Bold Face Flashcards by mitch Kennedy

Warning associated with the ejection checks?

Canopy must be closed and locked
Notify the other occupant as soon as possible
Make a conscious effort to adopt the ejection posture
Simultaneous ejection of both seats is inadvisable. Captain to wait for other occupant to eject first

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Emergency egress on the ground, and warning associated with it

SEAT PIN - IN THE SEAT
LEG RESTRAINTS - RELEASED
SEAT HARNESS - RELEASED
OXY MASK HOSE - DISCONNECT
MIC TEL - DISCONNECT
PSP - DISCONNECT
CANOPY - OPEN

WARNING - Eject if circumstances dictate however do not eject if; Canopy is not closed and locked, occupants are not strapped in, Seat pins or CFS pins are in

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Warning, note, Caution associated with gliding checks

Warning - Delaying ejection in a futile attempt to restart the engine, recover controlled flight may place the aircraft in marginal conditions for safe ejection

Note - Batt 1 & 2 have an endurance of 30 min of load is less than 60A

Caution - Do not attempt a restart if shut down due engine mechanical failure or fire

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Emergency landing checks with associated caution and note

AIRSPEED - BELOW 180
LANDING GEAR HANDLE - DOWN
EMRG GEAR HANDLE - PULL
FLAPS - AS REQUIRED
Once stopped 
BATT 1 & 2 - OFF

Note - Do not check brakes after emergency gear extension to preserve hyd pressure

CAUTION - Anti skid is inoperative with the main hyd system not operating, apply brakes carefully

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Engine fire or smoke and fumes on the ground and associated warning, caution and note

ACS SHUTOFF - PULL
PCL - FUEL OFF
FUEL HYD CUTOFF - PULL 
BATTS AND GENS - OFF
BRAKES - AS REQUIRED
EMERGENCY EGRESS ON THE GROUND

WARNING - EO2 may lead to pure O2 flowing into the cockpit, operate if greater risk due incapacitation due flames

Caution - Anti Skid is inoperative when main hyd system shutdown, apply brakes carefully

Note - DWP and MFD fire warnings indicate engine fire, smoke and fumes may exist without these captions

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Engine fire in flight and associated warning, caution and note

EO2 - PULL
ACS SHUTOFF - PULL
PCL - MIN PRACTICAL
PMS - MANUAL
Check for signs of fire, if not confirmed;
LAND AS SOON AS POSSIBLE

If fire confirmed;
PCL - FUEL KFF
FUEL HYD CUTOFF - PULL
BATT 1 - OFF
GEN 1 & 2 - OFF

If fire persists;
EJECT

WARNING - monitor EO2 contents and descend below safe alt before it runs out

Caution - observe engine limits manually and avoid rapid power changes in manual

Note - smoke and fumes may exist without DWP or MFD fire indications

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Smoke and fumes in the cockpit in flight and associated warning and note

EO2 - PULL
ACS SHUTOFF - PULL
CABIN PRESS - RAM

If fumes continue
GEN 1 & 2 - OFF

WARNING - Monitor EO2 contents and descent below safe altitude before it runs out

WARNING - visor down mask on gloves on prior to pulling MDC handle

Note - if source of fumes can be found, turn the system off and reset EO2

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Aborted takeoff and associated warning/ caution

PLC - IDLE
BRAKES - AS REQUIRED
If aborting due engine fire
ENGINE FIRE OR SMOKE AND FUMES ON THE GROUND

WARNING - eject if collision risk
CAUTION - Anti-skid inoperative with main hyd system out, apply brakes carefully

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Engine failure after T/O and associated warning

PCL - FUEL OFF
If suitable RWY available
FUEL HYD CUTOFF - PULL
EMERGENCY LANDING CHECKS

WARNING - delaying ejection decision in a futile attempt to restart the engine may place the aircraft in marginal conditions for safe ejection

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Engine mechanical failure and associated warning

PCL - FUEL OFF
FUEL HYD CUTOFF - PULL
EO2 - PULL

WARNING - Monitor EO2 contents and descend below safe altitude before it is exhausted

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Engine flame out and associated warning and caution

