Skidz Posted October 25, 2014 Report Share Posted October 25, 2014 Cadors Number: 2014P1791 Occurrence Category(ies): System/component failure or malfunction [powerplant] Other Fuel related Occurrence Information Occurrence Type: Incident Occurrence Date: 2014-10-18 Occurrence Time: 1955 Z Day Or Night: day-time Fatalities: 0 Injuries: 0 Canadian Aerodrome ID: Aerodrome Name: Occurrence Location: N VANCOUVER INTL BC (CYVR) Province: British Columbia TC Region: Pacific Region Country: Canada World Area: North America Reported By: NAV CANADA Transportation Safety Board of Canada AOR Number: 180605-V1 TSB Class Of Investigation: Class 5 TSB Occurrence No: A14P0175 Occurrence Event Information Aircraft Information Registration Mark: GHJL Foreign Registration: Flight #: JBA784 Flight Rule: VFR Aircraft Category: Helicopter Country of Registration: Canada Aircraft Make: SIKORSKY Aircraft Model: S-76A Year Built: 1981 Amateur Built: No Engine Make: ALLISON Engine Model: 250-C30S Engine Type: Turbo shaft Gear Type: Land Phase Of Flight: Cruise Damage: No Damage Owner: Helijet International Inc Operator: HELIJET INTERNATIONAL INC. (4622) Operator Type: Commercial CARs Subpart: Aircraft Event InformationFuel - other Engine failure Declared emergency/priority Diversion Occurrence Summary Date: 2014-10-20 Further Action Required: Yes O.P.I.: Commercial & Business Aviation Narrative: A Helijet International Sikorsky S76 (JBA784) from Victoria Harbour, BC (CBF7) en-route to Vancouver Harbour, BC (CYHC), called Vancouver Tower requesting to land Runway 13 at Vancouver, BC (CYVR). Vancouver Tower initiated a precautionary standby. The aircraft landed without incident at 2000Z. No operational impact. Date: 2014-10-24 Further Action Required: Yes O.P.I.: Commercial & Business Aviation Narrative: UPDATE: TSB Report#A14P0175: The Helijet S76 (C-GHJL), flight JBA784, from Victoria Harbour (CBF7) to Vancouver Harbour (CBC7) was at 3000 feet over Point Grey when the number 2 engine (Rolls Royce 250 C30) lost power. An emergency was declared with Vancouver Harbour Tower and the flight diverted to Vancouver International (CYVR). The aircraft landed on runway 13. There were no injuries. It was determined a fuel governor had failed. The governor was replaced and the aircraft returned to service. A Service Difficulty Report has been filed with Transport Canada. Please note that for the most part, CADORS reports contain preliminary, unconfirmed data which can be subject to change. Quote Link to comment Share on other sites More sharing options...
rainman Posted October 25, 2014 Report Share Posted October 25, 2014 Sounds like they did a good job! Good to have that second stove... Quote Link to comment Share on other sites More sharing options...
helicpilot Posted October 29, 2014 Report Share Posted October 29, 2014 It is 4th one within 4 years.. One failed in GHJV-medevack machine, second with fire in GHJT, third GHJL, and now GHJL again... How many engine chip lights...no need to know. Quote Link to comment Share on other sites More sharing options...
Skidz Posted November 6, 2014 Author Report Share Posted November 6, 2014 Date: 2014-11-04 Further Action Required: No O.P.I.: Narrative: Update Maintenance & Manufacturing: The amplifier for the #2 droop compensator was replaced. Test flight carried out. Found satisfactory. Quote Link to comment Share on other sites More sharing options...
Skidz Posted November 7, 2014 Author Report Share Posted November 7, 2014 2014-11-06 Further Action Required: No O.P.I.: Narrative: UPDATE: TSB Report#A14P0183: The Helijet Sikorsky S-76A (C-GHJL) was on a test flight about 7 nm S of CYVR when the number 2 engine (Allison 250-C30S) experienced an uncommanded acceleration. The crew reduced power to the number 2 engine, declared an emergency and returned to CYVR for an uneventful landing. The number 2 engine and N2 governor had been recently replaced because of an 18 October 2014 power-loss event (occurrence number A14P0175) and engine chip light events on 23 and 25 Oct 2014 (occurrence number A14P0179). Following the 29 Oct 2014 uncommanded engine acceleration event, company maintenance replaced the droop compensator amplifier (p/n 76900-01880-106) and inspected the associated wiring. Quote Link to comment Share on other sites More sharing options...
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