Credit
Artem Katranzhi from Bakashikha, Russia · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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Measured figures
Configuration
| Specification | Ilyushin Il-80 | Pilatus PC-24 |
|---|---|---|
| Crew | — | one or two[source] |
| Type | Airborne command post[source] | Light business jet[source] |
| Manufacturer | Ilyushin[source] | Pilatus Aircraft[source] |
| Status | In service[source] | In production[source] |
| Primary user |
Wingspan
Single source17.0 m (55 ft 9 in)[source]
Cruise; Cruise speed
Single source810 km/h (510 mph, 440 kn)[source]
2 × Williams FJ44-4A turbofans thrust each
Single source2 × Williams FJ44-4A turbofans , 15 kN (3,400 lbf) thrust each[source]
Wing area
Single source30.91 m 2 (332.6 sq ft)[source]
Maximum payload
Single source1,406 kg (3,100 lb)[source]
Service ceiling
Single source14,000 m (45,000 ft)[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.
Russian Aerospace Forces[source] |
| — |
| Number built | 212 (Q1 2024)[source] |
|---|
| Introduction date | 1992[source] | 1 April 2018[source] |
|---|
| First flight | 5 March 1987[source] | 11 May 2015[source] |
|---|
| Developed from | Ilyushin Il-86[source] | — |
|---|
| National origin | Russia[source] | Switzerland[source] |
|---|
| Source measurement | Unlike the standard Il-86 airliner, the Il-80 has two electrical generator pods mounted inboard of the engine nacelles . Each pod is approximately 9.5 metres (32 feet) long and 1.3 metres (4 feet) in diameter. Both pods include landing lights.[source]Ilyushin Il-80 · Development; only the objects and conditions stated in this passage When the present upgrades have reached the end of their life, it is expected that a new airborne command post, based on the Ilyushin Il-96-400M commercial aircraft and delivered as the so-called Doomsday plane , will replace them.[source]Ilyushin Il-80 · Replacement; only the objects and conditions stated in this passage As of 2011 three Il-80s remain in service. They are painted in the classic livery of Aeroflot , the Russian state airline; and carry international civilian registrations RA-86147, RA-86148, and RA-86149. The first Il-80, registration RA-86146, has been photographed without engines and is apparently out of service. As of 2011 the Il-80s remain based at Chkalovsky Airbase, located 30 km (19 mi) northeast of Moscow. The aircraft are rarely observed in operation, though at least one was seen at an air show .[source]Ilyushin Il-80 · Operation; only the objects and conditions stated in this passage | — |
|---|
| Primary users | — | Qatar Emiri Air Force PlaneSense Royal Flying Doctor Service[source] |
|---|
| Manufactured | — | 2015–present[source] |
|---|
| Capacity | — | 10 passengers[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] |
|---|