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B737-NG GENERAL

TRAINING MANUAL

737 GENERAL INTRODUCTION Introduction This section introduces you to the 737700/800/900 airplane. You will see general information about these topics:

Range Dimensions Engines Flight controls Doors Flight compartment panels Electronic equipment rack configuration Electrical.

Abbreviations and Acronyms A/P autopilot A/S airspeed ac alternate current ACARS ARINC communications addressing and

reporting system ACMS airplane condition monitoring system ADF automatic direction finder ADIRS air data inertial reference system AFCS automatic flight control system

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AGCU APU generator control unit altn alternate amp amplifier APB APU breaker APU auxiliary power unit ATC air traffic control att attendant auto automatic bat battery bcn beacon BL buttock line BPCU bus power control unit BTB bus tie breaker C/W control wheel capt captain CDS common display system CDU control display unit chgr charger comm communication comp computer conn connected cond condition cntl control det detector DEU display electronic unit dist distribution

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737 GENERAL INTRODUCTION DME distance measuring equipment DU display unit ECU electronic control unit EE electronic equipment EEC electronic engine control elex electronics ELT emergency locator transmitter EMDP electric motor driven pump ESDS electrostatic discharge sensitive ext external F/O first officer FCC flight control computer FMC flight management computer FMCS flight management computer system freq frequency fwd forward GCU generator control unit gnd ground GPS global positioning system HF high frequency HUD heads up display IDG integrated drive generator ILS instrument landing system inv inverter

L left LBL left buttock line LE leading edge LRRA low range radio altimeter LRU line replaceable unit mod module MLG main landing gear MCP mode control panel MPD maintenance planning document nav navigation NLG nose landing gear ovht overheat PA passenger address PCU power control unit PDP power distribution panel pnl panel prox proximity PSU passenger service unit pwr power R right RBL right buttock line REU remote electronics unit RLY relay SATCOM satellite communication S/B speedbrake

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737 GENERAL INTRODUCTION sec section sel select SCU start converter unit SPU start power unit SOV shutoff valve stab stabilizer STA station stdby standby sw switch TCAS traffic alert and collision avoidance

system TE trailing edge TRU transformer rectifier unit typ typical VHF very high frequency vlv valve VOR VHF omni range WL water line xfer transfer xfmr transformer

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737 GENERAL INTRODUCTION

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737 GENERAL RANGE Introduction The 737700 is a twoengine airplane. It is for short to medium range flights with a capacity of up to 149 passengers. The 737-900 has a capacity of up to 189 passengers. Features There are many new features. These new features increase the airplane payload, service ceiling, and range. The 700 airplane has a design range of 3,200 nautical miles. The 900 has a design range of 2,745 nautical miles.

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B737-900

B737-800

B737-700

737 GENERAL RANGE

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737 GENERAL STRUCTURE DIMENSIONS General These are the general dimensions of the airplane.

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737 GENERAL STRUCTURE DIMENSIONS

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737 GENERAL FUSELAGE DIMENSIONS General Dimensions give locations on the fuselage. The scale for each dimension is inches. You use these dimensions to find components on the fuselage:

Body station line Body buttock line Water line.

The body station line (STA) is a horizontal dimension. It starts at station line zero. You measure the body station line from a vertical reference plane that is forward of the airplane. The body buttock line (BL) is a lateral dimension. You measure the buttock line to the left or right of the airplane center line. The water line (WL) is a height dimension. You measure the water line from a horizontal reference plane below the airplane.

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737 GENERAL POWER PLANT INTRODUCTION General Two CFM567B engines supply thrust for the airplane. The engines also supply power for these systems:

Electric Hydraulic Pneumatic.

The CFM567B is a high bypass ratio, dual rotor, turbo fan engine.

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737 GENERAL POWER PLANT ENGINE HAZARDS General It is dangerous to work around engines. Use the entry/exit corridor when the engine is in operation. Stay out of the inlet and exhaust areas when the engine is in operation. These are the hazards around an engine in operation:

Inlet suction Exhaust heat Exhaust velocity Engine noise.

Inlet Suction Engine inlet suction can pull people and large objects into the engine. At idle power, the inlet hazard area is a 13 ft (4.0 m) radius around the inlet. WARNING: IF THE WIND IS OVER 25 KNOTS,

INCREASE THE INLET HAZARD AREA BY 20%.

Exhaust Heat The engine exhaust is very hot for a long distance behind the engine. This can cause damage to personnel and equipment.

Exhaust Velocity Exhaust velocity is very high for a long distance behind the engine. This can cause damage to personnel and equipment. Engine Noise Engine noise can cause temporary and permanent loss of your ability to hear. You must wear ear protection when near an engine in operation. Engine Entry/Exit Corridor Engine entry corridors are between the inlet hazard areas and the exhaust hazard areas. You should go near an engine in operation only when:

The engine is at idle You can speak with people in the flight

compartment. For additional safety, wear a safety harness when the engine is in operation. Training Information Point When the engine is in operation, the anticollision lights should be on.

