TCDS T00011AT

Page. No. 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 Rev. No. 38 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 30 34 34 33 33 30 30 30 33 Page. No 36 37 38 39 40 41 Rev. No 30 37 30 37 30 31 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION T00011AT Revision 38 Embraer EMB-145 EMB-145ER EMB-145MR EMB-145LR EMB-135ER EMB-135LR EMB-135KE EMB-135KL EMB-135BJ EMB-145XR EMB-145MP EMB-145EP January 21, 2022 TYPE CERTIFICATE DATA SHEET NO. T00011AT This data sheet which is part of Type Certificate Number, T00011AT, 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 Embraer S.A. Av. Brigadeiro Faria Lima, 2170 12227-901 - São José dos Campos - SP Brazil Type Certificate Holder Record Yaborã Indústria Aeronáutica S.A. transferred the TC No. T00011AT to Embraer S.A. on January 21, 2022. Embraer S. A. Transferred TC No. T00011AT to Yaborã Indústria Aeronáutica S.A. on January 31, 2020 Empresa Brasileira de Aeronáutica S.A. (Embraer) changed company name to Embraer S.A. effective January 2011. 1. - Model EMB-145, (Transport Category), approved December 10, 1996 Engine Two – Rolls Royce Corporation (See Note 16.) Model AE 3007A Fuel Brazilian Specification CNP-08/QAV1. ASTM Specification D-1655 JET A or JET A1 MIL-T-83133A JP-8. APU Sundstrand Aerospace Model T-62T-40C11 or T-62T-40C14 Limitations as stated in Sundstrand Doc. No. ESR 0921 and No. ESR 1112 Oil Engine Synthetic Oil conforming to MIL-L-23699 or MIL-L-7808 (below -40°F) APU MIL-L-23699 or MIL-L-7808 Revision 38 Page 2 of 40 T00011AT Engine Model AE3007A Limits Operating Conditions Static Thrust (lb.) Rotor Speed (%) Temperature Interturbine (°C) -1000ft SL N1 N2 ITT Takeoff 7,593 7,457 100(2) 102.5(N23) 921(1) (1690° F) Maximum Continuous 6,851 6,725 100 102.5 868 (1600° F) Ground 53.6 (min), 102.5 (max) Starting 800 (1472° F) (1) Time limited to 5 minutes. (2) 100 % N1 =8,700 rpm (3) 102.5 % N2 = 16,270 rpm Oil Temperature Maximum: 126°C (260°F) Normal oil temperature range: 21°C to 126°C (70 at 260°F) Minimum temperature for starting: above -40°C (-40°F) for lubrication oil specified by MIL-L-23699 above -54°C (-65°F) for lubrication oil specified by MIL-L-7808 Minimum to increase N2 above 83%: 40ºC (104°F) Oil Pressure Maximum: 95 psig - This limit may be exceeded during starts if oil temperature is below 21°C. For takeoff and go-around the maximum limit is 115 psi, limited to 5 minutes. For aircraft which have complied with SBAE30071-79-025 or equivalent, the maximum limit for takeoff and go around is 155 PSI, limited to 2 minutes. Minimum: 48 psig (N2 equal or above 88%) 34 psig (N2 below 88%) APU Limits (both models) Maximum RPM: 108% Maximum EGT: Steady State (Time limited to 5 minutes) 1323°F (717º C) Running (Normal) 1256°F (680° C) Airspeed Limits (EAS) Maximum Operating Limit Speed VMO: - 0 to 8,000 ft: 250 KEAS - 10,000 to 26,300 ft: 320 KEAS - 26,300 to 37,000 ft: 0.78 Mach - (Linear variation from 8,000 to 10,000 ft.) Maneuvering speed (VA): 200 KEAS Maximum flap extended speed (VFE): − Flaps 9° (Takeoff/Approach): 250 KEAS − Flaps 22°: 200 KEAS − Flaps 45° (Landing) : 145 KEAS Maximum landing gear extended speed (VLE): 250 KEAS Maximum landing gear operating speed (VLO): -VLO for retraction 200 KEAS -VLO for extension 250 KEAS Revision 38 Page 3 of 40 T00011AT C.G Limits (landing gear extended) 592.4 to 623.3 inches (15.6% to 43% MAC) with 42,549 lbs. (19,300 kg). 