Credit
BoomerTheDoomer · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
L-39C · Length
Single sourceL-39C · Only the source-declared variant L-39C · L-39C
Single sourceConfiguration
| Specification | L-39C | PZL-130 Orlik |
|---|---|---|
| Variant description | L-39C (C for Cvičná – training)[source]Only the source-declared variant L-39C Standard basic trainer for Soviet Union, Czechoslovakia and export. Originally designated L-39, but renamed L-39C when later variants appeared. Two pylons under wing. Approximately 2,260 built.[source]Only the source-declared variant L-39C | — |
| Airfoil | NACA 64A012 modified[source]Only the source-declared variant L-39C | — |
| Never exceed speed | 980 km/h (610 mph, 530 kn) / M0.8[source]Only the source-declared variant L-39C | — |
| Endurance | two hours and 30 minutes (internal fuel), three hours and 50 minutes (internal and external fuel)[source] |
12.13 m (39 ft 10 in)[source]Only the source-declared variant L-39C
39.8 ft[source]L-39C · Aero Vodochody L-39C (x2)
PZL-130TC II Orlik · Length
Single source9.3 m (30 ft 6 in)[source]
Empty; L-39C · Only the source-declared variant L-39C · L-39C
Single sourceMaximum take-off; L-39C · Max takeoff weight
Single sourceMaximum take-off; L-39C · Only the source-declared variant L-39C · L-39C
Single source3,455 kg (7,617 lb)[source]Only the source-declared variant L-39C
4,700 kg (10,362 lb)[source]Only the source-declared variant L-39C
10,360 lbs[source]L-39C · Aero Vodochody L-39C (x2)
Empty; PZL-130TC II Orlik · Empty weight
Single sourceGross; PZL-130TC II Orlik · Gross weight
Single sourceMaximum; L-39C · Only the source-declared variant L-39C · L-39C · at 5,000 m (16,000 ft)
Single source750 km/h (470 mph, 400 kn) at 5,000 m (16,000 ft)[source]Only the source-declared variant L-39C
Ferry; L-39C · Only the source-declared variant L-39C · L-39C · internal and external fuel
Single sourceL-39C · Only the source-declared variant L-39C · L-39C · internal fuel
Single source1,100 km (680 mi, 590 nmi)(internal fuel)[source]Only the source-declared variant L-39C
1,750 km (1,090 mi, 940 nmi) (internal and external fuel)[source]Only the source-declared variant L-39C
991 nm[source]L-39C · Aero Vodochody L-39C (x2)
PZL-130TC II Orlik · Range
Single source2,200 km (1,400 mi, 1,200 nmi)[source]
PZL-130TC II Orlik · 1 × Pratt & Whitney Canada PT6A-25C turboprop 750 shp
Single source1 × Pratt & Whitney Canada PT6A-25C turboprop, 560 kW (750 shp)[source]
L-39C · Only the source-declared variant L-39C · L-39C · 1 × Ivchenko AI-25TL turbofan engine thrust
Single source1 × Ivchenko AI-25TL turbofan engine, 16.87 kN (3,790 lbf) thrust[source]Only the source-declared variant L-39C
L-39C · Only the source-declared variant L-39C · L-39C
Single sourceL-39C · Wing Area
Single source18.8 m 2 (202 sq ft)[source]Only the source-declared variant L-39C
202.4 ft 2[source]L-39C · Aero Vodochody L-39C (x2)
PZL-130TC II Orlik · Wing area
Single source14.56 m 2 (156.7 sq ft)[source]
L-39C · Only the source-declared variant L-39C · L-39C
Single sourceL-39C · Service ceiling
Single source11,000 m (36,000 ft)[source]Only the source-declared variant L-39C
36,000 ft[source]L-39C · Aero Vodochody L-39C (x2)
PZL-130TC II Orlik · Service ceiling
Single source10,000 m (33,000 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Time to altitude | 5,000 m (16,000 ft) in 5 minutes[source]Only the source-declared variant L-39C | — |
|---|
| Wing loading | 250 kg/m 2 (51 lb/sq ft)[source]Only the source-declared variant L-39C | — |
|---|
| Thrust/weight | 0.37[source]Only the source-declared variant L-39C | — |
|---|
| Take-off roll | 530 m (1,740 ft)[source]Only the source-declared variant L-39C | — |
|---|
| Landing roll | 650 m (2,130 ft)[source]Only the source-declared variant L-39C | — |
|---|
| Hardpoints | Up to 284 kg (626 lb) of stores on two external hardpoints[source]Only the source-declared variant L-39C | 6 with a capacity of 700 kg (1,500 lb)[source] |
|---|
| Manufacturer | Aero Vodochody[source]L-39C · Aero Vodochody L-39C (x2) | Airbus Poland SA[source] |
|---|
| Country of origin | Czechoslovakia[source]L-39C · Aero Vodochody L-39C (x2) | — |
|---|
| Engine | Ivchenko AI-25TL[source]L-39C · Aero Vodochody L-39C (x2) | — |
|---|
| Thurst (mil) | 3,800 lbs[source]L-39C · Aero Vodochody L-39C (x2) | — |
|---|
| Vne | 530 kts[source]L-39C · Aero Vodochody L-39C (x2) | — |
|---|
| Climb Rate (Sea Level) | 4,100 fpm[source]L-39C · Aero Vodochody L-39C (x2) | — |
|---|
| Type | — | Trainer[source] |
|---|
| National origin | — | Poland[source] |
|---|
| Primary user | — | Polish Air Force[source] |
|---|
| Number built | — | 50 + 9 prototypes[source] |
|---|
| Introduction date | — | 1994[source] |
|---|
| First flight | — | 24 October 1984[source] |
|---|
Maximum take-off; PZL-130TC II Orlik · Max takeoff weight
Single source