TCDS 5A3

Page No. 1 2 3 4 5 6 7 8 9 10 Rev. No. 29 22 22 22 22 22 22 22 23 28 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION 5A3 Revision 29 Textron Aviation 45 (YT-34) A45 (T-34A, B-45) D45 (T-34B) November 27, 2017 TYPE CERTIFICATION DATA SHEET NO. 5A3 This data sheet which is a part of Type Certificate No. 5A3 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 Textron Aviation Inc. One Cessna Boulevard Wichita, KS 67215 Type Certificate Holder Record: Beech Aircraft Corporation transferred to Raytheon Aircraft Company on April 15, 1996 Raytheon Aircraft Company transferred to Hawker Beechcraft Corporation on March 26, 2007 Hawker Beechcraft Corporation transferred to Beechcraft Corporation on April 12, 2013 Beechcraft Corporation transferred to Textron Aviation Inc. on October 12, 2016. I. Model 45 (Military YT-34), 2 PCLM (Acrobatic Category), approved July 17, 1950 Engine Continental E-225-8 Fuel 80 minimum octane aviation gasoline Engine limits Takeoff (one minute) 2600 rpm (220 hp) For all other operations 2450 rpm (205 hp) Airspeed limits Maneuvering 171 mph (148 knots) True Ind. Maximum structural cruising 175 mph (152 knots) True Ind. Never exceed 252 mph (219 knots) True Ind. Flaps extended 125 mph (109 knots) True Ind. 5A3 2 Rev. 29 I. Model 45 (cont'd) Landing gear extended 125 mph (109 knots) True Ind. C.G. range (landing (+87.0) to (+89.5) at 2750 lbs. gear extended) (+83.2) to (+90.3) at 2540 lbs. (+82.0) to (+90.3) at 2475 lbs. or less Straight line variation between points given. Landing gear retraction moment +610 in.-lb. 81 82 83 84 85 86 87 88 89 90 91 2300 2400 2500 2600 2700 2800 IN. LB. Empty weight C.G. Range None Maximum weight 2750 lbs. Number of seats 2 (1 at +84, 1 at +135) Maximum baggage 100 lb. (+162) Fuel capacity 44 gal. (two 22 gal. wing tanks at +80) See Note 1 for unusable fuel. Oil capacity 12 qt. (+46) for O-470-13 or O-470-13A engine 10 qt. (+26) for IO-470-N engine (Kit 45-9002) See Note 1 for undrainable oil. Control surface movements Wing flaps Down 30 Aileron tab Fixed Aileron Up 20 Down 20 Elevator tab Up 10 Down 20 Elevator Up 25 Down 15 Rudder tab Right 15 Left 15 Rudder Right 30 Left 30 Rudder anti-servo 1/2 for 1 rudder movement Serial nos. eligible G-3 through G-6 Required equipment Items 1(a), 101(a) and (b), 102, 105(a), 201(a), 202, 205, 206, 301(a), 302(a), 303(a), 304(a), 401(a), 402(a), 601 II. Model A45 (Military T-34A, B-45), 2 PCLM (Acrobatic Category), approved September 21, 1953 Engine Continental O-470-13, O-470-13A, or IO-470-N (see Item 107(a)) Fuel 80 minimum octane aviation gasoline for O-470-13 and O-470-13A engine 100/130 minimum octane for IO-470-N engine (kit 45-9002) Engine limits For all operations O-470-13 or O-470-13A 2600 rpm (225 hp) IO-470--N (Kit 45-9002) 2625 rpm (260 hp) Rev. 29 3 5A3 II. Model A45 (cont'd) Airspeed limits Maneuvering 171 mph (148 knots) True Ind. Maximum structural cruising 175 mph (152 knots) True Ind. Never exceed 252 mph (219 knots) True Ind. Flaps extended 125 mph (109 knots) True Ind. Landing gear extended 125 mph (109 knots) True Ind. C.G. Range (landing (+87.6) to (+89.0) at 2950 lb. gear extended) (+84.1) to (+89.8) at 2750 lb. (+84.1) to (+90.3) at 2600 lb. Straight line variation between points given. Landing gear retraction moment +600 in.