UNDERCARRIAGE FOOTPRINT (Not to Scale)
Mainwheels:
4.27m
Contact Area (each): 374 cm2 Loading: 85 %
Tailwheel:
Contact Area: 277 cm2 Loading: 15 %
7.15m
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APPENDIX 12 – SIKORSKY S76 - DESIGN INFORMATION GENERAL DESIGN DATA (See Reference 49 for Additional Operational Data)
Overall Length (= ‘D’) 16 metres
Max. All Up Weight 5307 kg (t = 5.3)
0.83D Obstacle Limit Dimension = 13.28 m
0.62D Obstacle Limit Dimension = 9.92 m
0.12D Inner Obstacle Limitation = 1.92 m @ Height 800 mm
0.21D Outer Obstacle Limitation = 3.36 m @ Height 800 to 2480 mm
Minimum Foam Application Rate (where ‘D’ equals SLA) 1106 ltrs per min
RFF Category H1 / H2
Landing Net Size Medium, 12m x 12m
Passenger Access Central Cabin Door on Both Sides
Refuelling Method Gravity only
Refuelling Point Locations Both sides to rear of Cabin Doors
Fuel Type Jet A-1
Max. Fuel Load (Standard Tanks) 1850 lbs (839 kg)
Undercarriage Tricycle
UNDERCARRIAGE FOOTPRINT (Not to Scale)
Nosewheel:
Contact Area: 115 cm2 Loading: 25 %
5.0m
2.44m
Mainwheels:
Contact Area (each): 107 cm2 Loading: 75 %
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(Aircraft data supplied courtesy of Sikorsky Helicopters - Please note that helidecks designed to facilitate S92 operations should use the higher MAUW to accommodate planned future growth. All other dimensions remain the same)
GENERAL DESIGN DATA
APPENDIX 13 – SIKORSKY S92 - DESIGN INFORMATION
Overall Length (= ‘D’) = 20.88 m
Max. All Up Weight (current certified) Max. All Up Weight (planned growth) = 11859 kg (t = 11.9) = 12837 kg (t = 12.8)
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