B737B7 37--600/7 -600/700/ 00/800 800/90 /900 0
Genera Gen erall Fami Familiar liarizat ization ion
Training Manual
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Boeing B737B737 -- 600/700/800/900 600/700/8 00/900 AT ATA DIVERSE
General Familiarization
Level 1 OSA B737--6 DIVERSE L1
Issue: Jul 2007 Author: OSA For Training Purposes Only OSA 2007
Training Manual
One Stop Airline MRO Support Pvt. Ltd
Boeing B737B737 -- 600/700/800/900 600/700/8 00/900 AT ATA DIVERSE
General Familiarization
Level 1 OSA B737--6 DIVERSE L1
Issue: Jul 2007 Author: OSA For Training Purposes Only OSA 2007
One Stop Airline MRO Support Pvt. Ltd
Training Manual
For training purposes and internal use only. by One Stop Airline MRO Support Pvt. Ltd (OSA).
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GENERAL FAMILIARIZA AMILIARIZATION TION
B737-B737-- 600/700/800/900
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INTRODUCTION GENERAL AIRCRAFT
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GENERAL DESCRIPTION The design design of the B737 NG (Next Generation) Generation) is based on on the B737 Classic Classic family: B737--300/-400/-500. The Boeing B737 NG is a twin engine airplane. It is designed for short to medium range operation and consists of four models: B737--600 B737--700 B737--800 B737--900 In this document, the use of the designator B737 NG without a reference to a specific model indicates that this information applies to all four models.
Evaluation The Boeing 737 NG programme was launched in June 1993, starting with the B737--700 (22cm (9in) longer than the t he original B737--300 B737--300 and a seating up to 149). The B737--800 project was launched in September 1994 and is based on the B737--400 but is significantly longer at 39.4m (129ft 6in) and seats up to 189. The --800 has been available with winglets since May 2001. These reduce aerodynamic drag thereby reducing fuel consumption by up to 7%. The B737--600 was the third of the NG’s to be built and started in March 1995 and originated as the B737--500 with a similar length fuselage, seating between 108--132. Boeing began work on the stretched B737--900 in April 1997 and opted to use the same (-800) emergency exit layout, with 4 main exit doors and 4 overwing exits, thereby still restricting the maximum passenger load to 189.
B737-B737-- 600/700/800/900
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INTRODUCTION GENERAL AIRCRAFT
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35,80 mtr
12,60 mtr 14,30 mtr
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B737B737--600 B737B737--700 B737B737--800 B737B737--900
31,20 mtr 31,20 33,60 33,6 0 mtr 39,50 39,5 0 mtr 42,10 42,1 0 mtr
Figu Figure re 1
Dimen imensi sion on
B737-B737-- 600/700/800/900
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INTRODUCTION GENERAL AIRCRAFT
B737-B737-- 600/700/800/900
One Stop Airline MRO Support Pvt. Ltd B737 -- 600
B737-- 700
B737-- 800
B737 -- 900
Taxi
56530
60550
78460
79243
Maximum weight (kg): Take-off
56250
60330
78220
79016
Landing
54650
58060
65310
66360
Zero-fuel
51480
54660
61690
62730
Powerplant: Model
CFM56-- 7
CFM56--7
CFM56-- 7
CFM56-- 7
Type
B18
B20 / B22 / B24
B24 / B26 / B27
B24 / B26 / B27
Static Thrust (lb)
19500
20600 / 22700 / 24200
24200 / 26400 / 27300
24200 / 26400 / 27300
Bypass Ratio
5.5 : 1
5.4 : 1
5.3 : 1
5.1 : 1
Accomodation: Max. Seating (single class) Hold Volume (m3)
132
149
189
189
23.30
30.20
47.10
52.40
20536
20536
20536
20536
2926
2726
Fuel (kg): Standard Optional (BBJ) ! Y L N O S E S O P R U P G N I N I A R T R O F
30170
Long Range Cruise: Range with max. payload (nm)
3153
3299
Figu Figure re 2
Airc Aircra raft ft Data Data
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INTRODUCTION GENERAL AIRCRAFT
B737--600/700/800/900
One Stop Airline MRO Support Pvt. Ltd P7 P1
P2
P3
P8 P9
P7 (GLARESHIELD)
1 1 ! Y L N O S E S O P R U P G N I N I A R T R O F
P1 Figure 3
P2 FLIGHT DECK PANEL - FRONT VIEW
P3
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INTRODUCTION GENERAL AIRCRAFT
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P8
P8
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P9
PILOTS’ CONTROL STAND
P9
Figure 4
FLIGHT DECK PANEL - PEDESTAL
B737--600/700/800/900
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INTRODUCTION GENERAL AIRCRAFT
B737--600/700/800/900
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1
P 5 AFT
P 5 AFT P 5 FWD
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P 5 FWD
Figure 5
FLIGHT DECK PANEL - OVERHEAD
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INTRODUCTION GENERAL AIRCRAFT
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GROUND OPERATIONS The doors, service connections and access panels on the B737 NG are located to facilitate simultaneous ground operations and minimum ground operations and turn around times.
