ZEN AIR CH 701 STOL AC Technical Details and Performance

Vocabulary flashcards covering the technical specifications, performance limits, and engine details of the ZEN AIR CH 701 STOL AC aircraft.

Length

$$20\,\text{feet}$$

Height

$$7.8\,\text{feet}$$

Wing Span

$$27\,\text{feet}$$

Wing Area

$$127\,\text{Sq ft}$$

Tail plane span

$$87.5\,\text{inches}$$

Main plane chord

$$58.9\,\text{inches}$$

Wheel track

$$68.8\,\text{inches}$$

Wheel base

$$57.5\,\text{inches}$$

Empty weight

$$209\,\text{Kg}\,(\text{460\,lb.})$$

Gross weight

$$436\,\text{Kg}\,(\text{960\,lb.})$$

Useful load

$$227\,\text{Kg}\,(\text{500\,lb})$$

Wing loading

$$37\,\text{Kg/sq m}\,(\text{7.5\,psi})$$

Fuel capacity (standard tank)

$42\,\text{Lt}\,$(Refer Section 10, Annex- 1)

Fuel capacity (Wing tank)

$$22\,\text{Lt. Each}$$

Inside cabin width

$$42\,\text{inches}$$

Aileron deflection

$$15\,\text{deg Up/Dn}\pm1\,\text{deg}$$

Flaps deflection

$$26\,\text{deg Up/Dn}+2\,\text{deg}$$

Elevator deflection -up

$$32\,\text{to}\;35\,\text{deg}$$

Elevator deflection-Dn

$$28\,\text{to}\;30\,\text{deg}$$

Rudder deflection Lt/Rt

$$23+2\,\text{deg}$$

Limit Load Factor -Flaps Up

$$+4\,\text{G}\;\text{to}\;-2\,\text{G}$$

Limit Load Factor-Flaps Dn

$$+2\,\text{G}$$

Design Load Factor

$$+6\text{G}\;\text{to}\;-3\text{G}$$

Stalling speed -Flaps

$$30\,\text{mph}$$

Stalling speed-Flaps Up

$$35\,\text{mph}$$

Flaps extended speed range

$$30\,\text{to}\;60\,\text{mph}$$

Never exceed speed with flaps down

$$60\,\text{mph}$$

Normal operating speed range

$$35\,\text{to}\;85\,\text{mph}$$

Caution speed range

$$85\,\text{to}\;110\,\text{mph}$$

Never exceed speed (Vne)

$$110\,\text{mph}$$

Take Off speed

$$40\,\text{mph}$$

Best Rate of Climb speed

$35\,\text{mph}\,$(flaps down)

Best Angle of climb speed

$40\,\text{mph}\,$(flaps up)

Best Rate of Descent speed

$40\,\text{mph}\,$(flaps up)

Cruise speed

$$80\,\text{mph}$$

Cross wind limit

$$15\,\text{mph}$$

Service ceiling

$$14000\,\text{feet Density Altitude}$$

Rotax 912 A Engine Type

Four stroke, four cylinder, horizontally opposed, spark ignition $80\,\text{BHP}$ engine.

Rotax 912 A Cooling

Cylinder heads are liquid cooled and cylinders are ram-air cooled.

Rotax 912 A Lubrication System

Dry Sump Forced Lubrication type.

Rotax 912 A Ignition

Dual Breaker-less Capacitor Discharge Ignition (CDI).

Rotax 912 A Carburetors

Two Constant Depression carburetors.

Rotax 912 A Propeller Drive

Via a reduction gear with integrated shock absorber and overload clutch.