Bombardier Learjet 75 vs Embraer Phenom 300E: Light Jet Comparison

The Bombardier Learjet 75 is a high-altitude light jet built for operators who prioritize a 51,000 ft service ceiling, strong transcontinental range, and lower hourly fuel burn over maximum cabin volume.

The Bombardier Learjet 75 (FAA Type Certificate T00008WI, certified November 14, 2013) is the final production variant of a lineage that defined light jet travel for six decades. Produced from 2013 through 2022, the Learjet 75 represents Bombardier's most refined interpretation of the narrow-body, high-performance configuration: twin Honeywell TFE731-40BR turbofans producing 3,850 lbf each, a service ceiling of 51,000 ft, and a maximum cruise speed of 465 KTAS. Exactly 137 examples were delivered before production ended.

Inside the cockpit, Bombardier equipped the Learjet 75 with the Garmin G5000 integrated avionics suite featuring three 14.1-inch touchscreen displays, dual flight management systems, synthetic vision technology, and integrated weather radar. The G5000 brought a genuinely modern glass cockpit to the type, simplifying crew workload and reducing the training burden associated with older analog Learjet variants.

The Learjet 75 carries 6,062 lbs (905 gallons) of fuel, enabling an NBAA IFR range of 2,026 nm with four passengers. That fuel load, combined with the TFE731's thrust curve, also underpins the type's altitude advantage: the aircraft can cruise above most weather and many lighter competitors at FL510, where the Mach 0.76 cruise number translates to 465 KTAS on a standard day.

Cabin pressurization runs at a 9.3 PSI differential, which holds the cabin at the equivalent of 8,000 ft pressure altitude even at maximum cruise altitude. That differential is among the highest in the light jet class and contributes meaningfully to passenger comfort on longer sectors. On the ground, the Learjet 75 requires 4,440 ft of runway (sea level, over a 50-ft obstacle at maximum weight), a characteristic that limits its accessibility to longer runways compared to lighter competitors.

Bombardier discontinued Learjet production in February 2022, citing long-term strategic refocus on the Challenger and Global families. The mature secondary market now carries a healthy inventory of 2013-2022 airframes, and the type benefits from a broad MRO network built over decades of Learjet support. Operators valuing a known quantity with high-altitude cruise performance and a lower acquisition cost relative to newer alternatives continue to find the Learjet 75 a compelling choice.

The Embraer Phenom 300E is a single-pilot certified light jet suited for operators who weight cabin volume, best-in-class baggage capacity, and short-field performance alongside coast-to-coast range.

The Embraer Phenom 300E (FAA Type Certificate A48EM, type designation EMB-505, EASA TCDS EASA.IM.A.158) is Embraer's continuously refined light jet, with the 300E variant first delivered March 29, 2018 and the enhanced 300E receiving triple ANAC/EASA/FAA certification in March 2020 with first delivery on June 26, 2020. It remains in production. The 300E is powered by two Pratt & Whitney Canada PW535E1 engines producing 3,478 lbf each and cruises at a maximum of 464 KTAS (Mach 0.80) - making it the first single-pilot certified jet to reach Mach 0.80.

The Phenom 300E holds a single-pilot type rating under the EMB-505 designation, a meaningful operational advantage for charter operators and owner-flown operations where reducing crew requirements cuts both cost and scheduling complexity. Maximum occupancy reaches 11, though 7-8 passengers is the typical charter configuration. The aircraft is certified under EASA TCDS EASA.IM.A.158, and FAA type certificate A48EM covers U.S. operations.

Embraer fitted the 300E with a Garmin G3000-based Prodigy Touch flight deck specifically optimized for single-pilot operation. The system includes a runway overrun awareness and alerting system (ROAAS), predictive windshear detection, synthetic vision technology, TCAS II collision avoidance, and weather radar with turbulence detection - safety features that exceed the minimum regulatory baseline for the class. The flight deck also features 40% longer pilot seat tracks, accommodating pilots up to 6 ft 4 in.

