TCDS A31SO

Page No. 1 2 3 4 5 6 7 8 9 10 11 12 Revision No. 14 11 11 11 11 11 11 11 11 11 14 13 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A31SO Revision 14 Embraer EMB-120 EMB-120RT EMB-120ER EMB-120FC EMB-120QC January 21, 2022 TYPE CERTIFICATE DATA SHEET NO. A31SO This data sheet which is part of Type Certificate No. A31SO pres cribes 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. Brig. Faria Lima, 2170 12227-901 São Jose dos Campos, SP Brazil Type Certificate Holder Record Yaborã Indústria Aeronaútica S.A. transferred the TC No A31SO to Embraer S.A. on January 1st, 2022. Embraer S.A. transferred TC No A31SO 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 November 2010. 1. - Model EMB-120 Brasilia (Transport Category), Approved July 9, 1985 Engines 2 Pratt & Whitney of Canada Ltd PW 115 Fuel MIL-T-5624 JP-4, JP-5 and ASTM D1655 Jet A, Jet A-1 and Jet B conforming to P&W specifications PWA522 or CPW204. See NOTE 4. Oil In accordance with P&W Specification PWA521 Type II (MIL-L-23699) or CPW202 (MIL-L-23699A). Engine Limits Shaft HP Jet Thrust (lbf) Torque % Prop. NP % Int-Turbine T6 Temp.°C (°F) Gas Gen.NH % Max. Take-off (5 min. max.) 1760 212 110 100 785 (1445) 100 Max. Continuous 1600 212 100 100 785 (1445) 100 Transient (20 sec. max.) 110 850 (1562) 102 Starting (5 sec. max.) 950 (1742) Max. Reverse 80 NOTE: The above engine limits are individual maximum operating limits and are not for setting engine power. Refer to AFM Section 4 for power setting data. Propeller Limits Condition Levers must in MIN RPM position during all ground operations, except when Ground Operation cleared for takeoff or during landing roll. Power Levers must remain at or below Flight Idle during all ground operations, except for brief (approximately 5 seconds) excursions as needed to maneuver the airplane Max. Operating Altitude S/N 12000004, 12000006 through 12000011 Enroute - 25,000 ft. (Bleed on) - 20,000 ft. (Bleed off) Revision 14 A31SO January 21, 2022 Page 2 of 12 S/N 12000012 and up Bleed On Bleed Off Enroute - EEC on 32,000 ft. 25,000 ft EEC off 25,000 ft 20,000 ft Temperature Operating S/N 12000004, 12000006 through 12000020 Limits Maximum ISA +32° C Minimum -54° C S/N 12000021 and up Maximum ISA +35° C Minimum -54° C Maximum Weight (mass) lb. kg Start of take-off 25,353 11,500 Landing 24,802 11,250 Zero Fuel 23,148 10,500 Number of Seats Maximum 34, including 1 pilot, 1 copilot, 1 attendant, 1 check pilot and 30 passengers. Maximum Baggage 1213 lb (See NOTE 7). 2. - Model EMB-120RT Brasilia (Transport Category), Approved October 23, 1986 Engines 2 Pratt & Whitney of Canada Ltd. PW 118 or 2 Pratt & Whitney of Canada Ltd. PW 118A or 2 Pratt & Whitney of Canada Ltd. PW118B or 1 Pratt & Whitney of Canada Ltd. PW 118 and 1 Pratt & Whitney of Canada Ltd. PW 118A (see AFM for operating limits) Fuel MIL-T-5624 JP-4, JP-5 and ASTM D1655 Jet A, Jet A-1 & Jet B conforming to P&W. specifications PWA522 or CPW204. See NOTE 4. Oil In accordance with P&W Specification PWA521 Type II (MIL-L-23699) or CPW202 (MIL-L-23699A). Engine Limits Shaft HP Jet Thrust (lbf) Prop Torque % NP % Int-Turbine, T6 Temp.