Saab 35 Draken: Difference between revisions

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Updating info
(→‎Special indicators: plané info)
(Updating info)
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*GLÖM EJ LAND-STÄLL: ("Do not forget landing gear") flashes if altitude < 1450 m, airspeed < 450 km/h and throttle < 85%
*GLÖM EJ LAND-STÄLL: ("Do not forget landing gear") flashes if altitude < 1450 m, airspeed < 450 km/h and throttle < 85%


*HUVUDVARN.: Main caution light. Indicates important system warnings. See below.
*HUVUDVARN.: Main caution light. Indicates important system warnings. See below. Acknowledge by pressing the light to silence the alarm. No warning signal while taxing.


*HÖJDV: Flashes when autopilot HÖJD (altitude hold) is set and aircraft not at target altitude or vertical speed above 200 m/min. Lit when stable at target altitude. It is recommended to be at target altitude before setting autopilot to HÖJD.
*HÖJDV: Flashes when autopilot HÖJD (altitude hold) is set and aircraft not at target altitude or vertical speed above 200 m/min. Lit when stable at target altitude. It is recommended to be at target altitude before setting autopilot to HÖJD.
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Below Heading indicator. Sets course needle on the heading indicator (compass).
Below Heading indicator. Sets course needle on the heading indicator (compass).
'''Clock'''
Clock ring: Knob furthest right from clock turns the ring. Set pointing to the minute hand before lift off to keep track of flying time.
Clock mode button: Lowest knob. Switches between clock and stopwatch. In reality also setting of the clock but not implemented.
Stopwatch button: Starts, stops and resets the stopwatch.




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*!BRAND MOTOR: (fire engine) not implemented
*!BRAND MOTOR: (fire engine) not implemented
*!BRAND EBK P: (fire afterburner pump) not implemented
*!BRAND EBK P: (fire afterburner pump) not implemented
*STYR AUT: (autopilot) autopilot off
*!STYR AUT: (autopilot) autopilot off
*MOTOR IS: (engine ice) engine deicing on not implemented yet
*MOTOR IS: (engine ice) engine deicing on not implemented yet
*!TANK LUFT: (tank air) airpressure fault in fuel system. Not implemented
*!TANK LUFT: (tank air) airpressure fault in fuel system. Not implemented
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'''Radio'''
'''Radio'''
 
The radio equipment consists of two transceiver and one control unit of model Fr-21. They are on the left horizontal panel. In the simulation both transceivers are used for communication. In the real aircraft one was the receiver for combat control data feeding the AHK and other avionics. The letters A-K stores pre set frequencies for transceiver A (closest to the control unit) and the numbers 1-5 stores pre set frequencies for transceiver B. A stores the COM1 frequency at FG start up. Number 1 stores the COM2 frequency at FG start up. The frequency for the other letters and numbers are in the text file $FG_HOME/Export/SaabJ35F-Fr21.txt and can be changed by the user.
The radio equipment consists of two transceiver and one control unit of model Fr-21. They are on the left horizontal panel.(14) In the simulation both transceivers are used for communication. In the real aircraft one was the receiver for combat control data feeding the AHK and other avionics. The letters A-K stores pre set frequencies for transceiver A (closest to the control unit) and the numbers 1-5 stores pre set frequencies for transceiver B. A stores the COM1 frequency at FG start up. Number 1 stores the COM2 frequency at FG start up. The frequency for the other letters and numbers are in the text file Avionics/Fr21.txt and can be changed by the user. Pressing the buttons marked with dash (-) makes it possible to manually set the transceiver’s frequency using the knobs on the unit. The radio is off at simulation start. Transceiver B uses battery power and transceiver A uses main AC.
Pressing the buttons marked with dash (-) makes it possible to manually set the frequency using the knobs on the two manual units. Changing mode from Normal to Reserv changes sending unit from A to B.
The radio is off at simulation start. Transceiver B uses battery power and transceiver A uses main AC.




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'''Controls and switches'''
'''Important controls and switches'''


* Drag chute handle: (BROMSFALLSKÄRM) Lower left.(15) First use deploys drag chute. Second drops it. It takes approx. 3 seconds to deploy and should be done under 320 km/h and above 200 km/h. The handle can not be used if throttle above 85%.
* Drag chute handle: (BROMSFALLSKÄRM) Lower left.(15) First use deploys drag chute. Second drops it. It takes approx. 3 seconds to deploy and should be done under 320 km/h and above 200 km/h. The handle can not be used if throttle above 85%.
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