First officer’s instruments

First officer¶s instruments

Panel Panel light control PANEL LIGHT CONTROL

apttains control regula regul ates the PUSH/ROTATE  ± Cap  brightness of the integr al instrument lighting in the Cap C apttain and center instrument  pa  panels nels and the dis p dis pllay ayss and edge lighting of the Auto p Auto pilot ilot Flight Director Mode Control Panel Pa nel First Officers control regula regul ates First Officers  pa  panel nel and integr al instrument lighting.

GPWS INOPERATIVE LIGHT (amber) ILLUMINATED  ± GPWS com puter malfunction or  power loss.

GPWS

CONTROLS

Invalid in puts are being received from the r adio altimeter, ADC, or  ILS receiver with a MARK II GPWS com puter installed; r adio altimeter, ADC, ILS receiver, IR S, FMC, Digital Stall Warning (Management) com puters, or EFIS Control Panel with A MARK V GPWS com puter installed.

GROUND PROXIMITY SWITCH  NORMAL (guarded  position)

± Flap and landing gear  position logic is  provided for  Modes 2, 3, and 4. INHIBIT SWITCH ±

Inhibits or cancels warnings/alerts caused by the flaps not in the 30 or 40  position (FLAP INHIBIT), or  landing gear not down (GEAR INHIBIT). GROUND PROXIMITY SYSTEM TEST SWITCH

MARK V GPWS Com puter  PRESS (momentary on the ground, or above 1000 feet radio altitude inflight)

Illuminates the BELOW G/S, PULL UP, WINDSHEAR and INOP Lights, dis plays the EADI WINDSHEAR message, and causes the ³ GLIDE SLOPE´, ³WHOOP, WHOOP PULLUP¶, and ³WINDSHEAR´ aur als to sound. PRESS (at least 10 seconds, on the ground)

The a bove indications always occur first, followed by any additional aur als. The system test is inhibited from liftoff to 1000 feet r adio altitude.

Wndshd/foot air  WINDSHIELD/FOOT AIR CONTROLS

A pplies conditioned air to the No. 1 windows for anti-fogging.

A pplies conditioned air to the  pilot¶s leg position.

CHRONOGRAPH (CHR) CONTROL PRESS ± Controls the start, sto p and reset functions of the CHR Dis play and Second hand with successive ³ push´ o per ations.

TIME DISPLAY

Clock 

Dis play time in 24-hour format 9hours and minutes)/date in numerical format.

Overrides any existing ET Dis plays.

DATE CONTROL

Controls Date Dis play. PRESS ± Dis plays Date (DAY MO) alternating with YR at 1 second intervals.

Allows date to be set with time control.

TIME CONTROL

Controls the Time/Date Dis play RUN ± Starts

CHRONOGRAPH SECOND HAND

the Time/Date Dis play

counting.

Indicates chronogr aph seconds.

(Hold) ± Sto ps the Time/Date Dis play, sets seconds to zero, and advances years. HLD Y

Controlled by the CHR Control.

(Slow SS M 

Slew) ± Advances the Time/Date Dis play minutes/months.

ELAPSED TIME (ET) CONTROL

(s pring-loaded to HLD) RESET

HLD

- Returns the ET Dis play to zero time.

(Hold) ± Sto ps the ET Dis play at the indicated time.

RUN ± Starts

the ET Dis play counting time. Continues to count from HLD time when selected back to R U N.

(Fast Slew) ± Advances the Time/Date Dis play hours/days. FS D

ET/CHR DISPLAY

Dis plays Elapsed Time or Chronogr aph Time. ET Display Range : zero to 99 hrs 59 min. CHR Display Range : zero to 99 min.

Vertical s peed indicator  VERTICAL SPEED POINTER 

De picts r ate of climb or descent from 0 to 6000 feet  per minute. Indicates zero when IR S vertical s peed is unrelia ble.

OFF FLAG IN VIEW  ± The air data com puter  altitude r ate signal is lost, or a malfunction exists.

Selected IR S vertical s peed data are unrelia ble, or  Res pective VSI and/or ADC has f ailed.

Air tem per ature indicator  TAT/SAT/TAS ANNUNCIATORS

ILLUMINATED  ± Identifies the type of  data being dis played on the Digital Dis play.

DIGITAL DISPLAY

Dis plays TAT (oC), SAT (oC), or TAS (knots) indications in digital form.

SELECTOR PUSHBUTTON PRESS ± Sequences the dis play from TAT, to SAT, to TAS.

PRIMARY ALTIMETER  (electric)

DIGITAL COUNTER 

Altimeter 

Dis plays altitude in increments of thousands, hundreds and twenty feet. Warning flag appears whenever the ADC signal is lost or malfunction exists. Green

flag appears in the left window when altitude is below 10,000 feet.

A NEG flag appears in the two left-hand windows when altitude below zero feet is dis played.

ALTITUDE POINTER 

Makes one revolution each one thousand feet. BAROMETRIC SETTING WINDOW

REFERENCE ALTITUDE MARKER 

Manually positioned to the desired reference altitude using the Reference Altitude Marker  Control..

