Content      ..     43      44      45      46     ..

Boeing 737 - 600/700/800/900. Operations Manual (1997 year) - page 45

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

PFD Instrument Landing System Indications

[Option - Integrated cue command bar, rising runway]

IBFI/130°

1

DME 3.4

3

MM

4

5

2

1

Approach Reference

Displays the selected ILS identifier or frequency, approach front course, and

ILS/DME distance.

If the tuned ILS frequencies disagree, the frequency turns amber with an amber

horizontal line through it.

If the approach courses entered in the MCP disagree, the course turns amber with

an amber horizontal line through it.

2

Localizer Pointer and Deviation Scale

The pointer:

• indicates localizer position relative to the airplane

• in view when the localizer signal is received

• fills in solid magenta when within 21/2 dots from center.

10.11.16

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

5

Rising Runway (green with magenta stem)

[Option - Rising runway]

Displayed when:

• localizer signal usable and pointer is in view

• radio altitude is less than 2500 feet.

Rises towards airplane symbol when radio altitude is below 200 feet.

Expanded Localizer Indications

1

1

Expanded Localizer Scale

[Option - Autopilot or flight director activation]

Displayed when the autopilot or flight director is in LOC mode, deviation is

slightly more than one half dot and track is within 5 degrees of the MCP selected

course.

As deviation increases, the deviation pointer remains filled in solid magenta and

parks at the limit of the expanded scale. Once the deviation reaches the equivalent

of 2.4 dots from center on the standard scale, the pointer becomes unfilled.

Reverts to standard scale when out of LOC mode, and groundspeed is less than 30

knots or radio altitude is greater than 200 feet.

A rectangle equals 1/2 dot deviation.

PFD Radio Altitude Indications

[Option - Radio altitude above, round dial]

1250

1

300

10.11.18

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

1

Radio Altitude - Round Dial

[Option - Radio altitude above, round dial]

Displayed below 2500 feet AGL:

• digital display from 2500 to 1000 feet AGL

• box highlighted white for 10 seconds upon descent below 2500 feet

• round dial displays below 1000 feet AGL

• pointer indicates selected radio altitude minimums

• the circumference of the dial is added to, or taken away from, to depict the

airplane’s radio altitude

• the remaining perimeter and pointer turn amber and flash for 3 seconds

when below radio altitude minimums, the numeric readout does not flash.

Traffic Alert and Collision Avoidance Indications

[Option - Integrated cue command bar]

1

1

Traffic Alert and Collision Avoidance System Pitch Command (red)

The area(s) inside the red lines indicate(s) the pitch region(s) to avoid in order to

resolve the traffic conflict. The airplane symbol must be outside the TCAS pitch

command area(s) to ensure traffic avoidance. Refer to Chapter 15, Warning

Systems.

10.11.19

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

GPWS Annunciations

[Option - Integrated cue command bar]

1

PULL UP

1

GPWS Annunciations (red)

Displays WINDSHEAR or Pull UP alert.

Refer to Chapter 15, Warning Systems.

10.11.20

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

PFD - Altitude Indications

Altitude Indications- General

The altitude

indication

displays

ADIRS altitude

and

other

altitude

related

information.

4

5

M

1554

5100

5200

1

6

OM

5

000

2

1

2

1463M

3

4

800

1

4

600

2

6

1000

BARO

450

1011 HPA

1

Selected Altitude Bug (magenta)

Indicates the altitude set in the MCP altitude window.

When the selected altitude is off scale, the bug is parked at the top or bottom of

the tape, with only one half the bug visible.

2

Metric Digital Readout (readout and box-white, metric symbol-cyan)

Displays current altitude in meters when MTRS is selected on the EFIS control

panel.

10.11.21

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

3

Current Altitude

Displays current altitude in increments of thousands, hundreds and twenty feet:

• for positive values of altitude below 10,000 feet, a green crosshatch

symbol is displayed

• a negative sign appears when altitude below zero feet is displayed

• readout box becomes bold to denote altitude acquisition

• readout box is highlighted in amber and flashes to denote altitude

deviation (refer to Chapter 4, Automatic Flight and Chapter 15, Warning

Systems).

4

Metric Selected Altitude Readout (readout-magenta, metric

symbol-cyan)

Displays MCP altitude in meters when MTRS is selected on the EFIS control

panel.

