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1 #2 Serial Number: 20040 20533TEC NEW: 5684 2356 CYCLES: N1:7240 N1:8484 N2:5782 N2:8178 AVIONICS: Honeywell Primus II (package) EFIS: Honeywell EDZ 756 COMMUNICATIONS: (2) RCZ 850 NAVIGATION: (2) RNZ 850 FLIGHT CONTROL SYSTEM/AUTOPILOT: (2) Honeywell SPZ 7600 RADAR: Honeywell PRIMUS 700 TR
Report"), Purchaser shall, in its sole discretion, accept or reject the Aircraft not later than three (3) business days after Purchaser's receipt of the Inspection Report from the Inspection Facility. The Inspection Report shall include written estimates of the costs to repair each of the discrepancies noted. Such ac
TIONS: Dual Collins VHF-22A VHF Radios DISTANCE MEASURING EQUIPMENT: Dual Collins DME-42 DME Transceivers ELECTRONIC FLIGHT INSTRUMENTATION SYSTEM: Honeywell ED-800 EFIS System EMERGENCY LOCATOR TRANSMITTER: Artex C406-N ELT with Nav Interface FLIGHT CONTROL SYSTEM / AUTOPILOT: Dual Honeywell FZ-706 Fli
, LLC ("Buyer") and ASI Wings LLC ("Seller"), this notice confirms to Seller that Buyer has completed the Pre-Purchase Inspection and its review of the Inspection Report. Terms not otherwise defined herein shall have the meanings set forth therefore in the Agreement. CHECK ONE: The Aircraft is hereby conditionally
rs 3387 Eng. Its. 3367 Eng. Hrs. 4500 Eng. Hrs. 3500 Eng. Ws. N1: 8374 N2: 8081 2308 Eng. Hrs. AVIONICS: Honeywell Primus II (package) EFIS: Honeywell EDZ 756 COMMUNICATIONS: (2) RCZ 850 NAVIGATION: (2) RNZ 850 FLIGHT CONTROL SYSTEM / AUTOPILOT: (2) Honeywell SPZ 7600 RADAR: Honeywell PRIMUS 700
eport"), Purchaser shall, in its sole discretion, accept or reject the Aircraft not later than three (3) business days after Purchaser's receipt of the Inspection Report from the Inspection Facility. The Inspection Report shall include written estimates of the costs to repair each of the discrepancies noted. Such ac
X: 90 hrs TSO LANDINGS: ENGINES: (2) Turbomoca Arnel 2S2 Engines. #1 Serial Number: 42285 Time since NEW: 90 #2 42286 90 AVIONICS: EFIS: Honeywell EDZ 756 COMMUNICATIONS: (2) Collins VHF-22A NAVIGATION: (2) Cc:Mins VIR-32A FLIGHT CONTROL SYSTEM I AUTOPILOT: (2) Honeywell SPZ 7600 DAFCS RADAR
eport"). Purchaser shall, in its sole discretion, accept or reject the Aircraft not later than three (3) business days after Purchaser's receipt of the Inspection Report from the Inspection Facility. The Inspection Report shall include written estimates of the costs to repair each of the discrepancies noted. Such ac
d Arab Emirates registration number A6-DFR, equipped with Engine 1 and Engine 2 (as defined in Section 1.2 hereof) (together, the "Engines"), and a Honeywell GTCP 131-9B 3800702-1 auxiliary power unit bearing manufacturer's serial number P-5505 (the "APU"), together with all avionics, equipment (includin
e with Section 3(h) hereof within five (5) business days after the completion of the Pre-Purchase Inspection and Purchaser's and Seller's receipt of the Inspection Report. If Purchaser fails to so accept, technically accept or reject the Aircraft within such time period, Purchaser shall be deemed to have technically
Entities connected to both Honeywell and the Inspection Report

Samantha Power
PERSONLarry Visoski
PERSONDarren Indyke
PERSON
Oklahoma City
LOCATION
George W. Bush
PERSON
Oklahoma
LOCATIONAVIONICS
ORGANIZATION
Sikorsky
ORGANIZATIONthe Pre-Purchase Inspection
ORGANIZATION
Ghislaine Maxwell
PERSON
Wilmington
LOCATIONMERCHANTABILITY
ORGANIZATIONSale AC
ORGANIZATION
Keystone
ORGANIZATIONJoan Roberts
PERSONPre-Purchase Inspection of the Aircraft
ORGANIZATIONHoneywell Primus II
ORGANIZATIONthe International Registry
ORGANIZATIONFREEDOM AIR INTERNATIONAL, INC.
ORGANIZATIONthe FAA Civil Aircraft Registry
ORGANIZATION