This procedure points out that the FAA should be contacted prior to any alterations on airplane to ensure that airworthiness of the airplane is not violated.

The trailing edge flaps up limit switch sends flap position data to SMYD1.The SMYD1 uses this during yaw damping to limit rudder movement when flaps are up.

Where possible, examples, associated conditions and technique should be presented on the same page as the chart. If space is not sufficient to include the necessary information, then the page facing the chart should be used.

An “emergency” however, almost always involves a failure that requires immediate and rapid response, such as a total powerplant failure, fire or smoke, or rapid cabin decompression.

It is generally preferable to remove the damage prior to submitting information to Boeing for review except for dents on metallic and composite structures, and delamination or punctures to composite structure unless removal is already approved by SRM, CMM

The auxiliary battery and auxiliary battery charger connects in parallel with the main battery during non-normal conditions to help supply power.

They include the tail assembly ,the structures at the rear of the airplane that serve to control and maneuver the aircraft and structures forming part of and attached to the wing.

Move the IDG forward until the input shaft is free of the accessory gearbox and QAD ring, then move the IDG outboard and away from the power plant.

Differences in the fuel/water sample and the ability of the detection kits to consistently measure the level of microbial growth make it important to retest and verify test results.

If you push the LSK that is adjacent to EXIT, then the BITE will take you out of BITE test and put the airplane back to its usual condition.

The Preface has been omitted in the sample CAP in Section III and the necessary information has been included in the Objectives.