Tu-154B Examples
Материал из FlightGear
Содержание |
Fueling, loading and centering
To be done
Starting engines
First, we have the power:
Turn the battery (sw. 569).
Turn the converter 565 and 567.
Turn the lights Bano (341).
Secondly, we need to start the APU:
Includes APU start (570) and start/cold (571). After a few seconds, turn on board 577-F ( "APU door opened").
Turn the fuel pump sw. 572. Light board 577-G, H.
Turn automatic launcher by pressing the "START" (574). When the APU starts, turns placard "Out on the regime" (577-I).
Turn the APU generator on the network (switch 552 in the upper position).
And thirdly, we need to fuel pressure. Prepare to work the fuel system:
Turn fuel meter 5015 and 5020 flow meter. Exposes the fuel level on the device 530.
Turn automatic flow (5018), and automatic alignment (5016).
Toggle automatic flow in automatic mode (sw. 5019 in top position).
Turn pumps tanks 2,3,4 (sw. 580, 581, 5007, 5008, 5009).
Turn pumps expendable tank 1 (4-sw. 5012).
Turn cutoff valves 5014. I get a fuel pressure engines extinguished the placard "P fuel (579-P)
And fourthly, we need the hot air. Push the switch 573 in the upward position, and holds up until 577-H has gone.
Turn the temperature control of turbine exhaust (sw. 5030-5032).
Engines ready for launch. We translate the stop-cranes in the front position on the left side of the flight engineer desk, three-arm, with a red lamp failure.
Open the lid remote start engine 5038.
Turn launcher automatic (5038-A) and the "cold-launch" to upward ("launch") (5038-B).
On the real aircraft, in temperatures below -5 'C to include heating ignition device (5038-C). However, in this version of the model, the engine will run regardless of temperature and heating.
Start the engine:
Turn flashing lights OMI (342).
Choose 4-pos. switch (5038-D) engine for start.
Push button start 5038-E. If necessary preparatory procedures implemented correctly, the green lamp lights up "PDA works (5038-G) and the engine will gather rpms. After exiting the engine to idle rpm, quenched lamp 5038-G.
Choosing a switch (5038-D) following the engine and repeat the procedure.
If necessary, stop the process, you can start by clicking on 5038-F.
After starting the engines:
Set the 5038-D in the middle position and close the lid panel.
Connect generators to power bus (561-563) and put the switch 552 in the middle position.
By clicking 5026 charges Hydroaccumulator emergency brake (control manometer 535) until the 5024 lamp gone.
Connects hydropower to RA-56 aggregates (540-548).
Turn the system improve the longitudinal controllability (549).
Turn off APU. To do this:
Close bleed air valve switch 573 by pressing down, until the fire board "is ready to run" (577-H).
Stops turbine APU by pressing the "STOP" (575).
Disable fuel pump APU (572) launcher and automation (570).
Preparing avionics
Preparation electric power:
Switch to view 4 (overhead).
Turn switches 401-420 to the upper position on the overhead, .
Include both sets of Kurs-MP, 421, 422.
If you need RSBN - includes 423 and 424 if using RSBN in the VOR.
Turn switches 425-432.
Turn Diss, 433-435.
Turn placards in the passenger cabin 437. Passengers should keep in severity!
Preparation radio:
Set the frequency and course of ILS, or VOR radial (panels 445, 446).
Set frequency of ADF (panels 442, 443).
Set the COM-frequency radio (panels 440, 441).
Preparation work of gyro compass system TKS:
Press and hold "~" (tilde) to have a convenient overview of the panel PU-11 (436).
Set the current latitude by the handle 436-D, on a scale of 436-A. Or includes an automatic correction of latitude (436-B in the left position), if we do not care about reliability:)
Choosing the MK mode (switch 436-P in the left position).
Let's begin reserve gyro unit alignment. We put 436-G in the down position.
Press and hold the 436-H. At the bottom of screen, you can see a tips.
Hold down the correction, while the position of reserve gyro (GA-3-2) does not cease to evolve. When the fast adjusting of the reserve gyro is completed, an axis of reserve gyro will be displayed on the aircraft magnetic heading.
Proceed the main gyro. We put 436-G in the top position.
Again, press and hold the 436-H, until the cessation of rotation of the axis of main gyro. Controls are on the digital tip GA-3-1.
Axis of gyros on the magnetic course is not displayed perfectly, and between them will angle about a degree. This angle will be chosen later.
Turn off the regime of magnetic correction MK (switch 436-P in the middle of "GPK").
Let's set up blocks gyromagnetic course BGMK. To do so, press and hold fast to align 436-H prior to the termination of the magnetic changes in the course BGMK-2-1. After correction, the rate should match the main course gyro GA-3-1
We put 436-G in the down position, and holding the magnetic course correction control BGMK-2-2. Press and hold 436-H termination changes the magnetic course BGMK-2-2.
After making corrections, all courses are in line tips should coincide with the magnetic heading of aircraft, with a difference of no more than a degree.
Before take-off when the aircraft along the runway just presented, we need to manually adjust the axis of gyros GA-3-1 and GA-3-2 by 436-F switch, as accurately as possible based on the magnetic heading runway. The choice of the unit is made tumblers 436-G. Similarly, the axis of gyros will be transferred to the Meridian airport landing.
