TCDS A21EA-1

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A21EA-1 Revision No. 7 MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100 & 440) CL-600-2C10 (Regional Jet Series 700, 701 & 702) CL-600-2C11 (Regional Jet Series 550) CL-600-2D15 (Regional Jet Series 705) CL-600-2D24 (Regional Jet Series 900) CL-600-2E25 (Regional Jet Series 1000) June 5, 2026 TYPE CERTIFICATE DATA SHEET NO. A21EA-1 This data sheet, which is part of Type Certificate No. A21EA-1 (originally certified under Type certificate No. A21EA), prescribes conditions and limitations under which the product for which the Type Certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder: MHI RJ Aviation ULC 3655 Av. des Grandes Tourelles, suite 110 Boisbriand, Québec, Canada J7H 0E2 Type Certificate Holder Record: Bombardier Inc. 800 boul. René Lévesque West Montreal, Quebec, Canada H3B1Y8 I - Model CL-600-2B19 (Regional Jet Series 100) (Transport Category), Approved January 21, 1993, by the FAA and July 31, 1992, by Transport Canada. (See Note 8) Model CL-600-2B19 (Regional Jet Series 440) (Transport Category), Approved November 30, 2001, by the FAA and October 4, 2001, by Transport Canada. Engines Two General Electric CF-34-3A1 or Two General Electric CF-34-3B1 Engines may be intermixed in accordance with AFM as listed in Approved Publications. Fuel Type Specifications Canada U.S.A. U.K. China CIS/Ukraine NATO Jet A CGSB-3.23 ASTM D1655 - - - - Jet A-1 CGSB-3.23 ASTM D1655 DEF STAN 91-91 GB6537-2006 No. 3 Jet TS-1* or RT F-35 Grade JP-5 CGSB-3.24 MIL-DTL- 5624 DEF STAN 91-86 - - F-44 Grade JP-8 CGSB-3.24 MIL-DTL- 83133 DEF STAN 91-87 - - F-34 Jet B CAN2-3.22 ASTM D6615 D. Eng. RD2486 - - - Grade JP-4 CAN2-3.22 MIL-DTL- 5624 D. Eng. RD2454 - - - *Refer to appropriate AFM listed in Appr oved Publication section when using TS-1. Oil Engine, APU and IDG: MIL-L-7808 (Type I) or MIL-L-23699 (Type II) or CASTROL 4000. * * Mixing of different types of oils is prohibited. Page 2 of 25 A21EA-1 Engine Limits Fan RPM Core RPM ITT Ti me Limit %N1 %N2 °C °F (Min) Max. takeoff (APR operating) 98.6 99.4 900 1650 5*** 928 1702 2* Normal takeoff 96.2 98.2 884 1623 5*** - 900 1650 2* Max. Continuous 98.6 99.2 860/874 (3A1/3B1) 1580/1605 (3A1/3B1) - Idle Ran ge - 56.5 to 68.0** - - - Accele ration - - 900 1652 - Startin g - 20.0 900 1652 - * 2 minutes out of 5 total transient. ** Refe r to Idle Speed Limit Chart in the AFM If N 2 idle RPM is more than 2% lower, do not advance thrust lever above 70% N 2 until N2 idle RPM has stabilized to within normal limits. *** T ransient limits. NOTE: Above 40000 feet, one air conditioning unit or cowl anti-ice must be selected on for each engine Oil Temperature °C °F Maxi mum Permissible (15 minutes Maximum) +163 325 Maxi mum Continuous +155 311 Mini mum for Starting -40 -40 Oil Pressure Maxi mum Transient (after cold start) 156 psi (130 psi at idle, 10 minutes maximum)* Maxi mum Continuous 115 psi maximum Take-off Powe r 45 psi minimum Stead y State Idle 25 psi minimum * Engine must remain at idle until oil pressure returns to normal range. APU GARRETT GTCP-36-150R J APU Limits Maximum RPM 107% Maximum EGT: °C °F Starting 974 1785* Running 743 1369 * Not to be exceeded under any operating condition. Airspeed Limits (CAS) V