Challenger 3500

Year: 2024
Price: Price on request
Serial Number: 20999
Registration: G-RRPJ
Condition: Used
Total Time: 750 Hrs
Airframe Landings: 463
Maintenance: Maintenance Tracking on CAMP

Crew: 2
Max Passengers: 10
Max Take-Off Weight: 18415 KG
Cruise Speed: 533 Knots
Max Range: 3400 NM
Max Altitude: 45000 FT
Take-Off Distance: 4,835 FT
Landing Distance: 2,364 FT

Engines: Honeywell HTF7350 turbofans
Engine Hours: 750
APU:
APU Hours: 0 Hrs

Exterior: Black

Interior: Key Features - Fans 1/A+ - CPDLC - ADS-B OUT - TCAS 7.1 - KA Band-Wifi (Ultra Hi Speed Internet Video-Conferencing) - 10 Pax Interior (Nuage Seats X6) - VHf Radios X3 - Safe Runway (Proline Software) - Galley Sink - Engines and APU Enrolled On MSP Programme - Airframe Enrolled on Smart Parts Programme - Maintenance Tracking on CAMP - Entry Area • Airstair, LH wardrobe, RH and LH avionic cabinets, RH galley, entry door acoustical curtain, and cockpit curtain. Main Cabin • Stand-up cabin with flat floor throughout the cabin • Forward sliding door separating entry from cabin • Rear sliding door separating cabin from lavatory • Six Nuage seats that feature 180°-swivel, tracking, recline and berthing capability • Four GFCI protected universal single-plug outlets • Bi-folding retractable table at each seat pair (two smaller tables at emergency exit seats) Galley • An upper compartment with stowable liftup door and an integrated 10” flight attendant touch screen • An Aircraft-certified storage compartment equipped with two universal GFCI protected electrical outlets (115 V), a multiposition pull-out tray and a bi-fold stowable door • A microwave oven • One insulated stainless large ice drawer • Solid surface deep countertop with matching pull-out work surface • Galley sink • One waste drawer with a sealed trash bin, a garbage bag retainer ring, a recycle bin and a liquid drain funnel • Concealed Circuit breaker panel • One RJ-45 port (Maintenance/Wired Ethernet Connectivity). Lavatory & Water System • Four-gallon (15.14 liters) waste capacity electric flushing toilet • Vanity cabinet with mechanically operated sink, lighted mirror and storage • Drop-down oxygen mask • Two and a half US gallon (9.46 liters) pressurised potable water system including fresh water • One belted lavatory seat, One trash bin Cabin Communications and Entertainment • A Personal Electronic Devices centric Cabin Management System that provides interfaces with Aircraft and cabin systems and distributes data and commands between the Aircraft, avionics, cabin systems and the In Flight Entertainment portion of the CMS. • One Wireless access point to connect PEDs • One In-Flight Entertainment system including worldwide maps, audio cabin briefing, 4K distribution capability and library for locally stored films and music • One Media Centre Unit that provides 2TB internal storage, four USB-C ports and two 4K HDMI Ports for content distribution • One 24-inch 4K monitor on Fwd LHS cabin bulkhead • One 4K HDMI port for content distribution at seat Master Seat Location (MSL); • Four Qi wireless charging pads for PEDs at each forward-facing seat • USB-C charging ports at each seat • A communication system including passenger notification intercoms and flight attendant call • An immersive audio system comprising "Flat Trim" panel speakers located throughout the cabin • An Iridium Certus satellite communication system providing internet and voice capability Pressurized & Heated Baggage Compartment • Accessible through lavatory • Can hold up to 750 lbs and volume of 106ft3 • External baggage door • Smoke detector

Standard Avionic Equipment: A standard autothrottle system Available Head-up Display (HUD) with Enhanced Vision System(EVS) Advanced avionics suite with four large displays Dual Flight Management System with LPV and RNP approach capabilities Synthetic Vision System (SVS) MultiScan™ weather radar Dual Inertial Reference System (IRS) Dual SBAS/WAAS GPS
Additional Avionic Equipment: Auto Flight • Automatic Flight Control System (AFCS), including computations for: • Flight guidance • Autothrottle • Autopilot • Yaw damper • Automatic pitch trim Communications • Two VHF communication radios • Two HF communication radios • Two SELCAL systems capable of monitoring two HF and up to three VHF radios • One dual channel interphone system with handheld microphones for pilot/copilot Indicating / Recording Systems • Electronic Flight Instrument System (EFIS) • Engine Indication and Crew • Awareness System • Synchronized digital GPS clock • Cockpit Voice Recorder (CVR), 2 hours • Flight Data Recorder (FDR), up to 25 hours • Emergency Locator Transmitter (ELT) Navigation • Four 12”x10”portrait active matrix LCDs • Two Flight Management Systems (FMS) • Two Integrated Flight Information Systems (IFIS) • One Synthetic Vision System (SVS) • Electronic Integrated Standby Instrument (ISI) • Two Air Data Systems (ADS) • MultiScanTM Weather Radar • Two Inertial Reference Systems (IRS) • Two Satellite Based Augmentation System (SBAS) capable receivers • Two VHF navigation receivers • One ADF receiver • Two DME transceivers • One Mode S transponder capable of ADS-B Out in non-radar areas • One Traffic Surveillance System combining an integrated Mode S Transponder and TCAS Computer capable of TCAS II change 7.1 and ADS-B Out in non-radar areas • One radio altimeter system • Terrain awareness and warning system (TAWS)