Epstein Secrets

• 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

, &trash addltionatsheals. Identify with aircraft nationality and registration mark and date work completed.) REMOVED THE FOLLOWING EQUIPMENT: 2EA. HONEYWELL DIGITAL AIR DATA COMPUTERSP/N 7000700-962. INSTALLED THE FOLLOWING EQUIPTMENT: 2 EA. HONEYWELL DIGITAL AIR DATA COMPUTERS P/N 7000700-662 WITH STAT

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

OSITION AND OTHER NAVIGATION INFORMATION FROM THE NO. 1 UNS-ID FMS THROUGH AN EVENTIDE AVIONICS ARINC 419/429 ADAPTER UNIT AND THE AIRCRAFT'S NO. 3 HONEYWELL "LASERREF' INERTIAL REFERENCE SENSOR (IRS) DIRECTIONAL HEADING SYSTEM WHICH, PROVIDES MAP GRAPHICS AND BEARING ORIENTATION. THE FOLLOWING SWITCHES

ing Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors, and VOR/DME from the Collins No. 1 and No. 2 VORJDME systems in accordance with manufacture's Installation and Checkout Manual No. ?4-60-09, Rev. 2. dated August 15, 1997 or la

& RECEIVER / TRANSMITTER UNIT P/N 7012640-902 AND INSTALLED NEW WU- 880 ANTENNA & RECEIVER / TRANSMITTER UNIT P/N 7021450-801 (TSO C63c). INSTALLED A HONEYWELL LSZ-860 LIGHTNING SENSOR SYSTEM CONSISTING OF AN LP-860 PROCESSOR P/N 7011822-904 (TSO C110) AND AN AT-855 ANTENNA PIN 7014062-901 (TSO C110). THE

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

attach additional.sheets. Identify with aircraft nationality and registration mark and date work completed.) REMOVED THE FOLLOWING EQUIPTMENT; 2EA. HONEYWELL DIGITAL AIR DATA COMPUTERSP/N 7000700--962. INSTALLED THE FOLLOWING EQUIPTMENT: 2 EA. HONEYWELL DIGITAL AIR DATA COMPUTERS P/N 7000700-662 WITH STA