PZ04

PZL-OKECIE PZL-104 Wilga

Aircraft
Name
PZL-104 Wilga
Manufacturer
Body
Narrow
Wing
Fixed Wing
Position
High wing
Tail
Regular tail, high set
WTC
L
APC
A
Type Code
L1P
Engine
Piston
Engine Count
Single
Position
Nose mounted
Landing gear
Tailwheel fixed
Manufacturered as
PZL-OKECIE Wilga 35
PZL-OKECIE Wilga 80
PZL-OKECIE PZL-104 Wilga 80
PZL-OKECIE PZL-104 Wilga 35
LIPNUR Gelatik

PZ04

Light utility aircraft. In service since 1967. Polands most successful light aircraft development. More than 960 aircraft were built. Flat piston engined version PZL-104 Wilga 2000. Mostly used for agricultural and glider towing purposes.

Technical Data
Wing span (metric)
11.10 m
Length (metric)
8.10 m
Height (metric)
2.90 m
Powerplant

1 x 260 HP PZL IAI-14RA radial piston engine with 2 blade propeller.

Indicative Performance Data
Take-Off
V2
45 kts
Distance
120 m
MTOW
1300 kg
Initial Climb (to 5000 ft)
IAS
75 kts
ROC
900 ft/min
Initial Climb (to FL150)
IAS
22 kts
ROC
100
Initial Climb (to FL240)
IAS
22 kts
ROC
100 ft/min
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
80 kts
MACH
n/a
Ceiling
130
Range
275 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
80 kts
ROD
500 ft/min
Descent (FL100 & below)
IAS
n/a
MCS
40 kts
ROD
n/a
Approach
Vapp (IAS)
50 kts
Distance
100 m

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