iae v2500-a5 ltm neu
TRANSCRIPT
Book No: 518 7218
Lufthansa
Lufthansa Base
Issue: MAR. 2001For Training Purposes Only
Lufthansa 1995Technical Training GmbH
Training ManualA319/A320/A321
Location Identification-Training ManualIAE V2500-A5
ATA 72
For training purpose and internal use only.
Copyright by Lufthansa Technical Training GmbH.
All rights reserved. No parts of this trainingmanual may be sold or reproduced in any formwithout permission of:
Lufthansa Technical Training GmbH
Lufthansa Base Frankfurt
D-60546 Frankfurt/Main
Tel. +49 69 / 696 41 78
Fax +49 69 / 696 63 84
Lufthansa Base Hamburg
Weg beim Jäger 193
D-22335 Hamburg
Tel. +49 40 / 5070 24 13
Fax +49 40 / 5070 47 46
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5
LTM
HAM US/F FL 01. 2001 Page 1
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5
LTM
HAM US/F FL 01. 2001 Page 2
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5
LTM
HAM US/F FL 01. 2001
LOCATION TRAINING MANUAL V2500-A5
HOW TO USE
Identify the accessories, components or the lines marked with numbers.
Write the name and the purpose of the accessories, components or lines on the respective line of the adjacentworking sheet.
Page 3
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
4FRA US-T Bu MAR. 2001
1
4
5
3
2
7 6
Page 4
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
5FRA US-T Bu MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
1 ELECTRONIC ENGINE CONTROL (EEC)FADEC SYSTEM COMPUTER THAT CONTROLS ALL
ENGINE FUNCTIONS
2 FAN BLADE
ACCELERATE THE SECONDARY AIRFLOW AND
CONSTITUDE THE FIRST ROTOR STAGE OF PRI-
MARY AIRFLOW.
3 NOSE CONE ( SPINNER) PREVENTS THE FORMATION OF ICE
4 FAN EXIT GUIDE VANES (FEGV) 20 SEGMENTS, EACH CONTAINING
3 VANES THAT DIRECT THE SECONDARY AIRFLOW
5INLET GUIDE VANES
(STAGE 1 LPC STATOR) DIRECT THE SECONDARY AIRFLOW TO THE
BOOSTER
6 VENT AIR OUTLET OVERBOARD (BREATHER) VENT THE AIR FROM THE DEOILER OVERBOARD
7 AIR STARTERGIVES N2 ROTATION DURING START, USING AIR
PRESSURE
Page 5
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
6HAM US/F FL 01. 2001
FAN BLADE No. 17
“ T “ – MARK
NOSE CONE FLANGE ANNULUS FILLER
BALANCE WEIGHT
FAN DISK
FRONT BLADE RETAINING RING BOLT (RETAINING RING/ANNULUS FILLER)
BOLT (RETAINING RING/FAN DISK)
FAN BLADE No. 1
Page 6
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
7HAM US/F FL 01. 2001
STAGE 2.5 LPC STATOR
OIL SUPPLY LINE
SENSOR HARNESS
No. 2 BEARING
FWD BEARING COMPARTMENT
INTERMEDIATE CASE STRUTSFAN SPEED SENSORS
TRIM BALANCE SENSORTOWER SHAFT DRIVE
Page 7
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
8HAM US/F FL 01. 2001
THIS PAGE INTENTIONALLY LEFT BLANK
Page 8
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T Bu MAR. 2001
1
8
9
10
11
3
Page 9
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T Bu MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.SELECT THE PURPOSE THAT MATCHES THE EN-
