Gulfstream G150 vs Cessna Citation XLS: A Straight Comparison
TL;DR:The Gulfstream G150 carries up to 8 passengers across 3,200 nm with a full-stand cabin and Rolls-Royce turbofan power, while the Cessna Citation XLS covers 2,230 nm in a lighter, more fuel-efficient airframe that costs significantly less to acquire and operate. Buyers choosing between them are really choosing between intercontinental reach and lean economics.
At-a-Glance Spec Comparison
| Spec | G150 | Citation XLS |
|---|---|---|
| FAA TCDS | A28 | T9 |
| EASA TCDS | A.28 | A.307 |
| Production Years | 2005-2009 | 2004-2013 |
| Engines | 2x Rolls-Royce AE3007A1E (4,750 lbf each) | 2x Williams FJ44-3A (3,460 lbf each) |
| Max Cruise Speed | 480 KTAS | 476 KTAS |
| Long-Range Cruise Speed | 414 KTAS | 407 KTAS |
| NBAA IFR Range | 3,200 nm (6 pax) | 2,230 nm (8 pax) |
| Service Ceiling | 43,000 ft | 43,000 ft |
| MTOW | 35,100 lbs | 20,000 lbs |
| Operating Empty Weight | 24,250 lbs | 11,750 lbs |
| Fuel Capacity | approx. 1,645 USG | 5,996 USG |
| Typical Fuel Burn | 275 gph | 165 gph |
| Takeoff Distance (SL, ISA) | 5,200 ft | 2,550 ft |
| Landing Distance | 2,600 ft | 1,920 ft |
| Cabin Length | 43.5 ft | 32.75 ft |
| Cabin Width | 7.42 ft | 5.33 ft |
| Cabin Height | 6.17 ft | 5.42 ft |
| Cabin Volume | 1,250 cu ft | 450 cu ft |
| Typical Seating | 6 passengers | 6 passengers |
| Maximum Seating | 8 passengers | 8 passengers |
| Baggage Volume | 85 cu ft | 28 cu ft (external pod available) |
| Baggage Capacity | 1,500 lbs | 500 lbs |
| Cabin Pressurization (FL430) | 6,000 ft cabin altitude | 8,000 ft cabin altitude |
| Standard Avionics | Honeywell Primus 1000NX | Garmin G1000 (pre-2011) / G3000 (2011+) |
| Estimated Used Price (mid) | $8.5M - $16.0M | $3.5M - $9.0M |
| Typical Annual Fixed Costs | ~$750,000 | ~$450,000 |
| Fleet Size (FAA Registry) | ~180 aircraft | ~750 aircraft |
Gulfstream G150 Overview
The Gulfstream G150 is a super-midsize business jet certificated by the FAA under Type Certificate Data Sheet A28 and by EASA under TCDS A.28. It was produced by Gulfstream Aerospace from 2005 through 2009, with a total fleet of roughly 180 aircraft on the FAA registry. The G150 traces its lineage to the Israel Aircraft Industries Galaxy and Astra, which Gulfstream acquired and extensively redesigned to carry the G-series designation and service standards.
Power comes from two Rolls-Royce AE3007A1E turbofans producing 4,750 lbf of thrust each. That engine is closely related to the powerplant used on the Embraer ERJ regional jet family, which gives it a deep parts and MRO network for a relatively low-production airframe. The G150 has a maximum takeoff weight of 35,100 lbs and carries approximately 1,645 US gallons of fuel, enabling its published NBAA IFR range of 3,200 nm with six passengers and reserves.
Top cruise speed is 480 KTAS at 25,000 ft, with a long-range cruise of 414 KTAS. The aircraft shares its 43,000 ft service ceiling with the Citation XLS, but gets there carrying considerably more fuel and airframe. At altitude, the G150 maintains a cabin altitude of 6,000 ft -- meaningfully lower than the XLS -- which reduces passenger fatigue on longer sectors.
From a runway-performance standpoint, the G150 requires 5,200 ft of runway at sea level under ISA conditions. That limits access at shorter regional airports and is a practical consideration for owners who frequently operate from general aviation fields with limited pavement. Landing distance of 2,600 ft is more lenient and fits within most business aviation destinations.
Gulfstream positioned the G150 as a premium alternative to the light-midsize segment, aiming it at owner-operators who needed transatlantic or coast-to-coast range without stepping up to the larger G200 or G280. With production ending in 2009, all flying examples are now well-aged platforms with established maintenance histories.
