1 Flashcards
1
Q
CLEAR ENGINE PROCEDURE //
ABNORMAL START //
TP FIRE ON SHUTDOWN
A
- Throttle - OFF
- ENGINE switches - ON
- FUEL SHUTOFF handle - DOWN
- GTS - START
- IGNITION switch - ISOLATE
When RPM below 20 percent and GTS advisory light illuminates: - ENGINE switch - START
2
Q
EMERGENCY SHUTDOWN / EGRESS
A
- Throttle - OFF
- ENGINE switch - OFF
- FUEL SHUTOFF handle - PULL
- Ejection seats - SAFE
- BATT switches - OFF
3
Q
ENGINE FAILURE DURING CATAPULT LAUNCH
A
- Eject
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
5
Q
AIRSTART
A
- 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, recommend minimum 250 KIAS): - Repeat steps 3 and 4
6
Q
COMPRESSOR STALL //
EGT/RPM WARNING LIGHT
A
- Throttle - IDLE
- EGT/RPM - CHECK
If EGT is greater than 450 C for more than 6 seconds after throttle IDLE: - Execute Engine Failure procedure
If EGT responds normally: - Throttle - slowly advance to minimum for safe flight
7
Q
ABORT
A
- Throttle - IDLE
- Speed brakes - EXTEND
- Brakes - APPLY
- Hook - DOWN (IF REQUIRED)
- Release brakes prior to crossing the arresting gear
8
Q
EMERGENCY CATAPULT FLYAWAY
A
- Throttle - MRT
- Maintain 24 units AOA
If engine failed, or unable to stop settle: - Eject
9
Q
UNCOMMANDED ROLL/YAW
A
- FLAPS/SLATS lever - RETURN TO PREVIOUS SETTING
10
Q
BLOWN TIRE(S) AT THE CARRIER
A
- Gear and flaps - DO NOT REPOSITION
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)
12
Q
BRAKE FAILURE - AFLOAT
A
- Throttle - IDLE
- Parking brake handle - PULL
- Hook - DOWN
- Transmit
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
14
Q
TOTAL ELECTRICAL FAILURE
A
- Emergency oxygen green ring - PULL
15
Q
ELECTRICAL FIRE
A
- GEN switch - OFF
16
Q
SMOKE OR FUMES IN THE COCKPIT
A
- Mask - ON/TIGHT
- 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
- Warn other occupant / secure loose items
- Seat - LOWER
- MDC firing handle - PULL
17
Q
OXYGEN WARNING LIGHT
A
- Emergency oxygen green ring(s) - PULL
- OBOGS FLOW selector(s) - OFF
- 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
- Throttle - MINIMUM FOR SAFE FLIGHT
2. Minimize throttle movements
21
Q
BRK PRESS CAUTION LIGHT
A
- Suspend launch
22
Q
CANOPY CAUTION LIGHT
A
- 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
- Revert to standby instruments
25
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
26
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
```
27
LOW/NO MASK FLOW
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
RAPID DECOMPRESSION
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
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
30
CABIN ALT CAUTION LIGHT
1. Mask - ON/TIGHT
