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SUPPLEMENT 11
Approaches below 4.5 Degrees
07−11−01−4
REV 75, Feb 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
GENERAL 07−12−01−1
INTRODUCTION 07−12−01−1
LIMITATIONS 07−12−01−1
Structural Weight 07−12−01−1
Operating Limitations 07−12−01−1
Power Plant 07−12−01−2
Systems Limitations 07−12−01−2
Navigation Systems Limitations 07−12−01−2
EMERGENCY PROCEDURES 07−12−01−2
NORMAL PROCEDURES 07−12−01−3
Before Start Check 07−12−01−3
In Range Check 07−12−01−3
Before Landing Check 07−12−01−3
Go-Around 07−12−01−3
After Landing Check 07−12−01−3
ABNORMAL PROCEDURES 07−12−01−4
Engine Failure During Approach 07−12−01−4
Single Engine Go-Around 07−12−01−5
PERFORMANCE 07−12−01−6
Landing Performance 07−12−01−6
LIST OF ILLUSTRATIONS
Figure 07−12−1 Landing Field Length and Landing Speed, Flaps 45 07−12−01−7
Figure 07−12−2 Distance from Glideslope System Position on Runway to
Full Stop 07−12−01−9
SUPPLEMENT 12
Steep Approaches up to 5.5 Degrees
07−12−00−1
REV 71, Oct 31/07
07−12−00−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
SUPPLEMENT 12
Steep Approaches up to 5.5 Degrees
07−12−00−2
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
NOTE
This Airplane Flight Manual Supplement is only applicable to
airplanes incorporating Service Bulletin 604−34−055.
This Airplane Flight Manual Supplement is NOT applicable to
FAA registered airplanes.
This Airplane Flight Manual Supplement does not constitute
approval to conduct Steep Approach operations.
1. GENERAL
The data in this Supplement must be used when conducting steep approach landings from
4.5 degrees to 5.5 degrees, inclusive.
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. Structural Weight
Maximum landing weight: 15,875 kg (35,000 lb)
B. Operating Limitations
(1) ALTITUDE AND TEMPERATURE OPERATING LIMIT
Maximum landing altitude is 5,000 feet.
(2) OPERATION IN ICING CONDITIONS
Steep approaches in known icing conditions are prohibited.
(3) TAILWIND CONDITIONS
No tailwind component is permitted.
(4) APPROACHES
Operations with a glidepath angle that exceeds 5.5 degrees is prohibited.
Deliberate one engine inoperative steep approaches are prohibited.
Partial flap steep approaches and landings are prohibited.
Steep approach landing on contaminated runways is prohibited.
(5) MAXIMUM CROSSWIND COMPONENT
The maximum crosswind component for steep approach landings is 20 knots.
(6) LANDING DECISION POINT
The minimum height for go-around following an engine failure (Landing Decision Point) is
200 feet AGL.
SUPPLEMENT 12
Steep Approaches up to 5.5 Degrees
07−12−01−1
REV 70, Jun 08/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. LIMITATIONS (CONT'D)
C. Power Plant
(1) AUTOTHROTTLE (ATS) (IF INSTALLED)
Use of the ATS for steep approaches or landing is prohibited.
D. Systems Limitations
(1) AUTOMATIC FLIGHT CONTROL SYSTEM
Use of autopilot for steep approaches is prohibited.
(2) ANTI-ICE SYSTEM
Approach and landing with wing and/or cowl anti-ice selected ON is prohibited.
(3) SYSTEMS INOPERATIVE
Landings at a steep approach airfield are prohibited if any of the following systems are
inoperative:
• Flaps
• Ground Spoilers
• Anti-Skid
• Nose Wheel Steering
• Radio Altimeter
• Thrust Reverser
E. Navigation Systems Limitations
(1) FLIGHT MANAGEMENT SYSTEM
　
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