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T-45 EP 21' > EPs > Flashcards

EPs Flashcards

1
Q

COMPRESSOR STALL

A

In-Flight
1. Throttle - IDLE
2. EGT/RPM - CHECK
If EGT is greater than 450*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.

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2
Q

EGT/RPM WARNING LIGHT

A

In-Flight
1. Throttle - IDLE
2. EGT/RPM - CHECK
If EGT is greater than 450*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.

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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.
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4
Q

GTS FIRE WARNING LIGHT

A

GROUND
1. Execute Emergency Shutdown/Egress.
IN-FLIGHT
1. 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

AFTER TAKEOFF:
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

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

A
  1. Throttle - OFF
  2. ENGINE switches - ON
  3. FUEL SHUTOFF handle - DOWN
  4. GTS - START
  5. IGNITION switch - ISOLATE
    When rpm below 20% and GTS advisory light illuminates:
  6. ENGINE switch - START.
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12
Q

ABNORMAL START

A
  1. Throttle - OFF
  2. ENGINE switches - ON
  3. FUEL SHUTOFF handle - DOWN
  4. GTS - START
  5. IGNITION switch - ISOLATE
    When rpm below 20% and GTS advisory light illuminates:
  6. ENGINE switch - START.
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13
Q

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% and GTS advisory light illuminates:
  6. ENGINE switch - START.
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14
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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15
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. Attept braking.
If brakes still unavailable:
6. Hook - DOWN (if required)
7. Parking brake handle - PULL (if required)
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16
Q

BRAKE FAILURE - AFLOAT

A
  1. Throttle - IDLE
  2. Parking brake handle - PULL
  3. Hook - DOWN
  4. Transmit
17
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.
18
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.
19
Q

EMERGENCY CATAPULT FLYAWAY

A
  1. Throttle - MRT
  2. Maintain 24 units AOA.
    If engine failed, or unable to stop settle:
  3. Eject.
20
Q

BLOWN TIRE(S) AT THE CARRIER

A
  1. Gear and flaps - DO NOT REPOSITION.
21
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.

22
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, recommended minimum 250 KIAS):
  6. Repeat steps 3. and 4.
23
Q

ELECTRICAL FIRE

A

GEN switch - OFF

24
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:
  2. Airspeed - REDUCE (as practical)
  3. Warn other cockpit occupant/secure loose items.
  4. Seat - LOWER
  5. MDC firing handle - PULL.
25
Q

LOW/NO MASK FLOW (IN FLIGHT)

A

FLIGHT:
1. Throttle – Increase N2 RPM above 75% (80% above FL 300)
If no mask flow or low mask flow continues 10 seconds after increasing RPM and cabin altitude above 10,000 ft:
2. Emergency oxygen green ring(s) – PULL
3. OBOGS FLOW selector(s) – OFF

26
Q

TOTAL ELECTRICAL FAILURE

A
  1. Emergency oxygen green ring(s) - PULL.
27
Q

UNCOMMANDED ROLL/YAW

A
  1. FLAPS/SLATS lever - RETURN TO PREVIOUS SETTING.
28
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):

  1. Rudder pedal - FULL OPPOSITE TURN NEEDLE.
  2. Lateral stick - FULL WITH TURN NEEDLE.
  3. Longitudinal stick - NEUTRALIZE.

If recovery indicated or airspeed increasing through 160KAIS:
11. Lateral stick - NEUTRALIZE.
When recovery indicated:
12. Rudder pedals - SMOOTHLY CENTER.
If out of control passing through 10,000 feet AGL:
13. EJECT

29
Q

PCL Only ENGINE FAILURE DURING CATAPULT LAUNCH

A
  1. EJECT.
30
Q

CABIN ALT WARNING LIGHT

A

IN-FLIGHT:

1. Mask – ON/TIGHT

30
Q

RAPID DECOMPRESSION

A
  1. Mask – ON/TIGHT
  2. Initiate controlled descent to lowest safe altitude below 18,000 ft MSL.

If rapid decompression results in cabin altitude above 18,000 ft:

  1. Emergency oxygen green ring(s) – Pull
  2. OBOGS FLOW selector(s) – OFF
31
Q

ADVERSE PHYSIOLOGICAL SYMPTOMS

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

T-45 EP 21' (1 decks)

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