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,

oved by Transport Ains Group Canada Donor 49(0=1 or Rejection August 1, 2001 Catifiratcor Dosignaticas No. DU4R141M Sigmas a Authiciud Ind' L. Palm FAA Form 337 (12-88) SDNY_GM_02759747 SUBJECT TO PROTECTIVE ORDER PARAGRAPHS 7, 8, 9, 10, 15, and 17 EFTA 00246669 EFTA01331132 NOTICE Weight

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,

port Canada .. Aim() • .....4. Group - Data of Approval or Rejection August 1, 2001 Certificate or Designation Na • DU4R141M ' Signatu c • 1 / L. Palm Authorized Ind' y • ual 0 IIIIIP, On FAA Form 337 (12-88) EFTA00277664 NOTICE • Weight andbalance or operating limitation changes shall be e

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,

da Airworthiness Gro Date of Approval or Rejection August 7, 1999 Certificate or Designation No. DU4R141M Signature of Au - ed Individual out L. Palm FAA Form 337 (12-88) EFTA00277766 4 . NOTICE Weight and balance or operating limitation changes shall be entered in the appropriate aircraft re