N90TH - 1999 DASSAULT FALCON 900C

1999

DASSAULT

FALCON 900C

180

N90TH

Used

TEB

Aircell ATG 4000 Internet System Aircell Axxess II Iridium Phone System Undergoing 3C Inspection at Dassault Wilmington ADS-B, CPDLC, FANS 1A to be installed at 3C

7436.0

STATUS: As of May 11, 2018 TOTAL TIME: 7,436 LANDINGS: 2,614 ENGINES: Garrett TFE-731-5BR-1C

LEFT Total Time Since New: 7,371 Cycles Since New: 2,590 LAST MPI (HRS/CYCLES): 7085/2473 LAST CZI: 4602 SERIAL NUMBER: P-101357 CENTER Total Time Since New: 7,334 Cycles Since New: 2,580 LAST MPI (HRS/CYCLES): 7047.1/2463 LAST CZI: 4560.3/1582 SERIAL NUMBER: P-101360 RIGHT Total Time Since New: 7,334 Cycles Since New: 2,580 LAST MPI (HRS/CYCLES): 7047.1/2463 LAST CZI: 4564.5/1576 SERIAL NUMBER: P-101361 APU: Garrett GTCP 36-150F Serial Number: P-355 TSN: 2937

AIRBORNE FLIGHT INFORMATION SYSTEM: Honeywell VHF AFIS and SATAFIS AIR DATA COMPUTER: Dual Honeywell AZ-840 Air Data Computers AUTOMATIC DIRECTION FINDER: Dual Collins ADF-462 AUTOPILOT / FLIGHT DIRECTOR: Honeywell Primus 2000 with IC-800 IACs COCKPIT VOICE RECORDER: Allied Signal Cockpit Voice Recorder COMMUNICATIONS: Dual Collins VHF-422C Transceivers with 8.33 Spacing and FM Immunity CPDLC/FANS: Aircell DIU Level D for FANS/CPDLC Compliance DATALINK: Honeywell CMU MK III CPDLC FANS 1/A Capable DISTANCE MEASURING EQUIPMENT: Dual Collins DME-442 EFIS: Honeywell Primus 2000 Five Tube EFIS EMERGENCY LOCATOR TRANSMITTER: Socata Triband ELT 96 406 MHz ENHANCED GROUND PROXIMITY WARNING SYSTEM: Allied Signal EGPWS MK IV with Wind Shear Detection FLIGHT DATA RECORDER: Allied Signal Flight Data Recorder FLIGHT MANAGEMENT SYSTEM: Triple Honeywell FMZ-2000 FMS with triple FMS CDU-810 displays. GLOBAL POSITIONING SYSTEM: Dual Honeywell FMZ-2000 GPS Units LPV/ WAAS Compliant (TSO C145C & C146C) HIGH FREQUENCY COMMUNICATION: Dual High Frequency HF-9000 Radios INERTIAL REFERENCE SYSTEM: Triple Honeywell Laseref III Inertial Reference Systems NAVIGATION: Dual Collins VIR-432 Navigation Receivers RADAR: Honeywell Primus 880 Weather Radar with dual controllers RADIO ALTIMETER: Single Honeywell AA-300 Radio Altimeter SELCAL: 2 Channel Coltech CSD-714 Selcal Decoder TRAFFIC COLLISION AVOIDANCE SYSTEM: Collins TCAS II with Change 7.1 TRANSPONDER: Dual Collins TDR-94D with change 7 ADS-B Out (Level: DO-260B) COCKPIT Honeywell N1 DEEC’s Dual Baker Audio Control Panels with 3rd option at jumpseat Dual Davtron Clocks ? Baker M3071F Cabin chime/PA system 5.6” Rosen Cockpit Display for Airshow

2008

12

Original Interior, Lavatory Re-Upholstered in August 2015 The aircraft has a twelve-passenger interior with a forward four-place leather club-seating area followed by a fabric four-place conference group and mid-cabin credenza with an aft leather seat and a three-place fabric divan. Third flight deck seat certified for take-off and landing. All woodwork veneer is Elm Burl custom stain, Hi-Gloss. All hardwood moldings are Birdseye Maple. All metal surfaces are Satin Nickel.

INSPECTION---------------------------NEXT DUE 1C Inspection---------------------------December 2018 2C Inspection---------------------------May 2024 3C Inspection Inspection------------scheduled for 06/2018 Eng. #1 – 1000/1400 Hr. Insp.-----8,285 Hrs. Eng. #2 – 1000/1400 Hr. Insp.-----8,247.1 Hrs. Eng. #3 – 1000/1400 Hr. Insp.-----8,247.1 Hrs. Eng. #1 – 1200/1650 Hr. Insp.-----8,685 Hrs. Eng. #2 – 1200/1650 Hr. Insp.-----8,647.1 Hrs. Eng. #3 – 1200/1650 Hr. Insp.-----8,647.1 Hrs. Eng. #1 – MPI Insp.------------------9,585 Hrs. Eng. #2 – MPI Insp.------------------9,547.1 Hrs. Eng. #3 – MPI Insp.------------------9,547.1 Hrs. Main Landing Gear OH--------------05/17/2024 or 7874 Cycles