N951RM

Canadair CL-600-2A12 Challenger 601 (601)

CANADAIR LTD

8 Hours

Duration of Flight

3370 NM

Range

476 MPH

Max Speed

N951RM

Gallery

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Aircraft Class
Aircraft Class
Over 20,000lbs
Max passengers
Max passengers
22
Range
Range
3370 NM
Service Ceiling
Service Ceiling
41000 ft
Duration of Flight
Duration of Flight
8 Hours
Max Speed
Max Speed
476 MPH

Basic Information

Year Manufactured1985
LocationNew York, NY, US
Registration NumberN951RM
OwnershipSIILATS KEITH
Serial Number3042

Airframe

Data valid as of 2024-10-30
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
No flights

No flight history available

Flight records for this aircraft have not been tracked yet.

AI Summary

Fact-checked by AI

Canadair CL-600-2A12 Challenger 601 (601)

Overview

U.S. registration (standard/transport). Certificate issue 2024-10-30; airworthiness entry 2004-08-27; FAA Mode S hex AD39E1 listed on registry-derived summaries.

Specifications

  • Engines: 2× GE CF34-3A (9220 lbf each)
  • Range: 3370 nm
  • Cruise: 443 kts
  • Seats: 22
  • Ceiling: 41000 ft

Operations & Cabin

Typical executive 10–12-place layout (stand-up cabin ~28 ft); forward galley and aft lavatory commonly installed. Forward galley; aft lavatory; interior fit varies by completion (typical executive fit 10–12 seats, max certificated up to 19–22 depending on layout).

Model & Market Context

This entry documents a specific airframe, the Canadair-built business jet bearing tail number N951RM, a serial 3042 completed in 1985. The airframe is a Canadair CL-600-2A12 Challenger 601 manufactured by CANADAIR LTD and currently registered in the United States. Ownership is recorded to individual owner SIILATS KEITH of New York, NY, US, and the airframe remains US-registered; no additional registry actions or operator changes are published. Condition and market valuation details are Not published.

The cabin for this airframe conforms to a typical executive arrangement described as a 10–12-place stand-up cabin approximately 28 ft in length, with a forward galley and an aft lavatory commonly installed; the listed seating capacity for the airframe is 22. Specific avionics fitment and recent maintenance records are Not published, so operator-specific equipment and certification status are not detailed here. Typical missions consistent with the platform and the listed range and cruise performance would include transcontinental and medium international hops from a New York base; the registered owner’s location in New York, NY, US suggests operations centered on that region. No unique aftermarket amenities or exceptional maintenance considerations for this particular serial are published.

The airframe is a member of the Challenger 601 family, a twin‑engine business jet class known for its stand-up cabin and transcontinental performance niche reflected in the 3,370 nm range and 443 kt cruise listed for this aircraft. Competing models in the marketplace historically include other late‑generation midsize cabin business jets offering similar range and comfort; buyer and charter demand tends to favor airframes with complete maintenance records and up‑to‑date avionics, which are Not published for this unit. Resale and maintenance considerations for this serial should therefore emphasize verifiable logbooks and regulatory status given the aircraft’s 1985 build year.

Aircraft Comparison

ParameterN951RMN113SRN139LJ
Serial Number (MSN)304251645025
Year Manufactured198519941988
Duration of Flight8 Hours9 Hours8 Hours
Range3370 NM4119 NM3430 NM
Max Speed476 MPH488 MPH459 MPH
Aircraft ClassOver 20,000lbsOver 20,000lbsOver 20,000lbs
Service Ceiling41000 ft41000 ft41000 ft
Max Passengers222222
Cabin ComfortNo items found.No items found.No items found.

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