Brisafresca

No button assignments for the LABS system, even.

I agree with you:thumbup:

BST, Where are you?

Not, the oficial flight manual indicates: approximately range: 450ft - 9.000ft Regards Brisafresca

BST´s question, This switch allows you to arm and ensure missile system. :helpsmilie: Thanks Brisafresca

BST, Where are you?

Hi According to the official flight manual the approximate extent of the F-86F is about 450ft - 9.000ft, I checked this in DCSW and AN / APG-30 still aims at a maximum distance of 17.000ft (3.2 nm), this is wrong. On the other hand, I think that the radar has an azimuth of +/- 20 degrees, why is 30 degrees in DCSW? On the F-86F.lua the sensor is N008, ie Mig-23 radar Can anyone explain to me that radar features are not real? Thank You regards Briisafresca

Juan Oscar, del quince:thumbup:, me encantaría un F-104G.:D:D:D:D Saludos Brisafresca

What is EFM?

Yes, of course, only posting hoping to answer me Wags or tester :music_whistling: Regards Brisafresca

Del quince Ce_Zeta :thumbup:

DCSW 2.0 - Minimum graphics card? Hi With the arrival of new DCSW 2.0, which graphic card will be required?, currently, minimum recommended is a GTX560. Thank You regards Brisafresca

Hi It is possible if you maintain high speed, I tried out the ditching procedure and fly low at 185kts IAS and traveled somes milles. The correct procedure is release external stores and pull up inmediately after engine dead and when your speed is 185kts finish climb, next step is descent glide with engine windmilling, maintain 185kts IAS with speed brakes in, flaps and gear up, now the milles in windmilling depent of your altitude and speed. It is real, BST F-86 can travel 115nm with engine dead glide from 50.000ft, I did. regards Brisafresca

In principle, drop tanks are type I and III. Regards Brisafresca

Thanks you:thumbup:

Hi I answered myself, I had found the solution without knowing , it is not necessary to place the throttle off.:smilewink: regards Brisafresca

hello I tested this fault is simulated:thumbup:, however, I note that when the throttle is placed in idle position and advance slow to Full (100%) the compressor stall or loss of power disappear. Is it normal or is a Bug? Thank You regards Brisafresca

According to the flight manual the canopy can be opened below 215 knots IAS, in DCSW only up to 180 knots Could you correct that? Thanks and Happy New Year Regards Brisafresca

Hi Does anyone know what it means Type I, II, III and IV for droptanks 120 and 200gallons?:helpsmilie: Happy New Year!!!!!

Thanks you:thumbup:

Hi BST Someday will be functional the Landing Gear Unsafe Warning Light? Thanks you Regards Brisafresca

hello I'm trying to do a manual on Sabre, I'm currently writing the emergency procedures and I have met with surprise that this module is not faithful to reality faults, for example: A programmed failure (menu of random failures) in the single-phase inverter that powers the AN / APG-30 rangefinder and A-4 sight, not rendered inoperative by chance only illuminates the Main radar warning light, but no damage, even radar lock objects on the ground. Another fault that is not fully simulated is the lubrication system failure, the needle the instrument falls to zero, but this implies a reduction in rpm as there is friction between the axis of rotation of the motor and bearings, reaching stop engine, but it does not happen. So, are these the failures that will exist in the final version of Sabre or are these? Will you expand the list of failures? Today I can only recreate those emergency procedures related to air start, forced landing, ditching, engine failure at low altitude, belly landing and little else. Thank you regards Brisafresca

BST where you are?

Hi This question is addressed to BST: Do you have plans to expand the list of random failures for the Sabre? For example, engine damage due to overheating due to an engine windmilling? Regards Brisafresca

Hi BST Can you clarify this doubt? Thanks you Regards Brisafresca