*****AIRCRAFT “Antonov - 38”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

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

Wing position: High wing (wing struts)

Engine position: (Front) Wing leading mounted

Tail configuration: Double fin, mid set

Landing gear: Tricycle fixed

Wing Span: 22.1 m

Length: 15.5 m

Height: 4.3 m

Power plant: 2 x 1.118 KW AlliendSignal TPE331-14GR-801E turboprops

with 5 blade propellers.

Accommodation: Flightcrew of two and up to 27 passengers.

Notes: Commuter airliner and utility transport. In limited service since 1997 in Russia (mainly Siberia). A Russian stretched developement of the AN-28.
Alternative names:
ANTONOV An-38.

 

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

000,000 lbs - 8.800 kg

VMO - Maximum Operating Speed 360 KIAS

MMO - Maximum Operating Speed Mach  0.55 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:        M

Distance:   500 mt

V2 (IAS):   100 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:        130 kt

ROC:        1000 ft/min

-(to FL150)

IAS:        160 kt

ROC:        1000 ft/min

-(to FL240)

IAS:        na kt

ROC:        na ft/min

-(mach)

mach:       na

ROC:        na ft/min

 

*****Cruise*****

TAS:        n200 kt

MACh:       nd

Ceiling:    FL140

Range:      800 NM

 

*****Descent *****

- (to FL240)

mach:       na

ROD:        na ft/min

- (to FL100)

IAS:        290 kt

ROD:        800 ft/min

 

*****Approach*****

IAS:        200 kt

MCS:        nd kt

ROD:        800 ft/min

 

*****Landing*****

Vht (IAS):  120 kt

APC:        B

Distance:   900 mt