Fuel Levers (FFOD)................................................................................ OFF
FIRST FLIGHT OF DAY
Levers should be OFF to prevent any premature fuel flow or fuel lever
controlled ignition.
OTHER FLIGHTS
Same as FIRST FLIGHT OF DAY.
Cabin Altitude Controller (FFOD)...............................CHECKED, AUTO
FIRST FLIGHT OF DAY In the AUTO position, the cabin pressure controller indicator should be in the aft position. Place the cabin pressure controller lever in the manual (down) position, depress fully, and turn the cabin altitude control wheel/lever forward and check for freedom of motion over the full range of travel. Release the wheel when the indicator is at the full forward position, place the controller lever in AUTO position, and check that the indicator returns to the full aft position.
OTHER FLIGHTS
Verify the cabin altitude control lever is in the AUTO position and the
cabin pressure controller indicator is in the aft position.
Flaps, Slats (FFOD) ........................................................... WITH GAUGES
FIRST FLIGHT OF DAY
The flaps/slats lever should be full forward and both flap indicator pointers should be at full up. (No more than one needle width split between indicator needles). The TAKEOFF, DISAGREE, AUTO, and LAND lights on the slat position indicator should all be off. Verify that the AUTO-SLAT FAIL light is off.
Note: If the flap/slat handle is in any other position than UP/RETR, contact ground crew for clearance before moving the handle.
OTHER FLIGHTS
Same as FIRST FLIGHT OF DAY.
Communications Panel (FLOW) ......................................CHECKED, SET
FIRST FLIGHT OF DAY
A functional check of the communications panel should be accomplished. The flight deck interphone system should be checked and set for flight.
OTHER FLIGHTS
Same as FIRST FLIGHT OF DAY.
Trim Tabs.............................................................................................ZERO Caution: Do not hang plastic trash bags from rudder or aileron trim knobs. Plastic material can work into the trim mechanism and break it.
FIRST FLIGHT OF DAY
Verify rudder and aileron trim control knobs are at or near zero trim position.
OTHER FLIGHTS
Same as FIRST FLIGHT OF DAY.
PMS (If Installed) (FLOW)...............................................CHECKED, SET
FIRST FLIGHT OF DAY
.
Observe PMS light is out.
.
Push the Plan key. Observe the plan page is displayed.
.
Enter the aircraft gross weight into the scratch pad area and push line select key 1 to enter data.
.
Enter the fuel load into the scratch pad area and push line select key 2 to enter data.
.
Enter the trip distance (shown on the computer flight plan) into the scratch pad area. Push line select key 3 to enter data.
.
Using the slew switch, select Plan-Crz page.
.
Enter planned cruise altitude(s) into scratch pad area. Push line select key 1 to enter data.
.
Enter the flight plan average head/tail wind component into the scratch pad area. Use a Minus sign prefix for headwinds and a Plus sign prefix for tailwinds. Push line select key 2 to enter data.
.
Enter the forecast static air temperature into the scratch pad area. Push line select key 3 to enter data.
.
Push Vert Wpts key and observe the vertical waypoint page is displayed. Vertical waypoints include speed change point (250 KIAS at 10,000 ft. MSL), armed altitudes (on the DFGS), top of climb, start of step climb, top of descent, and bottom of descent.
.
If desired, enter indicated airspeed, wind direction/velocity, and temperature expected at the waypoint. Push line select key 2 to enter data.
.
Press the Climb button.
OTHER FLIGHTS
Same as FIRST FLIGHT OF DAY.
Autobrake Selector (if installed) (FLOW) ............................................ OFF
FIRST FLIGHT OF DAY
With selector in the off position, ABS is inoperative. Manual braking is available. Observe the ARM/DISARM switch is DISARM. (Switch is magnetically held in ARM position).
OTHER FLIGHTS
Same as FIRST FLIGHT OF DAY.
Stabilizer Brake Switch (FLOW) .................................................. CAPPED
FIRST FLIGHT OF DAY The stabilizer brake switch should be guarded in the NORMAL position and safety wired.
OTHER FLIGHTS
Same as FIRST FLIGHT OF DAY.
Parking Brake, Pressure, Temperatures...............OFF / SET, CHECKED
FIRST FLIGHT OF DAY
Observe the OVHT light is out. Verify the brake temperature selector is in ALL. Push the brake temperature test button and observe the brake temp gauge indicates between 425 and 475 degrees centigrade and the OVHT light comes on. Release the brake temperature test button and observe the brake temp gauge indication returns to the pretest valve and the OVHT light goes out.
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