Epstein Secrets

5.1353 (aXe) Based on 14 CFR §§ 21 115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Collins Profile 21 FMS-6100 with LPV Approach enabled and UASC TAWS was determined to be TCDS Al 6SW and the following later regulations: AmdclOriginall

ance Signature,. - Date Robert Beaumont 0 ‹ e :,./-0S-- Approved By SI? Date Todd Hattaway , / 01 /0/2-/i/4 74r Regulat'i ry Compliance 92 Major Repair 0 Minor Repair FAA Approval N Yes 0 No Weight & Balance Affected 0 Yes 0 No Weight 4 lb increase Ann 108 Parts Required Equipment List Upda

• 1. The following equipment was removed from the aircraft: PART NUMBER QTY MAKEJMODEUDE.SCRIPTION STATION INSTALLATION DATA 622-7203-101 3 Collins VHF-422b Comm 2. The following equipment was Installed In the aircraft. PART NUMBER QTY MAIEJMODEUDESCFtIPTIoN C37c, C38c TSO 450.0 • STATIO

PAIR AT STA 663 RBL 54 END • NOTES: 1. This approval is for Northwest Delaware aircraft N505LS, S/N 20115 only. PURPOSE OF OATH In support of a Major Repair accomplished on aircraft S/N 20115. This approval is for design and static analysis only and is not Installation approval. APPLICABLE REQUIREMENTS

ing 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 Checkout Manual No. ?4-60-09, Rev. 2. dated August 15, 1997 or la

T STA 663 RBL 54 . END . . NOTES: 1. This approval is for Northwest Delaware aircraft N505LS, S/N 20115 only. PURPOSE OF DATA In support of a Major Repair accomplished on aircraft S/N 20115. This approval is for design and static analysis only and is not installation approval. APPLICABLE REQUIREMENTS