Immediate Actions
Limitations
Emergency/ Flight Logics
WCA/AV Panel
Misc.
100

UGCS Electrical Power Failure

Heading - RTB

100

Max Flight Hours

9 Hours

100

Glide Logic

-Dual Up link loss for 2 seconds

1.) Throttle Returns to idle

2.) Flaps in prior commanded position

3.) All flight surfaces deflect neutral (to maintain wings level)




100

High Engine Temps

- av high engine temps

100

Where are inspections found

-18

200

Engine Failure Below 2,000 Feet AGL

Safe Heading - Establish

FTS - Deploy

200

Service Ceiling

16,000 ft MSL

200

Waveoff

WHAT IS

-proceed to the waveoff waypoint

-loiter at the waveoff altitude and airspeed

200

Generator Failure (No RPMs above 2000 ft AGL)

- engine fail above 2000 feet

200

what chapter of what TM is power up and power down found?

Chapter 8 10-2

300

 AV Generator Failure

Safe Heading - Establish

Vehicle Lights - All off, as required

Airspeed - Set

Bus Voltage - Monitor

Li-ion Battery Status  - Monitor time remaining/capacity




300

Duration at Max RPM (Ground)

10 seconds, operator command

300

Launch

WAT IZ

-causes AV to execute its internal launch routine

-maximum rpm

-straight level climb

-knobs flight mode automatically selected at approximately 1,000 ft AGL
300

servo fail (altitude continues to climb)

- stuck throttle high

300

Max flight time

9 hours

400

AV Fire on Launcher

Abort, Abort, Abort Fire on launcher - Announce(CE)

LHCU launch switch cover - closed (CE)

Throttle - Idle

Engine - Cut

LHCU pressurize switch - Off (CE)

LHCU safe when lit lamp - illuminated (CE)

LHCU HPU switch - off (CE)


400

Maximum Commanded Airspeed (Level Flight)

Refer to Table 7-13

400

Step 22 in the Preflight

AV Battery Test

500

Launcher Failure

Standby - Announce (CE)

LHCU launch switch - Release to hold position (CE)

LHCU ready to launch when lit lamp - illuminated (CE)

LHCU launch switch - launch (CE)

Step 2-Step 4: Repeat One More Time (CE)

Launcher Fail - Announce (CE)

LHCU launch switch cover - closed (CE)

LHCU pressurize switch - off (CE)

LHCU safe when lit lamp - illuminated (CE)

LHCU HPU switch - off (CE)

500

Allowable Fluctuation, on ground, engine running

+/- 3 VDC initial +/- 1 VDC prior to AV takeoff

500

who takes three days to complete presets and preflight

 PV2 Kenny Johnson

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