mo and Mmo (maximum operating) m.p.h. Knots Mach Sea Level to 8000 ft. 380 330 - 8000 ft. to 25400 ft. 386 335 - 25400 ft. to 28300 ft. - - 0.80 28300 ft. to 31400 ft. 362 315 - 31400 ft. to 41000 ft. - - 0.85 V fe (Flaps extended) 8° 265 230 - 20° 265 230 - 30° 226 196 - 45° 220 191 - V a (maneuvering) (See AFM for variation of V a with altitude and aircraft weight). V 1o (Landing Gear Operation) Extending 288 250 - Retracting 230 200 - V 1e (Landing Gear Extended) 288 250 - C.G. Range Refer to AFM (CSP A-012) for detail CG limits. Datum Fuselage station 0, located 375 inches forward of weighing datum jig point. Mean Aerodynamic Chord (MAC) 99.43 inches (MAC leading edge at fuselage sta. 494.793) Page 3 of 25 A21EA-1 Leveling Means Target plate and plumb bob bracket within rear fuselage, at fuselage station 718.75. Type Spec. Option Option Option Option Option Maximum Weights l b. lb. lb. lb. lb. lb. Ramp 47700 51250 51250 53250 53250 53250 Takeoff 47450 51000 51000 53000 53000 53000 Landing 44700 46750 47000 46750 47000 47000 Zero Fuel 42200 44000 44000 44000 44000 39500 Mini mum flight weight 30000 30000 30000 30000 30000 30000 NOTE: The maximum take-off weight and/or maximum landing weight may be further limited due to performance considerations (refer to Airplane Flight Manual). Minimum Crew Two (Pilot and Co-pilot) Maximum Occupants Series 100 - Fift y-five (55) (including 50 passengers, 4 crew, and 1 flight observer) Series 440 - Fort y-Nine (49) (including 44 passengers, 4 crew, and 1 flight observer) CL-600-2B19 Green Aircraft Configuration Refer to NOTE 4 & 5. Fuel Capacity (usable) Load* Weight* U.S. Gal. Imp. Gal. Kg. lb. 2 main tanks (each) 700.0 582.8 2159 4760 Cente r tank 735.0 612.0 2267 4998 Total 2135.0 1669.6 6585 14518 * P ressure refueling (based on 0.8028 kg/L) Oil Capacity Loa d Weight U.S. Gal. Imp. Gal. Kg. lb. 2 En gines (each) 1.70 1.42 5.94 13.09 Total 3.40 2.84 11.88 26.18 Usa ble 2 En gines (each) 1.38 1.14 4.80 10.59 Total 2.76 2.29 9.60 21.18 Maximum Operating Ta keoff and landing: 10000 ft. Altitude En route: 41000 ft. Control Surface R udder 33º Left* 33º Right Movements Elevato r 23.6º U p 18.4º Down Horizontal Sta bilizer 2º LE Up -13º LE Down Aile ron 25º U p 21.3º Down Fla p – Inboard 45.09º Down – Outboard 41.58º Down Fli ght Spoiler 50º U p G round Spoiler 45º Up S poileron 50º U p *Rudde r deflections of 33º left and 33º right apply when CF-34-3A1 engines are installed. *Rudde r deflections of 25º left and 25º right apply when optional CF-34-3B1 engines are installed. Serial Numbers Eligible 7001 an d subsequent Service Information Service Bulletins, structural repair manuals, and aircraft flight manuals which contain a statement that th e document is Transport Canada approved or Transport Canada approved through the Manufacturers Design Approval Representative are accepted by the FAA and are considered FAA approved. These approvals pertain to the type design only. For all weather flight capability, refer to Note 6. II - Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) (Transport Category), Approved February 16, 2001, by the FAA and December 22, 2000 by Transport Canada. Page 4 of 25 A21EA-1 Engines Two General Electric CF-34-8C1, or Two General Electric CF-34-8C5B1 