Epstein Secrets

al when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors,

DATED 06/01, SHEETS 1 THRU 5, TITLED - 28-14 VDC CONVERTER EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3 DATED 6/10/01 BY STRUCTURES DER NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER KGS ELECTRONIC MODEL UC-28-14 INSTALLATION MANUAL WITH NO DISCREPANCIES. AN

ED 911/01, SHEETS 1 THRU 7. TITLED - CABIN NO. 2 60 HZ EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8I10-3, DATED 6/13/01, BY STRUCTURAL D.E.R. NO. DERT-810028-NE AN EMI TEST, REPORT NO.: B727-16236080 REV IR. SHEETS 5, DATED 06119/01 WAS CONDUCTED AND THE INSTALLED EQUIPMENT DOES NOT INTERFERE WITH ANY OTHER

al when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors,

TITLED - MINOR DEVIATION TO STC SA3137S0, THE LIMITED 727-100 GENERAL ARRANGEMENT. REFERENCE F.A.A. FORM 8110 DATED 1/6/02 BY STRUCTURES D.E.R. NO. DERT-810028-NE. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED A

al when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors,

TITLED - MINOR DEVIATION TO STC SA3137SO, THE LIMITED 727-100 GENERAL ARRANGEMENT. REFERENCE F.A.A. FORM 8110 DATED 1/6/02 BY STRUCTURES D.E.R. NO. DERT-810028-NE. A LOGBOOK ENTRY REFLECTING THIS INSTALLATION WAS COMPLETED PER F.A.R. 43.9 AND ENTERED INTO THE AIRCRAFT LOGBOOK. THE EQUIPMENT LIST WAS AMENDED A

al when the airplane is modified by the installation of dual Universal Avionics Systems Corp. (UASC) (UNS-1D) Flight Management Systems (FMS), with Frequency Management via a UASC Radio Tuning Unit (RTU), receiving navigation inputs from Triple Honeywell Inertial Reference Sensors (IRS), dual internal GPS sensors,

DATED 6/6/01, SHEETS 1 THRU 5, TITLED - 28-14 VDC CONVERTER EQUIPMENT INSTALLATION. REFERENCE F.A.A. FORM 8110-3 DATED 6/10/01 BY STRUCTURES DER NO. DERT-810028-NE. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER KGS ELECTRONIC MODEL UC-28-14 INSTALLATION MANUAL WITH NO DISCREPANCIES. AN