-lb. 81 82 83 84 85 86 87 88 89 90 91 2500 2600 2700 2800 2900 3000 IN. LB. Empty weight C.G. range None Maximum weight 2950 lbs. Number of seats Two (2) (1 at +84, 1 at +135) Maximum baggage 100 lb. (+162) Fuel capacity 44 gal. (two 22 gal. wing tanks at +80) See NOTE 1 for unusable fuel Oil capacity 12 qt. (+46) for O-470-13 or O-470-13A engine 10 qt. (+25) for IO-470-N engine (kit 45-9002) See NOTE 1 for undrainable oil Control surface movements Wing flaps Down 30 Aileron tab Up 10 Down 10 Aileron Up 20 Down 20 Aileron servo 1/2 for 1 aileron movement Elevator tab Up 10 Down 20 Elevator Up 20 Down 15 Rudder tab Right 15 Left 15 Rudder Right 25 Left 25 Rudder anti-servo 1/2 for 1 rudder movement Serial numbers eligible G-7 and On, CG-1 and On. See NOTE 3 Required equipment Items 2, 102, 104(b), 105(b), 106(a)(b), 201(b) or (c), 202, 205, 206, 301(b), 302(b), 303(b), 304(b), 305 or 402(b), 401(b), 601. 5A3 4 Rev. 29 III. Model D45 (Military T-34B), 2 PCLM (Utility Category), approved March 9, 1960 Engine Continental O-470-4 Fuel 80 minimum octane aviation gasoline Engine limits For all operations 2600 rpm (225 hp) Airspeed limits Maneuvering 171 mph (148 knots) True Ind. Maximum structural cruising 175 mph (152 knots) True Ind. Never exceed 252 mph (219 knots) True Ind. Flaps extended 125 mph (109 knots) True Ind. Landing gear extended 125 mph (109 knots) True Ind. C.G. range (landing (+87.8) to (+89.5) at 2985 lbs. gear extended) (+84.1) to (+90.0) at 2775 lbs. (+84.1) to (+90.3) at 2675 lbs. Straight line variation between points given. Landing gear retraction moment +600 in.-lb. 81 82 83 84 85 86 87 88 89 90 91 2500 2600 2700 2800 2900 3000 IN. LB. Empty weight C.G. range None Maximum weight 2985 lbs. Number of seats Two (2) (at +87, 1 at +138) Maximum baggage 100 lb. (+162) Fuel capacity 50 gal. (two 25 gal. wing tanks at +80) See NOTE 1 for unusable fuel Oil capacity 12 qt. (+46) See NOTE 1 for data on unusable oil Control surface movements Wing flaps Down 30 Aileron tab Up 10 Down 10 Aileron Up 20 Down 20 Aileron servo 1/2 for 1 aileron movement Elevator tab Up 10 Down 20 Elevator Up 20 Down 15 Rudder tab Right 15 Left 15 Rudder Right 29 Left 25 Rudder anti-servo 1/2 for 1 rudder movement Rev. 29 5 5A3 III. Model D45 (cont'd) Serial numbers eligible BG-1 and On. Prior to civil certification of T-34B airplanes which have been operated by the military, they must be modified in accordance with Beech Dwg. 45-000060 (Kit No. 45-326). Required equipment Items 2, 102, 104(b), 105(b), 106(a)(c), 201(b) or (c), 202, 205, 206, 301(c), 302(b), 303(b), 304(b), 305, 401(c), 601. Specifications Pertinent to all Models Datum 88.1 in. forward of jack pads on front spar. Leveling means Two screws in bulkhead aft of baggage door. Plumb bob is used to level. Certification Basis Model 45 - Part 03 of the Civil Air Regulations as amended to November 1, 1949, no amendments. Model A45 (T34A), B45, and D45 - Part 03 of the Civil Air Regulations as amended to November 1, 1949, including Amendments 3-1, 3-2, and 3-3. Application for Type Certificate dated June 17, 1948. Type Certificate No. 5A3 issued July 17, 1950, obtained by the manufacturer under delegation option procedures. Production Basis Production Certificate No. 8. Delegation option manufacturer No. CE-2 authorized to issue airworthiness certificates under delegation option provisions of Part 21 of the Federal Aviation Regulations. Propeller and Propeller Accessories (excepting Deicing Equipment) 1. Beech constant speed propeller (Model 45) (a) Hub B200-119, blades B200-244-88 56 lb. (+ 2) (For interchangeable blade models see Prop. Spec. P-867, Note 6) Diameter: not over 88 in., not under 86-1/4 in. Pitch settings at 33 in. sta.: low 10, high not under 31 or (b) Hub 215-111, blades 215-207-88 Diameter: not over or under 88 in. 67 