时间：2014-12-02 10:10来源：蓝天飞行翻译公司 作者：公务机翻译 点击：次
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Waste Door (311CR) Main Entrance Door Telescoping Rods ATS Ground Service Compt. Door (311BL) Stabilizers Vertical Stabilizer Tip Cap Horizontal Stabilizer Tip Cap Elevators Actuator Fairing Horizontal Stabilizer Vortex Generator (V/G) (10 ea. side) Windows Windshields Wings Wing Vortex Generators (V/G) (42 ea. Side) Wing/Flap Gap Seals Wingtip Position Light Lens Wing Landing Light Lens Aileron Actuator Fairings Section X - Supplements LIST OF SUPPLEMENTS Supplement 1 - TAWS Escape Procedure TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) SYSTEM ACTIVATION SELF-TEST USER SELECTABLE CALLOUTS RESPONSE TO WARNINGS AND ALERTS TAWS ESCAPE PROCEDURE GROUND PROXIMITY WARNING BELOW GLIDESLOPE WARNING WINDSHEAR ESCAPE PROCEDURE SYSTEM DESCRIPTION TERRAIN PROXIMITY WARNING TERRAIN AWARENESS DISPLAY Terrain Background Display OBSTACLE ALERTING ALERTS AND WARNINGS Supplement 2 - TCAS II TSS-4100 System TCAS II TSS-4100 SYSTEM SELF-TEST TCAS II SYSTEM OPERATION TCAS II SYSTEM OPERATING CHARACTERISTICS RECOMMENDED INFLIGHT PROCEDURES TCAS II SYSTEM RESOLUTION ADVISORY (RA) AND TRAFFIC ADVISORIES (TA) ANNUNCIATIONS TCAS AURAL ADVISORY ANNUNCIATIONS TCAS II SYSTEM DESCRIPTION ALTITUDE THRESHOLDS FOR RVSM STANDARD TCAS II DEFINITIONS TCAS II CONTROLS AND INDICATORS DU TUNE PAGE - ATC1/TCAS Control Page TCAS 1/4 WINDOW TCAS 1/4 window Synoptic Display TCAS II RESOLUTION ADVISORY DISPLAY TCAS MESSAGES Supplement 3 - Brake Kinetic Energy (BKE) And Brake Cooling BRAKE KINETIC ENERGY (BKE) AND BRAKE COOLING BRAKE KINETIC ENERGY (BKE) AND BRAKE COOLING BKE LIMITS BKE DETERMINATION DURING LANDING OR RTO OPERATIONS TAXI BKE BRAKE COOLING FOR QUICK TURN-AROUND AND MULTIPLE BRAKING OPERATIONS FUSE PLUG INTEGRITY ZONES USE OF BKE COOLING CHART Brake Kinetic Energy and Cooling Time Requirements Supplement 4 - Rockwell Collins FMS-6100 Flight Management Systems ROCKWELL COLLINS FMS-6100 FLIGHT MANAGEMENT SYSTEM NAVIGATION APPROVAL STATUS SYSTEM LIMITATIONS SYSTEM FAILURES POWER LOSSES FMS CAUTION MESSAGES SYSTEM DESCRIPTION FLIGHT DIRECTOR/AUTOPILOT INTERFACE AIR DATA COMPUTER INTERFACE FMS-6100 MESSAGES AND ANNUNCIATIONS FMS-6100 MESSAGES ON MAP MFW Supplement 5 - Flaps - 0 Performance FLAPS - 0 PERFORMANCE MAXIMUM ALLOWABLE TAKEOFF WEIGHT MAXIMUM TAKEOFF WEIGHT AS PERMITTED BY TIRE SPEED LIMITATIONS MAXIMUM TAKEOFF WEIGHT AS PERMITTED BY BRAKE ENERGY LIMITATIONS TAKEOFF CHARTS AND TABLES HORIZONTAL STABILIZER TRIM SETTING Example Determination of Overall Longitudinal Center of Gravity Location Flaps - 0° |
