Apu 10

Ensure APU EGT does not exceed _____ for more than 2 sec below 60% RPM

Ensure APU EGT does not exceed _____ above 60% RPM

Ensure APU NO-LOAD governed condition is reached within_____

Ensure APU EGT DOES NOT exceed ______ in NO-LOAD governed condition.

Ensure APU RPM stabilizes at _______ in NO-LOAD governed condition

Ensure APU EGT DOES NOT exceed _____ in loaded governed condition

Ensure APU RPM stabilizes at _______ in LOADED governed condition

APU May be operated as long as necessary as long as the ________

All APU runs will be made in accordance with T.O.s________ and ________

APU is monitored by______

APU RPM indicator indicates from _____

what causes APU auto shutdowns

Prior to shutdown, operate in "NO LOAD" governed condition for 2 min if

APU EGT gauge indicate

During APU start up, at 10% RPM _______and ______ are introduced

During APU start up, at 60% RPM the ________

During APU Start up, at 95% RPM the _________

Above ______ the APU is self sustaining

If APU drops below 95% the load control valve ________ and the APU will attempt auto restart

APU starter duty cycles

APU operator must remain in cockpit during ________

Door _______ must be _________ for APU operation

APU must be in ______ governed condition prior to start and shutdown

On board fire extinguishing system is the _______ means of fighting APU fire

what agent is used for fire suppression?

To "ARM" APU Fire suppression system pull the________

Always notify ________ if FIRE PULL handle illumination

The Fire Detection ________ and ________ battery switches must be on to power the system

The Fire Detection circuit is operationally checked _________ to APU start by depressing the FIRE DETECT/ BLEED AIR LEAK TEST BUTTON on the auxiliary light panel

APU fuel is supplied from the ________ by the _________

DC fuel pump operates at anytime when _______

During APU operation, Hydraulic system is powered by _________ PSI and a _______ GPM hydraulic pump mounted on the APU

The APU generator must be _______ or the ________ will not produce pressure

The Hydraulic Transfer Selector handle is used to select APU hydraulic system to _______or _______ aircraft hydro system

The APU Hydro system is capable of powering ______ aircraft power but at a _________ normal rate

Hydraulic Transfer Selector handle has ______

When Hydro Transfer Selector is in ___________, it prevents Hydro pressure from entering the aircraft hydro system and is reduced to 1000 PSI to facilitate cooling

When Hydro Transfer Selector is in ___________, it prevents Hydro pressure from entering the aircraft hydro system and is reduced to 3000 PSI and it should not be left in this position for prolonged time during operation due to inadequate cooling

__________ handle up or ________ handle down powers the aircraft hydro system at _________

Hydro Transfer selector must be in __________ prior to APU shutdown

Th APU Generator switch is capable of powering _______ electrical components

APU Generator switch can only be cycled ______

APU Generator switch must be in _______ prior to APU start and shutdown

Instrument Inverter must be in the ________ during APU operation

Aircraft has _________ battery switches

The external battery switch is located under panel ______

DC electrical system is powered by _________ 100-ampere converters (transformer rectifiers)

converters are power by the ____________ through the ___________ and _________ main buses

Airflow from the APU into the Bleed Air system __________ be stopped except by ____________ the APU

Airflow into the cockpit is controlled by the _________

RAM position ________

TEMP/PRESS switch in norm_______

BLEED AIR switch has ________ on cockpit air flow

The Main AIR SUPPLY switch is to be left in __________ at all times

TEMP/PRESS switch must be in __________ prior to APU start up and prior to APU shutdown

What two switches will cause a SERVICE AIR HOT LIGHT to illuminate?

APU

An illuminated left or right CONVERTER FAIL light on the caution annunciator panel indicates that the converter has?

APU

If the battery switch is in the power position and at least one of the CONVERTER lights is not illuminated, the __________ DC system is powered

ENG run

The TF-34 100A engine produces _____of thrust _______ of the Thrust is produced by high bypass fan air.

ENG

The ENG compressor provides ________ stages of axial flow compression

ENG

The high pressure turbine has _____ Stages, and the low pressure turbine has _______stages.

