TCDS A-743

Page No. 1 2 3 4 5 6 7 8 9 10 11 Rev. No. 16 15 15 15 15 15 15 15 15 15 16   DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A-743 This data sheet which is part of Type Certificate No. A-743 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: The Boeing Company 6001 S. Air Depot Blvd Oklahoma City, OK 73135 Type Certificate Holder Record: Boeing Airplane Company Wichita Division transferred to The Boeing Company on April 2, 2014 I. Model A75L3, 2 PO-CLB, (Acrobatic Category) (S ee NOTE 7), approved June 3, 1941; 75 (Army PT-13), A75 (Army PT-13A, -13B, -13C), B75 (Navy N2S-5), E75 (Army PT-13D, Navy N2S-5, PT-13D/N2S-5), 2 PO-CLB, approved April 21, 1945 (Airplanes with the Model No. E75N1 marked on their na me plates are actually Model E75 (Army PT-13D, Navy N2S-5 or PT-13D/N2S-5) airplanes and are eligible for certification without correction of the name plates.) Engine Lycoming R-680-B4B 506 lbs. (-55) or Lycoming R-680-B4C 497 lbs. (-55) or Lycoming R-680-B4D 490 lbs. (-55) or Lycoming R-680-B4E 512 lbs. (-55) Fuel 65 minimum octane aviation gasoline Engine Limits For all operations, 2100 rpm (225 hp) Airspeed Limits (TIAS) Leve l flight or climb 125 mph Glide or dive 186 mph Propeller Limits S ee Item: 1(a)(b)(d)(e) C.G. Range (-1.0) to (+7.1) A-743 Revision 16 BOEING A75L3 75 (Army PT-13) A75 (Army PT-13A, -13B, -13C) B75 (Navy N2S-5) E75 (Army PT-13D, Navy N2S-5, PT-13D/N2S-5) A75J1 (Army PT-18) A75L300 A75N1 (Army PT-17, -17A; Navy N2S-1, -4) B75N1 (Navy N2S-3) D75N1 (Army PT-27) IB75A E75N1 April 25, 2023 Rev. 16 2 A-743   I. Model A75L3 (cont’d) Empty Weight C.G. Range (-1.5) to (+0.5) solo from either seat (-4.4) to (+0.5) placard in front cockpit: "Solo from rear seat only." When empty weight C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Ranges are not valid for non-standard arrangement or for crop duster or sprayer installations. Maximum Weight 2950 lbs. See NO TE 6 for 3200 lbs. maximum weight. Number of Seats 2 (+19) and (+55) Maximum Baggage 60 lbs. (+84) Fuel Capacity 46 gals. (-5) (One tank in upper wing center section) Oil Capacity 4.4 gals. (-26) Control Surface Movements Elevator tabs Up 15 ˚ Down 15 ˚ Elevator Up 24 ˚ Down 22 ˚ Aileron Up 23 ˚ Down 18 ˚ Rudder Right 30 ˚ Left 30 ˚ Serial Numbers Eligible 75001 and On and all Army and Navy serial numbers. Use manufacturer's number if available. Required Equipment See Items: 1(a) or (b) or (d) or (e); 105(a) or (b) or (c); 203(a) or (b); 204(a) or (b); 205(a) or (b); 401(a) or (b), 402 II. Model A75N1 (Army PT-17, -17A, Navy N2S-1, -4); B75N1 (Navy N2S-3, D75N1 (Army PT-27), 2 PO-CLB, (Acrobatic Category) (See NOTE 7), approved April 21, 1945 Engine Continental W-670-6A 465 lbs. (-55) or Continental W-670-6N 470 lbs. (-55) Fuel 65 minimum octane aviation gasoline Engine Limits For all operations, 2075 rpm (220 hp) Airspeed Limits (TIAS) Le vel flight or climb 125 mph Glide or dive 186 mph Propeller limits See Item 1(b), 1(d), or 1(e) C.G. Range (-1.0) to (+7.1) Empty Weight C.G. Range (-1.5) to +0.5) Solo from either seat (-4.4) to (+0.5) placard in front cockpit: "Solo from rear seat only." When empty weight C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Ranges are not valid for non-standard arrangements or for crop duster or sprayer installations. Maximum Weight 2950 lbs. See No te 6 for 3200 lbs. maximum weight. No. of Seats 2 (+19) and (+55) Maximum Baggage 60 lbs. (+84) A-743 3 Rev. 16 II. Model A75N1 (cont’d) Fuel Capacity 46 gals. (-5) (One tank in upper wing center section) Oil Capacity 4.4 gals. (-26) Control Surface Movements Elevator trim tabs Up 15 ˚ Down 15 ˚ Elevator Up 24 ˚ Down 22 ˚ Aileron Up 23 ˚ Down 18 ˚ Rudder Right 30 ˚ Left 30 ˚ Serial Numbers Eligible 75001 and On and all Army and Navy serial numbers. Use manufacturer's number if available. Required Equipment See Items: 1(b) or (d) or (e); 105(a) or (b) or (c); 203(a) or (b); 204(a) or (b); 205(a) or (b); 401(a) or (b); 402 III. Model A75J1 (Army PT-18) 2 PO-CLB, (Acroba tic Category) (See NOTE 7), approved May 28, 1945 Engine Jacobs R-755-7. See NOTE 4 for required modifications. Fuel 73 minimum octane aviation gasoline Engine Limits For all operations, 2000 rpm (225 hp) Airspeed Limits (TIAS) Le vel flight or climb 125 mph Glide or dive 186 mph Propeller Limits See item 1(b). C.G. Range (-1.0) to (+7.1) Empty Weight C.G. Range (-1.5) to +0.5) Solo from either seat (-4.4) to (+0.5) placard in front cockpit: "Solo from rear seat only." When empty weight C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Range s are not valid for non-standard arrangements or for crop duster or sprayer installations. Maximum Weight 2950 lbs. No. of Seats 2 (+19) and (+55) Maximum Baggage 60 lbs. (+84) Fuel Capacity 46 gals. (-5) (One tank in upper wing center section) Oil Capacity 4.4 gals. (-26) Control Surface Movements Elevator trim tabs Up 15 ˚ Down 15 ˚ Elevator Up 24 ˚ Down 22 ˚ Aileron Up 23 ˚ Down 18 ˚ Rudder Right 30 ˚ Left 30 ˚ Serial Numbers Eligible 75001 and On and all Army and Navy serial numbers. Use manufacturer's number if available. Required Equipment See Items: 1(b); 105(a) or (b) or (c); 203(a) or (b); 204(a) or (b); 205(a) or (b); 401(a) or (b); 402 Rev. 16 4 A-743   IV. *Model A75L300 (applies only to models listed under Sections I, II, and III wh en modified according to Mississippi Valley Aircraft Service, Clarksdale, MS, data or Mid-Continent Aircraft Corporation, Hayti, MO, data or equivalent) *Note: Models listed under Sections 1, II, or III when modified according to Brandt, Perkins & Brandt, Marysville, CA, data, eligible for certification with the following limitation but will retain original model designation: Engine Lycoming B680-E3 525 lbs. (-54) or Lycoming B680-E3A 535 lbs. (-55) or Lycoming B680-E3B 565 lbs. (-55) Fuel 87 minimum octane aviation gasoline Engine Limits Maximum, except takeoff 2200 rpm (285 hp) Takeoff (one minute) 2300 rpm (300 hp) Airspeed Limits (TIAS) Level flight or climb 125 mph Glide or dive 186 mph Propeller Limits See Item: 1(f) C.G Range Maximum Weights 2950 lbs. or less 3200 lbs. 3520 lbs. Fwd. C.G. Limit (-1.0) (-1.0) (-1.0) Aft. C.G. Limit (+7.1) (+4.5) (+4.5) Note: Straight line variation aft of C.G. limit above 2950 lbs. with Item 601 not installed. LBS. 3200 3100 3000 2900 -1 0 +1 2 3 4 5 6 7 8 INCHES Empty Weight C.G. Range (-1.3) to (-0.4) Solo from either seat. (-3.7) to (-0.4) When front cockpit placarded: “Solo from rear seat only.” When empty weight C.G. falls within this range, computation of critical fore and aft C.G. positions is unnecessary. Ranges are not valid for non-standard arrangements or for crop duster or sprayer installations. Maximum Weight Takeoff: NC Certification, 3200 lbs. ***NR certification 3520 lbs. (prior to October 11, 1950) Landing: 3200 lbs. Placards 1. “Intentional spins prohibited at weights above 2950 lbs.” with Item 601 not installed. 2. “Intentional spins prohibited” if elevator up-travel is more than 24°. ***3. For NR cer tification (prior to October 11, 1950): “Maneuvering speed at maximum weight not to exceed 115 m.p.h.” Required Equipment See Items: 1(f); 105(a) or (b) or (c); 204(a) or (b); 205(a) or (b); 401(a) or (b); 402   FRONT LIMIT AFT LIMIT A-743 5 Rev. 16 V. **Model IB75A (applies only to models listed under Sections I, II, or III when modified according to Inland Aviation Company, Los Banos, CA, data, or equivalent) **Note: Models listed under Sections I, II, or III modified accord ing to Air-Repair, Clarksburg, CA, data, eligible for certifi cation with the following limitations but will retain original model designation: Engine Pratt & Whitney T1B-3 (R-985-AN-1 or -AN-3) 668 lbs. or 669 lbs. (-48.5) Fuel 87 minimum octane aviation gasoline Engine Limits Maximum, except takeoff 1950 rpm (310 hp) Takeoff (one minute) 