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Neutral Reverse thrust levers ....................................................................... Set Position lever to agree with flap position. Set Verify PARK BRAKE light illuminated. STABILIZER TRIM cutout switches ............ NORM (guarded position) FUEL CONTROL switches..................................................... Locked Verify the lock lever is in the locked (forward) position and the WINDOW NOT CLOSED decal is not in view. Test and set Mask – Stowed Verify doors closed. NORMAL/100% switch – 100% RESET/TEST switch – Push and hold Verify the yellow cross appears momentarily in the flow indicator.

See title page for details. 2 D632T001-29LAL(LAL) December 15, 1999 A Normal Procedures Introduction 767 Operations Manual In LNAV and VNAV,all airplane course, vertical path, thrust, and speed changes must be verified. CDU Operation On the ground, the control display unit (CDU) manipulations are normally performed by the first officer and verified by the captain. In automatic flight, CDU entries are accomplished by the pilot flying and verified by the pilot not flying prior to execution. During high workload periods, using autopilot modes such as heading select, flight level change, and speed intervention features, along with the HSI MAP Switches, may be more efficient than entering complex route modifications into the CDU.

1 Non–AFM Operational Information ......................................... 2 Door Mounted Escape Slides.................................................... 3 Auto Flight ..................................................................................... 3 Engine ............................................................................................ 3 Engine Fuel System ....................................................................... 4 Copyright © The Boeing Company. See title page for details.

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767 Operations Manual - Lauda Air


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