N828WG

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

Bombardier (Canadair)

8 Hours

Duration of Flight

3430 NM

Range

459 MPH

Max Speed

N828WG

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 Manufactured1991
LocationAnchorage, AK, US
Registration NumberN828WG
OwnershipWG AERO LLC
Serial Number5080

Airframe

Data valid as of 2022-10-31
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
2025-11-07N/AN/AN/A✓ Landed
2025-10-27N/AN/AN/A✓ Landed
2025-08-05N/AN/AN/A✓ Landed
2025-07-07N/AN/AN/A✓ Landed

AI Summary

Fact-checked by AI

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

Overview

Assigned (transport/standard). Certificate issue: 2020-03-18; Airworthiness date: 1991-06-28; Last action: 2022-10-31; Expiration: 2026-03-31.

Specifications

  • Engines: 2× General Electric CF34 (CF34-3A typical) (9140 lbf each)
  • Range: 3430 nm
  • Cruise: 442 kts
  • Seats: 22
  • Ceiling: 41000 ft

Operations & Cabin

Typical 9–12-place executive layout with forward galley and aft lavatory (operator-specific) Forward service galley, enclosed aft lavatory, executive club seating; interior fit varies by operator/refit. Avionics: Collins Pro Line II / common Honeywell retrofit options (typical for 601-3A)

Model & Market Context

This entry covers the specific airframe bearing registration N828WG, a 1991-built Bombardier (Canadair) business jet with serial number 5080. The airframe is a Bombardier CL-600-2B16 Challenger 601-3A and is recorded as owned by WG AERO LLC, an LLC based in Anchorage, AK, US; the registration is United States. The airframe’s current ownership is documented to WG AERO LLC in Anchorage, and valuation records list the aircraft at $1,554,222, reflecting its market position as an early-1990s Challenger variant in present condition.

The cabin of this Challenger 601-3A is noted as a typical 9–12-place executive layout with a forward galley and aft lavatory, though the airframe’s seating configuration is listed at 22 seats and may reflect supplemental or alternate operator-specific arrangements. Avionics fit on this model is typically Collins Pro Line II with common Honeywell retrofit options for 601-3A examples, a configuration referenced for this airframe’s type equipment. Based from Anchorage under its registered owner, operations for this airframe are suited to long-range executive missions across the North American and transcontinental sectors, exploiting the Challenger’s 3,430 nm range and high-cruise capability. Maintenance considerations for this airframe type center on CF34 engine commonality and avionics retrofit paths when modernizing Pro Line II-equipped cockpits.

The Bombardier CL-600-2B16 Challenger 601-3A occupies a mid-size long-range business jet niche offering transcontinental performance, with a cruise speed around 442 kts and a service ceiling of 41,000 ft. Competing models in its era and aftermarket include other mid-size heavy-cabin jets where buyer demand is driven by cabin comfort and range rather than ultra-modern avionics; typical market considerations for this airframe include CF34 engine maintenance status, avionics upgrade costs, and the airframe’s 1991 build year when assessing resale value and operational economics.

Aircraft Comparison

ParameterN828WGN116HLN154EA
Serial Number (MSN)508051137629
Year Manufactured199119922002
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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