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180 KIAS
VREF
(Maximum correction is +10 KIAS)
Visual Descent Point (VDP) or
GF0408_003A
+ 1/2 GUST
Go−Around Thrust
Non−Precision Approach
Figure 04−08−2
———— END ————
NORMAL PROCEDURES
APPROACH AND LANDING
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
04−08−9
7. STANDARD VISUAL APPROACH (CONT'D)
1 − 1 1/2 miles
1,500 feet AGL
On Downwind:
Prior To Turning Base:
Turning Base:
Turning Final (approx. 500 − 700 feet):
Touchdown:
STANDARD VISUAL APPROACH
Spoilers − Check
Brakes − Apply
Thrust reversers − Deploy
Start descent
Landing gear − Down
Slats/Flaps − OUT/30 degrees
VREF + 1/2 GUST
Before Landing Check − Complete
Slats/Flaps − OUT/6 degrees
160 KIAS
Go−Around:
Go−Around switch − Press
Go−Around Thrust
Slats/Flaps − OUT/10 degrees
Go−Around Attitude
Positive Rate of Climb
Landing Gear − Up
Retract Slats/Flaps on Schedule
(Maximum correction is + 10 KIAS)
Mid−downwind:
Slats/Flaps − OUT/16 degrees
140 KIAS
GF0408_005A
Standard Visual Approach
Figure 04−08−4
———— END ————
NORMAL PROCEDURES
APPROACH AND LANDING
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
04−08−13
04--11--22
REV 2, Feb 24/04
NORMAL PROCEDURES
Prior to Landing
Vol. 2
Flight Crew Operating Manual
CSP C--013--067
Vol. 2
REV 3, May 03/05
ABNORMAL PROCEDURES 05--03--15
Single Engine Procedures
Flight Crew Operating Manual
CSP C--013--067
PF:
G “Go-Around”
GO - AROUND --- SINGLE ENGINE
G Press TOGA switch
G Thrust levers to TOGA detent
PF:
G Rotate towards FD
G “Flaps 8”
PNF:
G “Positive Rate”
PF:
G “Gear Up”
PF:
G V2
G “Speed Mode”
PF:
G Call Lateral Mode
as required
600 feet AGL
PF:
G “Autopilot On”
PF:
G Engage ALT
Acceleration ALT
PF:
G Call Flaps
on schedule
”Half Bank”:
G Speed < V2 + 10
PF:
G “Max Continuous Thrust”
G Set thrust levers to CLIMB detent
G Climb at VT
G “Climb Check”
Configuration prior to go--around:
G Single Engine
G FLAPS 20
Head-Up
Guidance System
HGS® Pilot Guide
for the Bombardier CRJ 700
Registration Notice
HGS® is a registered trademark of
Rockwell Collins Flight Dynamics
Proprietary Notice
The information contained in this document is proprietary, and it shall not
be reproduced or disclosed in whole or in part without prior authorization
from Rockwell Collins Flight Dynamics.
© 2002 Rockwell Collins Flight Dynamics
Document # 9701-1153
Revision A
We welcome your comments concerning this manual. Although every effort
has been made to keep it free of errors, some may occur. When reporting a
specific problem, please describe it and include the document number, the
paragraph or figure description, and the page number.
Mail your comments to:
Customer Service Publications
Rockwell Collins Flight Dynamics
16600 SW 72nd Avenue
Portland, Oregon 97224 USA
Or contact us at:
Tel: 503.443.3000
FAX: 503.443.3020
Email: custservepubs@rockwellcollins.com
Internet: www.flightdynamics.com
HGS® Pilot Guide for the Bombardier CRJ 700 Model 4200
9701-1153 Rev A November 2002 i
Table of Contents
Section 1: Introduction............................................................................ 1-1
Section 2: HGS Description .................................................................... 2-1
Overview ...............................................................................................2-1
HGS Combiner ......................................................................................2-2
Combiner Location ............................................................................2-3
Combiner Function ............................................................................2-3
Combiner Display Brightness ............................................................2-4
Combiner Sun Visor ..........................................................................2-5
　
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