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The Boeing 747 marked the beginning of a new era in air transport.

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A position transmitter is located below the PCUs.

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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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Accelerate Stop Distance is the distance required to accelerate an airplane to a specified Speed and, assuming failure of an engine at the instant that speed is attained, to bring the Airplane to a stop.

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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到调节器或等效装置的连杆装置和控制装置，以及从调节器 或等效装置到螺旋浆调速器、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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For purposes of this specification, ""airplane"" refers to the airframe and related Components specified in the Type Certificate or made available as options by the airplane Manufacturer.

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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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Examine the seal for defects.

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Hold the cylinder tightly.

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Make sure that the latch is fully engaged.

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Install the valve and the correct gasket.

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Database synchronization is in progress.

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Do not loosen the nut to align it.

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Bleed the system before you disconnect the components.

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Remove the sealant with a blunt scraper.

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The computer controls compressor airflows to prevent stall.

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You can stop the starting sequence at any time.

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Remove and discard the cotter pins and the nuts.

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Do an inspection of the adjacent area.

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This figure shows the structure of the system.

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We recommended that you do not do this procedure in the hangar.

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Use the manual control in an emergency.

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Make a careful estimate of the damaged area.

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The precision of this adjustment is important.

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If the values are different, do this test.

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Remove the valve located adjacent to pump.

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Loosen the nut one full turn.

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This shows that you can install an alternative relay.

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Do not disassemble or repair igniter plugs.

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The flow of fluid through the valve must be continuous.

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You can gain access to the machinery by removing the cover.

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Attach the panel to the structure with the bolts.

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If the circuit breaker opens, de-energize the circuit.

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Do not exceed this speed with landing gear extended.

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All personnel must fully know the safety precautions.

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Polish the window pane with a soft cloth.

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To remove the cover assembly (9), first remove the four screws (10).

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Make sure that there are no leaks.

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Cracks can have a maximum length of five inches.

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Set the rotary switch to INPUT.

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CAUTION: WHEN YOU REMOVE THE PROBES, DO NOT LET THEM TOUCH EACH OTHER.

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Connect the disconnected wires.

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Install the seat before you install the cushion.

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The dimensions are given in the table.

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Make sure that the landing-light cutoff-switch power connection is safe.

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Examine the removed parts for damage.

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The color of the indicator changes to green.

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One generator can supply power for all the systems.

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Adhere to the safety instructions.

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Lift the cylinder above its installed position.

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Fuel goes through the atomizers into the combustion chamber.

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Attach the cable to the structure with wire.

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Prevent movement of the components when you repair the unit.

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Write noun clusters of no more than three words.

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Use the specified tool to seal the opening.

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Vertical lists make long complex sentences much easier to understand.

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It is mandatory to do this procedure in this service bulletin.

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Remove the four screws that attach the flange to the cover.

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If the probes touch each other, they can become demagnetized.

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Future reference to the unit may be by abbreviation.

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Those instructions are necessary to carry out the scheduled servicing.

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Vertical pages rather than horizontal are preferred for all types of publication.

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This specification will meet the applicable government regulatory requirements.

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Torque the bolts to the force between 0.56 and 0.60 m.daN.

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Turn the clamps to free the pipes.

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Supply hydraulic power to system B with the pump.

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Operate the elevator in the full travel 6 times.

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Make sure that all the galley compartments are empty.

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More than one person is necessary for this procedure.

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Put the aircraft back to its initial configuration.

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Be careful when you use consumable materials.

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Clean the area from unwanted sealant.

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Do not point the compressed air outlet at your skin.

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Use gloves when you touch parts with edge serrations.

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The indicator shows the level of hydraulic fluid in the reservoir.