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Before Start Check 07−11−01−3
In Range Check 07−11−01−3
Before Landing Check 07−11−01−3
Go-Around 07−11−01−3
After Landing Check 07−11−01−3
ABNORMAL PROCEDURES 07−11−01−3
Flaps Failure 07−11−01−3
PERFORMANCE 07−11−01−4
LIST OF ILLUSTRATIONS
Figure 07−11−1 Approach Glidepath Angle Operating Limit 07−11−01−2
SUPPLEMENT 11
Approaches below 4.5 Degrees
07−11−00−1
REV 75, Feb 17/09
07−11−00−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
SUPPLEMENT 11
Approaches below 4.5 Degrees
07−11−00−2
REV 70, Jun 08/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. GENERAL
The data in this Supplement must be used when conducting approaches above 3.5 degrees, but
below 4.5 degrees.
These data complement or supersede data contained in the basic Airplane Flight Manual. This
supplement must therefore, be read in conjunction with the basic Airplane Flight Manual.
The effect of this Supplement on the basic Airplane Flight Manual is given in paragraphs
(2) to (7).
2. INTRODUCTION
The general information in Chapter 1 is applicable.
3. LIMITATIONS
The limitations in Chapter 2 are applicable, except as modified by the following:
A. Operating Limitations
(1) APPROACHES
On airplanes NOT incorporating Service Bulletin 604–34–055:
Operations with a glidepath angle exceeding the maximum shown in area A of
Figure 07−11−1 are prohibited.
On airplanes incorporating Service Bulletin 604–34–055:
Operations with a glidepath angle exceeding the maximum shown in area B of
Figure 07−11−1 are prohibited.
B. Systems Limitations
(1) AUTOMATIC FLIGHT CONTROL SYSTEM
The minimum autopilot use height for precision approaches (ILS) with a glidepath angle
that exceeds 3.5 degrees is 160 feet AGL.
SUPPLEMENT 11
Approaches below 4.5 Degrees
07−11−01−1
REV 75, Feb 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. LIMITATIONS (CONT'D)
DFM0711_001
SUPPLEMENT 11
Approaches below 4.5 Degrees
07−11−01−2
REV 75, Feb 17/09
Approach Glidepath Angle Operating Limit
Figure 07−11−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. EMERGENCY PROCEDURES
The emergency procedures in Chapter 3 are applicable.
5. NORMAL PROCEDURES
The normal procedures in Chapter 4 are applicable, in addition to the following:
A. Before Start Check
On airplanes incorporating Service Bulletin 604–34–055:
(1) GPWS, STEEP APPROACH
switch/light .......................................................Press out Check ON light out.
B. In Range Check
For operations in area B of Figure 07−11−1:
(1) GPWS, STEEP APPROACH
switch/light .........................................................Press in Check ON light on.
C. Before Landing Check
NOTE
1. For approaches at angles above 4.0 degrees, the airplane should
be fully configured for landing and slowed to VREF prior to
glideslope intercept.
2. Intermittent operation at idle when wing anti-ice and/or cowl anti-ice
is ON is acceptable during final approach provided no associated
EICAS caution messages are annunciated.
D. Go-Around
For operations in area B of Figure 07−11−1:
(1) GPWS, STEEP APPROACH
switch/light .......................................................Press out Check ON light out.
E. After Landing Check
On airplanes incorporating Service Bulletin 604–34–055:
(1) GPWS, STEEP APPROACH
switch/light .......................................................Press out Check ON light out.
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable, except as modified by the following:
A. Flaps Failure
The following applies, in addition to the existing flap failure procedure:
If flaps fail at 0 degrees, divert to a suitable landing field with a glidepath angle of 3.5 degrees
or less.
SUPPLEMENT 11
Approaches below 4.5 Degrees
07−11−01−3
REV 75, Feb 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE
The performance in Chapter 6 is applicable.
　
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