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FAM > Emergency Procedures > Flashcards

Emergency Procedures Flashcards

1
Q
  • *CLEAR ENGINE PROCEDURE/ABNORMAL START/**
  • *TP FIRE ON SHUTDOWN**
A
  • **1. Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF**
  • **2. ENGINE switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON**
  • **3. FUEL SHUTOFF handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN**
  • **4. GTS start button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS**
  • **5. IGNITION switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ISOLATE**
  • When rpm below 20 percent and GTS advisory light illuminates:*
  • **6. ENGINE switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START**
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2
Q

EMERGENCY SHUTDOWN/EGRESS

A
  • **1. Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF**
  • **2. ENGINE switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF**
  • **3. FUEL SHUTOFF handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL**
  • **4. Ejection seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SAFE**
  • **5. BATT switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF**
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3
Q

ENGINE FAILURE

A

If below 1,500 feet AGL and airspeed below 180 KIAS:
1. EJECT.
Otherwise:
2. EXECUTE AIRSTART. (P E5-E9)

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4
Q

AIRSTART

A
  1. EMERGENCY OXYGEN GREEN RING(S) . . . . . . . . . . . . . PULL
  2. THROTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
    Simultaneously perform steps 3. and 4.:
  3. GTS START BUTTON . . . . . . . . . . . . . . . . . . . PRESS
  4. THROTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
    If unsuccessful (no relight within 30 seconds after moving throttle to idle or EGT exceeds limits):
  5. THROTTLE . . . . . . . . . . . . . . . . . . . . OFF (ALLOW 30 SECONDS TO DRAIN IF PRACTICAL)
    If above 13% RPM and 250kts, repeat steps 3 and 4. Otherwise, proceed to step 6.
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5
Q

COMPRESSOR STALL OR EGT/RPM WARNING LIGHT

A
  1. THROTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
  2. EGT/RPM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
    If EGT is greater than 450 ºC for more than 6 seconds at IDLE:
  3. EXECUTE ENGINE FAILURE PROCEDURE.
    If EGT responds normally:
  4. THROTTLE . . . . . . . . . . . . . . SLOWLY ADVANCE TO MINIMUM FOR SAFE FLIGHT
  5. MINIMIZE THROTTLE MOVEMENTS.
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6
Q

ABORT

A
  • **1. THROTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE**
  • **2. SPEED BRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . EXTEND**
  • **3. BRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY**
  • **4. HOOK . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN (IF REQUIRED)**
  • **5. BRAKES . . . . . . . . . . . . . . . . . RELEASE PRIOR TO CROSSING THE ARRESTING GEAR**
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7
Q

EMERGENCY CATAPULT FLYAWAY

A
  • **1. THROTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MRT**
  • **2. MAINTAIN 24 UNITS AOA.**
  • If engine failed, or unable to stop settle:*
  • **3. EJECT.**
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8
Q

Brake Failure Ashore

A
  • If flyaway airspeed available:*
  • **1. GO-AROUND.**
  • If flyaway airspeed not available, or during taxi:*
  • **2. THROTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE**
  • **3. BRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE**
  • **4. ANTI-SKID SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF**
  • **5. BRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY GRADUALLY**
  • If brakes still unavailable:*
  • **6. HOOK . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN (IF REQUIRED)**
  • **7. PARKING BRAKE HANDLE . . . . . . . . . . . . PULL (IF REQUIRED)**
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9
Q

BRAKE FAILURE — AFLOAT

A
  • **1. THROTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE**
  • **2. PARKING BRAKE HANDLE . . . . . . . . . . . . . . . . . . . . . . . . . . PULL**
  • **3. HOOK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN**
  • **4. TRANSMIT.**
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10
Q

LOSS OF DIRECTIONAL CONTROL

A
  • If flyaway airspeed available:*
  • **1. GO-AROUND.**
  • If flyaway airspeed not available:*
  • **2. ABORT. (P E18)**
  • If blown tire suspected:*
  • **3. BRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RELEASE**
  • **4. ANTI-SKID SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF**
  • **5. BRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . . APPLY GRADUALLY**
  • If NWS failure suspected:*
  • **6. PADDLE SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS**
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11
Q

