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The content of this document is the property of Airbus. ... @A319 AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING HIGHLIGHTS Revision No. 23 - Dec 01/20 ... Final Approach Speed May 01/14 CHAPTER 4 Subject 4-1-0 General Information May 01/14 Subject 4-2-0 Turning Radii Dec 01/15
One ECU located on the engine with dual redundant channels (active and standby) each having separate 28V DC aircraft power sources to ensure engine starting on ground and in flight. In addition dedicated ECU alternator assures self power above 12% N2 for CFM56 (10% N2 for IAE V2500).
The A319 is a shortened-fuselage variant of the Airbus A320 and entered service in April 1996 with Swissair, around two years after the stretched Airbus A321 and eight years after the original A320.
This article aims to highlight how the reference, limit and operating speeds are useful during descent, approach and landing. It also provides a description of the tools that are available and operational recommendations on how to manage the aircraft energy during the last phases of flight.
• The minimum speed during take-off roll at which the aircraft can still be controlled after a sudden failure of one engine (be it a two or four-engine airplane).
Manuals and User Guides for Airbus A319. We have 5 Airbus A319 manuals available for free PDF download: Manual, Instructor Support, Instructions Manual.
The Airbus A319 is a two-engined short- to medium-range narrowbody airliner with a capacity of maximum 160 Passengers produced by the European manufacturer Airbus S.A.S.. The A319 has the longest range of the A320-singe-aisle-family.
