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‡aDOT/FAA/CT-90/14
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‡asdr-ucbk.b115444063
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‡aCU-IT
‡cCU-IT
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‡a(OCoLC)24185797
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‡aDecision-height windows for decelerating approaches in helicopters :
‡bpilot/vehicle factors and limitations /
‡c[R.H. Hoh ... et al.]
|
260 |
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‡aAtlantic City International Airport, N.J. :
‡bFederal Aviation Administration Technical Center ;
‡aSpringfield, Va. :
‡bAvailable through the National Technical Information Service,
‡c[1991]
|
300 |
⊔ |
⊔ |
‡aviii, 39, A-11, B-3 p. :
‡bill. ;
‡c28 cm.
|
500 |
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⊔ |
‡a"April 1991."
|
500 |
⊔ |
⊔ |
‡aCover title.
|
504 |
⊔ |
⊔ |
‡aIncludes bibliographical references (p. 39).
|
513 |
⊔ |
⊔ |
‡aFinal report.
‡bJan. 1989-May 1991.
|
536 |
⊔ |
⊔ |
‡aPrepared by Systems Control Technology, Inc. under contract no.
‡bDTFA01-87-C-00014.
|
538 |
⊔ |
⊔ |
‡aMode of access: Internet.
|
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‡aHelicopters
‡xPiloting
‡xHuman factors.
|
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‡aHelicopters
‡xPiloting.
|
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0 |
‡aHelicopters
‡xLanding.
|
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‡aHoh, R. H.
|
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‡aSystems Control Technology, Inc.
|
710 |
2 |
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‡aFederal Aviation Administration Technical Center (U.S.)
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‡dIII - MILLENIUM
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‡rpd
‡qbib
‡tUS fed doc--NTIS: pubdate < 2019
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