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STL 945.7136/97 AIRBUS A319/A320/A321 Flight deck and systems briefing for pilots THIS BROCHURE IS PROVIDED FOR INFORMATION PURPOSES ONLY AND ITS CONTENTS WILL NOT BE UPDATED. IT MUST NOT BE USED AS AN OFFICIAL REFERENCE. FOR TECHNICAL DATA OR OPERATIONAL PROCEDURES, PLEASE REFER TO THE RELEVANT AIRBUS DOCUMENTATION STL 945.7136/97 Issue September 1998 STL 945.7136/97 STL 945.7136/97 Contents 1. General 2. Flight deck layout 3. Electrical system 4. Hydraulic system 5. Flight controls 6. Landing gear 7. Fuel system 8. Engine controls 9. Auxiliary power unit 10. Automatic flight system 11. Environmental flight system 12. Electronic instrument system 13. Radio management and communication 14. Maintenance centralized fault display system 1 STL 945.7136/97 STL 945.7136/97 1. General 1.1 STL 945.7136/97 A319/A320/A321 General 1.2 A319 A320 A321 STL 945.7136/97 A319/A320/A321 general 1.3 A319-100 A320-100 A320-200 A321-100 Span Length Height Fuselage Diameter Track Max. pax Max. FL 34.10m 111ft 10in 33.84m 111ft 33.91m 111ft 3in 34.10m 111ft 10in 37.57m 123ft 3in 44.51m 146ft 11.76m 38ft 7in 3.95m 12ft 11in 7.59m 24ft 11in 145 180 390 220 STL 945.7136/97 A319/A320/A3210 general 1.4 Engine Maximum weights (kg) Operation limits Model Manuf. Type Mmo Vmo A319-111 A319-112 A319-113 A319-114 A319-115 A319-131 A319-132 A319-133 A319 Corporate Jet A320-111 A320-211 A320-212 A320-214 A320-231 A320-232 A320-233 A321-111 A321-112 A321-131 A321-211 A321-231 CFM CFM CFM CFM CFM IAE IAE IAE CFM IAE CFM CFM CFM CFM IAE IAE IAE CFM CFM IAE CFM IAE CFM56-5B5 CFM56-5B6 CFM565A4 CFM56-5A5 CFM56-5B7 V2522-A5 V2524-A5 V2527-M-A5 CFM56-5-B6/5B7 V2524-A5/V2527-M-A5 CFM56-5-A1 CFM56-5A1/5A3 CFM56-5A3 CFM56-5B4 V2500-A1 V2527-A5 V2527E-A5 CFM56-5B1 CFM56-5B2 V2530-A5 CFM56-5B3 V2533-A5 64 000 (options : 68 000 or 70 000) 75 500 68 000 73 500 (options : from 68 000 up to 77 000) 83 000 (options : 78 000 or 85 000) 89 000 61 000 62 500 63 000 64 500 73 500 (option : 74 500) 75 000 57 000 58 000 59 000 60 500 (option : 61 000) 69 500 (option : 70 500 71 500 MTOW MLW MZFW 0.82 350kt STL 945.7136/97 A319/A320/A321 introduction 1.5 The A319/A320/A321 are narrow body, twin-engined, short / medium-range aircraft, the A319 being the shortened version of the A320, and the A321 being the stretched version of the A320. They both offer an increased fuselage cross-section leading to an increased revenue potential through : - greater passenger comfort with wider seats and aisle - greater overhead baggage volume - greater cargo capacity - wide-body compatible container capability - quicker turnrounds. Advanced technology applied to aerodynamics, structure, systems and powerplant offer reduced costs through : - unmatched fuel efficiency - more accurate flight path control - reduced maintenance costs - increased reliability - reduced trouble-shooting time. Introduced for airline service in March 1988, the A320 represents the largest single advance in civil aircraft technology since the introduction of the jet engine and results in a major stride forward in airline profitability. A computer-managed system gives complete protection against excursions outside the normal flight envelope and greatly improves the man / machine interface.
STL 945.7136/97 2.1 2. A319/A320/A321 flight deck layout
STL 945.7136/97 2.3 A319/A320/A321 flight deck – plan view Capt. sidestick F / O sidestick F / O nav. bag 3rd occupant seat Capt. nav. bag 4th occupant seat (optional) Coat stowage An observer seat aft of the pedestal offers maximum visibility over all panels. www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A319/A320/A321飞行员驾驶舱和系统简介
