293.In order to achieve the objectives of this Specification ( ), each manufacturer is expected
to reasonably adhere to the Specification content and arrangement in
order Continuing Airworthiness Programs.

479.The exhaust gas temperature indicator, on piston engine powered
airplanes, is the instrument used to identify the lean fuel flow mixtures
for various power settings.

478.TIRE WEAR INCREASES WITH HIGH SPEED.

477.THE RED LIGHTS ( ) IN HALFSECOND INTERVALS.

476.Additional information, such as GAMA membership identification,
copyright notice, etc., may be included. Format and layout is to be
determined by the CAP producer, recognizing that it is desirable that
the format and layout be similar to the producer's existing documents.

475.DO NOT LET THE HEATER ( ) TOO HOT.

474.Do an inspection of the component interface and the adjacent area.

473.A list of Page Effectivity should be provided in the front of each
Manual and can be combined with the Table of Contents, or in front of
each System/Chapter.

472.After removal from cold storage, the rivets must be completely driven
within 15 minutes.

471.Detailed information on more complex and specialized subjects, such
as Structural Wiring Diagrams or Overhaul Information, may either be
included in the basic Maintenance Manual or made available as separate
documents at the option of the manufacturer determines appropriate.

470.Move the lever rearward.