with respect to /3F models, improved HPC diffuser, new HPT , new LPT and new exhaust diffuser (Boeing Part). NOTE 21. 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. NOTE 22. All engine models are in compliance with the emissions requirements in 14 CFR Part 34, effective September 10, 1990, as amended by 34-1 through 34-4. NOTE 23 NOTE DELETED.