Engines may be intermixed in accordance with AFM as listed in Approved publications Fuel T ype S pecifications Canada U.S.A. U.K. China CIS/Ukraine NATO Jet A CGSB-3.23 ASTM D1655 - - - - Jet A-1 CGSB-3.23 ASTM D1655 DEF STAN 91-91 GB6537-2006 No. 3 Jet TS-1* or RT F-35 Grade JP-5 CGSB-3.24 MIL-DTL- 5624 DEF STAN 91-86 - - F-44 Grade JP-8 CGSB-3.24 MIL-DTL- 83133 DEF STAN 91-87 - - F-34 *Refer to a ppropriate AFM listed in Approved Publication section when usin g TS-1. Oil Engine, APU and IDG: MIL-L-7808 (Type I) or MIL-L-23699 (Type II) or CASTROL 4000. * * Mixing of different types of oils is prohibited. Engine Limits Refe r to Limits Table in the AFM (CSP B-012) Oil Temperature °C °F Maxi mum Permissible (15 minutes Maximum) +163 325 Maxi mum Continuous +155 311 Mini mum for Starting -40 -40 Oil Pressure Maxi mum Transient (after cold start) 156 psi (130 psi at idle, 10 minutes maximum)* Maxi mum Continuous 45-116 psi Take-off Powe r 45-116 psi Stead y State Idle 25 psi minimum * Engine must remain at idle until oil pressure returns to normal operating range. APU ALLIED SIGNAL RE220 (RJ) APU Limits Maximum RPM 106% Maximum EGT: °C °F Starting 692-1038 1274-1900* Running - Ground 789 1452 Running - Flight 806 1482 * Dependent upon altitude and temperature. Refer to AFM (CSP B-012) ** Not to be exceeded under any operating condition. *** Refer to AFM for detail limitations Airspeed Limits (CAS) V mo and Mmo (maximum operating) m.p.h. Knots Mach Sea Level to 8000 ft. 380 330 - 8000 ft. to 25400 ft. 386 335 - 25400 ft. to 28300 ft. - - 0.80 28300 ft. to 31400 ft. 362 315 - 31400 ft. to 41000 ft. - - 0.85 V fe (Flaps extended) 1° 265 230 - 8° 265 230 - 20° 265 230 - 30° 213 185 - 45° 196 170 - V a (maneuvering) (See AFM for variation of V a with altitude and aircraft weight). V 1o (Landing Gear Operation) Extending 253 220 - Retracting 230 200 - V 1e (Landing Gear Extended) 253 220 - Page 5 of 25 A21EA-1 C.G. Range Refer to AFM (CSP B-012) for detail CG limits. Datum Fuselage station 0, located 144.0 inches forward of aircraft nose. Mean Aerodynamic Chord (MAC) 133.185 inches (MAC leading edge at fuselage sta. 743.1) Leveling Means Target plate and plumb bob bracket within rear fuselage, at fuselage station 1145.75 Maximum Weights Type Spec. Option l b. lb. Ram p 73000 75250 Takeoff 72750 75000 Landin g 67000 67000 Zero Fuel 62300 62300 Mini mum flight weight 42000 42000 NOTE: The maximum take-off weight and/or maximum landing weight may be further limited due to performance considerations. Refer to Airplane Flight Manual for aircraft eligibility. Minimum Crew Two (Pilot and Co-pilot) Maximum Occupants** Series 700 – 68 or less passengers Series 701 – 70 passengers Series 702 – 78 passengers Plus 5 crew-members (Pilot, Copilot, Obse rver forward and Aft Flight attendants) ** For any CL-600-2C10, the maximum passenger capacity may be further limited by the Equivalent Safety Finding against FAR 25.801 and 25.813 (see Note 13). Fuel Capacity (usable) Load* Weight* U.S. Gal. Imp. Gal. Kg. lb. 2 main tanks (each) 1110 924.1 3399 7493 Cente r tank 683 568.6 2091 4610 Total 2903 2416.7 8889 19596 See Note 1 (b) for system fuel * P ressure refueling (based on 0.809 kg/L) (6.75 lb./U.S. Gal.) Oil Capacity With option TS670-79-201 – Engine Oil – No Remote Replenishment System Loa d Weight U.S. Gal. Imp. Gal. Kg. lb. 2 En gines (each) 2.6 2.2 9.65 21.2 Total 5.2 4.36 19.30 42.4 See Note 1 (c) for system oil With option CR670-79-201 – Engine Oil – Remote Replenishment System Loa d Weight U.S. Gal. Imp. Gal. Kg. lb. 2 En gines (each) 2.6 2.2 9.65 21.2 Re plenishment Tank 1.6 1.3 5.9 13.0 Total 6.8 5.7 25.2 55.4 See Note 1(c) fo r system oil Maximum Operating Ta keoff and landing: 8000ft (without Modsum 670T82357) Altitude 9600ft (with Modsum 670T82357) En route: 41000 ft. Control Surface R udder 33º Left* 33º Right Movements Elevato r 23.6º U p 18.4º Down Horizontal Sta bilizer 2.0º LE Up 13.0º LE Down Aile ron 25.1º U p 21.3º Down Fla p – Inboard 45.0º Down – Outboard 41.6º Down Multi-Function Spoiler 48.0º Up Page 6 of 25 A21EA-1 G round Spoiler 44.9º U p Slat 25.0º Down Serial Numbers Eligible 10002 an d subsequent Service Information Service Bulletins, structural repair manuals, and aircraft flight manuals which contain a statement that th e document is Transport Canada approved or Transport Canada approved through the Manufacturers Design Approval Representative are accepted by the FAA and are considered FAA approved. These approvals pertain to the type design only. For all weather flight capability, refer to Note 6. III - Model CL-600-2C11 (Regional Jet Series 550) (Transport Category), Approved September 18, 2019, by the FAA and July 5, 2019 byTransport Canada. (See NOTE 16) Engines Two General Electric CF-34-8C1, or Two General Electric CF-34-8C5B1 Engines may be intermixed in accordance with AFM as listed in Approved publications Fuel Type Specifications Canada U.S.A. U.K. China CIS/Ukraine NATO Jet A CGSB-3.23 ASTM D1655 - - - - Jet A-1 CGSB-3.23 ASTM D1655 DEF STAN 91-91 GB6537-2006 No. 3 Jet TS-1* or RT F-35 Grade JP-5 CGSB-3.24 MIL-DTL- 5624 DEF STAN 91-86 - - F-44 Grade JP-8 CGSB-3.24 MIL-DTL- 83133 DEF STAN 91-87 - - F-34 *Refer to appropriate AFM listed in Appr oved Publication section when using TS-1. Oil Engine, APU and IDG: MIL-L-7808 (Type I) or MIL-L-23699 (Type II) or CASTROL 4000. * * Mixing of different types of oils is prohibited. Engine Limits Refe r to Limits Table in the AFM (CSP B-012) Oil Temperature °C °F Maxi mum Permissible (15 minutes Maximum) +163 325 Maxi mum Continuous +155 311 Mini mum for Starting -40 -40 Oil Pressure Maxi mum Transient (after cold start) 156 psi (130 psi at idle, 10 minutes maximum)* Maxi mum Continuous 45-116 psi Take-off Powe r 45-116 psi Steady State Idle 25 psi minimum * En gine must remain at idle until oil pressure returns to normal operating range. APU ALLIED SIGNAL RE220 (RJ) APU Limits Maximum RPM 106% Maximum EGT: °C °F Starting 692-1038 1274-1900* Running - Ground 789 1452 Running - Flight 806 1482 * Dependent upon altitude and temperature. Refer to AFM (CSP B-012) ** Not to be exceeded under any operating condition. *** Refer to AFM for detail limitations Airspeed Limits (CAS) V mo and Mmo (maximum operating) m.p.h. Knots Mach Sea Level to 8000 ft. 380 330 - 8000 ft. to 25400 ft. 386 335 - 25400 ft. to 28300 ft. - - 0.80 28300 ft. to 31400 ft. 362 315 - 31400 ft. to 41000 ft. - - 0.85 Page 7 of 25 A21EA-1 V fe (Flaps extended) 1° 265 230 - 8° 265 230 - 20° 265 230 - 30° 213 185 - 