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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/Reactivatio n 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

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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 EACHOTHER

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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.

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Turn the knob to make the display go out of view.

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Do an inspection of the damage and of the adjacent area.

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Drain approximately 2 liters of fuel from the tank.

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Do not do this procedure in the hangar

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Calculate the pressure with the applicable formula.

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Make sure that there is no dust on the surface

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Move the rod in the lopposite direction.

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This procedure is applicable only in digital mode.

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Explain how to avoid and notice fuel contamination.

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Maintenance information needs to be continuously updated.

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Other information may be displayed on the cover.

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Access and location instructions are provided here unless obvious.

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Operate the unit for two cycles to remove air from the lines.

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Move the tensiometer along the cable.

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Use the manual procedure if it is not possible to use the automatic control.

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Replace nuts and washers if removed during inspection.Do not reuse.

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The airplane has been maintained in accordance with manufacturer recommendations or equivalent.