時間：2015-01-22 15:21來源：藍(lán)天飛行翻譯公司 作者：民航翻譯 點(diǎn)擊：次
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To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. (v) Special operational conditions (such as unpaved runways, high altitude aerodromes and drift down requirements). (10) Normal, abnormal and emergency procedures on the aircraft type to be used. (b) Each AOC holder shall have an initial aircraft ground training curriculum for the flight crew applicable to their duties, the type of operations conducted and aircraft flown, including at least the following aircraft systems (if applicable): (1) Airframe. (i) Aircraft (ii) Aircraft dimensions, turning radius, panel layouts, cockpit and cabin configurations. (iii) Other major systems and components or appliances of the aircraft. (iv) Operating limitations. (v) Approved aircraft flight manual. (2) Powerplants. (i) Basic engine description. (ii) Engine thrust ratings. (iii) Engine components such as accessory drives, ignition, oil, fuel control, hydraulic, and bleed air features. (3) Electrical. (i) Sources of aircraft electrical power (such as engine driven generators, APU generator, external power, etc.). (ii) Electrical buses. (iii) Circuit breakers. (iv) Aircraft battery. (v) Standby power systems. (4) Hydraulic. (i) Hydraulic reservoirs, pumps, accumulators; filters, check valves, interconnects and actuators. (ii) Other hydraulically operated components. (5) Fuel. (i) Fuel tanks (location and quantities). (ii) Engine driven pumps. (iii) Boost pumps. (iv) System valves and crossfeeds. (v) Quantity indicators. (vi) Provisions for fuel jettisoning. (6) Pneumatic. (i) Bleed air sources (APU, engine or external ground air). (ii) Means of routing, venting and controlling bleed air via valves, ducts, chambers, and temperature and pressure limiting devices. (7) Air conditioning and pressurisation. (i) Heaters, air conditioning packs, fans, and other environmental control devices. (ii) Pressurisation system components such as outflow and negative pressure relief valves. (iii) Automatic, standby, and manual pressurisation controls and annunciators. (8) Flight controls. (i) Primary controls (yaw, pitch, and roll devices). (ii) Secondary controls (leading/trailing edge devices, flaps, trim, and damping mechanisms). (iii) Means of actuation (direct/indirect or fly by wire). (iv) Redundancy devices. (9) Landing gear and brakes. (i) Landing gear extension and retraction mechanism including the operating sequence of struts, doors, and locking devices, and brake and antiskid systems, if applicable. (ii) Steering (nose or body steering gear). (iii) Bogie arrangements. (iv) Air/ground sensor relays. (v) Visual downlock indicators. (10) Ice and rain protection. (i) Rain removal systems. (ii) Anti-icing and/or deicing system(s) affecting flight controls, engines, pitot static and other probes, fluid outlets, cockpit windows, and aircraft structures. (11) Equipment and furnishings. (i) Exits. (ii) Galleys. (iii) Water and waste systems. (iv) Lavatories. (v) Cargo areas. (vi) Crew member and passenger seats. (vii) Bulkheads. (viii) Seating and/or cargo configurations. (ix) Non-emergency equipment and furnishings. (12) Navigation equipment. (i) Flight directors. (ii) Horizontal situation indicator. (iii) Radio magnetic indicator. (iv) Navigation receivers (GPS, ADF, SDF/LDA, VOR, TACAN, LORAN-C, RNAV, Marker Beacon, DME) as required for the flight operations to be conducted. (v) Inertial systems (INS, IRS). (vi) Functional displays. (vii) Fault indications and comparator systems. (viii) Aircraft transponders. (ix) Radio altimeters. (x) Weather radar. (xi) Cathode ray tube or computer generated displays of aircraft position and navigation information. (13) Auto flight system. (i) Autopilot. (ii) Autothrottles. (iii) Flight director and navigation systems. (iv) Automatic approach tracking. (v) Autoland. (vi) Automatic fuel and performance management systems. (14) Flight instruments. (i) Panel arrangement. (ii) Flight instruments (attitude indicator, directional gyro, magnetic compass, airspeed indicator, vertical speed indicator, altimeters, standby instruments). (iii) Instrument power sources, and instrument sensory sources (e.g., pitot static pressure). (15) Display systems. (i) Weather radar. (ii) Other cathode ray tube (CRT) or computer generated displays (e.g., checklist, vertical navigation or longitudinal navigation displays). (16) Communication equipment. (i) VHF/HF/SAT COM radios. (ii) Audio panels. (iii) Inflight interphone and passenger address systems. (iv) Voice