925、The resulting data were used to determine if the component should be considered for incorporation into the CAP.

622 Those unitis and components which furnish a means of automatically controling the flight of the aircraft. Includes those units and components which control direction, heading,attitude, altitude and speed. This Chapter may refer to supplier data, furnished with the aircraft,in lieu of the following Sections -00 through 40, as applicable.

621 Those fuselage and crew compartment windows indlusive of windshield; also those windows installed in doors.

620 This topic shall include general information, limits, and Iprocedures. In the maintenance Imanual this section shall ncover subjectst osuch as engine changes, run-up,externally-mounted spare power plants, etc.

619 This Specification is designed toprovide guidance for the preparation of Handbooks for all types of general aviation airplanes originally certifica ted at maximum takeoff weights of 12,500 pounds or less(or 5,700 kg).

618 thickness

617 The torsion link assembly transmits torsional loads from the axle to the shock strut.

616 The static discharger is electrically bonded to the frame.

615 The same coding for each individual system shall be used throughout the manual.

614 The pump()operate because the shaft()broken.轴的损坏导致泵不能正常运行。

613 The material required above shall be presented as follows.