PCL - IDLE
IGNITERS - ON

Loss of Power
ITT below 400’
NG below 80% in Auto and 70% in manual

WARNING - Monitor EO2 contents and descend below safe altitude before it is exhausted

CAUTION - Minimise power changes following flameout

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Engine surge and associated warning, caution and note

PCL - IDLE
LAND AS SOON AS POSSIBLE

Loss of power
ITT excessively high and fluctuating
Rumbling or popping sounds from engine

WARNING - monitor EO2 contents and descend below safe altitude before it is exhausted

CAUTION - minimise power changes, observe engine limits manually and avoid rapid power changes with PMS manual

NOTE - max TQ in PMS manual 2850

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PMS FAILURE (PMS manual) and associated cautions

PCL- CONTROL ENGINE LIMITS MANUALLY

CAUTION - observe limits manually and avoid rapid power changes
CAUTION - PMS Reset once

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ENG TORQUE

PCL - MINIMUM PRACTICAL

If warning or caution remains

LAND AS SOON AS POSSIBLE

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PROP SPEED and caution

>2200NP = OVERSPEED
PCL - MINIMUM PRACTICAL
AIRSPEED - REDUCE
If warning remains 
LAND AS SOON AS POSSIBLE

>2080NP = OVERSPEED CAUTION
<1900NP = UNDERSPEED CAUTION

CAUTION - Continue flight at low speed using min prac power, monitor engine for indications of mechanical failure

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ENG ITT (GROUND), caution and note

PCL - FUEL OFF

After landing checks and shutdown checks. Keep BATTs on to make RT.

Limit for ground idle is 750’
Limit for air/>63%NG IS 860’

Note - Procedure not to be applied on landing roll, two types of rising ITT. Rapid increase in temp and slow increase in temp

CAUTION - Ensure NP is not maintained between 1600 and 1900 with a tailwind

With tailwind ensure the RPM is NOT kept between…

1600 and 1950rpm

ENG ITT (IN FLIGHT) with associated warning and caution

ITT ABOVE 860’
PCL - MINIMUM PRACTICAL

If warning was displayed even though extinguished

LAND AS SOON AS POSSIBLE

CAUTION - ITT BELOW 350’ = Possible flameout

WARNING - monitor EO2 contents and descend to safe alt before EO2 is exhausted

ENG NG

CAUTION - low NG may indicate a flameout

A.) NG <50.7 = FLAME OUT
IGNITERS - ON
PCL - INCREASE POWER

B.) NG >104% (caution for 2s then warning)
PCL - MINIMUM PRACTICAL
If warning remains
LAND AS SOON AS POSSIBLE

WARNING - Monitor EO2 contents and descend to a safe alt before EO2 is exhausted

OIL PRESS

CAUTION - Monitor

WARNING
PCL - MINIMUM PRACTICAL
If warning indicated
LAND AS SOON AS POSSIBLE

NOTE - Oil press may drop to 40PSI during manoeuvres for 20s. Recover S&L, monitor

OIL TEMP (On ground)

CAUTION - monitor and increase airflow by more power or turning into wind

WARNING
PCL - FUEL OFF
Conduct after landing checks and shutdown checks

NOTE - Increasing NG may reduce oil temp by increasing airflow through the cooler

OIL TEMP high

CAUTION - monitor

WARNING
PCL - MINIMUM PRACTICAL
LAND AS SOON AS POSSIBLE

METAL PARTICLES IN THE GEARBOX and associated caution

PCL - MINIMUM PRACTICAL
LAND AS SOON AS POSSIBLE

CAUTION - Minimise power changes, monitor for signs of engine failure, shut down ASAP after landing

Uncommanded power changes with associated caution and note

PCL - IDLE
PMS - MANUAL
PCL - AS REQUIRED

CAUTION - PMS in manual control engine limits manually

NOTE - Max TQ with PMS in manual is 2850

Oxygen system off (both cockpits) DWP - OXY MFD - OXY OFF NO ANTI G

OXY - ON, CHECK FLOW CONNECTIONS MASK If above 10,000ft and problem remains EO2 - PULL DESCEND BELOW 10,000ft CABIN ALTITUDE NOTE-Consider aircraft fuel state, fuel required to reach Aerodrome and EO2 remaining

