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Germany's Focke-Wulf Fw 189 Uhu (Eagle Owl) reconnaissance1,2
Focke-Wulf 189 Uhu:
Design
Designed by Kurt Tank.1
Undercarriage
The wheels were very tough allowing the Fw 189 to use rough air fields.1 The wheels retracted into armored doors.1
Wings / Tail
There were four ETC 50 racks that could carry anti-personnel bombs but were often empty.1
The wings were very strong.1 Flaps were electrically operated.1 The Rudders, elevator, and ailerons were manual.1
The twin booms and the full length elevator in the tail allowed for exceptional maneuverability.1
Prototype
Kurt Tank flew the prototype in June 1938.1
The first prototype flew in July 1938.2
The media called it "The Flying Eye."1,2
Production
Built at Focke-Wulf's Bremen factory, and in Czechoslovakia and France.1
- Fw 189V: 62
- Fw 189A-0: 102
- Fw 189A-1, Fw 189A-2, Fw 189A-3, Fw 189A-4: 8482
- Fw 189B: 132
- Fw 189F: 172
- Total: 8942
Variants
- Fw 189:
- Fw 189A-0: Pre production.2
- Fw 189A-1: Production model.2 Reconnaissance.2
- Fw 189A-2: Dual control trainer.2
- Fw 189A-3: Dual control trainer.2
- Fw 189A-4: Tactical support.2 Had 20 mm cannons in the wing roots replacing the MGs.2
- Fw 189B: Five seat trainer.1,2
- Fw 189C: Experimental version with a heavily armored cabin to be used for close assault.1 Only two crew.1
- Fw 189D: A trainer that had floats, but it was never flown.1
- Fw 189F: Built in France.2 Had Argus AS 411 engine (580 HP).2
- Fw 189 V4: Prototype that could spray mustard gas.1
Usage
Used primarily for reconnaissance, but also used for casualty evacuation, night fighting, and ground support.1
Entered service in late 1940.1 A total of nine long range and 15 short range reconnaissance groups were formed.1
Used by the Slovakian and Hungarian air forces.1,2 Hungary received about 30 Fw 189A-2s.2 Slovakia received 14 Fw 189A-1s.2
| Focke-Wulf Fw 189 Uhu2 | Focke-Wulf Fw 189A-1 Uhu2 | Focke-Wulf Fw 189A-2 Uhu1 | |
|---|---|---|---|
| Type | Reconnaissance2 Close support2 |
Reconnaissance1 Army cooperation1 |
|
| Crew | 32 | 31 | |
| Engine (Type) | 2: Argus As 410A-12 | 2: Argus As410A-1 piston1 | |
| Cylinders | Inverted V 122 | Inverted V-121 | |
| Cooling | |||
| Net HP | 465 each2 | 460 each1 | |
| Propeller blades | 22 | ||
| Dimensions | |||
| Span | 60' 4.5"2 18.4 m2 |
60' 4"1 18.4 m1 |
|
| Length | 39' 4"2 11.99 m2 |
39' 5"1 12.03 m1 |
|
| Height | 10' 2"2 3.1 m2 |
16' 2"1 3.1 m1 |
|
| Wing area | 409 ft2 1 38 m2 1 |
||
| Weight | |||
| Empty | 5,930 lb2 2,690 kg2 |
||
| Loaded | 8,708 lb2 3,950 kg2 |
9,174 lb1 4,170 kg1 |
|
| Performance | |||
| Speed | 217 mph1 350 kph1 |
||
| Speed @ 8,530' / 2,600 m |
221 mph2 355 kph2 |
||
| Cruising speed | 197 mph2 317 kph2 |
189 mph1 305 kph1 |
|
| Endurance | 2 hours 10 minutes1 | ||
| Climb | 1,017'/minute2 310 m/minute2 |
||
| Climb to 13,120' / 4,000 m |
8.3 minutes2 | ||
| Service ceiling | 27,560'2 8,400 m2 |
23,950'1 7,300 m1 |
|
| Range | 416 - 584 miles2 670 - 940 km2 |
415 miles1 670 km1 |
|
| Armament | |||
| Nacelle roof | 2: 7.9 mm MG 811 | ||
| Wing roots | 2: 7.9 mm MG2 | 2: 7.9 mm MG 811,2 | |
| Dorsal, above navigator | 1 or 2: 7.9 mm MG2 | 2: 7.9 mm MG 811 1 or 2: 7.9 mm MG2 |
|
| Tail position | 1 or 2: 7.9 mm MG2 | 1 or 2: 7.9 mm MG2 | |
| Bombs | 4: 110 lb2 4: 50 kg2 |
4: 110 lb2 880 lb1 4: 50 kg2 400 kg1 |
Sources:
- Aircraft of WWII, General Editor: Jim Winchester, 2004
- Aircraft of WWII, Stewart Wilson, 1998
