時(shí)間：2015-01-22 15:18來(lái)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. (3) Lighting should be such as to insure each inspection and maintenance task can be carried out. (4) Noise levels should not be permitted to rise to the point of distracting personnel from carrying out inspection tasks. Where it is impractical to control the noise source, such personnel should be provided with the necessary personal equipment to stop excessive noise causing distraction during inspection tasks. (e) Where a particular maintenance task requires the application of specific environmental conditions different to the foregoing, then such conditions shall be observed. (Specific conditions are identified in the approved maintenance instructions.) (f) Where the working environment for line maintenance deteriorates to an unacceptable level with respect to temperature, moisture, hail, ice, snow, wind, light, dust/other airborne contamination; the particular maintenance or inspection tasks shall be suspended until satisfactory conditions are re-established. (g) For both base and line maintenance where dust or other airborne contamination results in visible surface contamination, all susceptible systems shall be sealed until acceptable conditions are re-established. (h) Storage facilities for serviceable aircraft components shall be clean, well ventilated and maintained at an even dry temperature to minimise the effects of condensation. (i) Manufacturer and standards recommendations shall be followed for specific aircraft components. (j) Storage racks shall provide sufficient support for large aircraft components such that the component is not distorted. (k) All aircraft components, wherever practicable, shall remain packaged in protective material to minimise damage and corrosion during storage. 14 CFR 145.103 FAA Order 8900.1, Vol. 2, Chapter 11, Section 5 and Vol., 6, Chapter 9, Section 8 IS: 6.3.1.3 EQUIPMENT, TOOLS, AND MATERIAL (a) All applicable tools, equipment, and test equipment used for product acceptance and/or for making a finding of airworthiness shall be traceable to the [STATE] National Standards. (b) Except as provided in paragraph (a), in the case of foreign manufactured tools, equipment, and test equipment, the standard provided by the county of manufacture may be used if approved by the Authority. (c) Where the manufacturer specifies a particular tool, equipment, or test equipment then that tool, equipment, or test equipment shall be used unless the manufacturer has identified the use of an equivalent. (d) Except as provided in paragraph (c), tools, equipment, or test equipment other than that recommended by the manufacturer will be acceptable based on at least the following: (1) The AMO shall have a procedure in the Maintenance Procedures Manual if it intends to use equivalent tools, equipment, or test equipment other than that recommended by the manufacturer. (2) The AMO shall have a programme to include: (i) A description of the procedures used to establish the competence of personnel that make the determination of equivalency to tools, equipment, or test equipment. (ii) Conducting and documenting the comparison made between the specification of the tool, equipment or test equipment recommended by the manufacturer and the equivalent tool, equipment, or test equipment proposed. (iii) Ensuring that the limitations, parameters, and reliability of the proposed tool, equipment, or test equipment are equivalent to the manufacturer's recommended tools, equipment, or test equipment. (iv) Ensuring that the equivalent tool, equipment, or test equipment is capable of performing the appropriate maintenance function, all normal tests, or calibrations, and checking all parameters of the aircraft or aeronautical product undergoing maintenance or calibration. (e) The AMO shall have full control of the equivalent tool, equipment, or test equipment (i.e., ownership, lease, etc.) (f) An AMO approved for base maintenance shall have sufficient aircraft access equipment and inspection platforms/docking such that the aircraft may be properly inspected. (g) The AMO shall have a procedure to inspect/service and, where appropriate, calibrate tools, equipment, and test equipment on a regular basis and indicate to users that an item is within any inspection or service or calibration time limit. (h) The AMO shall have a procedure if it uses a standard (primary, secondary or transfer standards) for performing calibration, to ensure that standard cannot be used to perform maintenance. (i) A clear system of labeling all tooling, equipment and test equipment shall be used to give information on when the next inspection or service or calibration is due, and give status information if the item is unserviceable for any other reason where it may not be obvious. (j) A clear system of labeling all tooling, equipment, and test equipment shall be used to give information on when such tooling, equipment, and test equipment is not used for product acceptance and/or for making a finding of airworthiness. (k) A register shall be maintained for all calibrated tools, equipment and test equipment together with a record of calibrations and standards used. (l) Inspection, service, or calibration on a regular basis shall be in accordance with the equipment manufacturers' instructions except where the AMO can show by results that a different time period is appropriate in a particular case and is acceptable to the Authority. 