GINE COMPONENT
1 ELECTRONIC ENGINE CONTROL (EEC) FADEC SYSTEM COMPUTER THAT CONTROLS ALL
ENGINE FUNCTIONS
3 NOSE CONE ( SPINNER) PREVENTS THE FORMATION OF ICE
8 RELAY BOX HOUSES THE IGNITION AND P2/T2 HEATER RELAYS
9 P2 SENSE LINEPRESSURE USED FOR EPR.SENSE LINE IS CON-
NECTED TO THE EEC
10AIR COOLED OIL COOLER AIR
MODULATING VALVEMODULATES THE AIRFLOW THROUGH THE ACOC
11 MAIN GEARBOXSUPPORTS AND DRIVES ENGINE AND AIRCRAFT
ACCESSORIES
Page 10
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
1
14
8
12
16
10
11
13 15
Page 11
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.SELECT THE PURPOSE THAT MATCHES THE EN-
GINE COMPONENT
1 ELECTRONIC ENGINE CONTROL (EEC) FADEC SYSTEM COMPUTER THAT CONTROLS ALL
ENGINE FUNCTIONS
8 RELAY BOX HOUSES THE IGNITION AND P2/T2 HEATER RELAYS
10AIR COOLED OIL COOLER AIR
MODULATING VALVEMODULATES THE AIRFLOW THROUGH THE ACOC
11 MAIN GEARBOXSUPPORTS AND DRIVES ENGINE AND AIRCRAFT
ACCESSORIES
12 STARTER AIR VALVECOMMANDS AIR PRESSURE DELIVERY TO THE
STARTER
13 BLEED SOLENOID VALVESHANDLING BLEED VALVE, MAKE_UP AIR VALVE & HP
VALVE CONTROL
14 EEC PRESSURE PROBE CONNECTIONSPROVIDES AN INTERFACE BETWEEN THE EEC AND
THE PRESSURE SUBSYSTEMS
15 STARTER AIR DUCT DELIVERS AIR PRESSURE TO THE STARTER
16 AIR COOLED OIL COOLER (ACOC) OIL COOLER
Page 12
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T Bu MAR. 2001
1
17
19
18
22 23
20 21
22
25
24
15
8 21
Page 13
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T Bu MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
1 ELECTRONIC ENGINE CONTROL (EEC) FADEC SYSTEM COMPUTER THAT CONTROLS ALL
ENGINE FUNCTIONS
8 RELAY BOX HOUSES THE IGNITION AND P2/T2 HEATER RELAYS
15 STARTER AIR DUCT DELIVERS AIR PRESSURE TO THE STARTER
17 GENERATOR CABLE POWER ROUTING TO AIRCRAFT
18 EEC HARNESSLINK BETWEEN THE EEC AND THE VARIOUS
ENGINE COMPONENTS
19 DATA ENTRY PLUG (PROGRAMMING PLUG)PROVIDES THE ENGINE ELECTRONIC IDENTITY TO
THE EEC
20 P5 PRESSURE CONNECTIONENGINE EXHAUST PRESSURE FOR EPR MEA-
SUREMENT
21 P2 PRESSURE CONNECTION INLET PRESSURE FOR EPR MEASUREMENT
22 P12,5 PRESSURE CONNECTION FAN EXIT PRESSURE
Page 14
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T Bu MAR. 2001
23 P25 PRESSURE CONNECTION COMPRESSOR INLET PRESSURE / BOOSTER EXIT
24 PB PRESSURE CONNECTIONP3 HIGH PRESSURE COMPRESSOR OUTLET
PRESSURE
25 PAMB PRESSURE CONNECTIOJN PRESSURE AMBIEND
Page 15
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T Bu MAR. 2001
STUDENT NOTES:
Page 16
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
26
27
29
30
31
32
3433
35
36
28
Page 17
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.SELECT THE PURPOSE THAT MATCHES THE EN-
GINE COMPONENT
26 ACOC BYPASS VALVE BYPASSES THE COOLER
27 OIL TEMPERATURE SENSOROIL TEMPERATURE THERMOCOUPLE IS USED FOR