5

Selected Altitude (magenta)

Displays the altitude set in the MCP altitude window.

The selected altitude box appears in white during an altitude alert. For more

information, refer to Chapter 15, Warning Systems.

PFD Barometric Indications

[Option - Altimeter with QFE]

2

4 400

24400

1

29.86

IN

QFE

STD

29.86 IN QFE

3

1

Barometric Settings (green)

Indicates the barometric setting in either inches of mercury (IN) or hectopascals

(HPA) as selected on the EFIS control panel.

Display is boxed amber if numeric is set and airplane is climbing above transition

altitude, or if STD is set and descending below transition flight level.

2

Preselected Barometric Setting (white)

STD is displayed when the Barometric Standard (STD) switch is selected on the

EFIS control panel.

10.11.22

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

When STD is displayed, a barometric setting can be preselected on the EFIS

control panel barometric selector and is displayed below STD.

3

QFE Altitude Reference (green)

[Option - Altimeter with QFE]

Indicates QFE altitude reference if selected on the CDU APPROACH REF Page

or TAKEOFF REF Page 2/2.

When selected, QFE is boxed for 10 seconds.

The altitude tape is shaded green during QFE operation.

When QNH is selected, the green shading is removed; QNH is displayed for 10

seconds, then blanks.

When STD is displayed, QFE in small white characters is displayed below STD,

and a QFE altimeter setting can be preselected.

Landing Altitude/Minimums Indications

[Option - Radio altitude above ADI, landing altitude reference bar]

RADIO

200

5200

3

6

OM

5

000

2

4

1

4

800

1

1

4

600

2

2

6

600

BARO

3

4700

1011 HPA

10.11.23

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

4

Landing Altitude Reference Bar

[Option]

Indicates height above touchdown:

• White bar - 500 to 1000 feet above landing altitude

• Amber bar - 0 to 500 feet above landing altitude.

PFD - Vertical Speed Indications

Vertical Speed Indications - General

The vertical speed indication displays ADIRS instantaneous vertical speed.

[Option - VSI TCAS advisory]

6

2

4

1

1

1

2

2

6

3

500

1

Vertical Speed Pointer (white)

Indicates current vertical speed.

2

Selected Vertical speed Bug (magenta)

Indicates the speed selected in the MCP vertical speed window with V/S pitch

mode engaged.

3

Vertical speed (white)

Displays vertical speed when greater than 400 feet per minute.

The display is located above the vertical speed indication when climbing and

below when descending.

10.11.25

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

4

TCAS Vertical Speed Tape (red)

[Option - VSI TCAS advisory]

Tape turns red to indicate vertical speed values to avoid or exit during a TCAS

resolution advisory.

Vertical speed pointer is red if it is within the vertical speed tape range.

Supplements TCAS resolution advisory pitch commands on the attitude

indication.

PFD - Heading and Track Indications

Heading and Track Indications- General

The heading and track indications display current FMC/ADIRS heading, track and

other information.

1

4

2

3

135

H

MAG

5

1

Current Heading Pointer (white)

Indicates current heading.

2

Track Pointer (white)

Indicates current track.

3

Selected Heading (magenta)

Digital display of the selected heading bug.

4

Selected Heading Bug (magenta)

Indicates the heading selected on the mode control panel. If the selected heading

exceeds the display range, the bug parks on the side of the compass rose in the

direction of the shorter turn to the heading.

10.11.26

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

5

Magnetic/True Heading Annunciation (green)

Displays selected heading reference:

• MAG indicates display is oriented relative to magnetic north

• TRU indicates display is oriented relative to true north; a white box is

displayed continuously around TRU

• transition from TRU to MAG results in a green box around MAG for 10

seconds

• when TRU is displayed and the airplane descends more than 2000 feet at

a descent rate greater than -800 feet per minute, an amber box is drawn

around TRU; the box flashes for 10 seconds, then turns steady amber.

PFD Failure Flags

The flag replaces the appropriate display to indicate source system failure or lack

of computed information.

[Option - Radio altitude below ADI, Angle of Attack indicator

1

10

17

2

SEL SPD

11

DME

AOA

12

SPD

3

LIM

NO

4

V

13

FPV

FD

S

ATT

P

D

V

S

G

A

5

E

14

P

/

L

R

D

S

T

T

6

15

PITCH

ROLL

7

RA

LOC

8

LDG

ALT

16

9

HDG

1

Distance Measuring Equipment (amber)

The DME system has failed.

10.11.27

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

[Option - Radio altitude above ADI]

9

1

10

2

SEL SPD

DME

RA

11

SPD

3

LIM

12

NO

4

V

13

FPV

FD

S

ATT

P

D

V

S

G

A

5

E

14

P

/

L

R

D

S

T

T

6

15

PITCH

ROLL

LOC

7

LDG

ALT

16

8

HDG

1

Distance Measuring Equipment (amber)

The DME system has failed.

2

Selected Speed (amber)

Invalid data.

3

Speed Limit Flag (amber)

Displays related with stick shaker or maximum operating speed has failed:

• if the stick shaker warning has failed, the red and black stick shaker speed

bar is removed

• if the maximum operating speed has failed, the red and black maximum

operating speed bar is removed.

4

No V Speeds Flag (amber)

V1 (decision speed) or VR (rotation speed) has not been entered or is invalid.

5

Speed Flag (amber)

The speed indication is inoperative. All indication markings are removed.

10.11.30

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

16

Landing Altitude Flag (amber)

The landing altitude input is not available or invalid.

Additional Annunciations and Alerts

Displays Control Panel Annunciation

A

L

1

T

2

6

1000

BARO

450

DISPLAYS

1

CONTROL PANEL

1

Displays Control Panel Annunciation (amber)

With the CONTROL PANEL select switch on the overhead panel in:

• BOTH ON 1 - left (Capt) EFIS control panel has failed

• NORMAL - corresponding EFIS control panel has failed

• BOTH ON 2 - right (F/O) EFIS control panel has failed.

Altitude information is removed.

10.11.32

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

Display System Annunciations

Note: The following annunciations occupy the same display location in the lower

left corner of the primary flight display.

80

CDS

MAINT

135

H

MAG

1

1

Display System Annunciations

DSPLY SOURCE (amber) - A single DEU has been selected, either manually or

automatically, to drive all six display units.

• If the DEU fails on the same side as the engaged autopilot during climb or

descent -

[Option - Integrated cue command bar]

• the flight directors are removed from both pilots’ displays. The flight

directors reappear at ALT ACQ

• the pitch mode reverts to CWS pitch

• the autopilot remains engaged.

• If the DEU fails on the same side as the engaged autopilot during level

flight -

• climb or descent to a new MCP altitude is not possible in LVL CHG,

VNAV, or V/S modes with the autopilot engaged.

• If the DEU fails on the opposite side as the engaged autopilot or while in

manual F/D mode during climb or descent -

[Option - Integrated cue command bar]

• the flight director is removed from the pilot’s display on the failed side

until ALT ACQ

• climb or descent is possible in LVL CHG, VNAV or V/S modes with

the autopilot engaged.

• If the DEU fails on the same side as the engaged autopilot in the

APPROACH mode -

10.11.33

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

[Option - Integrated cue command bar]

• the flight directors are removed from the pilot’s display on the failed

side.

[Option - With CDS Block 99 software upgrade or higher]

CDS MAINT (white) - A dispatchable CDS fault has occurred. Displayed on the

ground only, prior to start of the second engine.

[Option - Without CDS Block 99 software upgrade or higher]

CDS MAINT (white) - A non-dispatchable CDS fault has occurred. Displayed on

the ground only, prior to start of the second engine.

CDS FAULT (amber) - A non-dispatchable CDS fault has occurred. Displayed

on the ground only, prior to start of the second engine.

Instrument Switch Annunciation

135

H

MAG

INSTR SWITCH

1

1

INSTR SWITCH Annunciation (amber)

Indicates both the Captain’s and First Officer’s displays are using the same source

of IRU data.

Displayed when the IRS switch on the overhead panel is not in the NORMAL

position.

10.11.34

Flight Instruments, Displays -

PFD/ND - Displays

Boeing 737 Operations Manual

Airspeed Disagree Alert

148

180

1

160

R

140

V1

1245

100

1

80

IAS

DISAGREE

1

Airspeed Disagree Alert (amber)

Indicates the Captain’s and F/O’s airspeed indications disagree by more than 5

knots for 5 continuous seconds.

10.11.35

Content      ..     43      44      45      46     ..