时间：2015-01-22 15:18来源：蓝天飞行翻译公司 作者：民航翻译 点击：次
|
To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. 14 CFR: 145.57; 145.105 JAR: 145.85 Annex 6 Part 1 Chapter 8: 8.7.2.2, 8.7.2.3 6.2.1.12 RATINGS OF THE AMO (a) The following ratings are issued under this Subpart— (1) Airframe ratings. (i) Class 1: Composite construction of small aircraft. (ii) Class 2: Composite construction of large aircraft. (iii) Class 3: All-metal construction of small aircraft. (iv) Class 4: All-metal construction of large aircraft. (2) Powerplant ratings. (i) Class 1: Piston engines of 400 horsepower or less. (ii) Class 2: Piston engines of more than 400 horsepower. (iii) Class 3: Turbine engines. (3) Propeller ratings. (i) Class 1: Fixed-pitch and ground-adjustable propellers of wood, metal orcomposite construction. (ii) Class 2: Other propellers, by make. (4) Avionics/radio ratings. (i) Class 1: Communication equipment: Radio transmitting equipment or receiving equipment, or both, used in aircraft to send or receive communications, regardless of carrier frequency or type of modulation used; including auxiliary and related aircraft interphone systems, amplifier systems, electrical or electronic inter-crew signaling devices, and similar equipment; but not including equipment used for navigation of the aircraft or as an aid to navigation, equipment for measuring altitude or terrain clearance, other measuring equipment operated on radio or radar principles, or mechanical, electrical, gyroscopic, or electronic instruments that are a part of communications radio equipment. (ii) Class 2: Navigational equipment: A radio system used in aircraft for en-route, approach navigation, to include the flight director system, except equipment operated on radar or pulsed radio frequency principles, but not including equipment for measuring altitude or terrain clearance or other distance measuring equipment operated on pulsed radio frequency principles. (iii) Class 3: Pulsed equipment: Any aircraft electronic system operated on pulsed radio frequency principles. (5) Instrument ratings. (i) Class 1: Mechanical: Any diaphragm, bourdon tube, aneroid, optical, or mechanically driven centrifugal instrument that is used on aircraft or to operate aircraft, including tachometers, airspeed indicators, pressure gauges, drift sights, magnetic compasses, altimeters, or similar mechanical instruments. (ii) Class 2: Electrical: Any self-synchronous and electrical indicating instruments and systems, including remote indicating instruments, cylinder head temperature gauges, or similar electrical instruments. (iii) Class 3: Gyroscopic: Any instrument or system using gyroscopic principles and motivated by air pressure or electrical energy, including automatic pilot control units, turn and bank indicators, directional gyros, and their parts, and flux gate and gyrosyn compasses. (iv) Class 4: Electronic: Any instruments whose operation depends on electron tubes, transistors, electronic displays, or similar devices including capacitance type quantity gauges, system amplifiers, and engine analysers. (6) Accessory ratings. (i) Class 1: Mechanical. The accessories that depend on friction, hydraulics, mechanical linkage, or pneumatic pressure for operation, including aircraft brakes, mechanically driven pumps, carburetors, aircraft wheel assemblies, shock absorber struts and hydraulic servo units. (ii) Class 2: Electrical. The accessories that depend on electrical energy for operation, and generators, including starters, voltage regulators, electric motors, electrically driven fuel pumps, magnetos, or similar electrical accessories (iii) Class 3: Electronic. The accessories that depend on the use of an electron tube transistors, or similar device, including supercharger, temperature, air conditioning controls, or similar electronic controls. 14 CFR: 145.59 EASA 145: Appendix II 6.2.1.13 AMO LIMITED RATINGS (a) Whenever the Authority finds it appropriate, it may issue a limited rating to an AMO that maintains or alters only a particular type of airframe, powerplant, propeller, radio, instrument, or accessory, or parts thereof, or performs only specialised maintenance requiring equipment and skills not ordinarily found in an AMO. Such a rating may be limited to a specific model aircraft, engine, or constituent part, or to any number of parts made by a particular manufacturer. (b) Limited ratings are issued for— (1) Airframes of a particular make and model; (2) Powerplants of a particular make and model; (3) Propellers of a particular make and model; (4) Radio equipment of a particular make and model; (5) Instruments of a particular make and model; (6) Accessories of a particular make and model; (7) Landing gear components; (8) Floats, by make; (9) Nondestructive inspection, testing, and processing; (10) Emergency equipment; (11) Rotor blades, by make and model; (12) Aircraft fabric work; and (13) Any other purpose for which the Authority finds the applicant’s request appropriate. (c) Specialised service ratings. A specialised service rating may be issued to a maintenance organisation to perform specific maintenance or processes. The operating specifications of the approved maintenance organisation must identify the specification used in performing that specialised service. The specification may be— (1) A civil or military specification that is currently used by industry and approved by the Authority; or (2) A specification developed by the approved maintenance organisation and approved by the Authority. 