Ilyushin Il-14 #6Risultati immagini per ilyushin il 14

 

*****AIRCRAFT “Ilyushin – IL 14”*****

REFERENCE INFORMATION (by Wikipedia)

 

*****Aircraft Features*****

Wing position: Low wing

Engine position: (Front) Wing leading mounted

Tail configuration: Regular tail, mid set

Landing gear: Tricycle retractable

Wing Span: 31.7 m

Wing Surface: 99,7

Length: 22.30 m

Height: 7.90 m

Power plant: 2 radial engines Shvetsov ASh-82T on two support, air cooled. Power 1.417 kW/ 1900 HP

Flightcrew of 3-4 and typical 24-28 passengers 3400 kg of freight

 

Notes: L'Ilyushin Il-14 (nome in codice NATO Crate) era un aereo da trasporto progettato dall'OKB 39 diretto da Sergej Vladimirovič Il'jušin e sviluppato in Unione Sovietica nei tardi anni quaranta.

Realizzato per soddisfare una richiesta della compagnia aerea nazionale Aeroflot per sostituire i Li-2 ed IL-12. Benché destinato principalmente all'aviazione civile venne utilizzato anche in ambito militare dalle forze aeree dell'Unione Sovietica e di molti stati aderenti al Patto di Varsavia o filocomunisti.

Volò per la prima volta il 13 luglio 1950

 

*****Total Flight Simulator aircraft weight with full fuel*****  

000,000 lbs - 18.000 kg

VMO - Maximum Operating Speed 225 Kt

MMO - Maximum Operating Speed Mach  0.00 Mach

Turbulent Air Penetration Speed   000 KIAS/.00 Mach

VLO - Maximum Gear Operating Speed   000 KIAS

VLE - Maximum Landing Gear Extension Speed   000 KIAS/.00 Mach

 

*****Maximum Flap Placard Speeds*****

Flaps degrees KIAS

1                      000

2                      000

5                      000

10                    000

15                    000

25                    000

30                    000

40                    000

 

*****Take-off*****

WTC:               -

Distance:         0000 mt

V2 (IAS):         000 kts

 

*****Climbing*****

Rate:    5 m/s   300 m/min

                        3.28 ft/s           590 ft/min       

 

-(to 5000 ft)

IAS:                 000 kt

ROC:               0000 ft/min

-(to FL150)

IAS:                 000 kt

ROC:               0000 ft/min

-(to FL240)

IAS:                 000 kt

ROC:               0000 ft/min

-(mach)

mach:              nd

ROC:               nd ft/min

 

*****Cruise*****

TAS max:         417 km/h (225 kts)

MACh:             0.34 data

Ceiling:            FL240 (7 400 m - 24 280 ft)

Range:             1 305 km (705 nmi) full load

 

*****Descent *****

- (to FL240)

mach:              nd

ROD:               nd ft/min

- (to FL100)

IAS:                 000 kt

ROD:               0000 ft/min

 

*****Approach*****

IAS:                 000 kt

MCS:               000 kt

ROD:               0000 ft/min

 

*****Landing*****

Vht (IAS):        000 kt

APC:                -

Distance:         000 mt