592.4 to 623.3 inches (15.6% to 43% MAC) with 42,328 lbs. (19,200 kg). 588.3 to 623.3 inches (12% to 43% MAC) with 34,171 lbs. (15,500 kg). 588.3 to 623.3 inches (12% to 43% MAC) with 28,660 lbs. (13,000 kg). 619.9 inches (40% MAC) with 26,455 lbs. (12,000 kg). Straight linear variation between the points given. Moment due to landing gear retraction - 10,155 in-lbs. (-117 kgf-m) (the aircraft C.G. is moved forward with the retraction). Maximum Weights Ramp 42,549 lbs. (19,300 kgf) Takeoff 42,328 lbs. (19,200 kgf) Landing 41,226 lbs. (18,700 kgf) Zero fuel 37,698 lb (17,100 kgf) Maximum Baggage 2,646 lb (1,200 kg) Fuel Capacity 1373.8 gallons (two tanks, 686.9 gallons each at +603.6 inches). Unusable fuel of 14.3 gallons (7.15 gallons for each tank). Serial Numbers Eligible 145004 and subsequent. A Brazilian Certificate of Airworthiness for Export endorsed as noted under “Import Requirements” must be submitted for each individual aircraft for which application for U.S. certification is made. 2. - Model EMB-145ER, (Transport Category), Approved December 10, 1996 Engine Two – Rolls Royce Corporation (See Note 16.) Model AE 3007A, AE3007A1/1, AE3007A1/2, AE3007A1, or Model AE3007A1P (See Note 12 for engine intermix operation.) Fuel Brazilian Specification CNP-08/QAV1. ASTM Specification D-1655 JET A or JET A1 MIL-T-83133A JP-8. APU Sundstrand Aerospace Model T-62T-40C11 or T-62T-40C14 Limitations as stated in Sundstrand Doc. No. ESR 0921 and No. ESR 1112 Oil Engine: MIL-L-7808 or MIL-L-23699 APU: MIL-L-23699 or MIL-L-7808 Engine Models AE3007A and AE3007A1/1 Limits Operating Conditions Static Thrust (lb.) Rotor Speed (%) Temperature Interturbine (°C) -1000ft N1 N2 ITT Takeoff 7,580 100(2) 102.5(3) 921(1) (1690° F) Maximum Continuous 6,820 100 102.5 868 (1600° F) Ground 53.6 (min), 102.5 (max) Starting 800 (1472° F) (1) Time limited to 5 minutes. (2) 100 % N1 =8,700 rpm (3) 102.5 % N2 = 16,270 rpm Revision 38 Page 4 of 40 T00011AT Engine Models AE3007A1/2 and AE3007A1 Limits Operating Conditions Static Thrust (lb.) Rotor Speed (%) Temperature Interturbine (°C) -1000ft N1 N2 ITT Takeoff 7,580 100(2) 102.5(3) 948(1) (1738° F) Maximum Continuous 6,820 100 102.5 901 (1653° F) Ground 53.6 (min), 102.5 (max) Starting 800 (1472° F) (1) Time limited to 5 minutes. (2) 100% N1 = 8,700 rpm (3) 102.5 % N2 =16,270 rpm Engine Model AE3007A1P Limits Operating Conditions Static Thrust (lb.) Rotor Speed (%) Temperature Interturbine (°C) -1000ft SL N1 N2 ITT Takeoff 8,338 8,195 100(2) 102.5(3) 948(1) (1738° F) Maximum Continuous 6,852 6,759 100 102.5(3) 901 (1653° F) Ground 53.6 (min), 102.5 (max) Starting 800 (1472° F) (1) Time limited to 5 minutes. (2) 100 % N1 =8,700 rpm (3) 102.5 % N2 = 16,270 rpm Oil Temperature Maximum: 126°C (260°F) Normal oil temperature range: 21°C to 126°C (70 at 260°F) Minimum temperature for starting: above -40°C (-40°F) for lubrication oil specified by MIL-L-23699 above -54°C (-65°F) for lubrication oil specified by MIL-L-7808 Minimum to increase N2 above 83%: 40ºC (104°F) Oil Pressure Maximum: 95 psig (This limit may be exceeded during starts if oil temperature is below 21°C (70oF)) (for Airplanes with engine FADEC software previous to version B7.6 installed). 