AN28
PZL-MIELEC An-28
PZL-MIELEC An-28
Aircraft
Name
An-28
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
High wing (wing struts)
Tail
Double fin, mid set
WTC
L
APC
A
Type Code
L2T
Engine
Turboprop
Engine Count
Multi
Position
(Front) Wing leading mounted
Landing gear
Tricycle fixed
Manufactured as
PZL-MIELEC M-28 Bryza
PZL-MIELEC An-28
PZL-MIELEC An-28 Bryza
PZL-MIELEC Bryza
ANTONOV An-28
AN28
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.
Technical Data
Wing span (metric)
22.10 m
Length (metric)
13.00 m
Height (metric)
4.60 m
Powerplant
An-28: 2 x 960 SHP Glushenkov TVD-103 turboprops with 3 blade propellers.
Engine Model(s)
Glushenkov TVD-10
Pratt & Whitney Canada PT6
Indicative Performance Data
Take-Off
V2
80 kts
Distance
400 m
MTOW
6500 kg
Initial Climb (to 5000 ft)
IAS
110 kts
ROC
900 ft/min
Initial Climb (to FL150)
IAS
140 kts
ROC
700
Initial Climb (to FL240)
IAS
140 kts
ROC
700 ft/min
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
180 kts
MACH
n/a
Ceiling
200
Range
1400 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
170 kts
ROD
800 ft/min
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
90 kts
Distance
210 m
