on of Pre-Purchase Inspection 1. Inspect complete records and documentation 2. Perform Visual Inspection 3. Perform Engine Power Check 4. Perform FADEC download EFTA00295195 AIRCRAFT PURCHASE AGREEMENT DATED AS OF APRIL 16, 2012 BY AND BETWEEN FREEDOM AIR INTERNATIONAL, INC. AND EAGLE COPTERS

on of Pre-Purchase Inspection I. Inspect complete records and documentation 2. Perform Visual Inspection 3. Perform Engine Power Check 4. Perform FADEC download EFTA00300140 AIRCRAFT PURCHASE AGREEMENT DATED AS OF APRIL 16, 2012 BY AND BETWEEN FREEDOM AIR INTERNATIONAL, INC. AND EAGLE COPTERS

on of Pre-Purchase Inspection 1. Inspect complete records and documentation 2. Perform Visual Inspection 3. Perform Engine Power Check 4. Perform FADEC download EFTA00311123 AIRCRAFT PURCHASE AGREEMENT DATED AS OF APRIL 16, 2012 BY AND BETWEEN FREEDOM AIR INTERNATIONAL, INC. AND EAGLE COPTERS

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

14 Selcal AlliedSignal Mark V EGPWS with RAAS Upgrade ACSS TCAS 2000 TCAS II (Change 7 Incorporated) Full Authority Digital Engine Control System (FADEC) Central Aircraft Information Maintenance System (CAIMS) Dual Full Flight Regime Auto Throttle System AlliedSignal SSCVR Cockpit Voice Recorder A

Blade Set • Re•Index (710036) Engine 2 71.00.00 0.0 Hrs 0 OL 29 Dec 2012 0.00 Engine Test 9 • Full Authority Digital Engine Control 710037 (FADEC) Operational TOM Engine 1 71.00.00 9.6 Hrs 4 CA_ 14 Jun 2013 1.00 Engine TOM 9 • Full Authority Digital Engine Control 710037 (FADEC) Operat

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

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

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

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

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

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

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

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

: 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

: AD Status: TERMINATED Rev: 00 CFM56-78-73-0204 DUAL ENGINE THRUST INSTABILITY EVENT Reason CFM56-76-734204 COMPLIED (INSTALULTION OF LATEST FADEC SOFTWARE VERSION 7.0.WF2) SATISFY THE AD REQUIREMENT LATEST 2015-18-04 Category: AD Status: N/A Rev: 01 CFM56-7B-72.0964 73-TOOTH GEARSHAFT L