110 psig (This limit may be exceeded during starts if oil temperature is below 21oC (70oF)) (for Airplanes with engine FADEC software version B7.6 or later approved version installed). For takeoff and go-around the maximum limit is 115 psi, limited to 5 minutes. For aircraft which have complied with SBAE 30071-79-025 or equivalent, the maximum limit for takeoff and go around is 155 PSI, limited to 2 minutes. Minimum: 48 psig (N2 equal or above 88%) 34 psig (N2 below 88%) APU Limits (both models) Maximum RPM: 108% Maximum EGT: Steady State (Time limited to 5 minutes) 1323°F (717º C) Running (Normal) 1256°F (680° C) Airspeed Limits (EAS) Maximum Operating Limit Speed VMO: - 0 to 8,000 ft: 250 KEAS - 10,000 to 26,300 ft: 320 KEAS - 26,300 to 37,000 ft: 0.78 Mach - (Linear variation from 8,000 to 10,000 ft.) Revision 38 Page 5 of 40 T00011AT Maneuvering speed (VA): 200 KEAS Maximum flap extended speed (VFE): − Flaps 9° (Takeoff/Approach): 250 KEAS − Flaps 18° ( Takeoff) 200 KEAS (See Note 15) − Flaps 22°: 200 KEAS − Flaps 45° (Landing) : 145 KEAS Maximum landing gear extended speed (VLE): 250 KEAS Maximum landing gear operating speed (VLO): -VLO for retraction 200 KEAS -VLO for extension 250 KEAS C. G. Limits (landing gear extended) 594.0 to 623.3 inches (17% to 43% MAC) with 45,635 lbs. (20,700 kg). 594.0 to 623.3 inches (17% to 43% MAC) with 45,414 lbs. (20,600 kg). 588.3 to 623.3 inches (12% to 43% MAC) with 34,171 lbs. (15,500 kg). 588.3 to 623.3 inches (12% to 43% MAC) with 28,660 lbs. (13,000 kg). 619.9 inches (40% MAC) with 26,455 lbs. (12,000 kg). Straight linear variation between the points given. Moment due to landing gear retraction - 10,155 in-lbs. (-117 kgf-m) (the aircraft C.G. is moved forward with the retraction). Maximum Weights Ramp 45,635 lbs. (20,700 kgf) Takeoff 45,414 lbs. (20,600 kgf) Landing 41,226 lbs. (18,700 kgf) Zero fuel 37,698 lbs. (17,100 kgf) Maximum Baggage 2,646 lbs. (1,200 kg) Fuel Capacity 1373.8 gallons (two tanks, 686.9 gallons each at +603.6 inches). Unusable fuel of 14.3 gallons (7.15 gallons for each tank). Serial Numbers Eligible 145004 and subsequent. A Brazilian Certificate of Airworthiness for Export endorsed as noted under “Import Requirements” must be submitted for each individual aircraft which application for U.S. certification is made. 3. - Model EMB-145MR, (Transport Category), Approved May 7, 1998 Engine Two – Rolls Royce Corporation (See Note 16.) Model AE 3007A1/1, AE 3007A1/2, AE3007A1 or AE3007A1P Fuel Brazilian Specification CNP-08/QAV1. ASTM Specification D-1655 JET A or JET A1 MIL-T-83133A JP-8. APU Sundstrand Aerospace Model T-62T-40C11 or T-62T-40C14 Limitations as stated in Sundstrand Doc. No. ESR 0921 and No. ESR 1112 Oil Engine: MIL-L-7808 or MIL-L-23699 APU: MIL-L-23699 or MIL-L-7808 Revision 38 Page 6 of 40 T00011AT Engine Model AE3007A1/1 Limits Operating Conditions Static Thrust (lb.) Rotor Speed (%) Temperature Interturbine (°C) -1000ft N1 N2 ITT Takeoff 7,580 100(2) 102.5(3) 921(1) (1690° F) Maximum Continuous 6,820 100 102.5 868 (1605° F) Ground 53.6 (min), 102.5 (max) Starting 