Preface -Revision Record 737 Flight Crew Operations Manual
Section 11 - Flight Management, Navigation
IRS Entries SP.11.4 - Changed for 737 cross-model standardization.
Section 16 - Adverse Weather
Introduction SP.16.1 -Revised Supplementary Procedures to match the new standardized Normal Procedures. This change affects multiple pages in this chapter/section. SP.16.1 - Deleted reference to crosswinds when operating from slippery runways. Hot Weather Operation SP.16.14 - Added 737-600 and 737-700 information. Precautions SP.16.17 - Revised for clarity.
Chapter PD - Performance Dispatch Section 11 - Enroute
Flight Crew Oxygen Requirements PD.11.6 - Corrected typo, as 35 degrees C are equivalent to 95 degrees F.
Section 21 - Enroute
Flight Crew Oxygen Requirements PD.21.6 - Corrected typo, as 35 degrees C are equivalent to 95 degrees F.
Section 31 - Enroute
Flight Crew Oxygen Requirements PD.31.6 - Corrected typo, as 35 degrees C are equivalent to 95 degrees F.
Section 41 - Enroute
Flight Crew Oxygen Requirements PD.41.6 - Corrected typo, as 35 degrees C are equivalent to 95 degrees F.
Section 51 - Enroute
Flight Crew Oxygen Requirements PD.51.6 - Corrected typo, as 35 degrees C are equivalent to 95 degrees F.
Copyright . The Boeing Company. See title page for details.
September 29, 2005
0.4.5
Preface -Revision Record 737 Flight Crew Operations Manual
Section 61 - Enroute
Flight Crew Oxygen Requirements PD.61.6 - Corrected typo, as 35 degrees C are equivalent to 95 degrees F.
Chapter 1 - Airplane General, Emergency Equipment, Doors, Windows Section 10 - Dimensions
Turning Radius
1.10.4 - Added the word clearance which was inadvertently omitted in earlier versions.
Section 40 - Systems Description
PSU Oxygen Mask Compartment
1.40.22 - Deleted text which applied to the 737-700C passenger oxygen mask compartment.
Chapter 4 - Automatic Flight Section 10 - Controls and Indicators
Vertical Navigation
4.10.8 - Added information on Mode S transponders.
Section 20 - System Description
Autothrottle Disengagement
4.20.8 - Changed description of Autothrottle Disengagement for airplanes with Collins EDFCS.
Chapter 5 - Communications Section 10 - Controls and Indicators
Radio Tuning Panel 5.10.4-6 - Revised HF SENS control to reflect proper panel configuration.
5.10.6 - Added text stating DATA is displayed in the ACTIVE Frequency Indicator if the selected radio is in the data mode. Audio Control Panel (ACP) 5.10.16 - Revised CALL Light description to state that CALL light resets when transmitter is selected and microphone is keyed.
Copyright . The Boeing Company. See title page for details.
September 29, 2005
Preface -Revision Record 737 Flight Crew Operations Manual
Chapter 7 - Engines, APU Section 11 - Over/Under – Displays
N1 Indications
7.11.6 - Reference N1 Readouts - revised description of indications for commonality among display options.
7.11.6 - Reference N1 Readouts - added Double Derate indications.
Section 30 - APU System Description
APU Start
7.30.3 - Added Note regarding fluctuating indications during APU start cycle. This Note was in "APU Start" which was removed from SP 7.
Chapter 9 - Flight Controls Section 20 - System Description
Flap Load Relief
9.20.21 - Added trailing edge flaps load relief light.
Chapter 10 - Flight Instruments, Displays Section 21 - PFD/ND System Description
Integrated Standby Flight Display (ISFD)
10.21.14 - Added heading information.
Section 41 - PFD/ND Navigation Displays
Map
10.41.14 - Added TERR map switch to range arc display conditions.
10.41.14 - Added weather radar auto-tilt symbology. TCAS
10.41.21 - Corrected TCAS arrow remarks text.
Chapter 11 - Flight Management, Navigation Section 31 - Flight Management System Operation
MCP Speed Intervention
11.31.24 - Added FMC Update U10.6 or later. Descent
11.31.28 - Deleted sentence "To maintain a path...LNAV course." from paragraph.
Copyright . The Boeing Company. See title page for details.
September 29, 2005
0.4.7
Preface -Revision Record 737 Flight Crew Operations Manual
Section 40 - FMC Preflight
Takeoff Reference Page 2/2
11.40.54 - Revised maximum thrust reduction altitude from "15,000" to "9,999" feet.
Section 60 - FMC Messages
FMC Alerting Messages
11.60.10 - Deleted "Inhibited during approach".
Chapter 12 - Fuel Section 10 - Controls and Indicators
Fuel Control Panel
12.10.3 - Added additional system information on the operation of the center tank FUEL PUMP LOW PRESSURE and MASTER CAUTION lights.
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