2300 rpm (450 hp) Airspeed Limits (TIAS) Le vel flight or climb 125 mph Glide or dive 150 mph Propeller Limits See Item: 1(g)(h). C.G. Range (-2.1) to (+4.0) Empty Weight C.G. Range (-5.3) to (-1.6) When empty weight C.G. falls within th is range, computation of critical fore and aft C. G. positions is unnecessary. Ranges are not valid for non-standard arrangements or crop duster or sprayer installations. Maximum Weight Takeoff: NC Certification, 3200 lbs ***NR certification (prior to October 11, 1950), 3520 lbs. Landing: 3200 lbs. Control surface movements Elevator Up 28° Down 22° Placards 1. "METO power not to exceed 310 hp (1950 rpm)" 2. Intentional spins prohibited" 3. "SOLO from rear seat only." ***4. NR certifica tion (prior to October 11, 1950): "Maneuvering speed at maximum weight not to exceed 115 mph." Required Equipment See Items: 1(g) or (h); 105(a) or (b) or (c); 203(a) or (b); 204(a) or (b); 205(a) or (b); 401(a) or (b); 402 ***All original certification in the Restricted Category afte r October 11, 1950, must be in accordance with CAR and CAM 8.   SPECIFICATIONS PERTINENT TO ALL MODELS Datum Leading edge of lower wing Leveling Means Leveling lugs provided in front cockpit Certification Basis Type Certificate No. 743 (CAR 4a) Production Basis None. Each aircraft manufactured subs equent to October 3, 1945, for civil use must, prior to original certification, satisfactorily pass a detailed inspection for workmanship, materials, and conformity with the approved technical data and a check of the flight characteristics by an FAA representative. Export Eligibility Eligible for export to all countries subject to the provisions of MOP 2-4, except as follows: Canada: Landplane - eligible Skiplane - not eligible Rev. 16 6 A-743   SPECIFICATIONS PERTINENT TO ALL MODELS (cont’d) Equipment A plus (+) or minus (-) sign preceding the weight of an item indicates net weight change when that item is installed. Approval for the installation of all items of equipment listed herein has been obtained by the aircraft manufacturer except those items preceded by four asterisks (****). The asterisks denote that approval has been obtained by other than the aircraft manufacturer. ***All original certification in the Restricted Category after October 11, 1950, must be in accordance with CAR and CAM 8. Propellers and Propeller Accessories 1. Propellers (a) Curtiss 55501-5 (eligible only with engines listed under Se ction I) ................................................. 57 lbs. ( -69) Static rpm at maximum permissible throttle setting: Not over 1750, not under 1650. No additional tolerance permitted. Diameter: Not over 102 in., not under 99 in. (b) Sensenich 98AA64 or 98AA66 or Fahlin D760-68-94 (including hub) or any other fixed pitch wood propeller meeting following limits which is eligible for the engine power and speed: ................................................................................. ...... 57 lbs. (-69) Static rpm at maximum permissible throttle setting: Not over 1950, not under 1725. No additional tolerance permitted. Diameter: Not over 98 in., not under 94 in. Reduce glide or dive speed to 150 mph. TIAS when using propeller with static rpm above 1775. Indexing: When this propeller is insta lled on Continental W-670-6A or -6N engine, the propeller must be indexed in the 90 degree position (blades at right angles to the crankthrow). (c) Deleted February 15, 1946. (d) McCauley with the following hubs and blades: (Eligible only when used with Continental W-670-6A, -6N (Army R-670) or Lycoming R-680-B4 engines.) Hubs Blades D-1093 SS-138-6 Or SS-135-6M 82 lbs. (-69) 41D5926 SS-135-6 82 lbs. (-69) Static rpm, at maximum permissible throttle setting: Not over 1925, not under 1575. No additional tolerance permitted. Pitch settings at 42 in. sta.: 9° to 11.7° Diameter: Not over 102 in., not under 100 in. When installed on Continental W-670-6A or -6N engine, this propeller must be indexed in the zero degree position (blades in line with the crankthrow) and the tachometer should be placarded as follows: "Avoid continuous operation between 1500 and 1650 rpm." (e) Hamilton Standard blades 11C1 (Navy 4350, 4350F, 4350F1) in hub 5404, or other eligible 2-way gr ound adjustable hub. (Eligible only with engines listed under Sections I an d II) ..................................................................................... ..... 