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9.32
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737 Flight Crew Operations Manual
Non-Normal Checklists Chapter NNC
Flight Instruments, Display Section 10
Copyright © The Boeing Company. See title page for details.
TOC.10.1
Table of Contents
NNAC.I10R NSoPn-ENEormDa lU CNhecRklEistLs-IFAligBht LInEstr u.m . e.n t.s ,. D. i.s p.l a.y . . . . . . . . . . . . . . . . . . . . 10.1
FLIGHT RECORDER OFF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.1
SG FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10.1
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Copyright © The Boeing Company. See title page for details.
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10.1
10.1
NNC.10 Non-Normal Checklists-Flight Instruments
Condition: Pitch attitude not consistent with existing phase of
flight, altitude, thrust, and weight, or noise and/or low
frequency buffeting.
Crosscheck ground speed and winds provided by the IRS
and FMC to determine airspeed accuracy if indicated
airspeed is questionable.
Note: Erroneous or unreliable airspeed indications may be
caused by blocked or frozen pitot-static system(s), or
a severely damaged or missing radome.
Condition: The flight recorder OFF light illuminated indicates
that the recorder is not operating.
No crew action required.
Condition: The SG FAIL alert or blanking of both EADI and EHSI
displays indicates a failure of the related symbol
generator.
EFI TRANSFER SWITCH . . . . . . . . . . . . . . . . . . AS REQUIRED
Do not engage either autopilot.
AIRSPEED UNRELIABLE
AIRPLANE ATTITUDE/THRUST . . . . . . . . . . . . . . . . . . ADJUST
Maintain airplane control. Attitude and thrust information
is provided in the Performance-Inflight section.
PITOT STATIC HEAT . . . . . . . . . . . . . . . . . . . . . . . . .CHECK ON
MACH/AIRSPEED INDICATORS . . . . . . . . . . . CROSS CHECK
FLIGHT RECORDER OFF
SG FAIL
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
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December 1, 2000
737 Flight Crew Operations Manual
Non-Normal Checklists Chapter NNC
Flight Management, Navigation Section 11
Copyright © The Boeing Company. See title page for details.
TOC.11.1
Table of Contents
NNC.11 Non-FMC/CDNoUrm Aal LChEeRckTlisItNs-FGlig Mht MEaSnSagAemGenEt, N .a .v i.g a. t.io .n . . . . . . . . . . . . . . . . . 11.1
FMC FAIL - SINGLE FMC AIRPLANES . . . . . . . . . . . . . . . . . . 11.1
FMC FAIL - DUAL FMC AIRPLANES . . . . . . . . . . . . . . . . . . . . 11.2
INSTRUMENT SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.2
IRS DC FAIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.3
IRS FAULT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.4
IRS ON DC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11.5
UNABLE REQD NAV PERF - RNP . . . . . . . . . . . . . . . . . . . . . . . 11.6
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Copyright © The Boeing Company. See title page for details.
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11.1
11.1
NNC.11 Non-Normal Checklists-Flight Management, Navigation
Condition: The FMC alert light and MSG light illuminated indicate
an FMC/CDU alerting message exists.
Take action as required by the message.
Condition: Illumination of the FMC alert light accompanied by
loss of information on the CDU.
Resume conventional navigation.
[Without an operating FMC, LNAV and VNAV are not available.
AN/CDU LNAV operation is available (as installed).]
When preparing for approach:
Use the manual N1 set knobs to set the N1 bugs.
FMC/CDU ALERTING MESSAGE
FMC FAIL - SINGLE FMC AIRPLANES
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
11.2
11.2
Condition: Illumination of the FMC alert light accompanied by:
• loss of FMC information on both CDU’s and loss of FMC data on the
captains’s navigation display map mode indicates left FMC failure
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