°C (°F) Gas Gen.NH % Gas Gen.NL % PW 118 Max. Take-off(5 min. max.) 1980 230 110 100 816 (1500) 100 100 PW 118A Max Take-off(5 min. max.) 1980 230 110 100 816 (1500) 102 102 PW 118B Max Take-off(5 min. max.) 1980 230 110 100 816 (1500) 102 102 PW 118 Max Continuous 1800 230 100 100 800 (1472) 100 100 PW 118A Max Continuous 1800 230 100 100 800 (1472) 102 102 PW 118B Max Continuous 1800 230 100 100 800 (1472) 102 102 Transient (20 Sec. max.) 120 110 850 (1562) 102 102 Starting (5 sec. max.) 950 (1742) Max. Reverse 80 Revision 14 A31SO January 21, 2022 Page 3 of 12 NOTE: The above engine limits are individual maximum operating limits and are not for setting engine power. Refer to AFM Section 4 for power setting data. Propeller Limits Condition Levers must in MIN RPM position during all ground operations, except when Ground Operation cleared for takeoff or during landing roll. Power Levers must remain at or below Flight Idle during all ground operations, except for brief (approximately 5 seconds) excursions as needed to maneuver the airplane. Max. Operating Altitude Bleed On Bleed Off EEC on 32,000 ft 25,000 ft. EEC off 25,000 ft. 20,000 ft Temperature Operating Limits Maximum ISA +35° C Minimum -54° C S/N 12000021 and up Maximum ISA + 35°C Minimum -54°C Maximum Weight (mass) lb. kg Start of take-off 25,529 11,580 Landing 24,802 11,250 Zero Fuel 23,148 10,500 Number of Seats Maximum 34, including 1 pilot, 1 copilot, 1 attendant, 1 check pilot and 30 passengers. Maximum Baggage 1213 lb (See NOTE 7). 3. Model EMB-120ER Brasilia (Transport Category), Approved March 20, 1992 Engines 2 Pratt & Whitney of Canada Ltd. PW 118 or 2 Pratt & Whitney of Canada Ltd. PW 118A or 2 Pratt & Whitney of Canada Ltd. PW118B or 1 Pratt & Whitney of Canada Ltd. PW 118 and 1 Pratt & Whitney of Canada Ltd. PW 118A (see AFM for operating limits) Fuel MIL-T-5624 JP-4, JP-5 and ASTM D1655 Jet A, Jet A-1 and Jet B conforming to P&W specifications PWA522 or CPW204. See NOTE 4 Oil In accordance with P&W specification PWA521 Type II (MIL-L-23699) or CPW202 (MIL-L-23699A). Engine Limits Shaft HP Jet Thrust (lbf) Torque % Prop NP % Int-Turbine, T6 Temp. °C (°F) Gas Gen. NH % Gas Gen. NL % PW 118 Max Take-off (5 min. max) 1980 230 110 100 816 (1500) 100 100 PW 118A Max Take-off (5 min. max.) 1980 230 110 100 816 (1500) 102 102 PW 118B Max Take-off (5 min. max.) 1980 230 110 100 816 (1500) 102 102 PW 118 Max Continuous 1800 230 100 100 800 (1472) 100 100 PW 118A Max Continuous 1800 230 100 100 800 (1472) 102 102 PW 118B Max Continuous 1800 230 100 100 800 (1472) 102 102 Transient (0 sec. max.) 120 110 850 (1562) 102 102 Revision 14 A31SO January 21, 2022 Page 4 of 12 Starting (5 sec. max.) 950 (1742) Max. Reverse 80 NOTE: The above engine limits are individual maximum operating limits and are not for setting engine power. Refer to AFM Section 4 for power setting data. Propeller Limits Condition Levers must in MIN RPM position during all ground operations, except when Ground Operation cleared for takeoff or during landing roll Power Levers must remain at or below Flight Idle during all ground operations, except for brief (approximately 5 seconds) excursions as needed to maneuver the airplane Max. Operating Altitude Bleed On Bleed Off EEC on 32,000 ft 25,000 ft. EEC off 25,000 ft. 20,000 ft Temperature Operating Limits Maximum ISA +35° C Minimum -54° C Maximum Weight (mass) lb. kg Ramp 26,609 12,070 Takeoff 26,433 11,990 Landing 25,794 11,700 Zero Fuel 24,030 10,800 Number of Seats Maximum 34, including 1 pilot, 1 copilot, 1 attendant, 1 check pilot and 30 passengers. Maximum Baggage 1213 lb (See NOTE 7). 