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canadair ctiauentjer OPERATING MANUAL PSP 606 SECTION 1 AIRCRAFT - GENERAL TABLE OF CONTENTS Subject Page MODEL DESIGNATION AND TYPE 1 OPERATING ROLE AND DESIGN CONCEPT 1 WING 1 IFUSELAGE 2 Nose Section Centre Section I Tail Section 3 AIRCRAFT DIMENSIONS 3 AIRCRAFT TURNING RADII 3 IDANGER AREAS 4 AIRCRAFT PARKING AND MOORING 4 SERVICING POINTS 4 AIRCRAFT ANTENNAS 4 DOORS 4 Passenger/Crew Upward Opening Door 5 Airstair Passenger/Crew Downward Opening Door 6 Emergency Exit Door 6 I Baggage Compartment Door 7 Rear Equipment Bay Door Service Doors |FLIGHT COMPARTMENT 8 Instrument and Control Panels Crew Seats Cabin Sign Controls cacnhaadllaeinr ger OPERATING MANUAL PSP 606 LIST OF ILLUSTRATIONS Figure Number Title Page 1 Aircraft General Details 9/10 2 Aircraft Basic Dimensions and Ground Clearances (2 sheets) 11 [3 Aircraft Turning Radii 13 4 Engine Intake and Exhaust Danger Areas 14 5 Aircraft Parking and Mooring 15/16 6 Aircraft Covers and Plugs 17/18 7 Aircraft Servicing Points 19/20 8 Aircraft Antenna Locations 21 9 Passenger/Crew Upward Opening Door (2 Sheets) 22 10 Passenger/Crew Downward Opening Door 24 111 Door Warning Indication (2 Sheets) 25 12 Baggage Compartment Door 27 13 Rear Equipment Bay Door 28 114 Service Doors and Panels 29 15 Flight Compartment Instrument and Control Panels (4 Sheets) 30 116 Crew Seats (2 Sheets) 35 J17 Cabin Sign Control Switches 37 1 - CONTENTS Page 2 Mar 01/85 cacnhaadllaeinr ger OPERATING MANUAL PSP 606 SECTION 1 AIRCRAFT - GENERAL MODEL DESIGNATION AND TYPE The aircraft, manufactured by Canadair Limited, is designated Model CL-600 and named Challenger. The Challenger is a swept-wing monoplane powered by two Avco Lycoming ALF 502L-2 Turbofan engines. OPERATING ROLE AND DESIGN CONCEPT Primarily, the Challenger is a long-range (transcontinental) business aircraft with a crew of two. The design concept is orientated toward carrying up to 19 passengers in spacious comfort oyer long distances. The combination of an advanced technology supercritical wing, quiet and efficient engines, and a wide body enables the Challenger to achieve a high standard of performance, economy and passenger comfort. WING (Figure 1) The aircraft wing is an advanced technology symmetrical airfoil structure manufactured as a single unit and bolted to the underside of the fuselage. The wing comprises left and right swept-back airfoils connected by a central box structure, and consists of skinned spars and ribs. Ailerons, flaps, spoilers, integral fuel tanks and the support structure of the main landing gear are incorporated into the wing. Wing leading edges are of aluminum alloy and incorporate thermal anti-icing. Wing tips are of Kevlar to save weight and to facilitate repair. On aircraft incorporating Canadair Service Bulletin 600-0401, the wing leading edge tapers toward a winglet. Each winglet is constructed from aluminum alloy with a Kevlar leading edge. Fuel for the aircraft is stored in three tank areas. The deep section airfoil each side is used as a main tank and the centre section is used as an auxiliary tank. A fuel-tight bulkhead each side of the centre section separates the tanks, and all tanks are compartmented to ensure a continuous supply of fuel to the engines under all normal flight conditions. On aircraft so modified, additional auxiliary tanks are installed, one forward and one aft of the main auxiliary tank. The main landing gear (MLG) assemblies, mounted under the wing left and right airfoils inboard of the trailing edge flaps, are conventional oleo-pneumatic, shock-absorbing struts, each fitted with two wheels. The MLG retracts inward into bins in a well in the underside of the fuselage. SECTION 1 Page 1 Mar 01/85 canatiair ctianenQer OPERATING MANUAL PSP 606 FUSELAGE (Figure 1) The fuselage is an all-metal, semi-monocoque structure comprising nose, centre and tail sections riveted together. The fuselage consists of externally skinned frames, stringers and longerons. The nose section is mainly the flight compartment area, the centre section is the passenger cabin area and avionics bay under which the wing is bolted, and the tail section is mainly an equipment bay to which the engines and empennage are attached. A. Nose Section The nose section is effectively divided by the flight compartment floor into upper and lower halves. The upper half comprises the flight compartment and www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：Bombardier-Challenger_00-Aircraft_General
