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

Bell 206B info requested

Wikiposts
Search

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

Bell 206B info requested

Thread Tools
 
Search this Thread
 
Old 23rd September 2008 | 12:27
  #1 (permalink)  
Thread Starter
20 Anniversary
Veteran: Army
 
Joined: Jan 2006
Posts: 90
Likes: 2
From: USA
Question Bell 206B info requested

Working on a Bell 206B model for a flight sim (X-Plane), the following info would be very helpful:
  • Approximate total weight of a main rotor blade, plus amount & location of any tip weight - or even better, the polar moment of inertia for the main rotor.
  • Approximate main rotor collective pitch range
  • Tail rotor pitch limits
Thanks in advance!
brett s is offline  
Reply
Old 24th September 2008 | 09:31
  #2 (permalink)  
20 Anniversary
 
Joined: Sep 2003
Posts: 482
Likes: 0
From: Wessex
Hi Brett
206 Blade weight depends on part number - for the 010-200 series its 42.16 - 43.07kg (or 42.16 - 43.67kg if an STC leading edge strip is fitted). For the 015-001 series blade the weight is 43.39 - 44.29kg (top limit 44.9kg with STC strip)
There is a 600gram weight fitted at the tip with the STC strip otherwise the weights in the pockets are set to adjust the balance moments.
PM me if you need any further info
R2
Rocket2 is online now  
Reply
Old 24th September 2008 | 11:42
  #3 (permalink)  
Thread Starter
20 Anniversary
Veteran: Army
 
Joined: Jan 2006
Posts: 90
Likes: 2
From: USA
Thanks, that helps!
brett s is offline  
Reply

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 © 2026 MH Sub I, LLC dba Internet Brands. All rights reserved. Use of this site indicates your consent to the Terms of Use.