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ADF115 > Bold Face > Flashcards

Bold Face Flashcards

1
Q

Warning associated with the ejection checks?

A
  • 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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2
Q

Emergency egress on the ground, and warning associated with it

A 
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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3
Q

Warning, note, Caution associated with gliding checks

A

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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4
Q

Emergency landing checks with associated caution and note

A 
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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5
Q

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

A 
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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6
Q

Engine fire in flight and associated warning, caution and note

A 
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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7
Q

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

A

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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8
Q

Aborted takeoff and associated warning/ caution

A

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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9
Q

Engine failure after T/O and associated warning

A

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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10
Q

Engine mechanical failure and associated warning

A

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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11
Q

Engine flame out and associated warning and caution

A

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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12
Q

Engine surge and associated warning, caution and note

A

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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13
Q

PMS FAILURE (PMS manual) and associated cautions

A

PCL- CONTROL ENGINE LIMITS MANUALLY

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

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14
Q

ENG TORQUE

A

PCL - MINIMUM PRACTICAL

If warning or caution remains

LAND AS SOON AS POSSIBLE

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15
Q

PROP SPEED and caution

A 
>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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16
Q

ENG ITT (GROUND), caution and note

A

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

17
Q

With tailwind ensure the RPM is NOT kept between…

A

1600 and 1950rpm

18
Q

ENG ITT (IN FLIGHT) with associated warning and caution

A

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

19
Q

ENG NG

A

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

20
Q

OIL PRESS

A

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

21
Q

OIL TEMP (On ground)

A

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

22
Q

OIL TEMP high

A

CAUTION - monitor

WARNING
PCL - MINIMUM PRACTICAL
LAND AS SOON AS POSSIBLE

23
Q

METAL PARTICLES IN THE GEARBOX and associated caution

A

PCL - MINIMUM PRACTICAL
LAND AS SOON AS POSSIBLE

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

24
Q

Uncommanded power changes with associated caution and note

A

PCL - IDLE
PMS - MANUAL
PCL - AS REQUIRED

CAUTION - PMS in manual control engine limits manually

NOTE - Max TQ with PMS in manual is 2850

25
Q

Oxygen system off (both cockpits)

DWP - OXY
MFD - OXY OFF
NO ANTI G

A

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

26
Q

OBOGS computed bit failure

DWP - OXY
MFD - OXY
OXY BIT

A

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

27
Q

OBOGS Failure

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

A

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

28
Q

Oxy pressure/ concentration low

DWP - OXY
MFD - OXY
LOW OXY

A

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

29
Q

OXY flow warning

DWP -
MFD - OXY FLOW

A

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

30
Q

CAB ALTITUDE

A

DESCEND TO 25,000ft CABIN ALTITUDE OR BELOW

31
Q

ACFT ALT

A

DESCEND TO 25,000ft AIRCRAFT ALTITUDE OR BELOW

32
Q

CAB HI PRESS

DWP - OVPR

A

CABIN PRESS - PRESS DUMP

PCL - MINIMUM PRACTICAL

33
Q

FPR FUEL PRESS
FPR

Associated CAUTION and NOTE

A

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

34
Q

TRIM RUNAWAY

Associated CAUTION AND NOTE

A

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

35
Q

Flap failure and associated caution and note

A

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

36
Q

GEAR RETRACTION FAILURE

Associated CAUTION and NOTE

A

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

37
Q

HYPOXIA

A

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

ADF115 (3 decks)

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