lb. (+ 2) Pitch settings at 33 in. sta.: low 13, high not under 34 (c) Propeller governor Flight Research 31A-45 7 lb. (+55) (d) Pitch control motor installation 5 lb. (+ 8) (e) Propeller spinner Beech 35-900026 3 lb. (+ 0) 2. Beech constant speed propeller (Models A45, D45) (a) Hub 278-100-1, blades 278-207-88 or 278-208-84 69 lb. (+ 2) Diameter: not over 88 in., not under 82 in. for 278 -207-88 not over 84 in., not under 82 in. for 278 -208-84 Pitch settings at 33 in. sta.: low 11-1/2, high not under 30 for 278-207-88 low 12-1/2, high not under 30 for 278-208-84 (b) Woodward propeller governor 210060 3 lb. (+40) 5A3 6 Rev. 29 Specifications Pertinent to all Models (cont’d) Propeller and Propeller Accessories (excepting Deicing Equipment) (cont’d) 3. Hartzell constant speed propeller installation (A-45, T-34A, B-45) (installed per Beech Kit 45-9002) (a) Hartzell BHC-L2YF-4F/FC8468 AR (Use actual weight change) Diameter: 84 in., not over or under 84 in. Pitch setting at 30 in. sta.: Low 13.5  1.0 High 30.0  1.0 (b) Hartzell A2297P spinner assembly (Use actual weight change) (c) Woodward Governor B216688 (Use actual weight change) Engine and Engine Accessories - Fuel and Oil Systems 101. Fuel pump (Model 45) (a) Engine driven, Thompson TF-1100-2 1 lb. (+40) and (b) Electric fuel booster, Thompson TF-36700-1 3 lb. (+80) 102. Carburetor air cleaner 1 lb. (+11) 103. Vacuum pump, AN6111-1 or ARO A-505-CDD (Model 45) 6 lb. (+41) 104. Starter (a) Beech 35-369005 (Model 45) 19 lb. (+42) (b) Bendix 756-10 or 756-22 (Models A45, D45) 19 lb. (+44) (c) 24 volt Prestolite MHJ4002 or Teledyne-Continental Motors 634433 (A45, T34A, B45) (installed per Beech Kit 45-9002) 105. Oil radiator (a) Harrison D20062 (Model 45) 6 lb. (+38) (b) Harrison 8521583 with fittings or replacement core assembly 6 lb. (+38) under Harrison P/N 8522827, 8517698 or 8517694 (Models A45, D45) (c) Harrison B528220 (TCM 627392) (installed per Beech Kit 45 -9002) 5 lb. (+11) 106. Fuel pump (a) Engine driven, Lear Romec RG9080D (Models A45, D45) 1 lb. (+40) (b) Two electric booster, ADEL 29306, 29306-1, 28549, 28549-1, 3 lb. ea. (+76) 26900-3, 26900-7, 56880 or Beech 45-921506 or Pesco 122723-120-01 (Model A45). Pressure setting must be adjusted to 11 to 12 psi. (c) One electric booster ADEL 29172 or Pesco 122723-113-01 (Model D45) 3 lb. (+81) (d) Engine driven, Teledyne Continental Motors (Model A45, T34A, B45) 626062, -1, -2, or -3 or 635135-3A1 2 lb. (+39) (e) One electric in-line booster, Duke 4401-00-1 installed per Beech Kit 45-9003. 3 lb. (+86) (Model A45, T34A, B45) Beech FAA Approved Airplane Flight Manual Supplement 131098 dated January 31, 1973 (Model A45, T34A, B45) 107. Optional engine installation (A45, B45, T34A) (installed per Beech Kit 45-9002) (a) Teledyne-Continental Motors IO-470-N (Spec. 12A) (Use actual weight change) Engine installed per Beech Dwg. Kit 45-9002. Note: The below items of equipment are required to be used when Item 107(a) is installed (per Beech Kit 45-9002) and in lieu of the corresponding items listed. Items not replaced and still listed are applicable as required: 3(a), 3(b), 3(c), 104(c), 105(c), 106(d), 106(e), 306(a), 307(a), 401(d) Rev. 29 7 5A3 Specifications Pertinent to all Models (cont’d) Landing Gear 201. Two main wheel-brake assemblies 6.50-8 Type III (a) Goodyear Model L6.50-8 HBDM 20 lb. (+102) Wheel assembly 530869 Brake assembly 9530367 (b) Goodyear Model L6.50-8HBM 20 lb. (+102) Wheel assembly 9531161 Brake assembly 9531138 (c) Goodyear Model L6.50-8HBM 20 lb. (+102) Wheel assembly 9531319 Brake assembly 9531281 