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Bold Face Flashcards

1
Q

BRAKE FAILURE

A

WARNING: If uncontrolled departure from hard surface will occur, consider PCL FUEL OFF, or ejection if at high speed.

  1. BRAKES……… RELEASE
  2. SERVICABLE BRAKES……… GRADUALLY RE-APPLY
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2
Q

EMERGENCY EGRESS ON THE GROUND

A

WARNING: Eject if circumstances dictate; however, do not attempt to eject if:
* Occupants are not correctly strapped in
* Canopy not closed and locked
* CFS and seat pins are not removed

  1. SEAT PIN……………………..IN
  2. LEG RESTRAINTS………….RELEASE
  3. SEAT HARNESS…………….RELEASE
  4. OXYGEN MASK HOSE……DISCONNECT
  5. MIC-TEL……………………….DISCONNECT
  6. PSP………………………………DISCONNECT
  7. CANOPY………………………OPEN
  8. EXIT THE COCKPIT
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3
Q

EMERGENCY LANDING CHECKS

A

CAUTION: Anti-skid is inoperative when the main hyd system is not operating. Apply the brakes carefully with anti-skid inoperative.

  1. AIRSPEED………………….BELOW 180 KIAS
  2. LANDING GEAR HANDLE………DOWN
  3. EMER LDG GR HANDLE………..PULL
  4. FLAPS………………………….AS REQUIRED

When aircraft has stopped:

  1. BATT 1 AND BATT 2……………..OFF
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4
Q

ENGINE FIRE OR SMOKE AND FUMES –
ON GROUND

MFD FIRE
DWP FIRE

A

WARNING: Activating the EO2 may lead to pure oxy flowing into the cockpit during egress. However, operate the EO2 if incapacitation is assessed to be a greater risk.

CAUTION: Anti-skid is inoperative when the main hyd system is not operating. Apply the brakes carefully with anti-skid inoperative.

Normal powered braking is not available when the main hyd system is not operating. Manual braking requires higher than normal pressure and travel.

  1. ACS SHUT OFF…………….…PULL
  2. PCL……………………………….FUEL OFF
  3. FUEL HYD CUTOFF…………PULL
  4. BATTS AND GENS………….OFF
  5. BRAKES…………………………AS REQUIRED
  6. EMERGENCY EGRESS ON THE GROUND
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5
Q

ENGINE FIRE – IN FLIGHT

MFD FIRE
DWP FIRE

A

WARNING: Monitor EO2 contents and descend to a safe altitude before EO2 is exhausted.

CAUTION: Observe eng limits manually and avoid rapid power changes with the PMS in manual mode.
1. PCL……………………MINIMUM PRACTICAL
2. EO2…………………………………..PULL
3. ACS SHUT OFF…………………..PULL
4. CHECK FOR FIRE
If fire confirmed:
5. PCL……………………………………FUEL OFF
6. FUEL HYD CUTOFF…………….PULL
7. BATT 1………………………………OFF
8. GEN 1 AND GEN 2……….…….OFF
If fire continues:
9. EJECT
If fire is not confirmed or FIRE warnings go out:
10. PMS……………………………….MANUAL

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6
Q

SMOKE OR FUMES IN THE COCKPIT – IN FLIGHT

MFD FIRE
DWP FIRE

A

WARNING: Monitor EO2 contents and descend to a safe altitude before EO2 is exhausted.

Land as soon as possible following smoke or fumes in the cockpit.

  1. EO2………………………………PULL
  2. DESCEND BELOW 10 000 FT AIRCRAFT ALTITUDE
  3. OXYGEN………………………..OFF (BOTH COCKPITS)
  4. ACS SHUT OFF………………PULL
  5. CABIN PRESS………………..RAM

If fumes continue:

  1. GEN 1 AND GEN 2………..OFF
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7
Q

ABORTED TAKE-OFF

A

WARNING: Eject if there is likely risk of collision.

If uncontrolled departure from the hard
surface will occur, consider PCL FUEL OFF, or ejection if at high speed.

CAUTION: Anti-skid is inoperative when the main hyd system is not operating. Apply the brakes carefully with anti-skid inoperative.

Normal powered braking is not available when the main hyd system is not operating. Manual braking requires higher than normal pressure and travel.

  1. PCL……………………………….IDLE
  2. BRAKES……………………..….AS REQUIRED
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8
Q

ENGINE FAILURE AFTER TAKE OFF

A
  1. PCL……………………………………….FUEL OFF

WARNING: Delaying ejection may place the aircraft in marginal conditions for safe ejection. Eject if unable to carry out a forced landing safely.