Cessna Citation XLS Overview
The Cessna Citation XLS is a midsize business jet certificated by the FAA under Type Certificate Data Sheet T9 and by EASA under TCDS A.307. Cessna produced it from 2004 through 2013 under the Textron Aviation group, resulting in a fleet of approximately 750 aircraft on the FAA registry -- one of the larger mid-cabin fleets in active service. The XLS is an evolution of the Citation Excel, which Cessna stretched and re-engined to improve hot-and-high performance.
Two Williams FJ44-3A turbofans provide 3,460 lbf of thrust each. The FJ44 family is among the most maintainable small turbofan engines in business aviation, with Textron Aviation service centers and Williams International MRO shops distributed widely across North America and Europe. The XLS has a maximum takeoff weight of 20,000 lbs and carries 5,996 USG of fuel.
Published NBAA IFR range is 2,230 nm with eight passengers and reserves -- shorter than the G150 by approximately 970 nm but achieved with a fuel burn of 165 gph, compared to 275 gph for the G150. On routes where the range is sufficient, the XLS delivers measurably lower trip costs. Max cruise is 476 KTAS at FL350 and long-range cruise is 407 KTAS, both within a few knots of the G150.
The XLS performs strongly at shorter runways. Its published sea-level takeoff distance of 2,550 ft is roughly half the G150's requirement, which opens access to a wide range of general aviation airports that the G150 cannot reliably serve. Landing distance of 1,920 ft reinforces that advantage. For charter operators and fractional programs serving diverse city-pairs, this field performance is operationally significant.
Avionics evolved during the production run. Aircraft built before 2011 received the Garmin G1000 glass cockpit, while 2011 and later models stepped up to the Garmin G3000 -- the same modern flight deck found in the newer HondaJet and Beechcraft King Air 360. This means the avionics generation on a specific XLS depends heavily on its build year, and buyers should inspect the avionics fit during due diligence.
The Citation XLS holds the strongest resale liquidity of any aircraft in the midsize category. Deep fleet depth, wide operator familiarity, and strong charter demand keep the market active and appraisal values predictable. Depreciation runs approximately 3-4% annually for 2010-2015 model year examples.
Range & Performance Compared
The G150's 3,200 nm NBAA IFR range versus the XLS's 2,230 nm creates a 970 nm gap -- roughly the difference between New York to Denver and New York to Dallas. In practical routing terms, the G150 can fly New York to London or Los Angeles to New York nonstop with a meaningful reserve. The XLS covers domestic US and intra-European routes comfortably, but transatlantic missions require a technical stop.
Both aircraft share an identical 43,000 ft service ceiling, which allows them to cruise above most weather and takes advantage of favorable winds at altitude. The speed numbers are also close: the G150's 480 KTAS versus the XLS's 476 KTAS are virtually indistinguishable on any trip under four hours. Over a 1,500 nm leg, the four-knot difference represents approximately eight minutes of flight time -- irrelevant in practice.
Where the two diverge sharply is in takeoff field length. The G150's 5,200 ft sea-level requirement is more than double the XLS's 2,550 ft. At high-altitude airports such as Aspen (KASE, elevation 7,820 ft) or Telluride (KTEX, elevation 9,070 ft), hot-and-high performance penalties are amplified further. The XLS's lighter airframe and runway flexibility are genuine operational advantages for operators who regularly serve mountain or short-field destinations.
The G150's heavier MTOW (35,100 lbs versus 20,000 lbs) is a byproduct of carrying significantly more fuel for its extended range mission. That fuel load enables the range advantage but also drives higher ramp fees, fuel truck time, and ferry costs for repositioning. For missions consistently under 2,000 nm, the extra fuel capacity on the G150 is largely dead weight.
Cabin altitude at cruise is one performance dimension that is often overlooked in spec comparisons. The G150 holds a 6,000 ft cabin altitude at FL430, while the XLS holds 8,000 ft at the same altitude. On a four-hour flight, 2,000 ft of differential cabin altitude is perceptible to passengers and meaningfully affects hydration, alertness, and comfort. This is a genuine differentiator favoring the G150 on longer missions.
