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1
Q

EMERGENCY EGRESS ON THE GROUND

A

If circumstances dictate
1. Eject
Otherwise
1. Warn other occupant
2. Seat pin - In
3. PCL - FUEL OFF
4. BATTs + GENs - OFF
5. MIC-TEL, oxygen hose Disconnect
6. Seat Harness - Release
7. PSP - Disconnect
8. Leg restraints - Release
Canopy - Open
10. Egress aircraft

If unable to open canopy - front cockpit -
MDC Handle - Pull
Rear Cockpit - Break Canopy with Breaker knife

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2
Q

ENGINE FIRE ON THE GROUND

A
  1. ACS SHUTOFF - Pull
  2. PCL - FUEL OFF
  3. FUEL HYD CUTOFF Pull
  4. Radio - Mayday
  5. BATTs + GENs - OFF
  6. PARK BRAKE - As required
  7. EMERGENCY EGRESS ON THE GROUND
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3
Q

ENGINE FIRE IN THE AIR

A
  1. EO2 - Pull
  2. ACS SHUT OFF - Pull
  3. PCL - Min Practical
  4. PMS - MAN
  5. Engine - Check for fire

If fire confirmed

  1. PCL - FUEL OFF
  2. FUEL HYD CUTOFF - Pull
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4
Q

SMOKE OR FUMES IN THE COCKPIT

A

ON THE GROUND
1. EMERGENCY EGRESS ON THE GROUND

IN THE AIR
1. EO2 Pull
2. ACS SHUT OFF Pull
3. CABIN PRESS RAM
Descend below 10,000ft
~~~

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5
Q

TAKE-OFF ABORT

A
  1. PCL - IDLE / FUEL OFF for fire
  2. Braking - As required

If collision likely:
3. Eject

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6
Q

ENGINE FAILURE AFTER TAKE-OFF

A

If unable to reach suitable runway - Eject

If suitable runway is available
PCL - FUEL OFF
2. Landing gear handle DN
3. EMER LDG GR handle Pull
4. Flaps - As required
5. FUEL HYD CUTOFF Pull

When aircraft has stopped
6. BATT 1 + BATT 2 OFF

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7
Q

ENGINE MECHANICAL FAILURE

A
  1. PCL - FUEL OFF
  2. FUEL HYD CUTOFF - Pull
  3. EO2 (above 10,000 ft) - Pull
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8
Q

ENGINE FLAMEOUT

A
  1. PCL IDLE
  2. Ignition IGN
  3. Attitude Minimize side slip/AOA
  4. Airspeed - 140 KIAS
  5. Engine indications Monitor

If normal engine indications NOT restored

  1. EO2 (above 10,000 ft) Pull
  2. OXYGEN OFF
  3. PCL FUEL OFF
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9
Q

ENGINE SURGE

A
  1. PCL IDLE
  2. Attitude Minimize side slip/AOA
  3. Airspeed 140 KIAS
  4. Engine Indications - Monitor

If normal engine indications not restored
PMS - MAN

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10
Q

PMS FAILURE

A
  1. PCL Mid to low power
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11
Q

ENGINE TORQUE

A
  1. PCL Min Practical
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12
Q

ENGINE TEMPERATURE

A

IN THR AIR

If ITT above 860C

  1. PCL Min practical
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13
Q

ENGINE SPEED

A

If NG above 104% (caution for 2 sec, then warning):

  1. PCL - Min Practical
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14
Q

PROPELLER SPEED

A

Overspeed (warning) NP above 2200 RPM

  1. PCL Min practical
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15
Q

OIL PRESSURE OUT OF LIMITS

A
  1. Ensure positive g

2. PCL - Min Practical

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16
Q

OIL TEMPERATURE HIGH

A

IN THE AIR

PCL. Min practical

17
Q

OIL TEMPERATURE LOW

A
  1. PCL Min practical
18
Q

CHIP DETECTION CAUTION

A

PCL Min practical, Minimize power changes

19
Q

UNCOMMANDED POWER CHANGES

A
  1. PCL. IDLE
  2. PMS MAN
  3. PCL. As required
20
Q

OXYGEN SYSTEM OFF IN BOTH COCKPITS

A

1.OXYGEN - Check ON, connections

If above 10,000 ft cabin altitude and problem remains:

  1. EO2 Pull
  2. Descend below 10,000 ft cabin altitude
21
Q

OXYGEN BIT FAILURE

A
  1. OXYGEN Check ON, connections

If above 10,000 ft cabin altitude and problem remains:

  1. EO2 Pull
  2. Descend below 10,000 ft cabin altitude
22
Q

OXYGEN FAILURE

A
  1. OXYGEN. OFF, both cockpits

If above 10,000 ft cabin altitude

  1. EO2 Pull
  2. Descend below 10,000 ft cabin altitude
23
Q

OXYGEN LOW PRESSURE OR LOW CONCENTRATION

A
  1. OXYGEN Check ON, connections
  2. PCL Increase power

If above 10,000 ft cabin altitude and problem remains:

  1. EO2 Pull
  2. Descend below 10,000 ft cabin altitude
24
Q

TRIM RUNAWAY

A
  1. TRIM/AIL PWR OFF
25
Q

AILERON CONTROL SYSTEM MALFUNCTION

A
  1. TRIM/AIL PWR OFF

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