# TCDS A21EA-1: MHI RJ Aviation ULC - Type: Type certificate data sheet - Status: Current - Holder: MHI RJ Aviation ULC - Revision: 7 - Revised: June 5, 2026 - Product: Aircraft, Large Airplane - Certification basis: Part 25 - Registered aircraft: 1,030, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/b3/95/b395700654590f76e444ae695c0bf9c618063d8a88e29f3b5a23d983fb536e2e - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174291983820260605211445.0001 - Page: https://openairdocs.org/tcds/A21EA-1 ## Models (9) As the data sheet lists them. - CL-600-2D15 (Regional Jet Series 705) - CL-600-2E25 (Regional Jet Series 1000) - CL-600-2C10 (Regional Jet Series 702) - CL-600-2B19 (Regional Jet Series 440) - CL-600-2C10 (Regional Jet Series 701) - CL-600-2B19 (Regional Jet Series 100) - CL-600-2C10 (Regional Jet Series 700) - CL-600-2D24 (Regional Jet Series 900) - CL-600-2C11 (Regional Jet Series 550) ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text 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 l b. lb. lb. Ram p 80750 82750 85000 Takeoff 80500 82500 84500 Landin g 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 and Co-pilot) Maximum Occupants** 90 or less passengers Plus 5 crew-members (Pilot, Copilot, Ob server, Forward and Aft Flight attendants) **For any CL-600-2D24, the maximum passenge r capacity may be further limited (see Note 19). 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.) 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 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. Control Surface R udder 33º Left 33º Ri ght Movements Elevato r 23.6º U p 18.4º Down Horizontal Sta bilizer 2.0º LE Up 13º LE Down Aile ron 25.1º U p 21.3º Down Fla p – Inboard 45.0 º Down – Outboard 41.6º Down Multi-Function S poiler 48.0º Up G round Spoiler 44.9º U p 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. VII – Model CL-600-2E25 (Regional Jet Series 1000) (Transport Category), Approved D ecember 17, 2010 by the FAA and November 1, 2010 by Transport Canada. Page 13 of 25 A21EA-1 Engines Two General Electric CF34-8C5 or optional CF34-8C5A1 optional CF34-8C5A2 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 GB6537-94 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 D-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 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 D-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. - - 0.84 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) Page 14 of 25 A21EA-1 Extending 253 220 - Retracting 230 200 - V 1e (Landing Gear Extended) 253 220 - C.G. Range Refer to AFM (CSP D-012) for detail CG limits. Datum Xarm 0, located 144.0 inches forward of aircraft nose Mean Aerodynamic Chord (MAC) 137.020 inches (MAC leading edge at Xarm 900.257 inches) Leveling Means Target plate and plumb bob bracket within rear fuselage, at fuselage station 1146.75 Maximum Weights T ype Spec. O ption O ption O ption O ption l b. lb. lb. lb. lb. Ram p 90500 92300 88673 90878 86469 Takeoff 90000 91800 88173 90378 85969 Landin g 81500 Zero Fuel 77500 Mini mum flight weight 51000 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 110, including 6 crew members (1 Pilot, 1 Co-pilot, 1 observer and 3 Flight Attendants) (104 passengers when fitted with an approved interior) Fuel Capacity (usable) Load* Weight* U.S. Gal. Imp. Gal. Kg. lb. 2 main tanks (each) 1113 926.8 3407 7513 Cente r tank 710 591.2 2174 4793 Total 2936 2444.7 8989 19818 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 19.3 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: 10000 ft. Altitude 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 13.0º LE Down Aile ron 24.1º Up 20.3º Down Fla p – Inboard 45.0 º Down – Outboard 34.0º Down Multi-Function S poiler 48.0º U p Page 15 of 25 A21EA-1 G round Spoiler 44.0º U p Slat 25.0º Down Serial Numbers Eligible 19013 an d subsequent (see NOTE 11) 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. Data Pertinent to all Models Approved Publications Model CL-600-2B19 (a) Airplane Flight Manual, Canadair Publ ication CSP A-012 for the appropriate weight configuration and approved revisions. (b) Maintenance Review Board (MRB) Report and subsequent revisions as contained in the Maintenance Requirements Manual (MRM), Ca nadair Publication CSP A-053, Part 2 and subsequent approved revisions. (c) Structural Repair Manual (SRM), Canadair Publication CSP A-008 and subsequent approved issues. (d) Certification Maintenance Tasks, Canada ir Regional Jet, Model CL-600-2B19 Engineering Report No. RBR-601R-167, as contained in Part 2 to the Maintenance Requirements Manual (MRM), Canadair Publication CSP A-053, and subse quent approved revisions. Model CL-600-2C10 (a) Airplane Flight Manual, Canadair Publ ication CSP B-012 for the appropriate weight configuration and approved revisions. (b) Maintenance Review Board (MRB) Report and subsequent revisions as contained in the Maintenance Requirements Manual (MRM), Cana dair Publication CSP B-053, Part I and subsequent approved revisions. (c) Structural Repair Manual (SRM), Canadair Publication CSP B-008 an d subsequent approved issues. (d) Airworthiness Limitations and Certification Maintenance Tasks, as contained in the Maintenance Requirements Manual (MRM), Cana dair Publication CSP B-053, Part II and subsequent approved revisions. Model CL-600-2C11 (a) Airplane Flight Manual, Ca nadair Publication CSP B-012, revision 28 dated September 18, 2019 or later approved revisions for the appropr iate weight configuration and approved revisions. (b) Maintenance Review Board (MRB) Report and subsequent revisions as contained in the Maintenance Requirements Manual (MRM), Canada ir Publication CSP B-053, Part I, revision 21 dated July 25, 2019 and subsequent approved revisions. (c) Structural Repair Manual (SRM), Canadair Publication CSP B-008, revision 37 dated August 15, 2019 and subsequent approved revisions. (d) Airworthiness Limitations and Certification Maintenance Tasks, as contained in the Maintenance Requirements Manual (MRM), Canadair Publication CSP B-053, Part II, revision 21 dated July 25, 2019 and subsequent approved revisions. Model CL-600-2D15/CL-600-2D24 (a) Airplane Flight Manual, Canadair Publication CSP C-012 for the appropriate weight configuration and approved revisions. (b) Maintenance Review Board (MRB) Report and subsequent revisions as contained in the Maintenance Requirements Manual (MRM), Canadair Publication CSP B-053, Part I and subsequent approved revisions. (c) Structural Repair Manual (SRM), Canadair Publication CSP B-008 and subsequent approved issues. (d) Airworthiness Limitations and Certification Maintenance Tasks, as contained in the Maintenance Requirements Manual (MRM), Cana dair Publication CSP B-053, Part II and subsequent approved revisions. Page 16 of 25 A21EA-1 Model CL-600-2E25 (a) Airplane Flight Manual, Canadair Publ ication CSP D-012 for the appropriate weight configuration and approved revisions. (b) Maintenance Review Board (MRB) Report and subsequent