4. Model EMB-120FC Brasilia (Transport Category, Full Cargo version), Approved July 17, 2000. Engines 2 Pratt & Whitney of Canada Ltd. PW 118 or 2 Pratt & Whitney of Canada Ltd. PW 118A or 2 Pratt & Whitney of Canada Ltd. PW118B or 1 Pratt & Whitney of Canada Ltd. PW 118 and 1 Pratt & Whitney of Canada Ltd. PW 118A (see AFM for operating limits) Fuel MIL-T-5624 JP-4, JP-5 and ASTM D1655 Jet A, Jet A-1 and Jet B conforming to P&W specifications PWA522 or CPW204. See NOTE 4. Oil In accordance with P&W specification PWA521 Type II (MIL-L-23699) or CPW202 (MIL-L-23699A). Engine Limits Shaft HP Jet Thrust (lbf) Torque % Prop NP % Int-Turbine, T6 Temp. °C (°F) Gas Gen. NH % Gas Gen. NL % PW 118 Max Take-off (5 min. max) 1980 230 110 100 816 (1500) 100 100 PW 118A Max Take-off (5 min. max.) 1980 230 110 100 816 (1500) 102 102 PW 118B Max Take-off (5 min. max.) 1980 230 110 100 816 (1500) 102 102 PW 118 Max Continuous 1800 230 100 100 800 (1472) 100 100 PW 118A Max Continuous 1800 230 100 100 800 (1472) 102 102 PW 118B Max Continuous 1800 230 100 100 800 (1472) 102 102 Transient (0 sec. max.) 120 110 850 (1562) 102 102 Revision 14 A31SO January 21, 2022 Page 5 of 12 Starting (5 sec. max.) 950 (1742) Max. Reverse 80 NOTE: The above engine limits are individual maximum operating limits and are not for setting engine power. Refer to AFM Section 4 for power setting data. Propeller Limits Condition Levers must in MIN RPM position during all ground operations, except when Ground Operation cleared for takeoff or during landing roll Power Levers must remain at or below Flight Idle during all ground operations, except for brief (approximately 5 seconds) excursions as needed to maneuver the airplane Max. Operating Altitude Bleed On Bleed Off EEC on 32,000 ft 25,000 ft EEC off 25,000 ft 20,000 ft Temperature Operating Limits Maximum ISA +35° C Minimum -54° C Maximum Weight (mass) lb. kg Ramp 26,609 12,070 Takeoff 26,433 11,990 Landing 25,794 11,700 Zero Fuel 24,030 10,800 Number of Seats None. Approved for cargo only. No passengers allowed. Maximum Occupants Not to exceed 3, including pilot, copilot and 1 check pilot; Maximum Load on Cargo Compartment 8150 lb. Maximum Loading Distribution on Cargo Compartment CARGO COMPARTMENT STATION LIMITS X (ft) MAX. LOAD (lb) FLOOR LOAD LIMIT (lb/sqft) E1 From x=18.57 to x=26.41 2490 61 E2 From x=26.41 to x=35.20 2645 61 E3 From x=35.20 to x=44.71 2550 61 E4 From x=44.71 to x=49.05 1210 100 E1+E2 From x=18.57 to x=35.20 4400 61 E1+E2+E3+E4 From x=18.57 to x=49.05 8150 According to corresponding cargo compartment 5. Model EMB-120QC Brasilia (Transport Category, Quick Change Cargo version), Approved October 1, 2003. Engines 2 Pratt & Whitney of Canada Ltd. PW 118 or Revision 14 A31SO January 21, 2022 Page 6 of 12 2 Pratt & Whitney of Canada Ltd. PW 118A or 2 Pratt & Whitney of Canada Ltd. PW118B or 1 Pratt & Whitney of Canada Ltd. PW 118 and 1 Pratt & Whitney of Canada Ltd. PW 118A (see AFM for operating limits) Fuel MIL-T-5624 JP-4, JP-5 and ASTM D1655 Jet A, Jet A-1 and Jet B conforming to P&W specifications PWA522 or CPW204. See NOTE 4. Oil In accordance with P&W specification PWA521 Type II (MIL-L-23699) or CPW202 (MIL-L-23699A). Engine Limits Shaft HP Jet Thrust (lbf) Torque % Prop NP % Int-Turbine, T6 Temp. °C (°F) Gas Gen. NH % Gas Gen. NL % PW 118 Max Take-off (5 min. max) 1980 230 110 100 816 (1500) 100 100 PW 118A Max Take-off (5 min. max.) 1980 230 110 100 816 (1500) 102 102 PW 118B Max Take-off (5 min. max.) 1980 230 110 100 816 (1500) 102 102 PW 118 Max Continuous 1800 230 100 100 800 (1472) 100 100 PW 118A Max Continuous 1800 230 100 100 800 (1472) 102 102 PW 118B Max Continuous 1800 230 100 100 800 (1472) 102 102 Transient (0 sec. max.) 120 110 850 (1562) 102 102 Starting (5 sec. max.) 950 (1742) Max. Reverse 80 NOTE: The above engine limits are individual maximum operating limits and are not for setting engine power. Refer to AFM Section 4 for power setting data. Propeller Limits Condition Levers must in MIN RPM position during all ground operations, except when Ground Operation cleared for takeoff or during landing roll Power Levers must remain at or below Flight Idle during all ground operations, except for brief (approximately 5 seconds) excursions as needed to maneuver the airplane Max. Operating Altitude Bleed On Bleed Off EEC on 32,000 ft 25,000 ft. EEC off 25,000 ft. 20,000 ft Temperature Operating Limits Maximum ISA +35° C Minimum -54° C Maximum Weight (mass) lb. kg Ramp 26,609 12,070 Takeoff 26,433 11,990 Landing 25,794 11,700 Zero Fuel (see NOTE 11) 24,030 10,800 Maximum Number of Occupants With an original forward lavatory configuration, maximum 34 including 1 pilot, 1 copilot, 1 flight attendant, 1 check pilot and 30 passengers. With an original aft lavatory configuration, maximum 31 including 1 pilot, 1copilot, 1 flight attendant, 1 check pilot and 27 passengers. With a cargo configuration, maximum 03, 1 pilot, 1copilot and 1 check pilot, no passengers or flight attendant are allowed. Revision 14 A31SO January 21, 2022 Page 7 of 12 Maximum Load on Cargo Compartment When operating with passenger version, 1213 lb (see NOTE 7). When operating with cargo (class E) version: 7715 lb to comply with the requirement FAR 121 7500 lb to comply with the requirement FAR 135 Maximum Loading Distribution on Cargo (Class E) Compartment CARGO COMPARTMENT STATION LIMITS X (ft) MAX. LOAD (lb) FLOOR LOAD LIMIT (lb/sqft) E1 From x=20.5 to x=28.4 2490 61 E2 From x=28.4 to x=36.6 2645 61 E3 From x=36.6 to x=44.5 2550 61 E4 From x=44.5 to x=49.0 1210 100 E1+E2 From x=20.5 to x=36.6 4400 61 Data Pertinent to All Models Propeller and Propeller Limits 2- Hamilton Standard Model 14RF-9 Blade: RFC11E1-6A, RFC11M1-6A, RFC11N1-6A or RFC11U1-6A Diameter: 10.5 ft. nominal Pitch settings at STA 42 ins Feather 79.2° Flight fine 17.3° Ground fine -4.5° Full reverse -15.0° Propeller (Np) - Takeoff 1300 rpm (100%) - Max. Continuous 1300 rpm (100%) Revision 14 A31SO January 21, 2022 Page 8 of 12 Airspeed Limits (IAS) Maximum Operating Limit Speed (Vmo) Knots MPH Vfe (Flaps extended) Flaps 15° 200 230 Flaps 25° 150 175 Flaps 45° 135 156 VA (Maneuvering) 200 230 VLO (Landing gear operation) 200 230 VLE (Landing gear extended) 200 230 Minimum Crew 2 (Pilot and Copilot) Fuel Capacity 882 gallons (441 gallons each tank) Unusable fuel 7.4 gallons (3.7 gallons each tank) Oil Capacity 13.0 gal. (6.5 gal. in each engine). Datum 366.4" forward of the 66% wing chord line (frame 28). The 66% wing chord line is 0.67" aft of the rear jack points. Leveling Means Plumb from the upper part of the floor frame 28 using a mark in the lower part of the frame as a reference. Maximum