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0.83D Obstacle Limit Dimension = 17.33 m
0.62D Obstacle Limit Dimension = 12.95 m
0.12D Inner Obstacle Limitation = 2.51 m @ Height 1044 mm
0.21D Outer Obstacle Limitation = 4.39 m @ Height 1044 to 3236 mm
Minimum Foam Application Rate (where ‘D’ equals SLA) = 1883 ltrs per min
RFF Category H1 / H2
Landing Net Size Large, 15m x 15m
Passenger Access Starboard Side at Front
Refuelling Method Pressure and Gravity
Refuelling Point Locations Gravity filling point at each sponson. Pressure connection on port sponson.
Fuel Type Jet A-1
Max. Fuel Load (Standard Tanks) 2877 ltrs (760 US galls)
Undercarriage Tricycle
UNDERCARRIAGE FOOTPRINT - LOADS FOR PLANNED AIRCRAFT GROWTH
(Not to Scale)
6.20 m 3.18 m
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Nosewheels (at max fwd C of G):
Static Load per u/c Gear: 4592 kg Static Contact Area per Tyre: 265.0 cm2 Dynamic Load per u/c Gear: 5970kg Dynamic Contact Area per tyre: 323.3 cm2
Mainwheels (at max aft C of G):
Static Load per u/c Gear: 4453 kg Static Contact Area per Tyre: 258.0 cm2 Dynamic Load per u/c Gear: 5788 kg Dynamic Contact Area per tyre: 316.7 cm2
GENERAL ARRANGEMENT
(Courtesy of Sikorsky Aircraft)
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离岸直升机起落甲板设计指南 OFFSHORE HELIDECK DESIGN GUIDELINES 2(82)
