FORCETALLY
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At a glance
Ilyushin Il-112larger figure on 5 of 7
Measured figures
Length
Single source24.15 m (79 ft 3 in)[source]
Length
Single sourceConfiguration
| Specification | Ilyushin Il-112 | Pilatus PC-24 |
|---|---|---|
| Type | Light military transport[source] | Light business jet[source] |
| National origin | Russia[source] | Switzerland[source] |
| Designer | Ilyushin[source] | — |
| Built by | Voronezh Aircraft Production Association[source] | — |
| Status | In development[source] |
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]
Maximum take-off; Max takeoff weight
Single source21,000 kg (46,297 lb)[source]
with 3,500 kg (7,700 lb) load
Single sourcewith max load
Single source2,400 km (1,500 mi, 1,300 nmi) with 3,500 kg (7,700 lb) load; 1,700 km (1,100 mi; 920 nmi) with max load[source]
6 passengers (1,200 lb payload)
Single sourceFerry; Ferry range
Single source2 × Klimov TV7-117ST turboprop each
Single source2 × Klimov TV7-117ST turboprop, 2,610 kW (3,500 hp) each[source]
2 × Williams FJ44-4A turbofans thrust each
Single source2 × Williams FJ44-4A turbofans , 15 kN (3,400 lbf) thrust each[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.
In production[source] |
| Primary user | Russian Aerospace Forces[source] | — |
|---|
| Number built | 2 Il-112V prototypes, only 1 flew[source] | 212 (Q1 2024)[source] |
|---|
| Introduction date | 2023 (planned)[source] | 1 April 2018[source] |
|---|
| First flight | 30 March 2019[source] | 11 May 2015[source] |
|---|
| Capacity | 5,000 kg (11,000 lb); 44 passengers[source] | 10 passengers[source] |
|---|
| Fuel capacity | 7,200 L (1,600 imp gal; 1,900 US gal)[source] | 2,705 kg (5,964 lb), 888.5 US gal (3,363 L)[source] |
|---|
| Propellers | 6-bladed constant-speed reversible pitch propellers[source] | — |
|---|
| Manufacturer | Voronezh[source] | Pilatus Aircraft[source] |
|---|
| Primary users | — | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] |
|---|
| Manufactured | — | 2015–present[source] |
|---|
| Aspect ratio | — | 9.35[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] |
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| Landing | — | 734 m; 2,408 ft (Over 50 ft obstacle, MLW, ISA, sea level, dry paved runway)[source] |
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