Epstein Secrets

ANUAL ATA Chapter(s), 22 AUTOPILOT, 24 Electrical Power, 32 LANDING GEAR; HONEYWELL CORP. Maintenance Ma

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

vice Change (ASO Nattier 231. SUBJECT: ELECTRICAL POWER (ATA 24) "E" BUS ALTERNATE POWER - MODIFICATION:

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

ine Discussion Verification Step(s) Symptom I Power is not available to ASE The handset display shou

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

ET CORPORATION STC SA313650. INSTALLED RSSENTIAL POWER SELECTION SYSTEM IN ACCORDANCE WITH PAGE AVJET C

ntinued airworthiness any time the above equipment Is removed and/or repaired and reinstalled. 9. The aircraft Weight and Balance is unchanged and Equipment List has been amended. 10. The aircraft must be loaded JAW the prescribed loading' Information from the manufacturer. END • 04 ti-Iffil 54 {4 C-2 A4

CORPORATION STC SA3136S0. . INSTALLED ESSENTIAL POWER SELECTION SYSTEM IN ACCORDANCE WITH .PAGE AVJET

ntinued airworthiness any time the above equipment is removed and/or repaired and reinstalled. 9. The aircraft Weight and Balance is unchanged and Equipment List has been amended. 10. The aircraft must be loaded IAW the prescribed loading information from the manufacturer. END • 0-1 S-A S-0 C-1 C-2 A