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Question 1

Describe the airframe

Answer 1

All metal
4 place
single engine
high wing
tricycle landing gear
fuselage is semimonocoque
wings braced with wing spars
wings contain fuel tanks

Question 2

Describe the flight controls

Answer 2

Ailerons and elevator controlled by the yoke
Rudder and brakes controlled with rudder pedals
Control surfaces manually operated via cables and mechanical linkage

elevator trim is controlled with a control wheel

Question 3

Describe the wing flap system

Answer 3

on inboard trailing edge
single slot wing flaps
controlled (electrically) with a lever (10, 20, 30 degrees)
protected by a 10 amp circuit breaker

Question 4

Landing gear

Answer 4

Fixed tricycle with steerable nose wheel
shock absorption provided by tubular spring steel main struts and air/oil nose gear shock strut
each MAIN wheel has a hydraulically actuated disc brake

Question 5

Engine

Answer 5

Lycoming IO-360-L2A
horizontally opposed
4 cylinder
180hp @ 2700 RPM
air cooled
fuel injected
wet sump lubrication system (oil)
starter & belt driven alternator
dual magnetos
dual vacuum pumps
oil filter

Engine operation monitored by:
oil pressure and temp gauge
tachometer
exhaust gas temp gauge