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EUROSAFETY INTERNATIONAL, LLC
United States
Registrace 28. 09. 2010
EuroSafety's Online Classroom.
In an age where operational safety and pilot proficiency play a crucial role in the survival of any operation, EuroSafety provides the tools necessary to give your pilots the skills needed to operate at their highest level.
EuroSafety's initial, advanced recurrent and differences training includes indepth ground schools using high-tech computer graphics and animations. EuroSafety's flight training includes full down autorotoations, hydraulic and tailrotor failures.
EuroSafety is the most cost effective manner in which you can provide high end training to your pilots. There is no better way to ensure that your crewmembers have the necessary skills and knowledge to operate your aircraft at the safest level than to utilize EuroSafety for your training needs.
In an age where operational safety and pilot proficiency play a crucial role in the survival of any operation, EuroSafety provides the tools necessary to give your pilots the skills needed to operate at their highest level.
EuroSafety's initial, advanced recurrent and differences training includes indepth ground schools using high-tech computer graphics and animations. EuroSafety's flight training includes full down autorotoations, hydraulic and tailrotor failures.
EuroSafety is the most cost effective manner in which you can provide high end training to your pilots. There is no better way to ensure that your crewmembers have the necessary skills and knowledge to operate your aircraft at the safest level than to utilize EuroSafety for your training needs.
Preliminary report from on-going Gold Coast helicopter mid-air collision investigation
The two Eurocopter EC130 helicopters were being operated by Sea World Helicopters (a separate corporate entity to the theme park) on 5-minute scenic flights. One helicopter with a pilot and 5 passengers on board was on approach to land at a helipad adjacent to the Sea World theme park and the second, with a pilot and 6 passengers, had just departed a separate but nearby helipad within the theme park when they collided above the Broadwater.
“The ATSB has released this preliminary report to detail the circumstances of this tragic accident as we currently understand them, but it is important to stress that we are yet to make findings,” said ATSB Chief Commissioner Angus Mitchell.
“Our findings as to the contributing factors to this accident, and the analysis to support those findings, will be detailed in a final report to be released at the conclusion of our investigation.”
Mr Mitchell said the preliminary report details factual information, including the accident’s sequence of events.
“The factual information detailed in this report is derived from interviews with survivors of the accident, including the surviving pilot and passengers, and witnesses; analysis of video footage and images taken by passengers on board both helicopters, onlookers on the ground, and CCTV from nearby buildings; examination of the wreckage of both helicopters; and a review of recorded radio calls and aircraft tracking and radar data.”
The preliminary report details that the helicopters were operating from two separate helipad facilities about 220 metres apart, a pad within the theme park, and a pad to the south at the operator’s own heliport, adjacent to the park. The 5-minute scenic flights were to follow the same counter-clockwise orbit, with the inbound helicopter, registration VH-XH9 (XH9) on approach to land at the heliport to the south and the outbound helicopter, registration VH-XKQ (XKQ) having departed the pad to the north from within the theme park.
The two helicopters collided at an altitude of about 130 feet, 23 seconds into the departing XKQ’s flight.
The main rotor blades of helicopter XKQ entered the forward cabin of XH9. XKQ broke apart in mid-air and impacted shallow water next to a sandbar. The pilot and 3 passengers were fatally injured, and 3 passengers were seriously injured. The helicopter was destroyed.
Helicopter XH9 sustained significant damage to the forward cabin, instrument console, and main rotor blades. The impact turned XH9 to the left, and the pilot continued with the momentum of that movement, completing a 270° descending turn to land on the sandbar below them near to XKQ. The pilot and 2 passengers were seriously injured, and 3 other passengers had minor injuries.
The helicopters were operating in non-controlled airspace where pilots use a common traffic advisory frequency (CTAF) to make radio calls to announce their position and intentions, and, as required, to arrange separation with other aircraft.
The report details the radio calls made by the pilot of the returning helicopter XH9, and that as they tracked south over the Broadwater, that the pilot saw passengers boarding XKQ as it was preparing to depart.
The pilot of XH9 recalled that their assessment was that XKQ would pass behind them, and that they did not recall the pilot of XKQ making a standard “taxiing” call announcing their intention to depart.