Cabin & Interior Compared
The cabin dimensions between these two aircraft are not close. The G150 measures 43.5 ft in length, 7.42 ft in width, and 6.17 ft in height, producing a cabin volume of 1,250 cu ft. The XLS measures 32.75 ft in length, 5.33 ft in width, and 5.42 ft in height, for a cabin volume of 450 cu ft. That is a 2.8-to-1 ratio in usable cabin space -- a difference that is immediately obvious to anyone who boards both aircraft back to back.
The G150's 6.17 ft interior height allows most adults to stand fully upright throughout the cabin. The XLS at 5.42 ft requires most passengers to duck slightly when moving fore and aft, though seated comfort at the individual seat position is acceptable. For short sectors under two hours the distinction matters less; for domestic coast-to-coast or international flights the G150's stand-up headroom changes the passenger experience substantially.
Baggage capacity reflects the same structural gap. The G150 offers 85 cu ft with a 1,500 lb limit, while the XLS provides 28 cu ft and a 500 lb limit. Cessna addressed this by offering an optional external belly pod for the XLS, which adds volume but is not available at all service configurations and must be factored into weight-and-balance planning. Groups traveling with golf clubs, ski bags, or significant luggage for multi-day trips will find the XLS's baggage compartment a constraint.
Both aircraft configure for up to 8 passengers and typically fly 6, with two flight crew. In the G150, that typical 6-passenger configuration allows for a center aisle with room for club seating arrangements, a work surface, and still leaving generous floor space. In the XLS at 6 passengers, the cabin fills more completely and the narrower fuselage (5.33 ft versus 7.42 ft) limits side-by-side seating width.
The G150 includes an enclosed forward lavatory and a midcabin galley with microwave capability. The XLS positions its lavatory and compact galley at the rear. Neither configuration is inherently superior, but the G150's forward lav placement keeps the full length of the cabin available for seating, which some operators prefer for larger groups. Both aircraft support optional satellite connectivity, cabin displays, and satellite telephone -- all add-on rather than standard.
Noise levels are close: 77 dB for the G150 and 78 dB for the XLS. The one-decibel difference is acoustically insignificant, and both are well within the range expected of modern business jets at cruise. The G150 features independent left and right thermal zones for cabin temperature control, while the XLS uses single-zone control -- a minor distinction for small groups but occasionally relevant when passengers have differing comfort preferences.
Avionics & Cockpit Technology
The G150 is equipped with the Honeywell Primus 1000NX integrated avionics suite. This is a glass cockpit system featuring multi-function displays, an integrated flight management system, Honeywell TAWS-B terrain awareness, and integrated weather radar. The autopilot operates on three axes and is coupled to the FMS, enabling coupled RNAV approaches and automatic altitude capture. For its production era, the Primus 1000NX represented a competitive and capable integrated package.
The Honeywell suite in the G150 is a fixed architecture -- there is no factory upgrade path to a Garmin or Rockwell Collins system without significant supplemental type certificate work. Operators evaluating used G150s should budget for avionics currency, particularly for ADS-B Out compliance, WAAS LPV approach capability, and any data-link additions. These are achievable through supplemental type certificates but add to acquisition cost.
The Citation XLS avionics picture is split by build year. Pre-2011 aircraft came with the Garmin G1000, a capable two-display glass cockpit with integrated weather and terrain. Aircraft built from 2011 onward received the Garmin G3000, a wider-screen touchscreen-based integrated avionics suite with superior situational awareness displays, improved FMS with wireless data loading, and synthetic vision. When evaluating specific XLS serial numbers, confirming the avionics generation is a due-diligence priority.
Garmin's installed base in business aviation is substantially larger than Honeywell's for this aircraft class, which has support infrastructure implications. Garmin avionics database subscriptions, software updates, and technically-trained maintenance personnel are available at a wider range of service locations than Honeywell Primus support. For operators who travel internationally or use diverse maintenance providers, this is a practical consideration.
Both cockpits require a specific type rating for each aircraft, and neither type rating is shared directly with a common pool. The G150 type rating documentation notes convertibility from Citation X experience in the research data, though crew qualification should always be verified against current FAA and EASA requirements. The XLS type rating is among the more widely held in the midsize category given the fleet depth, which supports pilot hiring and replacement staffing.