HEAT MANAGEMENT SYTEM
28 ACOC MODULATING VALVE ACTUATOR & SERVO
VALVE
IS SUPPLIED WITH FUEL PRESSURE AND DRIVES
THE MODULATING VALVE TO CONTROL THE AIUR
FLOW VIA THE COOLER
29 A/C HIGH STAGE BLEED VALVE SOLENOIDMAKES SURE THE HIGH STAGE BLEED VALVE IS
CLOSED IN CRUISE FLIGHT
30 HANDLING BLEED SOLENOID VALVE FOR 7A HANDLING BLEED VALVE
31 HANDLING BLEED SOLENOID VALVE FOR 7C HANDLING BLEED VALVE
32 HANDLING BLEED SOLENOID VALVE FOR 7B HANDLING BLEED VALVE
33 HANDLING BLEED SOLENOID VALVE FOR 10 HANDLING BLEED VALVE
34 TURBINE COOLING AIR SOLENOID VALVE MAKE-UP AIR (10th STAGE COOLING) VALVE
Page 18
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
35 NO.4 BEARING SCAVENGE & BREATHER LINEOIL/AIR RETURN LINE FROM NO.4 BEARING
COMPARTMENT
36 NO.4 BEARING SCAVENGE VALVEMAINTAINS NO. 4 BEARING COMPARTMENT SEAL
DIFFERENTIAL PRESSURE WITHIN LIMITS
Page 19
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
STUDENT NOTES:
Page 20
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T BU MAR. 2001
41
43
37
38 39
45
48
47
46
42 44
40
Page 21
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T BU MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
37 AFT ENGINE MOUNT AFT ENGINE SUPPORT
38 COOLING AIR TUBES PERMANENT COOLING HPT STAGE 2
39 HANDLING BLEED VALVE STAGE 10 HANDLING BLEED VALVE
40 HANDLING BLEED VALVE STAGE 7A HANDLING BLEED VALVE
41 TURBINE EXHAUST CASE (TEC) HOUSES THE LPT ROTOR/STATOR ASSEMBLY
42 LPT CASE HOUSES THE LPT
43 HPT CASE HOUSES THE HPT
44 DIFFUSER CASE HOUSES THE COMBUSTION CHAMBER
45 IGNITION EXITER UNIT A / BSTORE AND DISCHARGE HIGH VOLTAGE PULSES
TO THE IGNITERS
Page 22
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T BU MAR. 2001
46 AIR COOLED AIR COOLER (ACAC) OUTLET DUCT BUFFER AIR COOLER/ FAN COOLING AIR OUTLET
47 LPT CASE COOLING LPT ACTIVE CLEARANCE CONTROL
48 HANDLING BLEED VALVE STAGE 7B HANDLING BLEED VALVE
Page 23
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T BU MAR. 2001
STUDENT NOTES:
Page 24
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T Bu MAR. 2001
40
39
48
57
43
4950 51
52
53
45
58
56
5554
46
Page 25
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T Bu MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
39 HANDLING BLEED VALVE STAGE 10 HANDLING BLEED VALVE
40 HANDLING BLEED VALVE STAGE 7A HANDLING BLEED VALVE
43 HPT CASE HOUSES THE HPT
45 IGNITION EXITER UNIT ASTORE AND DISCHARGE HIGH VOLTAGE PULSES
TO THE IGNITERS
46 AIR COOLED AIR COOLER (ACAC) OUTLET DUCT BUFFER AIR COOLER/ FAN COOLING AIR OUTLET
48 HANDLING BLEED VALVE STAGE 7B HANDLING BLEED VALVE
49 LPT CASE COOLING MANIFOLD FAN AIR SUPPLY FOR LPT ACC
50 BORESCOPE PLUG BORESCOPE PLUG NGV STAGE 1 HPT
51 MAKE UP AIR DUCTSUPPLY OF 10 STAGE COOLING AIR FOR HPT
STAGE 2 ROTOR COOLING
Page 26
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T Bu MAR. 2001
