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BOMBARDIER CHALLENGER 350 – ANO 2015 – 523 H.T.
Jato Comercial
REF:
PL5243
Preço sob consulta
Status
Vendida
Fabricante
Bombardier
Modelo
CHALLENGER 350
Motor
AS907-2-1A
Combustível
Jet A - Querosene
Ano
2015
Horas totais
523
Assentos
N/A
Condição
Usado
Localização
Brasil
Ano
2015
Horas totais
523
H
Assentos
N/A
Condição
Usado
Localização
Brasil
Galeria do PDF (Não visível na página normal)
Visão geral
Especificações
Visão geral
- Ex-works
- Valor de venda + impostos para nacionalização
Airframe
- Total Time 523.3
- Total Landings 243
- Winglets
- Maintenance Tracking FLightDocs
Engine 1
- Engine 1 Time 523.3 SNEW
- Engine 1 Cycles 243
Engine 2
- Engine 2 Time 523.3 SNEW
- Engine 2 Cycles 243
Auxiliary Power Unit
- APU
- APU Time 235.75
Avionics
- ADS-B Equipped
- FANS
- CPDLC
Avionics/Radios
- Rockwell Collins Pro Line 21 Advanced Avionics Suite
- Single Three-Axis Category II Automatic Flight Control Systems (AFCS)
- Two (2) VHF Comm Radios
- Two (2) HF Comm Radios
- Two (2) SELCAL Systems capable of monitoring two (2) HF and up to three (3) VHF radios
- One (1) dual channels interphone system with hand-held microphones and individual controls for pilot and co-pilot
- Electronic Flight Instrument System (EFIS)
- Engine Indication and Crew Awareness System (EICAS)
- Synchronized Digital GPS Clock
- Cockpit Voice Recorder
- Flight Data Recorder
- Emergency Locator Transmitter
- Two (2) Flight Management Systems (FMS)
- Two (2) Integrated Flight Information Systems (IFIS) (require subscription)
- One (1) Synthetic Vision System (SVS)
- Two (2) EFB class 1 tablet computers including Bombardier’s Flight Deck application (loose equipment)
- One (1) Electronic Integrated Standby Instrument (ISI)
- Two (2) Inertial Reference Systems (IRS)
- Two (2) Global Navigation Satellite System (GNSS) Satellite Based Augmentation System (SBAS) capable receivers
- Two (2) VHF Navigation Receivers
- Two (2) DME Transceivers
- One (1) Mode S Transponder capable of ADS-B Out in non-radar areas
- One (1) 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 (1) Radio Altimeter system
- One (1) Terrain Awareness and Warning System (TAWS)
Additional Equipment
- Datalink (VDL Mode 2), Controller-Pilot Datalink Communication (CPDLC) and Iridium Interface
- FANS1/A+ (CPDLC & ADS-C) and Inmarsat Satcom SwiftBroadband with Cockpit Safety Service / ACARS Communications
- Second Automatic Direction Finder (ADF)
- Enhanced Map Overlays
- SRSL (Smart Runway Smart Landing C34-500)
- RNP AR 0.3
- ANR to USA
- Air-to-Ground Cabin Connectivity Solution
- Dual LED Navigation Lights
Exterior
- Year Painted 2015
Interior
- Year Interior 2015
- Galley
- Galley Configuration Forward
- Lavatory
- Lavatory Configuration Aft
Inspection Status
- 12 Month Inspection complied with December 2020; next due December 2021
- 24 Month Inspection complied with December 2019; next due December 2021
- 36 Month Inspection complied with December 2018; next due December 2021
- 48 Month Inspection complied with November 2019; next due December 2023
- 96 Month Inspection due December 2023
- 192 Month Inspection due December 2031
- 600 Hour Inspection due @ 600 hours
- 800 Hour Inspection due @ 800 hours
- 1200 Hour Inspection due @ 1200 hours
- 1600 Hour Inspection due @ 1600 hours
- 2400 Hour Inspection due @ 2400 hours
- 3200 Hour Inspection due @ 3200 hours
- 4200 Hour Inspection due @ 4200 hours
- 9600 Hour Inspection due @ 9600 hours
- Landing Gear Inspection due December 2023
- Landing Gear Overhaul due December 2031
- LH & RH Engine MPI/HSI/Combust due @ 4800 engine hours
- LH & RH Engine OVH/CZI/Compress due @ 9600 engine hours
A aeronave acima é de terceiros, os dados estão sujeitos a verificação.