Operating Cost Context
Fuel burn is the most direct operating cost difference between these two aircraft. At 275 gph for the G150 versus 165 gph for the XLS, the G150 burns 67% more fuel per hour at typical cruise. On a 2,000 nm leg at long-range cruise -- approximately 4.8 hours of flight time at 414 KTAS for the G150 -- the G150 burns roughly 1,330 gallons versus the XLS's 810 gallons over the same distance, a difference of approximately 520 gallons. At $6 per gallon of Jet-A -- a figure that varies by location and contract pricing -- that represents roughly $3,100 in additional fuel cost per trip.
Annual fixed costs compound that difference. The G150 runs approximately $750,000 per year in fixed costs covering crew compensation, maintenance reserves, insurance, and hangar. The XLS runs approximately $450,000. That $300,000 annual spread is meaningful for an owner-operator flying 200-300 hours per year -- it represents a cost per trip overhead that needs to be weighed against the range and cabin advantages the G150 provides.
Acquisition cost reinforces the economic gap. Used G150 pricing ranges from $8.5M at the low end to $16.0M for well-equipped recent examples, with mid-market values around $12.5M. The XLS ranges from $3.5M to $9.0M with mid-market values around $6.0M. The delta in acquisition cost alone -- approximately $6.5M at mid-market values -- represents a substantial capital commitment, and the financing cost on that difference further widens the effective operating cost gap.
Maintenance programs follow similar patterns for both aircraft. Both G150 and XLS operate on 3,600-hour major inspection intervals. Gulfstream service centers support the G150, while Textron Aviation service centers support the XLS, with both networks reasonably distributed across North America. The XLS benefits from greater fleet volume, which tends to drive more competitive labor rates and parts availability compared to the smaller G150 fleet.
Charter revenue potential adds another dimension for operators who place their aircraft on a charter certificate. The XLS's strong demand as a charter platform -- driven by its fleet size, pilot familiarity, and attractive per-leg economics for operators -- typically supports higher utilization than the G150, which is more commonly owner-operated. A G150 on a charter certificate in a competitive market may face more difficulty filling legs than an XLS in the same market.
Which One Should You Choose?
The Gulfstream G150 is the right choice when route network includes transatlantic or extended transcontinental missions that exceed 2,500 nm nonstop, when cabin size for six to eight passengers over multi-hour sectors is a priority, and when a lower cabin altitude at cruise translates directly to passenger experience expectations. The G150's 85 cu ft of baggage space and its stand-up headroom represent a meaningful step up in operational capability that the XLS cannot match on those dimensions.
The Citation XLS is the right choice when the mission profile stays within 2,200 nm -- which covers the vast majority of US domestic city-pairs and most intra-European sectors -- and when acquisition cost, fuel burn, and annual fixed costs are active constraints. The XLS's 2,550 ft takeoff requirement opens airport access that the G150 cannot serve, and for operators with diverse field profiles that advantage recurs on every trip.
Fleet depth matters beyond the individual aircraft. With approximately 750 XLS aircraft on the FAA registry versus roughly 180 G150s, the XLS has a substantially deeper support ecosystem: more available type-rated pilots, more parts inventory in the distribution chain, more maintenance shops with direct experience, and a more active used market with tighter bid-ask spreads. For a first-time buyer or a smaller flight department without deep established vendor relationships, that depth reduces operational risk.
Budget-constrained buyers who want Gulfstream branding and longer range at the lowest possible entry point will find the G150 acquisition cost ($8.5M entry) still meaningfully higher than a comparable XLS ($3.5M entry). The G150's higher fuel burn, annual fixed cost premium, and smaller support network mean the total cost of ownership gap widens further over a typical five-year holding period. That math only works in the G150's favor when the missions genuinely require what only the G150 can deliver.
Both aircraft are certificated to 43,000 ft, carry up to 8 passengers, and cruise within a few knots of each other. For a buyer who needs to pick one, the decision almost always comes down to mission range and budget -- not speed, not seating count, not service ceiling. Define the longest nonstop mission that will be flown with any regularity, and if it exceeds 2,200 nm nonstop, the G150 earns its cost premium. If it does not, the Citation XLS delivers the same travel experience at a lower price on every dimension.
Gulfstream G150 For Sale
The Gulfstream G150 is a super-midsize business jet powered by two Rolls-Royce AE3007A1E turbofans, with a 3,200 nm NBAA IFR range, a stand-up cabin measuring 43.5 ft long and 7.42 ft wide, and a 6,000 ft cabin altitude at FL430. Production ran from 2005 to 2009.