DEPARTURE/SPIN PROCEDURE

A
  • **1. CONTROLS . . . . . . . . . . . . . . . . . . . . . NEUTRALIZE/FORCIBLY**
  • *CENTER RUDDER PEDALS**
  • **2. SPEED BRAKES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT**
  • **3. THROTTLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE**
  • **4. CHECK ALTITUDE, AOA, AIRSPEED, AND TURN NEEDLE.**
  • If spin confirmed: INVERTED (AOA pegged at 0 units):*
  • **5. RUDDER PEDAL . . . . . . . . . . FULL OPPOSITE TURN NEEDLE**
  • **6. LATERAL STICK . . . . . . . . . . FULL OPPOSITE TURN NEEDLE**
  • **7. LONGITUDINAL STICK . . . . . . . . . . . . . . . . . . . . . . . NEUTRALIZE**
  • UPRIGHT (AOA above 28 units):*
  • **8. RUDDER PEDAL . . . . . . . . . . FULL OPPOSITE TURN NEEDLE**
  • **9. LATERAL STICK . . . . . . . . . . . . . . . FULL WITH TURN NEEDLE**
  • **10. LONGITUDINAL STICK . . . . . . . . . . . . . . . . . . . . . . . NEUTRALIZE**
  • If recovery indicated or airspeed increasing through 160 KIAS:*
  • **11. LATERAL STICK . . . . . . . . . . . . . . . . . . . . . . . . . . . . NEUTRALIZE**
  • When recovery indicated:*
  • **12. RUDDER PEDALS . . . . . . . . . . . . . . . . . . . SMOOTHLY CENTER**
  • If out of control passing through 10,000 feet AGL:*
  • **13. EJECT.**
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12
Q

TOTAL ELECTRICAL FAILURE

A

*1. EMERGENCY OXYGEN GREEN RING(S) . . . . . . . . . . . . . PULL

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13
Q

ADVERSE PHYSIOLOGICAL SYMPTOMS

A

If above 10,000 feet cabin altitude:
1. Emergency oxygen green ring(s) - pull
2. OBOGS FLOW SELECTOR . . . . . . OFF
3. Descend below 10,000 feet cabin altitude.

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14
Q

RAPID DECOMPRESSION

A
  1. EMERGENCY OXYGEN GREEN RING(S) . . . . . . . . . . . . . PULL
  2. OBOGS FLOW SELECTOR(S) . . . . . . . . . . . . . . . . . . . . . . . . OFF
  3. Descend below 10,000 feet cabin altitude.
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15
Q

ELECTRICAL FIRE

A

*1. GEN SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

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16
Q

SMOKE OR FUMES IN COCKPIT

A
  • **1. MASK . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON/TIGHT**
  • **2. INITIATE CONTROLLED DESCENT TO BELOW 18,000 FEET**
  • *MSL.**
  • *3. AIR FLOW KNOB . . . . . . . . . . . . . . . . OFF** *(BELOW 18,000 FEET
  • MSL IF POSSIBLE)*
  • If unable to clear smoke or unable to see:*
  • *4. AIRSPEED . . . . . . . . . . . . . . . . . . . . REDUCE** *(AS PRACTICAL)
  • **5. WARN OTHER COCKPIT OCCUPANTS/SECURE LOOSE ITEMS.**
  • **6. SEAT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOWER**
  • **7. MDC FIRING HANDLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL**
17
Q

FIRE

A
  • GROUND*
  • **1. EXECUTE EMERGENCY SHUTDOWN/EGRESS. (P E2)**
  • TAKEOFF*
  • If decision is made to stop:*
  • **1. ABORT. (P E18)**
  • If fire is confirmed and unable to abort:*
  • **2. EJECT.**
  • IN-FLIGHT*
  • **1. THROTTLE . . . . . . . . . . . . . . . . . . MINIMUM FOR SAFE FLIGHT**
  • **2. CHECK FOR SECONDARY INDICATIONS OF FIRE.**
  • If fire confirmed or flight control lost:*
  • **3. EJECT.**
  • If fire not confirmed and control effectiveness remains:*
  • **4. LAND AS SOON AS POSSIBLE.**
18
Q

GTS FIRE

A
  • GROUND*
  • **1. EXECUTE EMERGENCY SHUTDOWN/EGRESS. (P E2)**
  • IN-FLIGHT*
  • **1. ENGINE SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF**
19
Q

OIL PRESS WARNING LIGHT

A
  1. Throttle - Immediately set minimum power required within the range of 78 to 87% rpm.
  2. Avoid further power changes.
20
Q

OXYGEN WARNING LIGHT

A

IN FLIGHT
1. Throttle - Set minimum 80% rpm
2. Execute Adverse Physiological Symptoms (as required)

21
Q

TP HOT CAUTION LIGHT

A
  • GROUND*
  • **1. EXECUTE EMERGENCY SHUTDOWN/EGRESS. (P E2)**
  • IN-FLIGHT*
  • **1. THROTTLE . . . . . . . . . . . . . . . . . . MINIMUM FOR SAFE FLIGHT**
22
Q

ASYMMETRIC FLAPS/SLATS

A
  1. Flaps/Slats lever - Return to previous setting

FAM (10 decks)

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