Document ID: chunk:federal_register_of_legislation:F2006B03925:body:0:p4
Version: federal_register_of_legislation:F2006B03925
Segment Type: other
Provision Reference: 
Character Range: 9390–12702

brakes extended) will yield an airspeed of about 210 knots. Use pitch attitude as primary reference. Make small changes in pitch attitude and wait for AOA to stabilize.

                When Ready for Descent

5.         Seat Belts/Shoulder Harnesses - Fastened
6.         Cabin Sign - AS Required
7.         Anti/De-Ice Systems - As Required

Caution

                If icing conditions are anticipated during the descent and approach, turn ice protection systems ON as early as possible prior to penetrating clouds.
                Maintain wing anti/deice operation light ON (approximately 70% N2) during descent to assure proper wing anti-ice operation.

8.         Cabin Pressure Control - Set Field Elevation + 500 Feet
9.         Windshield Defog - As Required
10.     Altimeters - Set

                When Ready for Approach

                  11.     Airspeed - Slow to and Maintain 0.3 AOA

                Note: Maintain 0.3 AOA throughout the configuration change to Flaps 10 deg., Gear Down. This will yield an airspeed of about 180 knots.

                  12.     Fuel Management - Check
                  13.     N1, Landing Distance - Confirm
                  14.     Cabin Sign - Safety
15.     Windshield Anti-Ice - Low
                  16.     Hydraulic/Nitrogen Pressure - Check
17.     Engine Sync - Off
                  18.     Flaps - 10 deg.

                    19.              GPWS TAC and FLP ORIDE - Off

                Before Landing

                  20.     AOA Index - Preset 1.3 V/Vs
                  21.     Landing Gear - Down
                  22.     Airspeed - Slow to 0.4 AOA
23.     Landing Lights - As Required
                  24.     Ignitions - On
25.     Flaps - Set for Landing
                  26.     Approach Airspeed (VREF) - Slow to and Maintain 0.57 AOA

                Note: This will yield an approach speed of VREF (0.57 AOA) and normal landing distances.

                  27.     Yaw Damp - Off

Caution

                If icing conditions are encountered during flight, the maximum landing flap is 10 deg. unless one of the following are met.

                The icing conditions are encountered for less than 10 minutes, and the RAM Air Temperature (RAT) during the encounter was warmer than -8 deg.C.

                A RAT of +10 deg.C, or warmer, is observed during the descent, approach or landing.

                If either of the above two conditions are met, Flaps 30 deg. may be used for landing.

                Balked Landing

                  28.     Thrust - Takeoff N1
29.     Pitch Attitude - 10 deg.

                When Positive Climb Has Been Established

                  30.     Flaps - 10 deg.
31.     Landing Gear - Up
                  32.     Yaw Damp - On
33.     Airspeed - Accelerate to 0.3 AOA
34.     Flaps - Up
35.     Airspeed - Accelerate and Maintain 0.2 AOA

                    36.              Landing Lights - Ret/off

Emergency Procedures 400T(TX) Loss of Airspeed
                Note: If the pilot's, or copilot's and standby, or all three airspeed(s) are noted to be decreasing toward zero, refer to the standby attitude indicator, standby altimeter, standby heading and the AOA indicator for aircraft control and land at the nearest suitable airport. The pilot's and copilots altimeter's,