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Dash 1 > Section 3 > Flashcards

Section 3 Flashcards

1
Q

Define Land As Soon As Possible.

A

Emergency will be declared

Landing should be accomplished at the nearest suitable field

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2
Q

Define Land As Soon As Practical.

A

Emergency conditions less urgent
Mission should be terminated
Landing at nearest suitable airfield is not necessary.

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3
Q

GCS Loss of line power.

A

Push in UPS if pulled out
Send Emergency mission
Get alternate power

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4
Q

Smoke, Fumes, Fire in GCS

A

Evacuate Personnel
Turn off Power Distribution Circuit breakers
Hit the EPO button on the way out

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5
Q

Pilot Monitor Failure

A

Loss of video and telemetry
Use sensor display
Reset monitor
Rack Switch if necessary

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6
Q

Pilot Video Source Failure

A

No video, but still telemetry
Check sensor operator video
Switch to the sensor video source

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7
Q

PSO 2 Rack Lock-up Causes

A 
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
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8
Q

PSO 2 Rack Lock-up Actions

A

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

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9
Q

PSO 1 Rack Lock Up

A 
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
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10
Q

AN/DAS-1 Reset

A

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)

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11
Q

Engine Fire/Engine RPM Decay on the Ground

A 
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)
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12
Q

Loss of Control Prevent

A

LANDING CONFIGURATION - COMMAND
PAYLOAD - POSITION MODE
Reference other checklist that caused the loss of control
Come back to close out checklist

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13
Q

Structural Failure

A

Perform Controllability check

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14
Q

Controllability check

A

LR crew performs this checklist

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15
Q

Airframe Icing

A 
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
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16
Q

AOA Sensor fail

A 
Pitch oscillations
Stall protect off
Autopilot hold set as required
Stall plus 15
Controlability check
Land as soon as practical
17
Q

Airspeed or pitot/static failure

A 
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
18
Q

Multiple Nav Sensor Failure

A 
HDD warnings
Information could be inaccurate
Fly to C-Band range
Notify LRE
Update Emergency mission
Perform losing handover
Monitor through landing as practical
19
Q

Autopilot sensor failure

A 
HDD warnings
Uncommanded movements
AP sensor verify auto
Land as soon as practical
If all sensors failed, its a bad day
20
Q

UARB Failure

A

Loss of 5V or 12V power between BJA and RCM
VIT 58-61
UARB Select - Verify auto
Land as soon as practical

21
Q

FCA Failure

A

Check CCDL health on VIT 54
Processor Select - Verify auto
Land as soon as practicall

22
Q

Flight Control Servo Overheat

A

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

23
Q

Engine Failure

A 
(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
24
Q

Engine Air Restart

A 
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
25
Q

Generator Failure

A 
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
26
Q

Engine Overheat

A

Red EGT indication
Throttle as required to maintain safe altitude
Land ASAP

27
Q

Engine Fire

A

Condition lever aft as required
If aft, then run engine failure checklist
Land ASAP Come back to close checklist

28
Q

Engine Throttle Control Failure

A

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

29
Q

Torque Indication Failure

A

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

30
Q

Engine Speed Control Failure

A 
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
31
Q

DEEC Failure

A

Check cruise mode status

Dash 1 (4 decks)

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