Specifications

SECTION IV
OPERATING INFORMATION
MODEL 560
BEFORE TAXI (Continued)
2. Flight Controls/Speed Brakes/Flaps - CHECKED/SET.
NOTE
Verify flaps trim interconnect operation is between 15 and 25 degrees.
3. Pitch Trim - CHECK/SET for Takeoff.
a. LH - Push both trim switches down and verify elevator trim movement, and push AP TRIM
DISC, verify no elevator trim movement. Release AP TRIM DISC.
b. LH - Push both trim switches up, and verify elevator trim movement, and push AP TRIM
DISC, verify no elevator trim movement. Release AP TRIM DISC.
c. LH - Push left half of trim switch up and down, verify no elevator trim movement.
d. LH - Push right half of trim switch up and down, verify no elevator trim movement.
e. Verify manual trim wheel can move elevator trim.
f. RH - Push both trim switches down, and verify elevator trim movement, and push AP TRIM
DISC, verify no elevator trim movement. Release AP TRIM DISC.
g. RH - Push both trim switches up, and verify elevator trim movement, and push AP TRIM
DISC, verify no elevator trim movement. Release AP TRIM DISC.
h. RH - Push left half of trim switch up and down, verify no elevator trim movement.
i. RH - Push right half of trim switch up and down, verify no elevator trim movement.
4. Anti-Ice/Deice - CHECKED/SET AS REQUIRED.
NOTE
Proper tail deice system operation is indicated by the following:
AUTO - TL DEICE PRESS L advisory light, on 6 seconds.
TL DEICE PRESS L and R advisory lights, both off 6 seconds.
TL DEICE PRESS R advisory light, on 6 seconds.
TL DEICE PRESS L and R advisory lights, both off remainder of 3 minute
cycle.
MANUAL - TL DEICE PRESS L and R advisory lights, both on when switch is in
MANUAL.
TL DEICE PRESS L and R advisory lights, both off when switch is
released.
5. TEMPERATURE CONTROL - AS REQUIRED (AUTO above FL310).
6. PRESSURIZATION Controller - SET Landing Field Elevation.
7. ATIS/Clearance/FMS - AS REQUIRED.
8. Avionics/Flight Instruments - SET.
a. EFIS TEST switch - push, verify:
(1) Pilot and copilot radio altimeters display 50 feet.
(2) Red X displayed in barometric altimeters, airspeed, and CDI.
(3) All digits replaced with dashes (except radio altimeter).
(4) All error messages are displayed.
(5) Test message is displayed in upper left corner of PFD.
(6) Command cues (if selected) bias from view.
(Continued Next Page)
I 4-10 Configuration AA 56OMB-01