曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
OEI One Engine Inoperative
OGP International Association of Oil & Gas Producers
OHIR Offshore Helideck Inspection Report
OIAC Offshore Industry Advisory Committee
OIM Offshore Installation Manager
ON Operations Notice (HSE)
OPEX Operating Expense
OPITO Offshore Petroleum Industry Training Organisation (Now COGENT)
OSD Offshore Safety Division of the HSE Hazardous Industries Directorate
PFEER Prevention of Fire and Explosion and Emergency Response Regulations Emergency Response Regulations
PIR Passive Infra-Red
PO Point of Origin
POB Persons on Board
PPE Personal Protection Equipment
QFE Indication of height above a set datum (e.g. and airfield or helideck)
QNH Indication of altitude above mean sea level
RAO Response Amplitude Operator
RFF Rescue and Firefighting
RFFF Rescue and Fire Fighting Facilities
rms. root mean square
R/T Receive / Transmit
SCE Safety Critical Element
SCR Safety Case Regulations
SLA Safe Landing Area
SN Safety Notice (HSE)
SRG Safety Regulation Group (of CAA)
SSCV Semi Submersible Crane Vessel
TDP Take-Off Decision Point
TGWU Transport & General Workers Union
UKCS United Kingdom Continental Shelf
UKOOA United Kingdom Offshore Operators Association
UPS Un-interruptable Power Source
VHF Very High Frequency
WAT Aircraft Performance Curve (Weight, Altitude, Temperature)
INTENTIONALLY BLANK
APPENDIX 4 – BELL 214ST - DESIGN INFORMATION
GENERAL DESIGN DATA (See Reference 49 for Additional Operational Data)
Overall Length (= ‘D’) 18.95 metres
Max. All Up Weight 7936 kg (t = 8.0)
0.83D Obstacle Limit Dimension = 15.73 m
0.62D Obstacle Limit Dimension = 11.75 m
0.12D Inner Obstacle Limitation = 2.27 m @ Height 948 mm
0.21D Outer Obstacle Limitation = 3.98 m @ Height 948 to 2938 mm
Minimum Foam Application Rate (where ‘D’ equals SLA) 1552 ltrs per min
RFF Category H1 / H2
Landing Net Size Medium, 12m x 12m
Passenger Access Sliding Main Cabin Door Both Sides
Refuelling Method Gravity only
Refuelling Point Locations Single point to rear of Starboard Cabin Door
Fuel Type Jet A-1
Max. Fuel Load (Standard Tanks) 2840 lbs (2271 ltrs)
Undercarriage Tricycle
UNDERCARRIAGE FOOTPRINT (Not to Scale)
Nosewheels:
Contact Area (each): 123 cm2 Loading: 22 %
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：离岸直升机起落甲板设计指南 OFFSHORE HELIDECK DESIGN GUIDELINES 2(77)
