Section 3 Flashcards
Define Land As Soon As Possible.
Emergency will be declared
Landing should be accomplished at the nearest suitable field
Define Land As Soon As Practical.
Emergency conditions less urgent
Mission should be terminated
Landing at nearest suitable airfield is not necessary.
GCS Loss of line power.
Push in UPS if pulled out
Send Emergency mission
Get alternate power
Smoke, Fumes, Fire in GCS
Evacuate Personnel
Turn off Power Distribution Circuit breakers
Hit the EPO button on the way out
Pilot Monitor Failure
Loss of video and telemetry
Use sensor display
Reset monitor
Rack Switch if necessary
Pilot Video Source Failure
No video, but still telemetry
Check sensor operator video
Switch to the sensor video source
PSO 2 Rack Lock-up Causes
Loading large map files Loading multiple maps at a time Typing with mouse on the tracker Leaving a route in edit mode Too many commands at once
PSO 2 Rack Lock-up Actions
Turn Off/On the Processor Assembly Power Switch 2
If CCSM warning still up, turn of/on console switch
If functionallity restored, data loggers on, gcs vid source slaved
PSO 1 Rack Lock Up
If unable to control aircraft, sensor bring up flight graphics and match console commands (CONDITION LEVER) Speed lever must be at least 96% Verify Emergency mission Perform Checklist rack switch Reboot rack Switch back Reset everything
AN/DAS-1 Reset
Select rate mode (N: prevents rapid movement)
Reset
If no functionallity, cycle power
(W: LTM may fire for two seconds when reset or powered on)
Engine Fire/Engine RPM Decay on the Ground
CONDITION LEVER - AFT Monitor EGT/RPM decrease GCS Ignition COld Perform if link is lost (W: If weapons installed, 4000 ft safety zone, stay upwind)
Loss of Control Prevent
LANDING CONFIGURATION - COMMAND
PAYLOAD - POSITION MODE
Reference other checklist that caused the loss of control
Come back to close out checklist
Structural Failure
Perform Controllability check
Controllability check
LR crew performs this checklist
Airframe Icing
Execute when in icing or potentially entering icing Execute AOA sensor fail or airspeed / pitot/static fail checklist first as required Exit icing conditions Pitot Heat - On Verify alpha probe functional Stall Protect on unless for AOA reasons Ignitors - On Stall plus 15 Swing Ball
AOA Sensor fail
Pitch oscillations Stall protect off Autopilot hold set as required Stall plus 15 Controlability check Land as soon as practical
Airspeed or pitot/static failure
Occurs during icing usually If single, land as soon as practical If multiple, (C: pitch oscillations, lost link, be ready to take off autopilot mode) Preprogram - off airspeed hold - off Pitot heat - verify on Use AOA as speed reference (Max 2) Controlability Land ASAP
Multiple Nav Sensor Failure
HDD warnings Information could be inaccurate Fly to C-Band range Notify LRE Update Emergency mission Perform losing handover Monitor through landing as practical
Autopilot sensor failure
HDD warnings Uncommanded movements AP sensor verify auto Land as soon as practical If all sensors failed, its a bad day
UARB Failure
Loss of 5V or 12V power between BJA and RCM
VIT 58-61
UARB Select - Verify auto
Land as soon as practical
FCA Failure
Check CCDL health on VIT 54
Processor Select - Verify auto
Land as soon as practicall
Flight Control Servo Overheat
HDD
Check VIT 8
Turn off autopilot hold modes to alleviate servo overheat
Monitor servo amp draw
(C: if aileron or tail servo enters red region land as soon as possible)
Controllability check
Engine Failure
(Note: If "engine out detected" but still good indications check VIT 65 EFIU is zero, that means tach gen failure) GLIDE - ESTABLISH LANDING SITE - SELECT CONDITION LEVER - AFT AS REQUIRED Hack clock (C: Dont allow windmill between 18-28) IF TIME/CONDITIONS permit attempt resart Shed electricals (C: Min fuel temp is -40C) (N: Jettison weapons prior to turning SMS off) Monitor battery time Monitor battery voltage (C: battery voltage below 22 all electrical power will be lost, lower gear prior) Condition lever - aft as required GCS Ignition - cold Optimize KU for landing Gear down as required Forced Landing
Engine Air Restart
Consider tach gen failure Fuel mode auto Condition lever full forward GCS ignition Hot Airspeed 100-180 Throttle 20% Speed Lever High RPM verify increase EGT Monitor Oil PX - normal IF no restart Go to engine control menu and continue checklist
Generator Failure
Can be caused by engine failure Hack clock Reset generator Successful? Land as soon as practical Not successful Reduce electrical load Reset again Successful? Land as soon as practical Not successful Monitor time and voltage Compute Land time Land ASAP Consider landing with SPMA off
Engine Overheat
Red EGT indication
Throttle as required to maintain safe altitude
Land ASAP
Engine Fire
Condition lever aft as required
If aft, then run engine failure checklist
Land ASAP Come back to close checklist
Engine Throttle Control Failure
Lack of response to throttle movement
Perform engine failure checklist is power inadequate for flight
If adequate land ASAP
If unable to descend - shut down when in range
Torque Indication Failure
Torque is 0 or 120
HDD Closed loop power - failed
Autopilot hold modes off
Verify fuel flow rate and make sure it makes sense
If not, closed loop power off and land as soon as practical
Engine Speed Control Failure
Lack of response to speed lever movement Check engine speed Select DEEC mode backup Backup should restore RPM to 100 If 100% available land as soon as practical If not 100% land ASAP
DEEC Failure
Check cruise mode status