The oil system on the TF-34 ENG is a _____ sump

All components on the ENG are driven by the __________

ENG Start

Prior to engine ________, if TEMP is above ________, it will be necessary to _________ ENG

ENG run

If during the engine start, ITT does not rise within ________, move throttle to _______ and _______ the engine for a minimum of 30 seconds or until _________ ceases to exit from the engine.

ENG run

Elapsed time for the engine to reach idle speed shall not exceed ________ from the time throttle lever is set to ________ position

ENG run

Idle speed is approximately ______ core RPM

ENG run

The ENG may not reach idle within 80 seconds on the 1st start of the day due to ________________ loss from heating the casings, liners, and turbine.

ENG run

Prior to engine start, ensure the ENG OPER switch is in the ________ position

ENG Run

The start cycle is initiated by moving the throttle to the _______ position

ENG run

When the throttle is placed in the idle position, ensure there is a rise in ________ RPM and _____ pressure. The _____ _____ light should also come on.

Eng Run

Ensure light off occurs within______

Eng Run

Ensure HYD SYS indicator indicates ________ psi by _____ core RPM

Eng Run

Engine generator should come online at approximately _______core RPM

Eng Run

During the start sequence, TEMP should never exceed _______

Eng Run

Cold weather starts may result in oil pressure up to _______ . If pressure does not start to ______ after _____ , shutdown the engine

Eng Idle Limits

Max allowable TEMP at idle is _______

Eng Idle

Core RPM should be approximatley _______ at idle

Eng Idle

Oil pressure should be between _____ to _____ PSI

Eng Idle

Start Cycle light should be _______

MAX power

When running at maximum power, Temp should not exceed _______

MAX power

The engine cannot be operated at maximum power for longer than _________

MAX power

Core RPM should not exceed _______ at max power.

MAX power

Oil pressure should not exceed ________ PSI at max

MAX power

Fan speed should not exceed _______ at max

MAX power

Hydraulic pressure should not exceed ________ at max

ENG

The duty cycle for the engine STARTER system is __________ on, and _________ off, then continous

ENG

The engine start (ignition) circuit terminates at approximately ________ RPM

ENG

To deactivate the ignition system, you need to pull both ______ and ______ circuit breakers.

ENG

Placing the ENG OPER switch to IGN (L or R) will fire the ignitors for ________

ENG ECS

TEMP/PRESS switch should be in _______ position, prior to start up and shutdown of engines.

ENG ECS

The bleed air valves are controlled by the _______

ENG electric

Engine generators supply ______ power to both L and R main buses.

ENG electric

The left and right engine generators are controlled by the ___________ switch on the ELEC PWR control panel

ENG electric

If the L or R GEN lights illuminate during an engine run, you should place the ________ switch to ______ momentarily and then back to the ________ position

ENG fuel

Prior to starting aircraft engines, place the MAIN BOOST PUMPS switch on the FUEL management panel to the ________ position and the WING BOOST PUMPS switch to the _________ position

ENG fuel

Fuel flow to the engine starts by placing the throttle to the _______ position

ENG fuel

Pulling the FIRE PULL HANDLE will ______

ENG fuel

If an engine fails to light off, you should ______ the engine to clear out excess _______ prior to attempting a restart

ENG fuel

Failure to get a fuel drain after shutdown of an engine will more than likely result in an _________

ENG Hydro

The hydraulic servicing of the FWD and AFT hydraulic reservoirs is checked by ensuring the reservoir _______(green band) is visible beyond the end of the __________

ENG Hydro

Prior to starting engines, you should check the emergency brake accumulator for proper ________ pressure.

ENG Hydro

The HYDRAULIC TRANSFER SELECTOR handle must be in the _________ position prior to startup and shutdown of engines

ENG Hydro

The L or R HYD PRESS low light will illuminate when the_________ pressure falls below ________ PSI

ENG Hydro

The L or R HYD RES low light will illuminate when the fluid level in the hydraulic ________ drops below ________cubic inches

ENG start

Ensure full Hydraulic pressure at ?

ENG idle

Ensure hydro pressure is between ______