Hornet Red Page Flashcards
(20 cards)
Apu Fire
In flight/On Ground 1. APU Fire light - push 2. Fire extinguisher ready light - push On Ground 3. Both Throttles - Off 4. Egress
Egress
- Canopy - Open
- Both Throttles - Off
- Manual Override Handle - Actuate
- Parachute fittings - Disconnect
- Lap Belt Fasteners - Disconnect
- O2 Hose and comm cord - Pull to disconnect from ssk
- Egress
Hot Start
If EGT climbs rapidly through 750*c
- L/R throttle - Off
- Engine - Crank until EGT below 200*c. If starter had cut out, re-engage when rpm is below 30%
(refer to white page, start anomalies, pg 10)
Ground Fire
- Both throttles - Off
- Both engine fire warning lights - Push
- APU switch - Off
- Egress
L/R Engine Fire
on ground 1. Both throttles - off 2. L/R engine fire warning light - Push 3. Fire extinguisher ready light - push 4. Battery switch - off 5. Egress In flight 1. L/R throttle - off 2. L/R engine fire warning light - push 3. Fire extinguisher ready light - push 4. Arresting hook - Down
L Bleed & R Bleed (Dual)
- Both throttles - minimum practical for flight
- Bleed air knob - Off (Do not cycle)
- Maintain aircraft altitude below 25 000ft
- Arresting hook - Down
- Land as soon as possible
(refer to yellow page emergencies, single bleed section for “when av air hot caution appears”, pg E24)
Engine Fire / Thrust loss on Takeoff
If decision to stop is made
1. Abort
If takeoff is continued
1. Both throttles - Max
2. AOA - Maintain on-speed balanced flight
3. External stores - Jettison (if required)
Abort
- Both throttles - Idle
- Speed Brake - As desired
- Brakes - Apply
- Arresting hook - Down (if required)
- Brakes - Release prior to crossing arresting cable
If aircraft is about to leave runway in uncontrolled condition - Eject
Emergency Brakes
- Brakes - Release
- Emergency Brake Handle - Pull to detent
- Brake pedal pressure - use caution
If aircraft is about to leave runway in uncontrolled condition - Eject
Directional Control Problem on Takeoff or Landing Rollout
(Includes NWS / Brake problems, Planing-Link Failure, or Blown Tire) If decision to stop is made 1. Both throttles - Idle 2. Speed Brake - In If nose wheel steering failure is suspected 3. Paddle switch - Push Otherwise 4. nosewheel steering - Low (with rudders neutral) 5. Emergency brakes - Select 6. Good tire/side - Use light braking 7. Arresting hook - Down (if required) if a/c is about to leave runway in uncontrolled condition 8. Eject if decision to takeoff is made 1. Both throttles - max 2. Speed brake - In 3. AOA - maintain on-speed 4. landing gear and flaps - leave down 5. Engine instruments - monitor Safely airborne carry out procedure for landing with a blown tire, pg E48, Landing with a planing-link failure, pg e54, or NWS (failure), pg e34 as appropriate
Engine voice alerts (L/R in temp, L/R EGT high, L/R ovrspd, L/R Flameout, L/R oil pr caution, L/R vib hi displays)
1. L/R throttle - Idle If engine does not stabilize at normal in-flight idle parameters 2. L/R throttle - Off if practical in all cases 3. Land as soon as practical
L/R Stall / Compressor stall
- Both throttles - Reduce
- L/R throttle (affected engine) - Idle
If stall does not clear - L/R throttle (affected engine) - Off
In any case - Oxygen - 100%
- Land as soon as possible
If an engine is shut down, it should not be restarted unless other overriding considerations are present.
Oxygen
If restriction in flow or signs of hypoxia are experienced
- Emergency-oxygen green ring - Pull
- Oxygen - 100%
- Oxygen system - select off
- Breathe normally
- Descend immediately below 10 000 feet, cockpit altitude
- Land as soon as possible
Smoke / Fumes / Fire in Cockpit
- Oxygen - 100%
- Cabin pressure switch - Ram/Dump
- If practical - Descend below 25, 000FT
- Cabin temperature knob - Full Cold
- Airspeed - 200 to 300 KT
if unable to clear smoke - Canopy - Jettison
If electrical fire is present - All electrical equipment - off
- UFC avionics - off
- Required electrical equipment - on
Double Gen or Double TR failure
- Batt SW caution light - check on
If Batt SW caution light is not illuminated - Batt SW - ORIDE
In any case (light illuminated or not) - Radar - Off
- Gen switches ( double generator failure only) - Cycle individually
(refer to yellow page emergencies for double gen or double TR failure, pg e18)
DEL / Mech on or FCES
- Speedbrake - check in
- Airspeed - Decelerate slowly to below 400 KT/ Mach 0.8
(refer to yellow pg DEL on Pg e29, Mech on pg E30, and FCES pg e28)
Out-of-control Recovery
Departure / Falling leaf recovery 1. Controls - Release/Feet of Rudders/Speedbrake in 2. Both throttles - Idle If still out of control 3. Altitude, AOA, airspeed and yaw rate - check When recovery indicated by AOA and yaw rate tones removed, side-forces subside, and airspeed accelerating above 180 knots 4. Recover passing 6000ft AGL, dive recovery not initiated 5. Eject Spin Recovery Command arrow present 1. Lateral stick - full with arrow Command arrow not present 2. Spin recovery switch - RCVY 3. Lateral stick - Full with arrow when yaw rate stops 4. Lateral stick - smoothly neutral 5. Spin recovery switch - check norm when recovery indicated 6. Recover passing 6000ft AGL, dive recovery not initiated 7. Eject
Single-Engine failure in landing configuration
- Both throttles - Mil or Max
- AOA - Maintain on-speed and balanced flight
- Flaps - Half
Immediate Ejection
In extreme emergency situations, pilot shall immediately initiate ejection. If time and conditions permit, refer to yellow page emergencies for ejection, page e17
- Zoom and level wings
- Assume ejection position
- Command the ejection
- Ejection handle - Pull
Runaway Gun
Aircraft - Recover Master Arm switch - Safe Keep aircraft pointed in a safe direction Return to base and do not attempt firing Have aircraft put in quarantine