M+D JS-MD 1C 2017, Руководство по эксплуатации воздушного судна

Страница: 115 / 145

JS-MD 1C Aircraft Flight Manual
MD01-AFM-00-001
Issue: 02
Rev. 00 Rev. Date: 14.09.2017 Page 7-13
7.8 Pitot and static system
The aircraft pneumatic system consists of:
•
Static (P
STAT
) piping for ASI and Altimeter
•
Dynamic (P
TOT
) piping for ASI
•
Static piping for variometer from fin probe
•
Total Energy (TE) piping from fin probe
The pneumatic piping is colour coded as follows:
•
Static piping for ASI and Altimeter - Blue
•
Dynamic piping for ASI - Green
•
Static for electronic flight
Computer from multi-probe - Transparent/White
•
Total Energy piping from fin probe - Red
•
Mechanical variometer capacity - Yellow
Figure 7.7.0-1 gives a schematic of the instrument layout.
NOTE: The ASI must use the static sources located in the rear of
the fuselage tube. The airspeed calibration values are
based on these static port readings.
NOTE: Static ports located in the rear of the fuselage tube are marked
with a red ring and must be kept unobstructed to ensure correct ASI
readings.
Static
ports on
fuselage