Specifications

SECTION VI
MODEL 560 EMERGENCY PROCEDURES
PFD/MFD RED GUN FAILURE
The failure of a red gun in an electronic display indicator results in the following presentations:
PFD - Sky turns from dark blue to a dull dark blue.
Ground turns from brown to green hue
Compass rose turns from white to blue.
1. Use display with caution - MONITOR remaining displays for any red annunciators.
WARNING
FOLLOWING A FAILURE OF A RED GUN IN A DISPLAY UNIT, THE RED
WARNING ANNUNCIATORS WILL NOT BE VISIBLE.
2. Land as soon as practical.
PFD ATTITUDE FAILURE - DUAL (RED ATT FAIL ON PFD ADI)
1. Airplane Attitude - CONTROL by reference to appropriate standby attitude source.
2. Land as soon as practical.
PFD HEADING FAILURE - DUAL (RED HDG FAIL ON PFD HSI)
1. Airplane Heading - CONTROL by reference to appropriate standby magnetic heading source.
2. Land as soon as practical.
AIR DATA COMPUTER FAILURE - DUAL (RED X ON PFD
AIRSPEED/ALTITUDE TAPE)
1. Airplane Airspeed and Altitude - MONITOR by reference to standby flight display.
2. Land as soon as practical.
3. Refer to Abnormal Procedure, CABIN PRESSURIZATION CONTROLLER FAILURE.
DISPLAY GUIDANCE COMPUTER FAILURE - DUAL (RED “X” OR BLANK PFD’S/MFD)
1. Airplane - CONTROL by reference to standby flight display.
2. Land as soon as practical.
AUTOPILOT MALFUNCTION
NOTE
• The autopilot monitors normally detect failures and automatically disengages the
autopilot.
• Maximum altitude loss for autopilot malfunction:
Enroute 400 feet at 37,000 MSL
Climb 0 Feet at 17,000 MSL
ILS Approach 40 Feet. (Maximum deviation below
glideslope during recovery from a failure at
the critical fault point.) Refer to Figure 3-2
for Glideslope Deviation Profile.
1. AP TRIM DISC Switch - PRESS and RELEASE.
I
56OMB-01 Configuration AA 6-21