POH exam highlighted questions

Number on engines

1

Engine manufacturer

Lycoming

Engine model number(fuel injected)

IO-360-B4A

Takeoff power

180

Speed (RPM)

2700

Displacement (cubic inches)

361

Engine type (A)

Four cylinder, Direct drive

Engine type (B)

Horizontally opposed with fuel injection

Number of Propellers

1

Propeller manufacturer

Sensenich

Number of blades

2

Propeller diameter (inches)

Maximum 76, minimum 76

Propeller type

Fixed pitch

Fuel capacity total

50 gallons

Usable fuel

48 gallons

Fuel type

100 Green or 100LL Blue, Aviation grade

Oil capacity (US Quarts)

8

Maximum ramp weight

2558

Maximum takeoff weight

2550

Maximum landing weight

2550

Maximum weights in baggage compartment

200

Wing loading

15

Power loading

14.2

CAS

Calibrated airspeed

GS

Ground Speed

IAS

Indicated airspeed

TAS

True airspeed

Vfe

Maximum flap extension speed

Vne

Never exceed speed

Vno

Maximum structural cruising speed

Vs

stalling speed, minimum steady flight speed at which the airplane is controllable

Vso

stalling speed, minimum steady flight speed at which the airplane is controllable in the landing configuration

Vx

Best angle of climb speed, greatest gain of altitude in the shortest possible horizontal distance

Vy

Best rate of climb speed which delivers the greatest gain in altitude in the shortest possible time

ISA

The temperature at sea level is 15 degrees Celsius or 59 degrees F. The pressure at sea level is 29.92 inches Hg (1013.2 mb)

OAT

Outside air temperature

Pressure altitude

Altitude measured from standard sea level pressure by a pressure or barometric altimeter

EGT

Exhaust gas temperature

FFLOW

Fuel flow

RPM

Propeller speed

1

Pilot’s side

2

Co-pilot’s side

ADAHRS

Air data, altitude and heading reference system

CAS

Crew alerting system

EBD

Evolution backup display

EIS

Engine indication system

FOB

Fuel on board

GEA

Garmin engine/airframe processing unit

GIA

Garmin integrated avionics unit

GPS

Global positioning system

MFD

Multi-function display

PFD

Primary flight display

Accelerate-stop distance

The distance required to accelerate an airplane to a specified speed and, assuming failure of an engine at the instant that speed is attained, to bring the airplane to a stop

Basic empty weight

Standard empty weight plus optional equipment

Standard empty weight

Weight of a standard airplane including unusable fuel, full operating fluids and full oil

Unusable fuel

Fuel remaining after a runout test has been completed in accordance with governmental regulations

Usable fuel

Fuel available for flight planning

Maximum operating maneuvering speed at 2550 lb

113

Maximum operating maneuvering speed at 1917 lb

98

Maximum flap extension speed

102

Red line(Never exceed speed)

154

Yellow band(Caution range-smooth air only)

125 to 154

Green band(normal operating range)

50 to 125

White band(flaps down)

45 to 102

Max oil temperature

245 degrees F

Oil pressure minimum

25 PSI

Oil pressure maximum

115 psi

Propeller tolerance at ISA conditions

Not above 2340 RPM, not below 2240 RPM

Tachometer green arch(normal operating range)

500 to 2700 RPM

Tachometer red line(maximum)

2700 RPM

Oil temperature green band(normal operating range)

75 to 245 degrees F

Oil temperature red line(maximum)

245 degrees F

Oil pressure green band(normal operating range)

55 PSI to 95 PSI

Oil pressure yellow band(Caution range)(Idle)

25 PSI to 55 PSI

Oil pressure yellow band(ground warm-up)

95 PSI to 115 PSI

Oil pressure red line(minimum)

25 PSI

Oil pressure red line(maximum)

115 PSI

Alternator

70 AMPS

Emergency battery minimum

23.3 volts

Maximum ramp(lbs)

2558

Maximum weight(lbs)

2550

Maximum baggage(lbs)

200