Especificações
Exterior
- Exterior Height: 20 ft 0 in
- Wing Span: 69 ft 0 in
- Length: 68 ft 8 in
Interior
- Cabin Height: 6 ft 0 In
- Cabin Width: 7 ft 2 In
- Cabin Length: 25 ft 2 In
- Cabin Volume: 860 cu ft
Occupancy
- Crew: 2
- Passengers: 10
Operating Weights
- Max T/O Weight: 40600 Lb
- Max Landing Weight: 34150 Lb
- Operating Weight: 24800 Lb
- Fuel Capacity: 14150 lbs Lb
- Payload W/Full Fuel: 1800 Lb
- Max Payload: 3400 Lb
Range
- Max Range: 3200 nm
- Service Ceiling: 45000 ft
Distances
- Takeoff Distance: 4835 ft
- Landing Distance: 2364 ft
Performance
- Max Speed: 470 kts
- Economy Cruise: 459 kts
- Avionics: Rockwell Collins Pro Line 21 advanced suite
- 2019 List Price: $26,673,000
Power Plant
- Engines: 2
- Engine Mfg: Honeywell Engines
- Engine Model: HTF7350 turbofans
- Ex-works
- Valor de venda + impostos para nacionalização
Airframe
- Total Time 523.3
- Total Landings 243
- Winglets
- Maintenance Tracking FLightDocs
Engine 1
- Engine 1 Time 523.3 SNEW
- Engine 1 Cycles 243
Engine 2
- Engine 2 Time 523.3 SNEW
- Engine 2 Cycles 243
Auxiliary Power Unit
- APU
- APU Time 235.75
Avionics
- ADS-B Equipped
- FANS
- CPDLC
Avionics/Radios
- Rockwell Collins Pro Line 21 Advanced Avionics Suite
- Single Three-Axis Category II Automatic Flight Control Systems (AFCS)
- Two (2) VHF Comm Radios
- Two (2) HF Comm Radios
- Two (2) SELCAL Systems capable of monitoring two (2) HF and up to three (3) VHF radios
- One (1) dual channels interphone system with hand-held microphones and individual controls for pilot and co-pilot
- Electronic Flight Instrument System (EFIS)
- Engine Indication and Crew Awareness System (EICAS)
- Synchronized Digital GPS Clock
- Cockpit Voice Recorder
- Flight Data Recorder
- Emergency Locator Transmitter
- Two (2) Flight Management Systems (FMS)
- Two (2) Integrated Flight Information Systems (IFIS) (require subscription)
- One (1) Synthetic Vision System (SVS)
- Two (2) EFB class 1 tablet computers including Bombardier’s Flight Deck application (loose equipment)
- One (1) Electronic Integrated Standby Instrument (ISI)
- Two (2) Inertial Reference Systems (IRS)
- Two (2) Global Navigation Satellite System (GNSS) Satellite Based Augmentation System (SBAS) capable receivers
- Two (2) VHF Navigation Receivers
- Two (2) DME Transceivers
- One (1) Mode S Transponder capable of ADS-B Out in non-radar areas
- One (1) 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 (1) Radio Altimeter system
- One (1) Terrain Awareness and Warning System (TAWS)
Additional Equipment
- Datalink (VDL Mode 2), Controller-Pilot Datalink Communication (CPDLC) and Iridium Interface
- FANS1/A+ (CPDLC & ADS-C) and Inmarsat Satcom SwiftBroadband with Cockpit Safety Service / ACARS Communications
- Second Automatic Direction Finder (ADF)
- Enhanced Map Overlays
- SRSL (Smart Runway Smart Landing C34-500)
- RNP AR 0.3
- ANR to USA
- Air-to-Ground Cabin Connectivity Solution
- Dual LED Navigation Lights
Exterior
- Year Painted 2015
Interior
- Year Interior 2015
- Galley
- Galley Configuration Forward
- Lavatory
- Lavatory Configuration Aft
Inspection Status
- 12 Month Inspection complied with December 2020; next due December 2021
- 24 Month Inspection complied with December 2019; next due December 2021
- 36 Month Inspection complied with December 2018; next due December 2021
- 48 Month Inspection complied with November 2019; next due December 2023
- 96 Month Inspection due December 2023
- 192 Month Inspection due December 2031
- 600 Hour Inspection due @ 600 hours
- 800 Hour Inspection due @ 800 hours
- 1200 Hour Inspection due @ 1200 hours
- 1600 Hour Inspection due @ 1600 hours
- 2400 Hour Inspection due @ 2400 hours
- 3200 Hour Inspection due @ 3200 hours
- 4200 Hour Inspection due @ 4200 hours
- 9600 Hour Inspection due @ 9600 hours
- Landing Gear Inspection due December 2023
- Landing Gear Overhaul due December 2031
- LH & RH Engine MPI/HSI/Combust due @ 4800 engine hours
- LH & RH Engine OVH/CZI/Compress due @ 9600 engine hours
A aeronave acima é de terceiros, os dados estão sujeitos a verificação.
Exterior
- Exterior Height: 20 ft 0 in
- Wing Span: 69 ft 0 in
- Length: 68 ft 8 in
Interior
- Cabin Height: 6 ft 0 In
- Cabin Width: 7 ft 2 In
- Cabin Length: 25 ft 2 In
- Cabin Volume: 860 cu ft
Occupancy
- Crew: 2
- Passengers: 10
Operating Weights
- Max T/O Weight: 40600 Lb
- Max Landing Weight: 34150 Lb
- Operating Weight: 24800 Lb
- Fuel Capacity: 14150 lbs Lb
- Payload W/Full Fuel: 1800 Lb
- Max Payload: 3400 Lb
Range
- Max Range: 3200 nm
- Service Ceiling: 45000 ft
Distances
- Takeoff Distance: 4835 ft
- Landing Distance: 2364 ft
Performance
- Max Speed: 470 kts
- Economy Cruise: 459 kts
- Avionics: Rockwell Collins Pro Line 21 advanced suite
- 2019 List Price: $26,673,000
Power Plant
- Engines: 2
- Engine Mfg: Honeywell Engines
- Engine Model: HTF7350 turbofans
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