Credit
US Navy Employee · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Il-38 · Length
Single source40.185 m (131 ft 10 in)[source]
Length
Single sourceConfiguration
| Specification | Ilyushin Il-38 | Pilatus PC-24 |
|---|---|---|
| Crew | seven-eight[source] | one or two[source] |
| Type | Anti-submarine warfare and maritime patrol aircraft[source] | Light business jet[source] |
| Designer | Ilyushin[source] | — |
| Status | In limited service[source] | In production[source] |
| Primary users | Soviet Naval Aviation (historical) Russian Naval Aviation Indian Naval Air Arm (historical) |
16.85 m (55 ft 3 in)[source]
Il-38 · 4 × Ivchencko/ Progress AI-20M turboprop engines each
Single source4 × Ivchencko/ Progress AI-20M turboprop engines, 3,151 kW (4,225 hp) each[source]
2 × Williams FJ44-4A turbofans thrust each
Single source2 × Williams FJ44-4A turbofans , 15 kN (3,400 lbf) thrust each[source]
Il-38 · Endurance
Single source13 hours[source]
Maximum payload
Single source1,406 kg (3,100 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] |
| Number built | 58[source] | 212 (Q1 2024)[source] |
|---|
| Manufactured | 1967–1972[source] | 2015–present[source] |
|---|
| Introduction date | 1967[source] | 1 April 2018[source] |
|---|
| First flight | 28 September 1961[source] | 11 May 2015[source] |
|---|
| Developed from | Ilyushin Il-18[source] | — |
|---|
| Country of origin | Soviet Union[source] | — |
|---|
| Manufacturer | Ilyushin[source] | Pilatus Aircraft[source] |
|---|
| National origin | — | Switzerland[source] |
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| Capacity | — | 10 passengers[source] |
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| 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] |
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| Stall speed | — | 154 km/h (96 mph, 83 kn)[source] |
|---|
| Time to altitude | — | 45,000 ft (14,000 m) 27.1 mins[source] |
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| 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 takeoff weight
Single source