|
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
Conditions: Speed = 52 KIAS Wing Flaps in Landing Position (LDG) max take-off power
Example: Pressure altitude: 2000 ft Outside temperature: 70oF Result: Climb performance during balked landing: 374 ft/min
Figure 5.10. Climb Performance / Balked Landing
5.3.11. Landing Distance
Conditions: - Throttle: Idle
- Maximum T/O Weight
-Approach Speed 55 KIAS
-Level Runway, paved
- Wing Flaps in Landing position (LDG)
-Standard Setting, MSL Landing distance over a 50 ft (15 m) obstacle: approx. 1360 ft (414m) Landing roll distance: approx. 661 ft (201m)
Height above MSL ft. 0 1000 2000 3000 4000 5000 6000 7000
(m) (0) (305) (610) (914) (1219) (1524) (1829) (2134)
Landing Distance ft. 1360 1387 1417 1447 1478 1511 1545 1580
(m) 415 423 432 441 450 461 471 482
Landing Roll Distance ft. 661 680 701 722 744 767 791 815
(m) 201 207 214 220 227 234 241 248
Figure 5.11. Landing and Rolling Distances for Heights Above MSL
NOTE
Poor maintenance condition of the airplane, deviation from the given procedures as well as unfavorable outside conditions (i. e. high temperature, rain, unfavorable wind conditions, slippery runway) could increase the landing distance considerably.
NOTE
Aircraft with ground idle speed set to 1000 RPM, landing distance increased approx. 5% and ground roll increased approx. 7%.
5.4.
Noise Data
6.
WEIGHT AND BALANCE
Noise Measurement Method Noise Value Maximum Allowable
FAR36 Appendix G 71.7 dBA 75.7 dBA
ICAO Annex 16, Appendix 6 74.4 dBA 80.1 dBA
Model: DA20-C1 Serial Number Registration
Data with reference to the Type Certificate Data Sheet and the Flight Manual Reference Datum: Leading edge of wing at root rib. Horizontal reference line: Wedge 1000:55.84, 2000mm (78.7 in) aft of the step in the fuselage at the canopy
edge
Equipment list - dated Cause for Weighing
Weight and Balance Calculations
Weight Condition:
Include brake fluid, engine oil and Unusable fuel (Type 2 system, 2 liters unusable, 3.18 lbs/1.44 Kg)
Finding Empty Weight:
Finding Arm: (Measured)
Support Gross ([kg]) (lbs) Tare ([kg]) (lbs) Net Weight ([kg]) (lbs)
Front G1
Rear G2LH
Rear G2RH
EMPTY WEIGHT (G)
Lever Arm
([m]) (in)
X1 =
中国通航网 www.ga.cn
通航翻译 www.aviation.cn
本文链接地址：钻石20系列飞机维护手册 DA 20 SERIES AIRPLANE MAINTENANCE MANUAL(73)
| 
