Epstein Secrets

ce Pursuant to the authority g yen persons specified below, the u ' retied in rem 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration end is XIApproved I—Rejected BY FAA Fri Standards Inspector Manufacturer Maintenance Organization Pawns Approved by Canadian Depannuthr or T

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,

nt Administrator BY to the authority given persons specified below, the unit dentified in item 4 was inspected In the manner prescribed by the of the Federal Aviation Administration and is 0 APPROVED O REJECTED FM Fit. Standards Inspector Manufacturer Inspection Authorization Other (Specify) FM Designee X Repair Station

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,

tor. x,I.Z.-- L/C-6 -- , 7. Approval for Return to Sery Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 Was inspected in the manner prescribed by the K REJECTED Cs APPROVED FM Flt. Standards Inspector Manufacturer Insp

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,

nspector. 16, U -V 7. Approval for Return to Service k Pursuant Administrator BY to the authority given persons specified below, the unit of the Federal Aviation Administration and is identified in item 4 was inspected in the manner prescribed by the K REJECTED C4 APPROVED FAA Flt. Standards Inspector Manufacturer Ins

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,