14 CFR 145.109 FAA Order 8900.1, Vol. 2, Chapter 11, Section 5 IS: 6.4.1.1 PERSONNEL REQUIREMENTS (a) The AMO functions shall be subdivided under individual managers or combined in any number of ways, dependent upon the size of the AMO. (b) The AMO shall have, dependent upon the extent of approval, the following: (1) A base maintenance manager. (2) A line maintenance manager. (3) A workshop manager and a quality manager, all of whom should report to the accountable manager. Note: In small AMOs, one or more of the above positions may be combined subject to approval by the Authority. (c) The Accountable Manager shall be responsible for ensuring that all necessary resources are available to accomplish maintenance required to support the AMO's approval. (d) The Base Maintenance Manager shall be responsible for: (1) Ensuring that all maintenance required to be carried out in the hangar, plus any defect rectification carried out during base maintenance, is carried out to specified design and quality standards; and (2) Any corrective action resulting from quality compliance monitoring. (e) The Line Maintenance Manager shall be responsible for: (1) Ensuring that all maintenance required to be carried out on the line, including line defect rectification, is performed to the required standards; and (2) Any corrective action resulting from quality compliance monitoring. (f) The Workshop Manager shall be responsible for: (1) Ensuring that all work on aircraft components is performed to required standards; and (2) Any corrective action resulting from quality compliance monitoring. (g) The Quality Manager shall be responsible for: (1) Monitoring the AMO's compliance with Part 6; and (2) Requesting remedial action as necessary by the base maintenance manager/line maintenance manager/workshop manager or the accountable manager, as appropriate. (h) The AMO may adopt any title for managerial positions, but shall identify to the Authority the titles and persons chosen to carry out these functions. (i) Where an AMO chooses to appoint managers for all or any combination of the identified functions because of the size of the undertaking, these managers shall report ultimately through either the Base Maintenance Manager or Line Maintenance Manager or Workshop Manager or Quality Manager, as appropriate, to the accountable manager. (j) The managers specified in this subsection shall be identified and their credentials submitted to the Authority. To be accepted, such managers shall have relevant knowledge and satisfactory experience related to aircraft/aircraft component maintenance as appropriate in accordance with these regulations. Note: Certifying staff may report to any of the managers specified depending upon which type of control the AMO uses (for example, licensed engineers, independent inspection/dual function supervisors, etc.) so long as the quality compliance monitoring staff remain independent. (k) The AMO shall have a production man-hours plan showing that it has sufficient man-hours for the intended work. (l) If an AMO is approved for base maintenance, the plan shall relate to the aircraft hangar visit plan. (m) Man-hour plans shall regularly be updated. Note: Work performed on any aircraft registered outside [STATE] should be taken into account where it impacts upon the production man-hours plan. (n) Quality monitoring compliance function man-hours shall be sufficient to meet the requirement of 6.2.1.12(b). (o) Planners, mechanics, supervisors and certifying staff shall be assessed for competence by "on the job" evaluation or by examination relevant to their particular role within the AMO before unsupervised work is permitted. (p) To assist in the assessment of competence, job descriptions are recommended for each position. The assessment shall establish that: (1) Planners are able to interpret maintenance requirements into maintenance tasks, and have an appreciation that they have no authority to deviate from the aircraft maintenance programme. (2) Mechanics are able to carry out maintenance tasks to any standard specified in the maintenance instructions and will notify supervisors of mistakes requiring rectification to re-establish required maintenance standards. (3) Supervisors are able to ensure that all required maintenance tasks are carried out, and where not done or where it is evident that a particular maintenance task cannot be carried out to the maintenance instructions, then such problems will be reported to and agreed by the quality organisation. |
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