The sensor of the engine fire detection system is always a dual continuous loop.

Equipment without significant effect on the weight or balance of the airplane need not be listed.

The calculation procedures and “basic empty weight” data used in loading calculations shall be explained.

This paragraph describes the procedure for establishing weight and moment (relative to reference datum) of the empty airplane.

The manufacturer should use formats appropriate to the specific airplane and the size of the Pilot＇s Operating Handbook.

Additional weight and balance and related information may be provided.

Vertical Stabilizer Tip Rib Modification

Remove wing-fuselage attach fairings.

The operator may use standard ABC Condition Report form(s) or an equivalent containing the same information.

This reporting system does not supersede the normal channels of communication for items not covered by the CAP.

Both digits of Chapter Number in the Continuing Airworthiness Program lnspection number are determined by GAMA Specification No. 2 Numbering System.