52 HPT COOLING AIR HPT STAGE 2 COOLING AIR
53 IGNITOT PLUG IGNITOR PLUG A
54 ACTIVE CLEARANCE CONTROL VALVE LPT ACC VALVE
55 ACTIVE CLEARANCE CONTROL VALVE HPT ACC VALVE
56 FUEL DISTRIBUTION VALVE DISTRIBUTES THE FUEL TO THE BURNERS
57 ACC VALVE ACTUATOR OPERATES THE LPT/HPT ACC VALVE
58 BOOSTER STAGE BLEED VALVE (BSBV) ACTUATORSLAVE ACTUATOR IS OPERATED BY THE MASTER
ACTUATOR
Page 27
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
HAM US-T Bu MAR. 2001
STUDENT NOTES:
Page 28
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
59
54
6061
62
56
64
65
55
63
66
Page 29
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
54 ACTIVE CLEARANCE CONTROL VALVE LPT ACC VALVE
55 ACTIVE CLEARANCE CONTROL VALVE HPT ACC VALVE
56 FUEL DISTRIBUTION VALVE DISTRIBUTES THE FUEL TO THE BURNERS
59 HPT CASE COOLING MANIFOLD HPT ACC
60 BUFFER AIR DUCT STAGE 12 AIR FOR COOLING NO.4 BEARING
61 IGNITION LEAD IGNITION SYSTEM B
62 FUEL SPRAY NOZZLE NO.7 SPRAY FUEL INSIDE THE COMBUSTION CHAMBER
63 ACC ACTUATOR ELECTRICAL CONNECTOR SUPPLY OF CONTROL SIGNAL FROM THE EEC
64 ACC ACTUATION RODCONNECTION BETWEEN ACTUATOR AND ACC
VALVE GEARBOX
Page 30
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
65 SCAVENGE OIL TUBE SCAVENGE OIL NO.4 BEARING COMPARTMENT
66 FIRE DETECTION LOOP FIRE DETECTION (CONNECTED TO FDU)
Page 31
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
STUDENT NOTES:
Page 32
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
41
37
67
68
49
71
69
70
52
Page 33
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
37 AFT ENGINE MOUNT AFT ENGINE SUPPORT
41 TURBINE EXHAUST CASE (TEC) HOUSES THE LPT ROTOR/STATOR ASSEMBLY
49 CASE COOLING MANIFOLD LPT ACC
52 TURBINE COOLING AIR PERMANENT COOLING HPT STAGE 2
67 EGT PROBE EXHAUST GAS TEMPERATURE FOR INDICATING
68 EGT HARNESS ALUMEL/CROMEL
69 EGT JUNCTION BOXJUNCTION CONNECTION OF THE 4 EGT THERMO-
COUPLES
70 OIL PRESSURE LINE OIL SUPPLY TO NO. 5 BEARING
71 HPT CASE COOLING MANIFOLD HPT ACC
Page 34
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAR. 2001
75
73
74
76
72
37
Page 35
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
37 AFT ENGINE MOUNT SUPPORT OF THE ENGINE
72 LPT BLADES STAGE 7 BLADES
73 BEARING COMPARTMENT COVER NO. 5 BEARING COMPARTMENT
74 SCAVENGE OIL LINE NO. 5 BEARING
75 OIL PRESSURE LINIE NO. 5 BEARING
76 TEC STRUT WITH P4.9 PROBE
Page 36
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
89
87
80
88
9178
90
86
77
84
82
83
81
85
79
Page 37
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
77 SUPPLY LINIE FUEL SUPPLY TO PUMP
78 LOW OIL PRESSURE SWITCH MASTER WARNING ON E/WD
79 OIL PRESSURE TRANSMITTER INDICATION ON ECAM ENGINE PAGE
80 FUEL DIVERTER AND RETURN VALVE FUEL RETURN TO TANK / USED FOR HMS
81 FUEL COOLED OIL COOLER COOLS THE ENGINE OIL
82 HYDRAULIC LINE HYDRAULIC SUCTION LINIE
