8.2mT-41C · Length
9.3mPZL-130TC II Orlik · Length
LengthScopes differ
All recorded figures & sources
8.2 mT-41C · Length
Single source 26 ft 11 in (8.20 m)[source]
9.3 mPZL-130TC II Orlik · Length
Single source 9.3 m (30 ft 6 in)[source]
10.92mT-41C · Wingspan
10mPZL-130TC II Orlik · Wingspan
WingspanScopes differ
All recorded figures & sources
10.92 mT-41C · Wingspan
Single source 35 ft 10 in (10.92 m)[source]
10 mPZL-130TC II Orlik · Wingspan
Single source 10 m (32 ft 10 in)[source]
2.69mT-41C · Height
3.53mPZL-130TC II Orlik · Height
HeightScopes differ
All recorded figures & sources
2.69 mT-41C · Height
Single source 8 ft 10 in (2.69 m)[source]
3.53 mPZL-130TC II Orlik · Height
Single source 3.53 m (11 ft 7 in)[source]
1.1tGross; T-41C · Gross weight
3t
MassScopes differ
All recorded figures & sources
618 kgEmpty; T-41C · Empty weight
Single source 1,134 kgGross; T-41C · Gross weight
Single source 1,363 lb (618 kg)[source]
2,500 lb (1,134 kg)[source]
1,825 kgEmpty; PZL-130TC II Orlik · Empty weight
Single source 2,400 kgGross; PZL-130TC II Orlik · Gross weight
Single source 2,950 kgMaximum take-off; PZL-130TC II Orlik · Max takeoff weight
Single source 1,825 kg (4,023 lb)[source]
2,400 kg (5,291 lb)[source]
2,950 kg (6,504 lb)[source]
one
2PZL-130TC II Orlik · Crew
Crew
All recorded figures & sources
2 peoplePZL-130TC II Orlik · Crew
Single source 2[source]
232km/hMaximum; T-41C · Maximum speed
550km/h
SpeedScopes differ
All recorded figures & sources
232 km/hMaximum; T-41C · Maximum speed
Single source 125 kn (144 mph, 232 km/h)[source]
490 km/hCruise; PZL-130TC II Orlik · Cruise speed
Single source 550 km/hMaximum; PZL-130TC II Orlik · Maximum speed
Single source 550 km/h (340 mph, 300 kn)[source]
490 km/h (300 mph, 260 kn)[source]
1,159kmT-41C · Range
2,200kmPZL-130TC II Orlik · Range
RangeScopes differ
All recorded figures & sources
1,159 kmT-41C · Range
Single source 626 nmi (720 mi, 1,159 km)[source]
2,200 kmPZL-130TC II Orlik · Range
Single source 2,200 km (1,400 mi, 1,200 nmi)[source]
160kW
560kW
PowerScopes differ
All recorded figures & sources
160 kWT-41C · 1 × Continental IO-360-D Six-cylinder air-cooled horizontally-opposed piston engine
Single source 1 × Continental IO-360-D Six-cylinder air-cooled horizontally-opposed piston engine, 210 hp (160 kW)[source]
560 kWPZL-130TC II Orlik · 1 × Pratt & Whitney Canada PT6A-25C turboprop 750 shp
Single source 1 × Pratt & Whitney Canada PT6A-25C turboprop, 560 kW (750 shp)[source]
14.8m²T-41C · Wing area
14.6m²PZL-130TC II Orlik · Wing area
Wing areaScopes differ
All recorded figures & sources
14.8 m²T-41C · Wing area
Single source 159 sq ft (14.8 m 2 )[source]
14.56 m²PZL-130TC II Orlik · Wing area
Single source 14.56 m 2 (156.7 sq ft)[source]
5,200mT-41C · Service ceiling
10,000mPZL-130TC II Orlik · Service ceiling
Service ceilingScopes differ
All recorded figures & sources
5,200 mT-41C · Service ceiling
Single source 17,000 ft (5,200 m)[source]
10,000 mPZL-130TC II Orlik · Service ceiling
Single source 10,000 m (33,000 ft)[source]
4.5m/sT-41C · 880 ft/min (
14m/sPZL-130TC II Orlik · 2,830 ft/min
Rate of climbScopes differ
All recorded figures & sources
4.5 m/sT-41C · 880 ft/min (
Single source 880 ft/min (4.5 m/s)[source]
14.4 m/sPZL-130TC II Orlik · 2,830 ft/min
Single source 14.4 m/s (2,830 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
