AW139 accident India
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Joined: Aug 2011
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From: Brasil - Rio de Janeiro
AW139 accident India
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An Agusta Westland AW 139 (VT-GVI) helicopter with four occupants crashed in the Paud area of Pune, due to strong winds and bad weather.
The helicopter was going from Mumbai to Hyderabad.
The captain suffered injuries and was hospitalized.



An Agusta Westland AW 139 (VT-GVI) helicopter with four occupants crashed in the Paud area of Pune, due to strong winds and bad weather.
The helicopter was going from Mumbai to Hyderabad.
The captain suffered injuries and was hospitalized.




Joined: Feb 2006
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From: At home


Joined: Oct 1999
Aviation Qualifications: ATPL
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From: Den Haag


Joined: Mar 2011
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From: London/Atlanta
Quote
“Global Vectra AW-139 makes an emergency landing due to technical defect near Pune. Excellent work by the pilots and all on board safe.”
Is that an emergency landing or a crash?
Either way good news there were no fatalities.
“Global Vectra AW-139 makes an emergency landing due to technical defect near Pune. Excellent work by the pilots and all on board safe.”
Is that an emergency landing or a crash?
Either way good news there were no fatalities.


Joined: Oct 1999
Aviation Qualifications: ATPL
Posts: 7,373
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From: Den Haag

Joined: Sep 2005
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From: Montreal
Weather looks fine. Looks like an autorotation into trees, low rpm. Unlikely fuel starvation so soon after takeoff. Tail rotor? Would explain going into trees instead of maneuvering for a clearing. Pilot played the hand he was dealt.
Curious what "technical defect" they've identified so soon, even faster than the usual Pprune gunslingers.
Curious what "technical defect" they've identified so soon, even faster than the usual Pprune gunslingers.

Joined: Nov 2010
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From: Australia
From video on X, seemed like fuz / rotor disk was pitched up to around 60-70 degrees just before impact. Would a pilot intentionally do that to (say) wash off forward speed if this was indeed an autorotation?? That leaves little to arest the descent.


Joined: Oct 1999
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From: Den Haag
Joined: May 2002
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From: Wanaka, NZ

Joined: Mar 2005
Aviation Qualifications: Military
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From: Aus
Does the 139 have completely independent fuel system for each engine like the S76
§ 29.953 Fuel system independence.
(a) For category A rotorcraft—(1) The fuel system must meet the requirements of § 29.903(b); and
(2) Unless other provisions are made to meet paragraph (a)(1) of this section, the fuel system must allow fuel to be supplied to each engine through a system independent of those parts of each system supplying fuel to other engines.
(b) Each fuel system for a multiengine category B rotorcraft must meet the requirements of paragraph (a)(2) of this section. However, separate fuel tanks need not be provided for each engine.
§ 29.903 Engines
(b) Category A; engine isolation. For each category A rotorcraft, the powerplants must be arranged and isolated from each other to allow operation, in at least one configuration, so that the failure or malfunction of any engine, or the failure of any system that can affect any engine, will not—
(1) Prevent the continued safe operation of the remaining engines

Joined: Jul 2009
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From: Luna
There have been many issues with pilots over reacting on the flight controls due to a surprise or perceived upset (floats inflated in flight, resulting in full pedal and a 90 degree roll induced by the pilot, recent 9 minute UA, other inadvertent AP release incidents etc) where the behaviour of the Nf could trigger the overspeed protection and subsequent reversion to manual control. Inadvertently hitting the Tq limiter (if selected on) during a recovery from turbulence could also decay the Nr, leading to a perception of a failure.
Be careful with your collective rates of movement, unexpected stuff can happen as a result!
Having said that, I wasn't in the cockpit and I have no idea why they ended up like this. Wishing them all a speedy recovery.



