Boeing 737 - 600/700/800/900. Operations Manual (1997 year) - page 2
Preface -
Revision Record
Boeing 737 Operations Manual
Filing Instructions
Consult the List of Effective Pages (0.5). Pages identified with an asterisk (*) are
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Be careful when inserting changes not to throw away pages from the manual that
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correct content of the manual.
Revision Highlights
This section (0.4) replaces the existing section 0.4 in your manual.
Throughout the manual, airplane effectivity may be updated to reflect coverage as
listed on the Preface - Model Identification page, or to show service bulletin
airplane effectivity. Highlights are not supplied.
This manual is published from a database; the text and illustrations are marked
with configuration information. Occasionally, because the editors rearrange the
database markers, or mark items with configuration information due to the
addition of new database content, some customers may receive revision bars on
content that appears to be unchanged. Pages may also be republished without
revision bars due to slight changes in the flow of the document.
Chapter 0 - Preface
Section 3 - Abbreviations
0.3.1 - Updated Abbreviations table to expand definition coverage.
Chapter L - Limitations
Section 10 - Operating Limitations
Operational Limitations
L.10.1 - Added limit to ensure Photoluminescent Floor Emergency Lighting
is charged according to approved procedures prior to flight.
L.10.2 - Added restrictions for takeoff and landing on 30 meter wide runway.
Weight Limitations
L.10.3 - Added Note to provide Minimum Takeoff Weight and describe where
to find lower Minimum Takeoff Weights for actual takeoff conditions.
0.4.2
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Boeing 737 Operations Manual
Anti-Ice, Rain
L.10.4 - Added limitation for airplanes that have not been modified with
either PRR 38506 or Service Bulletin 737-55A1080; airspeed is restricted to
270 KIAS after deicing/anti-icing of horizontal stabilizer unless applicable
maintenance procedures have been accomplished.
Aircraft Communications Addressing and Reporting System
L.10.6 - Added caveat to ACARS use restrictions that allows certain message
traffic to be transmitted or received if verified by approved operational
procedures.
Flight Controls
L.10.8 - Added the limitation on use of the speedbrakes above 300 KIAS
which applies to airplanes that have not been modified with stiffened elevator
tabs on the horizontal stabilizer.
Look-Ahead Terrain Alerting (GPWS)
L.10.9 - Revised reference to Allied Signal document of airports in GPWS
database to now reference Honeywell as the document owner.
Chapter NP - Normal Procedures
Section 20 - Amplified Procedures
Flight Deck Preparation - Captain
NP.20.14 - Revised normal procedures to preflight new display.
Descent and Approach Procedure
NP.20.35 - Revised amplified procedures to direct flight crews to position
center tank fuel pump switch(es) off when low pressure light(s) illuminate.
NP.20.35 - Revised amplified procedures to direct flight crews to position the
center tank fuel pump switch(es) off when the LOW PRESSURE light(s)
illuminate.
Section 30 - Flight Patterns
Visual Traffic Pattern
NP.30.6 - Changed for standardization between the OM and FCTM.
0.4.3
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Revision Record
Boeing 737 Operations Manual
Chapter SP - Supplementary Procedures
Section 6 - Electrical
Standby Power Test
SP.6.1 - In the Standby Power Test, the standby power bus is powered by the
battery and should show battery voltage. The battery open circuit voltage is
26 volts; therefore the DC voltmeter readout can not be higher than 26 volts.
The lower end should be set at 22 volts. Therefore, the DC voltmeter is
changed to 24 +/- 2 volts. This change may have already appeared in your
Operations Manual. Re-submitted because all customers may not have
received this change.
Section 9 - Flight Controls
Flight Controls Check
SP.9.1 - The current Flight Controls Check supplementary procedure does not
provide an adequate check of the rudder trim system for airplanes with the
mechanical cam and spring rudder feel and centering unit. The test should be
conducted with hydraulic power on the airplane.
Section 11 - Flight Management, Navigation
Temporary Level Off during Climb or Descent (Not at FMC Cruise Altitude)
SP.11.14 - Corrected to proper switch name.
Section 16 - Adverse Weather
Taxi-Out
SP.16.6 - The requirement to slowly cycle the control column after deicing
only applies to airplanes that have not been modified with stiffened elevator
tabs on the horizontal stabilizer.
Climb and Cruise
SP.16.9 - Added a CAUTION stating that above approximately Flight Level
350 wing anti-ice should not be used.