recorder. (v) Air/ground passive communications systems (ACARS). (17) Warning systems. (i) Aural, visual, and tactile warning systems (including the character and degree of urgency related to each signal). (ii) Warning and caution annunciator systems (including airborne collision avoidance, ground proximity and takeoff configuration warning systems). (18) Fire protection. (i) Fire and overheat sensors, loops, modules, or other means of providing visual and/or aural indications of fire or overheat detection. (ii) Procedures for the use of fire handles, automatic extinguishing systems and extinguishing agents. (iii) Power sources necessary to provide protection for fire and overheat conditions in engines, APU, cargo bay/wheel well, cockpit, cabin and lavatories. (19) Oxygen. (i) Passenger, crew, and portable oxygen supply systems. (ii) Sources of oxygen (gaseous or solid). (iii) Flow and distribution networks. (iv) Automatic deployment systems. (v) Regulators, pressure levels and gauges. (vi) Servicing requirements. (20) Lighting. (i) Cockpit, cabin, and external lighting systems. (ii) Power sources. (iii) Switch positions. (iv) Spare light bulb locations. (21) Emergency equipment. (i) Fire and oxygen bottles. (ii) First aid and medical kits. (iii) Liferafts and life preservers. (iv) Crash axes. (v) Emergency exits and lights. (vi) Slides and sliderafts. (vii) Escape straps or handles. (viii) Hatches, ladders and movable stairs. (ix) Survival suits, if applicable to the operation. (22) Auxiliary Power Unit (APU). (i) Electric and bleed air capabilities. (ii) Interfaces with electrical and pneumatic systems. (iii) Inlet doors and exhaust ducts. (iv) Fuel supply. (23) Performance. (c) Each AOC holder shall have an initial aircraft ground training curriculum for the flight crew applicable to their duties, the type of operations conducted and aircraft flown, including at least the following aircraft systems integration items: (1) Use of checklist. (i) Safety checks. (ii) Cockpit preparation (switch position and checklist flows). (iii) Checklist callouts and responses. (iv) Checklist sequence. (2) Flight planning. (i) Preflight and in-flight planning. (ii) Performance limitations (meteorological, mass, and MEL/CDL items). (iii) Required fuel loads. (iv) Weather planning (lower than standard takeoff minimums or alternate requirements). (3) Display systems. (i) Weather radar. (ii) CRT displays (checklists, vertical navigation or longitudinal navigation displays). (4) Navigation and Communications systems. (i) Preflight and operation of applicable receivers. (ii) Onboard navigation systems. (iii) Flight plan information input and retrieval. (5) Autoflight/flight directors. (i) Autopilot. (ii) Autothrust. (iii) Flight director systems, including the appropriate procedures, normal and abnormal indications, and annunciators. (6) Cockpit familiarisation. (i) Activation of aircraft system controls and switches to include normal, abnormal and emergency switches. (ii) Control positions and relevant annunciators, lights, or other caution and warning systems. (d) Each AOC holder shall ensue that initial ground training for flight crew consists of at least the following programmed hours of instruction based on the aircraft to be used, unless a reduction is determined appropriate by the Authority: (1) For pilots and flight engineers— (i) Piston-engined aeroplane—64 hours. (ii) Turbropropeller-powered aeroplane—80 hours. (iii) Turbo-jet aeroplane—120 hours. (iv) Helicopter—64 hours. (v) Powered-lift—80 hours. (vi) Other aircraft—64 hours. (2) For flight navigators— (i) Piston-engined aircraft—16 hours. (ii) Turbropropeller-powered aircraft—32 hours. (iii) Turbojet-aircraft—32 hours. ICAO Annex 6, Part I: 4.2.1.3; 9.3.1; 10.2; 12.4 ICAO Annex 6, Part III, Section II: 7.3.1; 8.2(b)R; 10.3 ICAO Doc 9376, Preparation of an Operations Manual, para. 4.2.2 and attachment B, para. 4.15, 4.16. 14 CFR: 121.419, 121.420 FAA Order 8900.1, Vol. 3, Chapter 19, Section 5 IS: 8.10.1.14 (C) INITIAL AIRCRAFT GROUND TRAINING—CABIN CREW MEMBERS (a) Each AOC holder shall have an initial ground training curriculum for cabin crew members applicable to the type of operations conducted and aircraft flown, including at least the following general subjects, if applicable: (1) Aircraft familiarisation. (i) Aircraft characteristics and description. (ii) Flightdeck configuration. (iii) Cabin configuration. (iv) Galleys. (v) Lavatories. (vi) Stowage areas. (2) Aircraft equipment and furnishings. |
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