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Old 6th August 2012 | 19:47
  #861 (permalink)  
 
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From: 55 degrees north ish.
Why not submit a RFI (request for information) to EC UK, they have fitted many of these to UK aircraft.

pm me if you would like a specific email address.
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Old 8th August 2012 | 00:23
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From: UK
Aucky - to your question "does that swap with the window?", the answer is effectively "yes", although the "with ease" bit may be more of a challenge. It's effectively a one for one swap, just the skill of the engineer that dictates how long it takes them to get the rubber strip back in, as either window tend to be a bit of a b**tard to re-fit.

Just beware that if you intend to practice an emergency push out of a sliding door window, and you have the choice, use the one without the sliding insert. I heard on the (good authority) grapevine that someone tried pushing out one with the insert but, owing to the small amount of original plastic (frame) around the sliding insert, one good thump split the plastic and effectively wrote off the window! Didn't learn if the insert was able to be re-used?
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Old 8th August 2012 | 16:38
  #863 (permalink)  
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Ah another u/s Skyquest screen.........
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Old 8th August 2012 | 16:52
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From: 55 degrees north ish.
Ah another u/s Skyquest screen.........
You sound surprised...

Last edited by RotaryWingB2; 8th August 2012 at 16:53.
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Old 9th August 2012 | 07:42
  #865 (permalink)  
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From: After all, what’s more important than proving to someone on the internet that they’re wrong? - Manson
ASB EC135 62A-029

ASB62-029 MAIN ROTOR SYSTEM – Main Rotor Hub-Shaft - Visual inspection of the upper and lower hub-shaft flange for cracks - Rev3

With Revision 3 of this Alert Service Bulletin Part 3 of the Alert Service Bulletin is no longer required.


Part 3 being
(a) Accomplish the visual inspection in the area of the blade bolts i.a.w. Section 3.B. Part 3 within the next 10 fh after receipt of this Alert Service Bulletin and repeat every 10 fh.
Note: The preflight visual still remains

That removes a serious logistics headache for now at least!
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Old 9th August 2012 | 10:05
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From: 55 degrees north ish.
Still a requirement for the engineer to visit every 10fh, just no removal of the nuts necessary.

It's a step in the right direction though.
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Old 9th August 2012 | 12:18
  #867 (permalink)  
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Rotary Wing,
my sarcasm didn't come across me thinks.

Amazing how well they work.Not.

We have made sure the arm on which the screen is bolted on to is taken out as well when the screen is u/s because you couldn't really call it safe in case of an incident......
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Old 14th August 2012 | 16:11
  #868 (permalink)  
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From: Europe
Does anybody fly their 135 with cargo net fitted in the rear?

What is the part number of the net and approx. price?

Any problems installing the net beside flir guts?
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Old 5th October 2012 | 11:01
  #869 (permalink)  
WLM
 
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From: 3 Degrees North
Phoinix, I was quoted EUR3000 for that cargo net, in South East Asia... Part number is L850M4807053 from IPC EC135
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Old 5th October 2012 | 11:08
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From: 3 Degrees North
Stretcher for 135

Hi,

Can you recommend a supplier for a simple stretcher kit that would fit in the internal cabin rails? we are not a medevac operator, but a private timber operator in the South East Asian jungle.

I need to be able to do a quick change from a rear 4 seats corporate cabin interior to only keeping 2 rear seats and a stretcher whenever there is an emergency evacuation required

Rgds
WLM
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Old 5th October 2012 | 12:05
  #871 (permalink)  
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From: Europe
Thank you WLM!
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Old 5th October 2012 | 13:05
  #872 (permalink)  
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We use the Bucher stretcher which folds in half when stowed and uses the rails to secure itself.
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Old 5th October 2012 | 13:40
  #873 (permalink)  
 
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From: 55 degrees north ish.
Bucher Leichtbau AG

Air rescue / Police equipment - Bucher Leichtbau AG, Bucher Aerospace, Galleys, Stowages, Catering Carts, Trolleys, Aircraft Parts, Cabin Interior Equipment, Emergency Medical Systems, Aircraft Stretchers, Air Rescue Equipment, Video Arms, Video Depl

Same products used in UK Police Aircraft.
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Old 5th October 2012 | 14:18
  #874 (permalink)  
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From: After all, what’s more important than proving to someone on the internet that they’re wrong? - Manson
is another option as well.
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Old 5th October 2012 | 17:32
  #875 (permalink)  
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From: Europe
A question for which TM didn't have an answer. On Pratt, you get a fadec fail at very low power setting. With twistgrip in neutral you flip out the pins and rotate the twistgrip past neutral to high setting. Doest the rate of twistgrip ensure that even at very low power fadec fail, the twistgrip can still deliver max power if needed?
These fadec/twistgrip governing ranges are a bit unclear to me.

Last edited by Phoinix; 5th October 2012 at 17:34.
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Old 5th October 2012 | 20:02
  #876 (permalink)  
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From: Germany
Foldable stretcher

Hi WLM,
we also use the foldable Bucher-stretcher which works very well for as as we fly transports of injured persons only occasionally.
Sent you a PM.

Kind regards

Tom
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Old 5th October 2012 | 23:31
  #877 (permalink)  
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From: After all, what’s more important than proving to someone on the internet that they’re wrong? - Manson
Phoinix,

From what has been shown to me if you set the offending engine at ~ .7 VEMD or thereabouts you can fly the full flight envelope without the other good engine exceeding OEI limits.

The training policy at ECD these days is you can chase numbers all over the place yet the reality is you don't need to.

Apparently you do not get "FULL" power in manual. Whatever FULL means.

And you will not get it on a Bell 205 or 212 or 412 either so....................

Last edited by RVDT; 5th October 2012 at 23:37.
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Old 6th October 2012 | 03:56
  #878 (permalink)  
WLM
 
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From: 3 Degrees North
Thank you for the replies concerning the stretcher, I will check them all
Regards
WLM
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Old 9th November 2012 | 11:56
  #879 (permalink)  
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From: Europe
Just a feedback from a ECD test pilot... twist grips give you twice the range needed, so if FADEC is stuck in minimum position, you are able to get the whole twist for full power if needed.


And a really serious question I couldn't find a solution for on T.I.P.I.

The modification for tail mounted balancing weights. Where can we (our company) get the modification done (Other than ECD).

Is the modification really an airframe modification, or is it just "light upgrade work". - I'm not up to maintenance phraseology.
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Old 9th November 2012 | 17:28
  #880 (permalink)  
 
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From: below sea level
Tail balance weights mod

Hi Phoinix,
If your company is situated in Slovenia.
You can look if some big operator in Germany (ALT, DRF...) can perform this modification for you.

I think you can call this a modification because the aft structure of the fenestrone body is modified with a mounting bracket, weights and an access panel. Also your weight and balance is affected.
Its not an afternoons job...

Some of my own experience. We have the weights also installed but the brackets tend to crack after time. We received the upgraded brackets which are from thicker material but also these have cracks reported.

Hope you can use this info.
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