Continues preparation of avionics. Set attitude gyros MGV-SK:
Choose the view 1 (captain panel) and adjusts the review in such a way that you can see both the ADI (PKP) (101) and part of the IP-46 panel with a cap 357.
Open the lid 357, press and hold button below it. Seeing ADI turn to act.
Once ADI is aligned, close the lid 357.
Switch toggle switch 405 (on overhead) up and down, close the lid. This resets the bank signal error BKK.
Make sure that the signals are extinguished: "AG kontr" lamp, remove blankery AG with HSI (PNP) and ADI (PKP).
Set the pressure in the SVS, by operate hotspot by altimeter 105 set to zero, and put pressure in futomer UVID-15 (117).
Turn on busters. Open cover 339, turn on three switches, and close cover.
Avionics is prepared, except for the NVU.
Flying in pattern
Start the engine and prepare avionics, as described above.
Turn booster, closing the lid 339 if you don't do it early.
Turn the wheel steering (447), set the streering limit switch (448) to 63 deg (bottom).
Call a hint by clicking on the device 309, and determine the required position of stabilizer, depending on CoG % MAC position. When CoG least 28% selected "P", from 28% to 35% - the "C", more than 35% - the "Z".
Let's taxi. In the process of taxiing extract flaps in position 28, by the joystick or lever controlling 451. Stabilizer automatically take an right position, navigator report.
We put the plane precisely along the runway, and adjusts position of gyros of TKS on the PU-11 panel, switches 436-F, G.
Adjusts to the handle (102-D) the desired course of landing, if you plan to approach. White Arrow (102-F) to indicate a zero on the scale of the demolition of the figures in the PNP (102-C) coincide with the magnetic heading runway.
Turn calculator landing (352) and fly directors (354).
Adjusts handle (102-B) to crosswing course , usually under 90 degrees to the takeoff heading, based on the rolling yellow index of 102-L.
We put the steering switch (448) to 10 deg (up).
If we have done everything correctly, flashing off the placard "not ready for take-off" (155), and the crew will report on the readiness for take-off.
Set throttle to takeoff mode (or nominal if the take-off by nominal trust). Releases the brake (shift + B). Let's go!
During the run, control the speed and listen to the navigator. When the speed reaches Vr, raise the front wheel and taking off. At the time of take-off, are not increase the angle of attack and the sounding of the alarm AUASP.
Retract landing gear after the climb 5-10 m.
We continue to climb and acceleration, so that to a height of 120 m speed was 320-330 km / h. At an altitude of 120 m starting to retract flaps. In the process of retracting, changing the angle of pitch, accelerates the speed so that by the end of a cleaning speed of about 400 km / h (V0, safe speed for the clean wing).
At a height of not less than 450 m set thrust to nominal.
Turn autopilot - tumblers 365, 367, and button-lamp 363. Then the machine operates ABSU. In model, you can press key "D" for activate autopilot.
Upon reaching the desired altitude (about 600-700 m in normal condition), push-button light "H" (361). The longitudinal channel is beginning to stabilize altitude.
We fly our pattern. Push button-lamp "ZK" (348). The plane starts to turn on the course set by the left handle HSI, the yellow index. It is anticipated that the desired heading was set during the preparation procedure.
Managing yellow index "ZK", turn aircraft to downwing leg, controlling the position of the aircraft by radio navigation equippment.
During the downwing leg, reduces the speed so that the beam DPRM to have the speed of 400 km / h.
Set frequency of ILS to nav radio Kurs-MP, turn on landing calculator (352) and fly directors (354).
If the planned landing using autothrottle includes tumblers 373, 374.
Turn to base leg performing with a roll of 15-20 degrees at a speed of 360-370 km / h.
During the flight of 3 to 4-turn, produce flaps to 28, while braking at a speed not exceeding 360 km / h at the end of the release. Deploy gear. Reduce speed to 280-300 km / h.
Turn autothrottle (button 372) and set the desired speed of wheel 375.
Turn to final perform by heading wheel or left handle of HSI (ZK).
After the turn to final leg, at a speed of no more than 300km / h extract flaps to 45. Reduce speed to the value of Vref, and at this speed to fly up to the entrance to the glidepath.
At the moment of crossing the glidepath, if the automatic approach and landing of aircraft configuration, including automatic mode reduction GLISS. If the mode is not enabled, it can force the push of a button, the lamp 355.
If you fly manually \ by director, the plane balanced by using MET trimmer. For descent on glidepath, the deviations of vertical velocity from the estimated correct elevator, the speed deviation - only the rengine thrust. As the regime, the speed of the aircraft in landing configuration quickly drops, so throttle should move cautiously, with a step of no more than 5%.
Automatic mode of approach is necessary to disable the VPR (60 meters at standard conditions). Further descent and landing is done manually.
Fly of runway performed at an altitude of about 15 m.
Span end and fly to a height of 5 meters to continue to produce glidepath. At a height of 5 meters set throttle to idle and begin flare. By the end of flare make landing, the speed will be at 5-10 km / h less than the speed of crossing the front of runway. After landing engage reverse (slats will deploy automatically), gently lower the front landing gear leg and begin braking. At the speed of 140 km / h in normal conditions, reverse off. Apply braking.
We put the switch to turn (448) to 63 (bottom) before taxiing to parking. In the process of taxiing, retract flaps.
