|
|
 |
|
|
 |
|
|
|
 |
|
|
|
|
STATISTICS - O-470-11
|
|
Manufacturer:
|
Continental Motors
|
|
Model:
|
O-470
|
|
Engine Type:
|
Air Cooled Horizontally Opposed Piston Engine
|
|
Cylinders:
|
6
|
|
Bore:
|
5 in (127.0 mm)
|
|
Stroke:
|
4 in (101.6 mm)
|
|
Displacement:
|
471 cubic in. (7.8 L)
|
|
Length:
|
|
|
Width:
|
|
|
Height:
|
|
|
Dry Weight:
|
|
|
COMPONENTS
|
|
Valvetrain:
|
One Intake and One Exhaust Valve per Cylinder
|
|
Fuel System:
|
Bendix-Stromberg Model PS-5C Carburetor
|
|
Fuel Type:
|
80/87 octane aviation gasoline
|
|
Oil System:
|
Dry Sump
|
|
Cooling System:
|
Air-Cooled
|
|
PERFORMANCE
|
|
Power Output:
|
213 hp @ 2,575 rpm
|
|
Compression:
|
6:1
|
|
PRODUCTION MODELS
|
|
Variant
|
Horsepower Rating
|
Airframe Application
|
|
E165-2*
|
165 hp @ 2,050 rpm
|
Luscombe Model 11
|
|
E165-4*
|
165 hp @ 2,050 rpm
|
Boisavia B.602 Mercurey
|
|
E185-3*
|
205 hp @ 2,600 rpm
|
Ryan L-17A Navion
|
|
E185-5*
|
185 hp @ 2,300 rpm
|
Macchi M.B. 320
Muniz Casmuniz 52
Beechcraft Model A45T
|
|
E185-9*
|
205 hp @ 2,600 rpm
|
Ryan L-17A Navion
|
|
E225-2*
|
225 hp @ 2,650 rpm
|
Beechcraft T-34A Mentor
Beechcraft T-34B Mentor
Fletcher FL-23
Fuji LM-1 Nikko
|
|
E225-4*
|
225 hp @ 2,650 rpm
|
Beechcraft T-34A Mentor
Beechcraft T-34B Mentor
Fletcher FL-23
Fuji LM-1 Nikko
|
|
E225-8*
|
225 hp @ 2,650 rpm
|
Beechcraft T-34A Mentor
Beechcraft T-34B Mentor
Fletcher FD-25
Fletcher FL-23
Fuji LM-1 Nikko
|
|
E225-9*
|
225 hp @ 2,650 rpm
|
Beechcraft T-34A Mentor
Beechcraft T-34B Mentor
Fletcher FL-23
Fuji LM-1 Nikko
|
|
O-470-4*
|
225 hp @ 2,600 rpm
|
Beechcraft T-34A Mentor
|
|
O-470-11*
|
213 hp @ 2,600 rpm
|
Cessna L-19A
Cessna TL-19A
Cessna TL-19D
Cessna L-19E
Cessna O-1E Bird Dog
Cessna O-1F Bird Dog
Cessna O-1G Bird Dog
|
|
O-470-A*
|
225 hp @ 2,600 rpm
|
Cessna 180
Stinson 108
|
|
O-470-E*
|
225 hp @ 2,600 rpm
|
HAL HAOP-27 Krishak
|
|
O-470-G*
|
240 hp @ 2,600 rpm
|
Meyers 200
|
|
O-470-K*
|
230 hp @ 2,600 rpm
|
Cessna 182 to 182Q
Cessna 187
|
|
O-470-L*
|
230 hp @ 2,600 rpm
|
Cessna 182 to 182Q
Cessna 187
|
|
O-470-R*
|
230 hp @ 2,600 rpm
|
Cessna 182 to 182Q
Cessna 187
Cessna 188-230 AGpickup
DINFIA IA 53
|
|
O-470-S*
|
230 hp @ 2,600 rpm
|
Cessna 182 to 182Q
Cessna 187
|
|
O-470-T*
|
230 hp @ 2,400 rpm
|
Cessna 182 to 182Q
Cessna 187
|
|
O-470-U*
|
230 hp @ 2,400 rpm
|
Cessna 182 to 182Q
Cessna 187
|
|
IO-470-A
|
240 hp @ 2,600 rpm
|
Meyers 200A
|
|
IO-470-D
|
260 hp @ 2,625 rpm
|
Auster AOP.11
PAC FU-24 Fletcher
|
|
IO-470-E
|
260 hp @ 2,625 rpm
|
Cessna 210 Centurion
Cessna 210A Centurion
|
|
IO-470 J
|
225 hp @ 2,600 rpm
|
Beechcraft Model 35-33 Debonair
Beechcraft Model 35-A33 Debonair
Beechcraft Model 35-B33 Debonair
Beechcraft Model 35-C33 Debonair
Beechcraft Model E33 Bonanza
Beechcraft Model E33A Bonanza
Beechcraft Model E33B Bonanza
|
|
IO-470-L
|
260 hp @ 2,625 rpm
|
Beechcraft Model 55 Baron
Beechcraft T-42A Cochise
|
|
IO-470-N
|
260 hp @ 2,625 rpm
|
Beechcraft G33 Bonanza
|
|
IO-470-P
|
260 hp @ 2,600 rpm
|
SIAI_Marchetti NF.333 Riviera
|
|
IO-470-R
|
250 hp @ 2,600 rpm
|
Yeoman YA-1 250R Cropmaster
|
|
IO-470-S
|
260 hp @ 2,625 rpm
|
Cessna 210B Centurion
|
|
FSO-470-A**
|
260 hp @ 3,000 rpm
|
|
|
* denotes carbureted variants ** denotes helicopter model
|
|
|
|
|
The Beechcraft T-34 Mentor is a propeller-driven, single-engined, military trainer aircraft derived from the Beechcraft Model 35 Bonanza. The earlier versions of the T-34, dating from around the late 1940s to the 1950s, were piston-engined. These were eventually succeeded by the upgraded T-34C Turbo-Mentor, powered by a turboprop engine. The T-34 remains in service almost six decades after it was first designed.
|
|
|
|
|
STATISTICS - Beechcraft T-34A Mentor
|
|
Manufacturer
|
Beechcraft
|
|
Powerplant
|
One Continental O-470-4 Horizontally Opposed Air Cooled Piston Engine
|
|
Crew
|
Two
|
|
DIMENSIONS
|
|
Length
|
28 ft. 6 in.
|
|
|
Wing Span
|
33 ft. 5 in.
|
|
Height
|
9 ft. 7 in.
|
|
Empty Weight
|
2,960 lbs.
|
|
Loaded Weight
|
|
|
Gross Weight
|
4,400 lbs.
|
|
PERFORMANCE
|
|
Max Speed
|
191 mph
|
|
Cruise Speed
|
|
|
Combat Radius
|
|
|
Ferry Range
|
821 miles
|
|
Service Ceiling
|
20,000 ft.
|
|
Max Climb Rate
|
|
|
Thrust/Weight
|
|
|
ARMAMENT
|
|
None
|
|
|
|
|