202. Two main wheel 4 or 6-ply rating tires, 6.50-8 Type III with regular tubes 25 lbs. (+102) 205. One nose wheel, 5.00-5 Type III Goodyear Model L5NBD 4 lb. (+12) 206. One nose wheel 4-ply rating tires 5.00-5 Type III with regular tubes 6 lb. (+12) Electrical Equipment 301. Generators (a) 35 a. Delco-Remy P/N 1101880 (Model 45) 18 lb. (+42) (b) 50 a. Eclipse 1345-3-A or 30824-1-A (Model A45) 15 lb. (+32) or (c) 75 a. Eclipse 1298-1 or Beech 45-910203-1 (Models A45, D45) 23 lb. (+31) (Eclipse 1298-1 must be modified per Beech Dwg. 45-910203) 302. Batteries (a) 12 v. 34 a. hr. with box (Model 45) 42 lb. (+52) (b) 24 v. 24 a. hr. with box (Model A45, D45) 56 lb. (+54) 303. Landing lights (a) Two General Electric 4522 (Model 45) 1 lb. ea. (+77) (b) Two AN3129-4523 (Models A45, D45) 1 lb. ea. (+77) 304. Generator control (a) Delco-Remy 1118325 (Model 45) 2 lb. (+48) (b) Navy 17R21 or Eclipse 1589-1, 1042-16 or 1042-17 3 lb. (+67) (Models A45, D45) 305. Inverter: AN3499-1 or Eicor X3499-1 (Model A45) 6 lb. ea. (+247) 1-100A-115D-7 or E-1616-2 (Model D45) 6 lb. ea. (+ 55) (Required with electric gyro instruments) 306. Alternator (a) 50A. Prestolite 8403 or TCM 634692 (A45, T34A, B45) (Use actual weight change) (Installed per Beech kit 45-9002) 307. Voltage Regulator (a) Beech 60-389017-1 (A45, T34, B45) (installed per Beech Kit 45-9002) 2 lb. (+48) 5A3 8 Rev. 29 Specifications Pertinent to all Models (cont’d) Interior Equipment 401. (a) FAA Approved Airplane Flight Manual (AFM) dated July 17, 1950 (Model 45). (b) DMCR Approved AFM dated September 21, 1953, March 18, 1955, August 6, 1956; July 23, 1957 (P/N 45-590177) or December 8, 1961 (P/N 45-590177) (Model A-45). (c) DMCR Approved AFM dated March 8, 1960 (Model D45). (d) Beech FAA Approved AFM Supplement 131122 dated January 26, 1973, or later. 402. Ballast (a) Beech 45-410374 (15 lb. max.) (Model 45) (Use actual weight change) (b) Beech 45-400200 (12 lb. max) (Model A45) (Use actual weight change) (not to be used when Item 305 installed) Miscellaneous (not listed above) 601. Safe Flight stall warning indicator. 602. Oil pickup tube modification per Beech Dwg. 45-001057 (Model A45 only) Airplane Flight Manual Supplement dated August 14, 1961, required. -1 lb. (+43) NOTE 1. Current weight and balance report together with list of equipment included in certificated empty weight and loading instructions when necessary must be in each aircraft at the time of original certification. The certificated empty weight and corresponding c.g. location must include unusable oil and fuel as follows: Model 45 Unusable fuel - 2 lb. (+84) not included in fuel capacity. Unusable oil - 5 lb. (+36) not included in oil capacity. Model A45 Unusable fuel - 10 lb. (+84) not included in fuel capacity. Unusable oil - 3 lb. (+41) not included in oil capacity. Model D45 Unusable fuel - 5 lb. (+84) not included in fuel capacity. Unusable oil - 3 lb. (+41) not included in oil capacity. Model A45, T34A, and B45 with Beech Kit 45-9002 installed (Item 107) Unusable fuel - 36 lb. (+84) not included in fuel capacity. Unusable oil - 3 lb. (+21) not included in oil capacity. NOTE 2. The following placard must be displayed in front of and in clear view of the pilots: Model 45: "Acrobatic category airplane. Operate in accordance with FAA Approved Flight Manual." Model A45: "Acrobatic category airplane. Operate in accordance with DMCR Approved Flight Manual." Model D45: "Utility category airplane. Operate in accordance with DMCR Approved Flight Manual. Intentional spins prohibited. No acrobatic maneuvers approved