N360

Bombardier CL-600-2B16 Challenger 601-3A (601-3A)

Bombardier (Canadair)

8 Hours

Duration of Flight

3430 NM

Range

459 MPH

Max Speed

N360

Gallery

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Aircraft Class
Aircraft Class
Over 20,000lbs
Max passengers
Max passengers
22
Range
Range
3430 NM
Service Ceiling
Service Ceiling
41000 ft
Duration of Flight
Duration of Flight
8 Hours
Max Speed
Max Speed
459 MPH

Basic Information

Year Manufactured1990
Registration NumberN360
Serial Number5068

Airframe

Data valid as of 2025-11-26
AFTT (hrs)
Current
N/A
Flight
N/A
Est.
N/A
Landings/Cycles
Current
N/A
Flight
N/A
Est.
N/A
Nautical Miles
Current
N/A
Flight
N/A
Est.
N/A
DateFromToFlight TimeStatus
2016-03-16N/AN/AN/A✓ Landed
2013-10-04N/AN/AN/A✓ Landed
2012-03-11N/AN/AN/A✓ Landed

AI Summary

Fact-checked by AI

Bombardier CL-600-2B16 Challenger 601-3A (601-3A)

Overview

U.S. registration N360 — Bombardier CL-600-2B16 Challenger 601-3A, MSN 5068, built 1990.

Specifications

  • Engines: 2× General Electric CF34-3A (9220 lbf each)
  • Range: 3430 nm
  • Cruise: 442 kts
  • Seats: 22
  • Ceiling: 41000 ft

Operations & Cabin

Typical 8–12-place executive layout; forward galley, aft lavatory, internal baggage compartment Executive seating, forward galley, aft lav, cabin width ~8.2 ft and length ~28.3 ft (typical for 601-3A) Avionics: Typical Collins/Honeywell integrated Pro-Line/Primus-class suites (varies by retrofit)

Model & Market Context

This airframe, bearing federal registration N360, is a 1990-built example of the Bombardier CL-600-2B16 Challenger 601-3A with manufacturer serial number 5068. The airframe is registered in the US and carries a market valuation of $2,300,000, reflecting its age and installed systems. Detailed ownership timeline and operator history are not published for this specific airframe. Registry entries and condition highlights emphasize a typical late-production Challenger 601-3A life cycle: aging airframe economics with value driven by avionics retrofits and maintenance status.

The cabin in this airframe is fitted in a typical 8–12-place executive layout with a forward galley, aft lavatory, and internal baggage compartment, though the aircraft is certificated for 22 seats in other configurations. Avionics fit varies by retrofit but commonly includes Collins or Honeywell integrated Pro-Line/Primus-class suites. With a design range of 3,430 nm and cruise speeds around 442 kts, the aircraft is suited to transcontinental and medium long-range executive missions from U.S.-based operators; mission profiles typically include charter operations, corporate transport, and repositioning flights. Maintenance considerations for this airframe center on CF34-3A engine cycles and avionics retrofit history, both of which materially affect dispatch reliability and residual value.

The Challenger 601-3A occupies the large-cabin, medium long-range business jet niche, valued for its roomy cabin and solid performance at cruise speeds near 442 kts and a service ceiling of 41,000 ft. Competing models in this segment include later-generation Bombardier Challengers and large-cabin offerings from Gulfstream and Dassault; buyer and charter demand for 1990-vintage 601-3A airframes is driven largely by acquisition price and upgrade potential. Key resale and upkeep considerations for this specific serial involve age-related structural and interior refurbishment, CF34-3A life-limited component status, and the extent of avionics modernization performed during ownership, all of which influence the noted $2,300,000 valuation.

Aircraft Comparison

ParameterN360N116HLN154EA
Serial Number (MSN)506851137629
Year Manufactured199019922002
Duration of Flight8 Hours7 Hours4 Hours
Range3430 NM3000 NM1700 NM
Max Speed459 MPH459 MPH464 MPH
Aircraft ClassOver 20,000lbsOver 20,000lbsOver 20,000lbs
Service Ceiling41000 ft41000 ft41000 ft
Max Passengers221450
Cabin ComfortNo items found.No items found.No items found.

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