Epstein Secrets

P rsuant to the authority g yen persons specified below. the unit identified in item 5 was 'nspeded in the manner prescribed by the A minetrator of the Federal Aviation Administration and S InApproved JDRejected BY FAA Fit. Standards Inspector Manufacturer Maintenance Organization PiaraOnS ArCeOveci by Cartbdian Deparallel

replace Pratt & Whitney JT15D-5 series engines with Williams International F344-3AP engines (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems (Coatis. A) and (/or) the installation of Nextant Wingless (Config. B), in accordance with Nextant Aerospace Master Drawing

Date of Authorized Ircligdu r ,..„1 7. Approval foe Return Pursuant to the loth:fey given person; Spedtled Wog. the unit idettled Admiritarate Of the Federal Aviation Administration and is O:C in fern 5 was inspected In the manner presets by the APPROVED 0 REJECTED BY FAA Fit Standards IMpeCler tilanklecturer Maintenanc

cement of Pratt & Whitney JT15D-5 series engine with Williams International FJ44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins F

. Pursuant to the authority given persons speofied belOw. the unit identified In kern 5 was nspected in the miner prescribed by the Admvistrator of the Federal Aviation Administration and n e APProved O Rejected BY FAA FR. Standards inspector Manufactwe Maintenance Organization Persons Approves by Ceneclen Deparlrnent Of

e was computed. This equipment was found not to exceed the guidelines in FAA Rolorcaft Directorate poky letter ASW-2001.4. dated April 25. 2003 for FADEC controlled aircraft and is considered to be 'equipment not known to have potential for interference'. CONTINUED AIRWORTHINESS: Requires operational

. A • proval for Return to Service Pursuant to the authority paten persons specified below. the Lilt Wenn, In item 6 va tinspected Administrator of the Federal Aviation Administration and la I Approved In the mama prescribed by the Rigel:led BY --"' FAA Fit. Standards Inspector — Manufacturer — — Maintenance OrgaNzatlon

replace Pratt Whitney JT15D-5 series engines with Williams International F.144-3AP engines (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems (Config. A) and (tor) the installation of Nextarrt Winglets (Config. B), in accordance with Nextant Aerospace Master Drawing

Pursuant to the authority given persons speared ['Sow, the unit identified in item 5 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is El APPROVED K REJECTED BY FAA Fit Standards Inspector Manufacturer Maintenance Organization [Person Approved by Canadian Department of

cement of Pratt & Whitney JT15D-5 series engine with Williams International FJ44-3AP engine (TCDS E3GL) with Full Authority Digital Engine Control (FADEC) and associated systems. ST10959SC: Installation of Rockwell Collins Pro Line 21 Electronic Flight Instrument System (EFIS) with Rockwell Collins F

art 43 APP. B 0 05/30/2013 7. Approval for Return to Service Pursuant to the authority given persons specified below, the unit Administrator of the Federal Aviation Administration and is identified es in item 5 was inspected in me manner prescribed by the APPROVED 0 REJECTED BY FAA Flt Standards Inspector Manufacturer

n: This Aircraft is a standard Beech let 400A with new Williams F144-3AP engines and upgraded avionics with full authority digital engine controls (FADEC) a. Maintenance Program 1. Hawker Beechcraft Maintenance Manual Chapter 5 Rev C22 or later with the exception of the .1115D Engines. 2. Williams