Self--Sufficiency The 737 can operate from modern and non--modern airports. These are the Systems that make the airplane self sufficient: The APU supplies on--ground or in--flight electrical power The APU supplies air for engine starting The APU maintains an air--conditioned cabin during ground operations The APU is started from the airplane battery The airplane has large fuel and water capacity Alternative Systems allow dispatch with inoperative Systems Two or more Systems which have equal function but one System operates at a time which allows more rapid fault dispatching Self--contained airstairs (Option)
! Y L N O S E S O P R U P G N I N I A R T R O F
B737--600/700/800/900
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INTRODUCTION GENERAL AIRCRAFT
B737--600/700/800/900
One Stop Airline MRO Support Pvt. Ltd FUELING
GALLEY SERVICE
BAGGAGE HANDLING
BAGGAGE HANDLING
POTABLE WATER SERVICE
ELECTRICAL POWER APU 2
1
FORWARD AIRSTAIRS ! Y L N O S E S O P R U P G N I N I A R T R O F
STARTING AIR 1 1 2
NOT REQUIRED IF APU IS IN USE. AUXILIARY POWER UNIT CAN PROVIDE: w ELECTRICAL POWER w ENGINE START w AIR CONDITIONING
AIR CONDITIONING 1
Figure 6
VACUUM GALLEY LAVATORY SERVICE SERVICE (SECOND POSITION)
Servicing
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MAINTENANCE DOCUMENTS
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MAINTENANCE DOCUMENTS - INTRODUCTION General The maintenance documents will help you to do scheduled and unscheduled maintenance work. System Schematics Manual The System Schematic Manual (SSM) gives the user an understanding of system operation and helps in the fault isolation process. It supplies the interconnection of all LRUs of a system or subsystem. It also supplies a general know-ledge about system operation. Standard Wiring Practices Manual The Standard Wiring Practices Manual has instructions for maintenance and repair of the wiring of all Boeing airplanes. It is not customized. Fault Reporting Manual The flight crew uses the Fault Reporting Manual (FRM) to improve communication with maintenance personnel and for future automatized fault reporting. The flight crew uses the FRM to get fault codes for airplane faults. These faults can be flight deck effects or other faults. The FRM has standard log book write-ups for each fault code. FRM fault codes refer you to the FIM - Task.
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Structural Repair Manual The Structural Repair Manual (SRM) supplies descriptive information and specific instructions to help in field repair of airplane structure. The SRM is not customized. It has data relative to these areas: Allowable damage evaluation Typical repairs Material identification Material substitution Fastener installation Alignment check Planning.
B737--600/700/800/900
Dispatch Deviation Guide The Dispatch Deviation Guide (DDG) supplies Boeing’s recommended minimum equipment required for dispatch in the Master Minimum Equipment List (MMEL). It also supplies the procedures for dispatch with a fault if permitted. Training Information Point Each maintenance document has an introduction to show you how to use that document.
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MAINTENANCE DOCUMENTS
One Stop Airline MRO Support Pvt. Ltd
B737--600/700/800/900
NOTE:
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THE SHADOWED DOCUMENTS CAN BE FOUND IN THE BOEING PORTABLE MAINTENANCE AID (PMA)
PMA
Figure 7
MAINT. DOCUMENTS - INTRODUCTION
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MAINTENANCE DOCUMENTS
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Scheduled Maintenance These are examples of scheduled maintenance work: Through stop checks Airplane turn around Daily checks Planned checks.
Unscheduled Maintenance These are examples of unscheduled maintenance work: Flight faults Ground faults Service problems Structural damage.
You use these documents to do scheduled maintenance: Maintenance Planning Document (MPD) Airplane Maintenance Manual (AMM).
You use these documents to do unscheduled maintenance: Fault Reporting Manual (FRM) Fault Isolation Manual (FIM) (PMA)! Structural Repair Manual (SRM) Dispatch Deviations Guide (DDG) Airplane Maintenance Manual (AMM) (PMA)!
