*****AIRCRAFT “Antonov - AN30”*****

REFERENCE INFORMATION (by Aircraft performance database)

 

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

Wing position:  High wing

Engine position: (Front) Wing leading mounted

Tail configuration: Regular tail, high set

Landing gear: Tricycle retractable

Wing Span: 29.2 m

Length: 24.3 m

Height: 8.3 m

Power plant: 2 x 2.820 SHP Ivchenko AI-24VT turboprops

with 4 blade propellers.

Accommodation: Flightcrew of 4 and up to 50 passengers.

Notes: Aerial survey and mapping aircraft. In service since the early seventies. Special version of An-24 with a glazing nose for survey and cartography is used by many countries in the open skies programme.

Can easely be turned into and is often used as an An-26 type transport.
Alternative names:
ANTONOV An-30.

 

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

000,000 lbs - 21.800 kg

VMO - Maximum Operating Speed 235 KIAS

MMO - Maximum Operating Speed Mach nd 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:   800 mt

V2 (IAS):   110 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:        140 kt

ROC:        1500 ft/min

-(to FL150)

IAS:        200 kt

ROC:        800 ft/min

-(to FL240)

IAS:        200 kt

ROC:        700 ft/min

-(mach)

mach:       na

ROC:        na ft/min

 

*****Cruise*****

TAS:        235 kt

MACh:       nd

Ceiling:    FL270

Range:      1400 NM

 

*****Descent *****

- (to FL240)

mach:       nd

ROD:        nd ft/min

- (to FL100)

IAS:        240 kt

ROD:        1500 ft/min

 

*****Approach*****

IAS:        150 kt

MCS:        nd kt

ROD:        1000 ft/min

 

*****Landing*****

Vht (IAS):  95 kt

APC:        B

Distance:   700 mt