14 CFR: 145.61 EASA 145: Appendix II 6.2.1.14 QUALITY SYSTEM (a) The AMO shall establish a quality system and designate a quality manager to monitor compliance with, and adequacy of, procedures required to ensure safe maintenance practices and airworthy aircraft. Compliance monitoring shall include a feedback system to the accountable manager to ensure corrective action as necessary. (b) The quality system, and the quality manager, shall be acceptable to the Authority. (c) Each AMO shall ensure that the quality system includes a quality assurance programme that contains procedures designed to monitor compliance with required aircraft and aircraft component standards and adequacy of the procedures to ensure that such procedures invoke good maintenance practices and airworthy aircraft and aircraft components. (d) The quality assurance system shall include a procedure to initially qualify and periodically perform audits on persons performing work on behalf of the AMO. (e) The quality system shall include a feedback system to the designated management person or group of persons directly responsible for the quality system and ultimately to the accountable manager that ensures, as necessary, proper and timely corrective action is taken in response to reports resulting from the independent audits. (f) The AMO’s quality system shall be sufficient to review all maintenance procedures, as described in the Maintenance Control Manual and the Maintenance Procedures Manual, in accordance with an approved programme once a year. (g) The AMO’s quality system shall indicate when audits are due, when completed, and establish a system of audit reports, which can be seen by visiting Authority staff on request. The audit system shall clearly establish a means by which audit reports containing observations about non-compliance or poor standards are communicated to the accountable manager. (h) If the AMO is a small organisation, the independent audit part of the quality system may be contracted to another organisation approved under this part or a person with appropriate technical knowledge and proven satisfactory audit experience such as ISO 9000 qualification. (i) Where the AMO is part of an AOC under Part 9, the AOC holder’s quality management system may be combined with the requirements of an AMO and submitted for acceptance to the Authority. (j) Each AMO shall describe the quality system in relevant documentation as outlined in IS: 6.2.1.12. Note: Where the AMO is part of an AOC under Part 9, see IS: 9.2.2.3 for examples of a combined quality system. ICAO Annex 6: Part 1, 8.7.3.2 FAA AC 145-9 JAR: 145.65 6.2.1.15 LOCATION OF THE AMO (a) Principal place of business. An applicant for, or holder of, a certificated AMO under this Part shall establish and maintain a principal place of business office that is physically located at the address shown on its certificate. (b) Additional fixed locations. An AMO may have additional fixed locations without certificating each facility as a stand-alone AMO, which may be approved by the Authority provided that – (1) All of the facilities are localised and within a defined area, and (2) All locations operate under the approval of the AMO certificate and operations specifications. (c) Foreign locations of AMOs. An AMO approved by the Authority may be located in a country outside [STATE] and is subject to all the applicable requirements of this Part. FAA Order 8900.1, Vol. 2, Chapter 11, Section 1 6.3 HOUSING, FACILITIES, EQUIPMENT, MATERIALS AND DATA 6.3.1.1 GENERAL (a) A certificated approved maintenance organisation must provide, housing, facilities, equipment, materials, and data in quantity and quality that meet the standards required for the issuance of the certificate and ratings that the approved maintenance organisation holds. 14 CFR: 145.101 6.3.1.2 HOUSING AND FACILITY REQUIREMENTS (a) Housing for the facilities, equipment, materials, and personnel shall be provided appropriate for all planned work ensuring, in particular, protection from weather. (b) All work environments shall be appropriate for the task carried out and shall not impair the effectiveness of personnel. |
