LETOVÁ PŘÍRUČKA NOUZOVÉ POSTUPY ZMĚNA

8. 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. 9. Cabin Pressure Control Set Field Elevation + 500 Feet 10. Windshield Defog As Required 11. Altimeters Set When Ready for Approach 12. 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. 13. Fuel Management Check 14. N1, Landing Distance Confirm 15. Cabin Sign Safety 16. Windshield Anti Ice Low 17. Hydraulic/Nitrogen Pressure Check 18. Engine Sync Off 19. Flaps 10 deg. Before Landing 20. AOA Index Preset 1.3 V/Vs 21. Landing Gear Down 22. Airspeed Slow to 0.4 AOA 23. Recognition Light Off 24. Landing Lights As Required 25. Ignitions On 26. Flaps 30 deg. 27. Approach Airspeed (VREF) Slow to and Maintain 0.57 AOA Note: This will yield a normal approach speed of VREF (0.57 AOA) and normal landing distances. 28. Yaw Damp Off Balked Landing 29. Thrust Takeoff N1 30. Pitch Attitude 10 deg. When Positive Climb Has Been Established 31. Flaps 10 deg. 32. Landing Gear Up 33. Yaw Damp On 34. Airspeed Accelerate to 0.3 AOA 35. Flaps Up 36. Airspeed Accelerate and Maintain 0.2 AOA 37. Landing Lights Ret/off Emergency Procedures 400T(T 1A) 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, attitude displays and heading displays may be unreliable and the autopilot may disconnect. This may be accompanied by amber boxed A/S, ALT, ATT and/or HDG comparator flags. The comparator flags may be followed by red FAIL flags on the airspeed, altitude, attitude and heading displays. 1. Autopilot Disconnect 2. Airspeed Slow to and Maintain 0.2 AOA 3. Thrust As Required 4. Speed Brakes As Required (Slow to 0.25 AOA with speed brakes extended) Note: An AOA of 0.2 (0.25 speed 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, attitude displays and heading displays may be unreliable and the autopilot may disconnect. This may be accompanied by amber boxed A/S, ALT, ATT and/or HDG comparator flags. The comparator flags may be followed by red FAIL flags on the airspeed, altitude, attitude and heading displays. 1. Autopilot Disconnect 2. Airspeed Slow to and Maintain 0.2 AOA 3. Thrust As Required 4. Speed Brakes As Required (Slow to 0.25 AOA with speed brakes extended) Note: An AOA of 0.2 (0.25 speed 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/DeIce 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. Before Landing 19. AOA Index Preset 1.3 V/Vs 20. Landing Gear Down 21. Airspeed Slow to 0.4 AOA 22. Landing Lights As Required 23. Ignitions On 24. Flaps 30 deg. 25. Approach Airspeed (VREF) Slow to and Maintain 0.57 AOA Note: This will yield a normal approach speed of VREF (0.57 AOA) and normal landing distances. 26. Yaw Damp Off Balked Landing 26. Thrust Takeoff N1 27. Pitch Attitude 10 deg. When Positive Climb Has Been Established 29. Flaps 10 deg. 30. Landing Gear Up 31. Yaw Damp On 32. Airspeed Accelerate to 0.3 AOA 33. Flaps 0 deg. 34. Airspeed Accelerate and Maintain 0.2 AOA 35. Landing Lights Ret/off'' Note 1: When a previously specified Temporary AFM revision has been incorporated into the general revisions of the AFM, the general revision may be inserted in the AFM, provided the information contained in the general revision is identical to that specified in the specified Temporary AFM revision. Alternative Methods of Compliance (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Wichita Aircraft Certification Office (ACO), FAA. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Wichita ACO. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita ACO. Special Flight Permits (c) Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. Incorporation by Reference (d) Except as provided by paragraph (a) of this AD, the AFM revision shall be done in accordance with Raytheon Beechjet 400T Temporary Change, P/N 132 590002 5TC3, dated November 12, 2001; Beechjet 400T Temporary Change, P/N 134 590002 1TC3, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128 590001 91TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128 590001 95TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128 590001 107TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128 590001 109TC5, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128 590001 167TC7, dated November 12, 2001; Beechjet 400A Temporary Change, P/N 128 590001 169TC3, dated November 12, 2001; Beechjet 400 Temporary Change, P/N 128 590001 13BTC1, dated November 12, 2001; Beechjet 400 Temporary Change P/N 128 590001 13BTC2, dated November 12, 2001; MU 300 Diamond I Temporary Change, P/N MR 0460TC1, dated November 12, 2001; or MU 300 Diamond IA Temporary Change, P/N MR 0873TC1, dated November 12, 2001; as applicable. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Raytheon Aircraft Company, Department 62, P.O. Box 85, Wichita, Kansas 67201 0085. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid Continent Airport, Wichita, Kansas; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Effective Date (e) This amendment becomes effective on December 11, 2001. Issued in Renton, Washington, on November 26, 2001. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 01 30083 Filed 12 5 01; 8:45 am] BILLING CODE 4910 13 U