45° 196 170 - V a (maneuvering) (See AFM for variation of V a with altitude and aircraft weight). V 1o (Landing Gear Operation) Extending 253 220 - Retracting 230 200 - V 1e (Landing Gear Extended) 253 220 - C.G. Range Refer to AFM (CSP B-012) for detail CG limits. Datum Fuselage station 0, located 144.0 inches forward of aircraft nose. Mean Aerodynamic Chord (MAC) 133.185 inches (MAC leading edge at fuselage sta. 743.1) Leveling Means Target plate and plumb bob bracket within rear fuselage, at fuselage station 1145.75 Maximum Weights Type Spec. Option l b. lb. Ramp 66000 66000 Takeoff 65000 65000 Landing 61000 64000 Zero Fuel 59000 59000 Mini mum flight weight 42000 42000 NOTE: The maximum take-off weight and/or maximum landing weight may be further limited due to performance considerations. Refer to Airplane Flight Manual for aircraft eligibility. Minimum Crew Two (Pilot and Co-pilot) Maximum Occupants 50 or less passengers, when fitted with an a pproved interior Plus 5 crew-members (Pilot, Copilot, Obse rver, Forward and Aft Flight attendants) Fuel Capacity (usable) Load* Weight* U.S. Gal. Imp. Gal. Kg. lb. 2 main tanks (each) 1110 924.1 3399 7493 Cente r tank 683 568.6 2091 4610 Total 2903 2416.7 8889 19596 See Note 1 (b) for system fuel * P ressure refueling (based on 0.809 kg/L) (6.75 lb./U.S. Gal.) Oil Capacity With option TS670-79-201 – Engine Oil – No Remote Replenishment System Loa d Weight U.S. Gal. Imp. Gal. Kg. lb. 2 En gines (each) 2.6 2.2 9.65 21.2 Total 5.2 4.36 19.30 42.4 See Note 1 (c) for system oil With option CR670-79-201 – Engine Oil – Remote Replenishment System Loa d Weight U.S. Gal. Imp. Gal. Kg. lb. 2 Engines (each) 2.6 2.2 9.65 21.2 Re plenishment Tank 1.6 1.3 5.9 13.0 Total 6.8 5.7 25.2 55.4 See Note 1 (c) for system oil Maximum Operating Ta keoff and landing: 8000ft (without Modsum 670T82357) Altitude 9600ft (with Modsum 670T82357) En route: 41000 ft. Page 8 of 25 A21EA-1 Control Surface R udder 33º Left* 33º Right Movements Elevato r 23.6º U p 18.4º Down Horizontal Sta bilizer 2.0º LE Up 13.0º LE Down Aile ron 25.1º U p 21.3º Down Fla p – Inboard 45.0º Down – Outboard 41.6º Down Multi-Function Spoiler 48.0º Up G round Spoiler 44.9º Up Slat 25.0º Down Serial Numbers Eligible 10002 an d subsequent Service Information Service Bulletins, structural repair manuals, and aircraft flight manuals which contain a statement that th e document is Transport Canada approved or Transport Canada approved through the Manufacturers Design Approval Representative are accepted by the FAA and are considered FAA approved. These approvals pertain to the type design only. For all weather flight capability, refer to Note 6. IV – Model CL-600-2D15 (Regional Jet Series 705) (Transport Category), Approved May 4, 2005, by the FAA and May 3, 2005 by Transport Canada. Engines Two General Electric CF34-8C5 or optional CF34-8C5A1 TC No. E00063EN Fuel Type Specifications Canada U.S.A. U.K. China CIS/Ukraine NATO Jet A CGSB-3.23 ASTM D1655 - - - - Jet A-1 CGSB-3.23 ASTM D1655 DEF STAN 91-91 GB6537-2006 No. 3 Jet TS-1* or RT F-35 Grade JP-5 CGSB-3.24 MIL-DTL- 5624 DEF STAN 91-86 - - F-44 Grade JP-8 CGSB-3.24 MIL-DTL- 83133 DEF STAN 91-87 - - F-34 *Refer to appropriate AFM listed in Appr oved Publication section when using