revisions as contained in the Maintenance Requirements Manual (MRM), Cana dair Publication CSP B-053, Part I and subsequent approved revisions. (c) Structural Repair Manual (SRM), Canadair Publication CSP D-008 and subsequent approved issues. (d) Airworthiness Limitations and Certification Maintenance Tasks, as contained in the Maintenance Requirements Manual (MRM), Cana dair Publication CSP B-053, Part II and subsequent approved revisions. Import Eligibility Refer to the applicable bilateral agreement to verify eligibility for import into the United States of both new and used aircraft based on the scope of the ag reement, to identify any required statements by the exporting authority on the export certificate of ai rworthiness (or equivalent document), and for procedures for coordinating exceptions to conformity statements on these documents. Refer to FAA Order 8130.2, Airworthiness Certification of Aircraft , for requirements for issuance of an airworthiness certificate for imported aircraft. A U.S. Airworthiness Certificate may be issued on the basis of the Canadian Department of Transport "Certificate of Airworthiness for Export" signed by the Minister of Transport. This form must contain the following statement: (a) Model CL-600-2B19 "This certifies that the aircraft described below has been manufactured in conformity with data forming the basis for the Transport Canada Type Approval No. A-276 and includes the minimum type design defined in document RAZ-601R-111 as being required to comply with the basis for the FAA Type Certificate No. A21EA-1". The approved type design appropriate to the "as delivered" configurati on of a particular CL- 600-2B19 airplane is defined in the document RAL-601R-XXXX. (XXXX represents the Serial Number for the air plane concerned). Model CL-600-2B19 Green Configuration For CL-600-2B19 Green Configuration and asso ciated modifications refer to NOTE 4. ( b) Model CL-600-2C10/CL-600-2C11 "This certifies that the aircraft described below has been manufactured in conformity with data forming the basis for the Transport Canada Type Approval No. A-276 and includes the minimum type design defined in document RAL-670-0001 and RAL-670-0002 as being required to comply with the basis for the FAA Type Certificate No. A21EA-1" The approved type design appropriate to the "a s delivered" configurati on of a particular CL- 600-2C10/CL-600-2C11 airplane is defined in the document RAL-670-XXXX for S/N 10002 to 10132 and RAL-BA670-XXXX for S/N 10133 and subsequent. (XXXX represents the Serial Number for the airplane concerned). (c) Model CL-600-2D15/CL-600-2D24 "This certifies that the aircraft described below has been manufactured in conformity with data forming the basis for the Transport Canada Type Approval No. A-276 and includes the minimum type design defined in document RAZ- BA690-129 as being required to comply with the basis for the FAA Type Certificate No. A21EA-1". The approved type design appropriate to the "as delivered" configurati on of a particular CL- 600-2D15/CL-600-2D24 airplane is defined in the document RAL-690-XXXX for S/N 15001 to 15013 and RAL-BA690-XXXX for S/N 15014 and subsequent. (XXXX represents the Serial Number for the airplane concerned). (d) Model CL-600-2E25 "This certifies that the aircraft described below has been manufactured in conformity with data forming the basis for the Transport Canada Type Approval No. A-276 and includes the minimum type design defined in document RAZ- BA698-009 as being required to comply with the basis for the FAA Type Certificate No. A21EA-1". Page 17 of 25 A21EA-1 The approved type design appropriate to the "a s delivered" configurati on of a particular CL- 600-2E25 airplane is defined in the document RAL-BA698-19XXX. (19XXX represents the Serial Number for the air plane concerned). Certification Basis Model CL-600-2B19 14 CFR Part 25 dated February 1, 1965, including Amendments 25-1 through 25-62 with the following exceptions; 14 CFR 25.109 at Amendment 25-41, 14 CFR 25.832 not included, 14 CFR 25.1401 at Amendment 25-40, 14 CFR 25.1438 not included and 14 CFR 25.783(f) at Amendment 25-23 for the ca rgo compartment door, the main avionics compartment door and the service/emergency door. 14 CFR 25.773(b)(2) and 25.785(h) at Amendment 25-72. Model CL-600-2C10/CL-600-2C11 14 CFR Part 25 dated February 1, 1965, including Amendments 25-1 through 25-86 with the following exceptions; 14 CFR 25.783(f) at Amendment 25-23 for the ca rgo compartment door, the main avionics compartment door and the service/emergency door. 14 CFR 25.571 at Amendment 25-96 14 CFR 25.493 at Amendment 25-97 Model CL-600-2D15/CL-600-2D24 14 CFR Part 25, including Amendments 25- 1 through 25-86, Amendments 25-88 through Amendments 25-90, and Amendments 25-92 th rough 25-98 with the following exceptions: (a) 14 CFR 25.783(f) at Amendment 25-23 shall replace 14 CFR 25.783(f) at Amendment 25-88 for the Aft Cargo Compartment and Main Avionics Bay Doors only (common doors with CL- 600-2C10 (CRJ700); (b) 14 CFR 25.807(d)(6) at Amendment 25-72 shall replace 14 CFR 25. 807(h) at Amendment 25- 94; (c) 14 CFR 25.365, 14 CFR 25.831(a) and 14 CFR 25.1447(c) at Amendment 25-87. 14 CFR 25 Amendment 25-91 is not includ ed in Type Certification Basis. Model CL-600-2E25 14 CFR Part 25 including amendments 25-1 th rough 25-119 with the following exceptions: 14 CFR Part 25.415 (rudder system only) at Amdt. 25-72; 14 CFR Parts 25.772(c) (not applicable);, 14 CFR Part 25.783(f) at Amdt. 25-23; 14 CFR Part 25.809 at Amdt. 25-72; 14 CFR Part 25.831(g) at Amdt. 25-41; 14 CFR Part 25.841(a) at Amdt. 25-38; 14 CFR Part 25.1329 at Amdt 25-46; 14 CFR Part 25.1335 at Amdt 25-41; and 14 CFR Part 26.33 in lieu of 14 CFR Part 25.981(c) at Amdt 25-102; Plus the following requirements: 14 CFR Part 25, Appendix J at Amdt. 25-117; 14 CFR Part 25.1317 at Amdt. 25-122 for the Rudder Control S ystem; 14 CFR Part 25.812 (h) at Amdt. 25-128; Additional FAA Requirements (a) Model CL-600-2B19 (1) FAR Part 36 dated December 1, 1969 , as amended through Amendments 36-18 inclusive. Individual airplanes with FAA Approved Airc raft Flight Manual RS-564 installed are recertified to 14 CFR Part 36 dated December 1, 1969, including Amendments 36-0 thru 36-31 at Stage 4. (2) Applicable portions of 14 CF R 34 (previously codified as SFAR 27). (3) Special Conditions: - High Intensity Radiated Fields (HIRF) , No. 25-ANM-61 dated July 22, 1992 - Passenger seats with non-traditional, larg e, non-metallic panels No. 25-384-SC dated August 12, 2009 Page 18 of 25 A21EA-1 - No. 25-666-SC, Non-Rechargeable Lithiu m Batteries, effective to design changes applied for after May 9, 2017. S ee the applicability section of this special condition for more information on which desi gn change must meet it. Date of application for amendment to Type Certificate May 26, 1988. Type Certificate A21EA amended Januar y 21, 1993. (b) Model CL-600-2C10/CL-600-2C11 (1a) FAR Part 36 dated December 1, 1969, as amended through Amendments 36-22 