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T45C IJET > T45Emergen > Flashcards

T45Emergen Flashcards

1
Q

CABIN ALT Warning Light

A
  1. Mask- ON/TIGHT
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2
Q

COMPRESSOR STALL or EGT/RPM WARNING LIGHT

A
  1. Throttle- IDLE
  2. EGT/RPM- Check
    If EGT is greater than 450 degrees C 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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3
Q

FIRE WARNING LIGHT

A

GROUND
1. Execute Emergency Shutdown/Egress
TAKEOFF
If decision is made to stop:
1. Abort
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 is confirmed or flight control lost:
3. Eject.
If fire not confirmed and control effectiveness remains:
4. Land as soon as possible.

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4
Q

GTS FIRE WARNING LIGHT

A
  1. Execute Emergency Shutdown/Egress
    IN-FLIGHT
  2. ENGINE switch- OFF
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5
Q

OIL PRESS WARNING LIGHT

A
  1. Throttle- MINIMUM FOR SAFE FLIGHT

2. Minimize throttle movements

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6
Q

OXYGEN WARNING LIGHT

A
  1. Throttle—Increase N2 RPM above 75% (80% above FL300)
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7
Q

BRK PRESS CAUTION LIGHT CATAPULT

A
  1. Suspend Launch
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8
Q

CANOPY CAUTION LIGHT

A
  1. CANOPY control lever- CHECK LOCKED
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9
Q

SKID CAUTION LIGHT/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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10
Q

TP HOT CAUTION LIGHT

A

GROUND
1. Execute Emergency Shutdown/Egress
IN-FLIGHT
1. Throttle- MINIMUM FOR SAFE FLIGHT

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11
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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12
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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13
Q

BRAKE FAILURE- AFLOAT

A
  1. Throttle- IDLE
  2. Parking brake handle- PULL
  3. Hook- DOWN
  4. Transmit
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14
Q

LOSS OF DIRECTIONAL CONTROL

A 
If flyway airspeed available:
1. Go-around
If flyaway airspeed not available:
2. Abort
If blown tire suspected:
3. Brakes- RELEASE
4. ANTI-SKID switch- OFF
5. Brakes- Apply Gradually
If NWS failure suspected:
6. Paddle switch- PRESS
If airborne:
7. Gear and flaps- DO NOT REPOSITION
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15
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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16
Q

EMERGENCY CATAPULT FLYAWAY

A
  1. Throttle- MRT
  2. Maintain 24 units AOA
    If engine failed, or unable to stop settle:
  3. Eject
17
Q

BLOWN TIRE(S) AT THE CARRIER

A
  1. Gear and flaps- DO NOT REPOSITION
18
Q

ENGINE FAILURE

A

If below 1,500 feet AGL and airspeed below 180 KIAS:
1. Eject
If above 1,500 feet AGL or airspeed greater than 180 KIAS:
2. Execute Airstart

19
Q

AIRSTART

A
  1. Emergency oxygen green ring(s)- PULL
  2. Throttle- OFF
    Simultaneously perform steps 3 and 4:
  3. GTS start button- PRESS AND HOLD
  4. Throttle- IDLE
    If unsuccessful (no relight within 30 seconds after moving throttle to idle or EGT exceeds limits): [600+50*c for 10 sec]
  5. Throttle- OFF (allow 30 seconds to drain if practical)
    If within windmill airstart envelope (below 25,000 feet MSL, minimum 13% N2 RPM, recommended minimum 250 KIAS):
  6. Repeat steps 3 and 4
20
Q

ELECTRICAL FIRE

A
  1. GEN switch- OFF
21
Q

SMOKE OR FUMES IN THE 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 occupant/secure loose items
  6. Seat- LOWER
  7. MDC firing handle- PULL
22
Q

LOW/NO MASK FLOW

A

FLIGHT
1. Throttle- Increase N2 RPM above 75% (80% above FL300)
If low/no mask flow continues 10 seconds after increasing N2 RPM:
If cabin altitude above 10,000 feet:
2. Emergency oxygen green ring(s)- PULL
3. OBOGS FLOW selector(s)- OFF

23
Q

TOTAL ELECTRICAL FAILURE

A
  1. Emergency oxygen green ring(s)- PULL
24
Q

UNCOMMANDED ROLL/YAW

A
  1. FLAPS/SLATS lever- RETURN TO PREVIOUS SETTING
25
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 is 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 10,000 feet AGL:
  13. EJECT
26
Q

RAPID DECOMPRESSION

A
  1. Mask- ON/TIGHT
  2. Initiate controlled descent to lowest safe altitude below 18,000 feet MSL
    If rapid decompression results in cabin altitude above 18,000 feet
  3. Emergency oxygen green ring(s)- PULL
  4. OBOGS FLOW selector(s)- OFF
27
Q

ADVERSE PHYSIOLOGICAL SYMPTOMS

A
  1. Initiate controlled descent to below 10,000 feet cabin altitude (approximately 15,000 feet MSL)
  2. Control rate and depth of breathing (approximately one breath every 5 seconds).
    When cabin altitude below 10,000 feet:
  3. Mask- OFF (affected cockpit)
  4. OBOGS FLOW selector- OFF (affected cockpit)
  5. Continue controlling rate and depth of breathing with mask off

T45C IJET (12 decks)

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