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AN28

From SKYbrary Wiki
Aircraft
Name An-28
Manufacturer PZL-MIELEC
Body Narrow
Wing Fixed Wing
Position High wing (wing struts)
Tail Double fin, mid set
WTC Light
APC A
Type code L2T
Engine Turboprop
Engine count Multi
Position (Front) Wing leading mounted
Landing gear Tricycle fixed
Mass group 3


Manufacturered as:

ANTONOV An-28
PZL-MIELEC M-28 Bryza
PZL-MIELEC An-28
PZL-MIELEC An-28 Bryza
PZL-MIELEC Bryza


PZL-MIELEC An-28

PZL-MIELEC An-28 PZL-MIELEC An-28 3D

Description

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 22.1 m72.507 ft
Length 13 m42.651 ft
Height 4.6 m15.092 ft
Powerplant An-28: 2 x 960 SHP Glushenkov TVD-103 turboprops with 3 blade propellers.

M-28: 2 x 1.100 SHP Pratt * Whitney Canada PT6A-65B turboprops with 5 blade propellers.

Engine model Glushenkov TVD-10, Pratt & Whitney Canada PT6

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) 80 kts IAS 110 kts IAS 140 kts IAS 140 kts MACH TAS 180 kts MACH IAS 170 kts IAS kts Vapp (IAS) 90 kts
Distance 400 m ROC 900 ft/min ROC 700 ft/min ROC 700 ft/min ROC ft/min MACH ROD ft/min ROD 800 ft/min MCS kts Distance 210 m
MTOW 65006,500 kg
6.5 tonnes
kg
Ceiling FL200 ROD ft/min APC A
WTC L Range 14001,400 nm
2,592,800 m
2,592.8 km
8,506,561.686 ft
NM

Accidents & Serious Incidents involving AN28

None on SKYbrary