800 (1472° F) (1) Time limited to 5 minutes. (2) 100 % N1 =8,700 rpm (3) 102.5 % N2 = 16,270 rpm Engine Models AE3007A1/2 and AE3007A1 Limits Operating Conditions Static Thrust (lb.) Rotor Speed (%) Temperature Interturbine (°C) -1000ft N1 N2 ITT Takeoff 7,580 100(2) 102.5(3) 948(1) (1738° F) Maximum Continuous 6,820 100 102.5 901 (1653° F) Ground 53.6 (min), 102.5 (max) Starting 800 (1472° F) (1) Time limited to 5 minutes. (2) 100 % N1 =8,700 rpm (3) 102.5 % N2 = 16,270 rpm Engine Model AE3007A1P Limits Operating Conditions Static Thrust (lb.) Rotor Speed (%) Temperature Interturbine (°C) -1000ft N1 N2 ITT Takeoff 8,338 100(2) 102.5(3) 948(1) (1738° F) Maximum Continuous 6,852 100 102.5(3) 901 (1653° F) Ground 53.6 (min), 102.5 (max) Starting 800 (1472° F) (1) Time limited to 5 minutes. (2) 100 % N1 =8,700 rpm (3) 102.5 % N2 = 16,270 rpm Oil Temperature Maximum: 126°C (260°F) Normal oil temperature range: 21°C to 126°C (70 at 260°F) Minimum temperature for starting: above -40°C (-40°F) for lubrication oil specified by MIL-L-23699 above -54°C (-65°F) for lubrication oil specified by MIL-L-7808 Minimum to increase N2 above 83%: 40ºC (104°F) Oil Pressure Maximum: 95 psig (This limit may be exceeded during starts if oil temperature is below 21°C (70oF)) (for Airplanes with engine FADEC software previous to version B7.6 installed). 110 psig (This limit may be exceeded during starts if oil temperature is below 21oC (70oF)) (for Airplanes with engine FADEC software version B7.6 or later approved version installed). For takeoff and go-around the maximum limit is 115 psi, limited to 5 minutes. For aircraft which have complied with SBAE 30071-79-025 or equivalent, the maximum limit for takeoff and go around is 155 PSI, limited to 2 minutes. Minimum: 48 psig (N2 equal or above 88%) 34 psig (N2 below 88%) Revision 38 Page 7 of 40 T00011AT APU Limits (both models) Maximum RPM: 108% Maximum EGT: Steady State (Time limited to 5 minutes) 1323°F (717º C) Running (Normal) 1256°F (680° C) Airspeed Limits (EAS) Maximum Operating Limit Speed VMO: - 0 to 8,000 ft: 250 KEAS - 10,000 to 26,300 ft: 320 KEAS - 26,300 to 37,000 ft: 0.78 Mach - (Linear variation from 8,000 to 10,000 ft.) Maneuvering speed (VA): 202 KEAS Maximum flap extended speed (VFE): − Flaps 9° (Takeoff/Approach): 250 KEAS − Flaps 18° ( Takeoff) 200 KEAS (See Note 15) − Flaps 22°: 200 KEAS − Flaps 45° (Landing) : 145 KEAS Maximum landing gear extended speed (VLE): 250 KEAS Maximum landing gear operating speed (VLO): -VLO for retraction 200 KEAS -VLO for extension 250 KEAS C. G. Limits (landing gear extended) 595.6 to 619.4 inches (18.4% to 39.5% MAC) with 48,721 lbs. (22,100 kg). 595.6 to 619.4 inches (18.4% to 39.5% MAC) with 48,501 lbs. (22,000 kg). 592.5 to 619.4 inches (15.7% to 39.5% MAC) with 42,549 lbs. (19,300 kg). 590.1 to 623.3 inches (13.6% to 43.0% MAC) with 37,698 lbs. (17,100 kg). 588.3 to 623.3 inches (12.0% to 43.0% MAC) with 34,171 lbs. (15,500 kg). 588.3 to 623.3 inches (12.0% to 43.0% MAC) with 29,541 lbs. (13,400 kg). 