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on Computers (3), and a Single Honeywell VLF/OMEGA Sensor in accordance with data approved by STC SA3774NM. Flight Manual supplements provided and Equipment List revised. Aircraft weight and balance report revised. END 6 ADDITIONAL SHEETS ARE ATTACHED C FAA AC/2490A 0 U.S. GOVERNMENT PRINTING OF TICE I

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ance with applicable pardons of Advisory Circulars 43.13-1A, Chapter 2, and 43.13-2A, Chapter 3 and 13. The Aircraft Weight and BalanCe Report and Equipment List has been revised to reflect this installation. The work described has been found to be in conformity with the above data, and continues tomeet the

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ugust 9, 2012 or later FAA approved revision has been inserted into the Airplane Flight Manual. The aircraft Weight & Balance change negligible and Equipment List amended. The electrical load was computed and found not to exceed 80% of the system output. Log book entry made. INSTRUCTIONS FOR CONTINUED AIRWORT