## Exhibit B Pinnacl X Fixed Wing Aircraft Procedures

Pinnacl X Page 1 The FW Chameleon and the Ultra S tick 120 and 25e s UAS is not authorized to fly over uncontrolled

, public areas, road ways, boat traffic areas or any other areas which involve flight over privet property

and people.

Equipment

 Aircraft

 Pilot and observer transmitters

 Video receiver and screen or goggles

 Ground control station computer

 Battery cell tester

 Tools

 Sun glasses

 Safety vests

 VHF radio as necessary

 Multirotor Logbook: Flights must be recorded in the flight logbook

Documents

 Pilot; Current class II medical and pilots licenses for fixed wing or rotary wing manned aircraft

 Visual Observer; Current class II medical

 Fixed Wing Aircraft ; FAA Registration

Contact Information

 NOTAM is active

 Contact airspace controlling authority (as necessary)

 Have the phone number of the nearest airspace controlling authority in case of a lost link or

other emergency and or VHF radio tuned to the proper frequency

Preflight Procedure

Takeoff and Landing Site

 Takeoff and landing site secure

 Forced landing areas ident ified

Fixed Wing Aircraft

 Fully charged flight pack maximum allowed cell voltage difference . 1 V

 Autopilot secure on vibration isolation mounts

 GPS secure

 Receiver secure

 Data radio secure

 Video transmitter secure

 Camera secure and camera battery charged

## Exhibit B Pinnacl X Fixed Wing Aircraft Procedures

Pinnacl X Page 2  Secure battery in correct location for a balance aircraft

 CG correct

 Control rods tight (check each flight)

 Motor bolts tight (check each flight)

 Landing gear bolts tight (check each flight)

 Check for cracks in air frame, landing gear , and camera mounts

 Ch eck propellers for cracks and replace as necessary

 Propeller on correctly

 Propeller on tight (try to turn propellers while holding th e motors. Check each flight)

 Motor spring clip check (Pull up on propeller, if the propeller and motor case moves up the shaft

spring clip may be damage or disconnected. Replace motor or install a new clip . Check each

flight )

Aircraft Take off Procedure

 GSC on as necessary

 All switches in correct position on transmitters

 Transmitters on (Pilot and Visual Observer transmitters)

 Battery voltage in transmitters above 9.5 volts

 A ircraft battery connect on

 Establish link between GSC and aircraft , as necessary

 Check aircraft battery voltage on GSC and transmitter

 Range check transmitter , check signal strength

 Video displ ay acceptable on observer transmitter

 Wait for acceptable GPS signal

 Arm aircraft

 Mode set

 Engage motors , start timer

 Slowly advance throttle ( Launch aircraft into wind )

Aircraft In flight Procedure

 Control check in manual mode ( pitch and roll response c heck )

 Check position hold (Set mode to LTR, the aircraft should fly around a point ).

 Check semi

- autonomous flight

 Check autonomous flight

 Fly mission

Aircraft Emergency Procedure

 Loss of power ( Mode manual, best glide, land at forced landing area )

 Unable to fly ( Mode switch to manual, power off, set control surfaces to slowest airspeed)

 Loss of control (switch modes first to semi

- autonomous second to manual and land aircraft

immediately)

## Exhibit B Pinnacl X Fixed Wing Aircraft Procedures

Pinnacl X Page 3  Fly away (note altitude, direction of flight and check timer. Contact airspace controlling

authority and tell them altitude, direction of flight and remaining flight time)

 Transmitter beeps ( Aircraft approaching range limit. Fly aircraft closer)

 Flight out of range ( Aircraft should return to land)

 L ow voltage less th an 10.4 volts, aircraft will return and land.

Aircraft Landing Procedure

 Visual Observer advised pilot around obstacles

 Pilot or visual observer informs nearby people of landing

 Mode set to semi

- autonomous or manual and land aircraft

Maintenance and Test ing

 Maintenance and repair must be recorded in the maintenance log book

 Inspection prior to first flight each day , see preflight inspection

50 hour or 2 months or flight in a dusty environment, inspection and test

 Remove top cover , bottom cover (if on air craft) and top frame plate

 Check for cracks and replace as necessary

 Check the security of the, receiver, data radio, auto pilot, ESC and wiring

 Replace Velcro tape and or vibration mounting as necessary

 Check the ESC connections to the autopilot

 Check the receiver connection to the autopilot and receiver

 Check the wiring to the GPS, buzzer, switch, data radi o, video and power wiring

 Use lock tight medium on bolts and reassemble the top frame

 Recalibrate aircraft as necessary if any of the electronics were replaced

 Range check the pilot an d observer transmitters, see transmitter manuals

 Perform preflight check list

 Bench test aircraft , pitch roll and yaw control with computor . Check maximum power

 Record flights using GSC

 Flight test aircraft (In all cases listed below the fixed wing aircraft must be controllable to pass)

 Manual mode maximum thrust take off and climb out

 Manual mode roll aircraft, loop aircraft, stall and spin aircraft, at mid and maximum throttle

settings

 Manual mode stall sp in aircraft and switch modes to semi

- autonomous . Auto pilot should

recover aircraft

 Fly aircraft a ways away and switch to RTL

 Fly basic patterns in AUTO mode

 Perform post flight check list

100 hr or one year inspection and test

 Perform 50hr inspection an d test

## Exhibit B Pinnacl X Fixed Wing Aircraft Procedures

Pinnacl X Page 4  Replace propellers at 100hrs (Until propeller life is determined)

 Replace motors at 100hrs (Until motor life is determined)

 Replace ESCs at 100hrs (Until ESC life is determined)