BOMBARDIER BD-100-1A10, Руководство по эксплуатации

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FLIGHT INSTRUMENTS
Feb 22/2006 Flight Crew Operating Manual Volume 2
REV 5 CSP 100-6
11-01-13
AIR DATA SYSTEM (Cont)
PITOT STATIC SYSTEM
The aircraft is equipped with a primary pitot static system and a standby pitot static system. The primary pitot static system
provides total and static pressures to air data computers (ADC) 1 and 2. The pressures are sensed
by left and right pitot
static probes. The standby pitot static system provides total and static pressures to the integrated standby instrument. The
pressures are sensed by a standby pitot probe and two flush mounted standby static ports.
The primary pitot static probes each have one total pressure port and two static pressure ports. The standby pitot probe has
a single pressure port. All of the probes and the flush standby static ports are electrically heated. Probe heat is discussed in
Chapter 14, Ice and Rain Protection.
TAT PROBE
RIGHT PITOT/
STATIC PROBE
LEFT PITOT/
STATIC PROBE
LEFT STANDBY
STATIC PORT
CF
O
1
1
0
1
002
_0
03
RIGHT STANDBY
STATIC PORT
STANDBY PITOT
PROBE
REV 5