Chapter PD - Performance Dispatch
Section 13 - Text
Enroute
PD.13.3 - Corrected misspelled word minimum.
Landing
PD.13.5 - Replaced reference to A/C correction with reference to engine
bleed corrections.
0.4.4
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Revision Record
Boeing 737 Operations Manual
Section 21 - Enroute
Long Range Cruise Trip Fuel and Time
PD.21.2 - Reran data with new reference landing weight.
Section 23 - Text
Enroute
PD.23.3 - Corrected misspelled word minimum.
Section 33 - Text
Enroute
PD.33.3 - Corrected misspelled word minimum.
Section 40 - Takeoff
PD.40.1 - Section PD-900-26-LB-FAA-Sec40 added.
Section 41 - Enroute
PD.41.1 - Section PD-900-26-LB-FAA-Sec41 added.
Section 42 - Landing
PD.42.1 - Section PD-900-26-LB-FAA-Sec42 added.
Section 43 - Text
PD.43.1 - Section PD-900-26-LB-FAA-Sec43 added.
Enroute
PD.43.3 - Corrected misspelled word minimum.
Chapter 1 - Airplane General, Emergency Equipment, Doors, Windows
Section 20 - Instrument Panels
Aft Flight Deck Overview
1.20.2
- Added a graphic which depicts the Aft Flight Deck with
the
Enhanced Security Door installed.
Section 30 - Controls and Indicators
Flight Deck Security Door
1.30.9 - Added text and graphics which describe the Flight Deck Security
Door.
Section 40 - Systems Description
Emergency Exit Lighting
1.40.9 - Added a graphic which depicts the photoluminescent floor lighting.
0.4.5
Preface -
Revision Record
Boeing 737 Operations Manual
Portable Protective Breathing Equipment
1.40.13 - Revised the time available when using portable protective breathing
equipment. Some manufacturers produce a device which will operate for
over 20 minutes.
Emergency Equipment Symbols
1.40.19 - Added a symbol for the AED to the Emergency Equipment Location
graphic.
Flight Deck Security Door
1.40.23 - Added text and graphics describing the new Flight Deck Enhanced
Security Door.
Chapter 2 - Air Systems
Section 40 - Pressurization System Description
Auto Mode Operation
2.40.6 - Revised description of AUTO FAIL light operation.
Chapter 3 - Anti-Ice, Rain
Section 20 - System Description
Probe and Sensor Heat
3.20.5 - Added note to clarify operation of pitot probe for standby airspeed.
Chapter 4 - Automatic Flight
Section 10 - Controls and Indicators
Vertical Navigation
4.10.6 - Added FMC Update U10.3.
Lateral Navigation
4.10.12 - Added flight control computer -708 or later.
Section 20 - System Description
Autopilot Disengagement
4.20.2 - Added flight control computer -708 or later.
AFDS Flight Mode Annunciations
4.20.5 - Added flight control computer -708 or later.
Automatic Flight Takeoff and Climb
4.20.10 - Deleted automatic takeoff thrust reduction option.
0.4.6
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Automatic Flight Approach and Landing
4.20.15 - Revised description of ILS deviation monitoring system.
Go-Around
4.20.19-20 - Added flight control computer -708 or later.
Reversion Modes
4.20.27 - Amended description of minimum speed reversion.
Chapter 6 - Electrical
Section 10 - Controls and Indicators
AC and DC Metering Panel
6.10.4
- Revised information about the equipment controlled
by
the
CAB/UTIL Switch.
6.10.4
- Revised information about the equipment controlled
by
the
CAB/UTIL and IFE/PASS SEAT switches.
Section 20 - System Description
DC Voltmeter and Ammeter
6.20.9 - Revised paragraph to include voltage indications during the primary
charge cycle.
Chapter 7 - Engines, APU
Section 20 - Engine System Description
Electronic Engine Control (EEC)
7.20.4 - Revised description of EEC modes of operation for clarity.
EEC Normal Mode
7.20.5 - Revised description of takeoff bump thrust.
Chapter 8 - Fire Protection
Section 10 - Controls and Indicators
APU Ground Control Panel
8.10.7 - Corrected description of switch operation.
0.4.7
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Revision Record
Boeing 737 Operations Manual
Chapter 9 - Flight Controls
Section 10 - Controls and Indicators
Flight Control Panel
9.10.1 - Revised Flight Control Panel illustration and description to provide
additional information on the FLT CONTROL Switches and STANDBY
HYD Lights.
