*****AIRCRAFT “Antonov – AN28”*****

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: 13.0 m

Height: 4.6 m

Power plant: An-28: 2 x 960 SHP Glushenkov TUD-103 turboprops

with 3 blade propellers. M-28: 2 x 1.100 SHP P&W PT6A-65B turboprops

with 5 blade propellers.

Accommodation: Flightcrew of two and typical 17 passengers, up to 20 in high density configuration.

Notes: Commuter airliner and utility transport aircraft. In limited service since 1986. Light passenger and utility transport development for short haul routes based on the An-14. The production was transferred to Polands PZL Mielec in 1978. Used by Polish Air Force and Navy. Westernised version M-28 Skytruck has been exported by Poland since 1996. New stretched, more powerful development of Antonov is the An-38.
Alternative names:
ANTONOV An-28, Bryza, M-28,Skytruck,Bryza, PZL-MIELEC An-28,M-28, Skytruck,Bryza, Skytruck
.

 

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

000,000 lbs - 6.500 kg

VMO - Maximum Operating Speed 170 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:        L

Distance:   400 mt

V2 (IAS):   80 kts

 

*****Climbing*****

-(to 5000 ft)

IAS:        140 kt

ROC:        1500 ft/min

-(to FL150)

IAS:        110 kt

ROC:        900 ft/min

-(to FL240)

IAS:        na kt

ROC:        na ft/min

-(mach)

mach:       na kt

ROC:        na ft/min

 

*****Cruise*****

TAS:        170 kt

MACh:       nd

Ceiling:    FL200

Range:      550 NM

 

*****Descent *****

- (to FL240)

mach:       nd

ROD:        nd ft/min

- (to FL100)

IAS:        170 kt

ROD:        800 ft/min

 

*****Approach*****

IAS:        170 kt

MCS:        nd kt

ROD:        800 ft/min

 

*****Landing*****

Vht (IAS):  90 kt

APC:        A

Distance:   210 mt