Aircraft Accident Brief Ntsb/aab-02/01 (Pb2002-910401): Egypt Air Flight 990, Boeing 767-366er, Su-Gap - National Transportation Safety Board Page 16
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160 CAPTAIN’S
FIRST OFFICER’S
CONTROL COLUMN
CONTROL COLUMN
TENSION
CONTROL
FIRST OFFICER’S
REGULATOR
COLUMNS
QUADRANT
ELEVATOR CONTROL
OVERRIDE
(2 LOCATIONS)
CABLES
MECHANISM
OVERRIDE MECHANISM
STICK SHAKER
FEEL AND
(2 LOCATIONS)
CENTERING
UNIT
AUTOPILOT
CONTROL SERVO
(3 LOCATIONS)
CAPTAIN’S
ELEVATOR CONTROL
HORIZONTAL
CABLES
STABILIZER
FEEL
COMPUTER
SLAVE CABLE
INTERCONNECT
POSITION
AFT QUADRANT
TRANSMITTER
INTERCONNECT
(2 LOCATIONS)
ROD
LEFT AFT QUADRANT
OUTPUT ARM
SLAVE CABLE QUADRANT
CONTROL ROD
AFT QUADRANTS
(2 LOCATIONS)
OVERRIDE
MECHANISM
RIGHT AFT QUADRANT
RIGHT AFT QUADRANT
OUTPUT ARM CONTROL ROD
LEFT AFT QUADRANT
POWER CONTROL ACTUATORS (PCA’S)
LOST MOTION
(3 LOCATIONS ON EACH OUTBOARD ELEVATOR)
DEVICE
FWD
(2 LOCATIONS)
LEFT INBOARD ELEVATOR
(RIGHT SIDE EQUIVALENT)
LEFT OUTBOARD ELEVATOR
OUTBD
(RIGHT SIDE EQUIVALENT)
NOT TO SCALE
Figure 1a. Diagram of the components in the entire 767 elevator control system.
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