“This does not necessarily mean that a taxi call was not made, and the ATSB investigation will undertake a detailed analysis of the nature of the radio calls made,” Mr Mitchell noted.
The report also details that the pilot of XH9 did not see XKQ depart from the park helipad.
While video footage taken by passengers in both helicopters on mobile phones contained images of the other helicopter, this does not mean that the other helicopter was visible to either pilot.
“The investigation will look closely at the issues both pilots faced in seeing the other helicopter,” Mr Mitchell said.
“We have already generated a 3D model of the view from the pilot’s seat from an exemplar EC130 helicopter which we will use as part of a detailed visibility study to help the investigation determine the impediments both pilots faced in sighting the other helicopter.”
Mr Mitchell said the investigation will also look more broadly beyond the issues of radio calls and visibility.
“The ATSB will also consider the operator’s procedures and practices for operating scenic flights in the Sea World area and the process for implementing the recently-acquired EC130 helicopters into operation, and will review the regulatory surveillance of the operator and similar operators.”
“The ATSB has released this preliminary report to detail the circumstances of this tragic accident as we currently understand them, but it is important to stress that we are yet to make findings,” said ATSB Chief Commissioner Angus Mitchell.
“Our findings as to the contributing factors to this accident, and the analysis to support those findings, will be detailed in a final report to be released at the conclusion of our investigation.”
Mr Mitchell said the preliminary report details factual information, including the accident’s sequence of events.
“The factual information detailed in this report is derived from interviews with survivors of the accident, including the surviving pilot and passengers, and witnesses; analysis of video footage and images taken by passengers on board both helicopters, onlookers on the ground, and CCTV from nearby buildings; examination of the wreckage of both helicopters; and a review of recorded radio calls and aircraft tracking and radar data.”
The preliminary report details that the helicopters were operating from two separate helipad facilities about 220 metres apart, a pad within the theme park, and a pad to the south at the operator’s own heliport, adjacent to the park. The 5-minute scenic flights were to follow the same counter-clockwise orbit, with the inbound helicopter, registration VH-XH9 (XH9) on approach to land at the heliport to the south and the outbound helicopter, registration VH-XKQ (XKQ) having departed the pad to the north from within the theme park.
The two helicopters collided at an altitude of about 130 feet, 23 seconds into the departing XKQ’s flight.
The main rotor blades of helicopter XKQ entered the forward cabin of XH9. XKQ broke apart in mid-air and impacted shallow water next to a sandbar. The pilot and 3 passengers were fatally injured, and 3 passengers were seriously injured. The helicopter was destroyed.
Helicopter XH9 sustained significant damage to the forward cabin, instrument console, and main rotor blades. The impact turned XH9 to the left, and the pilot continued with the momentum of that movement, completing a 270° descending turn to land on the sandbar below them near to XKQ. The pilot and 2 passengers were seriously injured, and 3 other passengers had minor injuries.
The helicopters were operating in non-controlled airspace where pilots use a common traffic advisory frequency (CTAF) to make radio calls to announce their position and intentions, and, as required, to arrange separation with other aircraft.
The report details the radio calls made by the pilot of the returning helicopter XH9, and that as they tracked south over the Broadwater, that the pilot saw passengers boarding XKQ as it was preparing to depart.
The pilot of XH9 recalled that their assessment was that XKQ would pass behind them, and that they did not recall the pilot of XKQ making a standard “taxiing” call announcing their intention to depart.
“This does not necessarily mean that a taxi call was not made, and the ATSB investigation will undertake a detailed analysis of the nature of the radio calls made,” Mr Mitchell noted.
The report also details that the pilot of XH9 did not see XKQ depart from the park helipad.
While video footage taken by passengers in both helicopters on mobile phones contained images of the other helicopter, this does not mean that the other helicopter was visible to either pilot.
“The investigation will look closely at the issues both pilots faced in seeing the other helicopter,” Mr Mitchell said.
“We have already generated a 3D model of the view from the pilot’s seat from an exemplar EC130 helicopter which we will use as part of a detailed visibility study to help the investigation determine the impediments both pilots faced in sighting the other helicopter.”
Mr Mitchell said the investigation will also look more broadly beyond the issues of radio calls and visibility.
