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,

ada Airworthiness Group Date of Approval or Refection 6/12/02 Certificate or Designation No. EYKR782D Signature of Authorized Individual k ' John K. Urso. Inspector., -;l" , -: L us` I ' 6 FAA Form 337 risen / SDNY_GM_027 59737 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_

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,

and that the information furnished heroin Is true and correct to the best of my knowledge. Date 7201 Signature of Authorized Inane u ie.•(.4—e-- John K. Urso. Inspector. 7. Approval for Return to Servl Pursuant Administrator BY to the authority given persons specified below, the unit identified in ite

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,

rthiness Group Date of Approval or Rejection 6/12/02 • Certificate or Designation No. EYKR782D Signature of Authorized Individual .- C.. - . John K. Urso. Inspector. -- ' & 6 1 FAA Form 337 (12-88) EFTA00277654 NOTICE Weight and balance or operating limitation changes shall be entered in the app

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,

ons and that the information furnished herein is true and correct to the best of my knowledge. Date 7/2/01 • Signature of Authorized Individual John K. Urso. Inspector. 16, U -V 7. Approval for Return to Service k Pursuant Administrator BY to the authority given persons specified below, the unit