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737 GENERAL FLIGHT CONTROL SURFACES General The flight controls keep the airplane at the necessary attitude during flight. They have movable surfaces on the wing and the empennage. These are the two types of flight controls:

Primary Secondary.

Primary Flight Controls The primary flight controls has these components:

Aileron (2) Elevator (2) Rudder.

Secondary Flight Controls The secondary flight control system has these components:

Leading edge flaps (4) Leading edge slats (8) Trailing edge flaps (4) Spoilers (12) Horizontal stabilizer.

The 12 spoilers consists of ground and flight spoilers. The spoilers are numbered 1 to 12, left to right.

Power Source Hydraulic actuators or electric motors move the surfaces. You must be very careful when you work near flight control surfaces. When hydraulic power is on, make sure that all the flight control surfaces are clear of personnel and equipment.

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737 GENERAL DOORS INTRODUCTION Purpose The doors are movable units that give access to the airplane compartments. General Description These are the types of doors on the airplane:

Forward and aft entry doors Forward and aft galley service doors Emergency exit hatches (and pilots' sliding

windows) Cargo doors Interior doors (crew door and lavatory doors) Miscellaneous access doors.

Location The entry doors are on the left side of the airplane. The galley service doors are on the right side of the airplane. The emergency exit hatches are above the wings on both sides of the airplane. The pilots' sliding windows are in the flight compartment. The crew door and lavatory doors are inside the airplane.

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The cargo doors are on the right side of the airplane. The miscellaneous access doors are near the systems they serve. Training Information Point You can open and close entry, galley service, and cargo doors in winds up to 40 knots without structural damage. You can let these doors stay latched open in winds up to 65 knots without structural damage. If a door is left open for a long time, a protective cover should be put over the door frame. This prevents bad weather damage to the airplane.

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737 GENERAL DOORS INTRODUCTION

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737 GENERAL - FLIGHT COMPARTMENT PANELS Flight Compartment Panels These are the major panels in the flight compartment:

- P1 captain instrument panel - P2 center instrument panel - P5 forward overhead panel - P5 aft overhead panel - P7 glareshield panel - P3 first officer instrument panel - P9 forward electronic panel - Control stand - P8 aft electronic panel.

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737 GENERAL - FLIGHT COMPARTMENT PANELS

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737 GENERAL MAIN INSTRUMENT PANELS General The controls and displays on the main instrument panels (P1 and P3) include these components:

Clock (2) Display unit (4) Display select panel (2) Master dim and test switch Brake pressure indicator Autoflight status annunciator (2) GPWS control panel Lighting control (2) Conditioned air outlet control (2).

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737 GENERAL GLARESHIELD PANELS General The controls and displays on the P7 glareshield include these components:

Master caution annunciator (2) System caution annunciator (2) Mode control panel (MCP) EFIS control panel (2) Fire warning light (2)

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737 GENER LARESHIELD PANELSAL G

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737 GENERAL P2 CENTER INSTRUMENT PANEL AND P9 FORWARD ELECTRONICS PANEL General The controls and displays on the P2 center instrument panel include these components:

Yaw damper indicator Standby instruments Engine display control panel Antiskid and autobrake switches and lights Flap position indicator Landing gear lever and position indicator Upper center display unit.

The controls and displays on the P9 forward electronics panel include these components:

Lower center display unit Control display unit (CDU) (2).

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737 GENERAL P2 CENTER INSTRUMENT PANEL AN ORWARDD P9 F

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737 GENERAL CONTROL STAND GENERAL The controls and indicators on the control stand include these components:

Forward thrust lever (2) Reverse thrust lever (2) Speed brake handle Horizontal stabilizer trim wheel and indicator (2) Parking brake lever and indication light Flap lever Stabilizer trim cutout switch (2) Start lever (2).

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737 GENERAL P8 AFT ELECTRONICS PANEL General The P8 aft electronics panel has these components:

Weather radar control panel Overheat/fire protection panel ATC/TCAS control panel Radio communication panels Navigation control panels Audio control panels Aileron/rudder trim panel ACMS printer Lighting control.

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737 GENERAL P5 AFT OVERHEAD PANEL General The controls and displays on the P5 aft overhead panel include these components:

Inertial system display unit Engine panel Observer audio control panel Oxygen panel Landing gear indicator lights White dome light switch Service interphone switch IRS mode select unit Proximity switch electronics unit light Leading edge devices annunciator panel.

