Do not do this procedure in the hangar.

For the CAP to be successful on a continuing basis, it is essential that a free flow of information exist between the operator, FAA and ABC Aircraft Company. The significant details of inspection results, repairs and modifications accomplished must be communicated to ABC Aircraft Company in order to assess the effectiveness of the recommended inspection procedures and time intervals. In some cases, extension of inspection frequencies may be possible if the data suggests that the onset of fatigue problems occurs at a greater number of flight hours than initially predicted.

The Obiectives statement contains the following inforination: (1).The relationship of the CAP to existing inspection programs and the manufacturer’s objectives for the CAP. (2).Optional information including (but not limited to) the rationale utilized to select CAPs - how the CAP requirements were determined (discussions of service history, tests and analyses)

Wherever the CAP is directed to a specific part or component, it is implied that the inspection will include observation and evaluation of the surrounding area of parts and equipment. Any maintenance anomaly would subsequently be brought to the attention of both the owner and maintenance personnel. Any anomaly should be reported to ABC, through the Condition Reporting System, so that additions and/or revisions can be made to the CAP where deemed necessary.

Recommended or Required Retirement Times of Life Limited Parts. Use of the word CAUTION, with appropriate 10-point uppercase for the text, enclosed in a box, is recommended. Sets forth manufacturer recommended retirement times for parts or assemblies (using hours, cycles or another appropriate determinant) and FAA required retirement (removal from service) times for life limited parts or assemblies.

Data shall be presented as landing distance versus outside air temperature, altitude, weight and wind. Both ground roll and the total distance over a 50 foot obstacle shall be included. The speed(s) at the 50 foot height point required to obtain the total distance shall be scheduled.

For all engines operating takeoff distance, data shall be presented as distance versus outside air temperature, altitude, weight, and wind. Both ground roll and total distance over a 50 foot obstacle shall be included.

Range values should include an allowance for fuel to start, taxi, takeoff, climb and reserve. For start, taxi and takeoff, allow 5 minutes of fuel flow at takeoff power. Reserve shall be computed as 45 minutes at the cruise power to be used for the flight.

The effective wind components along the runway shall be taken as 50% of headwind components and 150% of tailwind components in all takeoff, landing, accelerate-stop, accelerate-go and other runway performance.

The procedure shall specify that intentionally rendering one engine inoperative for the purpose of demonstrating, or training in, the recognition of VMCA will be done by starting at or above VSSE, then gradually reducing the speed (at approximately one knot per second) until either VMCA or stall warning, whichever occurs first, is obtained.

The recommended fuel conservation procedures shall contain a caution, if applicable, that the power settings recommended by the manufacturer must be used during the break-in period of new and newly overhauled engines. The use of economy power settings during this period may be detrimental to the engine life.