# TCDS 5A3: Textron Aviation Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Textron Aviation Inc.
- Revision: 29
- Revised: November 27, 2017
- Product: Aircraft, Small Airplane
- Certification basis: CAR 3
- Registered aircraft: 257, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/42/66/4266f4df1768aab63004312d8741d5b359a9a4934c5d340d96f32d1976209ae4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AAE89317835ECFD9862581EF005D5294.0001
- Page: https://openairdocs.org/tcds/5A3

## Models (3)

As the data sheet lists them.

- 45 (Military YT-34)
- D45 (Military T-34B)
- A45 (Military T-34A; B-45)

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
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 -----
```

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- [AD 2004-25-51](https://openairdocs.org/ad/2004-25-51): Center wing section · Textron 45 (Military YT-34), A45 (Military T-34A, B-45) and D45 (Military T-34B). Effective Dec 21, 2004
- [AD 2001-13-18 R1](https://openairdocs.org/ad/2001-13-18-R1): Wing spar assembly · Textron 45 (Military YT-34), A45 (Military T-34A, B-45) and D45 (Military T-34B). Effective Mar 15, 2004
- [AD 2001-23-10](https://openairdocs.org/ad/2001-23-10): Flap Flex Shaft Assemblies · Textron 35, 35-33, 35-A33 and 60 more. Effective Dec 13, 2001
- [AD 99-05-13 R1 WD](https://openairdocs.org/ad/99-05-13-R1-WD): Withdrawal of AD 99-05-13 · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Jul 5, 2000
- [AD 91-17-01](https://openairdocs.org/ad/91-17-01): Elevator Trim Tab Actuators · Textron 35-33, 35-A33, 35-B33 and 40 more. Effective Nov 25, 1991
- [AD 89-05-02](https://openairdocs.org/ad/89-05-02): Elevator Control Fittings · Textron 35, 35-33, 35-A33 and 42 more. Effective Mar 24, 1989
- [AD 78-05-06](https://openairdocs.org/ad/78-05-06): Flexible Fuel Cells · Cessna 180, 182, 185 and 98 more. Effective Jun 30, 1978
- [AD 75-24-11](https://openairdocs.org/ad/75-24-11): Cable and Bellcrank Assembly · Textron A45 (Military T-34A, B-45) and D45 (Military T-34B). Effective Nov 28, 1975
- [AD 61-26-01](https://openairdocs.org/ad/61-26-01): Oil Pickup Hoses · Textron A45 (Military T-34A, B-45). Effective Jan 16, 1962
- [AD 2007-06-01](https://openairdocs.org/ad/2007-06-01) (historical): Front and rear horizontal stabilizer spars · Hawker Beechcraft 45 (Military YT-34), A45 (Military T-34A, B-45) and D45 (Military T-34B). Effective Apr 16, 2007
- [AD 2001-13-18](https://openairdocs.org/ad/2001-13-18) (historical): Wing Spar Assemblies · Hawker Beechcraft 45 (Military YT-34), A45 (Military T-34A, B-45) and D45 (Military T-34B). Effective Aug 16, 2001
- [AD 99-12-02](https://openairdocs.org/ad/99-12-02) (historical): Placard - Acrobatic Maneuvers · Hawker Beechcraft 45 (Military YT-34), A45 (Military T-34A, B-45) and D45 (Military T-34B). Effective Jul 9, 1999
- [AD 99-05-13](https://openairdocs.org/ad/99-05-13) (historical): Fuel Tank Selector · Beech B17B, B17L, B17R (Army UC-43H) and 107 more. Effective Apr 19, 1999
- [AD 72-22-01](https://openairdocs.org/ad/72-22-01) (historical): Landing Gear Uplock Rollers · Raytheon 35-33, 35-A33, 35-B33 and 49 more. Effective Oct 25, 1972
- [AD 62-24-01](https://openairdocs.org/ad/62-24-01) (historical): Stabilizer Spar · Hawker Beechcraft 45 (Military YT-34), A45 (Military T-34A, B-45) and D45 (Military T-34B). Effective Nov 26, 1962

## Registered aircraft by registry model (OpenAirDocs)

- [Beech A45](https://openairdocs.org/model/beech-a45): 162 aircraft (registry code 1152006)
- [Beech D-45](https://openairdocs.org/model/beech-d-45): 70 aircraft (registry code 1152012)
- [Beech A45 (T-34A)](https://openairdocs.org/model/beech-a45-t-34a): 5 aircraft (registry code 1152024)
- [Beech D-45 (T-34B)](https://openairdocs.org/model/beech-d-45-t-34b): 5 aircraft (registry code 1152020)
- [Beech-Nogle D-45](https://openairdocs.org/model/beech-nogle-d-45): 4 aircraft (registry code 1152013)
- [Beech-Parks BEECH-PARKS D-45](https://openairdocs.org/model/beech-parks-beech-parks-d-45): 4 aircraft (registry code 1152018)
- [Beech 45](https://openairdocs.org/model/beech-45): 2 aircraft (registry code 1152002)
- [Beech-Curtis D-45](https://openairdocs.org/model/beech-curtis-d-45): 1 aircraft (registry code 1152017)
- [Beech-Parks A45](https://openairdocs.org/model/beech-parks-a45): 1 aircraft (registry code 1152005)
- [Beech-Sarver D-45](https://openairdocs.org/model/beech-sarver-d-45): 1 aircraft (registry code 1152019)
- [Beech/Blackwell D D A-45](https://openairdocs.org/model/beech-blackwell-d-d-a-45): 1 aircraft (registry code 1152025)
