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Use and distribution of these pitot-static probes are as follows:
Source Use
PS 1 Normal pitot/static input to the pilot’s side Mach transducer (if installed) and ADC 1.
PS 2 Normal pitot/static input to the copilot’s side Mach transducer (if installed) and ADC
2. PS 3 Normal pitot/static input to ADC 3. PS Standby
Normal pitot/static input to standby instruments.
Three Total Air Temperature (TAT) probes are provided to supply temperature input to the ADCs. Ice protection is provided by electric heating elements for the PS probes and TAT probes (refer to Chapter 14, Ice and Rain Protection).
TAT 1
PS 1
PS 3TAT 2 PS STANDBY
TAT 3 PS 2
PSPS 3 STANDBY
PS 1 PS 2
TOP VIEW
TAT 1/2 PROBE
TAT 3
ENGINE INLET
GF1110_004
Rev 5, Jul 21, 2005 Flight Crew Operating Manual Volume 2
FLIGHT INSTRUMENTS
ADC 1
STANDBY INSTRUMENT
COPILOT VALVE
ADC 3 ADC 2 TEMPERATURE PROBE NO. 1 LEFT ENGINE
UPPER LEFT PITOT/STATIC NO. 1 P1
S1
S2
TEMPERATURE PROBE NO. 3 FUSELAGE
LOWER LEFT PITOT/STATIC NO. 3
P1
S1
S2
UPPER RIGHT
STANDBY
P1 PITOT/STATIC
S1
S2
MACH TRANSDUCER SELECTOR VALVE (on airplane 9002 thru 9158)
MACH TRANSDUCER (on airplane 9002 thru 9158)
TEMPERATURE PROBE NO. 2 RIGHT ENGINE
LOWER RIGHT P1
PITOT/STATIC NO. 2
S1
S2
GF1110_005a
Volume 2 Flight Crew Operating Manual Rev 5, Jul 21, 2005
AIR DATA SYSTEM
The air data system provides computed air data (speed, altitude and temperature data) to various systems:
.
Integrated Avionics Computers (IAC).
.
Data Acquisition Units (DAU).
.
Inertial Reference System (IRS).
.
Stall Protection Computer (SPC).
.
Electronic Display System (EDS) . EFIS and EICAS.
.
Automatic Flight Control System (AFCS).
Pitot and static pneumatic inputs and total air temperature provide raw air data information to the ADCs. Static input to each ADC absolute sensors produces the altitude sensor data. Static and pitot inputs to each ADC differential sensor produces the airspeed sensor data.
PS STANDBY
GF1110_006
Rev 5, Jul 21, 2005 Flight Crew Operating Manual Volume 2
FLIGHT INSTRUMENTS
Each ADC computes the following:
.
Pressure altitude and barometric-corrected altitude.
.
Vertical speed, indicated airspeed, Mach number and true airspeed (TAS).
.
Static air temperature (SAT), TAT and temperature variations from ISA.
.
IAS reference (using AFCS or manually using SPD switch on guidance panel).
.
Vertical speed reference (VS switch on guidance panel).
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