CPL - Cessna 172 Specifications

Diagrams (Fuel System)

Diagrams (Vacuum System)

Diagrams (Pitot-Static System)

Airframe

#NAME?

Wings (Ailerons)

#NAME?

Flaps

0

Empennage

#NAME?

Landing Gear

#NAME?

LHANDF

0

Speed (Engine)

0

Reasons for engine roughness, ground and flight

SMELL:
= spark plug fouling
= magnetos malfunctioning
= excessive fuel vapor (vapor lock)
= low fuel flow (engine-driven fuel pump malfunctioning)
= low oil pressure
= preignition or detonation (prolonged ground operations)

Oil

0

Quartz (Oil)

0

Propeller

0

Fuel Capacity

0

Fuel System

0

Fuel instrument

0

Annunciator Panel and LEFT/RIGHT Position (Fuel)

0

Weight and Gs (Normal)

0

Weight and Gs (Utility)

0

Electrical System

0

Alternator Control Unit (ACU) (Electrical System)

0

Power-off glide distance

1.5 times the altitude in whole thousand
1.5 x altitude = power-off glide distance (nm)
Example:
Given - 7,000ft.
1.5 x 7 = 10.5nm

Vacuum system

0

EP - EF during T/O roll

EP - EF after T/O

EP - EF during flight (restart procedure)

EP - Forced landing w/o engine

EP - forced landing w/ engine

EP - ditching

EP - Engine fire on ground

EP - Engine fire in flight

EP - electrical fire in flight

EP - cabin fire

EP - wing fire

Placards (locations)

12 placards:
1. Full view of the pilot (Day/Night/VFR/IFR)
2. Fuel selector
3. Fuel Cap
4. Flap control indicator
5. In baggage compartment for weight
6. Compass deviation card
7. Oil filter cap
8. Yoke control lock.
9. Near ASI for maneuvering speed 99KI

type of circuit breaker

#NAME?

De/Anti-icing equipements

0

Fuel auxiliary pump off during T/O and Landing

#NAME?

Magnetic Compass

#NAME?

Purpose of Vacuum Relief Valve

#NAME?

Purpose of Vacuum Manifold Valve

#NAME?