- [Beech/Briggs A-45 (B-45)](https://openairdocs.org/model/beech-briggs-a-45-b-45): 1 aircraft (registry code 1152050)
- [Beech D-45 (T-34)](https://openairdocs.org/model/beech-d-45-t-34): 0 aircraft (registry code 1152021)
- [Beech-Novak D-45](https://openairdocs.org/model/beech-novak-d-45): 0 aircraft (registry code 1152011)
- [Beech-Stafford A45](https://openairdocs.org/model/beech-stafford-a45): 0 aircraft (registry code 1152007)
- [Beech/Blackwell Daniel D BEECH A-45](https://openairdocs.org/model/beech-blackwell-daniel-d-beech-a-45): 0 aircraft (registry code 1152027)

## STCs approved under this data sheet (184, first 50)

- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of  existing instrument panel lights dimmer control.. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc.
- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International Inc.
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc.
- [STC SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less.. Airwolf Filter Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc.
- [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International Inc.
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc.
- [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS  (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc.
- [STC SA01240SE](https://openairdocs.org/stc/SA01240SE): Installation of secondary voltage indication system. Visual Instruments LLC
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd.
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA01757WI](https://openairdocs.org/stc/SA01757WI): To allow the use of UL91 or UL94 (minimum) grade aviation fuel. Swift Fuels LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc.
- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc.
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc.
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine
- [STC SA01561CH](https://openairdocs.org/stc/SA01561CH): Installation of Hartzell Model PHC-(C, L)3YF-1RF/F8068(-2) three bladed propeller on Raytheon Aircraft Company (Beech) aircraft equipped with Teledyne Continental Motors six-cylinder engines. D'Shannon Products Ltd.
- [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance  Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA19GL](https://openairdocs.org/stc/SA19GL): Install Cleveland 7.00-8 wheels and brakes.. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc.
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV).. Genesys Aerosystems Inc.
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc.
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02430SE](https://openairdocs.org/stc/SA02430SE): Fabrication and installation of a camera housing. Airborne Sensor LLC
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc.
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA10081SC](https://openairdocs.org/stc/SA10081SC): Remove existing two piece wing spar web and replace with a single piece, heavier gauge aluminum web. Remove vertical stiffeners and horizontal reinforcement with heavier gauge aluminum and omit joggles in reinforcements.. T-34 Mentors LLC
- [STC SA10616SC](https://openairdocs.org/stc/SA10616SC): Modifies the main wing spar center section carry through. T-34 Mentors LLC
- [STC SA1450SW](https://openairdocs.org/stc/SA1450SW): Installation of Continental IO-520-B, -BA, or -BB engine and McCauley 2A36C23/84-B-0 or 3A32C76/82NB-2 propeller.. T-34 Mentors LLC
- [STC SA2460SW](https://openairdocs.org/stc/SA2460SW): Installation of inverted fuel and oil system. T-34 Mentors LLC
- [STC SA2677SW](https://openairdocs.org/stc/SA2677SW): Installation of Continental O-470-4 engine. T-34 Mentors LLC
- [STC SA2678SW](https://openairdocs.org/stc/SA2678SW): Installation of supplemental oil cooler. T-34 Mentors LLC
- [STC SA3755SW](https://openairdocs.org/stc/SA3755SW): Modification of the horizontal stabilizer front spar.. T-34 Mentors LLC
- [STC SA5549SW](https://openairdocs.org/stc/SA5549SW): Installation of Beech B-45 Stall modification kit.. T-34 Mentors LLC
- [STC SA5722SW](https://openairdocs.org/stc/SA5722SW): Installation of external stores racks. T-34 Mentors LLC
- [STC SA01831WI](https://openairdocs.org/stc/SA01831WI): To allow the use of UL91 (minimum) grade aviation fuel. Petersen Aviation Inc
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.. Garmin International Inc
- [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation

All 184: https://openairdocs.org/tcds/5A3/stcs.md

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