Tu-154B Views: Captain's panel
Материал из FlightGear
<< Views | Tu-154B | Overhead >>
Captain's panel
101 - Flight Director Indicator
102 - Horizontal Situation Indicator
103 - Angle-of-attack and acceleration indicator
104 - Rate-of-climb indicator VAR-30
105 - Barometric altimeter. Click lower right button to set pressure
106 - Radio Magnetic indicator IKU-1 , controlled from the compass system TKC-1 and Course system Kurs-MP-2.
107 - Distance measuring indicator IDR-1 (DME/RSBN)
108 - Indicated airspeed indicator US-I-6. The red index refers to commanded speeds for the Autothrottle system. With Autothrottle switched off, the index is slaved to the actual speed
109 - Mach Indicator UM-1, feeded from the SVS system (system of air signals)
110 - Vertical Speed Indicator VAR-75
111 - Clock AChS-2. Additional controls are not implemented
113 - Combined Speed Indicator KUS
114 - External air temperature indicator TNV-15, shows True Air Temperature (TAT). Based on airflow and speed dependent
115 - Backup artificial horizon AGR
116 - Radar altimeter RV-5M. Mouse area in lower part allows to set warning altitude for "H" indicator and sound signal
117 - Altimeter UVID-15, indication in feet. This electrical device is independent from the SVS system.
118 - Altimeter VM-15, SVS dependent
119 - Test/control button for signal light system
120 - Selection of device for the IDR-1 (DME). It differs a bit from the real plane. In the real plane the indicators are independent and have their own panels for different frequency input. Due to the limited channels in the simulator the indicators are blocked from the Course system Kurs-MP. The Kurs-MP system is the Russian equivalent to VOR navigation and has been added for international flights. It was decided to use one channel for the Russian short range Navigation System RSBN. The switch 131 toggles between DME-1, DME-2 and RSBN.
121-123 - Hydraulic systems 1-3 warning lights
124 - Emergency brake system low pressure warning light
125-127 - Hydraulic systems 1-3 pressure gauges
128 - Emergency brake system pressure gauge
129 - Localizer Mode. AFCS stabilizes landing course using ILS
130 - ZK Heading Select Mode. AFCS stabilizes course selected using ZK bug (see HSI, mark D)
131 - Bank Stabilization Mode. AFCS stabilizes banking
132 - NVU mode. AFCS stabilizes course using NVU signals
133 - VOR mode. AFCS stabilizes course using VOR signals
134 - Marker I (outer marker). Flashes while passing outer marker
135 - Marker II (middle marker). Flashes while passing middle marker
136 - Failure of the Roll Monitor Unit BKK-18
137 - Glideslope (Glissade). AFCS stabilizes Glideslope using ILS signal
138 - Autothrottle. Autothrottle is active
139 - Pitch Stabilization". AFCS stabilizes pitch
140 - Altitude Hold Mode (H). AFCS stabilizes altitude by varying pitch
141 - IAS Mode (V). AFCS stabilizes air speed by varying pitch
142 - MACH Mode (M). ABSU stabilizes MACH value by varying pitch
143 - Marker III (Inner Marker) - not used
144 - Fuel Below 2500 KG Warning
145 - AOA Warning
146 - G Overload Warning
147 - Lights up when Pilots send signal about hijacked plane (of course not used in sim)
148 - Lights up if Cabin Crew sends signal about hijacked plane (not used in sim)
149 - Overspeed Warning
150 - Left bank above safe limit (33 deg)
151 - Go Around Mode. AFCS goes around automatically
152 - Decision Height H indicator
153 - Terrain danger
154 - Right Bank above safe limit (33 deg)
155 - Not ready for takeoff. Flashes if pre-takeoff procedures are not completed
156 - False trim, MET Failure or MET has come to a stop or attempt to work on MET during Autopilot operation.
157 - Autopilot (AFCS) - failure in Bank channel (not implemented)
158 - Autopilot (AFCS) – failure in Pitch Channel (not implemented)
159 - Go Around in automatic mode failure (not implemented)
160 - Landing approach CTY failure or Airplane Glidepath deviation exceeded
161 - Autothrottle Control Failure. Operate Thrust manually (not implemented)
162 - Maximum Localizer Deviation during ILS Approach exceeded
163 - Glideslope Deviation, below 100m until DH if plane is 1 dot above glidepath
164 - Engine FIRE (not implemented)
FDI
A - Авиагоризонт
B - Шкала отклонения скорости. Перемещение круглого индекса вверх означает, что скорость выше, чем заданная скорость автотяги
C - Индекс глиссады. Дублирует планку положения глиссады прибора ПНП
D - Шарик индикатора скольжения
Е - Бланкер отказа канала крена
F - Бланкер отказа канала глиссады
G - Бланкер отказа гировертикали
H - Директорная стрелка курса
I - Директорная стрелка глиссады
J - Индекс крена
K - Индекс курса. Дублирует планку отклонения курса прибора ПНП
HSI
A - Шкала дальности. В Ту-154 не используется
B - Кремальера заданного курса
C - Шкала заданного путевого угла (ЗПУ)
D - Кремальера ЗПУ
Е - Подвижная шкала компаса. Может показывать либо гиромагнитный, либо гироскопический курс, в зависимости от положения переключателя на оверхеде
F - Стрелка ЗПУ
G - Планка отклонения курса. Показывает отклонение самолета от ЛЗП в различных режимах работы АБСУ (ILS, VOR, НВУ)
H - Планка отклонения глиссады
I - Бланкер отказа глиссады
J - Бланкер отказа курса
К - Бланкер отказа курсовой системы
L - Подвижный индекс заданного курса (ЗК)
M - Индикатор режима (СП-VOR-НВУ)
N - Шкала сноса. Подвижный теругольный индекс показывает угол сноса, измеренный аппаратурой ДИСС