inclusive (CL-600-2C10 Only). (1b) For both models CL-600-2C10 and CL-600-2C11, individual airplanes with FAA Approved Aircraft Flight Manual RS-347 installed are recertified to 14 CFR Part 36 dated December 1, 1969, includin g Amendments 36-0 thru 36-31 at Sta ge 4. (1c) For model CL-600-2C11, individual ai rplanes with FAA Approved Aircraft Flight Manual RS-377 option code <1253> “Perform ance – Basic Range: 65000 lb / 29484 kg MTOW with 64000 lb / 29030 kg MLW” installed are certified to 14 CFR Part 36 dated December 1, 1969, includin g Amendments 36-0 thru 36-31. (1d) For model CL-600-2C11, individual ai rplanes with FAA Approved Aircraft Flight Manual RS-382 Update to Approach Actual Noise Level from 96.0 to 92.5 EPNdb for option code <1253> (MTOW 65000 lb, MLW 6 4000 lb) installed are certified to 14 CFR Part 36 dated December 1, 1969, includin g Amendments 36-0 thru 36-32. (2) Applicable portions of 14 CFR 34 (3) Special Conditions: - High Intensity Radiated Fields, No. 25-ANM-109 dated October 31, 1995 - Go-around performance credit for use of au tomatic power reserve (APR) No. 25-167-SC dated October 24, 2000. - Passenger seats with non-traditional, larg e, non-metallic panels No. 25-384-SC dated August 12, 2009 - No. 25-666-SC, Non-Rechargeable Lithiu m Batteries, effective to design changes applied for after May 9, 2017. S ee the applicability section of this special condition for more information on which desi gn change must meet it. (4) 14 CFR 25.975 at Amendment 25-143 (See NOTE 15) CL-600-2C10: Date of application for amendment to Type Certificate May 6, 1996. Type Certificate A21EA amended Februar y 16, 2001. CL-600-2C11: Date of application for amendment to Type Certificate March 1, 2019. Type Certificate A21EA amended Septembe r 18, 2019. (c) Model CL-600-2D15/CL-600-2D24 (1a) 14 CFR Part 36, effective September 10, 1990, and including all amendments effective on the date of Type Certification. (1b) 14 CFR Part 36, effective August 7, 2002 (Amendment 36-24) for CL-600-2D24 incorporating conical nozzle with CF-34-8C5 and CF-34-8C5A1 engines. (1c) For both models CL-600-2D15 and CL-600-2D24, individual airplanes with FAA Approved Aircraft Flight Manual RS-344 inst alled are recertified to 14 CFR Part 36 dated December 1, 1969, including Amendments 36-0 thru 36-31 at Stage 4. (2) 14 CFR Part 34, effective September 10, 1990, and including all amendments effective on the date of Type Certification. (3) Special Conditions: - High Intensity Radiated Fields, No. 25-ANM-109 dated October 31, 1995 - Go-around performance credit for use of automatic power reserve (APR) No. 25-167-SC dated October 24, 2000 (same as CL-600-2C10) - Sudden Engine Stoppage, No. 25-217-SC dated October 04, 2002 - Passenger seats with non-traditional, large, non-metallic panels No. 25-384-SC dated August 12, 2009 - No. 25-666-SC, Non-Rechargeable Lithiu m Batteries, effective to design changes applied for after May 9, 2017. S ee the applicability section of this special condition for more information on which design change must meet it. (4) Exemption: Exemption No. 7447 Hydraulic Systems Testing for 14 CFR 25.1435(b)(1) (5) 14 CFR 25.975 at Amendment 25-143 (See NOTE 15) Date of application for amendment to Type Certificate November 1, 1999. Type Certificate A21EA amended October 31, 2002. Page 19 of 25 A21EA-1 (d) Model CL-600-2E25 (1) 14 CFR Part 36 effective September 10, 1990, and including all amendments effective on the date of Type Certification. Individual airplanes with FAA Approved Airc raft Flight Manual RS-164 installed are recertified to 14 CFR Part 36 dated Decemb er 1, 1969, including Amendments 36-0 thru 36-31 at Stage 4. (2) 14 CFR Part 34, effective September 10, 1990, and including all amendments effective on the date of Type Certification. (3) Special Conditions: - Interaction of Systems a nd Structures (for CBW Rudder System), 25-412-SC, dated November 5, 2010 - Operation Without Normal Electrical Power, 25-413-SC, dated November 5, 2010 - Limit Torque Loads for Su dden Engine Stoppage, 25-217-SC, dated October 4, 2002 - Go-around performance credit for use of au tomatic power reserve (APR) 25-167-SC, dated October 24, 2000 (sam e as CL-600-2C10 & CL-600-2D24) - Passenger seats with non-traditional, la rge, non-metallic panels, 25-409-SC dated July 27, 2010 - High Intensity Radiated Fields, 25- ANM-109, dated October 31, 1995, for changes other than the rudder control system and the unchanged areas. - No. 25-666-SC, Non-Rechargeable Lithiu m Batteries, effective to design changes applied for after May 9, 2017. S ee the applicability section of this special condition for more information on which desi gn change must meet it. (4) Exe mption: Exemption No 10175, 14 CFR Part 25.981( a)(3) for Structural Lightning Protection Features. See NOTE 11 Date of application for amendment to Type Certificate Feb 23, 2007. Type Certificate A21EA amended December 17, 2010. Equivalent safety has been established for the following requirements: (a) CL-600-2B19 (1) 14 CFR 25.811 (d)(2) Emergency Exit Marking Sign (2) 14 CFR 25.813(c)(1) Access to T ype III exit-seat cushion intrusion (3) Several 14 CFR’s for the use of 1-g Stall Speed (nonstructural items) (4) 14 CFR 25.621 (c)(2) Overwing Emergency Exit Door Critical Castings, P/N 601R38685-1, (documented in Transport Airplane Directorate ELOS Memo TD3995NY-T-A-1) (5) 14 CFR 25.1441(c) – Oxygen Quantity Indication of Passenger Lavatory Oxygen Dispensing Units, documented in Transport Airplane Directorate ELOS Memo AT07852NY-T-S-1 dated October 14, 2014. (6) 14 CFR 25.1443(c) – Minimum Mass Flow of Supplemental Oxygen - Passenger Lavatory Oxygen Dispensing Units, documented in Transport Airplane Directorate ELOS Memo AT07852NY-T-S-2 dated October 14, 2014. (b) CL-600-2C10/CL-600-2C11 (1) 14 CFR 25.103 an d others Reduced Minimum Operating Speed Factors (2) 14 CFR 25.107 (e)(1)(iv) Vlof and Vmu (3) 14 CFR 25.109 Rejecte d Takeoff and Landing Performance Criteria (4) 14 CFR 25.811 (d)(2) Main Door Exit Marking Sign (5) 14 CFR 25.813(c)(2)(i) Emergency Exit Access documented in Transport Airplane Directorate ELOS Memo AT07658NY-T-C-1 dated April 3, 2014. (6) 14 CFR 25.904 Pe rformance Credit for Use of APR During Reduced Thrust Takeoff (7) 14 CFR 25.933 (a)(1)(ii) Thrust Reverser System (8) 14 CFR 25 App. I 25.5(b)(4) Lack of On/Off Switch for Automatic Takeoff Thrust Control System (ATTCS) (9) 14 CFR 25.841(b)(6) – High Altitude Takeoff and Landing Operations documented in Transport Airplane Directorate ELOS Memo AT2587NY-T-S-5. (10) 14 CFR 25.841 (a) and (b)(6) – High Elevation Airport Operations documented in Transport Airplane Directorate ELOS Memo TD6802NY-T-S-1. Page 20 of 25 A21EA-1 (11) 14 CFR 25.1441(c) – Oxygen Quantity Indication of Passenger Lavatory Oxygen Dispensing Units documented in Transport Airplane Directorate ELOS Memo AT07660NY-T-S-1. (12) 14 CFR 25.1443(c) – Minimum Mass Flow of Supplemental Oxygen – Passenger Lavatory Oxygen Dispensing Units documented