HAC Oil & Gas IBP - Helicopter Association of Canada

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Reserve fuel weight required upon landing (lb orkg)Remarks:Notes:1. Hover Out of Ground Effect (HOGE) Performance:In calculating HOGE or one engine inoperative (OEI), planned performance shouldbe based on zero wind conditions, ambient temperature, based on the seasonalaverage for the area, and density altitude for the lowest level – mid Level- andhighest level of the intended work sites. Account should be taken of the additionalpower required to transition to forward flight over and above that required to hoverOGE.OGC IBP | Revision Date: Sept 2009 DRAFT41
CONSIDERATION OF SINGLE OR MULTI ENGINE HELICOPTER TYPEChoice of helicopter type for seismic support operations is dependant on a number offactors, but should include the exposure to risk in the event of an engine failure.The risk in the event of an engine failure can be summarized in the following table:Single Engine HelicopterTwin engine without OEIHOGETwin engine with OEIHOGENon HostileTerrainHostileTerrainTotal % Hostile terrain(From Part 1 Section 2)Mitigation factors that apply to this operation:1 New FAA/JAA 27/29 Certification Aircraft type.2 No passenger flights. Cargo/load only.3 Routing to avoid hostile terrain.4 HUMS/Engine Vibration Monitoring (EVMS) daily monitoring.5 Fuel quality assurance completed daily.67Helicopter Type for operationTypeRoleOGC IBP | Revision Date: Sept 2009 DRAFT42
Page 1: Oil & Gas Land Exploration Best Pra
Page 5 and 6: Table of ContentsOil & Gas Land Exp
Page 7 and 8: Oil & Gas Land Exploration Best Pra
Page 9 and 10: 1.5. Recommended minimum requiremen
Page 11 and 12: 3.0. Personnel Qualifications, Trai
Page 13 and 14: 3.1.6 MOUNTAIN FLYINGAimDemonstrate
Page 15 and 16: 3.2.1.8 Flight:a) Aircraft Emergenc
Page 17 and 18: 3.2.5 Other personnel and visitors
Page 19 and 20: 3.3.2 Engineers3.3.2.1 A minimum ma
Page 21 and 22: 5.1.5. ICAO Performance Class5.1.6.
Page 23 and 24: For external load work involving ve
Page 25 and 26: 6.3. Staging’s6.3.1 Staging and C
Page 27 and 28: 7. HELI-PADS (LZ)7.1 Detailed refer
Page 29 and 30: 9.1.5. For multi destination flight
Page 31 and 32: 10. PASSENGER TRANSPORT10.1 Passeng
Page 33 and 34: 8. Decision/Approval matrix for Med
Page 35 and 36: HETS (HELICOPTER EXTERNAL TRANSPORT
Page 37 and 38: (3) Authorization may be granted fo
Page 39 and 40: weight and balance calculation proc
Page 41 and 42: ANNEX A RISK ASSESSMENTHELICOPTER S
Page 43 and 44: Operating ConditionsProject Name(co
Page 45 and 46: 4. There is an unacceptable risk of
Page 47: Aircraft Performance PlanningProjec
Page 51 and 52: 25 Local/regulatory constraints on
Page 53 and 54: RISK MATRIXRisk Assessment MatrixPR
Page 55 and 56: Methods of Reducing Risk Factors -
Page 57 and 58: B.5.3B.5.4Slings should be inspecte
Page 59 and 60: ANNEX C FIRE SAFETYC 1C.1.1GENERALS
Page 61 and 62: ANNEX D FUEL MANAGEMENTD.1 GENERALD
Page 63 and 64: D.5 FUEL TRANSPORT TO, AND STORAGE
Page 65 and 66: 3. Pump standpipes should extend no
Page 67 and 68: ANNEX F LINE HELIPAD DIAGRAM AND CO
Page 69 and 70: 3. Three months from construction:
Page 71 and 72: LightningHazard descriptionAircraft
Page 73 and 74: BOPERATIONAL HAZARDS & SUGGESTED CO
Page 75 and 76: Slings and nets, external cargo ope
Page 77 and 78: Local activitiesHazard descriptionN
Page 79 and 80: ANNEX H FATIGUE MANAGEMENT PROGRAMS
Page 81: ANNEX I AVIATION SERVICES CONTRACTI

HAC Oil & Gas IBP - Helicopter Association of Canada

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