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CHC find S92 & AW139 "Unacceptable"

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CHC find S92 & AW139 "Unacceptable"

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Old 29th Mar 2007, 04:45
  #61 (permalink)  
 
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yes you do, though I think 'short', rather than 'receding', was the word you were looking for!

Not sure where the 16 comes from: we have 18 plus a cabin attendent.
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Old 29th Mar 2007, 06:30
  #62 (permalink)  
 
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'Open Door' management..

... perhaps if CHC had listened to one of their employees back in May of 2006, they wouldn't have this problem now...? I gather that he's still looking for work, but I loved the report he wrote entitled 'S92 Doomsday Report'. Suddenly being on the other side of the apron seems like a good thing!!
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Old 29th Mar 2007, 09:32
  #63 (permalink)  
 
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Question

... perhaps if CHC had listened to one of their employees back in May of 2006, they wouldn't have this problem now...?
And what problem is that? I'm not quite sure what you are getting at! As someone who flies the 139 for CHC I would like to know what you think the problem is!
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Old 29th Mar 2007, 09:36
  #64 (permalink)  
 
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Availability of resources..

... including adequate (minimal) numbers of pilots and engineers trained on type before the aircraft arrived in country? I'm up north, so haven't heard much on the 139 front, but can't walk across the apron without hearing about the 92!
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Old 29th Mar 2007, 11:47
  #65 (permalink)  
 
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S-92 seating

Worldwide survey of potential operators stated they wanted S-92 w/o a non-paying passenger (flight attendant). Present S-92 seating complies with the FAA regarding how many passengers can be seated w/o a flight attendant. IOW, crew of two is $$ ahead.
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Old 31st Mar 2007, 16:52
  #66 (permalink)  
 
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I've been reading the last issue of vertical mag. and there is a good report about the 139 in the field.
You can read it from the website.

Regards
Aser ( 139 lover)
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Old 31st Mar 2007, 22:34
  #67 (permalink)  
 
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During it's early years the S76A shed main rotor blades due to spindle failures. I believe that at least one aircraft was also lost due to tail rotor cable failure. Hence the big mod to the bellcrank on the tail gearbox.

In the days when Bond operated 6 S76A's at one point they used to remove a pair of turbines from one aircraft every Friday night, send them to overhaul for a decoke and then refit them in time for monday morning.

Then they also had to armour the engine compartment in case of uncontained turbine failures. I recollect that mod weighed about 20 kilos.

The current fleet is now mature and maybe people have forgotten what a pain it can be to integrate a completely new type in the offshore environment.

The only aircraft I remember arriving quietly was the 365N, but that was on the back of the 365C which had operated for a number of years.
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