(A)6.Weight and Balance
Update aircraft weight and balance report as required:
(A)7.Electrical Load
Installation of the Spider 8 introduces a maximum continuous draw of 1.0A at 12VDC.
Update the aircraft electrical load analysis report as required.
(A)8.Continuing Airworthiness
Maintenance of the modification is in accordance with the applicable OEM maintenance
manual. Instructions for Continued Airworthiness (ICA) are not required.
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