608.6 inches (30% MAC) with 27,337 lbs. (12,400 kg). Straight linear variation between the points given. Moment due to landing gear retraction - 10,763 in-lbs. (-124 kgf-m) (the aircraft C.G. is moved forward with the retraction). Maximum Weights Ramp 48,721 lbs. (22,100 kgf) Takeoff 48,501 lbs. (22,000 kgf) Landing 42,549 lbs. (19,300 kgf) Zero fuel 39,462 lbs. (17,900 kgf) Maximum Baggage 2,646 lbs. (1,200 kg) Fuel Capacity 1373.8 gallons (two tanks, 686.9 gallons each at +603.6 inches). Unusable fuel of 14.3 gallons (7.15 gallons for each tank). Serial Numbers Eligible 145048 and subsequent. A Brazilian Certificate of Airworthiness for Export endorsed as noted under “Import Requirements” must be submitted for each individual aircraft for which application for U.S. certification is made. Revision 38 Page 8 of 40 T00011AT 4. - Model EMB-145LR, (Transport Category), Approved May 7, 1998 Engine Two – Rolls Royce Corporation (See Note 16.) Model AE 3007A1/1, AE 3007A1/2, AE3007A1 or AE3007A1P Fuel Brazilian Specification CNP-08/QAV1. ASTM Specification D-1655 JET A or JET A1 MIL-T-83133A JP-8. APU Sundstrand Aerospace Model T-62T-40C11 or T-62T-40C14 Limitations as stated in Sundstrand Doc. No. ESR 0921 and No. ESR 1112 Oil Engine: MIL-L-7808 or MIL-L-23699 APU: MIL-L-23699 or MIL-L-7808 Engine Model AE3007A1/1 Limits Operating Conditions Static Thrust (lb.) Rotor Speed (%) Temperature Interturbine (°C) -1000ft N1 N2 ITT Takeoff 7,580 100(2) 102.5(3) 921(1) (1690° F) Maximum Continuous 6,820 100 102.5 868 (1605° F) Ground 53.6 (min), 102.5 (max) Starting 800 (1472° F) (1) Time limited to 5 minutes. (2) 100 % N1 =8,700 rpm (3) 102.5 % N2 = 16,270 rpm Engine Models AE3007A1/2 and AE3007A1 Limits Operating Conditions Static Thrust (lb.) Rotor Speed (%) Temperature Interturbine (°C) -1000ft N1 N2 ITT Takeoff 7,580 100(2) 102.5(3) 948(1) (1738° F) Maximum Continuous 6,820 100 102.5 901 (1653° F) Ground 53.6 (min), 102.5 (max) Starting 800 (1472° F) (1) Time limited to 5 minutes. (2) 100 % N1 =8,700 rpm (3) 102.5 % N2 = 16,270 rpm Engine Model AE3007A1P Limits Operating Conditions Static Thrust (lb.) Rotor Speed (%) Temperature Interturbine (°C) -1000ft N1 N2 ITT Takeoff 8,338 100(2) 102.5(3) 948(1) (1738° F) Maximum Continuous 6,852 100 102.5(3) 901 (1653° F) Ground 53.6 (min), 102.5 (max) Starting 800 (1472° F) (1) Time limited to 5 minutes. (2) 100 % N1 =8,700 rpm (3) 102.5 % N2 = 16,270 rpm Revision 38 Page 9 of 40 T00011AT Oil Temperature Maximum: 126°C (260°F) Normal oil temperature range: 21°C at 126°C (70 at 260°F) Minimum temperature for starting: above -40°C (-40°F) for lubrication oil specified by MIL-L-23699 above -54°C (-65°F) for lubrication oil specified by MIL-L-7808 Minimum to increase N2 above 83%: 40ºC (104°F) Oil Pressure Maximum: 95 psig (This limit may be exceeded during starts if oil temperature is below 21°C (70oF)) (for Airplanes with engine FADEC software previous to version B7.6 installed). 110 psig (This limit may be exceeded during starts if oil temperature is below 21oC (70oF)) (for Airplanes with engine FADEC software version B7.6 or later approved version installed). For takeoff and go-around the maximum limit is 115 psi, limited to 5 minutes. For aircraft which have complied with SBAE 30071-79-025 or equivalent, the maximum limit for takeoff and go around is 155 PSI, limited to 2 minutes. Minimum: 48 psig (N2 equal or above 88%) 34 psig (N2 below 88%) APU Limits (both models) Maximum