in Transport Airplane Directorate ELOS Memo AT07660NY-T-S-2. (13) 14 CFR 25.807 and 25.813 – Passenger Seating Configuration with Additional 2 Passengers Aft of Overwing Exits, documented in Transport Airplane Directorate ELOS Memo AT08045NY-T-C-1 (See Note 13). (14) 14 CFR 25.1389(b)(3) and 25.1395 - LED Position Lights (Overlapping Intensity) documented in Policy and Innovation ELOS Memo AT11542IB-T-25.1389(b)(3) (15) 14 CFR 25.1397 - LED Position Lights (Alternate Color Definition) documented in Policy and Innovation ELOS Memo AT11542IB-T-25.1397 (c) CL-600-2D15/CL-600-2D24 (1) 14 CFR 25.103 and others Reduced Minimum Operating Speed Factors documented in Transport Airplane Directorate ELOS Memo AT2587NY-T-F-1 dated July 9, 2010. (2) 14 CFR 25.811(d)(2) Main Door Exit Marking Sign documented in Transport Airplane Directorate ELOS Memo AT2587NY-T-SE-1 dated March 25, 2010. (3) 14 CFR 25.813(c)(2)(i) Emergency Exit Access documented in Transport Airplane Directorate ELOS Memo AT07658NY-T-C-2 dated April 3, 2014. (4) 14 CFR 25.904 Performance Credit for Use of APR During Reduced Thrust Takeof f documented in Transport Aiplane Directorate ELOS Memo AT2587NY-T-P-1 dated July 6, 2010. (5) 14 CFR 25.933(a)(1)(ii) Thrust Reverser System documented in Transport Airplane Directorate ELOS Memo AT2587NY-T-P-2 dated July 6, 2010. (6) 14 CFR 25 App. I 25.5(b)(4) Lack of On/Off Switch for Automatic Takeoff Thrust Control System (ATTCS) documented in Transport Airplane Directorate ELOS Memo AT2587NY- T-P-5 dated July 6, 2010 (7) 14 CFR 25.841(b)(6) – High Altitude Takeoff and Landing Operations documented in Transport Airplane Directorate ELOS Memo AT2587NY-T dated January 31, 2007. (8) 14 CFR 25.841 (a) and (b)(6) – High Elevation Airport Operations documented in Transport Airplane Directorate ELOS Memo TD6802NY-T-S-1 dated July 31, 2013. (9) 14 CFR 25.1441(c) – Oxygen Quantity Indication of Passenger Lavatory Oxygen Dispensing Units documented in Transport Airplane Directorate ELOS Memo AT07660NY-T-S-1 dated February 10, 2014. (10) 14 CFR 25.1443(c) – Minimum Mass Flow of Supplemental Oxygen - Passenger Lavatory Oxygen Dispensing Units documented in Transport Airplane Directorate ELOS Memo AT07660NY-T-S-2 dated March 6, 2014. (11) 14 CFR 25.811(g) and 25.812(b)(1) – Symbolic Exit Signs documented in Transport Standards Branch ELOS Memo AT08649NY-T-CS -1 dated July 5, 2018. (Applicable to CL-600-2D24 only). (12) 14 CFR 25.1389(b)(3) and 25.1395 - LED Position Lights (Overlapping Intensity) documented in Policy and Innovation ELOS Memo AT11542IB-T-25.1389(b)(3) (13) 14 CFR 25.1397 - LED Position Lights (Alternate Color Definition) documented in Policy and Innovation ELOS Memo AT11542IB-T-25.1397 ( d) CL-600-2E25 (1) 14 CFR 25.107(e)(1) Take-off Speeds documented in Transport Airplane Directorate ELOS Memo AT5627NY-T-F-2 dated December 24, 2009. (2) 14 CFR 25.811(d)(1)&(2) Emergency Exit Marking Sign and Locator documented in Transport Airplane Directorate ELOS Memo AT5627NY-T-C-4-1 dated September 18, 2009. (3) 14 CFR 25.813(c)(2) Type III Emergency Exit Access documented in Transport Airplane Directorate ELOS Memo AT5627NY-T-C-4-2 dated September 18, 2009. (4) 14 CFR 25.841(b)(6) – Cabin Pressurization – High Altitude Airfield Operations documented in Transport Airplane Directorate ELOS Memo AT5627NY-T-S-4 dated December 16, 2010. (5) 14 CFR 25.933(a) Thrust Reverser System documented in Transport Airplane Directorate ELOS Memo AT5627NY-T-P-1 dated November 03, 2010. (6) 14 CFR 25.5(b)(4) App. I Lack of On/Off Switch for Automatic Takeoff Thrust Control System (ATTCS) documented in Transport Airplane Directorate ELOS Memo AT2587NY- T-P-5 dated July 6, 2010. Page 21 of 25 A21EA-1 (7) 14 CFR 25.904 App. I Performance credit for use of APR documented in Transport Airplane Directorate ELOS Memo AT2587NY-T-P-1 dated July 6, 2010 (8) 14 CFR 25.1441(c) – Oxygen Quantity Indication of Passenger Lavatory Oxygen Dispensing Units documented in Transport Airplane Directorate ELOS Memo AT07660NY-T-S-1 dated February 10, 2014. (9) 14 CFR 25.1443(c) – Minimum Mass Flow of Supplemental Oxygen - Passenger Lavatory Oxygen Dispensing Units documented in Transport Airplane Directorate ELOS Memo AT07660NY-T-S-2 dated March 6, 2014. (10) 14 CFR 25.1389(b)(3) and 25.1395 - LED Position Lights (Overlapping Intensity) documented in Policy and Innovation ELOS Memo AT11542IB-T-25.1389(b)(3) (11) 14 CFR 25.1397 - LED Position Lights (Alternate Color Definition) documented in Policy and Innovation ELOS Memo AT11542IB-T-25.1397 Compliance with the following optional requirements has been established for the CL- 600-2B19, CL- 600-2C10, CL-600-2C11, CL-600-2D15/CL-600-2D24 an d CL-600-2E25: (1) Ice P rotection of 14 CFR 25.1419 (2) Ditching provisions of 14 CFR 25.801 when the safety equipment requirements of 14CFR 25.1411 and the ditching equipment requirements of 14 CFR 25.1415 are satisfied. Equipment The basic equipment as prescribed in the applicable airworthiness requirements (See Certification Basis) must be installed in the aircraft for certification. 14 CFR Part 26 – Continued Airworthiness and Safety Improvements for Transport Category Airplanes Model CL-600-2B19 Based on 14 CFR § 21.101(g) for changes to TCs, applicable provisions of Part 26 are included in the certification basis. For any future 14 CFR Part 26 amendments, the holder of this TC must demonstrate compliance with the applicable sections. Compliance has been found for the following regulations 14 CFR §§ 26.11, 26.33, 26.43, 26.45 and 26.49. (Amdt.No.26-0, through 26-1) Model CL-600-2C10/CL-600-2C11 Based on 14 CFR § 21.101(g) for changes to TCs, applicable provisions of Part 26 are included in the certification basis. For any future 14 CFR Part 26 amendments, the holder of this TC must demonstrate compliance with the applicable sections. Compliance has been found for the following regulations 14 CFR §§ 26.11, 26.33, 26.43, 26.45 and 26.49. (Amdt.No.26-0, through 26-1) Model CL-600-2D15/CL-600-2D24 Based on 14 CFR § 21.101(g) for changes to TCs, applicable provisions of Part 26 are included in the certification basis. For any future 14 CFR Part 26 amendments, the holder of this TC must demonstrate compliance with the applicable sections. Compliance has been found for the following regulations 14 CFR §§ 26.11, 26.21, 26.33, 26.43, 26.45 and 26.49. (Amdt.No.26-0, through 26-1). Model CL-600-2E25 Based on 14 CFR § 21.101(g) for changes to TCs, applicable provisions of Part 26 are included in the certification basis. For any future 14 CFR Part 26 amendments, the holder of this TC must demonstrate compliance with the applicable sections. Compliance has been found for the following regulations 14 CFR §§ 26.11, 26.21, 26.33, 26.43, 26.45. (Amdt.No.26-0, through 26-3) Additional Design Requirements and Conditions The following design details or information must be maintained to ensure that an unsafe design condition is not present: The engines of the CL-600-2C10, CL-600-2C11, CL-600-2D15, CL-600-2D24, and