Reflects barometric correction (in millibars and inches of mercur y as set by the Barometric Setting Control.

BAROMETRIC SETTING CONTROL ROTATE ± Adjusts the barometric correction in the Barometric Setting Window.

REFERENCE ALTITUDE MARKER CONTROL

Used to manually set the Reference Altitude marker.

MACH/AIRSPEED INDICATOR (electric)

Mach airs peed indicator  AIRPSEED CURSOR  MODE ANNUNCIATOR 

Auto Mode: Out of View Manual Mode: In View

AIRSPEED CURSOR 

Indicates target airs peed.

Positioned manually or automatically, as selected by the Airs peed Cursor Control. MACH DIGITAL COUNTER 

Shows Mach number, from .40 to .99 Mach, in digital form.

VMO POINTER 

Indicates the maximum o per ating (indicated) airs peed in knots.

Masked below .40 Mach Digits are covered by a warning flag when the dis play is unrelia ble.

VMO FLAG IN VIEW: Indicates the MO is ino per ative.

AIRSPEED CURSOR FLAG Manual mode: Flag is retr acted.

AIRSPEED POINTER  Indicates airs peed in knots. AIRSPEED CURSOR CONTROL PUSH IN - Auto Mode.

Airs peed Cursor is  positioned from the AFDS FCC.

Auto mode : Flag in view if Airs peed Cursor signals, as determined by the AFDS FCC, are unrelia ble. AIRSPEED DIGITAL COUNTER 

Digital dis play of indicated airs peed in knots. Warning flag covers the counter when the Airs peed Pointer and Airs peed Digital Counter are unrelia ble.

AIRSPEED MARKER ( bugs)

Positioned manually to the desired airs peed reference.

DME INDICATORS

300 nautical miles maximum search for all DME stations

R adio distance magnetic indicator  Warning Flag. Electrical Power lost or invalid DME receiver.

DME receiver  powered,  but not receiving a DME station, BEARING POINTER NO.1 or during Agility ±Tuning. WARNING FLAG VOR MODE - Power f ailure.

HEADING WARNING FLAG Selected com pass signal is invalid.

VHF NAV signal unrelia ble. ADF MODE - Power f ailure.

Power f ailure.

BEARING POINTERS

Signals to the VOR Bearing Pointers are not affected by the VHF NAV tr ansfer switch.

BEARING POINTER NO. 2 WARNING FLAG

NARROW POINTER  ± Uses signals from the VHF NAV receiver   No. 1 or ADF No. 1 receiver. WIDE POINTER  ± Uses signals from VHF NAV receiver No. 2 when in VOR mode.

ADF No. 2 receiver not installed.

VOR MODE ± Power f ailure.

VHF NAV signal unrelia ble. ADF MODE ± Always in view. ADF NO. 2 not installed. ADF/VOR BEARING POINTER SWITCHES PRESS ± Selects ADF or  VOR for the bearing pointer.

HYDRAULIC BRAKE PRESSURE INDICATOR  Indicates accumulator  precharge plus residual hydr aulic  pressure prior to activation of any hydr aulic  pum p.

Hydr aulic indicators  Normal pressure ± 3000 psi.

Maximum pressure ± 3500 psi.  Normal precharge ± 1000 psi.

HYDRAULIC SYSTEM PRESSURE INDICATOR  Indicates hydr aulic system A and B pressure.

When both  pum ps for a system are OFF, the res pective pointer reads zero.  Normal pressure ± 3000 psi. Maximum pressure ± 3500 psi.

HYDRAULIC SYSTEM QUANTITY INDICATORS SYSTEM A ± F (full) 4.7 U.S. gallons

RFL (refill) 4.2 U.S. gallons. SYSTEM B  ± F (full) 7.2 U.S. gallons

RFL (refill) 6.4 U.S. gallons.

Marker beacon lights MARKER BEACON LIGHTS AIRWAYS (white) ± Illuminates over an inner or airways marker beacon.  AIRWAYS

MIDDLE (amber) ± Illuminates over a middle marker beacon. OUTER (  blue) ± Illuminates over an outer marker beacon.

 MIDDLE

OUTER 

GPWS

indicator  PULL UP WARNING LIGHT (red)

BELOW GLIDE SLOPE ALERT LIGHT (amber) ILLUMINATED  ± Air   plane is more than 1.3 dots below the glide slo pe. PRESS ± Inhibits or cancels below glide slo pe alerting if  pressed while in the alerting area.

ILLUMINATED  ± Indicates that one or  more of the following conditions exist:

Excessive descent r ate Excessive terr ain closure r ate Altitude loss after takeoff or go-around Unsafe terr ain clear ance when not in the landing configur ation.

FLIGHT DIRECTOR COMMAND BARS (magenta)

Dis played when res pective FD switch is ON and valid command steering is availa ble or during automatic o per ation of the FD.

