EPs Flashcards
COMPRESSOR STALL
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.
EGT/RPM WARNING LIGHT
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.
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
- 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
- Throttle - OFF
- ENGINE switches - ON
- FUEL SHUTOFF handle - DOWN
- GTS - START
- IGNITION switch - ISOLATE
When rpm below 20% and GTS advisory light illuminates: - ENGINE switch - START.
ABNORMAL START
- Throttle - OFF
- ENGINE switches - ON
- FUEL SHUTOFF handle - DOWN
- GTS - START
- IGNITION switch - ISOLATE
When rpm below 20% and GTS advisory light illuminates: - ENGINE switch - START.
TP FIRE ON SHUTDOWN
- Throttle - OFF
- ENGINE switches - ON
- FUEL SHUTOFF handle - DOWN
- GTS - START
- IGNITION switch - ISOLATE
When rpm below 20% and GTS advisory light illuminates: - 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. Attept 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
- Throttle - MRT
- Maintain 24 units AOA.
If engine failed, or unable to stop settle: - Eject.
BLOWN TIRE(S) AT THE CARRIER
- 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
- Emergency oxygen green ring(s) - PULL
- Throttle - OFF
Simultaneously perform steps 3. and 4. - GTS start button - PRESS AND HOLD
- Throttle - IDLE
If unsuccessful (no relight within 30 seconds after moving throttle to idle or EGT exceeds limits): - 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): - Repeat steps 3. and 4.
ELECTRICAL FIRE
GEN switch - OFF
SMOKE OR FUMES IN THE COCKPIT
- 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: - Airspeed - REDUCE (as practical)
- Warn other cockpit occupant/secure loose items.
- Seat - LOWER
- MDC firing handle - PULL.
LOW/NO MASK FLOW (IN FLIGHT)
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
TOTAL ELECTRICAL FAILURE
- Emergency oxygen green ring(s) - PULL.
UNCOMMANDED ROLL/YAW
- FLAPS/SLATS lever - RETURN TO PREVIOUS SETTING.
DEPARTURE/SPIN PROCEDURE
- Controls - NEUTRALIZE/FORCIBLY CENTER RUDDER PEDALS.
- Speed brakes - RETRACT.
- Throttle - IDLE.
- 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):
- Rudder pedal - FULL OPPOSITE TURN NEEDLE.
- Lateral stick - FULL WITH TURN NEEDLE.
- 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
PCL Only ENGINE FAILURE DURING CATAPULT LAUNCH
- EJECT.
CABIN ALT WARNING LIGHT
IN-FLIGHT:
1. Mask – ON/TIGHT
RAPID DECOMPRESSION
- Mask – ON/TIGHT
- Initiate controlled descent to lowest safe altitude below 18,000 ft MSL.
If rapid decompression results in cabin altitude above 18,000 ft:
- Emergency oxygen green ring(s) – Pull
- OBOGS FLOW selector(s) – OFF
ADVERSE PHYSIOLOGICAL SYMPTOMS
- Initiate controlled descent to below 10,000 ft cabin altitude (approximately 15,000 ft MSL)
- Control rate and depth of breathing (approximately one breath every 5 seconds).
When cabin altitude below 10,000 ft: - Mask – OFF (affected cockpit)
- OBOGS FLOW selector – OFF (affected cockpit)
- Continue controlling rate and depth of breathing with mask off.
