Airports & Sceneries
– External Model:
– Fixed visibility conditions causing STA8 and STA9 loads to be reversed
– Minor adjustment to crew boarding ladder position
– Empty pylons can be made to appear by applying a 51 lbs weight to the desired station.
– Flight Model:
– Adjustments to engine rpm vs. Mach vs. thrust table at low Mach numbers
– Minor tweaks to external induced drag scripts
– Minor tweaks to ground effect
– Minor tweaks to slow speed handling control effectiveness
– Minor tweaks to supersonic drag index table
– Tweaks to weight and balance distribution – this can now be changed in the MSFS 2024 EFB
– Rewritten script to limit altitude for smoother behavior
– Avionics:
– Fixed minor glitches in MISC page
– Fixed minor glitch in RMHDD soft keys when VS radar mode is selected on MSFS 2024
– Fixed bug causing GS to display on HDHUD format even if Mach number is above 0.9
– Systems:
– Fixed minor glitch on fuel transfer causing slightly incorrect fuel quantity in rare occasions
– Fixed bug causing engine anti-ice not to work in certain conditions
– Fixed bug causing air data probe automatic heating system not to work in certain conditions. Code moved to avionics module.
– Changed formation lights knob default position to off
– Minor fixes to cockpit mouse areas
– Liveries:
– Added Royal Saudi Air Force 92nd, 93rd, 94th and 95th National Day special liveries, courtesy of Matteo Baiocchi
– Miscellaneous:
– Removed unnecessarily duplicated bitmap files
– Added Appendix 1 “Creating a flight plan in MSFS2024” to the manual
– Added Appendix 2 “Managing a custom loadout with the EFB in MSFS2024” to the manual
The Typhoon is a dual-engine, loosely coupled delta canard tailless design, featuring a 53-degree leading edge sweepback, relaxed stability and a digital fly-by-wire control system. It is a highly agile aircraft at all speeds, both subsonic and supersonic, achieved by having intentionally relaxed stability, combined canard and flaperon control surfaces, and a very low wing loading. The quadruplex digital fly-by-wire control system manages the inherent instability, allowing better manoeuvrability than direct pilot control. It is described as ‘carefree’ and prevents the permitted manoeuvre envelope being exceeded.
Roll control is primarily achieved by differential use of the flaperons. Pitch control is by coupled operation of the canards and flaperons. The wing leading edges are fitted with automatic movable slats. A single large rudder provides yaw control. Engines are fed by a chin double intake ramp situated below a splitter plate.
A hydraulically operated air-brake is integrated behind the cockpit, moving into a near-vertical position to maximise drag when required.
The Typhoon uses lightweight construction (82% composites consisting of 70% carbon fibre composite materials and 12% glass fibre reinforced composites) as well as aluminium lithium and titanium components on leading edge surfaces. The airframe has an estimated lifespan of 6,000 flying hours.
Features:
• High detail visual models
• Liveries for every squadron that operates the EF-2000
• Detailed and realistic avionic and systems simulation
• Finely tuned flight model
• Accurate sound package