CL-600-2E25 are able to be restored to a sufficient power/thrust level following an all engines out case, in order to enable the aircraft to achieve level flight without excessive loss of altitude. Page 22 of 25 A21EA-1 NOTE 1 This Aircraft Type Certificate Data Sheet de fines a configuration which does not include passenger provision for the CL-600-2B19 model green configurat ion, and the CL-600-2C11 model. Carriage o f persons in the cabin is permitted when an approved seating arrangement and related required passenger provisions are incorporated. For the CL-600-2B19 Gr een Configuration and associated modifications refer to NOTE 4 & 5. (a) Current weight and balance report including the list of equipment included in the certificated empty weight, and loading instructions when necessary, must be provided for each aircraft at the time of original certification. (b) Model CL-600-2B19 System fuel, which must be included in the empty weight, is the amount of fuel required to fill the system plumbing and tank to the undrainable level plus unusable fuel in the fuel tanks. The total amount of "system fuel" is 14.5 U.S. Gal., 97 lb. (arm +494.3). Model CL-600-2C10/CL-600-2C11 System fuel, which must be included in the empty weight, is the amount of fuel required to fill the system plumbing and tank to the undrainable level plus unusable fuel in the fuel tanks. The total amount of "system fuel" is 33.8 U.S. Gal., 228.2 lb. (arm +819.7 in). Model CL-600-2D15/CL-600-2D24 System fuel, which must be included in the empt y weight, is the amount of fuel required to fill the system plumbing and tank to the undrainable level plus unusable fuel in the fuel tanks. The total amount of "system fuel" is 33.8 U.S. Gal., 228.2 lb. (arm+929.3 in). Model CL-600-2E25 System fuel, which must be included in the empty weight, is the amount of fuel required to fill the system plumbing and tank to the undrainable level plus unusable fuel in the fuel tanks. The total amount of "system fuel" is 37.5 U.S. Gal., 252.8 lb. (arm +997.6 in). (c) Model CL-600-2B19 System oil, which must be included in the empty weight, is the amount of oil n ecessary for engine lubrication. The total amount of "system oil" is as follows: 5.83 U.S. gal. (total), 47 lb., (arm +785.67) Model CL-600-2C10/CL-600-2C11 System oil, which must be included in the empty weight, is the amount of oil required to fill the system plumbing and tanks. The total amount of "s ystem oil" is as follows: With option TS670-79-201 – Engine O il – No Remote Replenishment System, 6.1 U.S. Gal., 49.9 lb. (arm +1077.7 in) With option CR670-79-201 – Engine Oil – Remote Replenishment System, 7.8 U.S. Gal., 62.9 lb. (arm +1091.2 in) Model CL-600-2D15/CL-600-2D24 System oil, which must be included in the empty weight, is the amount of oil required to fill the system plumbing and tanks. The tota l amount of "system oil" is as follows: With option TS670-79-201 – Engine O il – No Remote Replenishment System, 6.1 U.S. Gal., 49.9 lb. (arm +1229.7 in) With option CR670-79-201 – Engine Oil – Remote Replenishment System, 7.8 U.S. Gal., 62.9 lb. (arm +1243.2 in) Model CL-600-2E25 System oil, which must be included in the empty weight, is the amount of oil required to fill the system plumbing and tanks. The total amount of "s ystem oil" is as follows: With option TS670-79-201 – Engine Oil – No Remote Replenishment System, 5.2 U.S. Gal., 42.4 lb. (arm +1345.6 in) With option CR670-79-201 – Engine Oil – Remote Replenishment System, 6.8 U.S. Gal., 55.4 lb. (arm +1356.8 in) Page 23 of 25 A21EA-1 NOTE 2 Model CL-600-2B19 All placards must be installed in accordan ce with Canadair Limite d Drawings: 601R47600, 601R47602, 601R47700. Note: Customized markings and pl acards drawings are not included. Model CL-600-2C10/CL-600-2C11 All placards must be installed in accordance with Canadair Limited Drawings: BA 670-47501, BA670-47506, BA670-47800. Self-illuminated Signs and Electrical Signs must be installed in accordance with BA670-47802 and BA670-47803. Note: Customized markings and placards drawings are not included. Drawings noted above are for basic type certification only. For as-delivered aircraft configurations, refer to customer options listed in RAL-670-300. Model CL-600-2D15/CL-600-2D24 All placards must be installed in accordance with the Bombardier Aerospace Drawings: BA 690-47500, BA690-47506, BA690-47804. Self-illuminated Signs and Electrical Signs must be installed in accordance with BA690-47805 and BA690-47806. Drawings noted above are for basic type certification only. For as- delivered aircraft configurations, refer to RAL-690-XXXX for S/N 15001 to 15013, and RAL-BA690-XXXX for S/N 15014 and subsequent. (XXXX denotes the serial number for the aircraft concerned). Model CL-600-2E25 All placards must be installed in accordance with the Bombardier Aerospace Drawings: BA 670-47850, BA670-47869, BA690-47504, BA690-47518, BA690-47525, BA690-47526, BA690-47528, BA690- 47529, BA690-47530, BA698-47203, BA698-47502, BA698-47519, BA698-47800, BA698-47805 and CC698-47251. Self-illuminated Signs and Electrical Signs must be installed in accordance with BA690-47805 and BA698-47801. Drawings noted above are for basic type certification only. For as- delivered aircraft configurations, refer to RAL-BA698-19XXX for S/N 19001 and subsequent. (19XXX denotes the serial number for the aircraft concerned). NOTE 3 Model CL-600-2B19 The airplane life limits and repetitive inspections for components and equipment and information essential for proper maintenance, are listed in Bombardier Document CSP A-053, Part 2. These limitations may not be changed without FAA Engineering approval. Model CL-600-2C10/CL-600-2C11 The airplane life limits and repetitive inspections for components and equipment and information essential for proper maintenance, are listed in Bombardier Document CSP B-053, Part 2. These limitations may not be changed without FAA Engineering approval. Model CL-600-2D15/CL-600-2D24 The airplane life limits and repetitive inspections for components and equipment and information essential for proper maintenance, are listed in Bombardier Document CSP B-053, Part 2. These limitations may not be changed without FAA Engineering approval. Model CL-600-2E25 The airplane life limits and repetitive inspections for components and equipment and information essential for proper maintenance, are listed in Bombardier Document CSP B-053, Part 2. These limitations may not be changed without FAA Engineering approval. NOTE 4 Model CL-600-2B19 Major modifications which define the aircraft as the “Green Configuration” are recorded in document RAZ-601R-110 (Definition of Type Design for Trans port Canada approval), as Appendix 2 to that document. NOTE 5 Model CL-600-2B19 The green aircraft type design does not include passe nger provisions. Carriage of persons in the cabin is permitted when an approved seati ng arrangement and related requi red passenger provisions are incorporated in accordance with the Type