RPM: 108% Maximum EGT: Steady State (Time limited to 5 minutes) 1323°F (717º C) Running (Normal) 1256°F (680° C) Airspeed Limits (EAS) Maximum Operating Limit Speed VMO: - 0 to 8,000 ft: 250 KEAS - 10,000 to 26,300 ft: 320 KEAS - 26,300 to 37,000 ft: 0.78 Mach - (Linear variation from 8,000 to 10,000 ft.) Maneuvering speed (VA): 202 KEAS Maximum flap extended speed (VFE): − Flaps 9° (Takeoff/Approach): 250 KEAS − Flaps 18° ( Takeoff) 200 KEAS (See Note 15) − Flaps 22°: 200 KEAS − Flaps 45° (Landing) : 145 KEAS Maximum landing gear extended speed (VLE): 250 KEAS Maximum landing gear operating speed (VLO): -VLO for retraction 200 KEAS -VLO for extension 250 KEAS C. G. Limits (landing gear extended) 595.6 to 619.4 inches (18.4% to 39.5% MAC) with 48,721 lbs. (22,100 kg). 595.6 to 619.4 inches (18.4% to 39.5% MAC) with 48,501 lbs. (22,000 kg). 592.5 to 619.4 inches (15.7% to 39.5% MAC) with 42,549 lbs. (19,300 kg). 590.1 to 623.3 inches (13.6% to 43.0% MAC) with 37,698 lbs. (17,100 kg). 588.3 to 623.3 inches (12.0% to 43.0% MAC) with 34,171 lbs. (15,500 kg). 588.3 to 623.3 inches (12.0% to 43.0% MAC) with 29,541 lbs. (13,400 kg). 608.6 inches (30% MAC) with 27,337 lbs. (12,400 kg). Revision 38 Page 10 of 40 T00011AT For aircraft modified 595.6 to 619.4 inches (19.0% to 38.5% MAC) with 50,044 lbs. (22,700 kg). according to SB 145-00-0032 595.6 to 619.4 inches (19.0% to 38.5% MAC) with 49,824 lbs. (22,600 kg). 592.5 to 619.4 inches (15.7% to 39.5% MAC) with 42,549 lbs. (19,300 kg). 590.2 to 623.3 inches (13.6% to 43.0% MAC) with 37,698 lbs. (17,100 kg). 588.3 to 623.3 inches (12.0% to 43.0% MAC) with 34,171 lbs. (15,500 kg). 588.3 to 623.3 inches (12.0% to 43.0% MAC) with 29,541 lbs. (13,400 kg). 608.6 inches (30% MAC) with 27,337 lbs. (12,400 kg). Straight linear variation between the points given. Moment due to landing gear retraction - 10,763 in-lbs. (-124 kgf-m) (the aircraft C.G. is moved forward with the retraction). Maximum Weights Ramp 48,721 lbs. (22,100 kgf) Takeoff 48,501 lbs. (22,000 kgf) Landing 42,549 lbs. (19,300 kgf) Zero fuel 39,462 lbs. (17,900 kgf) For aircraft modified Ramp 50,044 lbs. (22,700 kgf) according to SB 145-00-0032 Takeoff 49,824 lbs. (22,600 kgf) Landing 43,651 lbs. (19,800 kgf) Zero fuel 40,565 lbs. (17,900 kgf) Maximum Baggage 2,646 lbs. (1,200 kg) Fuel Capacity 1701.4 gallons (two tanks, 850.7 gallons each at +596.6 inches). Unusable fuel of 11.6 gallons (5.8 gallons for each tank). Serial Numbers Eligible 145002, 145003, 145048 and subsequent. A Brazilian Certificate of Airworthiness for Export endorsed as noted under “Import Requirements” must be submitted for each individual aircraft for which application for U.S. certification is made. 5. - Model EMB-135ER, (Transport Category), Approved July 15, 1999 Engine Two – Rolls Royce Corporation (See Note 16.) Models: AE 3007A1/3 or AE 3007A3 Fuel Brazilian Specification CNP-08/QAV1. ASTM Specification D-1655 JET A or JET A1 MIL-T-83133A JP-8. APU Sundstrand Aerospace Model T-62T-40C11 or T-62T-40C14 Limitations as stated in Sundstrand Doc. No. ESR 0921 and No. ESR 1112 Oil Engine: MIL-L-7808 or MIL-L-23699 APU: MIL-L-23699 or MIL-L-7808 Engine Model AE3007A1/3 Limits Operating Conditions Static Thrust (lb.) Rotor Speed (%) Temperature Interturbine (°C) -1000ft SL N1 N2 ITT Takeoff 7,580 7,462 100(2) 102.5(3) 948(1) (1738° F) Maximum Continuous 6,820 6,760 100 102.5 901 (1653° F) Ground 53.6 (min), 102.5 (max) Starting 800 (1472° F) (1) Time limited to 5 minutes. (2) 100 % N1 =8,700 rpm (3) 102.5 % N2 = 16,270 rpm Revision 38 Page 11 of 40 T00011AT Oil Temperature Maximum: 126°C (260°F) Normal oil temperature range: 21°C to 126°C (70 to 260°F) Minimum temperature for starting: above -40°C (-40°F) for lubrication oil specified by MIL-L-3699 above -54°C (-65°F) for lubrication oil specified by MIL-L-7808 Minimum to increase N2 above 83%: 40ºC (104°F) Oil Pressure Maximum: 95 psig (This limit may be exceeded during starts if oil temperature is below 21°C (70ºF)) (for Airplanes with engine FADEC software previous to version B7.6 installed). 110 psig (This limit may be exceed during starts if oil temperature is below 21oC (70oF)) (for Airplanes with engine FADEC software version B7.6 or later approved version installed). For takeoff and go-around the maximum limit is 115 psi, limited to 5 minutes. For aircraft which have complied with SBAE 30071-79-025 or equivalent, the maximum limit for takeoff and go around is 155 PSI, limited to 2 minutes. Minimum: 48 psig (N2 equal or above 88%) 34 psig (N2 below 88%) APU Limits (both models) Maximum RPM: 108% Maximum EGT: Steady State (Time limited to 5 minutes) 1323°F (717º C) Running (Normal) 1256°F (680° C) Airspeed Limits (EAS) Maximum Operating Limit Speed VMO: - 0 to 8,000 ft: 250 KEAS - 10,000 to 26,300 ft: 320 KEAS - 26,300 to 37,000 ft: 0.78 Mach - (Linear variation from 8,000 to 10,000 ft.) Maneuvering speed (VA): 202 KEAS Maximum flap extended speed (VFE): − Flaps 9° (Takeoff/Approach): 250 KEAS − Flaps 18° ( Takeoff) 200 KEAS (See Note 15) − Flaps 22°: 200 KEAS − Flaps 45° (Landing) : 145 KEAS Maximum landing gear extended speed (VLE): 250 KEAS Maximum landing gear operating speed (VLO): -VLO for retraction 200 KEAS -VLO for extension 250 KEAS C. G. Limits (landing gear extended) 518.4 to 538.7 inches (20.0% to 38.0% MAC) with 42,107 lbs. (19,100 kg). 518.4 to 538.7 inches (20.0% to 38.0% MAC) with _41,887 lbs. (19,000 kg). 517.7 to 538.7 inches (19.4% to 38.0% MAC) with 40,789 lbs. (18,500 kg). 514.7 to 538.7 inches (16.7% to 38.0% MAC) with 34,391 lbs. (15,600 kg). 512.7 to 538.7 inches (15.0% to 38.0% MAC) with 31,996 lbs. (14,500 kg). 512.7 to 538.7 inches (15.0% to 38.0% MAC) with 27,557 lbs. (12,500 kg). 521.2 to 538.7 inches (22.5% to 38.0% MAC) with 26,455 lbs. (12,000 kg). 529.7 inches (30% MAC) with 25,353 lbs. (11,500 kg). Straight linear variation between the points given. Revision 38 Page 12 of 40 T00011AT Moment due to landing gear retraction -10,155 in-lbs. (-117 kgf-m) (the aircraft C.G. is moved forward with the retraction). Maximum Weights Ramp 42,108 lbs. (19,100 kgf) Takeoff 41,887 lbs. (19,000 kgf) Landing 40,785 lbs. (18,500 kgf) Zero fuel 34,392 lbs. (15,600 kgf) Maximum Baggage 2,205 lbs. (1,000 kg) Fuel Capacity 1373.8 gallons (two tanks, 686.9 gallons each at +524.4 inches). Unusable fuel of 13.3 gallons (6.6 gallons for each tank). Serial Numbers Eligible 145145 and subsequent. A Brazilian Certificate of Airworthiness for Export endorsed as