Baggage (Passenger Configuration) 1213 lb Maximum Cargo Deleted. Previous note not applicable to US configuration Revision 14 A31SO January 21, 2022 Page 9 of 12 C.G. Limits EMB-120 and EMB-120RT 26000 24000 22000 20000 18000 16000 14000 0 10 4020 30 50 % MAC W EIGHT -lb 19.5% 21.0% 42.0% 43.5% 16.3% 13.4% 4.0% 6.0% 15873 lb (7200 kg)MOW 18297 lb (8300 kg) 22707 lb (10300 kg) MTOW=25353 lb (11500 kg) 19.8% MZFW=23148 lb (10500 kg) 22707 lb (10300 kg) MRW=25529 lb (11580 kg) 44.0%14330 lb-(6500 kg) MLW=24802 lb (11250 kg) TAKEOFF AND LANDING LIMITS IN-FLIGHT LIMITS (FLAPS AND GEAR UP) Revision 14 A31SO January 21, 2022 Page 10 of 12 C.G. Limits EMB-120ER, EMB-120FC and EMB-120QC • TAKEOFF AND LANDING LIMITS - - IN-FLIGHT LIMITS (FLAPS AND GEAR UP) 28000 23.3% 42.0% 12000 mad = MTOW = 26433 lb (11990 kg) = MRW = 26609 lb (12070 kg; 26000 MLW = 25794 lb (11700 kg) 43.5%: : 25353 Ib (11500 kg) 21.9% 11000 - MZFW = 24030 Ib = 24000- : (10900 kg) €19.5% 18.2% 22707 1b: 22707 Ib (10300 kg) 1(10300 kg) 10000 - 22000 13.4%; | 44.0%: 9000 - 20000 18297 Ib (8300 kg) 18000 8000 - 4.0% 1: • 6.0% 16000 715873 16 7000 - EMOV =(7200 kg) 14330 Ib (6500 kg) 14000 6000 - 10 20 30 40 50 % MAC Control Surface Movements Deflections measured normal to hinge lines: Main Rudder (hinge at 70% chord) Right 20° + 1° Left 17° + 1° Secondary Rudder (hinge at 86% chord) Right 15°+ 1° Left 13°+ 1° Up 20° + 1° Down 15° + 1° Up 25° + 1° Down 15° + 1° Flaps (Outboard and Inboard) Max. deflection 45° + 1° Flap (Middle) - Max. deflection 51° + 1° Elevator Tabs (Trim deflections) Up 3.3° + 0.5° or Down 22° + 1° 5.5° + 0.5° Right Aileron Tab Trim Deflections (Aileron Neutral) Up 11° + 1° Down 11° + 1° Aileron Automatic Tab 25° Up 14.7° + 1° 15° down 8.5° + 1° Revision 14 A31SO January 21, 2022 Page 11 of 12 Serial Numbers Eligible 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. Import Requirements 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 agreement, to identify any required statements by the exporting authority on the export certificate of airworthiness (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. Certification Basis Federal Aviation Regulation (FAR) Part 21, including Amendments through 21-49, effective September 10, 1979; FAR 25, including Amendments through 25-54, effective October 14, 1980; FAR 25.832, Amendment 25-56; Special FAR (SFAR) 27, including Amendments through 27-5 effective January 11, 1984, and FAR 36, including Amendments through 36-12 effective August 1, 1981 for EMB-120 and EMB-120RT, through 36-18 effective August 18, 1992 for EMB-120ER, through 36-22 effective October 13, 1999 for EMB-120FC and through 36-24 effective August 07, 2002 for EMB-120QC ; Exemption from FAR 25.571 (e) (2) as specified in Exemption No. 3722; Equivalent Safety Finding to FAR 25.783 (f) Cargo Door. Airplanes incorporating Embraer Service Bulletin No. 120-25-0220 comply with FAR 25.811(c)(2)(ii), Amendment 25-79, instead of FAR 25.811(e)(3), Amendment 25-54. Date of application for EMB-120; June 8, 1981. Date of application for EMB-120RT; August 20, 1986. Date of application for EMB-120ER; August 16, 1991. Date of application for EMB-120FC; December 2, 1999. Date of application for EMB-120QC; October 6, 2000. Part 26 – Continued Airworthiness and Safety Improvements for Transport Category Airplanes: Based on § 21.29(a) for