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* ADIRS - air data inertial reference system
* ADIRU - air data inertial reference unit
* ADR - air data reference
* AOA - angle of attack
* ARINC - Aeronautical Radio Inc.
* asym - asymmetry
* ATR - Austin Trumbull Radio
* BITE - built-in Test equipment
* CAA - Civil Aviation Authority
* capt - captain
* CB - circuit breaker
* CDS - common display system
* CMD - command
* com - common
* CPC - cabin pressure controller
* DC - direct current
* deg - degree
* DEU - display electronics unit
GUN 001-099, 101-113, 115, 201-999
* EFS - elevator feel shift
* EFSM - elevator feel shift module
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* eng - engine
* F/O - first officer
* FCC - flight control computer
* FDAU - flight data acquisition unit
* ft - feet
* FMCS - flight management computer system
* FSEU - flap slat electronics unit
* gnd - ground
* GPWC - ground proximity warning computer
* IR - inertial reference
* k - knot
* L - left
* LE - leading edge
* MCP - mode control panel
* MMO - mach maximum operating
* No. - number
* norm - normal
* PLI - pitch limit indication
* POS - position
* PSEU - proximity switch electronics unit
* R - right
* RA - radio altitude
* sec - second
* SMYD - stall management yaw damper
* SS - stick shaker
GUN 001-099, 101-113, 115, 201-999
* stall ID - stall identification
GUN ALL
* sws - stall warning system
STALL WARNING SYSTEM - INTRODUCTION
EFFECTIVITY
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
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* TAI - thermal anti-ice
* TE - trailing edge
* TOGA - takeoff/go-around
* UCM - uncommanded motion
* v - volt
* Vcas - computed airspeed
* VMO - velocity maximum operating
* Vsf - speed floor velocity
* warn - warning
* WTRIS - wheel-to-rudder interconnect system
STALL WARNING SYSTEM - INTRODUCTION
EFFECTIVITY
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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
27-32-00-001
STALL WARNING SYSTEM - INTRODUCTION
STALL WARNING SYSTEM - INTRODUCTION
EFFECTIVITY
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
27-32-00-001
General
The stall warning system shakes the control column when the
airplane gets close to a stall.
GUN 001-099, 101-113, 115, 201-999
The stall ID system makes sure the pilot cannot easily
overcome automatic nose down trim of the airplane during a
stall. During a stall, the stall warning system increases control
column feel forces.
GUN ALL
These are the components of the stall warning system:
* Stall management yaw dampers (SMYDs)
* Control column shakers
GUN 001-099, 101-113, 115, 201-999
* Elevator feel shift module (EFSM)
GUN ALL
* Stall warning test panel.
GUN 001-099, 101-113, 115, 201-999
During a stall, the FCCs command the stabilizer to trim the
airplane nose down. The EFSM and column cut-out switch
modules operate to make sure the pilot cannot easily stop this
automatic stabilizer movement with the elevator control column
nose up input.
GUN ALL
These are the components and systems that supply data to the
stall warning system:
* Stall warning test panel
* Angle of attack sensors
* Air data inertial reference system (ADIRS)
* Flap position transmitters
* Flap slat electronics unit (FSEU)
* Common display system (CDS)
* Mode control panel (MCP)
* Proximity switch electronic unit (PSEU).
GUN 001-099, 101-113, 115, 201-999
The EFSM and the control column shakers receive discrete
signals from the stall warning system.
GUN 114
The control column shakers receive a discrete signal from the
stall warning system.
GUN ALL
SWS - GENERAL DESCRIPTION
EFFECTIVITY
GUN ALL 27-32-00
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BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
27-32-00-002
SWS - GENERAL DESCRIPTION
SWS - GENERAL DESCRIPTION
EFFECTIVITY
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Page 5
D633A101-GUN Jun 10/2006
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
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