These documents supply supporting data to do scheduled maintenance: System Schematics Manual (SSM) Wiring Diagram Manual (WDM) Structural Repair Manual (SRM) Illustrated Parts Catalog (IPC). Maintenance Planning Document The Maintenance Planning Document (MPD) defines the tasks for each type of scheduled maintenance check. Airlines use the MPD to make task cards that the technician uses during the maintenance checks.
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B737--600/700/800/900
NOTE:
NOTE: SOME OF THIS DOCUMENTS CAN BE FOUND IN THE DIGITAL BOEING PORTABLE MAINTENANCE AID (PMA)!
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MAINTENANCE DOCUMENTS
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SCHEDULED MAINTENANCE
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B737--600/700/800/900
UNSCHEDULED MAINTENTANCE
NOTE: THE SHADOWED DOCUMENTS CAN BE FOUND IN THE BOEING PORTABLE MAINTENANCE AID (PMA)
Figure 8
MAINT. DOCUMENTS - MAINTENANCE
PMA
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ELECTRICAL POWER
DC AMP
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24--00
CPS FREQ
SYS DATA
A EPC
DC VOLTS / AC AMPS / AC VOLTS
BPCU BAT
TR1
BAT BUS
GRD PWR
TR3 TEST
STBY PWR
A
EXTERNAL POWER
APU GEN GEN1 GEN2
TR2
INV TEST
STBY PWR
OFF
OFF
BAT
ON DC
GALLEY ON
STATIC INV
TRU 1
TO SYS
GCB 2
AC
P5--13 2
1 STANDBY POWER DISCONNECT
DISCONNECT
BAT
GCU 2 SYS STATUS
IDG 2
OFF AUTO
TO SYS
A SCU
P5--5
APB
ON
O F F
BUS TRANSFER A U T O
OFF ON GEN 1
DC STDBY
TRU 3
GRD PWR OFF
! Y L N O S E S O P R U P G N I N I A R T R O F
AC STDBY
TRU 2
SYS STATUS
AGCU
APU STARTER--GENERATOR
CHARGER
A
DC BUSES
OFF
APU GEN APU
ON GEN 2
GCB 1
P5--4
GCU 1
Figure 9
IDG 1
POWER / CONTROL - GEN. DESCRIPTION
AC BUSES
BATTERY
SPCU
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ELECTRICAL POWER
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EL. METERS, BATTERY & GALLEY POWER MODULE General You use the electrical meters, battery and galley power module (P5-13) for these functions: See electrical power parameters for AC and DC components or buses Connect battery power to electrical buses with the battery switch Supply and remove power to the galleys with the galley switch. The module also has these BITE functions: Supplies DC and standby power system failure indication Monitors the dc and standby power and saves fault messages in memory. Shows fault messages on the LED alphanumeric display. See the training information point page in this section for more information on BITE. AC Meter Selector The AC meter selector is a rotary selector with seven positions. Each position, except the TEST position, is related to an AC power source or AC bus. The alphanumeric display shows these parameters for the three generators: Voltage (AC VOLTS) Load (AC AMPS) Output frequency (CPS FREQ). The alphanumeric, display shows only voltage and frequency when you select one of these: STBY PWR GRD PWR INV. The selector must be in the TEST position to use the P5-13 BITE.
B737--600/700/800/900 24--00
DC Meter Selector The DC meter selector is a rotary selector with seven positions. Each position, except the TEST position, is related to a DC power source or DC bus. Voltage (DC VOLTS) and load (DC AMPS) show on the alphanumeric display when you put the selector in any of the TR positions or any of the BAT positions. Only voltage shows when you put the selector to the BAT BUS or STBY PWR positions. The selector must be in the TEST position to use the P5-l3 BITE. BAT DISCHARGE Light The amber BAT DISCHARGE light gives indication of main battery discharge or auxiliary battery discharge. The BAT DISCHARGE light temporarily comes on during an APU start with battery power. See the APU chapter for more information on APU starting.(AMM PART I 49) TR UNIT Light The amber TR UNIT light gives indication of transformer rectifier unit (TRU) failure. The TR UNIT light comes on for any one of these reasons: Any TRU fails on the ground, or TRU 1 fails in flight, or TRU 2 and TRU 3 fail in flight. ELEC Light The ELEC light gives indication that the DC system or standby power system has a failure. You use BITE to find the failure. The amber ELEC light comes on only when the airplane is on the ground. MAINT Switch You use the maintenance switch during BITE. The BITE operates only on the ground. The maintenance switch is a momentary push-button switch.
