时间:2016-06-08 11:39来源:蓝天飞行翻译公司 作者:通航翻译 点击:次
Flaps Up (Anti-Ice ON) Maximum Takeoff Weight Pounds Permitted by Climb Requirements, Flaps 15° (Anti-Ice OFF) Maximum Takeoff Weight Pounds Permitted by Climb Requirements, Flaps 15° (Anti-Ice ON) 4-37/4-38 Takeoff Field Length - Feet, With 0° Flaps Takeoff Field Length - Feet, With 15° Flaps Single-Engine Takeoff Flight Path - Flaps 0° (First and Second Segment) Single-Engine Takeoff Flight Path Distances - Flaps 0° Single-Engine Takeoff Flight Path Distances - Flaps 0° Anti-Ice OFF Single-Engine Takeoff Flight Path Distances - Flaps 0° Anti-Ice ON Single-Engine Takeoff Flight Path - Flaps 15° (First and Second Segment) Single-Engine Takeoff Flight Path Distances - Flaps 15° Single-Engine Takeoff Flight Path Distances - Flaps 15°Anti-Ice OFF Single-Engine Takeoff Flight Path Distances - Flaps 15° Anti-Ice ON First Segment Takeoff Net Climb Gradient - Percent Flaps Up (Anti-Ice OFF) First Segment Takeoff Net Climb Gradient - Percent Flaps Up (Anti-Ice ON) First Segment Takeoff Net Climb Gradient - Percent 15° Flaps (Anti-Ice OFF) First Segment Takeoff Net Climb Gradient - Percent 15° Flaps (Anti-Ice ON) Second Segment Takeoff Net Climb Gradient - Percent Flaps Up (Anti-Ice OFF) Second Segment Takeoff Net Climb Gradient - Percent Flaps Up (Anti-Ice ON) Second Segment Takeoff Net Climb Gradient - Percent 15° Flaps (Anti-Ice OFF) Second Segment Takeoff Net Climb Gradient - Percent 15° Flaps (Anti-Ice ON) Single-Engine Enroute Net Climb Gradient Flaps Up (Anti-Ice OFF) Single-Engine Enroute Net Climb Gradient Flaps Up (Anti-Ice ON) Procedures for Use of Approach and Landing Performance Tables Maximum Landing Weight - Pounds Permitted by Climb Requirements or Brake Energy Limits Landing Distance - Feet Approach Gross Climb Gradient - Percent Flaps 15° (Anti-ice Systems-Off) Approach Gross Climb Gradient - Percent Flaps 15° (Anti-ice Systems-On) Landing Gross Climb Gradient - Percent Flaps Land (Anti-ice Systems-Off) Landing Gross Climb Gradient - Percent Flaps Land (Anti-ice Systems-On) Reduced Vertical Separation Minimum Universal UNS-1K Flight Management System (With or Without Unilink) Honeywell MK V Enhanced Ground Proximity Warning System Without Windshear Cockpit Speaker Audio Inhibit Switch Honeywell CAS66A Traffic Alert and Collision Avoidance System 1 Safeflight N1 Reminder KLN-900 with GPS Fault Detection and Exclusion (FDE) BFGoodrich WX-1000E (EFIS) Stormscope BFGoodrich Skywatch SKY497 Traffic Advisory System CMS-400 Audio Checklist GNS-XLS with GPS Fault Detection and Exclusion (FDE) EROS Oxygen Mask High Altitude Takeoff and Landing (Above 10,000 Feet Pressure Altitude) Airplanes Operating Under French Configuration Airplanes Operating Under German Configuration SkyLight Avionics CDI-500 Course Deviation Indicator Dual Honeywell MST-67A Enhanced Mode-S Transponders Automatic Pulselite System Collins TWR-850 Weather Radar Garmin GPS 400 Airplanes Certified to Italian Configuration Transponder 2 On Emergency Bus Model A200S Cockpit Voice Recorder Aero-M SATCOM Telephone Airplanes with Second ADF Installed Garmin GNC-420 Cabin/Cockpit Interphone System AirCell Phone System Airplanes Certified to Canadian Configuration Airplane 525-0003 Dispatch Switch Honeywell MK V Enhanced Ground Proximity Warning With Windshear KGS Electronics, Inc 1200W Inverter Avionics Instruments, Inc 2A350-1B1 350W 115V Inverter Mark VIII Enhanced Ground Proximity Warning System, Without Windshear Gravel Runway Modification BFGoodrich SKY899 Skywatch HP TCAS I 525-0473 Dual Davtron M803 Clocks with Independent Cabin Air Temp and Standby Equipment Battery Voltage monitor Universal UNS-1Esp Flight Management System Collins DME-42 Garmin GNS-530 KGS Electronics, Inc 500W/115V Inverter UNS-1L Flight Management System Airplanes Certified for Steep Approaches Goodrich Avionics Terrain Awareness and Warning System Landmark TAWS8000 Airplanes Certified to Dutch Configuration Japanese Registered Airplanes Garmin GTX 330(D) Enhanced Mode S Transponder Citation Performance Calculator (CPCalc) Collins IFIS-5000 Integrated Flight Information System Universal UNS-1L or UNS-1Esp Flight Management System with 802.X Software |