N25V

Canadair CL-600-1A11 Challenger 600

CANADAIR

7 Hours

Duration of Flight

2909 NM

Range

443 MPH

Max Speed

N25V

Gallery

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Aircraft Class
Aircraft Class
Over 20,000lbs
Max passengers
Max passengers
21
Range
Range
2909 NM
Service Ceiling
Service Ceiling
41000 ft
Duration of Flight
Duration of Flight
7 Hours
Max Speed
Max Speed
443 MPH

Basic Information

Year Manufactured0
LocationCarson City, NV, US
Registration NumberN25V
OwnershipRR AERO LLC
Serial Number1015

Airframe

Data valid as of 2022-12-22
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-600-1A11 Challenger 600

Overview

U.S. registration N25V (standard/transport). Registered to RR AERO LLC (Carson City, NV). Certificate issue date 2022-12-22; airworthiness date 2004-01-15; Mode S A25700.

Specifications

  • Engines: 2× Lycoming ALF502L (7500 lbf each)
  • Range: 2909 nm
  • Cruise: 425 kts
  • Seats: 21
  • Ceiling: 41000 ft

Operations & Cabin

Flexible executive layouts commonly 8–12 passengers (registry lists up to 21 seats in higher-density configs) Wide, stand-up cabin (approx. 6 ft 1 in high × 8 ft 2 in wide); multiple executive layout options Avionics: Original Sperry SPZ-600 analog flight guidance (many airframes later upgraded to modern suites)

Model & Market Context

This airframe, registered as N25V, is a CANADAIR-built Canadair CL-600-1A11 Challenger 600 with manufacturer serial number 1015. The aircraft is recorded in civil registry as U.S.-registered and is owned by RR AERO LLC, an LLC based in Carson City, NV, US; this ownership appears as the primary registered operator for the airframe. No public build year is provided in the supplied data, and there are no additional documented transfers or notable registry actions in the dataset beyond the current ownership record. Condition and valuation highlights are not published in the provided information.

The airframe's cabin is described as adaptable to flexible executive layouts, with typical operator configurations commonly seating eight to twelve passengers, although the registry lists up to 21 seats in higher-density configurations. The aircraft originally carried the factory Sperry SPZ-600 analog flight guidance avionics suite; many Challenger 600-series airframes have subsequently been retrofitted with modern avionics, and this airframe’s documented original fit is the Sperry SPZ-600 with later upgrades possible though not specified. Typical mission profiles for this model and configuration include medium‑ to long-range business transport and executive charter routes consistent with a 2,909 nm range and a cruise speed around 425 kts, operating from the owner’s home base in Carson City, NV, for regional to transcontinental flights. Maintenance considerations reflect the twin-engine layout and older-generation avionics baseline, which can influence retrofit and avionics modernization schedules.

The Canadair CL-600-1A11 Challenger 600 occupies a performance niche as a transcontinental business jet offering robust range and payload capacity relative to its era, driven by twin Lycoming ALF502L turbofan powerplants producing 7,500 lbf each. Competing models historically include other late‑1970s and 1980s wide‑cabin business jets, with buyer and charter demand favoring airframes maintained to modern avionics and cabin standards. From a maintenance and resale standpoint, the original analog Sperry SPZ-600 guidance fit and the potential for higher-density seating layouts are key considerations for prospective buyers and operators evaluating upgrade costs versus operational role.

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