TS-1. Oil Engine, APU and IDG: MIL-L-7808 (Type I) or MIL-L-23699 (Type II) or CASTROL 4000. * * Mixing of different types of oils is prohibited. Engine Limits Refe r to Limits Table in the AFM (CSP C-012) Oil Temperature °C °F Maxi mum Permissible (15 minutes Maximum) +163 325 Maxi mum Continuous +155 311 Mini mum for Starting -40 -40 Oil Pressure Maxi mum Transient (after cold start) 182 psi (95 psi after 10 minutes) Maxi mum Continuous 45-95 psi Take-off Powe r 45-95 psi Steady State Idle 25 psi minimum * En gine must remain at idle until oil pressure returns to normal operating range. APU ALLIED SIGNAL RE220 (RJ) Page 9 of 25 A21EA-1 APU Limits Maximum RPM 106% Maximum EGT: °C °F Starting 692-1038 1274-1900* Running - Ground 789 1452 Running - Flight 806 1482 * Dependent upon altitude and temperature. Refer to AFM (CSP C-012) ** Not to be exceeded under any operating condition. *** Refer to AFM for detail limitations Airspeed Limits (CAS) V mo and Mmo (maximum operating) m.p.h. Knots Mach Sea Level to 8000 ft. 380 330 - 8000 ft. to 25400 ft. 386 335 - 25400 ft. to 28300 ft. - - 0.80 28300 ft. to 31400 ft. 362 315 - 31400 ft. to 34000 ft. - - 0.85 34000 ft. to 41000 ft. - - 0.84 V fe (Flaps extended) 1° 265 230 - 8° 265 230 - 20° 253 220 - 30° 213 185 - 45° 196 170 - V a (maneuvering) (See AFM for variation of V a with altitude and aircraft weight). V 1o (Landing Gear Operation) Extending 253 220 - Retracting 230 200 - V 1e (Landing Gear Extended) 253 220 - C.G. Range Refer to AFM (CSP C-012) for detail CG limits. Datum Fuselage station 0, located 144.0 inches forward of aircraft nose. Mean Aerodynamic Chord (MAC) 133.185 inches (MAC leading edge at fuselage sta. 833.1 inches) Leveling Means Target plate and plumb bob bracket within rear fuselage, at fuselage station 1146.75 Maximum Weights Type Spec. Option Option l b. lb. lb. Ramp 80750 82750 85000 Takeoff 80500 82500 84500 Landing 73500 73500 75100 Zero Fuel 70000 70000 70750 Mini mum flight weight 45000 45000 45000 NOTE: The maximum take-off weight and/or maximum landing weight may be further limited due to performance considerations. Refer to Airplane Flight Manual for aircraft eligibility. Minimum Crew Two (Pilot an d Co-pilot) Maximum Occupants 75 or less passengers Plus 5 crew-members (Pilot, Copilot, Observer, Forward and Aft Flight attendants) Fuel Capacity (usable) Load* Weight* U.S. Gal. Imp. Gal. Kg. lb. 2 main tanks (each) 1110 924.1 3398 7492 Cente r tank 683 568.6 2091 4610 Total 2903 2416.7 8888 19595 See Note 1( b) for system fuel * P ressure refueling (based on 0.809 kg/L) (6.75 lb./U.S. Gal.) Page 10 of 25 A21EA-1 Oil Capacity With option TS670-79-201 – Engine Oil – No Remote Replenishment System Loa d Weight U.S. Gal. Imp. Gal. Kg. lb. 2 Engines (each) 2.6 2.2 9.65 21.2 Total 5.2 4.36 19.3 42.4 See Note 1(c) fo r system oil With option CR670-79-201 – Engine Oil – Remote Replenishment System Loa d Weight U.S. Gal. Imp. Gal. Kg. lb. 2 En gines (each) 2.6 2.2 9.65 21.2 Re plenishment Tank 1.6 1.3 5.9 13.0 Total 6.8 5.7 25.2 55.4 See Note 1 (c) for system oil Maximum Operating Ta keoff and landing: 8000ft (without Modsum 670T82357) Altitude 9600ft (with Modsum 670T82357) En route: 41000 ft. Control Surface R udder 33º Left 33º Ri ght Movements Elevato