Sentera
PHX Unmanned Aircraft Pilot User Guide
www.sentera.com
Page 6
March 19, 2020
844.SENTERA
© 2020 Sentera Inc. All rights reserved.
Table 1: Airspeed
Airspeed
Vstall
22 mph (19 kts, 10 m/s), standard sea level conditions
Vmin
30 mph (26 kts, 13 m/s), autopilot limited
Vcruise
35 mph (30 kts, 16 m/s), autopilot default
Vmax
45 mph (40 kts, 20 m/s)
2.2
Altitude Limits
The PHX UAS autopilot automatically maintains commanded altitude based on the onboard barometric
and Global Positioning System (GPS) altitude sensors. Aircraft altitude limit guidelines are provided in
Table 2: Altitude
Altitude
Minimum recommended cruise altitude
150 ft. (46 m) AGL
Maximum density altitude
14,000 ft. (4300 m) MSL (mean sea level)
Maximum altitude above ground
Flight operations must remain below the maximum altitude
allowed by local regulations or local airspace authority. Often this
means below 400 ft. (120 m) AGL (height above ground).
2.3
Wind Limits
The PHX UAS has recommended operating limits depending on wind speeds, as shown in Table 3: Wind
Table 3: Wind Limits
Wind
Speed
Maximum winds aloft
28 mph (24 kts, 12 m/s)
Maximum crosswind takeoff
5 mph (4 kts, 2 m/s) crosswind component
Maximum crosswind landing
15 mph (13 kts, 7 m/s) crosswind component
2.4
Precipitation and Moisture Limits
Do not fly in precipitation, fog, mist, or clouds.
2.5
GPS Limits
Minimum 10 GPS satellite fix recommended.
2.6
Temperature Limits
The following tables describe the various temperature limits, as shown in Tables 4: Temperature Limits.