THE FLIGHT COMPUTER TRUE AIRSPEED (TAS)
[Pages:27]THE FLIGHT COMPUTER TRUE AIRSPEED (TAS)
POSITION THE TEMPERATURE OVER THE ALTITUDE
PRESSURE WINDOW
Temperature Celsius Above
Density Altitude
Altitude below CAS
TAS
FIND CALIBRATED AIRSPEED ON "B", THE TAS IS JUST ABOVE
Ground School 2011
Created by Steve Reisser
THE FLIGHT COMPUTER TRUE AIRSPEED (TAS)
Problem ALT
37
5,000
TEMP C CAS
0
100
TAS Density Alt.
107
4389
Ground School 2011
Created by Steve Reisser
THE FLIGHT COMPUTER TRUE AIRSPEED (TAS)
Problem ALT
38
3, 500
TEMP C +10
CAS 105
TAS Density Alt.
111
3728
Ground School 2011
Created by Steve Reisser
THE FLIGHT COMPUTER TRUE AIRSPEED (TAS)
Problem ALT
39
8, 500
TEMP C -20
CAS 120
TAS Density Alt.
132
6253
Ground School 2011
Created by Steve Reisser
Problem 40
THE FLIGHT COMPUTER
TRUE AIRSPEED (TAS)
ALT
TEMP C CAS
TAS Density Alt.
12,000
-30
250
285
9350
Ground School 2011
Created by Steve Reisser
THE FLIGHT COMPUTER TRUE ALTITUDE
TRUE ALTITUDE : Indicated altitude corrected for temperature & altitude.
4. T Alt 3. P Alt
1.Temp
2.Ind. Alt
1. Adjust wheel so that "indicated altitude" is under the outside air temperature (C) 2. Find "pressure altitude" on the B scale and read the TRUE ALTITUDE above on the A scale. [GET PRESSURE ALTITUDE BY ADJUSTING THE KOLLSMAN WINDOW TO READ 29.92]
Problem P Alt TEMP C TRUE ALTITUDE
41
5,000 0
4900
Ground School 2011
Created by Steve Reisser
THE FLIGHT COMPUTER TRUE ALTITUDE
Problem P Alt TEMP C TRUE ALTITUDE
43
8, 500 -20
7930
Ground School 2011
Created by Steve Reisser
THE FLIGHT COMPUTER TRUE ALTITUDE
Problem 44
P Alt TEMP C TRUE ALTITUDE
12,000 -30
11037
Ground School 2011
Created by Steve Reisser
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