Mooney Executive 21 1968 - Propeller; Landing Gear

and fuel- inj ected engine with a wet- sump lubricating sys-
tem.
Model (Lycoming).
................ .I8- 360-A1A
Rated Horsepower @ 2700 RPM ............. 200
............................
Bore 5.125 IN.
..........................
Stroke 4.375 IN.
..................
Displacement 361.0 CU. IN.
.....................
Compression Ratio 8.7: 1
...............
Fuel Injector, Bendix RSA- 5-AD1
.............
Magnetos, Scintilla S4LN- 200 Series
PROPELLER
TYPE: Constant- speed hydraulically- controlled propeller
with a single- acting governor.
..........
Model (Bartzell)
Hc-
62~ K- 1~/'7666 A- 2
..........................
Diameter .94 IN.
Blade Angle (@ 30 IN. STA):
...........................
Low. 14O 1' o0
.............
High ..........'. :.
290 f 2'
LANDING GEAR
TYPE: Manually retracted tricycle gear with rubber shock
discs, steerable nose wheel, and hydraulic disc brakes.
Wheel Base
.................. 5 FT 11-9/16 IN.
Wheel Tread. .............. : .... 9 FT 314 IN.
Tire Size:
Nose .......................... 5.00 x 5
Main ................... .'-. ...... 6. OOx 6
Tire Pressure:
Nose
........................... 49 PSI
Main
........................... 30 PSI