N828WG
Bombardier CL-600-2B16 Challenger 601-3A (601-3A)
Bombardier (Canadair)
8 Hours
Duration of Flight
3430 NM
Range
459 MPH
Max Speed

Gallery




Basic Information
Airframe
Data valid as of 2022-10-31| Date | From | To | Flight Time | Status |
|---|---|---|---|---|
| 2025-11-07 | N/A | N/A | N/A | ✓ Landed |
| 2025-10-27 | N/A | N/A | N/A | ✓ Landed |
| 2025-08-05 | N/A | N/A | N/A | ✓ Landed |
| 2025-07-07 | N/A | N/A | N/A | ✓ Landed |
AI Summary
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
| Parameter | N828WG | N116HL | N154EA |
|---|---|---|---|
| Serial Number (MSN) | 5080 | 5113 | 7629 |
| Year Manufactured | 1991 | 1992 | 2002 |
| Duration of Flight | 8 Hours | 7 Hours | 4 Hours |
| Range | 3430 NM | 3000 NM | 1700 NM |
| Max Speed | 459 MPH | 459 MPH | 464 MPH |
| Aircraft Class | Over 20,000lbs | Over 20,000lbs | Over 20,000lbs |
| Service Ceiling | 41000 ft | 41000 ft | 41000 ft |
| Max Passengers | 22 | 14 | 50 |
| Cabin Comfort | No items found. | No items found. | No items found. |