uAvionix AV-30-E Installation Manual page 101

Record configured values on a printed copy of Table 13-1, and retain in
aircraft records.
Label
UNIT FUNCTION
FUNCTION LOCK
PITCH TRIM
ROLL TRIM
SLIP TRIM
OAT TRIM
SPD ASST
IAS TRIM LO
IAS TRIM HI
ALT TRIM LO
ALT TRIM HI
PITOT ZERO
AOA FUNC
IAS UNITS
TAS UNITS
IAS VSO
IAS VS1
IAS VFE
UAV-1004234-001, AV-30-E Installation Manual
Rev H
Figure 38 – Setup Done / Exit Option
Table 13-1 – Installation Menu Setting
Description
Unit functionality
Functionality Lock
Pitch trim
Roll trim
Slip trim
OAT probe trim
Use airspeed to enhance
attitude calculation
IAS trim at low speed
IAS trim at high speed
Barometric altitude trim
Barometric altitude trim
at value > 10,000' from
ALT TRIM LO
Pressure sensor age
compensation
Angle of Attack Alert
IAS display units (also
affects groundspeed and
V-speed settings units)
TAS display units
Stalling speed in landing
configuration
Stalling speed in a
specific configuration
Maximum flap extended
speed
Possible Values
Set to default mode: AI* or
DG
If locked, pilot may not
change unit function
Trim as needed: ±27 Degrees
(0*)
Trim as needed: ±5 Degrees
(0*)
Trim as needed: ±5 Degrees
(0*)
Trim as needed: ±200
(Unitless) (0*)
Yes* (on) or No (off)
Trim as needed: ±100 (in IAS
UNITS) (0*)
Trim as needed: ±100 (in IAS
UNITS) (0*)
Trim as needed: ±500 Feet
Trim as needed: ±500 Feet
Automatically determined by
measurement
ENABLED*, DISABLED
Knots* (KTS), Miles Per Hour
(MPH), or Kilometers Per
Hour (KPH)
Knots* (KTS), Miles Per Hour
(MPH), or Kilometers Per
Hour (KPH)
Set to match limits: 40 to 555
(50*) in IAS UNITS
Set to match limits: 40 to 555
(60*) in IAS UNITS
Set to match limits: 40 to 555
(100*) in IAS UNITS
Configured
Value(s)
101