9.10.2 - Added Flight Control Panel illustration and description to reflect the
addition of the STBY RUD ON Light.
9.10.3 - Added description of the STBY RUD ON Light.
Section 20 - System Description
Rudder
9.20.12 - Corrected grammatical error in text.
9.20.12 - Revised text to clarify rudder system operation.
9.20.12 - Added description of 737 modified rudder system.
9.20.12 - Revised text to clarify the operation of the standby rudder PCU
system.
Yaw Damper
9.20.14 - Added description of Yaw Damper system with 737 modified
rudder installed.
Yaw Control Schematic
9.20.15 - Added Yaw Control Schematic for 737 modified rudder system.
In-Flight Operation
9.20.16 - Revised text to be consistent with text in the Limitations Chapter L,
Section 10.
Autoslats
9.20.20 - Revised information about Autoslat system operation for airplanes
with winglets.
Chapter 10 - Flight Instruments, Displays
Section 10 - EFIS/Map - Controls and Indicators
Mach/Airspeed Indicator - General
10.10.8 - Added Flaps 30 Upper amber band logic due to software upgrade.
Attitude Indicator - LNAV/VNAV Deviation Indicators
10.10.15 - Added LNAV/VNAV deviation EFIS option.
0.4.8
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Section 11 - PFD/ND - Displays
PFD Airspeed Indications - General
10.11.6 - Deleted FMC update 10.2 or 10.2A.
PFD Airspeed Indications - Takeoff and Approach
10.11.10 - Added Flaps 30 Upper amber band logic due to software upgrade.
PFD LNAV/VNAV Deviation Indications
10.11.14 - Added LNAV/VNAV deviation PFD option.
Section 15 - EFIS Instruments - Controls and Indicators
Standby Flight Instruments
10.15.10 - Added integrated standby flight display.
Integrated Standby Flight Display
10.15.11,13 - Added integrated standby flight display.
Section 16 - EFIS Instruments (PFD) - Controls
Standby Flight Instruments
10.16.10 - Added integrated standby flight display.
Integrated Standby Flight Display
10.16.11,13 - Added integrated standby flight display.
Section 20 - EFIS/Map System Description
Standby Flight Instruments
10.20.13 - Added integrated standby flight display.
Integrated Standby Flight Display (ISFD)
10.20.14 - Added integrated standby flight display.
Section 21 - PFD/ND System Description
Standby Flight Instruments
10.21.14 - Added integrated standby flight display.
Integrated Standby Flight Display (ISFD)
10.21.14 - Added integrated standby flight display.
Section 41 - PFD/ND Navigation Displays
Map
10.41.8 - Added LNAV/VNAV deviation MAP symbols.
0.4.9
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Chapter 11 - Flight Management, Navigation
Section 20 - Navigation Systems Description
Marker Beacon
11.20.10 - Deleted the term "airway"
Section 31 - Flight Management System Operation
Navigation Performance
11.31.7 - Combined RNP paragraphs for clarity.
11.31.7 - Added FMC Update U10.5 or later.
11.31.7 - Deleted FMC Update U10.0.
Actual Navigation Performance
11.31.8-9 - Added new ANP graphic with GPS.
Descent
11.31.33 - Changed "PATH" to "path (VNAV PTH)".
11.31.33 - Changed "SPEED" to "speed".
Early Descent
11.31.33 - Repositioned "1000 fpm".
Approach
11.31.34 - Changed title to read "Approach".
11.31.34 - Added "on approach" information.
11.31.35 - Revised text for clarity.
Go-Around
11.31.35 - Added additional information to Go-Around section.
Section 32 - Flight Management Computer
Thrust Management
11.32.3 - Deleted automatic takeoff thrust reduction option.
11.32.3 - Revised thrust reduction altitude.
11.32.3 - Added FMC Update U10.3.
Reduced Thrust Takeoff
11.32.4 - Deleted FMC Update U10.0.
Loss of FMC Electrical Power
11.32.5 - Changed MOD RTE LEGS to RTE LEGS.
0.4.10
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Revision Record
Boeing 737 Operations Manual
Section 40 - FMC Preflight
Preflight Page Sequence
11.40.1 - Deleted FMC Update U10.0.
Identification Page
11.40.7 - Added -900 to model list.
