时间:2017-12-16 09:15来源:蓝天飞行翻译公司 作者:民航翻译 点击:次
WORDING DEFINITIONS Warning Definition Caution Definition Note Definition LAND ASAP Definition ABBREVIATIONS Abbreviations UNITS Correspondence Between Units 3-VIEW DRAWING 3-View Drawing LIMITATIONS Preliminary Pages Table of Contents Summary of Highlights GENERAL Introduction Kind of Operations Minimum Flight Crew Maximum Operating Altitude Maneuver Limit Load Factors Icing Conditions Definition WEIGHTS AND LOADING General Establishment of Aircraft Noise Certificate Weight Limitations OW1 - Weight Limitations OW1 - Center of Gravity Envelope OW2 - Weight Limitations OW2 - Center of Gravity Envelope Performance Limitations Loading AIRSPEEDS VMO/MMO VA VFE VLO and VLE/MLE OPERATIONAL PARAMETERS Environmental Envelope Tailwind Runway Slope 09 TOWING AND TAXIING Maneuvers on Ground Towbarless Operations Towbarless Operations 21 AIR COND/PRESS/VENT Cabin Pressurization 22 AUTO FLIGHT SYSTEM Flight Management System General Airworthiness Standards Compliance Navigation Performance Navigation Performance Use of NAV Mode Approaches Flight Guidance System Airworthiness Standards Compliance Autoland Databases with Honeywell ADIRU Autoland AUTOLAND with OEI Minimum Height for Use of the Autopilot CAT II / CAT III Operations 24 ELECTRICAL POWER Electrical 28 FUEL Fuel and Additive Specifications Usable Fuel Fuel Imbalance Fuel Temperature Limits 29 HYDRAULIC Hydraulics Fluid 32 LANDING GEAR Tire Speed 34 NAVIGATION Inertial Reference System (IRS) Reduced Vertical Separation Minimum (RVSM) Mode S - ADS-B Out Enhanced Surveillance 46 INFORMATION SYSTEMS Airline Operation Control Applications 49 AUXILIARY POWER UNIT Auxiliary Power Unit (APU) 70 POWER PLANT Main Engines Engine Parameters Reverse Thrust Oil Reduced Thrust Takeoff Operations in Icing Conditions EMERGENCY PROCEDURES Preliminary Pages Table of Contents GENERAL INTRODUCTION LANDING DISTANCE DETERMINATION IN CASE OF IN-FLIGHT FAILURE 21 AIR COND/PRESS/VENT CAB PR - EXCESS CAB ALT CAB PR - EXCESS RESIDUAL PR 22 AUTO FLIGHT SYSTEM Incorrect FAC Weight due to Dashed CG on FUEL PREDpage 24 ELECTRICAL POWER ELEC - EMER CONFIG (BOTH ENGINE GENERATORS FAILED) 26 FIRE/SMOKE GENERAL ENG 1 (2) FIRE (In Flight) ENG 1 (2) FIRE (On Ground) APU FIRE SMOKE - FWD or AFT CARGO SMOKE SMOKE/FUMES/AVNCS SMOKE REMOVAL OF SMOKE/FUMES 27 FLIGHT CONTROLS F/CTL - L + R ELEV FAULT F/CTL - FLAP LVR NOT ZERO 29 HYDRAULIC HYD - G + B SYS LO PR HYD - B + Y SYS LO PR HYD - G + Y SYS LO PR 32 LANDING GEAR L/G - GEAR NOT DOWNLOCKED LOSS OF BRAKING 34 NAVIGATION NAV - ADR 1+2+3 FAULT 70 POWER PLANT DUAL ENG FAILURE (BOTH ENGINES FLAME OUT) ENG - 1(2) OIL LO PR 90 MISCELLANEOUS STALL RECOVERY EMER DESCENT EMER DESCENT EMERGENCY EVACUATION DITCHING FORCED LANDING Emergency Landing (All Engines Failure) ABNORMAL PROCEDURES Preliminary Pages Table of Contents Summary of Highlights GENERAL INTRODUCTION LANDING DISTANCE DETERMINATION IN CASE OF IN-FLIGHT FAILURE ONE ENGINE INOPERATIVE TO TAKEOFF ENGINE FAILURE BEFORE V1 (REJECTED TAKEOFF) ENGINE FAILURE BETWEEN V1 AND V2 ENGINE FAILURE DURING INITIAL CLIMB OUT LDG APPROACH AND LANDING APPROACH AND LANDING MISSED APPROACH (FROM INTERMEDIATE APPROACH CONFIGURATION) BALKED LANDING 21 AIR COND/PRESS/VENT AIR - PACK 1 + 2 FAULT CAB PR - SYS 1 + 2 FAULT CAB PR - SAFETY VALVE OPEN COND - HOT AIR FAULT VENT - SKIN VALVE FAULT 22 AUTO FLIGHT SYSTEM AUTO FLIGHT SYSTEM AUTO FLT - FCU 1(2) FAULT AUTO FLT - RUD TRV LIM SYS AUTO FLT - FAC 1+2 FAULT AUTO FLT - YAW DAMPER SYS 22-CATII FAILURES OR WARNINGS DURING A CAT II APPROACH WITH OR WITHOUT AUTOMATIC LANDING Multiple Failures or Warnings (CAT II) Altitude Loss with Autopilot Malfunction (CAT II) Failure Leading to Slats/Flaps less than FLAPS 3 (CAT II) Antiskid System and/or Nosewheel Steering Failure(CAT II) Alpha Floor Activation (CAT II) One Engine Failure (CAT II) Red "RA" Flag on two PFDs (CAT II) Amber "CHECK ATT" Flag on two PFDs (CAT II) Red "ATT" Flag on one PFD (CAT II) |