*****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:
Length:
Height:
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*****
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
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