“The ATSB will also consider the operator’s procedures and practices for operating scenic flights in the Sea World area and the process for implementing the recently-acquired EC130 helicopters into operation, and will review the regulatory surveillance of the operator and similar operators.”
zhlédnutí: 439
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My left ear found this really informative, but my right ear got a bit bored.
I got what you are saying. Yes I know helicopters.... film/audio and and still working on that skill set. I just figured out the mistake I was making with editing and now audio out of both sides.
@@EUROSAFETYTRAINING Don't mind my comment, I was just having a bit of a laugh, I don't even know what a swashplate is, I'm a software engineer. I'm guessing YT recommended me this video cause I look stuff up for Microsoft Flight Sim and DCS, but your videos are really cool :)
I like your helmet.
Excellent tip. To combat this issue our SOP is to cycle the rotor brake handle and make sure it is locked all the way forward as part of our pre-start procedure.
It would have been a water landing for me. Thank God.
Does it shut down immediately if it's a hot start etc ,or do you do it manually?
I am not quite sure if I understand the question, but if the engine is running and the start selector is placed in the off position the engine is shut off
Most of time faced it.
Thanks for this important information
You should show this to Kevin
Plus the engines at full throttle, while it would brake the rotor significantly even if it was pulled back and locked; wouldn’t immediately make it drop like a rock; if the pilot couldn’t throw that back forward quick enough to recover, he shouldn’t be flying. Let’s say I was oblivious the rotor brake was engaged, I’d immediately see we’re losing rotor speed while maintaining full flight power and that would be the first thing to check, did my idiot sitting next to me pull the rotor brake; otherwise I’d start staging for an autorotation looking for where I can land since something has happened that’s seizing the driveshafts, but in that case you can’t even do a good autorotation, so just hope and pray really 😳
In the welding world they always told us to first use the back of your hand ,I guess the logic being is you can sense heat radiation more readily.......but I suspect it's not the same temp ranges as weldaments etc
I always thought that was because it’s easier to dress a burn on the back of your hand than the palm 😂
Great advice! Just one small nitpick: the swashplate bearing is now greased every 150 hours. Especially in the dual hydraulic B3e’s like your on. Perhaps the 100 hour requirement is still in place for the older models….
Thank you! I will look into that
Yeah, I think we do this every 150h too
Realistic and very helpful. Nice!
Thanks for your his video, was told a while ago that it was 4” but couldn’t find any documentation to confirm. Can you say where the 4”’s comes from? Does it make a difference between different types? (ie Astar vs EC120)
Good morning... that information along with other ground handling information can be found in Chapter 10 of the maintenance manual.
Demonstrate it then and let's see.
Does the tail rotor blade pitch synchronize to the main rotor?
The pitch of the tail rotor blades are controlled by the yaw pedals in cockpit
Although I agree, nothing should be touched unless authorized by the pilot. Theres no telling if certain parts of the aircraft will fail prematurely while meddling. Best to save those mechanisms for when it matters most and test/meddle while not in the air.
How many times has pulling the rotor brake handle in mid flight been tested to see what actually will happen? (My point is the pilot reaction was understandable)
I really like your channel
Thanks
Aerospace engineer here, rotor brake would fail quickly, but in the short time, it would throw an incredible amount of torque through the air frame.
Feed the beast 😊
Can you perform ground resonance? I will pay for the damages as well!
What happens when the torque limitations are exceeded? For 1 or 2 seconds above 104% what is the maintenance required?
Yes, any limitation that is exceed a maintenance action is required. Regarding the specific action required will be dependent on the amount and time the over limit was exceeded. For a light over limit an inspection is required. If sever enough the transmission has to be overhauled.
seriously, so simple)
Let's say you are at KPHX - Phoenix Sky Harbor Airport in the summer. The metar reports 115 F which is below the 50 degree operations limit .The VEMD however is at 120 F due to the temp probe reading the heat coming off the ramp -which is above the 50 degree limit. Are you then above the 50 degree temperature limit for operations or are you ok to fly? Thanks!