Cabin volume measures 425 cu ft - 31 cu ft more than the Learjet 75 despite the Phenom 300E being 2.5 ft shorter in cabin length. Baggage capacity reaches 84 cu ft split between forward and aft compartments, with 19 cu ft more than the Learjet 75. Wi-Fi is standard on new production aircraft, and the cabin management system integrates lighting, temperature control, and entertainment from a single interface. Under-seat storage includes 12-inch deep drawers with USB charging at each position.

Field performance is a defining strength of the type. A takeoff distance of 3,209 ft at sea level - 1,231 ft less than the Learjet 75 under comparable conditions - opens a wider range of secondary airports. At the other end, the landing distance of 2,212 ft over a 50-ft obstacle keeps the type flexible at destination airports with shorter usable runways. With active manufacturer support, a global authorized service center network of 185+ locations, and predictive maintenance analytics, the Phenom 300E offers an infrastructure suited to high-utilization operations.

On published NBAA IFR range, the two aircraft are statistically even: Learjet 75 at 2,026 nm with four passengers versus the Phenom 300E at 2,010 nm with five occupants. A 16 nm difference at comparable passenger loads is operationally irrelevant; route planning for both types will encounter the same city-pair limitations in the 2,000-2,050 nm band. Neither reaches Europe nonstop from the U.S. East Coast, and both comfortably handle transcontinental U.S. sectors.

At maximum cruise, the gap is equally narrow: 465 KTAS for the Learjet 75 versus 464 KTAS for the Phenom 300E - a 1 KTAS difference that disappears in any practical planning calculation. The more meaningful cruise number is long-range cruise, where the Learjet 75 holds 432 KTAS versus the Phenom 300E's 414 KTAS. On a 1,500 nm sector, that 18 KTAS difference saves roughly 9 minutes of block time - noticeable on high-frequency operations but not a decisive factor for occasional users.

The most consequential performance gap is service ceiling: 51,000 ft for the Learjet 75 versus 45,000 ft for the Phenom 300E. FL510 access allows the Learjet 75 to route above heavy commercial traffic layers on high-demand corridors, and the higher cabin pressure differential (9.3 PSI versus 6.15 PSI) sustains an equivalent cabin altitude of 8,000 ft at both aircraft's respective ceilings. At FL450, the Phenom 300E is operating at its maximum; the Learjet 75 can continue climbing another 6,000 ft to clear convective activity or optimize cruise fuel flow.

Takeoff performance reverses the advantage decisively. The Learjet 75 requires 4,440 ft to clear a 50-ft obstacle at sea level and maximum weight; the Phenom 300E needs only 3,209 ft - a 1,231 ft reduction. That gap matters most in hot-and-high environments or when accessing business aviation fields with 5,000-6,000 ft runway lengths. The Phenom 300E's lighter MTOW of 18,387 lbs (versus 21,500 lbs for the Learjet 75) contributes directly to this advantage, as does the lower wing loading at typical operating weights.

Fuel capacity gives the Learjet 75 more reserve: 6,062 lbs (905 gallons) versus the Phenom 300E's 5,424 lbs (807 gallons). At their respective cruise fuel burn rates of 195-210 gal/hr (Learjet 75) and 225-245 gal/hr (Phenom 300E), the Learjet 75 burns less fuel per hour and carries more of it - a combination that supports longer stage lengths and more flexibility when planning fuel stops on transcontinental routing.

Cabin geometry tells two different stories depending on the metric. The Learjet 75 has a longer cabin at 19.7 ft versus the Phenom 300E's 17.17 ft - a 2.5 ft advantage that allows a full double-club seating layout with fore-and-aft facing seat pairs separated by a credenza or work surface. The Phenom 300E offsets this length difference through wider internal proportions, resulting in a larger total cabin volume: 425 cu ft versus the Learjet 75's 394 cu ft. That 31 cu ft difference is the Phenom 300E's headline passenger comfort advantage.

