Emergencies Flashcards

1
Q

GROUND EGRESS

A
  1. SEAT PIN……………………………………………………….INSTALL (if time permits) 2. LIFE VEST CONNECTOR………………………………………………….DISCONNECT TA TR 343 SECTION III 3-4 3. QRF…………………………………………………………………………………RELEASE 4. LEG GARTER/PEC RELEASE…………………………………………………ACTUATE 5. CANOPY………………………………………………………………………………..OPEN If unsuccessful: 6. CANOPY………………………………………………………………………..FRAGILIZE
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2
Q

ENGINE FIRE ON THE GROUND If the fire light(s) illuminate(s) or signs of fire are detected, perform the following:

A
  1. THROTTLES…………………………………………………………………………………………………………..STOP 2. LP COCKS ……………………………………………………………………………………………………………CLOSE
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3
Q

ABORT / BARRIER ENGAGEMENT

A
  1. THROTTLES ……………………………………………………………………………..IDLE / STOP for fire 2. HOOK…………………………………………………………………………………………..DOWN, if necessary 3. BRAKES/NWS ………………………………………………….RELEASE BEFORE ENGAGEMENT
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4
Q

ENGINE FIRE / FAILURE DURING TAKEOFF

A

If committed to continue the takeoff and no single engine climb performance exists - EJECT If decision is made to stop: 1. ABORT If committed to takeoff with single engine climb performance: 2. THROTTLES ……………………………………………………………………………………………MIL POWER 3. OVERHEAT SWITCH…………………………………………………………………………………ACTIVATE 4. THROTTLE (affected engine) …………………………………………………………………….STOP for fire

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5
Q

BLOWN TIRE DURING TAKEOFF

A

If decision is made to stop: 1. ABORT 2. ANTI-SKID…………………………………………………………………………………………………………..OFF

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6
Q

DOUBLE ENGINE FLAME OUT

A
  1. Throttles…………………………………………………………………………………………………………………..STOP 2. Airspeed……………………………………………………………………………………………………………..195 KIAS
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7
Q

OUT OF CONTROL / SPIN RECOVERY

A

If below 10,000 feet AGL and the aircraft is still out of control EJECT . 1. CONTROLS…………………………………………………………………………………………………..RELEASE 2. THROTTLES ………………………………………………………………………………………………………..IDLE If spin is not recovered: 3. AILERON ……………………………………………………………………………..IN DIRECTION OF SPIN

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8
Q

EJECTION IN FLIGHT

A
  1. EJECTION HANDLE……………………………………………………………………PULL
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9
Q

MANUAL SEPARATION PROCEDURE

A
  1. MOR HANDLE…………………………………………………………………………PULL
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10
Q

AFTER EJECTION

A
  1. CANOPY………………………………………………………………………………CHECK 2. MASK……………………………………………………………………………….RELEASE 3. QRF……………………………………………………………UPON TOUCHDOWN OPEN
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11
Q

FUEL SYSTEM FAILURE LP L or LP R WARNING LIGHT ON

A
  1. POSITIVE G’s …………………………………………………………………………………………………………….MAINTAIN
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12
Q

OIL L or OIL R WARNING LIGHT

A
  1. THROTTLE (AFFECTED ENGINE) ……………..RETARD (UNTIL LIGHT GOES OUT)
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13
Q

FIRE WARNING LIGHT ON

A
  1. THROTTLE (affected engine) …………………………………………………………………………….IDLE
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14
Q

SMOKE OR FUMES / ELECTRICAL FIRE

A

the cockpit should be considered toxic. 1. OXYGEN……………………………………………………………………………………………………………..EMERG

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15
Q

OXY R or OXY F WARNING LIGHT ON / HYPOXIA

A
  1. Emergency Oxygen Handle…………….PULL (Yellow and Black handle on left side of seat) 2. OXYGEN…………………………………………………………………………………………………………..100% 3. MASK connections ………………………………………………………………………………………………..CHECK 4. EMERGENCY DESCENT………………………………………………to 10,000 ft or below
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16
Q

LANDING WITH BOTH ENGINES OUT

A
  1. AIRSPEED ……………………………………………………………………………………………………195 KIAS 2. HEADING………………………………………TURN TO THE NEAREST SUITABLE AIRPORT 3. HIGH KEY…………………………………………………………………………………………6000 FEET AGL 4. GEAR …………………………………………………………………………………………………………………………DOWN 5. LOW KEY………………………………………………………………………………………….3000 FEET AGL 6. FLAPS……………………………………………………………………………………………………………….HALF 7. FINAL KEY………………………………………………………………………………………1,500 FEET AGL 8. FLAPS…………………………………………………………………………….FULL (when landing assured) 9. EL PUMP………………………………………………………………………………………………….CHECK ON 10. AIRSPEED AT 300 FT…………………………………………………………………………..MIN 150 KIAS
17
Q

HYD 1 – HYD 2 AND HYD EM WARNING LIGHT ON

A
  1. EL PUMP ………………………………………………………………………………………………………CHECK ON If total hydraulic failure is confirmed: 2. EJECT