except those listed in the Airplane Flight Manual." Rev. 29 9 5A3 NOTE 3. Model T-34A and B-45 aircraft manufactured by the Canadian Car and Foundry Company (covered in Section II of this specification) must have a fireproof identification plate bearing the manufacturer's name, model designation, serial number, and type certificate number securely attached to the aft fuselage structure in an accessible location between fuselage stations 240 and 280. Prior to civil certification of T-34A airplanes, which have been operated by the military, or B-45 airplanes manufactured for export, they must be modified in accordance with Beech Dwg. 45-000060 (Kit No. 45-322A). Serial numbers eligible, 34-1 through 34-125, and corresponding USAF or RCAF serial numbers are as follows: MFR's S/N USAF or RCAF S/N MFR's S/N USAF or RCAF S/N MFR's S/N USAF or RCAF S/N 34-1 52-8253 34-43 52-8270 34-85 53-4116 34-2 52-8254 34-44 52-8271 34-86 53-4117 34-3 52-8255 34-45 52-8272 34-87 53-4118 34-4 24201 34-46 52-8273 34-88 52-4119 34-5 24202 34-47 52-8274 34-89 53-4120 34-6 24203 34-48 52-8275 34-90 53-4121 34-7 24204 34-49 52-8276 34-91 53-4122 34-8 24205 34-50 52-8277 34-92 53-4123 34-9 24206 34-51 52-8278 34-93 53-4124 34-10 24207 34-52 52-8279 34-94 53-4125 34-11 24208 34-53 52-8280 34-95 53-4126 34-12 24209 34-54 52-8281 34-96 53-4127 34-13 24210 34-55 52-8282 34-97 53-4128 34-14 24211 34-56 52-8283 34-98 53-4129 34-15 24212 34-57 52-8284 34-99 53-4130 34-16 24213 34-58 52-8285 34-100 53-4131 34-17 24214 34-59 52-8286 34-101 53-4132 34-18 24215 34-60 53-4091 34-102 53-4133 34-19 24216 34-61 53-4092 34-103 53-4134 34-20 24217 34-62 53-4093 34-104 53-4135 34-21 24218 34-63 53-4094 34-105 53-4136 34-22 24219 34-64 53-4095 34-106 53-4137 34-23 24220 34-65 53-4096 34-107 53-4138 34-24 24221 34-66 53-4097 34-108 53-4139 34-25 24222 34-67 53-4098 34-109 53-4140 34-26 24223 34-68 53-4099 34-110 53-4141 34-27 24224 34-69 53-4100 34-111 53-4142 34-28 24225 34-70 53-4101 34-112 53-4143 34-29 52-8256 34-71 53-4102 34-113 53-4144 34-30 52-8257 34-72 53-4103 34-114 53-4145 34-31 52-8258 34-73 53-4104 34-115 53-4146 34-32 52-8259 34-74 53-4105 34-116 53-4147 34-33 52-8260 34-75 53-4106 34-117 53-4148 34-34 52-8261 34-76 53-4107 34-118 53-4149 34-35 52-8262 34-77 53-4108 34-119 53-4150 34-36 52-8263 34-78 53-4109 34-120 53-4151 34-37 52-8264 34-79 53-4110 34-121 53-4152 34-38 52-8265 34-80 53-4111 34-122 53-4153 34-39 52-8266 34-81 53-4112 34-123 53-4154 34-40 52-8267 34-82 53-4113 34-124 53-4155 34-41 52-8268 34-83 53-4114 34-125 53-4156 34-42 52-8269 34-84 53-4115 5A3 10 Rev. 29 NOTE 4. Parks Industries, Ltd., Inc. Kit PI-326 for conversion of military surplus Beech T-34A and T-34B airplanes is an alternate to: (a) The Beech Kit 45-322A for the Model T-34A (B-45) airplanes, and (b) The Beech Kit 45-326 for the Model T34B airplanes. Parks Kit PI-326 is the same as the Beech Kits 45-322A and 45-326, except for the following: (a) STC SA5549SW is required in lieu of the rudder aileron interconnect system on the T-34A and T-34B. In accordance with STC SA5549SW the elevator down spring change installed by Beech Kit 45-326 is not used on T-34B airplanes. (b) T-34A (B-45) airplanes with PI-326 kits installed require FAA Approved Parks Industries AFM dated December 1, 1983, and titled Beech Model A45 Landplane (T-34A) (B-45) Serial No. G-7 and On, CG-1 and On. (c) The T-34B airplanes with PI-326 kits installed require FAA Approved Parks Industries AFM dated December 1, 1983, and titled Beech Model D45 landplane (T-34B) Serial No. BG-1 and On. ----- END -----