Study Guide

Empty Weight

Max Takeoff Gross Weight

Max Shaft Horsepower

Shaft torque at 100% indicated

Thrust at SL - zero speed

Prop in low pitch (degrees from reference pane)

Prop Feathered (degrees from ref plane)

Altitude which 100% torque is available

Oil Capacity

Time which oil level must be serviced within

Time which oil readings are most accurate

Red OIL PX annunciator with PCL above idle

Red Oil PX annunciator with PCL at Idle

Amber OIL PX annunciator with PCL above idle

Amber Oil PX annunciator with PCL at Idle

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Power turbine output shaft speed

Prop operating speed

Propeller size and material

Mechanical overspeed governer w/ PMU

Mechanical overspeed governer w/ no PMU

Ground mode at idle

Flight Mode at Idle

Np at idle above 10,000 ft MSL

PMU automatically switches to 28 VDC

PMU auto abort start if light off has not occured within

PMU will abort auto start attempt

PMU will go offline ( amber dashes in IOAT and ITT counters, Removal of ITT pointers, PMU Fail)

N1 acceleration rate at which PMU will abort auto start

Starters and Ignitors are deenergized during auto start

PCL may be advanced during auto start

Max increase in power with PMU off

Max decrease in power with PMU off 550 SHP

Usable fuel through single point refueling

additional fuel available using over the wing refueling

Ramp slope at which fuel is vented overboard through pressure relief valve

Amount and time for auto fuel balancing system before transfer valve closes

FUEL BAL annunciator illuminates and auto balance system shuts off

Red FUEL PX annunciator is activated

Amber L FUEL LO and R FUEL LO annunciators are activated

Number of Fuel Probes

Fuel Level outer fuel probes reads to...

Middle fuel probe leads to...

Inner fuel probe reads to...

Minimum time provided by the fuel system for inverted flight

Start/generator provides

Battery provides

M

Auxiliary battery provides:

Battery volts at which external power should not be connected

Time provided by the battery to power all items on the battery bus

Number of hydraulic master cylinders for brake system

Hydraulic system fluid capacity

Pressure relief valve for primary hydraulic system

Normal Hydraulic pressure

Minimum hydraulic pressure needed to power components

Amber HYDR FL LO annunciator illumintaes for primary hydraulic reservior

Amber EHYD PX LO annunciator illuminates for the emergency accumulator

Restricted flow rate to the emergency acculmulator

Hydraulic fluid loss limit by the hydraulic fuse

How long does it take to normally extend/retract the gears?

PCL mid-range position

Nose wheel turn limits (160 deg total)

Takeoff flaps extension

Landing flaps extension

Speed brake extension

Aileron travel limits

Elevator travel limits

Rudder travel limits

TAD provides further trim in addition to weight off wheels

Standby attitude indicator accuracy with complete power loss

Accelerometer display range

Accelerometer tolerance

Allowable difference between accelerometers in front and rear cockpit (notify maintenence if higher)

Stall AOA

Normal approach speed AOA (1.3X) stall speed

Maximum endurance AOA (white diamond)

Maximum range AOA (white triangle)

Optimum approach airspeed (amber donut)

Optimum approach speed decrease versus fuel used

Stick shaker above stall speed

Stick shaker AOA

Windscreen and front transparency bird strike limits

Ejection seat capability up to what altitude and what airspeed?

Ejection seat/ pilot seperation and parachute deployment delay

Seat/pilot seperation pending completion of TCTO...

Altitude for mountainous terrain which the MOR handle should be used

Emergency oxygen system supply duration

Minimum oxygen cylinder pressure at 70 deg F

m

Front seat ejection delay with ISS both

SSK lowered after man/seat seperation

Inflow valve (bleed air) automatically closed with A/C on

Amber DUCT TEMP annuciator (ECS)

G-suit safety valve

Temperature range that is maintained with the TEMP CONTROL set to auto

Heat exchanger bypass valve is moved to full close (ECS)

If the DEFOG switch is placed to OFF, how long can it take the electrically controlled defog valve to close?

Altitude which 3.6 +/- 0.2 pressure differential is reached

Cockpit pressure altitude at 31,000' MSL

Amber CKPT ALT annunciator illuminates if cockpit altitude rises above?

Red CKPT PX annunciator illuminates when?

Fresh air valve is automatically closed when?

RMU cursor automatically reverts to the top field

RMU direct tuning and transponder memory recall

UHF/VHF & UHF backup memory capacity

NAV memory capacity

ELT transmission duration (battery powered)

EADI unusual attitude declutter > +30 deg NH, -20 deg NL, 65 deg bank

EADI unusual attitude recovery (red chevrons)

EHSI VOR CDI 1 dot indicates how many degrees off course?

EHSI localizer & glideslope 1 dot (width of localizer/glideslope)

EHSI GPS EN ROUTE, APR ARM, APR ACT 1 dot

NACWS upward/downward pointing triangle with vertical separation displayed

NACWS upward/downward pointing triangle

NACWS rectangle is

TAS normal mode range

TAS above/below mode range

TAS tracking range/altitude

GPS can store up to how many flight plans?

Max GPS waypoints per flight plan?

When will the GPS will flash prior to beginning of turn anticipation for waypoint

IDARS memory level when Green FDR MAINT illuminates

Aux bat capacity when light does not illuminate during aux bat test

Aural tones are inaudible during engine start until engine gas generator indication is above what?

OBOGS warm-up time when OBOGS fail light will be inhibited

Amber OBOGS TEMP annunciator

Oxygen concentration in NORMAL from sea level to 15,000' MSL

Oxygen concentration in NORMAL from 15,000' to 31,000' MSL

Oxygen concentration in MAX

Maximum weight in baggage compartment

Main gear tire pressure (max)

Main gear tire pressure

Nose wheel tire pressure

Acceptable external power voltage limits for off-station engine starts

Wind speed which aircraft should be moved to hanger