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Optimal Category-A Helicopter Flight Trajectories for Operation From a Clear HeliportEngine failure represents a major safety hazard to helicopter operation. As a result, FA certifies helicopters according to their abilities to survive engine failures. Federal Aviation Regulation Part 29 specifies that transport helicopters must be certified as either category A or B. Category-B certification applies to either single or multi-engine helicopters with gross weight less than 20,000 lbs. A Category-B helicopter must be able to land safely in the case of one or all engine failures. There is no requirement for continued flight capability. In contrast, Category-A certification applies to multi-engine helicopters with independent engine systems. It requires that helicopter can continue flight with one engine inoperative (OEI). Therefore, Category-A helicopters are capable of operating from rooftops and oil rigs and flying to areas where no emergency landing sites are available. While there is no maximum weight limit, a Category-A helicopter must be able to satisfy OEI operation requirements within the available runway field. Additional information is contained in the original extended abstract.
Document ID
20020011642
Acquisition Source
Ames Research Center
Document Type
Other
Authors
Sharma, Vivek
(Minnesota Univ. Minneapolis, MN United States)
Zhao, Yiyuan
(Minnesota Univ. Minneapolis, MN United States)
Chen, Robert T. N.
(NASA Ames Research Center Moffett Field, CA United States)
Hindson, William S.
(NASA Ames Research Center Moffett Field, CA United States)
Aiken, Edwin W.
Date Acquired
August 20, 2013
Publication Date
January 1, 1995
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: AHS 51st Forum and Technology Display
Location: Fort Worth, TX
Country: United States
Start Date: May 9, 1995
End Date: May 11, 1995
Sponsors: American Helicopter Society, Inc.
Funding Number(s)
PROJECT: RTOP 505-59-36
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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