11.40.8 - Added FMC Update U10.4A.
11.40.8 - Added FMC Update U10.5.
11.40.8 - Added engine thrust designations.
Route Page 1/X
11.40.14 - Added FMC Update U10.3.
11.40.14 - Added option for flight crew entry of flight number via CDU.
11.40.18 - Added Flight Number Entry option.
Performance Initialization Page
11.40.27 - Deleted FMC Update U10.0.
11.40.28 - Added FMC U10.1 or later with plan fuel option.
N1 LIMIT Page - Preflight
11.40.39-40 - Added CLB thrust statement.
Takeoff Reference Page 1/2
11.40.43,47,54 - Deleted FMC Update U10.0.
11.40.50 - Added assumed temperature to QRH definition.
Takeoff Reference Page 2/2
11.40.61 - Added FMC Update U10.3.
11.40.61 - Revised thrust reduction altitude.
Section 41 - FMC Takeoff and Climb
Arrivals Page
11.41.37 - Added section reference for additional information.
Section 42 - FMC Cruise
Progress Page
11.42.4 - Changed page number to read 1/X.
Reference Navigation Data (REF NAV DATA) Page
11.42.41 - Added waypoint identifier information.
11.42.41 - Added airport identifier information.
0.4.11
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Revision Record
Boeing 737 Operations Manual
11.42.42 - Added navaid identifier information.
Navigation Options (NAV OPTIONS)
11.42.53 - Expanded text on VOR/DME inhibit function.
Fix Information Page
11.42.54 - Added FMC Update U10.5 or later.
Section 43 - FMC Descent and Approach
Descent Forecast Page
11.43.11-12 - Added AOC datalink option.
11.43.12 - Added informational note for TAI.
11.43.12 - Added ACARS note.
Added AOC datalink option.
Approach Reference Page
11.43.21,23 - Revised callout label to read Approach Information.
11.43.24 - Changed line select key to 4L.
11.43.24 - Added Flap/Speed formatting information.
11.43.24 - Added FMC Update U10.5.
HOLD Page
11.43.32 - Revised text next to HOLD button to read "does not exist".
11.43.34 - Added FMC Update U10.4 or later.
11.43.35 - Revised NEXT HOLD description.
Section 60 - FMC Messages
FMC Alerting Messages
11.60.2 - Added FMC Update U10.4 or later CDU messages.
11.60.2,7,9 - Added FMC Update U10.5 or later CDU messages.
11.60.4,6 - Added Integrated Approach Navigation CDU message.
FMC Advisory Messages
11.60.13 - Added GLS information.
11.60.13 - Added FMC Update U10.4 and U10.5 CDU messages.
11.60.16 - Added FMC Update U10.5 or later CDU messages.
0.4.12
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Boeing 737 Operations Manual
Chapter 12 - Fuel
Section 10 - Controls and Indicators
Fuel Alert Indications
12.10.5 - Added kilogram measurement to the Fuel Alert Indications section.
Chapter 13 - Hydraulics
Section 10 - Controls and Indicators
Flight Control Panel
13.10.5 - Added Flight Control Panel illustration and information for the
STBY RUD ON Light for the 737 modified rudder system.
Section 20 - System Description
A and B Hydraulic System Pumps
13.20.3
- Changed "electric hydraulic pump" to "electric motor-drive
hydraulic pump" for Operations Manual standardization.
Standby Hydraulic System
13.20.5
- Revised Standby Hydraulic System description to provide
information about the 737 modified rudder system.
Standby Hydraulic System Schematic
13.20.7 - Added graphic to incorporate 737 modified rudder system.
Chapter NC - Normal Checklists
NC.1 - Added head-up display information.
Chapter PI - Performance Inflight
Section 10 - General
Takeoff Speeds - Dry Runway
PI.10.1 - Reran V1mcg data for A/C off and expanded table coverage to
10000 ft.
Takeoff Speeds - Wet Runway
PI.10.2 - Reran V1mcg data for A/C off and expanded table coverage to
10000 ft.
Takeoff %N1
PI.10.7 - Revised Takeoff %N1 table for consistent coverage of Outside Air
Temperature (OAT).
0.4.13
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Boeing 737 Operations Manual
Assumed Temperature Reduced Thrust
PI.10.8 - Extended coverage up to 10000 ft pressure altitude, and revised Max
Assumed Temperature to match AFM-DPI limit of ISA+56°C.
