New EP Flashcards
Cabin Alt Warning light in flight
*1. Mask – ON/TIGHT
COMPRESSOR STALL OR EGT/RPM WARNING LIGHT
IN-FLIGHT
*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
FIRE WARNING LIGHT
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
GTS FIRE WARNING LIGHT
GROUND
*1. Execute Emergency Shutdown/Egress
IN-FLIGHT
*1. ENGINE switch - OFF
OIL PRESS WARNING LIGHT
- Throttle – MINIMUM FOR SAFE FLIGHT
* 2. Minimize throttle movements
OXYGEN WARNING LIGHT
AFTER TAKEOFF:
*1. Throttle – Increase N2 rpm above 75% (80% above FL300)
BRK PRESS CAUTION LIGHT
CATAPULT
*1. Suspend launch
CANOPY CAUTION LIGHT
CANOPY control lever – CHECK LOCKED
SKID CAUTION LIGHT
*1. Go-around if practical If go-around not practical: *2. Brakes – RELEASE *3. ANTI-SKID switch - OFF *4. Brakes – Apply gradually
TP HOT CAUTION LIGHT
GROUND
*1. Execute Emergency Shutdown/Egress
IN-FLIGHT
*1. Throttle – MINIMUM FOR SAFE FLIGHT
CLEAR ENGINE PROCEDURE/ABNORMAL START/TP FIRE ON SHUTDOWN
*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
EMERGENCY SHUTDOWN/EGRESS
- Throttle - OFF
- ENGINE switch - OFF
- FUEL SHUTOFF handle - PULL
- Ejection seats - SAFE
- BATT switches - OFF
BRAKE FAILURE — ASHORE
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)
BRAKE FAILURE — AFLOAT
- Throttle - IDLE
- Parking brake handle - PULL
- Hook - DOWN
- Transmit
LOSS OF DIRECTIONAL CONTROL
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
ABORT
- Throttle - IDLE
- Speed brakes - EXTEND
- Brakes - APPLY
- Hook – DOWN (if required)
- Release brakes prior to crossing the arresting gear
EMERGENCY CATAPULT FLYAWAY
*1. Throttle - MRT
*2. Maintain 24 units AOA
If engine failed, or unable to stop settle:
*3. Eject
ENGINE FAILURE DURING CATAPULT LAUNCH
*1. Eject
BLOWN TIRE(S) AT THE CARRIER
*1. Gear and flaps – DO NOT REPOSITION
ENGINE FAILURE
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
AIRSTART
*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.
ELECTRICAL FIRE
*1. GEN switch - OFF
SMOKE OR FUMES IN THE COCKPIT
*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
RAPID DECOMPRESSION
*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
LOW/NO MASK FLOW
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
ADVERSE PHYSIOLOGICAL SYMPTOMS
*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
TOTAL ELECTRICAL FAILURE
*1. Emergency oxygen green ring(s) - PULL
UNCOMMANDED ROLL/YAW
*1. FLAPS/SLATS lever – RETURN TO PREVIOUS SETTING
DEPARTURE/SPIN PROCEDURE
*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
