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Gross Climb Performance 07−05A−01−12
ABNORMAL PROCEDURES 07−05A−01−16
PERFORMANCE 07−05A−01−16
LIST OF ILLUSTRATIONS
Figure 07−05A−1 Stick Shaker Speed (KIAS) − Flaps 0°, Landing Gear Up 07−05A−01−4
Figure 07−05A−2 Stick Shaker Speed (KIAS) − Flaps 20°, Landing Gear Up 07−05A−01−5
Figure 07−05A−3 Stick Shaker Speed (KIAS) − Flaps 30°, Landing Gear Up 07−05A−01−6
Figure 07−05A−4 Stick Shaker Speed (KIAS) − Flaps 45°, Landing Gear
Down 07−05A−01−7
Figure 07−05A−5 Stick Pusher Speed (KIAS) − Flaps 0°, Landing Gear Up 07−05A−01−8
Figure 07−05A−6 Stick Pusher Speed (KIAS) − Flaps 20°, Landing Gear Up 07−05A−01−9
Figure 07−05A−7 Stick Pusher Speed (KIAS) − Flaps 30°, Landing Gear Up 07−05A−01−10
Figure 07−05A−8 Stick Pusher Speed (KIAS) − Flaps 45°, Landing Gear
Down 07−05A−01−11
Figure 07−05A−9 Take-Off Gross Rate of Climb − Flaps 20°, Landing Gear
Up 07−05A−01−13
Figure 07−05A−10 Final Take-Off/Enroute Gross Rate of Climb − Flaps 0°,
Landing Gear Up 07−05A−01−15
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−00−1
REV 66, Feb 01/07
07−05A−00−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−00−2
REV 66, Feb 01/07
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
airplane 5622 on the HKCAD Registry.
1. GENERAL
The data in this Supplement must be used when conducting Airworthiness Flight Tests or Crew
Training Operations.
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.
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. High Speed Flight
An appropriate airspeed limitation is established for the case where there is a need for crews
to experience the airplane’s high speed characteristics above VMO/MMO during training, or for
VMO/MMO to be exceeded to permit correct operation of the high speed warning to be tested
up to the maximum upper limit of tolerance of the system. In order to satisfy this requirement,
an airspeed limitation of VMO + 10 KIAS or MMO + 0.01 has been defined for the purpose of
airworthiness flight tests or crew training operations, provided the following conditions are
observed:
• Passengers are not carried;
• Wings are level and no “g” is applied throughout the maneuver; and
• There is no significant turbulence.
(1) ENTRY AND RECOVERY PROCEDURES
The maneuver should be commenced in level flight by setting the thrust levers to achieve
maximum continuous thrust (MCT) and then lowering the nose of the airplane gently. To
recover from the maneuver, set the thrust levers to IDLE, extend the flight spoilers and
carry out a gentle pull up. If an airspeed greater than VMO + 10 KIAS or MMO + 0.01 is
inadvertently achieved, or any airframe or aileron buffet is encountered, recovery action
should be taken immediately.
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES (CONT'D)
B. Intentional Stalls
Intentional stalls may be carried out, when authorized, for the purpose of airworthiness flight
tests or crew training operations, subject to the following conditions:
• Altitude is between 13,000 feet and 15,000 feet;
• Autopilot is disengaged;
• Stall protection system is fully operative;
• Airplane is free from ice;
　
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