Oct 1, 2006 #1 amorrison Mechanical Joined Dec 21, 2000 Messages 605 Location CA Can anyone state what the design "g" load for a commercial helicopter fuselage should be? Sites? Two hours of Googling has got me nothing <(
Can anyone state what the design "g" load for a commercial helicopter fuselage should be? Sites? Two hours of Googling has got me nothing <(
Oct 18, 2006 2 #2 Nigel New member Joined Mar 7, 2000 Messages 136 Location CA Depends on the flight condition. Ultimate positive maneuvering load factor is 5.25g. Emergancy landing is 20g down. http://www.airweb.faa.gov/Regulator...9DEF90770C26A3EC85256613006B2A8B?OpenDocument http://www.airweb.faa.gov/Regulator...358E4FDB3E6DA09585256613006B87A3?OpenDocument http://www.airweb.faa.gov/Regulator...B44B8F62F28BEFCE85256613006B8902?OpenDocument Nigel Waterhouse B Eng (Hon's) Can-Am Aerospace,LLC, Canadian Aircraft Certification Centre http://www.canamaero.com Upvote 0 Downvote
Depends on the flight condition. Ultimate positive maneuvering load factor is 5.25g. Emergancy landing is 20g down. http://www.airweb.faa.gov/Regulator...9DEF90770C26A3EC85256613006B2A8B?OpenDocument http://www.airweb.faa.gov/Regulator...358E4FDB3E6DA09585256613006B87A3?OpenDocument http://www.airweb.faa.gov/Regulator...B44B8F62F28BEFCE85256613006B8902?OpenDocument Nigel Waterhouse B Eng (Hon's) Can-Am Aerospace,LLC, Canadian Aircraft Certification Centre http://www.canamaero.com