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737 GENERAL P5 FORWARD OVERHEAD PANEL General The controls and displays on the P5 forward overhead panel include these components:

APU control switch APU indicator panel Fuel control panel Ground power and bus switching panel Equipment cooling panel Generator drive and standby power panel AC and DC meter panel Flight control panel Airconditioning/bleed air controls panel Hydraulic control panel Cabin altitude panel Cabin pressure control panel Engine start panel.

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737 GENERAL P5 FORWARD OVERHEAD PANEL - 700

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737 GENERAL P5 FORWARD OVERHEAD PANEL /900

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737 GENERAL AFT FLIGHT COMPARTMENT PANELS General The main circuit breaker panels are behind the first officer and captain seats. The P6 and P18 have the component load circuit breakers. Circuit breakers are organized by airplane systems. The P61 panel has the data loader controls.

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737 GENERAL AFT FLIGHT COMPARTMENT

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737 GENERAL ELECTRONIC EQUIPMENT COMPARTMENT General Electronic equipment is in a compartment below the main cabin floor, aft of the nose wheel well. On the ground, you enter this electronic equipment (EE) compartment through a door in the bottom of the fuselage. The door is just aft of the nose landing gear. There are five standard equipment racks. These are the E1, E2, E3, E4, and E5 racks. Shelf assemblies have equipment mounts, interconnected wiring, and accessory boxes. Most equipment rack shelves are cooled with air. Air is blown through or drawn through the equipment racks. There is a drip shield over the racks to protect the equipment from moisture condensation.

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737 GENERAL ELECTRONIC EQUIPMENT COMPARTMENT

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737 GENERAL EE COMPARTMENT DOOR OPERATION Operation You manually operate an external access door to the electronic equipment (EE) compartment. You open and close the door from outside the airplane. Open Door The handle on the door fairs in a recess. A pushbutton trigger releases the handle, and it comes out of fair by spring force. Turn the handle counterclockwise to disengage the latch pins. When the latch pins are free you can push the door upward and slightly to the right to the first detent. Then push the door to the right to the fully open detent. When the door is fully open, the roller tracks can be folded to improve access to the equipment racks. A spring catch on the end of each roller track holds the track in the folded or unfolded position. Close Door Before you close the door, release the spring catch and extend the roller tracks. Make sure the door frame area is clear.

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Pull the door out of the fully open detent and then restrain it as gravity causes it to slide down the tracks. When the door reaches the lower detent you can release it. Turn the handle counterclockwise to retract the latch pins. If you do not do this, the door will not seat in the door frame. Pull the handle to the left and the door will come out of the partially open detent. Then it slides down into the door frame. Turn the handle clockwise to latch the door. Then push the door handle back into its recess.

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737 GENERAL EE COMPARTMENT DOOR OPERATION

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737 GENERAL ELECTRONIC EQUIPMENT RACK E1 General The equipment on the E1 rack includes electronics for these functions:

Autothrottle Autopilot Communication Navigation Flight control.

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PROGRAM SWITCH MODULE (TYP)

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737 GENERAL ELECTRONIC EQUIPMENT RACK E1

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737 GENERAL PROGRAM SWITCH MODULE General Many of the line replaceable units (LRUs) are controlled by internal digital computers. These computers follow instructions (or programs) to do a certain task. The program switch module gives an external method to customize a computer's program. The program switch module has these components:

Switches Pin contacts Switch seal plug Security cover.

An LRU's programming pin inputs come in on the pin contacts. The switches set the programming pins. The security cover goes over the switch seal plug. The security cover and the switch seal plug keeps the switches stationary. The program switch module gives this information to an LRU:

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Equipment physical orientation Airplane type Number of units installed Customer specific options.

See the Standard Wiring Practices Manual for more information on the program switch module.

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737 GENERAL PROGRAM SWITCH MODULE

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737 GENERAL ELECTRONIC EQUIPMENT RACKS E2, E3, AND E4 General The equipment in the E2, E3, and E4 racks include electronics for these functions:

Window heat Communications Electrical power Common display system (CDS) Flight control Fire detection APU.

The EE compartment light switch is on a panel just aft of the access door opening.

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737 GENERAL ELECTRONIC EQUIPMENT RACKS E2, E3, AND E4

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737 GENERAL ELECTRONIC EQUIPMENT RACK E5 General The equipment in the E5 rack includes electronics for these functions:

Air data inertial reference system (ADIRS) Flight management computer system (FMCS).

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737 GENERAL ELECTRONIC EQUIPMENT RACK E5

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737 GENERAL ELECTRONIC EQUIPMENT RACK E8 General The equipment in the E8 rack includes electronics for these functions:

HF transceivers Passenger entertainment Quick access recorder (QAR)

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737 GENERAL ELECTRONIC EQUIPMENT RACK E8

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737 GENERAL LOADABLE SOFTWARE General Some of the LRUs in the 737 need both hardware and software. Without the software, the logic circuits in the LRUs can not do their specified function. They must have the proper software load. You can load the software in the LRU at the shop or you can load it at the airplane. Systems These LRUs have loadable software features:

Flight management computer (FMC) Control Display Unit (CDU) based on effectivity Display electronic unit (DEU) ARINC communications addressing and reporting

system (ACARS)/Communications Management Unit (CMU) based on effectivity

Flight Control Computer (FCC) based on effectivity

Flight data acquisition unit (FDAU) Airplane condition monitoring system (ACMS) Electronic engine control (EEC) APU engine control unit (ECU).