87 lbs. (-69) Static rpm at maximum permissible throttle setting: Not over 1975, not under 1500. No additional tolerance permitted. Diameter: Not over 102 in., not under 100 in. On Continental W-670 engines, index in the zero degree (blades in line with crankthrow) position and placard tachometer as follows: "Avoid continuous cruise operation above 1900 rpm." (f) Hamilton Standard, constant speed, hub 2B20, blades 6135-9 through -16, with 1012G1 or 1012A1 governor, eligible on Lycoming R-680-E3, -E3A, and -E3B engines only ....................................................................................................... ........... 110 lbs. (-70) Pitch settings at 42 in. sta.: Low 7° for 6135-9 blades and 10° for 6135-16 blades Diameter: 8'3" max., 7' 7-1/8" min. allowable for repairs (g) Hamilton Standard, ground adjustable 5406-AL hub, 1C1-12 through 1C1-14 blades Eligible with P&W T1B3 engine only .......................................................................................... .... 99 lbs. (-67) Pitch setting at 42 in. sta.: 13.0° Diameter: 9'0" max., 8' 9-7/ 8" min. allowable for repairs A-743 7 Rev. 16 SPECIFICATIONS PERTINENT TO ALL MODELS (cont’d) (h) Hamilton Standard, controllable, 2D30 hub, 6101-12 through -20 blades ...... ................................ 163 lbs. (-67) Eligible with P&W T1B3 engine only. Pitch setting at 42 in. sta.: low 12-1/2°, high 16-1/2° Diameter: 9'0" max., 8' 3-7/8" min. allowable for repairs Engines and Engine Accessories - Fuel and Oil System 101. Starter and shaft (manual) (a) Eclipse M-2046-C (ACO 150976, Ty pe B-11) ............................................................................... 24 lbs. (-36) (on Models A75L3, 75, A75, B75, and E75 only) (b) Eclipse 94C, Model 1 (ACO 150976, Type B-11) .......................................................................... 24 lbs. (-44) (on Models A75N1, B75N1, D75N1 only) 102. Magneto, booster (a) Bendix - Scintilla 10-12290-1 (modified to fit airplane) (on Model 75 only) ................................... 4 lbs. (-11) (b) Bendix - Scintilla 10-15590-1 ......................................................................................... ................. 6 lbs. (-24) 103. Carburetor air cleaner, Air Maze 5AWA ................................................................................... ............... 6 lbs. (-33) 104. Oil dilution system ................................ ..................................................................... ............................. 2 lbs. (-34) 105. Oil tank (a) Plain type, Boeing-Wichita Dwg. 75-3001 or 75- 3028 ..................................................................... 6 lbs. (-26) (b) Hopper type, Boeing-Wichita Dwg. D75N1-3001 ............................................................................ 6 lbs. (-26) (c) Hopper type, Boeing-Wichita Dwg. E75N1-3002 .............................................................................. 8 lbs. (-26) Capacity: 4.76 gals. 106. Winter front cowl installation (Models A75N1, B75N1 and D75N1 only) ….............................................. 9 lbs. (-61) 107. Engine fire extinguisher system ................. ........................................................................ ....................... 