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时间:2011-10-21 17:06来源:蓝天飞行翻译 作者:航空
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Overall Length (= ‘D’)  22.2 metres 
Max. All Up Weight   9298 kg  (t = 9.3) 
0.83D Obstacle Limit Dimension   = 18.43 m 
0.62D Obstacle Limit Dimension   = 13.76 m 
0.12D Inner Obstacle Limitation   = 2.66 m @ Height 1100 mm 
0.21D Outer Obstacle Limitation  = 4.66 m @ Height 1100 to 3431 mm 
Minimum Foam Application Rate (where ‘D’ equals SLA)  2129 ltrs per min 
RFF Category  H1 / H2 
Landing Net Size  Large, 15m x 15m 
Passenger Access  Starboard Side Front and Rear Doors 
Refuelling Method  Pressure and Gravity 
Refuelling Point Locations  Starboard side adjacent to Sponson 
Fuel Type  Jet A-1 
Max. Fuel Load (Standard Tanks)  4350 lbs (2475 ltrs) 
Undercarriage  Tailwheel 

UNDERCARRIAGE FOOTPRINT (Not to Scale)
Mainwheels:
4.27m
Contact Area (each): 374 cm2 Loading: 85 %

 

 


Tailwheel:
Contact Area: 277 cm2 Loading:  15 %
7.15m
INTENTIONALLY BLANK

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 %
INTENTIONALLY BLANK

(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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本文链接地址:离岸直升机起落甲板设计指南 OFFSHORE HELIDECK DESIGN GUIDELINES 2(81)