Epstein Secrets

y other A/R applicable task after AD 2012-24.08 C/W. 4. Compliance with AD 2010-24-11 / SB 737.57A12

SEALS (2) (OFF OPEN AIRCRAFT) NO. 1 ENGINE - ENGINE FUEL AND CONTROL - MODIFY THE ENGINE BY REMOVING FULL AUTHORITY DIGITAL OPEN ENGINE CONTROL (FADEC) SOFTWARE, VERSION 7.B.V4 OR EARUER, INSTALLED IN THE ELECTRONIC ENGINE CONTROL (EEC) NO. 2 ENGINE - ENGINE FUEL AND CONTROL - MODIFY THE ENGINE BY

MER OF INGRES 2 9 PROPELLER WADERS MK me, N/A W. PROPOSER 1100EL OFFIGNATION II. AIRCRAFT 6 rim d

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

prescribed under tho provisions of 14 CFR 91.319 W. 3. R&D flights must be conducted lAW Nextant Aer

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

SapaturefDate of Authorized Individual ,R obert W. Vogt 40/2012 ..------,:a . 9. 774 20 A FAA F

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 . 1T1SD Engines. 2. Williams

NU- NAME N/A ,0 4 FACTURER ADORESS /..? 0, *W. FUGHT FROM 45 TO A -'• __. N 405PJ MODEL

lteration 8.) This equipment was found not to exceed the guidelines in FAA Roiorcraft Directorate policy letter ASW.2001-4, dated Apri 25. 2003 for FADEC controlled aircraft and is considered to be "equipment not known to have potential for interference. 9.) CONTINUED AIRWORTHINESS' Requires operation

y lloy complale Solana Wm, NON& use NAN% R. W. and w as NOON. L AIRCRAFT 0ISCIIP TON I REGIST

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

ANGAR FITTING WAS MARKED Status: TERMINATED I.A.W. SB 737-71A1462 R3 Rev: 3 EARLIEST Reason Frog

: AD Status: TERMINATED Rev: 00 CFM56-715-73-0204 DUAL ENGINE THRUST INSTABILITY EVENT Reason CFM56-76-734204 COMPLIED (INSTALUWEIN OF LATEST FADEC SOFTWARE VERSION T.E.WF2) SATISFY THE AD REQUIREMENT LATEST 2015-18-04 Category: AD Status: N/A Rev: 01 CFM56-7B-72.0964 73-TOOTH GEARSHAFT L