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2nd Annual Business Aircraft Conference
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The Effect of a Light Aircraft Stability Augmentation System on Pilot Performance
- Technical Paper
- 660220
- DOI: https://doi.org/10.4271/660220
Published
1966-02-01
by SAE International in United States
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Defining the Fatigue Load Environment for Business Aircraft
- Technical Paper
- 660215
- DOI: https://doi.org/10.4271/660215
Published
1966-02-01
by SAE International in United States
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A Practical Data Processing Approach for Achieving Effective Management Control of Aircraft Manufacture
- Technical Paper
- 660205
- DOI: https://doi.org/10.4271/660205
Published
1966-02-01
by SAE International in United States
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Development and Flight Testing a Simplified Fixed Shaft Turboprop Flight Control System
- Technical Paper
- 660218
- DOI: https://doi.org/10.4271/660218
Published
1966-02-01
by SAE International in United States
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Support Breeds Success and Successors
- Technical Paper
- 660213
- DOI: https://doi.org/10.4271/660213
Published
1966-02-01
by SAE International in United States
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Cessna Aircraft Commercial Division Quality Control Program
- Technical Paper
- 660204
- DOI: https://doi.org/10.4271/660204
Published
1966-02-01
by SAE International in United States
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The Jet Pump as a Fuel Pump for Today's Aircraft
- Technical Paper
- 660223
- DOI: https://doi.org/10.4271/660223
Published
1966-02-01
by SAE International in United States
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FAA Research, Development, and Airworthiness Compliance for General Aviation Aircraft
- Technical Paper
- 660217
- DOI: https://doi.org/10.4271/660217
Published
1966-01-01
by SAE International in United States
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An Evaluation of General Aviation Aircraft Flying Qualities
- Technical Paper
- 660219
- DOI: https://doi.org/10.4271/660219
Published
1966-02-01
by SAE International in United States
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Adapting the Automotive Alternator to the Light Commercial Airplane Environment
- Technical Paper
- 660203
- DOI: https://doi.org/10.4271/660203
Published
1966-02-01
by SAE International in United States