Computer Testing Supplement for IA.indb - Aviation Supplies ...

V - Model 210D (cont’d)
Empty wt. C.G. range None
*Maximum weight 3100 lb.
No. of seats 4 (2 at +36, 2 at +70)
Maximum baggage Reference weight and balance data
Page 6 of 43 3A21
Fuel capacity 65 gal. (63.4 gal. usable); two 32.5 gal. tanks in wings at +48.
See Note 1 for data on unusable fuel.
Oil capacity 12 qt. (-19.4), 6 qt. usable.
See Note 1 for data on undrainable oil.
Control surface Wing flaps Up 0° Down 40° +1°, -2°
movements Ailerons Up 21° ±2° Down 14°30' ±2°
Elevator Up 26°30' ±1° Down 18° ±1°
Elevator tab Up 20° +1°, -0° Down 10° +1°, -0°
Rudder Right 24° ±1° Left 24° ±1°
(measured parallel to 0.0. W.L.)
Serial Nos. eligible Model 210D: 21058221 through 21058510 (1964 Model)
VI - Model 210E, 4 PCLM (Normal Category), Approved September 17, 1964
Engine Continental IO-520-A
*Fuel 100/130 minimum grade aviation gasoline
*Engine limits For all operations, 2700 rpm. (285 b.hp.)
Propeller and 1. (a) McCauley E2A34C64/90AT-8
propeller limits Diameter: not over 82 in., not under 80 in.
Pitch settings at 36 in. sta.:
low 10.3°, high 25.8°
(b) Cessna spinner 1250411
(c) Woodward hydraulic governor D210452
2. (a) McCauley E2A34C73/90AT-8
Diameter: not over 82 in., not under 80 in.
Pitch settings at 36 in. sta.:
low 10.3°, high 25.8°
(b) Cessna spinner 1250415
(c) Woodward hydraulic governor D210452
*Airspeed limits (CAS) Never exceed 225 mph. (196 knots)
Maximum structural cruising 190 mph. (165 knots)
Maneuvering 134 mph. (116 knots)
Flaps extended 110 mph. ( 96 knots)
Landing gear operating speed 160 mph. (139 knots)
Landing gear extended speed 160 mph. (139 knots)
C.G. range (landing (+39.2) to (+46.6) at 3100 lb.
gear extended) (+33.0) to (+46.6) at 2250 lb. or less
Straight line variation between points given.
Moment change due to retracting landing gear (+2456 in.-lb.)
Empty wt. C.G. range None