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Note: Do not engage either autopilot.
* * * *
737
Flight Manual
Continental
FLT MGMT, NAV
Sec. 2.11 TOC-1
Rev. 11/15/02 #41
2.11 – FLIGHT MANAGEMENT, NAVIGATION
TABLE OF CONTENTS
CDU FAIL ................................................................................................ 1
BCD DUAL FMC FAILURE .......................................................... 2
FMC/CDU ADVISORY MESSAGES ...................................................... 3
FMC/CDU ALERTING MESSAGES....................................................... 7
>>@ FMC FAILURE WITH SINGLE FMC .................................. 11
BCD GPS .................................................................................... 11
IRS ALIGN LIGHT FLASHING ............................................................. 12
IRS DC FAIL.......................................................................................... 12
> IRS FAILURE (IN FLIGHT)............................................................. 13
IRS FAULT ............................................................................................ 13
IRS MODE SELECTOR PLACED IN ATTITUDE (ATT)
MODE PRIOR TO TAKEOFF........................................................ 14
IRS ON DC............................................................................................ 15
LOSS OF ALIGNMENT (INFLIGHT).................................................... 16
BCD SINGLE FMC FAILURE WITH DUAL FMC’S................... 17
VHF NAV FAILURE .............................................................................. 18
VOR/ILS NAVIGATION SYSTEM FAILURE........................................ 18
FLT MGMT, NAV
Sec. 2.11 TOC-2
Rev. 11/15/02 #41
Continental 737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
FLT MGMT, NAV
Sec. 2.11 Page 1
Rev. 11/15/02 #41
FLIGHT MANAGEMENT, NAVIGATION
CDU FAIL
Note: If FMC annunciation is displayed in the center of the CDU you
have had:
BCD DUAL FMC Failure.
>>@ SINGLE FMC Failure.
Refer to the applicable Abnormal above.
IF One CDU Display Is Completely Blank And Other Side Is Operable
Check FMCS C/Bs (>>@ P18-2, E6-9) (BCD P6-1,
D15 &16; P18-2, A6 & 7, E8).
Operable CDU may be used to make all required entries.
* * * *
IF Both CDU Displays Are Completely Blank Check FMCS C/Bs
(>>@ P18-2, E6-9) (BCD P6-1, D15 &16; P18-2, A6 &
7, E8).
FMC/CDU, LNAV and VNAV are inoperative. Resume conventional
navigation.
BCD Refer to (in the DUAL FMC FAILURE Non-Normal)
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OR
FLT MGMT, NAV
Sec. 2.11 Page 2
Rev. 11/15/02 #41
Continental
737
Flight Manual
BCD DUAL FMC FAILURE
The failure of both FMC’s is indicated by:
· FMC ALERT light.
· Failure of MAP information on both sides.
· Blank MCDU except for MENU with ACARS available.
If dual FMC failure occurs the FMC, LNAV and VNAV are inoperative.
Resume conventional navigation.
Select VOR or APP as appropriate on the displays control panel.
Ensure appropriate NAV frequency has been selected to the active
side of the NAV control panel.
Note: When preparing for approach:
· Use SPD REF selector located above upper engine display
to set the reference airspeed bugs for VREF. This speed is
found in the QRH / Flight Manual Sec. 5 performance
section. Set the current WT so the displayed VM speed
bugs will be displayed correctly. Ensure selector is
returned to SET after speed entry is made.
· Use the N1 SET located above upper engine display to set
the N1 bugs for appropriate go around setting.
* * * *
737
Flight Manual
Continental
FLT MGMT, NAV
Sec. 2.11 Page 3
Rev. 11/15/02 #41
FMC/CDU ADVISORY MESSAGES
These messages relate to incorrect scratch pad entries or to FMC/CDU status.
This is a general list: some messages may not apply to all FMC configurations.
The white CDU MSG light illuminates and the message is displayed in the CDU
scratch pad. Some messages will displace an existing scratch pad entry and are
displayed immediately when generated. Other messages will not be displayed
until the scratch pad has been cleared; however, the MSG light will still be
illuminated. A new entry in the scratch pad overrides any displayed message.
Messages caused by CDU entry errors are displayed only on the associated
CDU; other messages are displayed on both CDUs. When multiple messages
have been generated, they will be stacked for display in priority sequence, or in
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