If a suitable runway is available:

  1. FUEL HYD CUTOFF…………………….PULL
  2. EMERENCY LANDING CHECKS
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9
Q

ENGINE MECHANICAL FAILURE

A
  1. PCL……………………….……..FUEL OFF
  2. FUEL HYD CUTOFF………..PULL

WARNING: Monitor EO2 contents and descend to a safe altitude before EO2 is exhausted.

  1. EO2……………..PULL IF ABOVE 10 000 FT
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10
Q

PMS FAILURE (PMS MANUAL)

MFD PMS MANUAL
DWP PMS

A

CAUTION: Observe eng limits manually and avoid rapid power changes with the PMS in manual mode.

  1. PCL…………………………CONTROL ENGINE LIMITS MANUALLY

When at safe height:

  1. PCL…………………………MID TO LOW POWER (PCL < 55◦)
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11
Q

ENGINE SURGE

A

CAUTION: Minimise power changes following engine surge.
NOTE
If an engine surge is identified, set aircraft
attitude for minimum sideslip and AOA as
soon as practicable. Achieve best glide
speed as soon as practicable.

  1. PCL……………………………..……….IDLE

Indications:
* Loss of power
* ITT excessively high or fluctuating
* Unusual engine noise (popping or rumbling)

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12
Q

ENGINE FLAMEOUT

A

CAUTION: Minimise power changes following engine flameout.
NOTE
If an engine flameout is identified, set
aircraft attitude for minimum sideslip and
AOA as soon as practicable. Achieve best
glide speed as soon as practicable.

  1. PCL………………….……………..IDLE

Indications:
* Loss of power
* ITT below 400°C
* NG decreasing:
* below 80% PMS auto
* below 70% PMS man

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13
Q

ENGINE TORQUE

MFD ENG TORQUE
DWP ——

A
  1. PCL………………….MINIMUM PRACTICAL
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14
Q

PROPELLER SPEED
OVERSPEED – NP ABOVE 2200 RPM (WARNING)

MFD PROP SPEED
DWP ——

A

CAUTION: Continue flight at low speed using minimum practical power.

Monitor the engine for indications of mechanical failure.

  1. PCL………………….MINIMUM PRACTICAL
  2. AIRSPEED………..REDUCE
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15
Q

ENGINE TEMPERATURE – ON GROUND

MFD ENG ITT
DWP ——

A

CAUTION: Ensure NP is not maintained between 1600 and 1900 RPM with tailwind.

NOTE: Above 63% NG the ITT limit is 860C

If ITT rapidly increases towards and exceeds 750°C in ground idle with warning displayed:

  1. PCL……………………………FUEL OFF
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16
Q

ENGINE TEMPERATURE – IN FLIGHT
(High or low?)

MFD ENG ITT (red)
or ENG ITT (yellow)
DWP ——

A

ITT ABOVE 860C

  1. PCL………………..MINIMUM PRACTICAL

ITT BELOW 350C:

CAUTION: Low ITT may indicate engine flameout.

17
Q

ENGINE SPEED
(High or low?)

MFD ENG NG (red)
or ENG NG (yellow)
DWP ——

A

NG BELOW 50.7% (CAUTION)

CAUTION: Low ITT may indicate engine flameout.

  1. IGNITERS……………………ON
  2. PCL…………………………….SLOWLY INCREASE POWER

NG ABOVE 104% (CAUTION FOR 2 SECOND, THEN WARNING)

  1. PCL…………………MINIMUM PRACTICAL
18
Q

OIL PRESSURE OUT OF LIMITS

MFD OIL PRESS
or OIL PRESS
DWP OIL

A

NOTE: Oil pressure may be as low as 40 psi during aerobatics if recovery is within 20 seconds.
Verify under positive G.

If warning or caution remains indicated:

  1. PCL……………..MINIMUM PRACTICAL
19
Q

OIL TEMPERATURE HIGH – ON GROUND

MFD OIL TEMP
DWP ——

A

OIL TEMP WARNING

  1. PCL…………………………………….FUEL OFF
20
Q

OIL TEMPERATURE HIGH - IN FLIGHT

MFD OIL TEMP
DWP ——

A

OIL TEMP WARNING

  1. PCL……………………MINIMUM PRACTICAL
21
Q

UNCOMMANDED POWER CHANGES

A

CAUTION: Observe eng limits manually and avoid rapid power changes with the PMS in manual mode.

NOTE
The maximum approved torque is 2850 ft lb
(67.5%) with the PMS in manual mode.

