Go Back  PPRuNe Forums > Aircrew Forums > Rotorheads
Reload this Page >

Category A Helicopter's

Wikiposts
Search
Rotorheads A haven for helicopter professionals to discuss the things that affect them

Category A Helicopter's

Thread Tools
 
Search this Thread
 
Old 26th Jan 2004, 21:45
  #1 (permalink)  
Thread Starter
 
Join Date: Jul 2002
Location: Ca
Posts: 13
Likes: 0
Received 0 Likes on 0 Posts
Category A Helicopter's

Hi

Anyone know's where i can find a list of the certified helis, for the different category??

Or, at least, if you could, reply with the ones, thar you know that
they are, and in witch conditions (weight,configuration... etc.)

What are the one's REALLY category A , class 1.


thanks

best regards
USRotor is offline  
Old 2nd Feb 2004, 04:29
  #2 (permalink)  
 
Join Date: Feb 2004
Location: longwayplace
Posts: 239
Likes: 0
Received 3 Likes on 2 Posts
Howdy,

Are you searching for multis that satisfy Class I performance criteria at maximum gross mass?......Or just at any mass at all?.......Clear area?......or Helipad?.....What is your mission profile?.........How warm might it be?.....or would sir prefer Class A certification?.........

............just curious
Bomber ARIS is offline  
Old 2nd Feb 2004, 21:17
  #3 (permalink)  
Thread Starter
 
Join Date: Jul 2002
Location: Ca
Posts: 13
Likes: 0
Received 0 Likes on 0 Posts
Hi

yes, at a reduced weight, is possible to perform, but in most cases the fuel/payload relation will be downgraded

imagine a profile like this

5/6 POB, +2hrs fuel, IFR, helipads/confined areas, 8000ft DA

* what are the ones, that do it at MGW
and

* the ones that with this profile, and with "that" reduced weight can perform class 1

and tell me if you dn't think that well be needed to use "ovesized" helos, to comply with everything...

regaards
USRotor is offline  
Old 2nd Feb 2004, 21:58
  #4 (permalink)  
 
Join Date: Dec 2001
Location: Philadelphia PA
Age: 73
Posts: 1,835
Likes: 0
Received 2 Likes on 2 Posts
8,000' DA??
Have to do better than that, I'm afraid.
Is that 8,000' Pressure Altitude, ISA (which would be -1C), or something else?
12,000' PA, -40C, or 4,000' +40C - makes a huge difference to the engines, you know.
With turbine engines you can't just talk about a density altitude, especially for something like Category A where you are going to be engine limited.
Shawn Coyle is offline  
Old 2nd Feb 2004, 23:33
  #5 (permalink)  
Thread Starter
 
Join Date: Jul 2002
Location: Ca
Posts: 13
Likes: 0
Received 0 Likes on 0 Posts
sorry, my fault

let's use, your number

4000ft +40 ºC
USRotor is offline  
Old 3rd Feb 2004, 22:11
  #6 (permalink)  
 
Join Date: Dec 2001
Location: Philadelphia PA
Age: 73
Posts: 1,835
Likes: 0
Received 2 Likes on 2 Posts
US rotor
sorry to leap on you like that. Bit of a pet peeve of mine - most helicopter pilots don't know that power required is a density altitude thing, and power available is a pressure altitude and OAT thing - and there is a difference as you can see above.
I don't know of too many Category A machines that will have much worthwhile performance at +40C, regardless of the pressure altitude - good luck.
Shawn Coyle is offline  
Old 3rd Feb 2004, 22:58
  #7 (permalink)  
Thread Starter
 
Join Date: Jul 2002
Location: Ca
Posts: 13
Likes: 0
Received 0 Likes on 0 Posts
Shawn : no problem

yes, this was only an "academic" type of question,

but we can change to a little more "real" profile

3000ft and 30ºc seems ok ?


i only want to find out, in a typicall EMS/utility, profile mission what sould be the minium "sized" helo needed. for a class 1, Jar ops requirements..
USRotor is offline  
Old 3rd Feb 2004, 23:04
  #8 (permalink)  
 
Join Date: Feb 2004
Location: longwayplace
Posts: 239
Likes: 0
Received 3 Likes on 2 Posts
That's a big ask

EC135 at 4000' PA, +40*C, plus 2 hours fuel leaves approx 120 kg payload.
i.e. enough for one pilot plus a 3 year old passenger!

Buena suerte!!!
Bomber ARIS is offline  
Old 4th Feb 2004, 04:17
  #9 (permalink)  
 
Join Date: Jul 2002
Location: CH
Posts: 116
Likes: 0
Received 0 Likes on 0 Posts
EC 135 P2

LBA approved 9.1-1 FM supplement (not FAA)

Cat A clear area PA 3000' OAT +32C 2835 kg (Gross weight)

Cat A Vertical 2580kg in the same conditions and NO H/V area! Depending on the EEW that gives me a useful of 780 kgs at the "reasonable temps". Aircraft is air conditioned and "lite" SPIFR as well.
John Bicker is offline  
Old 5th Feb 2004, 05:38
  #10 (permalink)  
 
Join Date: Dec 2001
Location: Philadelphia PA
Age: 73
Posts: 1,835
Likes: 0
Received 2 Likes on 2 Posts
Re EC-135 Cat A performance...
Ah, the benefit of the 30" and 2' OEI ratingst that Digital Fuel controls have given us...
Shawn Coyle is offline  

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are Off
Refbacks are Off



Contact Us - Archive - Advertising - Cookie Policy - Privacy Statement - Terms of Service

Copyright © 2024 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.