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roll rate commands 4°/sec.
AUTOMATIC FLIGHT CONTROL SYSTEM
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
04−10−27
MULTI-AXIS MODES (CONT'D)
Approach Mode
APPROACH MODE CAPTURE
HDG
045
090°
INBOUND
COURSE
LOCALIZER
TX
TYPICAL CAPTURE POINT
BETWEEN 1 AND 2 DOTS
APPROACH MODE INTERCEPT
HDG
045
HDG AP1 FLC
LOC
RUNWAY
SELECTED
HEADING
045°
LOC AP1 FLC
HDG
040
LOC AP1 GS
APPROACH MODE TRACK
RUNWAY
LOCALIZER
TX
MIDDLE
MARKER
3500 FEET
OUTER
MARKER
4.0−7.0 MILES
RADIO ALTITUDE
BETWEEN 1200
AND 1500 FEET
CRS
090
CRS
090
CRS
090
LOC1 12.0 NM
SRP
LOC1 9.0 NM
SRP
LOC1 4.0NM
SRP
GS
H
H
H
RUNWAY
GLIDESLOPE BEAM
TYPICAL CAPTURE POINT,
IS 1/3 DOT ON GS SCALE
RADIO ALTITUDE
BETWEEN 200
AND 300 FEET
Vertical
Deviation
Scale
Vertical
Deviation
Pointer
N
6
33
E
W
24
21
s
15
30
12
3
N
6
33
E
W
24
21
s
15
30
12
3
N
6
33
E
W
24
21
s
15
30
12
3
GF0410_092
20 20
20 20
20
10 10
10 10
20
20 20
20 20
20 20
AUTOMATIC FLIGHT CONTROL SYSTEM
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
04−10−28
TAKE-OFF (TO) MODE
TO mode provides pitch and lateral commands during the takeoff
phase of flight.
TO mode is activated by pushing one of the throttlemounted
TOGA buttons, while on the ground.
When TO mode is selected, all other lateral and vertical modes are cleared.
GF0410_093
20 20
160 3 000
1500
1000
180
170
160
150
140
130
ROL TO
145
6
4
TOGA BUTTON
ROL TO
TO mode is a heading submode of ROL. TO mode will track the current heading at the time the
airplane passes 80 KIAS during the takeoff
roll.
Vertical TO mode generates a fixed pitch attitude of 17.5°, based on power being developed by the
engines. In the event of a loss of an engine, (N1 <70% on either engine), the pitch command will be
reduced to 13°.
TO mode can be cleared by selecting the AP on, or by selecting another vertical mode.
GO AROUND (GA) MODE
GA mode provides pitch and lateral commands for a transition from an approach to climb out
condition, when a missed approach has occurred.
GA mode is activated by pushing one of the throttlemounted
TOGA buttons, while airborne. When
GA mode is selected, autopilot is disengaged and all other lateral and vertical modes are cleared.
The resultant AP disengage warning may be cancelled by another push of the TOGA button, or by
AP DISC switch.
GF0410_094
20 20
160 3 000
1500
1000
180
170
160
150
140
130
ROL
145
6
4
TOGA BUTTON
ROL AP1 GA
AP1 GA
The GA mode is a heading submode of ROL. GA mode will track the current heading at the time of
GA selection.
GA mode will capture the preselected altitude under the following circumstances:
· If a BARO minimum was not set on the coupled PFD, GA will transition to ASEL and capture
the altitude preselector;
· If a BARO minimum was set on the coupled PFD and the altitude preselector is at least 500 ft
higher than the BARO minimum, GA will transition to ASEL and capture the altitude
preselector.
AUTOMATIC FLIGHT CONTROL SYSTEM
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
04−10−29
GO AROUND (GA) MODE (CONT'D)
Effectivity:
· Airplanes 9002, 9004 thru 9089 not incorporating Service Bulletin:
· SB 700−31−013, IAC/DAU − Software Upgrade for Post Full Functionality Certification.
GA mode will not capture the preselected altitude. Another flight director mode must be selected to
enable altitude capture of the preselected altitude.
Vertical GA mode generates a fixed pitch attitude of 10° whether dual or single engine.
GA mode can be cleared by selecting the AP on, or by selecting another vertical mode.
AUTOMATIC FLIGHT CONTROL SYSTEM
Flight Crew Operating Manual REV 41, Jul 08, 2004
　
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