Cabin width is effectively identical: 5.1 ft for the Learjet 75 and 5.08 ft for the Phenom 300E. Cabin height is also comparable at 4.9 ft and 4.92 ft respectively. In practice, both aircraft require passengers above average height to duck slightly when moving through the aisle, which is standard across the light jet class. The dimensional differences that matter most are in cabin volume and baggage capacity rather than width or height.

Baggage capacity favors the Phenom 300E substantially: 84 cu ft spread across forward and aft compartments versus 65 cu ft in the Learjet 75 (15 cu ft accessible in-flight plus 50 cu ft in a heated external hold). For groups traveling with golf equipment, ski bags, or substantial luggage, the Phenom 300E's 19 cu ft advantage is significant. The Learjet 75's in-flight accessible storage is a workflow benefit for shorter sectors where passengers want access to gear mid-flight.

Pressurization methodology creates a meaningful real-world difference. The Learjet 75's 9.3 PSI differential holds the cabin at 8,000 ft equivalent even at its FL510 ceiling, while the Phenom 300E operates at 6.15 PSI. Both aircraft set the same 8,000 ft cabin altitude target at their respective service ceilings - the higher differential in the Learjet 75 simply means the system works harder less often and provides more margin against outflow valve variation at extreme altitude.

The Phenom 300E's cabin technology integration is more current for new production: Wi-Fi is standard, the cabin management system handles lighting, temperature, and entertainment from a unified interface, and under-seat storage includes USB charging at each position. Learjet 75 connectivity relied on optional Inmarsat or Iridium satellite communications packages, meaning that connectivity capability depends heavily on the specific aircraft's option sheet. Buyers evaluating pre-owned examples of both types should verify installed avionics and cabin equipment rather than relying on model-year assumptions.

Both aircraft use Garmin platforms, but different generations. The Learjet 75 runs the Garmin G5000, featuring three 14.1-inch touchscreen primary flight displays with dual flight management systems, synthetic vision technology, and integrated weather radar. The G5000 was a significant upgrade over legacy Learjet avionics when the type launched in 2013, and it remains a capable, supportable platform with an established training ecosystem.

The Phenom 300E uses a Garmin G3000-based Prodigy Touch flight deck. Embraer and Garmin co-developed the integration specifically for single-pilot operations, adding systems that exceed the regulatory minimums for the class: ROAAS provides real-time runway overrun alerting, predictive windshear detection activates before the aircraft enters hazardous conditions, and TCAS II collision avoidance meets the latest ACAS X compatibility standards. The cockpit ergonomics received attention as well - pilot seat tracks extend 40% farther than the previous generation to accommodate a wider range of pilot builds.

The single-pilot certification on the Phenom 300E is both a regulatory achievement and a cockpit design outcome. The G3000 Prodigy integration was certified to allow one qualified EMB-505-rated pilot to conduct Part 135 operations without a co-pilot, a distinction that reduces direct operating costs for charter and corporate flight departments. The Learjet 75 requires two-crew operations regardless of mission profile.

For operators who fly primarily under Part 91 with a two-crew cockpit, the avionics generation gap matters less than the specific installed equipment on any given pre-owned airframe. The G5000 in the Learjet 75 supports all required navigation modes including RNP AR approaches, and Garmin's software update infrastructure has kept the platform current through database and capability updates. Neither aircraft should be disqualified on avionics grounds for standard IFR operations; the Phenom 300E's advantage is most pronounced in the safety enhancement features and single-pilot operational flexibility.

Fuel burn is the primary hourly cost driver where the two types diverge most clearly. The Learjet 75 burns approximately 195-210 gallons per hour at cruise; the Phenom 300E burns 225-245 gallons per hour. At an illustrative jet-A price of $6.50/gallon, the Learjet 75 costs roughly $1,268-$1,365/hr in fuel alone versus $1,463-$1,593/hr for the Phenom 300E - a gap of $195-$228/hr that compounds over annual utilization. At 400 flight hours per year, that difference represents $78,000-$91,000 in annual fuel cost.

