FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Learjet 55larger figure on 2 of 6
Pilatus PC-24larger figure on 4 of 6
Measured figures
Length
Single source55 ft 1 in (16.80 m)[source]
Length
Single sourceConfiguration
| Specification | Learjet 55 | Pilatus PC-24 |
|---|---|---|
| Type | Business jet[source] | Light business jet[source] |
| National origin | United States[source] | Switzerland[source] |
| Manufacturer | Learjet[source] | Pilatus Aircraft[source] |
| Status | In service[source] | In production |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
16.85 m (55 ft 3 in)[source]
with four passengers and fuel reserves
Single source2,492 mi (4,010 km, 2,165 nmi) with four passengers and fuel reserves[source]
Maximum payload
Single source1,406 kg (3,100 lb)[source]
(3,960 ft/min) MTOW, at Sea level
Single source20.1 m/s (3,960 ft/min) MTOW, at Sea level[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 147[source] | 212 (Q1 2024)[source] |
|---|
| Manufactured | 1979–1987[source] | 2015–present[source] |
|---|
| Introduction date | 1981[source] | 1 April 2018[source] |
|---|
| First flight | 19 April 1979[source] | 11 May 2015[source] |
|---|
| Developed into | Learjet 60[source] | — |
|---|
| Capacity | 10[source] | 10 passengers[source] |
|---|
| Primary users | — | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] |
|---|
| Aspect ratio | — | 9.35[source] |
|---|
| Fuel capacity | — | 2,705 kg (5,964 lb), 888.5 US gal (3,363 L)[source] |
|---|
| Cabin | — | 7.01 m × 1.69 m × 1.55 m long × wide × high ( 23 ft 0 in × 5 ft 7 in × 5 ft 1 in)[source] |
|---|
| Cabin altitude | — | 2,438 m at 13,716 m (8,000 ft at 45,000 ft), 8.78 psi (0.605 bar)[source] |
|---|
| Stall speed | — | 154 km/h (96 mph, 83 kn)[source] |
|---|
| Time to altitude | — | 45,000 ft (14,000 m) 27.1 mins[source] |
|---|
| Wing loading | — | 259 kg/m 2 (53 lb/sq ft)[source] |
|---|
| Fuel consumption | — | 0.58 kg/km (2.1 lb/mi) Mach 0.72/416 kn (770 km/h) cruise, 15,375 lb (6,974 kg) weight, FL 450, ISA+3C[source] |
|---|
| Thrust/weight | — | 0.36[source] |
|---|
| Take-off | — | 942 m; 3,091 ft (MTOW, ISA, sea level, dry paved runway)[source] |
|---|
| Landing | — | 734 m; 2,408 ft (Over 50 ft obstacle, MLW, ISA, sea level, dry paved runway)[source] |
|---|
Maximum take-off; Max ramp weight
Single source