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boxed: speed readout and tapes removed).
The following annunciations can be displayed:
· ATT for discrepancy in pitch > 5 degrees or in roll > 6 degrees
· IAS for discrepancy of more than 20 knots (for IAS > 60 knots)
· ALT for discrepancy of more than 200 feet
· HDG for discrepancy of more than 10 degrees
· GS or LOC for excessive deviation
· RAD for radio altitude miscompare.
Attitude
Heading Localiser
Glide Slope
Indicated
Airspeed
Altitude
Radio Altitude
415 00
405 00
410 00
SPD
F250
280
260
253
240
220
405 00
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FLIGHT INSTRUMENTS
Rev 7, Dec 01, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
11−10−93
FLIGHT PROFILE
Powerup
GF1110_094
Takeoff
T/O
ASEL
HDG
GF1110_095
When the Flight Director is in the takeoff
mode and the nose wheel is off the ground, the pitch
scale changes to a pitch target. The takeoff
mode pitch target is normally set at 17.5 degrees;
however, if an engine failure is detected, it is reset automatically to 13 degrees.
The aircraft symbol is superimposed on the roll and pitch scale to provide airplane attitude
reference.
FLIGHT INSTRUMENTS
Flight Crew Operating Manual Rev 7, Dec 01, 2005
CSP 700−5000−6
Volume 2
11−10−94
FLIGHT PROFILE (CONT'D)
Cruise
GF1110_096a
Approach CAT I
GF1110_097a
FLIGHT INSTRUMENTS
Rev 7, Dec 01, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
11−10−95
FLIGHT PROFILE (CONT'D)
Approach CAT II
GF1110_098a
FLIGHT INSTRUMENTS
Flight Crew Operating Manual Rev 7, Dec 01, 2005
CSP 700−5000−6
Volume 2
11−10−96
FLIGHT PROFILE (CONT'D)
Excessive Attitude
The excessive attitude format is used in the following conditions:
· Roll is greater than 65° or less than −65°
· Pitch is greater than 29° or less than −20°
The excessive attitude format is kept until the Roll is between ±63° and the Pitch is between 28°
and −18°.
To enable the pilot to focus on the essential parameters for the excessive attitude recovery, some
parameters (for example, navigation information) are removed to provide a decluttered display.
When an excessive attitude occurs, a sphere is included in the center of the FPV. The sphere has
3 positions according to Pitch angle:
· One third illuminated when Pitch is greater than 5°
· One half illuminated when Pitch is between ±5°
· Two thirds illuminated when Pitch is lower than −5°.
When excessive attitude occurs, chevrons are displayed each 10° from 30° to 80° and from −20°
to −80° on the pitch tape, and a roll command is displayed around the FPV. The roll command
indicates the direction to roll the aircraft to return to wings level.
Roll
Command
Excessive
Attitude
Sphere
GF1110_099
FLIGHT INSTRUMENTS
Rev 7, Dec 01, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
11−10−97
ENHANCED VISION SYSTEM (EVS) (IF INSTALLED)
General
The EVS consists of cockpit controls, a Head−Up Display (HUD) System, an Infrared Sensor
System (ISS) and FMS CDU. The ISS consists of an Infrared Sensor Unit (ISU) and an Infrared
Window (IRW).
The EVS imagery can significantly improve the pilot’s capability to detect approach lights and
visual references of the runway environment that may not otherwise be visible under poor visibility
conditions. The EVS also provides enhanced situational awareness during night operations.
The EVS enable descent and operation below decision altitude (DA) based on the pilot’s
observation of the EVS image.
EVS Overview
The EVS is composed of two sub systems,
1. The Head−Up Display (HUD) System, which is comprised of the following units:
· Head−Up Display Computer (HUD Computer)
· Computer Mounting Tray
· Optical Projector Unit (OPU)
· Combiner Optical Unit (COU)
· Mounting Tray (MTR)
· Sun Visor
· Cockpit Controls
2. The Infrared Sensor System (ISS), which is comprised of the following units:
· Infrared Sensor Unit (ISU)
· Infrared Window (IRW)
The Infrared Sensor Unit (ISU) is mounted inside the aircraft TRU bay, aft of the radome. The ISU
　
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