Cessna Citation XLS For Sale
The Cessna Citation XLS is a midsize business jet powered by two Williams FJ44-3A turbofans, with a 2,230 nm NBAA IFR range, a fuel burn of 165 gph at cruise, and a 2,550 ft sea-level takeoff distance. Production ran from 2004 to 2013 with over 750 aircraft delivered.
Frequently Asked Questions
What is the range difference between the Gulfstream G150 and the Citation XLS?
The G150 has a published NBAA IFR range of 3,200 nm with six passengers and reserves. The Citation XLS is rated at 2,230 nm with eight passengers and reserves. That is a 970 nm gap, sufficient to make the G150 capable of nonstop transatlantic routes that the XLS cannot cover without a technical stop.
Can the Citation XLS fly coast to coast nonstop?
On many US coast-to-coast routes, yes. New York to Los Angeles is approximately 2,450 nm great-circle, which can push the XLS's 2,230 nm NBAA IFR range depending on winds, payload, and reserves. With favorable westerly tailwinds on the eastbound leg, the mission is typically feasible. Westbound against headwinds, a fuel stop in the Midwest is often required. Buyers flying that route regularly should verify performance with specific weight-and-balance analysis.
Which aircraft has better field performance at short or high-altitude airports?
The Citation XLS holds a significant advantage. Its published sea-level takeoff distance of 2,550 ft compares to 5,200 ft for the G150. At high-elevation airports such as Aspen or Telluride, the XLS's lighter airframe handles performance penalties more favorably. The XLS also has a shorter landing distance of 1,920 ft versus 2,600 ft for the G150.
How much larger is the G150 cabin compared to the Citation XLS cabin?
The G150 cabin measures 43.5 ft long, 7.42 ft wide, and 6.17 ft tall for a volume of 1,250 cu ft. The XLS measures 32.75 ft long, 5.33 ft wide, and 5.42 ft tall for 450 cu ft. The G150's cabin is approximately 2.8 times larger by volume, and its 6.17 ft height allows most adults to stand fully upright throughout.
What avionics does the Gulfstream G150 use?
The G150 is equipped with the Honeywell Primus 1000NX integrated glass cockpit, which includes a three-axis autopilot coupled to the FMS, integrated weather radar, and Honeywell TAWS-B terrain awareness. The architecture is fixed from the factory; upgrades to current-generation Garmin or Rockwell Collins systems require supplemental type certificate work.
Does the Citation XLS have Garmin avionics?
It depends on the build year. Citation XLS aircraft produced before 2011 were delivered with the Garmin G1000 glass cockpit. Aircraft built from 2011 onward received the Garmin G3000, a more capable touchscreen-based suite with synthetic vision and improved FMS functionality. Confirming the avionics generation of a specific serial number is an important step in the evaluation process.
How do the fuel burn rates compare between the G150 and XLS?
The G150 burns approximately 275 gallons per hour at typical cruise conditions, while the XLS burns approximately 165 gallons per hour. The G150 uses 67% more fuel per hour. On a 2,000 nm leg, that translates to roughly 520 additional gallons for the G150 -- a trip cost difference of approximately $3,100 at $6 per gallon, varying by location and contract pricing.
Which aircraft is more common on the used market?
The Citation XLS is significantly more common. There are approximately 750 XLS aircraft on the FAA registry versus roughly 180 G150s. The XLS's greater fleet depth means more frequent transaction data, tighter appraisal accuracy, more pilot-qualified buyers, and generally shorter time-to-sell. Average XLS resale velocity is 1-3 months, compared to 2-4 months for the G150.
What is the cabin pressurization difference between the two aircraft?
At a cruise altitude of 43,000 ft, the G150 maintains a cabin altitude of 6,000 ft, while the XLS holds a cabin altitude of 8,000 ft. The G150's lower cabin altitude reduces passenger fatigue and dehydration on longer sectors. On short trips under two hours the difference is minor; on legs exceeding four hours it is perceptible.
What type of buyer is best suited for each aircraft?
The G150 suits owner-operators or flight departments with regular mission requirements exceeding 2,200 nm nonstop, groups of 6-8 passengers who value a stand-up cabin and lower cabin altitude, and buyers willing to absorb higher fuel burn and annual fixed costs in exchange for range and interior space. The XLS suits charter operators, small flight departments, and cost-conscious buyers whose missions consistently stay within 2,000-2,200 nm, particularly those who value runway flexibility and a deep maintenance network.





