Epstein Secrets

ished Of more space Is required attach additional sheets. Identify with aircraft nationality and registration mark and date work completed) Removed Collins Part Number 822.9210-008 TDR-94D Mode S Diversity Transponders Serial Numbers 2221 and 3672 and Installed factory modified per Service Bulletin 504

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

(II more Span is reclulfiCC art•ch additional 'Meta Identity with annul natantiCy and ItylVrtriCn frank and date work arnpieted.j Removed existing Collins TDR-90 Mode C Transponder Systeni and Stalled Collins TDR-94D/Mode S Transponder System in accordance with FAA approved Western Commander Installat

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

ing Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VORIDME from the Collins No. 1 and No. 2 VORIDME systems in accordance with manufacture's InstalatIon and Checkout Manual No. 34-60-09, Rev. 2, dated August 15, 1997 or lat

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

• 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKEJMODEUDE.SCRIPTION STATION INSTALLATION DATA 622-7203-101 3 Collins VHF-422b Comm 2. The following equipment was Installed In the aircraft. PART NUMBER QTY MAIEJMODEUDESCFtIPTIoN C37c, C38c TSO 450.0 • STATIO

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

date work completed.) 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKE/MODEL/DESCRIPTION STATION 622-7293-101 3 Collins VHF-422b Comm C37c, C38c 450.0 2. The following equipment was installed in the aircraft. • PART NUMBER QTY MAKE/MODEL/DESCRIPTION ISO ,j= S

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