Total direct operating costs run $3,100-$3,700/flight hour for the Learjet 75 and $3,300-$4,100/flight hour for the Phenom 300E when fuel, maintenance, and crew costs are aggregated. The broader range in the Phenom 300E reflects variability in single-pilot versus two-crew operations: single-pilot charter operations recover some fuel cost disadvantage by eliminating one crew position. Two-crew Phenom 300E operations carry a cost structure comparable to the upper range of Learjet 75 operating costs.

Maintenance structures are comparable in format, with both manufacturers offering structured inspection cycles and AOG support networks. Bombardier's support network for the Learjet family spans 150+ authorized service centers; Embraer's Phenom support network covers 185+ locations globally. The Phenom 300E benefits from active manufacturing support and predictive maintenance analytics on newer airframes, while the Learjet 75's mature secondary market has produced competitive independent MRO options that can reduce scheduled maintenance costs on pre-owned examples.

Acquisition pricing reflects the production status difference. Pre-owned Learjet 75 airframes from 2013-2022 trade in a range of roughly $4.2M-$9.5M depending on year, total time, and equipment. Phenom 300E pre-owned examples from 2015-2023 carry premiums, ranging from approximately $5.5M-$11.8M. Newer airframes of both types converge at the top of those ranges. Operators prioritizing lower entry cost for a capable light jet will generally find the Learjet 75 market more accessible, while those prioritizing new-production warranties and current avionics will pay the Phenom 300E premium.

Residual value trajectory differs by production status. The Learjet 75's fixed inventory (137 aircraft total) creates a predictable depreciation curve; values have shown roughly 40-45% depreciation over a 10-year holding period. The Phenom 300E's continued production means that new airframes continuously enter the pre-owned market, which can pressure pre-owned pricing for older examples but also means that manufacturer support programs, service bulletins, and avionics updates flow to the entire fleet continuously.

Choose the Bombardier Learjet 75 if altitude access is a core mission requirement. The 51,000 ft ceiling with a 9.3 PSI pressure differential is a genuine operational advantage on long sectors where routing above weather layers saves fuel and improves comfort. For operators flying primarily domestic U.S. routes at high frequency and prioritizing a lower acquisition cost for a proven platform, the Learjet 75 offers compelling value - particularly in the 2013-2017 vintage range where pricing reflects the type's end-of-production status rather than any operational limitation.

The Learjet 75 also has a lower hourly fuel burn: 195-210 gallons per hour versus 225-245 for the Phenom 300E. Over a full year of moderate utilization, that gap can offset a meaningful portion of any price premium in a competing aircraft. For corporate flight departments or charter operators who fly primarily two-crew and value a known, well-documented maintenance history, the Learjet 75 is the lower-risk selection.

Choose the Embraer Phenom 300E if cabin volume, baggage capacity, and field performance matter more than altitude ceiling. The 31 cu ft additional cabin volume and 19 cu ft baggage advantage affect every trip; the 51,000 ft ceiling advantage of the Learjet 75 affects primarily routes where FL510 is accessible and strategically useful. For operators accessing shorter runways or high-altitude airfields, the Phenom 300E's 3,209 ft takeoff distance and lower MTOW provide a practical margin that the Learjet 75 cannot match.

Single-pilot certification is the Phenom 300E's most structurally significant advantage for certain operators. Charter companies authorized for single-pilot Part 135 operations, and owner-pilots with EMB-505 type ratings, can reduce direct crew costs by approximately $150,000-$200,000 per year compared to two-crew operations. No avionics upgrade or maintenance optimization on the Learjet 75 can replicate that structural cost reduction.

For operators who fly both types of mission - long sectors where altitude matters, and short sectors into secondary airports - the choice comes down to which limitation is more tolerable. The Learjet 75 gives up field performance and cabin volume to gain altitude and lower fuel burn. The Phenom 300E gives up the upper altitude band and some cruise efficiency to gain a roomier cabin, superior baggage room, and short-field access. Neither aircraft is the wrong answer; the mission profile determines which trade-off fits.