21 lbs. (-20) Landing Gear and Floats (Main gear shock struts of the air-oil type and conforming to Boeing-Wichita Dwg. 75-2602 and main landing gear carry-through structures conforming to Boeing-Wichita Dwg. 75-2603 may be used on Model 75 (Army PT-13) only.) 201. Main landing gear wheels a. 24 in. streamline (Bendix or Hayes) with hyd. brakes and 24 in. 4-ply streamline tires.............................................................................................................. ................... 94 lbs. (-17) b. 24 in. streamline (Bendix or Hayes) with hyd. brakes and 8.90-12.50 4-ply low pressure tires. .............................................................................................................. ...................... 96 lbs. (-17) 202. Tail wheel (a) 8 in. smooth contour wheel and 6-ply tire.................................................................................. ......... 4 lbs. (+196) (b) 10 in. smooth contour wheel and 6-ply tire................................................................................. ........ 7 lbs. (+196) 203. Tail wheel gear (less wheel and tire) (a) Steerable ................................................................................................................. ......................... 18 lbs. (+190) (b) Free swivel with lock...................................................................................................... .................. 18 lbs. (+190) Electrical Equipment 301. Battery (a) 12 volt - 34 amp. hr. (5 hr. rate)......................................................................................... ............... 41 lbs. (-16) (b) 24 volt - 11 amp hr. (5 hr. rate).......................................................................................... ............... 34 lbs. (-16) 302. Interphone (a) Type TIC .................................................................................................................. ........................... 9 lbs. (-13) (b) Type RC-73 ................................................................................................................ ......................... 5 lbs. (+39) 303. (a) Wing (NAF 1021) (b) Wing (AN 3033) Interior Equipment 401. Seats (a) Metal (Boeing-Wichita Dwg. 75-3720) .............................................................................. 8 lbs. ( +26) & (+62) (b) Wood (Boeing-Wichita Dwg. B75N1-3610 ...................................................................... 13 lbs. (+26) & (+62) 402. Safety belts, Army Types B-6, B-10, B-11, and B-12 and NAF 1045-1 403. Fire extinguisher - portable (a) One quart carbon tetrachloride (Type A-2) ................................................................................. ........ 7 lbs. (+51) (b) Two Pound CO 2 (Type 2TA 2TB) ..................................................................................................... 6 lbs. (+4 6) Rev. 16 8 A-743   SPECIFICATIONS PERTINENT TO ALL MODELS (cont’d) Miscellaneous 601. Spoilers (spin strips) over leading edge upper and lower wings or lower wing only 602. (a) Blind flying hood..................................................................................................... ............................ 6 lbs. (+67) (b) Fling flying hood provisions............................................................................................... ................. 2 lbs. (+55) 603. Cockpit enclosure (Boeing). When this it em is installed, airplane not eligible for night flying and must be placarded as follows: "Close hatches before entering spin or dive." 604. Windshield extension...................................................................................................... .......................... 9 lbs. (+19) ****605. Cockpit enclosure (R.A.D. Air Devices, St. Louis, MO) ................................................................ ......... 47 lbs. (+50) ****606. Cockpit enclosure (Rawdon Dwg. PT-1050) .............................................................................. ............. 