OBOGS computed bit failure DWP - OXY MFD - OXY OXY BIT

OXYGEN SYSTEM OFF (BOTH COCKPITS) OXY - ON, CHECK FLOW CONNECTIONS MASK If above 10,000ft cabin altitude EO2 - PULL DESCEND BELOW 10,000ft CABIN ALTITUDE NOTE-Consider aircraft fuel state, fuel required to reach Aerodrome and EO2 remaining

OBOGS Failure DWP - OXY MFD - OXY OXY FAIL, NO ANTI G

OXYGEN - OFF BOTH COCKPITS If above 10,000ft cabin altitude EO2 - PULL DESCEND BELOW 10,000ft CABIN ALTITUDE NOTE-Consider aircraft fuel state, fuel required to reach Aerodrome and EO2 remaining

Oxy pressure/ concentration low DWP - OXY MFD - OXY LOW OXY

OXY - ON, CHECK FLOW CONNECTIONS MASK PCL - INCREASE IF POSSIBLE If above 10,000ft cabin altitude and problem remains EO2 - PULL DESCEND BELOW 10,000ft CABIN ALTITUDE NOTE-Consider aircraft fuel state, fuel required to reach Aerodrome and EO2 remaining

OXY flow warning DWP - MFD - OXY FLOW

OXY - ON, CHECK FLOW CONNECTION MASK If rear cockpit affected INSTRUCTOR SWITCH - FRONT OR REAR SELECTED If above 10,000ft cabin altitude and problem remains EO2 AFFECTED COCKPIT - PULL DESCEND BELOW 10,000ft CABIN ALTITUDE NOTE - Check flow indicators to ID affected cockpit, EO2 activation will isolate OBOGS causing a FLOW warning until EO2 is reset NOTE-Consider aircraft fuel state, fuel required to reach Aerodrome and EO2 remaining

CAB ALTITUDE

DESCEND TO 25,000ft CABIN ALTITUDE OR BELOW

ACFT ALT

DESCEND TO 25,000ft AIRCRAFT ALTITUDE OR BELOW

CAB HI PRESS | DWP - OVPR

CABIN PRESS - PRESS DUMP | PCL - MINIMUM PRACTICAL

FPR FUEL PRESS FPR Associated CAUTION and NOTE

FUEL PUMPS - ON PCL - MINIMUM PRACTICAL If warning remains LAND AS SOON AS POSSIBLE CAUTION - Operating below 0’ without icing inhibitor may cause filter blockage due icing NOTE - Change altitude to warmer alt if possible

TRIM RUNAWAY Associated CAUTION AND NOTE

TRIM AILERON POWER OFF CAUTION - TRIM/AIL PWR off de energises trim and you loose powered aileron, spoilers, powered brakes and anti skid Manual braking required higher than normal pressure, landing roll is +8%, pull emergency gear handle if powered braking is required NOTE- To avoid leg fatigue, slip indicator may be off centre below 220KIAS

Flap failure and associated caution and note

AIRSPEED - BELOW 180 CAUTION - Observe flaps extended airspeed and G limits if flaps cannot be confirmed up NOTE - Return clap lever to last position following subsequent selection NOTE - Consider aircraft fuel state and fuel required to reach suitable Aerodrome

GEAR RETRACTION FAILURE Associated CAUTION and NOTE

AIRSPEED - BELOW 180 CAUTION - Anti Skid and powered brakes is inoperable with the emergency gear angle pulled or main hyd system not operating. Apply brakes carefully NOTE - Landing gear cannot be retracted following emergency gear selection. Do not check brakes to save hyd pressure for flap extension and powered brake application

HYPOXIA

OXY - ON, MAX, CHECK FLOW CONNECTIONS MASK If oxy system is operating normally EO2 - PULL DESCEND BELOW 10,000ft CA Once below 10,000ft CA ACS - PULL CABIN PRESS - RAM LAND AS SOON AS POSSIBLE if fumes continue GEN 1 & 2 OFF