Epstein Secrets

T MANAGEMENT SYSTEM. REFERENCE F.A.A. FORM 8110-3 DATED 4/19/02 BY SYSTEMS AND EQUIPMENT DER NO. DERT510087-NM. ACCOMPLISHED OPERATIONAL CHECKS PER UNIVERSAL AVIONICS CORP. RETURN TO SERVICE MAINTENANCE AND CHECKOUT PROCEDURES MANUAL NO. 34-60-21. DATED 19 MARCH 200) writ NO DISCREPANCIES NOTED. AN EMI TEST. REPORT NO.

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,

FORM 8110-3, DATED 05/29O001 BY SYSTEMS AND EQUIPMENT DER NO. DEBT-510087-NM. THE NEW EQUIPMENT AND ASSOCIATED SYSTEMS WERE FUNCTIONALLY TESTED PER UNIVERSAL AVIONICS CORP. RETURN TO SERVICE MAINTENANCE AND CHECKOUT PROCEDURES MANUAL NO. 34-60-21, DATED 19 MARCH 2001 WITH NO DISCREPANCIES NOTED. AN EMI TEST, REPORT NO

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,

T MANAGEMENT SYSTEM. REFERENCE F.A.A. FORM 8110-3 DATED 4/19/02 BY SYSTEMS AND EQUIPMENT DER NO. DERT510087-NM. ACCOMPLISHED OPERATIONAL CHECKS PER UNIVERSAL AVIONICS CORP. RETURN TO SERVICE MAINTENANCE AND CHECKOUT PROCEDURES MANUAL NO. 34-60-21, DATED 19 MARCH 2001 WITH NO DISCREPANCIES NOTED. AN EMI TEST, REPORT NO.

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,