Approval Basis. Aircraft delivered in the “Green Configuration” and incorporating Mod. Summary TC60255 (Blocking of Emergency Exits) are limited to carrying a maximum of twenty-two (22) occupants including the crew and no more than 19 passengers in accordance with FAR 25 requirements. Page 24 of 25 A21EA-1 NOTE 6 Refer to appropriate AFM as lis ted in Approved Publications for all weather flight capability (CAT II / CAT IIIa). NOTE 7 RESERVED NOTE 8 The CRJ200 is a marketing designation for the CL-600- 2B19 (Regional Jet Series 100) aircraft with the General Electric CF-34-3B1 engines installed. All Airworthiness Directives issued against any CL-600- 2B19 aircraft are similarly applicable to the CRJ200. Special Edition (SE) and Challenger 850 are marketing designations used for a CL-600-2B19 delivered in a green configuration (See NOTES 4 & 5) and subs equently finished with an approved interior via Supplemental Type Certificates. NOTE 9 RESERVED NOTE 10 RESERVED NOTE 11 Exem ption No. 10175B-C amends Exemption No. 10175 for Structural Lightning Protection Features. NOTE 12 Model CL-600-2E25 aircraft Serial Number (S/N) 19001 to 19012 have not been shown to comply with 14 CFR Part 25.856(b) at time of delivery. Serial Numbers 19001 through 19012 are not eligible for a US Certificate of Airworthiness unless modified to comply with 14 CFR Part 25.856(b). NOTE 13 For Model CL-600-2C10 – Series 702 aircraft fitted with an approved interior including the Equivalent Safety Finding against 14 CFR 25.801 and 25.813, the maximum passenger capacity is limited to 71 passengers with a maximum of 28 passenger seats aft of the Type III overwing exit. For Model CL-600-2C10 – Series 700 and Series 701 aircra ft fitted with an approved interior including the Equivalent Safety Finding against 14 CF R 25.801 and 25.813, the maximum passenger capacity remains the same (68 and 70 passengers respectively) with a maximum of 28 passenger seats aft of the Type III overwing exit. NOTE 14 RESERVED NOTE 15 Model CL-600-2C10 – CRJ Series 700, 701, & 702 aircraft; Model CL-600-2C11 – CRJ Series 550 aircraft; Model CL-600-2D15 – CRJ Series 705 aircraft; and Model CL-600-2D24 – CRJ Series 900 aircraft, which received an original Certificate of Airworthiness on or after 23 August, 2018 and which have had Bombardier Modification Summary (ModSum) number 670T72560 (Introduction of Flame Arrestors) installed in production, comply with 14 CFR Part 25.975(a)(7) at amendment 143. NOTE 16 The CRJ550 is a marketing designation for the CL -600-2C11 (Regional Jet Series 550) aircraft. All Airworthiness Directives issued against any CL-600-2C10 (Regional Jet Series 700, 701, & 702) aircraft are similarly applicable to the CL-600-2C11 (Regional Jet Series 550) aircraft. NOTE 17 The following models were previously recorded on Revision No. 49 of TCDS A21EA and have been administratively transferred to this TCDS A21EA-1 Revision No. IR on November 26, 2019 pursuant to 14CFR § 21.47: • 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) Existing manufactured Regional Jet Series aircraft have identification data plates which still refer to FAA Type Certificate A21EA since the approved type design was recorded on FAA Type Certificate A21EA at the time of manufacture. Since both FAA Type Certificates A21EA and A21EA-1 cross-reference each other via a record on the first page of both FAA Type Certificate Data Sheets, these aircraft will not require Supplemental aircraft identification data plates to comply with 14CFR §§ 21.182, 45.11, & 45.13. FAA Airworthiness Directives (ADs) and any associated Alternate Means of Compliance (AMOCs) that refer to FAA Type Certificate A21EA and apply to any of the approved Regional Jet Series aircraft models listed above, continue to remain applicable following this administrative change. Page 25 of 25 A21EA-1 ...END... Existing FAA Supplemental Type Certificates (STCs), Part Manufacturing Approvals (PMAs), Airworthiness Directives (ADs) or Alternate Means of Compliance (AMOCs) that refer to FAA Type Certificate A21EA and apply to any of the approved Regional Jet Series aircraft models listed above, are not required to be revised following this administrative change. When revising FAA STCs or PMAs for any other reason in the future, the STCs or PMAs may directly refer to both Type Certificates. New production Regional Jet Series aircraft identification data plates will refer to the Transport Canada Type Certificate A-276 and this FAA Type Certificate A21EA-1. NOTE 18 The following Serial Numbers are manufactured by Bombardier Inc. under its manufacturing permits (12-58), under licensing agreement with MHI RJ Aviation ULC.: •CL-600-2D24: Serial Number: 15485 to 15499, which were manufactured on or after June 1, 2020. NOTE 19 Model CL-600-2D24 aircraft f itted with an approved interior where the aft pair of overwing emergency exit doors are blocked, are limited to carrying a maximum of fifty-six (56) occupants including 6 crew- members (1 Pilot, 1 Copilot, 1 Observer, and 3 Flight Attendants) and no more than 50 passengers in accordance with FAR 25 requirements. ``` ## ADs (347, first 50, in force first) - [AD 2026-15-16](https://openairdocs.org/ad/2026-15-16): Time Limits/Maintenance Checks · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 3 more. Effective Sep 3, 2026 - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2026-08-02](https://openairdocs.org/ad/2026-08-02): Stabilizers · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective May 26, 2026 - [AD 2026-05-05](https://openairdocs.org/ad/2026-05-05): Flight controls · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Mar 23, 2026 - [AD 2026-02-03](https://openairdocs.org/ad/2026-02-03): Flight control · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Feb 5, 2026 - [AD 2025-25-03](https://openairdocs.org/ad/2025-25-03): Time Limits/Maintenance Checks · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Jan 16, 2026 - [AD 2025-13-04](https://openairdocs.org/ad/2025-13-04): Flight Controls · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Aug 5, 2025 - [AD 2025-11-11](https://openairdocs.org/ad/2025-11-11): Time Limits/Maintenance Checks · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Jul 15, 2025 - [AD 2025-09-09](https://openairdocs.org/ad/2025-09-09): Communications · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Jun 18, 2025 - [AD 2025-04-08](https://openairdocs.org/ad/2025-04-08): Navigation · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Apr 25, 2025 - [AD 2025-02-03](https://openairdocs.org/ad/2025-02-03): Fuselage · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100) and CL-600-2B19 (Regional Jet Series 440). Effective Mar 17, 2025 - [AD 2024-24-07](https://openairdocs.org/ad/2024-24-07): Equipment/furnishings · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100) and CL-600-2B19 (Regional Jet Series 440). Effective Jan 13, 2025 - [AD 2024-16-08](https://openairdocs.org/ad/2024-16-08): Equipment/furnishings · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 2 more. Effective Oct 23, 2024 - [AD 2024-13-07](https://openairdocs.org/ad/2024-13-07): Electrical power · MHI RJ Aviation ULC CL-600-2D15 (Regional Jet Series 705) and CL-600-2D24 (Regional Jet Series 900). Effective Sep 25, 2024 - [AD 2024-14-01](https://openairdocs.org/ad/2024-14-01): Oxygen · MHI RJ Aviation ULC CL-600-2D15 (Regional Jet Series 705) and CL-600-2D24 (Regional Jet Series 900). Effective Sep 25, 2024 - [AD 2024-10-09](https://openairdocs.org/ad/2024-10-09): Time Limits/Maintenance Checks · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100) and CL-600-2B19 (Regional Jet Series 440). Effective Jul 19, 2024 - [AD 2024-07-08](https://openairdocs.org/ad/2024-07-08): Fuselage · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 3 more. Effective Jun 5, 2024 - [AD 2024-06-05](https://openairdocs.org/ad/2024-06-05): Time Limits/Maintenance Checks · MHI RJ Aviation ULC CL-600-2E25 (Regional Jet Series 1000). Effective May 14, 2024 - [AD 2024-03-02](https://openairdocs.org/ad/2024-03-02): Time Limits/Maintenance Checks · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Apr 9, 2024 - [AD 2023-25-01](https://openairdocs.org/ad/2023-25-01): Equipment/Furnishings · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Feb 6, 2024 - [AD 2023-24-03](https://openairdocs.org/ad/2023-24-03): Fire Protection · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Jan 22, 2024 - [AD 2023-21-12](https://openairdocs.org/ad/2023-21-12): Pneumatic · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100) and CL-600-2B19 (Regional Jet Series 440). Effective Dec 26, 2023 - [AD 2023-19-08](https://openairdocs.org/ad/2023-19-08): Fire Protection · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Nov 9, 2023 - [AD 2023-20-09](https://openairdocs.org/ad/2023-20-09): Landing Gear · MHI RJ Aviation ULC CL-600-2E25 (Regional Jet Series 1000). Effective Oct 30, 2023 - [AD 2023-10-03](https://openairdocs.org/ad/2023-10-03): Fire Protection · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Jul 11, 2023 - [AD 2023-09-02](https://openairdocs.org/ad/2023-09-02): Fire Protection · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Jun 26, 2023 - [AD 2023-07-07](https://openairdocs.org/ad/2023-07-07): Pneumatic · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Jun 20, 2023 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2023-06-06](https://openairdocs.org/ad/2023-06-06): Air conditioning · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Apr 28, 2023 - [AD 2022-20-03](https://openairdocs.org/ad/2022-20-03): Oxygen · MHI RJ Aviation ULC CL-600-2C11 (Regional Jet Series 550), CL-600-2C10 (Regional Jet Series 702), CL-600-2C10 (Regional Jet Series 701) and 4 more. Effective Apr 14, 2023 - [AD 2022-26-04](https://openairdocs.org/ad/2022-26-04): Oxygen · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100) and CL-600-2B19 (Regional Jet Series 440). Effective Feb 2, 2023 - [AD 2022-24-10](https://openairdocs.org/ad/2022-24-10): Fire protection · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Jan 18, 2023 - [AD 2022-21-10](https://openairdocs.org/ad/2022-21-10): Landing gear · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Dec 21, 2022 - [AD 2022-18-15](https://openairdocs.org/ad/2022-18-15): Fuel · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Nov 25, 2022 - [AD 2022-12-03](https://openairdocs.org/ad/2022-12-03): Navigation System · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Nov 3, 2022 - [AD 2022-18-17](https://openairdocs.org/ad/2022-18-17): Wings · MHI RJ Aviation ULC CL-600-2D24 (Regional Jet Series 900). Effective Oct 11, 2022 - [AD 2022-16-05](https://openairdocs.org/ad/2022-16-05): Fuselage · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100) and CL-600-2B19 (Regional Jet Series 440). Effective Sep 27, 2022 - [AD 2022-13-02](https://openairdocs.org/ad/2022-13-02): Fuel system · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Aug 31, 2022 - [AD 2022-15-08](https://openairdocs.org/ad/2022-15-08): Information systems · Airbus A318-111, A318-112, A319-111 and 49 more. Effective Aug 12, 2022 - [AD 2021-22-24](https://openairdocs.org/ad/2021-22-24): Periodic Inspections · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Dec 29, 2021 - [AD 2021-19-12](https://openairdocs.org/ad/2021-19-12): Landing Gear · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective Nov 10, 2021 - [AD 2021-13-11](https://openairdocs.org/ad/2021-13-11): Fuselage · MHI RJ Aviation ULC CL-600-2D15 (Regional Jet Series 705) and CL-600-2D24 (Regional Jet Series 900). Effective Sep 3, 2021 - [AD 2021-11-02](https://openairdocs.org/ad/2021-11-02): Auto Flight · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Jul 13, 2021 - [AD 2021-08-03](https://openairdocs.org/ad/2021-08-03): Rain and Ice Protection · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 4 more. Effective May 25, 2021 - [AD 2021-07-10](https://openairdocs.org/ad/2021-07-10): Ice and Rain Protection · MHI RJ Aviation ULC CL-600-2C10 (Regional Jet Series 700), CL-600-2C10 (Regional Jet Series 701), CL-600-2C10 (Regional Jet Series 702) and 2 more. Effective May 12, 2021 - [AD 2021-07-03](https://openairdocs.org/ad/2021-07-03): Fuselage · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100) and CL-600-2B19 (Regional Jet Series 440). Effective May 10, 2021 - [AD 2021-01-01](https://openairdocs.org/ad/2021-01-01): Landing gear · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100) and CL-600-2B19 (Regional Jet Series 440). Effective Mar 30, 2021 - [AD 2020-21-02](https://openairdocs.org/ad/2020-21-02): Fire protection · Airbus Canada Limited Partnership BD-500-1A10, BD-500-1A11, A330-201 and 45 more. Effective Nov 19, 2020 - [AD 2020-17-15](https://openairdocs.org/ad/2020-17-15): Navigation · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100), CL-600-2B19 (Regional Jet Series 440), CL-600-2C10 (Regional Jet Series 700) and 6 more. Effective Nov 3, 2020 - [AD 2020-12-13](https://openairdocs.org/ad/2020-12-13): Wings · MHI RJ Aviation ULC CL-600-2B19 (Regional Jet Series 100) and CL-600-2B19 (Regional Jet Series 440). Effective Sep 10, 2020 All 347: https://openairdocs.org/tcds/A21EA-1/ads.md ## Registered aircraft by registry model (OpenAirDocs) - [Bombardier CL-600-2B19](https://openairdocs.org/model/bombardier-cl-600-2b19): 395 aircraft (registry code 1390008) - [Bombardier CL-600-2D24](https://openairdocs.org/model/bombardier-cl-600-2d24): 314 aircraft (registry code 1390016) - [Bombardier CL-600-2C10](https://openairdocs.org/model/bombardier-cl-600-2c10): 177 aircraft (registry code 1390015) - [Bombardier CL-600-2C11](https://openairdocs.org/model/bombardier-cl-600-2c11): 110 aircraft (registry code 1390021) - [Canadair CL-600-2B19](https://openairdocs.org/model/canadair-cl-600-2b19): 19 aircraft (registry code 1900309) - [Bombardier CL-600-2E25](https://openairdocs.org/model/bombardier-cl-600-2e25): 10 aircraft (registry code 1390116) - [Bombardier Inc Canadair