Tecnam P2010 2015 - 4. ICAO Standard Atmosphere

AFMS N'D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
~TECNAM [p~@1J@ c &H!Y@IT'&)~ l:PD~@OuQ !K'il@ODQIJ@D Page APV5-5
4. ICAO STANDARD ATMOSPHERE
....
w
!6
14
12
10
~ 8
0
g
x
w
Q
::::>
= 4
....
...J
<[
>-
....
;;;;
z
w
Q
-2
- 4
-6 ""- ~""""""~ ~ ~~.._~ ........ ~--''--i~~ ~ ........ '--~~~ ~~
- <a
Examples:
Den•itv Altitude:
-JO
- ID " E 20 8 JO
••
O UTSIDE AIR TEMPERA TURE 'C
!ill!!!
A: Pressure altitude = 1600[1
8: Temperature • lO"C
C: Density Altitude • 2550/1
A
ISA Temeerature: D: Pressure altitude = 1600ft E: ISA Air T emperature • 12°C
Section 5 - Performance
ICAO STANDARD ATMOSPHERE
Ed. 2. Rl!V.0