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Use an oil can to lubricate the turnbuckle.
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Examine the contents of the box for missing items.
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Additional information provided by the manufacturer should be appropriately integrated into the order shown in paragraphs 5.37 or 5.41.
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If one of the compounds that follow is applied to the fastener, use the torque value for “ lubed fastener.
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Count the number of treads on the tire.
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Calibrated Airspeed means the indicated speed of an aircraft.
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修理受损的封严。
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拆除中间的双臂曲柄装置,
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燃油样品检查发现有微生物污染。
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No legal significance or implications should be attached to the rules and terms in this document.
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When the indicator comes into view, stop the pump.
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Identify the disassembled parts with tags, this method will help you during the subsequent assembly procedures.
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The battery energizes the emergency exit light circuit.
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If you cannot install the rigging pin easily, adjust the length of the rod.
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If this maneuver cannot be performed safely, a warning against attempting it shall be provided.
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Each page must bear the date of the original issue until revised and, when revised, that of the latest revision.
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Recommended fuel conservation information shall be integrated into this section to show the pilot how to minimize fuel usage during operation of the airplane.
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The ventilation system uses differential pressure to pull air out of the airplane. The air moves through overboard vents from the cabin galley and the lavatory areas.
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Gas pressure in the sense tube holds the fault pressure switch in the closed position. The other two pressure switches close when the gas pressure increases because of an overheat or fire condition.
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Each page shall bear a page number and date of issue or revision at the bottom.
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NOTE: During the subsequent test, you get the cracking pressure when the fuel flow from the CROSS FEED port is more than 5 cc/minute.
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The flow of the system shall be presented in patterned shading with a minimum of turns in the lines.
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Be careful when you open or close circuit breakers in the P91 and P92 panels while the panels have power. Electrical shock can cause injuries to personnel.
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For landing distance, both ground roll and the total distance over a 50 foot obstacle shall be included. 。
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The positive pressure relief valves are fail safe devices that bleed fuselage pressure overboard if the aft outflow valve fails closed.
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Apply grease to the V-clamp before you install it.
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To calibrate the test set, refer to the manufacturer's instructions.
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Communication system includes voice and C-W communicating components, PA system, and intercom system.
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Make sure that the shelf life is not expired.
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Make sure that the diameter of the hole is less than the specified value.
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In two digits of Section Number in the Continuing Airworthiness Program lnspection number, the first digit is determined by GAMA Specification No. 2 Numbering System, and the second digit is determined sequentially by the manufacturer.。
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INSPECTION COMPLIANCE sets forth instructions regarding “when” an inspection is required and whether it is repetitive. Also state if additional repetitive inspections are required based on initial inspection results.。
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In addition to understanding FAA Advisory Circulars AC 91-60 and AC 91-56, familiarity with GAMA Specification No.2, Manufacturers Maintenance Data and Air Transport Association of America Specification No.100, Specification for Manufacturers Technical Data, will aid in the preparation of a CAP for a specific airplane.。
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The effects of corrosion have not been considered in the rationale in selecting inspection times or in the effects on the fatigue stresses. It is very difficult to determine the effects of corrosion but, as the reports from the CAP inspections are received, the inspection times will be adjusted for any severe problems.。
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A review of test results applicable to the design was made. The loading conditions together with the resulting margins of safety were evaluated. The resulting data were used to determine if the component should be considered for incorporation into the CAP.
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There should be a reference in this Section to the Federal Aviation Regulation (FAR's 43 and 91 or other applicable regulations) as to who may perform the required and manufacturer recommended inspections.
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The effect of anti - icing or de - icing systems on the approval of the airplane for operating in known icing conditions should be clearly defined in the limitations section of the Supplements.
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供压时,人员和设备要远离所有操纵面和起落架。
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扰流板和副翼类似,它们也辅助并提供飞机滚转操纵。
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在紧急情况下,可使用 F - 43 燃油替代 F - 34 和 F - 40 燃油。
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针对飞机类别适合的机动飞行,应提供以下信息:(a)获准的机动飞行以及合适的进入速度的相关信息;(b)未获授权的机动飞行的相关信息;(c)已获准或未获准或不适合进行螺旋演练的相关信息。
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推荐的燃油节约信息应整合到本节中,以便向飞行员展示如何在飞行过程中尽量减少燃油的使用。
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检查单也可能包含飞行员可能经常使用的与飞机操作相关的补充信息,如性能数据、可选设备操作等。
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当章节或子系统单元编号后面的主题单元编号(28 - 20 - 00)为零时,该信息适用于系统内的子系统。
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The Airworthiness Section must set forth each mandatory replacement time, structural inspection interval, and related structural inspection procedure required for type certification.
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The equipment included in the basic maintenance manual may be only that which is normally included and installed in quantity. Data for “Special Order” or other than standard options may be in separate manuals or as separate data furnished with the individual aircraft.
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On reciprocating (piston) engine powered airplanes, the mixture control provides a mechanical linkage with the mixture control valve of the carburetor, or the fuel control unit of fuel injection engines, to control the size of the fuel feed aperture, and thus, the air/fuel mixture.
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Devices used to stabilize the aircraft while on the ground and prevent damage by ground contact. Includes items such as shock strut, skid blocks, wheels, etc.