Takeoff Speeds - Dry Runway (20K Derate)
PI.10.10 - Reran V1mcg data for A/C off and expanded table coverage to
10000 ft.
Takeoff Speeds - Wet Runway (20K Derate)
PI.10.11 - Reran V1mcg data for A/C off and expanded table coverage to
10000 ft.
Takeoff %N1 (20K Derate)
PI.10.15 - Revised Takeoff %N1 table for consistent coverage of Outside Air
Temperature (OAT). Extended coverage of Airport Pressure Altitude up to
10000 ft.
Assumed Temperature Reduced Thrust (20K Derate)
PI.10.16 - Extended coverage up to 10000 ft pressure altitude, and revised
Max Assumed Temperature to match AFM-DPI limit of ISA+56°C.
Takeoff Speeds - Dry Runway (18.5K Derate)
PI.10.18 - Reran V1mcg data for A/C off and expanded table coverage to
10000 ft.
Takeoff Speeds - Wet Runway (18.5K Derate)
PI.10.19 - Reran V1mcg data for A/C off and expanded table coverage to
10000 ft.
Takeoff %N1 (18.5K Derate)
PI.10.23 - Revised Takeof %N1 table for consistent coverage of Outside Air
Temperature (OAT).
Section 12 - Advisory Information
Slippery Runway Landing Distance
PI.12.1 - Removed 15% factor from dry runway landing distances.
PI.12.1
- Removed
15% factor from dry runway landing distance
adjustments.
Brake Cooling Schedule
PI.12.7 - Removed advice for overheat after takeoff, which requires BTMS to
be detected.
0.4.14
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Revision Record
Boeing 737 Operations Manual
Section 16 - Text
Alternate Mode EEC
PI.16.11 - Revised wording of Alternate Mode EEC paragraphs to reflect
termonology used in respective Operations Manual System Description.
Changed PRIMARY Mode to normal mode (ON EEC switch illuminated),
ALTERNATE to alternate (ALTN EEC switch illuminated).
Section 20 - General
Takeoff %N1
PI.20.11 - Revised Takeoff %N1 table for consistent coverage of Outside Air
Temperature (OAT). Extended coverage of Airport Pressure Altitude up to
10000 ft.
PI.20.11 - Amended Engine Bleed %N1 Adjustment for -1000 ft pressure
altitude.
Assumed Temperature Reduced Thrust
PI.20.12 - Extended coverage up to 10000 ft pressure altitude, and revised
Max Assumed Temperature to match AFM-DPI limit of ISA+56°C.
Takeoff %N1 (22K Derate)
PI.20.20 - Revised Takeoff %N1 table for consistent coverage of Outside Air
Temperature (OAT).
Assumed Temperature Reduced Thrust (22K Derate)
PI.20.21 - Extended coverage up to 10000 ft pressure altitude, and revised
Max Assumed Temperature to match AFM-DPI limit of ISA+56°C.
Takeoff %N1 (20K Derate)
PI.20.28 - Revised Takeoff %N1 table for consistent coverage of Outside Air
Temperature (OAT). Extended coverage of Airport Pressure Altitude up to
10000 ft.
PI.20.28 - Amended Engine Bleed %N1 Adjustment for -1000 ft pressure
altitude.
Assumed Temperature Reduced Thrust (20K Derate)
PI.20.29 - Extended coverage up to 10000 ft pressure altitude, and revised
Max Assumed Temperature to match AFM-DPI limit of ISA+56°C.
0.4.15
Preface -
Revision Record
Boeing 737 Operations Manual
Section 26 - Text
Alternate Mode EEC
PI.26.11 - Revised wording of Alternate Mode EEC paragraphs to reflect
termonology used in respective Operations Manual System Description.
Changed PRIMARY Mode to normal mode (ON EEC switch illuminated),
ALTERNATE to alternate (ALTN EEC switch illuminated).
Section 30 - General
Takeoff %N1
PI.30.7 - Revised Takeoff %N1 table for consistent coverage of Outside Air
Temperature (OAT). Extended coverage of Airport Pressure Altitude up to
10000 ft. Amended Engine Bleed %N1 Adjustment for -1000 ft pressure
altitude.
Assumed Temperature Reduced Thrust
PI.30.8 - Revised Max Assumed Temperature to match AFM-DPI limit of
ISA+56°C.