r 23.6º Up 18.4º Down Horizontal Sta bilizer 2.0º LE U p 13º LE Down Aile ron 25.1º Up 21.3º Down Fla p – Inboard 45.0 º Down – Outboard 41.6º Down Multi-Function S poiler 48.0º U p G round Spoiler 44.9º Up Slat 25.0º Down Serial Numbers Eligible 15001 an d subsequent Service Information Service Bulletins, structural repair manuals, and aircraft flight manuals which contain a statement that th e document is Transport Canada approved or Transport Canada approved through the Manufacturers Design Approval Representative are accepted by the FAA and are considered FAA approved. These approvals pertain to the type design only. For all weather flight capability, refer to Note 6. V – Model CL-600-2D24 (Regional Jet Series 900) (Transport Category), Approved October 25,-2002, by the FAA and September 9, 2002 by Transport Canada. Engines Two General Electric CF34-8C5 or optional CF34-8C5A1 TC No. E00063EN Fuel T ype S pecifications Canada U.S.A. U.K. China CIS/Ukraine NATO Jet A CGSB-3.23 ASTM D1655 - - - - Jet A-1 CGSB-3.23 ASTM D1655 DEF STAN 91-91 GB6537-2006 No. 3 Jet TS-1* or RT F-35 Grade JP-5 CGSB-3.24 MIL-DTL- 5624 DEF STAN 91-86 - - F-44 Grade JP-8 CGSB-3.24 MIL-DTL- 83133 DEF STAN 91-87 - - F-34 *Refer to a ppropriate AFM listed in Approved Publication section when usin g TS-1. Oil Engine, APU and IDG: MIL-L-7808 (Type I) or MIL-L-23699 (Type II) or CASTROL 4000. * * Mixing of different types of oils is prohibited. Engine Limits Refe r to Limits Table in the AFM (CSP C-012) Page 11 of 25 A21EA-1 Oil Temperature °C °F Maxi mum Permissible (15 minutes Maximum) +163 325 Maxi mum Continuous +155 311 Mini mum for Starting -40 -40 Oil Pressure Maxi mum Transient (after cold start) 182 psi (95 psi after 10 minutes) Maxi mum Continuous 45-95 psi Take-off Powe r 45-95 psi Stead y State Idle 25 psi minimum * Engine must remain at idle until oil pressure returns to normal operating range. APU ALLIED SIGNAL RE220 (RJ) APU Limits Maximum RPM 106% Maximum EGT: °C °F Starting 692-1038 1274-1900 Running – Ground* 789 1452 Running – Flight* 806 1482 * Dependent upon altitude and temperature. Refer to AFM (CSP C-012) ** Not to be exceeded under any operating condition. *** Refer to AFM for detail limitations Airspeed Limits (CAS) V mo and Mmo (maximum operating) m.p.h. Knots Mach Sea Level to 8000 ft. 380 330 - 8000 ft. to 25400 ft. 386 335 - 25400 ft. to 28300 ft. - - 0.80 28300 ft. to 31400 ft. 362 315 - 31400 ft. to 34000 ft. - - 0.85 34000 ft. to 41000 ft. - - 0.85 34000 ft. to 41000 ft. - - 0.84* V fe (Flaps extended) 1° 265 230 - 8° 265 230 - 20° 253 220 - 30° 213 185 - 45° 196 170 - V a (maneuvering) (See AFM for variation of V a with altitude and aircraft weight). *with the incorporation of M/S 690T002727 – Introduction of new winglet V 1o (Landing Gear Operation) Extending 253 220 - Retracting 230 200 - V 1e (Landing Gear Extended) 253 220 - C.G. Range Refer to AFM (CSP C-012) for detail CG limits. Datum Fuselage station 0, located 144.0 inches forward of aircraft nose. Mean Aerodynamic Chord (MAC) 133.185 inches (MAC leading edge at fuselage sta. 833.1 inches) Leveling Means Target plate and plumb bob bracket within rear fuselage, at fuselage station 1146.75 Page 12 of 25 A21EA-1 Maximum Weights T ype Spec. O ption O ption