This is a good question that is often asked. The temp limit is not 50, it is ISA+35. Fifty was the cap they put on it because in Israel ISA + 35 can get you above 50 which is a limit on many components on helicopter. So as a pilot in the US you disregard 50 and use ISA + 35. In Phoenix the temp limit would be 47.7. The temperature limit is based on the effects of high temperature on components and longevity of components on the helicopter. If the helicopter is operating in those temperatures the limit applies. Reported temperature is the temperature somewhere different than the helicopter, hence the helicopter is not effected by that temperature. If there will be high temperatures it is best to park the helicopter on a surface that will not create higher temperatures.
@@EUROSAFETYTRAINING Thank's for the reply! Much appreciated!
I'll remember that when loading my helicopter.
Thanks for the explanation. I came looking for it bc I didn’t buy that you could just manually brake the rotor while it’s spinning at full speed lmao
One suggestion: You might want to show them how to remove and install the chip detector. I find that it is difficult to remove unless you take the wiring plug off first. Also where to look for the chips. Or tell the viewers to get training from their mechanic on how to check the chip plug prior to getting a light. I appreciate all your hard work on these videos!! Keep them coming!
Can you guys demonstrate landing in slopes please?
I love you ecureuil!
if a manufacturer makes a self destruction handle so accessible, it would be sued and had gone bankrupt long before. It can cause trouble but obviously it can’t be that lethal.
1200 feet gos quick auto rotating
Collective?!
I am a physician worked at a trauma center. We had an mbb twin jet helicopter. I was friends with the pilot. He took me up and let me take the controls. Flying around is easy! Taking off is not that difficult. Landing and hovering is goddamn impossible! I don't even know how you work up to it. Respect.
Hi Glen, goes without saying that this is another great video. Question on the delta Ng gauge: is it normal to have a decent split between the engines? For example, Engine 1 running at -2.7 and then Engine 2 running at -4.5 in flight at cruise.
Thank you, I appreciate it! No that is not normal at all. Have you done a power check on engines?
@@EUROSAFETYTRAINING Will do one this week
@@EUROSAFETYTRAINING To get back to you on this, we discovered it was a faulty ambient air pressure reading from the computer in engine 1
I want this guy flying any helicopter I'm in
I have been in an auto and never realized it till we landed and the rotors slowed on there own.
So hard to tell what the rotors are doing with the frame rate of the camera doing its thing but certainly sounded like rpm decade a lil but them he got them back.must have been the glide slope or lack there of that amounted to the rough landing.
I never knew a VEMD even existedm so thanks - but is that an avionics fit?
It is in many of the Airbus Helicopters products
You guys are awesome. Love the app and all the yt content. Looking at coming over from New Zealand to upskill with your company. Thanks for the great videos 👍👍👍
thanks! We look forward to flying with you!
Thanks for letting us know 👍. Is it a bias value or direct info from thermocouples to the gauge? For start up i mean. Thanks Glen 😊
On the 2D engine the thermocouple voltage goes to EECU which then bias' the value that is programmed into the EDR, on the 2B/2B1 the thermocouple is connected to the T4 confirmation box which bias' the value to the specific engine.
So, if we faced ECU failure, May we see different values for T4 on the gauge or EBCAU can handle this on 2D?
I love these little jewels of knowledge. Thanks Glen! 👏👏👏
Glad you like them!
Really appreciate what you do. 12 years inspection, At what time the TBO inspection
Nice autorotation. It's a life saving maneuver. Any landing you can walk away from is a good landing! 🚁
Well I guess it is written this way because not all 350 have a filter on the intake. Very unlikely that you will have snow in the intake with an IBF or sand filter installed. Still need to check that the filter is not covered with snow.
Most helicopters in the US have barrier filters. But a barrier filter does not remove the possibility of ice around the bend in the air intake. Why do you think it would be very unlikely? Does a carburetor filter remove the possibility of carb ice? Nothing in the flight manual or supplement indicate the removal of this limitation with the installation of a filter. Very easy to check in the intake for ice.
I really like your channel it's very clear and well done
Thank you!
when the indicator mark more negative is better beacuse the engine have enough power and when is more positve means is close to maximun trasient is reach maximun performance or the engine will no longer be able to give more power
These are great, Kevin. Keep them coming!
While in an autorotation he gives a selfie ☺️
Скажу по английски: It's a good thing I wasn't there, otherwise I would have had to sniff the shit, or maybe end up in it.