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The waste disposal system is that portion of the system which is used for disposal of water and waste. It includes items such as wash basins, water closets, flushing systems, etc.
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To get correct clearance, add special shims as necessary.
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The CAP will address primary and secondary airframe components, and primary and secondary systems to accomplish the stated objective of continued airworthiness.
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If desired, the manufacturer may include more than one airplane model in the Maintenance Manual.
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Each approved word in the dictionary has a specified approved meaning which can be more restricted than its meaning in standard English.
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If necessary, initiate CA (compliance action) per Volume 14, Chapter 1, Section 2 to identify the root cause that led to any deviations from rules, standards, or procedures; analyze corrective action to resolve them; and schedule follow-up to validate the repair
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The equipment included in the basic maintenance manual may be only that which is normally included and installed in quantity. Data for “Special Order” or other than standard options may be in separate manuals or as seperate data furnished with the individual aircraft.
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“警告”、“警戒”和“注意”之类的插入语应简短明了,并用干强调重要的指示。
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考虑到发动机的冷却、性能和经济性,应将适用于所有地面运行和飞行运行的建议节油程序包含入本节中。
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应将推荐的节油信息整合到本节中, 以向飞行员展示如何在飞机运行期间最大程度地 减少燃油消耗。
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描述飞机燃油系统时,应说明和阐述加热器如何对燃油加温(如适用)。
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来自于前后腔、滑油-燃油换热器、可调放气活门、可调静子叶片的油液也会通过这些 放泄管排到外面。
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在航空器运行中的“循环”指的是从一次起飞到着陆。“循环”在航空器维修中很重 要因为它用来追踪寿命件的使用情况来决定什么时候对其检查或更换。
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在接地三角系统中,会建立一个接地相作为系统的基准点。
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针对整架飞机的补液、定期和非定期维护的说明。该信息应简明扼要,并可用表格或 图表形式呈现,标题为“维护”。
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真实空速表示飞行器飞行时相对于空气运动的速度。
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动力装置限制包括对燃油等级或规格以及获批的燃油添加剂的限制。
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那些能在地面或水上支撑和控制飞机飞行方向,并能在飞行中收回和储存起落架的装 置和部件,包括刹车、机轮、浮筒、门、减震支柱、支腿、连杆、位置指示灯和警告系统。
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这部分包括发动机架、减震器、支撑杆、安装螺栓等。
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如适用,本章可以参考随飞机提供的厂商数据来代替某些章节。
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In general, it is desired that the following chapter arrangements and breakdown be followed uniformly and to the maximum extent practicable in all manuals.
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A position transmitter is located below the PCUs.
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These two groups explored the existing controlled languages and researched texts in several maintenance manuals. The results confirmed that a simplified language was necessary.
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The Boeing 747 marked the beginning of a new era in air transport.
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Each manual shall contain an Introduction which shall include a brief statement explaining the organization, content and method of using the manual in addition to lists, or references to locations of lists, of vendor technical publications.
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相关组件和部件包含:乙醇泵、阀门、存储箱、螺旋桨防冰系统、机翼加热器、水管加热器、空速管加热器、进气道加热器、风挡雨刮,以及风挡防冰中的电防冰和热防冰装置。不包括基本的风挡面板。
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涡轮发动机包括控制流经发动机空气流量的压气机引气系统、空气冷却系统、用于发动机防冰的热空气系统和发动机启动系统。
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涡桨发动机控制装置包括调节器或等效装置的连杆装置和控制装置,以及从调节器或等效装置到螺旋桨调速器、燃油控制组件的连杆装置和控制装置,或其他受控组件。
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Water displacing corrosion inhibiting compound has been applied during construction on certain airplanes in the locations shown in this figure. Periodic reapplication in these, and other locations, is required to maintain effectiveness of this protection.
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If the flap extension does not agree with the position of the flap control lever, do the rigging procedure again.
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Procedures for a parked aircraft are included in AMM such as periodic engine running, control or drainage of fluid systems, static grounding, etc.
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Figure 2 is an example of a repair procedure for a damaged web.
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Make sure that the guards are installed on the switches.
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在动力装置表面或其周围安装有阻热隔板或封严层。
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Recommendations for ATC holding operation in icing conditions for up to 45 minutes shall provided.
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NOTE: The Preface has been omitted in the sample CAP in Section Ⅲ and the necessary information has been included in the Objectives.
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When there is an ""emergency"" situation, it is usually a failure that requires an immediate and quick response, such as an entire engine failure, fire or smoke, or perhaps a rapid drop in cabin pressure.
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If you see discoloration, replace the part.
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If you find a crack, do the applicable repair procedure.
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Remove the tag.
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Disconnect the cable from the rear side of the instrument.
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These parts can easily bend, break or become incorrectly aligned.
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The navigation lights change from dim to bright.
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In this configuration, the hydraulic pressure bypasses the valve.
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Move the lever rearward.
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If the radio signal is not clear, adjust the frequency.
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Corrosion can have many causes.
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The user of the schematic diagram is the pilot.
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Deactivation/Reactivation procedures for circuits, systems, units, etc., shall be included.
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Documents must be readily revisable.
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Install the manifold.
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The control unit is installed aft of the cockpit.
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