曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Figure 07−05−6 Stick Pusher Speed (KIAS) − Flaps 20°, Landing Gear Up 07−05−01−9
Figure 07−05−7 Stick Pusher Speed (KIAS) − Flaps 30°, Landing Gear Up 07−05−01−10
Figure 07−05−8 Stick Pusher Speed (KIAS) − Flaps 45°, Landing Gear
Down 07−05−01−11
Figure 07−05−9 Take-Off Gross Rate of Climb − Flaps 20°, Landing Gear
Up 07−05−01−13
Figure 07−05−10 Final Take-Off/Enroute Gross Rate of Climb − Flaps 0°,
Landing Gear Up 07−05−01−15
SUPPLEMENT 5
Airworthiness Flight Test/Crew Training
07−05−00−1
REV 66, Feb 01/07
07−05−00−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
SUPPLEMENT 5
Airworthiness Flight Test/Crew Training
07−05−00−2
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
airplanes 5442 and 5467, on the CAA (UK) 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 + 0.03 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 + 0.03 is
inadvertently achieved, or any airframe or aileron buffet is encountered, recovery action
should be taken immediately.
SUPPLEMENT 5
Airworthiness Flight Test/Crew Training
07−05−01−1
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;
• Airplane maneuver area is clear of cloud and turbulence; and
• Yaw damper is on.
(1) STALL CHARACTERISTICS
There is no natural stall warning or aerodynamic buffet prior to the stall in the altitude
range of between 13,000 feet and 15,000 feet. As a high angle of attack approaches,
continuous ignition is activated. Stall warning is provided by a stick shaker, which is set to
operate at varying percentages of indicated airspeed above the stalling speed. Stick
shaker speeds are presented in tabular form in Figure 07−05−1 to Figure 07−05−4.
The stall is defined by the operation of the stick pusher and the associated nose down
attitude change. Alternate stall identification are provided by the STALL switch/lights on
the glareshield panel flashing red and the warbler coming on. Stick pusher speeds are
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：龐巴迪挑戰者604飛機飛行手冊CL604 Airplane Flight Manual 2(82)