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rigging pages. You can always go back to the RIGGING INDEX
page if you push LSK 6R when it says PREV MENU.
DFCS - TRAINING INFORMATION POINT - DFCS BITE PAGES - RIGGING - STABILIZER 1
EFFECTIVITY
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DFCS - TRAINING INFORMATION POINT - DFCS BITE PAGES - RIGGING - STABILIZER 1
DFCS - TRAINING INFORMATION POINT - DFCS BITE PAGES - RIGGING - STABILIZER 1
EFFECTIVITY
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Stabilizer Rigging Continue
This shows more pages of the stabilizer rigging test.
DFCS - TRAINING INFORMATION POINT - DFCS BITE PAGES - RIGGING - STABILIZER 2
EFFECTIVITY
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DFCS - TRAINING INFORMATION POINT - DFCS BITE PAGES - RIGGING - STABILIZER 2
DFCS - TRAINING INFORMATION POINT - DFCS BITE PAGES - RIGGING - STABILIZER 2
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General
This graphic is for reference.
DFCS - SYSTEM SUMMARY 1
EFFECTIVITY
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DFCS - SYSTEM SUMMARY 1
DFCS - SYSTEM SUMMARY 1
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General
This graphic is for reference.
DFCS - SYSTEM SUMMARY 2
EFFECTIVITY
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DFCS - SYSTEM SUMMARY 2
DFCS - SYSTEM SUMMARY 2
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
Purpose
The yaw damper system keeps the airplane stable around the
airplane yaw (vertical) axis. During flight, the yaw damper
commands rudder movement in proportion to and opposite to
the airplane yaw moment. This keeps unwanted yaw motion to
a minimum and makes the flight smoother. The yaw damper is
an autoflight system.
Unwanted airplane yaw motion is caused by either of the
following conditions:
* Dutch roll
* Air turbulence.
Abbreviations and Acronyms
* ac - alternating current
* ADR - air data reference
* ADIRU - air data inertial reference unit
* AOA - angle of attack
* ARINC - Aeronautical Radio Incorporated
* ATR - Austin Trumbull Radio
* BITE - built in test equipment
* CAA - Civil Aviation Authority
* CDS - common display system
* CDU - control display unit (FMC)
* CPC - cabin pressure controller
* CPU - central processing unit
* dc - direct current
* DEU - display electronic unit
* DFCS - digital flight control system
* EHSV - electro-hydraulic servo valve
* FAA - Federal Aviation Administration
* FMC - flight management computer
* FMCS - flight management computer system
* FMS - flight management system
* IR - inertial reference
* I/O - input/output
* LRU - line replaceable unit
* LVDT - linear variable differential transformer
* MCP - mode control panel
* N1 - engine low pressure rotor (fan) speed
* N2 - engine high pressure rotor speed
* NN - a number from 01 to 99
* PCU - power control unit
* PLI - pitch limit indicator
* SMYD - stall management yaw damper
* SWS - stall warning system
　
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