CL-600-2B19](https://openairdocs.org/model/bombardier-inc-canadair-cl-600-2b19): 2 aircraft (registry code 1390025) - [Bombardier Aerospace CL-600-2C10](https://openairdocs.org/model/bombardier-aerospace-cl-600-2c10): 1 aircraft (registry code 1390075) - [Mhi RJ Aviation ULC CL-600-2B19](https://openairdocs.org/model/mhi-rj-aviation-ulc-cl-600-2b19): 1 aircraft (registry code 1390099) - [Mhi RJ Aviation ULC CL-600-2C10](https://openairdocs.org/model/mhi-rj-aviation-ulc-cl-600-2c10): 1 aircraft (registry code 1390031) - [Mhi RJ Aviation ULC CL-600-2D24](https://openairdocs.org/model/mhi-rj-aviation-ulc-cl-600-2d24): 0 aircraft (registry code 1390030) ## STCs approved under this data sheet (79, first 50) - [STC ST11370DS](https://openairdocs.org/stc/ST11370DS): Installation of a Cabin Interior Reconfiguration. Altitude Aerospace USA - [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center - [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles.. AMETEK AMERON, LLC d/b/a MASS Systems - [STC ST12455IB](https://openairdocs.org/stc/ST12455IB): Cabin reconfiguration to add an extra row of business class seating and remove one row of economy seating. Airhawke Aérospatial Inc. - [STC ST04755NY](https://openairdocs.org/stc/ST04755NY): Installation of the SpaceX Starlink Aviation System. Space Exploration Technologies Corp. / Starlink Aviation - [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc. - [STC ST12396IB](https://openairdocs.org/stc/ST12396IB): Installation of Laseref V Inertial Reference System. Avmax Aviation Services Inc. - [STC ST12397NY](https://openairdocs.org/stc/ST12397NY): Installation of Class E Freighter Cargo Conversion. Cascade Aerospace Inc. - [STC ST04790NY](https://openairdocs.org/stc/ST04790NY): Installation Bruce Cabin Lighting. Delta Engineering Corporation - [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles.. AMETEK AMERON LLC d/b/a MASS Systems - [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc - [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc. - [STC ST04812NY](https://openairdocs.org/stc/ST04812NY): Installation of Hughes Satellite Connectivity and Wifi Cabin Distribution System. ALOFT AeroArchitects - [STC ST00030IB](https://openairdocs.org/stc/ST00030IB): Installation of Test Tech ELT. APTOZ EHF - [STC ST12199IB](https://openairdocs.org/stc/ST12199IB): Modification of Original Overhead Bins. GAL AVIATION INC. - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc. - [STC ST02721LA](https://openairdocs.org/stc/ST02721LA): Updates the aircraft recording system by installing a new SRVIVR25 Cockpit Voice Recorder (CVR) with Integrated Recorder Independent Power Supply (RIPS). Acron Aviation Inc. - [STC ST02398LA](https://openairdocs.org/stc/ST02398LA): Interior Installations and Modifications. Safran Cabin Inc. - [STC ST02400LA](https://openairdocs.org/stc/ST02400LA): Interior Installations and Modifications. Safran Cabin Inc. - [STC ST02566LA](https://openairdocs.org/stc/ST02566LA): Interior installations and modifications. Safran Cabin Inc. - [STC ST02567LA](https://openairdocs.org/stc/ST02567LA): Interior Installations and Modifications. Safran Cabin Inc. - [STC ST02569LA](https://openairdocs.org/stc/ST02569LA): Interior Installations and Modifications. Safran Cabin Inc. - [STC SA7081NM](https://openairdocs.org/stc/SA7081NM): Installation of interior fluorescent cabin lighting system.. Bruce Aerospace Inc. - [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc. - [STC ST02811LA](https://openairdocs.org/stc/ST02811LA): Installation of six Rockwell Collins Electronic Flight Displays Model EFD-4076 upgraded with Light Emitting Diode display screen. Thomas Global Systems LLC - [STC ST04796NY](https://openairdocs.org/stc/ST04796NY): Installation of Cabin Connectivity. Delta Engineering Corporation - [STC ST11865IB](https://openairdocs.org/stc/ST11865IB): The modification and installation of Cabin Sound Proofing Material. Nigel Waterhouse (DAR 367) - [STC ST02586AK](https://openairdocs.org/stc/ST02586AK): Approval of the Thomas Global Systems TFD-4000/4100 Active Matrix Liquid Crystal Display. ADS-B Technologies - [STC ST11843IB](https://openairdocs.org/stc/ST11843IB): nstallation of Passenger Seat Modifications. B/E Aerospace Limited - [STC ST00224IB](https://openairdocs.org/stc/ST00224IB): Modification and Installation of Cabin Reconfiguration to 30 and 38 PAX LOPA. Airhawke Aérospatial Inc. - [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc. - [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST00214IB](https://openairdocs.org/stc/ST00214IB): Installation of replacement cabin equipment. B/E Aerospace Limited - [STC ST04797NY](https://openairdocs.org/stc/ST04797NY): Installation of Connectivity Antenna. Delta Engineering Corporation - [STC ST04794NY](https://openairdocs.org/stc/ST04794NY): Installation of Stellar Blu Solutions Cabin Connectivity. Delta Engineering Corporation - [STC ST04793NY](https://openairdocs.org/stc/ST04793NY): Installation of Stellar Blu Solutions Connectivity Antenna. Delta Engineering Corporation - [STC ST00489IB](https://openairdocs.org/stc/ST00489IB): Modification and Installation of Lavatory Countertop, Toilet Shroud, Floor Pan, and Sink Light. GAL Aviation Inc - [STC ST04839NY](https://openairdocs.org/stc/ST04839NY): Installation of LED Position/Anti-Collision Lights. Sterling Helicopter - [STC ST04624CH](https://openairdocs.org/stc/ST04624CH): Installation of Astronics In-Seat Power System. Astronics Armstrong Aerospace - [STC ST04622CH](https://openairdocs.org/stc/ST04622CH): Installation of Cabin Interior Modifications. JST Shuttle Holdings LLC - [STC ST04113NY](https://openairdocs.org/stc/ST04113NY): Update of a Cabin Interior. Delta Engineering Corporation - [STC ST00117IB](https://openairdocs.org/stc/ST00117IB): Installation of a Complete Custom Aircraft Interior. Flying Colours Corp. - [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH - [STC ST02800LA](https://openairdocs.org/stc/ST02800LA): Installation of USB Ports Type A and Type C and Power Inverters in the cabin. U.S. Technical Consultants Inc. - [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited - [STC ST00072IB](https://openairdocs.org/stc/ST00072IB): Installation of the Rockwell Collins TDR-94D Transponder Upgrade - ADS-B Out. New United Goderich Inc. - [STC ST00041IB](https://openairdocs.org/stc/ST00041IB): Installation of VIP Cabin Interior and miscellaneous aircraft systems. Lufthansa Technik AG - [STC ST03663AT](https://openairdocs.org/stc/ST03663AT): Installation of an Artex C406-2 Emergency Locator Transmitter (ELT). Woven Electronics LLC - [STC ST04720NY](https://openairdocs.org/stc/ST04720NY): Installation of structural provisions for AeroH Antenna system. Lufthansa Technik AG - [STC ST04719NY](https://openairdocs.org/stc/ST04719NY): Installation of Structural Provision for Cabin Completion. Lufthansa Technik AG All 79: https://openairdocs.org/tcds/A21EA-1/stcs.md --- 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.