Epstein Secrets

rp. (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 VORIDME from the Collins No. 1 and No. 2 VORIDME systems in accordance with manufacture's InstalatIon and Che

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_

rp. (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 VOR/DME from the Collins No. 1 and No. 2 VOR/DME systems in accordance with manufacture's Installation and Ch

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

rp. (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 VOR/DME from the Collins No. 1 and No. 2 VOR/DME systems in accordance with manufacture's Installation and Ch

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

rp. (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 VOR/DME from the Collins No. 1 and No. 2 VORJDME systems in accordance with manufacture's Installation and Ch

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