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Volume 2 Flight Crew Operating Manual Rev 3, Apr 25, 2005
The digital readout of the IAS/Mach will be displayed in red on the PFDs. The target airspeed will follow Vmo.10. A target speed of 250 KIAS will be selected when the ASEL FD mode becomes active.
The FD will fly a HDG/FLC descent to 15,000 feet The FD will transition to ASEL mode and then ALT when levelling off at 15,000 feet. The EDM annunciation will flash for 5 seconds when transitioning between modes.
The FD will remain in EDM mode until the autopilot is disengaged. The only way to cancel EDM mode is to disengage the autopilot. The autopilot can be disengaged at anytime while in EDM mode. Pressing the TCS switches longer than one second will be considered as disengaging the autopilot. When the autopilot is disengaged, the FD modes will be the lateral and vertical modes that were active at the time.
Autothrottle automatic engagement will only occur upon initiation of EDM. Autothrottle can be manually disengaged and re.engaged while in EDM. Autothrottle will not be re.engaged automatically if disengaged.
The EMERGENCY DESCENT CAS message will be recorded by the FDR when posted.
Rev 3, Apr 25, 2005 Flight Crew Operating Manual Volume 2
AUTOPILOT - FLIGHT DIRECTOR EICAS MESSAGES
EMERGENCY DESCENT
Indicates that the AFCS is in
automatic emergency descent mode.
GF0410_097
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
AP PITCH TRIM FAIL
Indicates that autopilot pitch trim is inoperative.
AFCS ENGAGE INVAL
Indicates that fault warning computer detects invalid autopilot engagement.
YD 1.2 FAIL
Indicates that yaw
damper 1 (2) has failed.
AP TRIM IS NU. ND
Indicates that autopilot pitch mistrim monitor detects excessive forces.
AP TRIM IS LWD . RWD
Indicates that autopilot roll mistrim monitor detects excessive forces.
YD OFF
Indicates that fault warning computer detects that no yaw damper is engaged.
GF0410_095
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
AUTOMATIC FLIGHT CONTROL SYSTEM
AUTOPILOT - FLIGHT DIRECTOR EICAS MESSAGES (CONT'D)
Indicates that AFCS (one or both) functions has failed. The AFCS functions include yaw damper,
YD NOT CENTERED
Indicates that the YD linear actuator is not centered while on the ground.
GF0410_096a
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
AUTOMATIC FLIGHT CONTROL SYSTEM EMS CIRCUIT PROTECTION
CB - AFCS SYSTEM
A/T CTLR CB . AFCS SYSTEM AC 1 A/T SERVOS DC 1 AP 1 SERVOS DC 1 AP 2 SERVOS DC 2 GUID PANEL CH 1 BATT GUID PANEL CH 2 DC ESS CCBP 1/3 IN IN IN IN IN IN
IAC 1 CB . AFCS SYSTEM BATT IAC 2 DC ESS IAC 3 BATT YD 1 BATT YD 2 DC ESS YD HEAT 1 DC 1 2/3 IN IN IN IN IN IN
YD HEAT 2 CB . AFCS SYSTEM DC 2 3/3 IN
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