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3 Select ENT to view selected checklist.
APU FIRE
APU SWITCH OFF
APU DISCH HANDLE PULL
2 Pull down on joystick to select next line.
Line that is selected is inside of box.
EMERGENCY
PROCEDURES
1/4
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
1. ENGINE FIRE
APU DISCH HANDLE TURN
FIRE HANDLE UNLK PIN SLIDE
APU DISCH HANDLE TURN
LAND AT NEAR SUITABLE AIRPORT
To acknowledge checklist item, select ENT
button. Once item is acknowledged, it will
annunciate green and the box automatically
scrolls to the next line.
4
NOTE
The remainder of the emergency
procedures are accessed and
acknowledged in the same manner.
GF1110_049
HDG
315
360 FMS1
N
50 50
KPHX
TOC
LUF
KDVT
KSRP
30
6
33
3
ETE1+36
12.5
KDVT
NM
WX
EMERGENCY
PROCEDURES
1. ENGINE FIRE
1/4
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
SAT
GSPD
−56
TAT
TAS
−40
234
345
FLIGHT INSTRUMENTS
Flight Crew Operating Manual REV 46, Jul 21, 2005
CSP 700−6
Volume 2
11−10−44
STANDBY ATTITUDE INDICATOR
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.
Effectivity:
· Airplanes 9002 thru 9104 not incorporating Service Bulletin:
· SB 700−34−022, Standby ArtificialHorizon
System − Change Power Source to 28 V dc
Direct From Avionics Battery Bus.
The standby attitude indicator is powered from the battery bus via the SPDA No.1.
FAILURE
FLAG
ROLL
POINTER
DRUM
AIRCRAFT
SYMBOL
HORIZON
LINE
CAGE
KNOB
BALL LEVEL
INDICATOR
ROLL
INDEX
GF1110_050
FLIGHT INSTRUMENTS
REV 46, Jul 21, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 2
11−10−45
STANDBY ALTIMETER/AIRSPEED INDICATOR
The standby Altimeter/Airspeed indicator uses the standby pitotstatic
source. The standby indicated
airspeed readout displays noncorrected
indicated airspeed.
80 100 120 140 160 180 200 220 250 300 350 400 450
mb/hPa in Hg
746 22.00
1013 29.92
ALTIMETER RANGE
1049 30.99
7
6
3
2
87
6
5
4
3
21
9
0
ALTITUDE DRUM RANGE
1,000 FT
DRUM
10,000 FT
Below DRUM
Sea Level
Indication
− 1,000 to + 51,000 FT
ALTITUDE RANGE
IAS KNOTS
000
999
100 FT
DRUM
SPEED IAS RANGE
0 60
Below
10,000 feet
Indication
NEG
GF1110_051
8
5
4
1
2 5 0
FLIGHT INSTRUMENTS
Flight Crew Operating Manual REV 46, Jul 21, 2005
CSP 700−6
Volume 2
11−10−46
STANDBY MAGNETIC COMPASS
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
BRACKET
COMPENSATORS
COMPASS
DIAL
LIGHT UNIT
COMPASS
CORRECTION
CARD
B 10 10 C
FLIGHT INSTRUMENTS
REV 46, Jul 21, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 2
11−10−47
STANDBY AIRSPEED/ATTITUDE/ALTIMETER (IF INSTALLED)
Incorporated in the indicator is a light sensor that provides ambient light level data to the automatic
lighting system.
A navigation (NAV) button is selected to display ILS (localizer and glideslope) deviation information.
The ATT button is used to erect the display.
AIRSPEED
TAPE
MACH NUMBER
ALTITUDE TAPE
ALTIMETER SETTING HECTOPASCALS
ALTIMETER SETTING
INCHES
LIGHT SENSOR
NAVIGATION ATTITUDE BAROMETRIC SET
ATTITUDE
INDICATOR
GF1110_054
20 20
10 10
10 10
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