曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

test/crew training is prohibited.
D. Airworthiness Flight Test/Crew Training (Airplanes on the HKCAD Registry)
When dispatching with one hydraulic AC motor pump inoperative, airworthiness flight
test/crew training is prohibited.
E. Flight with Landing Gear Down
(1) WEIGHT ALTITUDE TEMPERATURE LIMITS
When dispatching with one hydraulic AC motor pump inoperative, the following penalty
must be applied to the performance data as a weight decrement:
FLIGHT SEGMENT WEIGHT DECREMENT (%)
Take-off – Flaps 20° 16%
Landing – Approach Flaps 20°
– Landing Flaps 45° 13%
(2) CLIMB GRADIENTS AND CLIMB SPEEDS
When dispatching with one hydraulic AC motor pump inoperative, the following gradient
penalty must be subtracted from the climb gradient data:
CLIMB GRADIENT GRADIENT PENALTY (%)
Obstacle Clearance Reference Climb Gradient
(Flaps 20°) 2.9%
Final Segment / Enroute (Flaps 0°) 3.3%
Approach (Flaps 20°) 2.6%
Landing (Flaps 45°) Not applicable
The approach climb speed in the flaps 20° configuration must be increased by 2 knots.
8. PERFORMANCE
The performance data in Chapter 6 of the Airplane Flight Manual are applicable, except as
modified by the following:
A. Ground Spoilers Inoperative
With the ground spoilers inoperative:
Take-off distance for dry or wet runways Multiply by a factor of 1.08 (8%)
Landing distance and landing field length Multiply by a factor of 1.14 (14%)
NOTE
No correction to the take-off decision speed (V1) is required.
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−4
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
8. PERFORMANCE (CONT'D)
B. Cowl Anti-Ice Pressure Relief Blow-Off Valve Inoperative
If cowl or wing and cowl anti-ice is on, with one cowl anti-ice pressure relief blow-off valve
failed open:
• Use cowl and wing anti-ice thrust settings (N1), and reduce as follows:
Thrust settings (N1) Subtract 1.4%
NOTE
N1 thrust setting reduction is applicable to both engines.
• Use cowl and wing anti-ice performance, and adjust as follows:
Take-off distance for dry or wet runways Multiply by a factor of 1.14 (14%)
Obstacle clearance reference climb gradient Subtract 1.5%
Final segment and enroute climb gradient (gross) Subtract 1.4%
Approach climb gradient Subtract 1.5%
Landing climb gradient Subtract 3.0%
Take-off weight limited by climb requirements Multiply by a factor of 0.95 (–5%)
Landing weight limited by climb requirements Multiply by a factor of 0.95 (–5%)
NOTE
No correction to the take-off decision speed (V1) is required.
C. Nose Wheel Steering Inoperative
With nose wheel steering inoperative:
Take-off distance Multiply by a factor of 1.02 (2%)
NOTE
1. The maximum crosswind component for take-off and landing is
20 knots.
2. Take-off and landing is not permitted on contaminated runways.
3. Excessive use of asymmetric braking may lead to fusible plug release
or failure.
D. Flap Power Drive Unit Inoperative
With flaps operating at half speed:
• Reduce the maximum landing weight as follows:
Landing weight limited by climb requirements Reduce by 3,500 lb
• Increase the acceleration distance as follows:
Net take-off flight path Increase by 4,000 ft
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−5
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
8. PERFORMANCE (CONT'D)
E. Anti-Skid Inoperative
CAUTION
Extreme caution is required during braking to avoid tire damage or
blowout. Maximize use of reverse thrust.
With anti-skid inoperative:
Take-off distance for dry or wet runways Multiply by a factor of 1.90 (90%)
Decision speed (V1) – 17 KIAS
Landing distance and landing field length Multiply by a factor of 1.95 (95%)
NOTE
1. Corrected V1 may not be less than V1MCG .
2. Take-off and landing is not permitted on contaminated runways.
3. Reduced thrust take-off is not permitted.
A brake cooling time of 50 minutes must be observed between a landing or a low energy
rejected take-off and a subsequent take-off.
The maximum take-off weight limited by brake energy is determined in Figure 06−24−2.
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−6
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
8. PERFORMANCE (CONT'D)
DFO1_0624_001 WTBE604BB_HA−17/09/02
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：龐巴迪挑戰(zhàn)者604操作手冊 Operating Manual 2(97)