Except for the EEC, you use the data loader at the P61 to load the software.

You load the EEC software at the engine with a portable loader. Loadable Software Binder A binder is in the book compartment at the bottom of the P61. The binder has all the software necessary to load software at the airplane. Installation Procedure These are the basic steps to load software at the airplane:

Supply electrical power Open the DATA LOADER circuit breaker Connect the portable data loader (PDL) to the data

transfer unit receptacle Close the DATA LOADER circuit breaker Set the data load select switch to the applicable

LRU position Put the diskette into the disk drive Remove the diskette when the software load is

complete Open the DATA LOADER circuit breaker Set the data load select switch to NORM Remove the PDL from the data transfer unit

receptacle Use the FMCS to do a check of the software part

number.

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737 GENERAL LOADABLE SOFTWARE A software installation procedure is in the maintenance manual, maintenance practices section (200 page block) for each software loadable LRU.

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737 GENERAL ANTENNA LOCATIONS Antenna Location These are the communication and navigation system antennas:

Weather Radar Traffic alert and collision avoidance system (TCAS) Air traffic control (ATC) Global positioning system (GPS) Very high frequency (VHF) communication High frequency (HF) communication VHF omni range (VOR) Marker beacon Radio altimeter Distance measuring equipment (DME) Localizer Glideslope.

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737 GENERAL ANTENNA LOCATIONS

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737 GENERAL FMCS CONTROL DISPLAY UNIT General The flight crew uses the control display unit (CDU, also called the MCDU) to put in flight data and to select displays and modes of operation. They also use the CDU to start ADIRU alignment. You use the CDU to test the FMCS and other systems. There are two CDUs in the airplane. They are functionally and physically interchangeable. Physical Description The CDU has a keyboard and a display unit. The keyboard has alphanumeric keys, function keys and flight phase keys. Line select keys (LSK) are on the left and right of the display unit. The CDU has these annunciators:

Fail CALL MSG (Message) OFST (Offset) EXEC (Execute).

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The EXEC light is on the right of the CDU keyboard. Maintenance BITE Page You use the MAINT BITE index page to select BITE for these systems:

Flight management computer system (FMCS) Digital flight control system (DFCS) Autothrottle system (A/T) Air data inertial reference system (ADIRU) Common display system (CDS) Engines Auxiliary power unit (APU) Fuel quantity indication system (FQIS).

This shows how to get to the MAINT BITE index page from airplane electrical power up.

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737 GENERAL FMCS CONTROL DISPLAY UNIT

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CRT MCDU

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LCD MCDU

737 GENERAL INTRODUCTION737 GENERAL RANGE737 GENERAL STRUCTURE DIMENSIONS737 GENERAL FUSELAGE DIMENSIONS737 GENERAL POWER PLANT INTRODUCTION737 GENERAL POWER PLANT ENGINE HAZARDS737 GENERAL FLIGHT CONTROL SURFACES737 GENERAL DOORS INTRODUCTION737 GENERAL - FLIGHT COMPARTMENT PANELS737 GENERAL MAIN INSTRUMENT PANELS - 1737 GENERAL MAIN INSTRUMENT PANELS - 2737 GENERAL GLARESHIELD PANELS737 GENERAL P2 CENTER INSTRUMENT PANEL AND P9 FORWARD737 GENERAL CONTROL STAND737 GENERAL P8 AFT ELECTRONICS PANEL737 GENERAL P5 AFT OVERHEAD PANEL737 GENERAL P5 FORWARD OVERHEAD PANEL - 700737 GENERAL P5 FORWARD OVERHEAD PANEL 800/900737 GENERAL AFT FLIGHT COMPARTMENT737 GENERAL ELECTRONIC EQUIPMENT COMPARTMENT737 GENERAL EE COMPARTMENT DOOR OPERATION737 GENERAL ELECTRONIC EQUIPMENT RACK E1737 GENERAL PROGRAM SWITCH MODULE737 GENERAL ELECTRONIC EQUIPMENT RACKS E2, E3, AND E4737 GENERAL ELECTRONIC EQUIPMENT RACK E5737 GENERAL ELECTRONIC EQUIPMENT RACK E8737 GENERAL LOADABLE SOFTWARE737 GENERAL ANTENNA LOCATIONS737 GENERAL FMCS CONTROL DISPLAY UNITCRT MCDULCD MCDU

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