Tu-154B Views: Central panel

Материал из FlightGear

Fig. . Central panel.

301 - Manual stabilizer control switch. To manage, open the cap, there is a switch under cap.

302 - Auto stabilizer handle

303-305 - Engine failure placards

306-308 - Turbine N2 RPM indicators

309 - Elevator and stabilizer gauge. In the center of the device there is a hotspot for call hints for current weight, CoG position, Vr and Vref. The values of velocities are calculated for the current configuration

310 - Flaps indicator

311 - Gear lamps

312 - Turn indicator EUP

313 - Placard "Stab work". Shows the work of resettable electric stabilizer

314, 315 - Placard "Flaps I","Flaps II". Show work of two drive flaps hydro driver. The model has always included together

316, 319 - Placard "middle" spoilers extracted

317, 318 - Placard "inner" spoilers extracted

320 - Speed indicator USVPK. In the "air" mode shows the air speed of the system of SVS, in a "ground" mode - ground speed from the diss equipment . At the bottom of the device there is a hotspot for mode selection

321 - Range-azimuth indicator PPDA-Sh by RSBN equipment

322 - switch the source of ZK (captain-copilot PNP heading)

323, 324 - Placard of spring loaders. In this model, both boards have always managed together, the system of loaders is not implemented

325-327 - Placard neutral position trimmers. On board there are a hotspots to reset trimmers in neutral

328 - Status of RA-56 actuators. This device can be seen on ABSU work, the device shows the output of RA-56 units, attached to the aircraft control

329 - Placard "NVU failure". Failures is not implemented

330 - Placard "Failure of reserve MGVK".

331 - Placard "NVU-VOR Automatic." Lights when the navigation computer ABSU responsible for the operation of the VOR and NVU or with loss of signal VOR. Denial is not implemented

332 - Placard "Correction on". Lights up when the mode of correction signals for NVU RSBN

333, 334 - Placard "Range autonomy","Azimuth autonomy" Lights in the loss of signal range or azimuth of RSBN

335 - Placard Memory Diss. Lights when the system Diss is failure

336 - Placard "Change ChO" Lights for 2 km to the next waypoint

337 - USh navigator instrument. Arrow in a silhouette of the plane shows the main gyro heading from TKS, movable triangular index - position of the reserve gyro. Deviate arrow shows the drift angle, measured equipment Diss

338 - UShDB indicator. While the ADF arrow indicates the angle of the NDB, the VOR mode, the opposite end of the arrow shows the current radial. Selecting the switch is made to the overhead

339 - lid switch booster. Before take-off booster should be included, the lid is closed

340 - Instrument for input angle maps to the NVU. There are hotspots right and left of two mobile scales. The upper scale introduces dec of degrees, lower - ones

341 - Switch navigational lights

342 - Switch flashing lights

343 - Switch lighting instrument boards. Lighting is turned on throughout the cabin, including flight engineer panel

344 - Placard "Slats extend". In this model slats management only incorporated in the flap, a separate management not implemented