uAvionix AV-30-E - Page 101

UAV-1004234-001, AV-30-E Installation Manual 101
Rev H
Figure 38 – Setup Done / Exit Option
Record configured values on a printed copy of Table 13-1, and retain in
aircraft records.
Table 13-1 – Installation Menu Setting
Label
Description
Possible Values
Configured
Value(s)
UNIT FUNCTION
Unit functionality
Set to default mode: AI* or
DG
FUNCTION LOCK
Functionality Lock
If locked, pilot may not
change unit function
PITCH TRIM
Pitch trim
Trim as needed: ±27 Degrees
(0*)
ROLL TRIM
Roll trim
Trim as needed: ±5 Degrees
(0*)
SLIP TRIM
Slip trim
Trim as needed: ±5 Degrees
(0*)
OAT TRIM
OAT probe trim
Trim as needed: ±200
(Unitless) (0*)
SPD ASST
Use airspeed to enhance
attitude calculation
Yes* (on) or No (off)
IAS TRIM LO
IAS trim at low speed
Trim as needed: ±100 (in IAS
UNITS) (0*)
IAS TRIM HI
IAS trim at high speed
Trim as needed: ±100 (in IAS
UNITS) (0*)
ALT TRIM LO
Barometric altitude trim
Trim as needed: ±500 Feet
ALT TRIM HI
Barometric altitude trim

ALT TRIM LO
Trim as needed: ±500 Feet
PITOT ZERO
Pressure sensor age
compensation
Automatically determined by
measurement
AOA FUNC
Angle of Attack Alert
ENABLED*, DISABLED
IAS UNITS
IAS display units (also
affects groundspeed and
V-speed settings units)
Knots* (KTS), Miles Per Hour
(MPH), or Kilometers Per
Hour (KPH)
TAS UNITS
TAS display units
Knots* (KTS), Miles Per Hour
(MPH), or Kilometers Per
Hour (KPH)
IAS VSO
Stalling speed in landing
configuration
Set to match limits: 40 to 555
(50*) in IAS UNITS
IAS VS1
Stalling speed in a
specific configuration
Set to match limits: 40 to 555
(60*) in IAS UNITS
IAS VFE
Maximum flap extended
speed
Set to match limits: 40 to 555
(100*) in IAS UNITS