Takeoff %N1 (24K Derate)
PI.30.16 - Revised Takeoff %N1 table for consistent coverage of Outside Air
Temperature (OAT). Extended coverage of Airport Pressure Altitude up to
10000 ft. Amended Engine Bleed %N1 Adjustment for -1000 ft pressure
altitude.
Assumed Temperature Reduced Thrust (24K Derate)
PI.30.17 - Extended coverage up to 10000 ft pressure altitude, and revised
Max assumed Temperature to match AFM-DPI limit of ISA+56°C.
Takeoff %N1 (22K Derate)
PI.30.24 - Revised Takeoff %N1 table for consistent coverage of Outside Air
Temperature (OAT). Extended coverage of Airport Pressure Altitude up to
10000 ft. Amended Engine Bleed %N1 Adjustment for -1000 ft pressure
altitude.
Assumed Temperature Reduced Thrust (22K Derate)
PI.30.25 - Extended coverage up to 10000 ft pressure altitude, and revised
Max Assumed Temperature to match AFM-DPI limit of ISA+56°C.
Section 34 - Alternate Mode EEC
Alternate Mode EEC Limit Weight
PI.34.1 - Revised labeling of Alternate Mode EEC Limit Weight table to
eflect termonology used in respective Operations Manual System
Description. Changed PRIMARY to NORMAL.
0.4.16
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Revision Record
Boeing 737 Operations Manual
Section 37 - Text
Alternate Mode EEC
PI.37.11 - Revised wording of Alternate Mode EEC paragraphs to reflect
termonology used in respective Operations Manual System Description.
Changed PRIMARY Mode to normal mode (ON EEC switch illuminated),
ALTERNATE to alternate (ALTN EEC switch illuminated).
Section 40 - General
PI.40.1 - Section PI-900-26-LB-FAA-Sec40 added.
Takeoff %N1
PI.40.8 - Corrected %N1 Adjustment for engine bleed configuration packs off
at -1000 ft.
Assumed Temperature Reduced Thrust
PI.40.9 - Revised Max Assumed Temperature to match AFM-DPI limit of
ISA+56°C.
PI.40.9 - Added missing row for Minimum Assumed Temperature.
Assumed Temperature Reduced Thrust (24K Derate)
PI.40.18 - Added missing Minimum Assumed Temp °C row.
Section 41 - All Engine
PI.41.1 - Section PI-900-26-LB-FAA-Sec41 added.
Section 42 - Advisory Information
PI.42.1 - Section PI-900-26-LB-FAA-Sec42 added.
Section 43 - Engine Inoperative
PI.43.1 - Section PI-900-26-LB-FAA-Sec43 added.
Section 44 - Alternate Mode EEC
PI.44.1 - Section PI-900-26-LB-FAA-Sec44 added.
Alternate Mode EEC Limit Weight (1000 LB)
PI.44.1 - Revised labeling of Alternate Mode EEC Limit Weight table to
eflect termonology used in respective Operations Manual System
Description. Changed PRIMARY to NORMAL.
Section 45 - Gear Down
PI.45.1 - Section PI-900-26-LB-FAA-Sec45 added.
Section 46 - Gear Down, Engine Inop
PI.46.1 - Section PI-900-26-LB-FAA-Sec46 added.
0.4.17
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Boeing 737 Operations Manual
Section 47 - Text
PI.47.1 - Section PI-900-26-LB-FAA-Sec47 added.
Alternate Mode EEC
PI.47.11 - Revised wording of Alternate Mode EEC paragraphs to reflect
termonology used in respective Operations Manual System Description.
Changed PRIMARY Mode to normal mode (ON EEC switch illuminated),
ALTERNATE to alternate (ALTN EEC switch illuminated).
Chapter NNC - Non-Normal Checklists
Section 0 - Unannunciated Checklists
ELEVATOR TAB LIMIT CYCLE OSCILLATION
NNC.0.14 - Incorporated Airworthiness Directive 2002-08-20.
JAMMED OR RESTRICTED ELEVATOR OR AILERON
NNC.0.21 - Indented steps to improve procedural logic.
NNC.0.21 - Added a note clarifying that when VREF ICE is required, the
wind correction should not exceed 10 knots.
JAMMED STABILIZER
NNC.0.24 - Added a note clarifying that when VREF ICE is required, the
wind correction should not exceed 10 knots.
