View the embedded image gallery online at:
http://www.pcpilot.hu/microsoft/fs2004/project-tupoljev-team-tu-154m-v203.html#sigProGalleria9342fd7fb0
http://www.pcpilot.hu/microsoft/fs2004/project-tupoljev-team-tu-154m-v203.html#sigProGalleria9342fd7fb0
View the embedded image gallery online at:
http://www.pcpilot.hu/microsoft/fs2004/project-tupoljev-team-tu-154m-v203.html#sigProGalleria7720a5bd93
http://www.pcpilot.hu/microsoft/fs2004/project-tupoljev-team-tu-154m-v203.html#sigProGalleria7720a5bd93
A javítások listája:
- The fuel automation for the engines is now modelled.
- The wheels cooling system operation with regard to the brake disks heat depend now on the braking conditions (with brake overheat effect).
- New fire protection system was added.
- Precise time indicator.
- SRD controller with pressure control device for initial pressurization altitude.
- On the pressure control devise for the initial pressurization altitude - QFE pressure is set after selecting the aircraft when starting the simulator.
- Coarse setting of pressure value for pressurization (with increments of 10 mm of mercury) by right mouse-click was added.
- SSOS (dangerous speed alarm system) control was added.
- A row of dummy toggle-switches was added to the Flight Engineer overhead panel.
- "Обогрев дверей" ('Doors heating') toggle-switch is simulated.
- Additional sound and animation were added to certain instrument buttons and toggle-switches.
- Vertically oriented DME selection toggle-switch is added.
- The 'Zero' position for the hydraulic fluid level indicator needle was corrected.
- БКК-ТЕСТ (BKK-TEST) light was added.
- The rotary switch position sequence for 100V power network control is corrected.
- The СО-72М transponder was remodelled.
- The engine vibration detector check is simulated.
- The 'Transparency' of the rotary switches on the electric system panel was eliminated.
- The mouse zones for the landing gear lever were corrected.
- The landing gear warning light for the Flight Engineer was added.
- Water supply system is modelled.
- The alarm system control elements for the tail compartment temperature are now serviceable.
- The control elements of the drain outlet heating system are now serviceable.
- PTS phase designation for the 36V power network rotary switch is corrected.
- The needles on the Flight Engineer panel are movable now.
- The engine oil pressure is adjusted in accordance with the Tu-154M Flight Manual.
- РВ-5 radio-altimeter check buttons are added.
- The "Неисправность двигателя" ('Engine failure') warning light operation logic was corrected.
- The upper indication value of the radio-altimeter scale on ИП-33 is corrected (25 instead of 30).
- APK (ADF) needles motion is corrected for the cases when a signal is unavailable.
- If the aft luggage compartment is opened, the 3rd engine start-up will be blocked.
- The engines start-up will be blocked unless all the pumps of the feed fuel tank are engaged.
- ТВГ (exhaust gas temperature) check can be performed only when the control is on and 27V power supply.
- The error of an engine starting up without any fuel supply (by РОД (engine stop handle) switching over) is corrected.
- Now the engines can continue operating, being supplied with fuel remaining in pipelines (for 20 seconds).
- THB fuel pump indicator on the Flight Engineer panel will now operate only when 27V power supply is on.
- The standby fuel pump can operate only in flight.
- There are new warning light bitmaps on the Pilot-in-Command panel.
- Now the temperature adjustment toggle-switches on ПКМ are switched over mutually.
- When power supply is being turned off, the APU instrument needles, air-conditioning system temperature indicator needles and oil temperature indicator needles will move to the extreme left zone of the scale.
- The beacon sounds error is corrected.
- The intercom console is insonified.
- AHT and PAM APK-15 modes are realized.
- The intercom toggle-switch on the pilot's upper electric panel is serviceable now.
Forrás: