mvsgas

https://forums.eagle.ru/showpost.php?p=4057215&postcount=218 By 2014, not all USAF F-16C block 50 had AGCAS, and control flight into terrain where still occurring. This is an Accident Investigation Board (AIB) report on one (direct PDF link) http://www.airforcemag.com/AircraftAccidentReports/Documents/2015/120114_F-16CM_MiddleEast.pdf

Inboard - Depressed <0.5 seconds rotaries the datalink declutter options (ALL, FTR+, TGTS) or if NONE is selected, changes to last-left. -- If MIDS is OFF, toggles declutter between ALL and NONE. - Depressed ≥ 0.5 seconds with XMIT IDM selected on HSD: --If HSD or HAD is SOI, transmits the designated (boxed) threat as a SEAD DL. --If HSD is SOI and CAS IP or TGT is designated, transmits a CAS mission update. --If FCR or TGP is in track and is the SOI, transmits the SPI as a MKPT. --If none of the conditions above are met, transmits the currently selected steerpoint location (without nav cursor corrections) as a MKPT. - Depressed ≥ 0.5 seconds with XMIT L16 selected on HSD: -- If HSD or HAD is SOI, transmits the designated (boxed) threat as a SEAD DL with Lock Line. -- If FCR or TGP is in track and is the SOI, transmits the SPI as a MKPT with Lock Line -- If HSD is SOI and CAS IP or TGT is designated, transmits the currently selected steerpoint (without nav cursor corrections) as a MKPT Outboard Depressed < 0.5 seconds toggles FCR format datalink declutter between NONE and ALL. Depressed ≥ 0.5 seconds initiates IDM one-round or round-robin intraflight datalink.

For what is worth, In the USAF version of the -1, it mentions that due to the Nose Landing Gear (NLG) design, the aircraft will tent to drift right with Nose Wheel Steering (NWS) off. This is exacerbated with forward stick force, heavy breaking or additional weight of the pod/pods but easily corrected or controlled by rudder.

At what fuel weight are you landing? I tend to land with 3500lbs or less, having no problem stopping so far.

https://forums.eagle.ru/showpost.php?p=3798164&postcount=361

Could you elaborate?

https://forums.eagle.ru/showthread.php?t=251170&page=2

In addition, If you look, the last F-16C delivered to the USAF was 01-7053. On the list I provided this aircraft is shown as a block 50 without sub-block. So the aircraft contract was created in 2001 ( hence the serial number start with 01) it was finally delivered in 2005. https://www.af.mil/News/Article-Display/Article/134773/air-force-receives-last-f-16/ So, four years after the contract was created it was delivered and our F-16C in DCS are circa 2007, meaning this aircraft would have undergone two years of service. In that time it could have been updated/upgraded further, so the sub-block wold be meaningless since we no longer know what is the aircraft configuration (meaning specific engine sub versions, cockpit arrangement, software, etc.) For the sub-block to matter we would need ED to tell us the specific serial number they base the aircraft in and then we would need the specific history of that aircraft so we know what TCTO was completed when. We would also need to know what was every TCTO. Because all of this, in my opinion, sub-block are inconsequential in this specific case.

Sub block is one of the things the Common Configuration Implementation Program (CCIP) was trying to address for the USAF block 40/42/50 and 52. If your looking for specific serial number, al tho some differences exists, DCS F-16C would be one of these, circa 2007. http://www.f-16.net/aircraft-database/view_airframes_byadvancedsearch/acshort/F-16/fy/0/plant/0/status/0/version/11579/program/0/airforce/11055/unit/0/deployment/0/displayteam/0/actype/F-16/startnum/1 Edit Unless ED tell us they are modeling a specific serial number, we would never know the sub block, and on this particular instance, the sub block would be irrelevant.

Shore−based pitch trim shall be 2° nose down. These trim settings are based upon rotation of the aircraft/nozzles at the calculated rotation airspeed while the stick remains guarded at the trimmed position. Use of additional airspeed in order to provide a performance pad will produce nose down pitching moments after rotation that will have to be arrested with aft stick deflections.

JFS used to have a lot of problems back on the ESSC days, but in the last couple of years with the DESSC and other components is a lot better. Back in 1997, JFS where change 500 starts and it was rare if they ever get there. By 2012, they where change every 1700 starts and normally get there without issues.

En este avion de combate, si. Es la realiadad de el combate aereo

You have to select tracers rounds on the arming insert or in the mission editor.

By selecting CCIP with TGP, you are telling the MMC to use the TGP to calculate the impact point. So the MMC should moves the TGP to the CCIP aim point. If the TGP is tracking a target and CCIP is selected, the TGP should also break tracking.

No. Amber light will change depending on AOA

I wish the camera was on the right side of the pit, so we could better see the control stick and engine gauges. You see the MFL/PFL list at 20:36?

Caucasus map single player starting on the runway Upon engine shutdown, flaperon move up. This should only happen if the DFLCC looses power and there is still hydraulic pressure on the system. On normal shutdowns, flaperon should stay down.

https://forums.eagle.ru/showthread.php?t=250870

Caucasus map single player starting on the runway Shunting downs the engine, looking at the hydraulic gauges you can see zero pressure, yet the flight control surfaces still move.

Caucasus map Single player Starting on the runway. When shutting down the engine, the nozzle closes as if transferring to sec. This should only occur if the battery switch is turn off before engine is below 20% RPM.

What mods do you guys have installed? Does it behave like this even without mods?

Not sure if it modeled correctly in DCS, but the real aircraft has a speed limit for the door in transition from close to open (and vise versa) and open. The limit is 400 knots or mach .85 ( which ever is less) for transition and 400 knot or mach .95 for the door open. Maybe this is ED's ways of simulating what happens if door is open above the limit, since the manuals never say what would happen.

The F-16C Upfront Control (UFC) is control through the Integrated Control Panel (ICP)