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· Checks each shaker individually.
· Checks audio and visual warnings.
· Activates and monitors pitch disconnect lock for proper operation.
· Checks pusher for activation only under correct conditions (computer logic).
· Simulates a stall event and verifies AOA serviceability electronically (no AOA movement).
· Pushes both columns forward at the end of test.
Stall Protection Computer
A dualchannel
stall protection computer (avionics bay) monitors the following inputs:
· LH, RH Angleofattack
(AOA) transducers − Angle of attack
· LH, RH Lateral accelerometers − Lateral acceleration
· LH, RH Flap/slat − Flap/slat position
· #1, #2 weight on wheels (WOW) − WOW and SPS inhibit
· #1, #2 and #3 ADC, MACH Transducer − Airspeed, altitude and Mach
· Inertial Reference Unit (IRU) − Normal and lateral acceleration
· WOW Fail − Weight on wheels
The SPC receives data input from the bleed management controller, landing gear electronic
control unit, heater brake monitor unit and EMS CDU through the data acquisition units. The
EGPWS uses the AOA for windshear requirements.
Low speed awareness output is a function of the SPC to the Electronic Flight Instrument System
(EFIS).
· Red line − Shaker or stall warning speed.
FLIGHT CONTROLS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
10−10−59
STALL PROTECTION COMPUTER SCHEMATIC
FLIGHT CONTROLS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
10−10−60
STALL PROTECTION EICAS MESSAGES
STALL PROTECT FAIL
STALL WARN ADVANCE
STALL WARN BASIC
PITCH DISC FAULT
MACH XDUCER FAIL
SHAKER 12
FAIL
SHAKER 12
FAIL
GF1010_072a
(on airplane 9002 thru 9158).
FLIGHT CONTROLS
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
10−10−61
FLIGHT CONTROLS
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
10−10−62
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CB - FLT CONTROLS SYSTEM
STAT SYS BUS PREV CNTL TEST
PAGE
NEXT
PAGE
EMER
CNTL
BUS
CIRCUIT BREAKER − SYSTEM 1/2
CIRCUIT BREAKER SYSTEM
AFCS
AIR COND/PRESS
APU
BLEED
CAIMS
COMM
DOORS
ELEC
ENGINE
FIRE
FLT CONTROLS
FUEL
BRT
CB − FLT CONTROLS SYSTEM 1/4
CB − FLT CONTROLS SYSTEM 2/4
CB − FLT CONTROLS SYSTEM 3/4
CB − FLT CONTROLS SYSTEM 4/4
FLIGHT CONTROLS
EMS CIRCUIT PROTECTION
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
10−20−1
FLIGHT CONTROLS
EMS CIRCUIT PROTECTION
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
10−20−2
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