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Emergency Procedures
APU FIRE APU SWITCH FIRE HANDLE UNLK PIN APU DISCH HANDLE OFF SLIDE TURN
APU DISCH HANDLE TURN
LAND AT NEAR SUITABLE AIRPORT
Selecting EMER will display Emergency Procedures index.
Select ENT to view selected checklist.
EMERGENCY 1/4PROCEDURES
1.
ENGINE FIRE
2.
APU FIRE
3.
ELECTRICAL SMOKE/FIRE
4.
AIR COND SMOKE
5.
CABIN SMOKE
6.
SMOKE REMOVAL PROCEDURE
7.
GEAR BAY OVHT
8.
BRAKE OVHT
9.
WING OVHT
NOTE
The remainder of the emergency procedures are accessed and acknowledged in the same manner.
GF1110_049
Rev 5, Jul 21, 2005 Flight Crew Operating Manual Volume 2
FLIGHT INSTRUMENTS
A standby magnetic compass is located below the overhead panel, at the centre of the windscreen. The standby magnetic compass retracts into a compartment in the overhead panel. The compass lighting is controlled by the Cockpit Lights Integral panel, located on the pedestal.
GF1110_052
Volume 2 Flight Crew Operating Manual Rev 5, Jul 21, 2005
STANDBY ATTITUDE INDICATOR (ON AIRPLANES 9127 TO 9158)
The standby attitude indicator displays airplane pitch and bank angle. It is a 28 volt DC.driven gyro that provides pitch and roll information independently from the aircraft generated electrical power. The standby attitude indicator is powered from the Avionic Battery bus via the Cockpit Circuit Breaker Panel.
ROLL FAILUREINDEX FLAG
HORIZON LINE
ROLL POINTER
GF1110_050
Rev 5, Jul 21, 2005 Flight Crew Operating Manual Volume 2
STANDBY ALTIMETER/AIRSPEED INDICATOR (ON AIRPLANES 9127 TO 9158)
The standby Altimeter/Airspeed indicator uses the standby pitot-static source. The standby indicated airspeed readout displays non-corrected indicated airspeed.
SPEED IAS RANGE
060 80 100 120 140 160 180 200 220 250 IAS KNOTS 300 350 400 450
GF1110_051
Volume 2 Flight Crew Operating Manual Rev 5, Jul 21, 2005
INTEGRATED STANDBY INSTRUMENT (ON AIRPLANES 9159 AND SUBSEQUENT)
The Integrated Standby Instrument (ISI) displays standby attitude, altitude, airspeed, Mach number, slip.skid indication, ILS deviation, corrected altitude, barometric pressure and VMO/MMO. It also calculates the Static Source Error Correction (SSEC).
The ISI is a self-contained instrument which receives pitot pressure input from the standby PS and static pressure input from PS 1 and the standby PS. It is powered by 28 VDC. The ISI also receives inputs from the SPS to compute the SSEC.
Operation of the ISI is accomplished with the use of a BARO rotary knob and 4 push.buttons: CAGE (gyro.caging), STD (baro.settings), + and .. The CAGE button resets the horizon line when the button is depressed for more than 2 seconds. A warning flag appears on the display when re.alligning. When depressed, the STD button will select the standard pressure reference of 1013 hPa or 29.92 inHg. The BARO knob can be used to adjust the baro.correction pressure. The + and . buttons are used to control the brightness of the display.
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