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T-45C EPs (PCL IC17 23 NOV 2020) > 1 > Flashcards

1 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
  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 DURING CATAPULT LAUNCH

A
  1. Eject
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4
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

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5
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):
  5. Throttle - OFF (allow 30 seconds to drain if practical)
    If within windmill airstart envelope (below 25,000 feet MSL, minimum 13% N2 RPM, recommend minimum 250 KIAS):
  6. Repeat steps 3 and 4
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6
Q

COMPRESSOR STALL //

EGT/RPM WARNING LIGHT

A
  1. Throttle - IDLE
  2. EGT/RPM - CHECK
    If EGT is greater than 450 C for more than 6 seconds after throttle IDLE:
  3. Execute Engine Failure procedure
    If EGT responds normally:
  4. Throttle - slowly advance to minimum for safe flight
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7
Q

ABORT

A
  1. Throttle - IDLE
  2. Speed brakes - EXTEND
  3. Brakes - APPLY
  4. Hook - DOWN (IF REQUIRED)
  5. Release brakes prior to crossing the arresting gear
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8
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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9
Q

UNCOMMANDED ROLL/YAW

A
  1. FLAPS/SLATS lever - RETURN TO PREVIOUS SETTING
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10
Q

BLOWN TIRE(S) AT THE CARRIER

A
  1. Gear and flaps - DO NOT REPOSITION
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11
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. Attempt braking
If brakes still unavailable:
6. Hook - DOWN (IF REQUIRED)
7. Parking brake handle - PULL (IF REQUIRED)
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12
Q

BRAKE FAILURE - AFLOAT

A
  1. Throttle - IDLE
  2. Parking brake handle - PULL
  3. Hook - DOWN
  4. Transmit
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13
Q

LOSS OF DIRECTIONAL CONTROL

A 
If flyaway 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
If NWS failure suspected:
6. Paddle switch - PRESS
If airborne:
7. Gear and flaps - DO NOT REPOSITION
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14
Q

TOTAL ELECTRICAL FAILURE

A
  1. Emergency oxygen green ring - PULL
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15
Q

ELECTRICAL FIRE

A
  1. GEN switch - OFF
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16
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:
  3. Airspeed - REDUCE
  4. Warn other occupant / secure loose items
  5. Seat - LOWER
  6. MDC firing handle - PULL
17
Q

OXYGEN WARNING LIGHT

A
  1. Emergency oxygen green ring(s) - PULL
  2. OBOGS FLOW selector(s) - OFF
  3. Initiate rapid descent to below 10,000 FEET MSL OR MINIMUM SAFE ALTITUDE
18
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
19
Q

GTS FIRE

A

GROUND
1. Execute Emergency Shutdown / Egress
IN-FLIGHT
1. ENGINE switch - OFF

20
Q

OIL PRESS

A
  1. Throttle - MINIMUM FOR SAFE FLIGHT

2. Minimize throttle movements

21
Q

BRK PRESS CAUTION LIGHT

A
  1. Suspend launch
22
Q

CANOPY CAUTION LIGHT

A
  1. CANOPY control lever - CHECK LOCKED
23
Q

TP HOT

A

GROUND
1. Execute Emergency Shutdown / Egress
IN-FLIGHT
1. Throttle - Minimum for safe flight

24
Q

SIM MODE

A
  1. Revert to standby instruments
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 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
26
Q

SKID CAUTION LIGHT

A 
1. Go-around if practical
If go-around not practical:
2. Brakes - RELEASE
3. ANTI-SKID switch - OFF
4. Brakes - Apply gradually
27
Q

LOW/NO MASK FLOW

A

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

28
Q

RAPID DECOMPRESSION

A
  1. Mask - ON/TIGHT
  2. Initiate controlled descent to lowest safe altitude below 18,000 feet MSL
    If rapid decompression result in cabin altitude above 18,000 feet:
  3. Emergency oxygen green ring(s) - PULL
  4. OBOGS FLOW selector(s) - OFF
29
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
30
Q

CABIN ALT CAUTION LIGHT

A
  1. Mask - ON/TIGHT

T-45C EPs (PCL IC17 23 NOV 2020) (1 decks)

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