83 HYDRAULIC LINE HYDRAULIC PRESSURE LINIE
84 FILTER DIFFERNTIAL PRESSURE SWITCH OIL SCAVENGE FILTER
85 FUEL FILTER FILTERS THE FUEL SUPPLIED TO THE PUMP
Page 38
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
86 HYDRAULIC PUMP FILTER CASE DRAIN FILTER
87 OIL TANK STORES THE ENGINE OIL
88 OIL FILTER FILTER SCAVENGE OIL
89 HANDLING BLEED VALVE STAGE 7C
90 OIL SCAVENGE LINIE BEARING NO. 5
91 COOLING AIR TUBE PERMANENT COOLING STAGE 2 HPT
Page 39
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
STUDENT NOTES:
Page 40
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAR. 2001
15 7
94
93
87
83 92
85
82
Page 41
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
7 STARTER
15 STARTER DUCT
82 HYDRAULIC LINE HYDRAULIC PUMP SUCTION LINE
83 HYDRAULIC LINE HYDRAULIC PUMP PRESSURE LINE
85 FUEL FILTER
87 OIL TANK OIL STORAGE
92 HYDRAULIC PUMP YELLOW OR GREEN SYSTEM
93 OIL FILTER PRESSURE FILTER
94 OIL TANK REMOTE CONNECTIONS FILL CONNECTIONS (PRESS / OVERFLOW)
Page 42
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
4
9395
6
597
967
98
Page 43
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
4 FAN EXIT GUIDE VANES (FEGV) 20 SEGMENTS, EACH CONTAINING
3 VANES THAT DIRECT THE SECONDARY AIRFLOW
5INLET GUIDE VANES
(STAGE 1 LPC STATOR) DIRECT THE SECONDARY AIRFLOW TO THE
BOOSTER
6VENT AIR OUTLET OVERBOARD (BREATHER)
VENT THE AIR FROM THE DEOILER OVERBOARD
7STARTER
93 OIL FILTER PRESSURE FILTER
95 HYDRAULIC PUMP PAD FEATURES A SEALOL SEAL
96 EEC DEDICATED ALTERNATOR POWER SUPPLY EEC >12% N2
97 ABRADABLE LINING
98 ANNULUS FILLER AERODYNAMIC
Page 44
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu Bu. 2001
101
42
104
10389102
44100
99
Page 45
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu Bu. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
42 LPT CASE
44 DIFFUSER CASE
89 HANDLING BLEED VALVE HPC STAGE 7 C
99 HPC REAR OUTER CASE
100 HPC FRONT CASE
101 IDG OIL COOLER FUEL COOLED OIL COOLER
102 VSV ACTUATOR COMPRESSOR CONTROL
103 CUSTOMER BLEED AIR DUCT STAGE 7
104 AIR COOLED AIR COOLERBUFFER AIR COOLER FOR COOLING HEATSHIELD
BEARING NO. 4
Page 46
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
89
107
88
101
106
102
105
103
Page 47
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
88 LPT CASE
89 HANDLING BLEED VALVE HPC STAGE 7 C
101 IDG OIL COOLER
102 VSV ACTUATOR COMPRESSOR CONTROL
103 CUSTOMER BLEED AIR DUCT STAGE 7
105 CUSTOMER BLEED AIR DUCT STAGE 10
106 BSBV MASTER ACTUATOR COMPRESSOR CONTROL
107 FUEL METERING UNIT (FMU) HAS A FUEL METERING, OVERSPEED & PSRV
Page 48
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
108
110
111
109
88
112113
107
Page 49
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAR. 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
88 SCAVENGE OIL FILTER
107 FUEL METERING UNIT (FMU) HAS A FUEL METERING, OVERSPEED & PSRV
