Palm Springs Pilots Association

 

Engine Continental TSIO-520-R

Fuel 100LL/100 minimum grade aviation gasoline

*Engine Limits Takeoff (5 min.) at 2700 r.p.m.,

36.5 in. Hg. mp. (310 hp. rating)

For all other operations 2600 r.p.m.,35 in. Hg.mp. (285 hp. rating)

Propeller and 1.

(a) McCauley D3A34C402/90DFA-10

Propeller Limits Diameter: not over 80 in., not under 78.5 in.

Pitch settings at 30 in. sta.: Low 12.4°, high 28.5°

Avoid continuous operation between 1850 and 2150 r.p.m.. Above 24 in. mp.

(b) Cessna spinner 1250419

(c) McCauley hydraulic governor C290D4/T2 or Woodward hydraulic

governor G210452

*Airspeed Limits (IAS) 1. Model T210N (S/N 21062954 and up)

(See NOTE 4 on Use of IAS) Never exceed 203 knots

Maximum structural cruising 168 knots

Maneuvering 130 knots

Flaps extended 115 knots

Landing gear operating speed 165 knots

Landing gear extended speed 203 knots

 

C.G. Range (Landing (+43.9) to (+52.0) at 4000 lbs.

Gear Extended) (+42.5) to (+53.0) at 3800 lbs.

(+37.0) to (+53.0) at 3000 lbs.

Straight line variation between points given

Moment change due to retracting landing gear (+2907 in.-lb.)

Empty Wt. C.G. Range None

*Maximum Weight 4000 lb. takeoff and flight

3800 lb. landing

4016 lb. ramp

No. of Seats 6 (2 at +34 to 46, 2 at +61 to +77, 2 at +101)

Maximum Baggage Reference weight and balance data

 

FUEL

Fuel Capacity 90 gal. (89 gal. usable), S/N 21062955 through 21064535

90 gal. (87 gal. usable), S/N 21064536 and up

two 45.0 gal. tanks in wings at +43

See NOTE 1 for data on unusable fuel.

Oil Capacity 10 qt. (-12.5); 8 qt. usable

CONTROL SURFACES

Control Surface Wing flaps Up 0° Down 30° +1°, -2°

Movements Ailerons Up 20° ±2° Down 15° ±2°

Elevator Up 23° ±1° Down 17° ±1°

Elevator tab Up 25° ±1° Down 10° ±1°

Rudder Right 24° ±1° Left 24° ±1°

(measured parallel to 0.0 W.L.)

Rudder Right 27° 13' ±1 Left 17° 13' ±1°

(measured perpendicular to hinge line)

Serial Nos. Eligible Model T210N: 

21062955 through 21063640 (1979 Model)