10 lbs. (+44) ****607. Sprayer and Duster Installations (all 75 series airplanes unless otherwise noted) (a) Goettl's Metalcraft Co., 2431 E. Buhanan, Phoenix, AZ. Duster installation kit approved, subject to inspection, when installed according to drawings and installation instru ctions furnished with kit. (b) Barrie Aeronautical Corp., Lee Airport, Lockport, NY. Model 20 dust hopper approved, subject to inspection, when installed according to Barrie Dwg. 001. (c) Transland Company, 223 California St., El Segundo, CA. Spray installation approved, subject to inspection, when installed in accordance with combination Spray Tank and Hopper Dwg. 1001, Dwgs. 1 through 10, and installation instructions: Airspeed Limits: Level flight or climb 100 mph TIAS Glide or dive 120 mph TIAS (d) Transland Company, 223 California St., El Segundo, CA. Duster installation approved, subject to inspection, when installed in accordance with combination Spray Tank and Hopper Dwg. 1001, Dwgs. 2001, 2004 and 2005 and installation instructions: Airspeed Limits: Level flight or climb 112 mph TIAS Glide or dive 134 mph TIAS (e) Rawdon Bros. Aircraft, Inc., Box 1135, Wichita, KS. Spray kit approved, subject to inspection, when installed according to Rawdon Report PT-6025. (f) Burnam Aviation Co., Arlington, TX. Six venturi spray kit approved, subject to inspection, when installed according to Burnam Dwgs. and Instructions B-1, B-2, B-3, RB-100, RB-101, RB-102, RB-1 and RB-2. Airspeed Limits: Level flight or climb 119 mph TIAS Glide or dive 143 mph TIAS (g) Independent Crop Dusting, Inc., Campbell, CA. ICD Model 600 rotary spray two unit kit approved, subject to inspection, when installed according to ICD Dwgs. 600-102 to -106 inclusive and installation instructions, and when mounted to the wing structure in accordance with ICD Dwg. 600-101 or ICD Mounting Kit No. 600-1B. Airspeed Limits: Level fli ght or climb 92 mph TIAS Glide or dive 110 mph TIAS (h) Airplane Vapor Spray Company, Route 3, Box 567b, Visalia, CA. Duster, spray or combination duster and spray kit approved, subject to inspection, when installed according to assembly Dwg. No 8904-A and P-100 through P-107, inclusive, and installation Dwgs. 1001 through 1008 inclusive. Kits include instructions for Pratt and Whitney R-985-AN3 engine installation and the airplane was eligible for NR certification prior to October 11, 1950, with the engine and limitations listed in Section V. (i) Ong Aircraft Corp., Kansas City, MO. Aero Dust King Model DS-12 kit approved, subject to inspection, when installed according to Ong Installation Instructions and DWg. DS-1200. (j) Airplane Dust and Spray Equipment Company, Kern County Airport, Bakersfield, CA. Sprayer pump and boom assembly kit, subject to inspection, when installed according to Dwg. 50320-207-75 and installation instructions. Airspeed Limits: Level fli ght or climb 92 mph TIAS Glide or dive 110 mph TIAS (k) Rawdon Seeder-Duster, Rawdon Bros. Aircraft Inc., Box 1135, Wichita, KS. Kit approved, subject to inspection, when installed according to Rawdon Report No. PT-7100. A-743 9 Rev. 16 SPECIFICATIONS PERTINENT TO ALL MODELS (cont’d) ****608. Metal cente r wing section, Goettls Metalcraft Company, 2431 E. Buchanan Street, Phoenix, AZ. Per Goettls Metalcraft Company Dwgs. Nos. G-2348-M, and/or G-2348-M modified. ****609. Wings ma de in accordance with Dwgs. 53040-1 through 53040-5, owned by Arvin-Wings, Inc., P.O. Box 668, Arvin, CA, comply with the structural requirements of CAR 8 when installed on 75 Series aircraft. This configuration was substantiated under Part 8 for the following weights and speeds: 3200 lbs. gross weight, takeoff and landing Vc = 110 mph V ne - 139 mph Airplanes equipped with these wings are eligible for certification under CAR 8 only. For certification at higher weights and speeds than those shown above, these airplanes should be flight tested in accordance with