108 OIL RETURN LINE COMMON SCAVENGE LINE
109 MAGNETIC CHIP DETECTOR MASTER
110 OIL FILTER PRESS LINE SCAVENGE OIL DIFFENTIAL
111 OIL TEMPERATURE SENSOROIL TEMPERATURE INDICATION ECAM ENGINE
PAGE
Page 50
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
103
105
114
119
102
117
118
116
106
115
120
Page 51
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
102 VSV ACTUATOR COMPRESSOR CONTROL
103 CUSTOMER BLEED AIR DUCT STAGE 7
105 CUSTOMER BLEED AIR DUCT STAGE 10
106 BSBV MASTER ACTUATOR COMPRESSOR CONTROL
114 RETRACT & EXTEND LINE TO SLAVE ACTUATOR FUEL SUPPLY FROM THE MASTER ACTUATOR
115 HP FUEL SUPPLY HYDRAULIC POWER
116 BSBV FEEDBACK SIGNAL FEEDBACK TO EEC
117 LP FUEL RETURN
118 BSBV COMMAND SIGNAL
Page 52
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
119 VSV ACTUATOR WITH LVDT FEEDBACK SIGNAL
120 BSBV AIR OUTLET DISCHARGE OF 2.5 LP AIR
Page 53
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
STUDENT NOTES:
Page 54
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T BU MAY 2001
122
123
121
102
119
Page 55
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T BU MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
102 VSV ACTUATOR
119 VSV ACTUATOR WITH LVDT FEEDBACK SIGNAL
121 VSV ACTUATOR TORQUE MOTOR
122 VSV CRANKSHAFT
123 VSV ACTUATING LEVER STAGE 5
Page 56
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T BU MAY 2001
STUDENT NOTES:
Page 57
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
104
127
55
126
54
64
125
56
57
122 124
Page 58
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
54 LPT ACC VALVE (ACTIVE CLEARANCE CONTROL) SUPPLY OF FAN AIR TO THE LPT CASE
55 HPT ACC VALVE (ACTIVE CLEARANCE CONTROL) SUPPLY OF FAN AIR TO THE HPT CASE
56 FUEL DISTRIBUTION VALVE DISTRIBUTION OF FUEL TO THE FUEL NOZZLES
57 ACTIVE CLEARANCE CONTROL ACTUATOR ACTUATION OF LPT AND HPT ACC VALVE
64 ACTIVE CLEARANCE CONTROL ACTUATION RODCONNECTION BETWEEN ACC GEARBOX AND ACC
ACTUATOR
104 ACAC (AIR COOLED AIR COOLER)12th STAGE AIR COOLING WITH FAN AIR (FOR NO.4
BEARING COMPARTMENT HEATSHIELD COOLING)
122 VSV CRANKSHAFT
124 MAIN FUEL LINE (METERED FUEL)
125 FUEL NOZZLE SUPPLY LINE
Page 59
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
126 ACC VALVE GEARBOX
127 BUFFER AIR TO/FROM ACAC COOLED 12th STAGE AIR FOR COOLING BEAR NO.4
Page 60
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
STUDENT NOTES:
Page 61
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
4
75
67
90
128
37
41
Page 62
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
4 FAN EXIT GUIDE VANES (FEGV)20 SEGMENTS, EACH CONTAINING 3 VANES THAT
DIRECT THE SECONDARY AIRFLOW
37 AFT ENGINE MOUNT AFT ENGINE SUPPORT
41 TURBINE EXHAUST CASE (TEC)
67 EGT PROBE MEASURMENT OF T4.9 (T5)
75 NO.5 BEARING OIL PRESSURE LINE OIL SUPPLY
90 NO.5 BEARING OIL SCAVENGE LINE OIL RETURN