new import TCs, or § 21.101(g) for changes to TCs, applicable provisions of Part 26 are included in the certification basis. For any future Part 26 amendments, the holder of this TC must demonstrate compliance with the applicable sections. Service Information Service bulletins, structural repair manuals, vendor manuals, aircraft flight manuals, and overhaul and maintenance manuals, which contain a statement that the document is ANAC approved, are accepted by the FAA and are considered FAA approved. These approvals pertain to the type design only. Ditching Compliance has been shown with the ditching requirements of FAR 25.801. When the operating rules require emergency ditching equipment, compliance with 25.1415 must be demonstrated. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. The "Basic Equipment Checklist," "Chart A," lists all the required and optional equipment and is included in the POH and ANAC approved AFM Revision 14 A31SO January 21, 2022 Page 12 of 12 NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight and loading instructions must be provided for each aircraft at the time of original certification. For loading procedures the Weight and Balance Manual WB120/701, must be followed. The certificated empty weight and corresponding center-of-gravity location must include system (undrainable) oil (not included in oil capacity) and unusable fuel (not included in usable fuel) as follows: Fuel: 48 lbs. at 348.8 in. Oil: 16 lbs. at 272.2 in. NOTE 2 The aircraft must be operated in accordance with the ANAC Approved Airplane Flight Manual. For cargo configuration required placards see also Embraer Service Bulletin nº 120-25-0245 NOTE 3 The Airworthiness Limitations are listed on Section 6 of document MRB-HI-200 “Maintenance Review Board Report”, as follows Part A - System & Powerplant Part B - Strucuture Part C - Life-Limited Components Part D - Critical Design Configuration Control Limitations (CDCCL) Part E - Fuel System Limitations NOTE 4 If fuel conforming to specifications PWA522 or CPW204 is not available it is permissible to use aviation gasoline MIL-G-5572 of all grades for a total time period not exceeding 150 hours during any overhaul period. JET B or JP-4 fuel should only be used when no other fuel is available. NOTE 5 Aircraft S/N 12000004 and 12000006 through 12000021, inclusive, have been converted to the model EMB-120RT by the accomplishment of the Embraer Service Bulletin nº 120-72-0001. NOTE 6 The engine Pratt & Whitney PW-118A may be installed in accordance with the Embraer Service Bulletin nº 120-072-0002. NOTE 7 The passenger baggage compartment maximum capacity may be increased to 1540 lb thru accomplishment of SB 120-25-0205. All pax aircraft S/Ns 12000281, 12000286 through 12000288, and 12000290 and on are factory modified for 1540 lb. NOTE 8 All EMB-120RT S/Ns may be converted into the model EMB-120ER by the accomplishment of Embraer Service Bulletin nº 120-00-0008. NOTE 9 All EMB-120ER S/Ns may be converted into the model EMB-120FC by the accomplishment of Embraer Service Bulletin nº 120-25-0245 NOTE 10 All EMB-120ER S/Ns may be converted into the model EMB-120QC by the accomplishment of Embraer Service Bulletins nº 120-25-0244 and 120-25-0243. NOTE 11. All EMB-120QC operating cargo must comply with Embraer Service Bulletins nº 120-25-0252 and 120-25-0253. ...END...