EasyManua.ls Logo

Vertical Technologies DeltaQuad V1 - Page 32

Default Icon
67 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
The airframe conforms with all local rules and regulations and is permitted to fly the intended mission.
The propellers are mounted in the correct position, orientation and direction as specified in the
.Assembly section
Visual inspection for damage, dirt, correctly mounted and securely fastened:
Propellers
Motors
Wings
Servos
Elevons
Devices inside the fuselage
Flight battery
Before closing hatch
When the vehicle sits outside, the hatch must not be closed until the vehicle is ready for takeoff as the
components inside could overheat when sitting idle. Exposure to direct sunlight when idle for more than
5 minutes should be avoided.
Flight battery - Securely attached, moved as far forward as possible, connector fully joined.
Telemetry - Attached and working.
SD-card installed.
Aileron linkage - Properly secured without slop or play.
Payload sits within the payload bay (center bay) and does not exceed 1.2kg.
Components inside the fuselage are securely fastened and cannot move during flight.
After closing hatch
Hatch secured (unable to pull up)
Hatch sits flush with the fuselage (no obstructions under the hatch legs)
VTOL modules and wing joiners properly secured with lock clips down.
Before takeoff
Weather conditions and mission within . tolerances