| Date: |
Flight Nr.: |
Take-off: |
Landing: |
Duration: |
Pilot: |
| 27.2.1943 |
9 |
1353 |
1410 |
17' |
Burgen |
| 27.2.1943 |
10 |
1440 |
1504 |
24' |
Burgen
|
| 3.3.1943 |
12 |
1438 |
1442 |
04' |
Kampmeier |
| 4.3.1943 |
13 |
858 |
943 |
45' |
Märschel
|
| 6.3.1943 |
14 |
1148 |
1218 |
30' |
Bartsch
|
| 6.3.1943 |
15 |
1737 |
1815 |
38' |
Sander |
| 7.3.1943 |
16 |
1123 |
1144 |
21' |
Bartsch
|
| 8.3.1943 |
17 |
1507 |
1518 |
11' |
Bartsch
|
| 8.3.1943 |
18 |
1605 |
1642 |
37' |
Bartsch
|
| 11.3.1943 |
19 |
819 |
832 |
13' |
Bartsch
|
| 1.3.1943 |
11 |
1550 |
1623 |
33' |
Märschel
|
| Condition: |
| Engine BMW 801 D2/20244 |
| Tight engine cowling. |
| Split flaps. |
| Armament: 2 MG 151 |
| Autopilot. |
| Variometer installation |
| Robotic system. |
| Auxiliary wing tanks with standard Ju 87 rack fairing, or two faired ETC 50 each wing in accordance with 8-190862-Z01. |
| ETC 501 under the fuselage with ER 4 lock 50 L 2. |
| 1. | Check the auxiliary wing tank system. |
| 2. | Level speeds for various operational conditions with ETC 50 or bomb locks. |
| 3. | Assessment of the instrument panels. |
| 4. | Ram pressure calibration on the test course. |
| 1. | The re-check of the fuel flow from the auxiliary wing tank gave 960 l/h. The pump limiter responded at 285 liters indicated
in the rear tank. It is noted in this context that in some cases the pump limiter reopens only at 245 liters in the rear tank, so that the
auxiliary tank pumps must be switched off only after the indicator shows less than 240 liters. | |
| 2. | Level speed values at combat power for the various operational conditions were as follows (see graph) : | |
| Conditions | Speed | Speed loss ΔV
from attachments |
|
Flugbericht Fw 190/861 Staffel Nr. 6, Nr. 2
Translation by Jörn Dietrich and Mike Williams
© 2013 WWIIaircraftperformance.org. All Rights Reserved
By Mike Williams and Neil Stirling - Rebuilt By Badatflyski - All rights reserved.
