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,

Canada Airworthiness Group Date of Approval or Rejection 1/14/02 Certificate or Designation No. EVICR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance. FAA Form 337 (1288) SDNY_GM_02759743 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA_0O246665 EF

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,

y Transport Airworthiness Group Date of Approval or Rejection 1/14/02 Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assurance. 11-V. FAA Form 337 (12-88) EFTA00277660 NOTICE Weisht.andtalanca Or operating limitation changes shall be entered i

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,

Transport Airworthiness Group Date of Approval or Rejection 7/2/01 Certificate or Designation No. EYKR782D Signature of Authorized Individual Ronald K. Bystrom. Manager Quality Assuranc FAA Form 337 (12-88) EFTA00277690 NOTICE Weight and balance or operating limitation changes shall be entered in the ap