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ELECTRICAL POWER
B737--600/700/800/900
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ELECTRICAL METERS, BATTERY, AND GALLEY POWER MODULE (P5)
24--00
DC AMP
CPS FREQ
LED ALPHANUMERIC DISPLAY
DC VOLTS / AC AMPS / AC VOLTS BAT DISCHARGE
a
FLIGHT COMPARTMENT DC METER SELECTOR
TR UNIT a
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OFF
OFF
ON
ON
BATTERY SWITCH (BEHIND COVER)
STBY PWR TEST
GRD PWR
TEST
OFF OFF
DC
AC METER SELECTOR
INV
STBY PWR
TR3
ON
IFE/PASS SEAT
MAINT
APU GEN GEN1 GEN2
TR2
BAT CAB/UTIL
a
TR1
BAT BUS 2
ELEC
AUX BAT BAT
MAINTENANCE SWITCH
GALLEY ON
GALLEY POWER SWITCH
1 AC
ELECTRICAL METERS, BATTERY, AND GALLEY POWER MODULE (P5) 1
AIRPLANES WITH GALLEY SWITCH
2
AIRPLANES WITH CABIN UTILITY AND IFE SWITCHES
Figure 10
EL. METERS / BATTERY / GALLEY PWR MODULE
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LED Alphanumeric Display The LED alphanumeric display shows this type of information: DC parameters (amps, volts) AC parameters (amps, volts, frequency) As many as two lines of maintenance fault messages. The selectors and the maintenance switch control what shows on the alphanumeric display. Battery Switch The main battery energizes these buses and components when you put the battery switch to the ON position: Switched hot battery bus Battery bus Static inverter AC standby bus DC standby bus P5-13 alphanumeric display. The battery switch is a two-position switch. The cover, when down, is a guard for the switch in the ON position. You must lift the cover before you move the switch to the OFF position. Galley Switch The galley switch controls galley electrical power. The switch is a two-position switch.
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Cab/Util Switch and IFE / Pass Seat Switches Airplanes with CAB/UTIL and IFE/PASS SEAT switches; the CAB/UTIL switch controls galley and some utility’s electrical power. A second switch, the IFE/PASS SEAT switch, controls electrical power to passenger in--flight entertainment, cabin phones and passenger seat outlets. The two cabin power control switches are two--position switches
B737--600/700/800/900 24--00
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ELECTRICAL POWER
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ELECTRICAL METERS, BATTERY, AND GALLEY POWER MODULE (P5)
24--00
DC AMP
CPS FREQ
LED ALPHANUMERIC DISPLAY
DC VOLTS / AC AMPS / AC VOLTS BAT DISCHARGE
a
FLIGHT COMPARTMENT DC METER SELECTOR
TR UNIT a
! Y L N O S E S O P R U P G N I N I A R T R O F
OFF
OFF
ON
ON
BATTERY SWITCH (BEHIND COVER)
STBY PWR TEST
GRD PWR
TEST
OFF OFF
DC
AC METER SELECTOR
INV
STBY PWR
TR3
ON
IFE/PASS SEAT
MAINT
APU GEN GEN1 GEN2
TR2
BAT CAB/UTIL
a
TR1
BAT BUS 2
ELEC
AUX BAT BAT
MAINTENANCE SWITCH
GALLEY ON
GALLEY POWER SWITCH
1 AC
ELECTRICAL METERS, BATTERY, AND GALLEY POWER MODULE (P5) 1
AIRPLANES WITH GALLEY SWITCH
2
AIRPLANES WITH CABIN UTILITY AND IFE SWITCHES
Figure 11
EL. METERS / BATTERY / GALLEY PWR MODULE
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GENERATOR DRIVE AND STBY POWER MODULE General The generator drive and standby power module (P5-5) has these indications and manual controls: IDG low oil pressure indication (DRIVE lights) Indication that the battery bus or either standby bus do not have power (STANDBY PWR OFF light) Generator drive disconnect switches Standby power switch. DRIVE Light The amber DRIVE light comes on when the IDG oil pressure is less than the operation limit. Generator Drive Disconnect Switch The generator drive disconnect switch operates the disconnect mechanism for its (IDG) when the respective engine start lever is in the idle position. This removes engine accessory gearbox power from the IDG. There is one witch for each IDG. Each switch is spring-loaded to the NORMAL position. The DISCONNECT position is a momentary position. The cover is a guard for the switch in the NORMAL position. Break-away wire usually keeps the cover down. You must lift the cover and break the wire to move the switch.
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STANDBY PWR OFF Light The amber STANDBY PWR OFF light comes on when any of these buses do not have power: AC standby bus DC standby bus Battery bus.
B737--600/700/800/900 24--00
Standby Power Switch The standby power switch gives you manual control of the AC and DC standby power bus sources. The switch is a three-position switch. The switch is usually in the AUTO position. The cover is a guard for the switch in the AUTO position.