  1. PCL…………………………IDLE
  2. PMS……………………….MANUAL
  3. PCL…………………………AS REQUIRED
21
Q

METAL PARTICLES DETECTED IN GEARBOX

MFD CHIP PROP
or CHIP AGB
DWP CHIP

A

CAUTION: Minimise power changes with CHIP indicated.
Monitor the engine for signs of mechanical failure.
Shut down the engine as soon as possible after landing

  1. PCL……………………MINIMUM PRACTICAL
  2. LAND AS SOON AS POSSIBLE
22
Q

OXYGEN SYSTEM OFF (BOTH COCKPITS)

MFD OXY OFF
DWP OXY

A

If above 10 000ft cabin altitude:

  1. EO2……………….…..PULL
  2. DESCEND BELOW 10 000 FT CABIN ALTITUDE
23
Q

MFD OXY WARNING

MFD OXY
DWP OXY

A

If above 10 000ft cabin altitude:

  1. EO2……………….…..PULL
  2. DESCEND BELOW 10 000 FT CABIN ALTITUDE
24
Q

OXY FLOW WARNING

MFD OXY FLOW
DWP —–

A

NOTE
Check the flow indicators to identify the
affected cockpit.
EO2 activation will isolate OBOGS oxygen
flow in the affected cockpit, causing an OXY
FLOW warning until the EO2 is depleted or
reset.
1. OXYGEN………………………………..ON, CHECK FLOW, CONNECTIONS, MASK
2. INSTRUCTIOR SWITCH…………..CHECK FOR CORRECT SELECTION

If above 10 000ft cabin altitude and problem remains:

  1. EO2 ………..PULL (AFFECTED COCKPIT)
  2. DESCEND BELOW 10 000 FT CABIN ALTITUDE
25
Q

PHYSIOLOGICAL EVENT AND HYPOXIA

A

NOTE
If an almost loss of consciousness (ALOC)
or gravity-induced loss of consciousness
(GLOC) event occurs at any time, the sortie
is to be terminated and aircraft recovered
without excessive manoeuvring.

  1. EO2 ………………. PULL (BOTH COCKPITS)
  2. DESCEND BELOW 10 000FT AIRCRAFT ALTITUDE
  3. OXYGEN …………… OFF (BOTH COCKPITS)

When at or below 10 000 ft aircraft altitude:
4. ACS SHUTOFF ……………………. PULL
5. CABIN PRESS …………………….. RAM

If symptoms persist and incapacitation is likely:
9. EJECT

26
Q

EJECTION CHECKS

A

WARNING: The canopy must be closed and locked before ejecting.
Notify the other occupant as soon as possible.
Make a conscious effort to adopt the correct
ejection posture:
* Buttocks well back in seat
* Back pressed firmly against the seat
back and sitting as straight as possible
* Press head firmly against headpad
* Eyes closed
* Legs forward with feet touching the
rudder pedals to ensure optimum thigh
support
* Grip the seat firing handle with the preferred hand. Use the other hand
to grip the wrist of the pulling hand to
prevent flailing at high speeds.
Simultaneous ejection of both seats is not
advisable as seat entanglement could occur.
The aircraft captain should order and wait for
the other occupant to eject when operating
with the ISS selector INDEPENDENT

If time critical:
1. SEAT FIRING HANDLE……PULL

27
Q

GEAR LOWERING FAILURE

MFD GEAR
DWP —

A
  1. AIRSPEED……….BELOW 180 KIAS
28
Q

TRIM RUNAWAY

A

CAUTION: TRIM/AIL PWR off de-energises electric trims and the powered ailerons, roll spoilers, powered braking and anti-skid systems are inoperative.

  1. TRM/AIL PWR……………..OFF
29
Q

FUEL PRESSURE LOW

MFD FPR FUEL PRESS
DWP FPR

A

CAUTION: Operating below 0C OAT without fuel icing inhibitor may cause filter blockage.

NOTE: Change altitude to find higher OAT if possible. Ensure positive g.

  1. FUEL PUMPS…….. PUMP L AND PUMP R
  2. PCL……………………MINIMUM PRACTICAL

If warning remains:

  1. LAND AS SOON AS POSSIBLE
30
Q

CABIN OVERPRESSURE WARNING

MFD CAB HI PRESS
DWP OVPR

A
  1. CABIN PRESS…….PRESS DUMP
  2. PCL……………………MINIMUM PRACTICAL
31
Q

AILERON CONTROL SYSTEM MALFUNCTION

Indications: * Uncommanded roll or increased aileron force

A

CAUTION: TRIM/AIL PWR off de-energises electric trims and the powered ailerons, roll spoilers, powered braking and anti-skid systems are inoperative.

  1. TRM/AIL PWR……………..OFF
32
Q

FLAP FAILURE

MFD FLAP
DWP —

A

CAUTION: Observe flaps extended airspeed and g limitations if flaps cannot be confirmed up.

  1. AIRSPEED………….BELOW 180 KIAS
33
Q

GEAR RETRACTION FAILURE

MFD GEAR
DWP —

A

If lights not extinguished after up selection:

  1. AIRSPEED……..BELOW 180 KIAS

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