Northwind

Very thanks.

No, I didn't. I have read these topics, although not every posts. Anyway, thanks for your help.

Dcs Multi-Threading every 3-6 secs freezes for 5-6 secs,in at least last three versions. This PC is not new. But without high settings, there is an acceptable FPS for light mission. Even in last three versions,FPS of 3-6 seconds between freezing and next freezing is an acceptable. System specifications:In the attachment. Test mission: Caucasus Default Weather Default Time Civilian traffic off One aircraft on runway of Sukhumi,no other unit. Current DCS version：DCS Open Beta 2.9.2.49629 dcs.log DxDiag.txt

Yes. Beta. The decrease of FPS is obvious.

Sorry,Just noticed this,At 0.95 to 2.0 IMN,SYM (G): +6.5, -3.0 (T.O.1F-5E-1 Page 268). Is this an OPERATING LIMITATION for transonic pitch-up? I don't know.

That's what I mean. And load limit of F-5E is +7 .33, -3.0 (T.O.1F-5E-1 Page 268)，Plus the 150% design safety factor，+10.995G. So it is correct that F5E pulls about 11g without break up. The structural damage should be consistent across the speed range.

Track file. This is not the Most extreme case. f5e g overload.trk

The current version of DCS F5E seems that the G overload damage limit decreases with the increase of speed. At IAS 500 knots, it can pull more than 11g without overload damage. At IAS 800 knots, overload damage occurs at approximately 7-8.x G. Note that it is correct that F5E pulls about 11g without break up, and break up should occur at higher overload. It's easy to reproduce. No track file. DCS version:open beta 2.7.7.14727

Track stable version 2.5.5.41371 FA-18C Button 7.trk

When radar on right DDI,In RWS mode,move the TDC to no target place and press designate.At this moment,before the scan line returns to normal scanning,press right DDI button 7 will cycle L&S. This doesn't look like the correct behavior.

Looks like I'm mistaken how CDI works. Thank you guys.

CDI only need bearing.It should work.

CDI(course deviation indicator) does not work when using DF, it works when using TACAN. CDI no deviation when using DF. stable version 2.5.5.39384

DCS F-5E ADF behavior is different from what is written in the manual( T.O. 1F-5E-1 and DCS F-5E manual). To use ADF navigation, the DCS F-5E need to rotate the UHF Radio Function Selector to the ADF position and the NAV MODE selector to the DF position. When the NAV MODE selector in the DF position, the MAIN and BOTH positions of the UHF Radio Function Selector does not activate the ADF navigation. However On T.O. 1F-5E-1,Page 115,item 2 is written: Page 109,item 8 is written: Page 116,item 9 is written(Same as DCS F-5E manual,different from DCS F-5E actual behavior): So,ADF position of UHF Radio Function Selector is Nonfunctional on aircraft with UHF DF selection on NAV MODE selector. This means when the NAV MODE selector in the DF position,the MAIN and BOTH positions of the UHF Radio Function Selector should activate the ADF navigation.The ADF position of the UHF Radio Function Selector is unknown. DCS F-5E with UHF DF selection on NAV MODE selector. RL F-5E in T.O. 1F-5E-1 and DCS F-5E equipped with the AN/ARC-164 UHF radio, AN/ARA-50 UHF/ADF automatic direction finder,and RL F-5E are equipped AN/ARN-118 TACAN systems(The pictures and examples in the manual are AN/ARN-1 1 8 ),DCS F-5E equipped TACAN AN/ARC(N)-118 NAVIGATION SYSTEM. Did I make a mistake? Or DCS F-5E simulates different variant? Or the behavior of the F-5E ADF does not match the manual( T.O. 1F-5E-1 and DCS F-5E manual).