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Numerically the ACN is two times the derived single wheel load expressed in thousands of kilograms. The derived single wheel load is defined as the load on a single tire inflated to 1.25 Mpa (181 psi) that would have the same pavement requirements as the aircraft.
The AS350 B3 is powered with a TURBOMECA ARRIEL 2 engine of 847 shp (632 kW) and equipped with a dual channel FADEC system (Full Authority Digital Engine Control). This engine makes it perfectly suited for operations in conditions such as mountainous or elevated areas or hot and dry areas.
The A350 AIRCRAFT CHARACTERISTICS - AIRPORT AND MAINTENANCE PLANNING (AC) manual is issued for the A350-900 and A350-1000 series aircraft to provide necessary data to airport operators, airlines and Maintenance/Repair Organizations (MRO) for airport and maintenance facilities planning.
Flight Manual AS 350 B Flight Manual, initially approved by DGAC FR on 27 October 1977, or later EASA (or DGAC FR) approved revision (reference: in French language).
Can carry up to 369 passengers in a two class configuration (54 + 315). Track width between the center of the landing gears is 10.73 meters (35 feet and 2.4 inches) and 12.84 meters (42 feet and 1.5 inches) between outer sides of landing gear.
Tractors in this line are equipped with diesel powered engines, power shift transmissions, and four wheel drive axles with rubber pneumatic tires. The B350 tractor is capable of maneuvering aircraft under a wide range of climatic conditions. NOTE: MAINTENANCE SPECIFICATIONS ARE CONTAINED IN CHAPTER2, SECTION4. ALL
documents that require manual searching by engineers and mechanics. Completion of diagnosis while the flight is still in progress will save time when rectifying the fault during turnaround. Without fault data transmission, line mechanics have to examine fault codes on the MCDU after the aircraft has landed, and enter them on the tech log before