ADI

Blanked when the res pective FD switch is OFF, or  command steering becomes invalid. GLIDESLOPE POINTER AND DEVATION SCALE

(magenta/white) FLIGHT MODE ANNUNCIATIONS

Pointer indicates glideslo pe  position. Scale indicates deviation. Pointer is not dis played when the glideslo pe signal is unusa ble or when tr ack and the front course on the MCP differ by more than 90o ( back Course)

BANK INDICATOR AND SCALE (white)

PITCH LIMIT SYMBOL (yellow)

DECSION HEIGHT (green)

Indicates  pitch attitude corres ponding to stick shaker activation with flaps extended.

Dis plays selected decision height as set on the EFIS control  panel when r adio altitude is a bove 1000 feet AGL. Blank when negative DH is selected.

SPEED TAPE

RADIO ALTITUDE (white)

Dis plays r adio altitude below 2,500 feet AGL. Blanked a bove 2,500 feet AGL.

AIRPLANE SYMBOL ( black with white outline)

Changes color from white to yellow when below selected DH on descent.

CURRENT MACH (white)

Changes to white when  passing selected DH  plus 75 feet during go-around, after touchdown or after  pressing R ST Switch on EFIS Control Panel.

Dis played when MACH increases a bove .40 Mach. Dis play is blanked when Mach decreases below .38 Mach. GROUNDSPEED (white)

Dis plays FMC/IR S grounds peed in knots. LOCALIZER POINTER AND DEVIATION SCALE (magenta/white)

Pointer indicates localizer  position. Scale indicates deviation. When LOC is engaged and deviation is slightly more than one half dot scale ex pands. Pointer is blanked when ILS LOC signal is too weak to be usa ble.

HORIZON LINE AND PITCH ANGLE SCALE (white) RISING RUNWAY (green)

Dis played when Localizer Pointer is in view and r adio altitude is valid. Rises towards air  plane symbol when r adio altitude is  below 200 feet AGL.

Auto pilot controls and indicators

Click on button or switch to view details

Auto pilot controls A/P and indicators

AUTOPILOT DISENGAGE LIGHT (red/amber)

Flashes red and tone sounds when auto pilot has disengaged. Can be reset by pressing either disengage light or either A/P disengage switch. Steady red if: Sta bilizer is out of trim below 800 feet on a dual channel approach. Altitude acquire mode is inhibited during an A/P go-around. (Sta bilizer not trimmed for a single A/P o per ation). Test switch is held in  position 2. Failure of automatic ground system tests. Steady Amber when flight mode annunciator test switch held at position 1. Flashes Amber if A/P automatically reverts to CWS pitch or roll while in CMD. Resets when either light is  pressed or another mode engaged.

Auto pilot controls A/T and indicators AUTOTHROTTLE DISENGAGEMENT LIGHT (red/amber) FLASHING RED: Autothrottle has disengaged. STEADY RED: When flight mode annunciator test switch is held at position at position 2. STEADY AMBER : When flight mode annunciator test switch is held at position 1. FLASHING AMBER : Indicates A/T airs peed error if s peed not held within +10 or ±5 knots of commanded s peed when all of following conditions exist: In Flight: Flaps not u p, A/T engaged in MCP SPD, or FMC SPD mode.

An automatic test of the A/T flashing amber function is  performed if the A/T is engaged and following conditions exists: MCP SPD or FMC SPD is A/T active mode. More than 150 seconds after lift-off. Flaps Extended. A/T amber light flashes for 2 seconds, rem ains extinguished for 2 seconds and then flashes for 2 seconds again.

Auto pilot controls test and indicators

TEST SWITCH  ± Spring loaded to center  position. TEST 1 ± Illuminate steady amber. TEST 2 ± Illuminate Steady red.

Auto pilot controls fmc and indicators FMC ALERT LIGHT (amber) ILLUMINATED  ± 

The FAIL light on the CDU(s) is illuminated, or  An alerting message exists for both CDU(s), or  The TEST switch is in  position 1 or 2.

ALT ALERT ALTITUDE ALERT ANNUNCIATION

One on each pilot¶s primar y dis play a bove altimeter. ILLUMINATED (amber) ±  STEADY ± acquisition alert:

Within 900 feet from MCP ± selected altitude, ALT ALERT annunciation shows Momentar y tone also sounds Within 300 feet from MCP ± selected altitude, ALT ALERT annunciation no longer sounds FLASHING ± deviation alert:

Deviation more than 300 feet from MCP ± selected altitude, ALT ALERT annunciation flashes Momentar y tone also sounds Flashing continues until: Altitude deviation less than 300 feet, or  Altitude deviation more than 900 feet, or  New MCP altitude selected

MAGNETIC/TRUE REFERECENCE HEADING POINTER 

EHSI

CURRENT TRACK  DISTANCE TO NEXT ACTIVE WAYPOINT

ESTIMATED TIME OF ARRIVAL AT NEXT ACTIVE WAYPOINT

SELECTED HEADING BUG

WEATHER RADAR RETURNS

ACTIVE LNAV ROUTE POSITION TREND VECTOR 

AIRPLANE SYMBOL