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Ka-226 Hoodlum-C vs SW-4 Puszczyk

Ka-226 Hoodlum-C vs SW-4 Puszczyk at a glance — top speed 205 vs 260 km/h, range 600 vs 790 km, max takeoff weight 3,450 vs 1,800 kg, built 269 vs 40 units.

Specifications
Ka-226 Hoodlum-C SW-4 Puszczyk
Origin country 🇷🇺 Russia 🇵🇱 Poland
Category Military Helicopters Military Training Aircraft
Manufacturer Kamov PZL-Świdnik
First flight 4 September 1997 29 October 1996
Year introduced 2002 2002
Number produced 269 units 40 units
Average unit price -- $700K
Wingspan 13.0 m 9.0 m
Height 4.2 m 3.1 m
Length 8.1 m 10.6 m
Maximum speed 205 km/h 260 km/h
Operational range 600 km 790 km
Service ceiling 6,200 m 5,200 m
Max. takeoff weight 3,450 kg 1,800 kg
Empty weight 1,950 kg 1,050 kg
Total thrust 2 x 336 kW 1 x 336 kW
Performance Radar Chart
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Frequently Asked Questions

Which is faster, the Ka-226 Hoodlum-C or SW-4 Puszczyk?
The SW-4 Puszczyk is faster with a maximum speed of 260 km/h compared to the Ka-226 Hoodlum-C's 205 km/h, a difference of 55 km/h.
Which has longer range, the Ka-226 Hoodlum-C or SW-4 Puszczyk?
The SW-4 Puszczyk has a longer range at 790 km compared to the Ka-226 Hoodlum-C's 600 km.
Which can fly higher, the Ka-226 Hoodlum-C or SW-4 Puszczyk?
The Ka-226 Hoodlum-C has a higher service ceiling at 6,200 meters (20,341 ft) compared to the SW-4 Puszczyk's 5,200 meters (17,060 ft).
Which is heavier, the Ka-226 Hoodlum-C or SW-4 Puszczyk?
The Ka-226 Hoodlum-C has a higher maximum takeoff weight at 3,450 kg compared to the SW-4 Puszczyk's 1,800 kg.
Which is larger, the Ka-226 Hoodlum-C or SW-4 Puszczyk?
The SW-4 Puszczyk is longer at 10.6 meters compared to the Ka-226 Hoodlum-C's 8.1 meters.
Which entered service first, the Ka-226 Hoodlum-C or SW-4 Puszczyk?
Both the Ka-226 Hoodlum-C and SW-4 Puszczyk entered service in the same year: 2002.
Which has been built in greater numbers, the Ka-226 Hoodlum-C or SW-4 Puszczyk?
The Ka-226 Hoodlum-C has been produced in greater numbers with 269 units compared to 40 units of the SW-4 Puszczyk.