DEVELOPMENTAL FLIGHT TEST AND CERTIFICATION DETAILS OF THE MARK II LEARJET

760472

02/01/1976

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
A program to develop and certify a system utilizing advanced technology designed to improve the basic Learjet is discussed. The specific goals of the design included improvement of stall characteristics, reduction in stall speeds, improvement of low speed handling characteristics, reduction of takeoff and landing distances, improving the high altitude hot day takeoff performance and reduction of high speed drag.
Successful, as well as unsuccessful ideas are discussed, along with the significant FAA certification details including determination of stall speeds, determination of climb performance, and determination of the takeoff and landing distances.
Meta TagsDetails
DOI
https://doi.org/10.4271/760472
Pages
41
Citation
GRAYSON, S., and FRINELL, R., "DEVELOPMENTAL FLIGHT TEST AND CERTIFICATION DETAILS OF THE MARK II LEARJET," SAE Technical Paper 760472, 1976, https://doi.org/10.4271/760472.
Additional Details
Publisher
Published
Feb 1, 1976
Product Code
760472
Content Type
Technical Paper
Language
English