PASSENGER EVACUATION
NNC.0.28 - Added the word "engine" for nomenclature standardization.
SMOKE/FUMES REMOVAL
NNC.0.30 - Changed checklist from a recall to a reference only checklist to
be consistent with other Boeing models that have the same checklist.
Section 1 - Airplane General, Emergency Equipment, Doors, Windows
ELT
NNC.1.2 - Added checklist for airplanes equipped with an emergency locator
transmitter control panel.
Section 2 - Air Systems
BLEED TRIP OFF
NNC.2.4 - Inappropriate use of wing TAI may cause dual bleed trip off
incidents. As a result, added a step to turn the wing anti-ice off.
Section 6 - Electrical
TR UNIT
NNC.6.6 - Transposed procedures to match proper index order.
0.4.18
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Boeing 737 Operations Manual
TRANSFER BUS OFF
NNC.6.6 - Transposed procedures to match proper index order.
Section 7 - Engines, APU
ONE ENGINE INOPERATIVE LANDING
NNC.7.22 - Added a note clarifying that when VREF ICE is required, the
wind correction should not exceed 10 knots.
Section 8 - Fire Protection
SMOKE/FUMES REMOVAL
NNC.8.10 - Changed checklist from a recall to a reference only checklist to
be consistent with other Boeing models that have the same checklist.
Section 9 - Flight Controls
ALTERNATE FLAPS OPERATION
NNC.9.4 - Added a note clarifying that when VREF ICE is required, the wind
correction should not exceed 10 knots.
NNC.9.4 - Changed to clarify system operation.
NNC.9.4 - Added a Descent and Approach checklist for consistency with
other 737 NNC’s.
ASYMMETRICAL TRAILING EDGE FLAPS
NNC.9.8 - Added a note clarifying that when VREF ICE is required, the wind
correction should not exceed 10 knots.
ELEVATOR TAB LIMIT CYCLE OSCILLATION
NNC.9.10 - Incorporated Airworthiness Directive 2002-08-20.
JAMMED OR RESTRICTED ELEVATOR OR AILERON
NNC.9.13 - Indented steps to improve procedural logic.
NNC.9.13 - Added a note clarifying that when VREF ICE is required, the
wind correction should not exceed 10 knots.
JAMMED STABILIZER
NNC.9.16 - Added a note clarifying that when VREF ICE is required, the
wind correction should not exceed 10 knots.
YAW DAMPER
NNC.9.25 - The FCTM includes the note "With yaw damper inoperative, do
not exceed flaps 30 if crosswinds exceed 30 knots." This limitation is now
included in the YAW DAMPER Non-Normal checklist.
0.4.19
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Section 11 - Flight Management, Navigation
GPS
NNC.11.3 - Expanded the GPS NNC to advise the flight crew that terrain
alerting and associated display will be lost in the event of dual sensor failure.
Section 13 - Hydraulics
LOSS OF SYSTEM B
NNC.13.4 - Added a note clarifying that when VREF ICE is required, the
wind correction should not exceed 10 knots.
NNC.13.4 - Changed to clarify system operation.
MANUAL REVERSION
NNC.13.7 - Added a note clarifying that when VREF ICE is required, the
wind correction should not exceed 10 knots.
NNC.13.7 - Changed to clarify system operation.
Chapter NNM - Non-Normal Maneuvers
Section 2 - Flight Patterns
Visual Traffic Pattern
NNM.2.6 - Changed for standardization between the OM and FCTM.
0.4.20
Boeing 737 Operations Manual
Preface
Chapter 0
List of Effective Pages
Section 5
0.5 Preface-List of Effective Pages
Page
Date
Page
Date
Volume 1
Normal Procedures (tab)
* NP.TOC.0.1-2
* Title Page
NP.10.1
Copyright
NP.10.2-4
0.0.1-2
NP.10.5
0.1.1
NP.10.6
0.1.2
NP.20.1-6
0.2.1-3
NP.20.7
0.2.4
October 15, 2001
NP.20.8-9
0.2.5-6
* NP.20.10-12
0.3.1-6
NP.20.13
0.4.1-20
* NP.20.14-42
0.5.1-12
* NP.20.43-44
Deleted
Bulletins (tab)
NP.30.1-2
0.6.1-4
NP.30.3-5
Limitations (tab)
* NP.30.6
* L.TOC.0.1-2
* L.10.1-10
* = Revised, Added, or Deleted
0.5.1