AUTOFLIGHT System has been demonstrated with & without Yaw Dampers and autothrottle & with both 25 & 30 landing flaps Headwind : 25 kt / Tailwind : 24 kt / Crosswind : 33 kt (Rollout performance has been demonstrated on dry runways using each autobrake setting (AFM Section 3.1 page 8) On approach, for autoland verify LAND2 or LAND3 status, as appropriate, prior to 600 ft.
(AFM Section 3.1 page 8)
Demonstrated RNP Flight capability Versus Mode of Flight MODE OF FLIGHT FMC GPS OPERATIONAL FMC GPS NOT OPERATIONAL LNAV with A/P engaged LNAV with FD engaged Manual control with MAP display only
0.20 NM 0.39 NM 0.92 NM
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0.26 NM 0.52 NM 1.79 NM
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BOEING 767 SYSTEMS REVIEW
AUTOMATIC FLIGHT Copyright Smartcockpit.com Ludovic ANDRE / version 00
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BOEING 767 SYSTEMS REVIEW
AFDS DIAGRAM
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Page 3
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BOEING 767 SYSTEMS REVIEW
AUTOTHROTTLE DIAGRAM AUTOTHROTTLE DIAGRAM
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