Specifications are subject to verification by purchaser. Aircraft is subject to prior sale, and/or removal from market without notice.
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7 Highlights: Engines, APU and Airframe on Programs Aircell ATG-4000 New Carpet One Owner All Major Maint. Performed by Bombardier Airframe: Bombardier Smart Parts Total Time 3, 472 Hrs 2,891 Cy Entry Into Service Jan 2011 Maintenance Tracking Flightdocs Certification Part 91 Engines: Honeywell MSP HTF7000 Left Right Serial Numbers P P Hours 3,503 3,503 Cycles 2,915 2,915 Next Shop Visit (MPI) On-Condition On-Condition Core Zone Insp (CZI) On-Condition On-Condition Improved Combustion Liner SB Rev. 3 APU: Honeywell MSP Honeywell GTCP36-150(BD) Serial Number P-410 Total Time 2,982 Entertainment / Connectivity: Aircell ATG-4000 Datalink (C23-406) DVD/CD Player Airshow 4000 with two 20 Monitors Lufthansa Technik CL-300 NICE System CMS Maintenance Last Next Remain 12 Month Dec 2016 Dec Mo. 24 Month Dec 2016 Dec Mo. 36 Month Dec 2016 Dec Mo. 48 Month Dec 2014 Dec Mo. 96 Month N/A Jan Mo. 192 Month N/A Jan Mo. 600 Hour 2979 Hrs 3579 Hrs 106 Hrs 800 Hour 3182 Hrs 3982 Hrs 510 Hrs 1200 Hour 3182 Hrs 4382 Hrs 910 Hrs 1600 Hour 2446 Hrs 4046 Hrs 574 Hrs 2400 Hour 2397 Hrs 4797 Hrs 1325 Hrs 3200 Hour 3065 Hrs 6265 Hrs 2793 Hrs 4200 Hour N/A 4200 Hrs 727 Hrs 9600 Hour N/A 9600 Hrs 6127 Hrs 7
8 Avionics Qty Description ADC (Air Data Computer) Dual ADC-3000 CVR (Cockpit Voice Recorder) Single L3 Technologies FA2100 CVR Data Loader Single Collins DBU-5000 DME (Distance Measuring Equipment) Dual Collins DME-4000 EFIS (Electronic Flight Instrument System) 4 LCD Collins Pro-Line 21 w Dual IFIS EGPWS (Enhanced Ground Proximity Warning System) w Windshear and Terrain Display Single Honeywell TAS-5000, Mark V w/ RAAS ELT (Emergency Locator Transmitter) Single Artex C406-N w NAV Interface FDR (Flight Data Recorder) Single L3 Technologies FA2100 FDR FMS (Flight Management System) w SBAS, LPV Dual Collins FMS-5000 GPS with WAAS Dual Collins GPS-4000S Lightning Detection System Single L3 WX-1000E NAV (Navigation Radio) Dual Collins NAV-4000 RADAR ALT (Radar Altimeter) Single Collins ALT-4000 SATCOM (Satellite Communications) Single Aircell Iridium System (ST4200) w ACARS TCAS (Traffic Collision Avoidance System) Single Collins TTR-4000, Vers 7.0 VHF COM (Very High Freq. Communication) Triple Collins VHF-4000 XM Weather Single XMWR-1000 (displayed on MFD) (C46-419) XPNDR (Transponder) Dual Collins TDR-94B Mode-S 8
9 Additional Equipment / Options: Pulse Landing Light (SB ) Exterior Logo Light (SB ) FMS V-Speed option for Dual FMS (SB ) FMS Optional 3D Maps (C34-407) Enhanced Map Overlays (SB ) Control Wheel Lighted Chart Holders (25-417) Folding Step Ladder in Equipment Bay Interior (2010/2017): 9 Pax, Eight place with double club configuration with executive fold out tables and a Belted Lav New Carpet (2017) Aft Lav Pocket Door between Galley and Cabin Forward Galley with Microwave and with Two Hot Liquid Dispensers Exterior (2010): White with Black, Red, and Grey Stripes 9
10 Contact Us MENTE Group, LLC North Dallas Parkway, Suite 1010 Addison, Texas Delray Dobbins Cell Office Fax
2009 Bombardier Challenger 300 S/N: Reg: T7-GOB
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2007 BOMBARDIER CHALLENGER 605
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2007 bombardier challenger 605. serial number 5709 registration 9H-AFQ
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1996 Dassault Falcon 2000 Serial Number: 006 Registration: N954SC
Airframe: C of A Issue Date: July 17, 1995 Delivery Date: 1996 Airframe Total Time: 6,975 Airframe Total Cycles: 4,283 Engines: CFE Model CFE738-1-1B Engine #1: SN P105121, 6,249.6 TT, 3,850 ENC Engine
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G U L F S T R E A M G S / N 1 4 6
MAX CRUISE SPEED 470 ktas PASSENGERS 8 RANGE (NM) 2,790 HIGHLIGHTS NEW CUSTOM PAINT IN PROCESS ENGINES & APU ENROLLED ON JSSI CUSTOM INTERIOR BY DUNCAN UPGRADED FMS W/ WAAS & LPV WI FI OVERVIEW Best G100
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AIRFRAME Status as of November 13, 2007 Total Airframe Hours Since New : 60,488 Hours Total Airframe Cycles Since New : 26,881 Cycles
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MDC , 402, 403, -404, -405 Display Control Panel DCP , 104, 106, -204, 206 Electronic Flight Display (PFD, MFD)
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As a proud Gulfstream owner, you are aware of the outstanding characteristics of your aircraft. From record-setting performance capabilities to state-ofthe-art technology, your Gulfstream was designed
apply nose down control wheel force upon autopilot disconnect. Preflight system test has failed.
13.4 AFCS ALERTS System Status Annunciation System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD. Figure 13-5 AFCS System Status Annunciation
(12) United States Patent (10) Patent No.: US 8,102,301 B2. Mosher (45) Date of Patent: Jan. 24, 2012
USOO8102301 B2 (12) United States Patent (10) Patent No.: US 8,102,301 B2 Mosher (45) Date of Patent: Jan. 24, 2012 (54) SELF-CONFIGURING ADS-B SYSTEM 2008/010645.6 A1* 2008/O120032 A1* 5/2008 Ootomo et
Aeródromo Municipal de Cascais, Hangar 6 Tires S. Domingos de Rana Tel Fax
ATA 0502 AIRBORNE COLLISION AVOIDING SYSTEM ELEMENTARY MODE S TRANSPONDER DO 228 202K ATA 0601 INSTALLATION OF TERRAIN AWARENESS AND WARNING SYSTEM (TAWS) SHORT S SD 3.60I ATA 0602 RETROFIT OF AIRBORNE