Transcription of TECHNICAL SPECIFICATIONS & STANDARD EQUIPMENT LIST
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TECHNICAL SPECIFICATIONS & STANDARD EQUIPMENT LIST
TECHNICAL SPECIFICATIONS & STANDARD EQUIPMENT LIST TECHNICAL SPECIFICATIONS & STANDARD EQUIPMENT LIST Page 2 Note: Information contained within this report is proprietary to Viking Air Limited and provided for reference purpose only. Provision of this information does not constitute any form of contractual commitment between Viking Air Limited and the recipient. No warranty or representation is made to the accuracy or applicability of the information contained herein, and data is subject to change without notice. DOCUMENT REVISION: 01-18 Aircraft Overview The Viking DHC-6 Series 400 Twin Otter aircraft is an all-metal, high wing monoplane, powered by two wing-mounted turboprop engines, each driving a three-bladed, reversible pitch, fully feathering propeller. The aircraft carries a pilot, co-pilot, and up to 19 passengers, depending upon the seating configuration. The Series 400 is an updated version of the Series 100, 200, and 300 Twin Otters.
aileron control systems. Five hinge arms are provided on each mainplane rear spar to carry the flap/aileron system. The wing tips, which are removable for servicing and maintenance, have internal lightning protection bonding strips that are secured to each wing structure to provide a ground for electrical discharge.
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