April 25, 201511 yr Hi All, I've put together a brief album for the cold and dark start up following normal procedures. Hope it helps. http://imgur.com/a/CFUBk Shuai Li
April 25, 201511 yr Slightly nicer than my "4 year old crayon pictures" lol! Thanks very much! | My Liveries | FAA ZMP | PPL ASEL | | Windows 11 | MSI Z690 Tomahawk | 12700K 4.7GHz | MSI RTX 4080 | 64GB 6000 MHz DDR5 | 500GB Samsung 860 Evo SSD | 2x 2TB Samsung 970 Evo M.2 | EVGA 850W Gold | Corsair 5000X | HP G2 (VR) / LG 27" 1440p |
May 22, 201511 yr Just to be clear - does the APU actually work? I seem to remember that I got it working once but I could just be dreaming... Christopher Allan
May 22, 201511 yr I'm thinking that electrical systems are not modeled. Everything is on the same bus, the valves are dummies and APU is like BAT ON...
May 22, 201511 yr What does the APR arming actually do for the Hawker? It's not defined in the manuals anywhere that I have found.
May 22, 201511 yr nothing, it's not simulated... more info: http://www.smartcockpit.com/aircraft-ressources/Hawker_00XPC-Engines.html
May 22, 201511 yr For those who don't want to download the manual (although you should as it's a great resource from blahhhblahhh) AUTOMATIC PERFORMANCE RESERVE (APR) When armed, the APR system allows an automatic increase in engine performance in the event of an engine failure or transient fault during takeoff, or during a go-around following a single engine approach. There will be no increase in thrust if the ambient conditions are such that the engines are N1 RPM limited (at normal rating). The APR system is powered from the PE busbar and consists of two mechanically latching, push on/push off, control switches in the flight compartment plus an APR/ Sychronizer control unit in the rear equipment bay.
May 27, 201511 yr For those who don't want to download the manual (although you should as it's a great resource from blahhhblahhh) AUTOMATIC PERFORMANCE RESERVE (APR) When armed, the APR system allows an automatic increase in engine performance in the event of an engine failure or transient fault during takeoff, or during a go-around following a single engine approach. There will be no increase in thrust if the ambient conditions are such that the engines are N1 RPM limited (at normal rating). The APR system is powered from the PE busbar and consists of two mechanically latching, push on/push off, control switches in the flight compartment plus an APR/ Sychronizer control unit in the rear equipment bay. Interesting info!, sadly it's not simulated...
May 28, 201511 yr Hi All, I've put together a brief album for the cold and dark start up following normal procedures. Hope it helps. http://imgur.com/a/CFUBk I had missed this post. Great job autogyro.
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