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P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
PACK HIGH FLOW L (R) Left and/or right pack in high flow mode 13
PACK LOW FLOW L (R) Left and/or right pack in low flow mode 13
PACK MAN TEMP L (R) Left and/or right pack manual selection 13
PACK OFF L (R) Left and/or right pack off 13
PARK/EMER BRAKE ON Park brake is on with aircraft stopped 4/10/1
PLT ROLL SPLRS Displayed if the pilot roll spoilers control PBA is selected; the message is
accompanied by the illumination of the “PLT ROLL” legend on the PBA 10
PRI PUMPS OFF L (R) Left and/or right primary (AC) pump off 11
RAM AIR ON Ram air on 13
RAT GEN OFF The RAT is deployed and the RAT Line Connector (LC) is selected off 6
RECIRC FAN OFF Recirculation fan off 13
STAB CH 1 (2) OFF
Displayed if channel 1-2 of the horizontal stabilizer trim is selected OFF via the
cockpit panel CH1/CH2 PTRIM OFF PBA; the message is accompanied by the
lighting of this PBA
10
TRIM AIR OFF Trim air off 13
WING A/ICE AUTO Wing anti-ice manually selected to AUTO 3
WING A/ICE ON Wing anti-ice manually selected on 3
WING FUEL XFER OFF Wing fuel transfer off 11
WING XBLEED FROM L Wing anti-ice supplied by left bleed 3
WING XBLEED FROM R Wing anti-ice supplied by right bleed 3
WSHLD HEAT OFF L (R) Left windshield temperature controller switch (and/or right windshield
temperature controller switch) is at off/reset 3
XBLEED CLOSED Bleed crossfeed closed 13/17
XBLEED OPEN Bleed crossfeed open 13/17
XFEED VALVE OPEN Fuel crossfeed open 11
STATUS MESSAGES (WHITE)
CAS MESSAGE DESCRIPTION CH.
7-62 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
PAGE INTENTIONALLY LEFT BLANK
For Training Purposes Only
Sept 04
7-63
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
ELECTRONIC FLIGHT INSTRUMENTS
The flight instruments require pitot-static data, air data, attitude and heading data, and
input from various electronic components to provide the following information to the
flight crew:
Each Primary Flight Display (PFD) and Multifunction Display (MFD) receives
altitude, heading, airspeed and attitude data from the on-side sensors. Flight crew
access to display format and display controls is provided via the PFD control panel,
located on the glareshield, the reversion control panel and MFD control panel, both
located on the pedestal.
• Altitude (barometric/radio) • True Airspeed
• Groundspeed • Temperature Data
• Airspeed (MACH/KIAS) • Airplane Attitude
• Vertical Speed • Navigation Information
• Airspeed & Vertical Speed Trend • Heading Information
MINIMUMS
RAD BARO IN Hpa
NAV SRC BARO SET
BRG V/L FMS BRG
HSI
Honeywell
PUSH STD
AIRSPEED LIMITS - (INDICATING SPEEDS)
VSE (SLATS OUT, 0°FLAPS) . . . . . . . . . . . .
VFE (SLATS OUT, 6°FLAPS) . . . . . . . . . . . .
VFE (SLATS OUT, 16°FLAPS) . . . . . . . . . . .
VFE (SLATS OUT, 30°FLAPS) . . . . . . . . . . .
VA (MANEUVERING)
(AT SEALEVEL@96,000 LB) . . . . . . . . . . .
(AT 20,000 FT @ 78,600 LB) . . . . . . . . . . . . .
VMO
VMO
MMO
MMO
MMO
MMO
VLO
VLO
VLE
(BELOW 8,000 FT) . . . . . . . . . . . . . .
(8,000FT TO 30,267 FT) . . . . . . . . . .
30,267FT TO 35,000 FT) . . . . . . . . . .
(AT 41,000 FT) . . . . . . . . . . . . . . . . .
(AT 47,000 FT) . . . . . . . . . . . . . . . .
(AT 51,000 FT) . . . . . . . . . . . . . . . .
(EXT) (L/G EXTENSION) . . . . . . . . .
(RET) (L/G RETREACTION) . . . . . .
(L/G EXTENDED) . . . . . . . . . . . . . . .
225
210
210
185
254
250
300
340
0.89
0.88
0.858
0.842
200
200
250
AIRSPEED LIMITS - (INDICATING SPEEDS)
VSE (SLATS OUT, 0°FLAPS) . . . . . . . . . . . .
VFE (SLATS OUT, 6°FLAPS) . . . . . . . . . . . .
VFE (SLATS OUT, 16°FLAPS) . . . . . . . . . . .
VFE (SLATS OUT, 30°FLAPS) . . . . . . . . . . .
VA (MANEUVERING)
(AT SEALEVEL@ 96,000 LB) . . . . . . . . . . .
(AT 20,000 FT @ 78,600 LB) . . . . . . . . . . . . .
VMO
VMO
MMO
MMO
MMO
MMO
VLO
VLO
VLE
(BELOW8,000 FT) . . . . . . . . . . . . . .
(8,000FT TO 30,267 FT) . . . . . . . . . .
30,267FT TO 35,000 FT) . . . . . . . . . .
(AT 41,000 FT) . . . . . . . . . . . . . . . . .
(AT 47,000 FT) . . . . . . . . . . . . . . . .
(AT 51,000 FT) . . . . . . . . . . . . . . . .
　
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