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
Figure 01.10.23 Hazard Areas . Engines and APU 01.10.40
AIRPLANE GENERAL General Vol. 2 01.10.1
Oct 05/06
GENERAL
The Challenger 605 is a sweptwing, twin-engine monoplane, certified as a CL–600, model 2B16 Challenger airplane (Serial No. 5701 and subsequent), in accordance with FAR 25, FAR 36 and their amendments. Maximum ramp and takeoff weights are 48,300 and 48,200 lb respectively. The airplane is designed for two crew members, with accommodation for up to 19 passengers, and is powered by two General Electric CF34.3B engines.
The airplane is certified capable of RVSM operation in accordance with FAA "interim guidance material on the approval of operations/aircraft for RVSM operations" 91. RVSM, dated March 14, 1994.
The following sections will be addressed:
.
Wings
.
Fuselage
.
Doors and emergency exits
.
Service panels and accesses
.
Antennas
.
Cockpit controls and indicators
.
Crew seats and eye locator
.
Taxiing and turning radii
.
Hazard areas
AIRPLANE GENERAL General Vol. 2 01.10.2
Oct 05/06
GENERAL (CONT'D)
Airplane Basic Dimensions
Figure 01.10.1
AIRPLANE GENERAL General Vol. 2 01.10.3
Oct 05/06
WING
Description
The wing is an all-metal, advanced-technology airfoil, manufactured as a single unit and bolted to the bottom of the fuselage. The wing incorporates ailerons, flaps, flight and ground spoilers, internal fuel tanks, and the support structure for the main landing gear. Thermal anti-icing is incorporated into the polished aluminum wing leading edges. The attached winglets are made of Kevlar, and significantly reduce drag.
Components
Fuel Tanks
The wing contains fuel in three areas. The right and left wings contain the main tanks (between the spars), and the wing center section forms the auxiliary tank. A bulkhead on either side of the wing center section separates the auxiliary and wing tanks.
Main Landing Gear
The main landing gear, mounted in the wings, are conventional oleopneumatic, shock-absorbing struts, fitted with two wheels on each strut.
FUSELAGE
Description
The CL–605 fuselage is a semimonocoque structure, and is made up of three sections: the nose, center and tail sections. The nose section includes the nose landing gear and flight compartment, while the center section includes the avionics area and cabin. The wing, which contains the main landing gear, is bolted to the fuselage behind the avionics bay. The tail section encloses an equipment bay, and supports the engines and empennage.
Components
Nose Section
The nose section contains:
.
中国公务机网 www.gongwuji.com
公务机翻译 www.aviation.cn
本文链接地址：庞巴迪挑战者605公务机机组操作手册 CL605-AIRPLANE_GENERAL(2)
| 