128 P 4.9 PROBE EPR
Page 63
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
90
67
132
51131
130
129
5242
Page 64
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
42 LPT CASE
51 MAKE UP AIR HPT STAGE 2 ROTOR COOLING
52 HPT STAGE 2 AIR DUCT PERMANENT COOLING AIR
67 EGT PROBE MEASUREMENT T4.9 (T5)
90 NO. 5 BEARING OIL SCAVENGE LINE RETURN LINE
129 BUFFER AIR LINE TO NO 4 BEARING COMPARTMENT HEATSHIELD
130 FUEL SPRAY NOZZLE
131 COMBUSTION CHAMBER LOCATING PINLOCATING INNER AND OUTER COMPUSTIN CHAM-
BER CASE
132 BORESCOPE PLUG ACCESS TO HPT STAGE 2
Page 65
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
88
108
136
135
133 134
87
Page 66
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
87 OIL TANK STORAGE OF OIL
88 SCAVENGE OIL FILTER FILTERING THE RETURN OIL
108 COMMON SCAVENGE OIL RETURN LINE
133 OIL TANK FILLER CAP
134 OIL QUANTITY TRANSMITTER ECAM INDICATION ( ENGINE PAGE)
135 OIL LEVEL SIGHT CLASS DIRECT OIL QUANTITY INDICATION
136 ANTI SYPHON LINE
Page 67
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
140
139
138
107
137
88
109
112
Page 68
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
88 SCAVENGE OIL FILTER FILTERING THE RETURN OIL
107 FUEL METERING UNIT (FMU)
109 COMMON SCAVENGE RETURN LINE
112 FUEL FLOW TRANSMITTER
137 HP FUEL PUMP INLET INLET FROM FCOC
138 FMU SPILL FLOW TO FD&RV
139 ENGINE FUEL PUMP
140 SCAVENGE OIL PUMP
Page 69
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
139
143140141
142
96
144
93
11
Page 70
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRAUS-T Bu MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
11 MAIN GEARBOX
93 STAGE 10 HANDLING BLEED VALVE
96 EEC DEDICATED ALTERNATOR POWER SUPPLY EEC & N2 SPEED SIGNAL
139 ENGINE FUEL PUMP
140 SCAVENGE OIL PUMP
141 LEFT SCAVENGE OIL LINE GEARBOX COMPART-
MENT
142 RIGHT SCAVENGE OIL LINE GEARBOX COMPART-
MENT
143 MAGNETIC CHIP DETECTOR FOR ANGLE GEARBOX
144 12.5 COOLING AIR COOLING DEDICATED ALTERNATOR
Page 71
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
11
6
7
35
146
145
36
Page 72
Lufth
ansa
Tec
hnic
al T
rain
ing
For
Tra
inin
g P
urpo
ses
Onl
y
ENGINELOCATION TRAINING MANUAL
V2500-A5A319/A320/A321 AIRCRAFT
LTM
FRA US-T Bu MAY 2001
ITEMNO.
IDENTIFY THE ENGINE COMPONENTITEM
NO.
SELECT THE PURPOSE THAT MATCHES THE
ENGINE COMPONENT
6 VENT AIR OUTLET OVERBOARD (BREATHER) VENT THE AIR FROM THE DEOILER OVERBOARD
7 AIR STARTERGIVES N2 ROTATION DURING START, USING AIR
PRESSURE
11 MAIN GEARBOX
35 NO.4 BEARING SCAVENGE & BREATHER LINE
36 NO.4 BEARING SCAVENGE VALVE
145 PRESSURE LINEACTUATING PRESSURE (10th STAGE)
146 NO.4 BEARING VENT PRESSURE TRANSMITTER MONITORING
Page 73
LTM
V2500-A5
LIST OF COMPONENTSLOCATION TRAINING MANUALENGINE
HAM US/F FL 01. 2001 Page: 1Book No.: 518 7218
1. EEC, Electronic Engine Control
2. Fan Blade
3. Nose Cone ( Spinner )
4. FEGV, Fan Exit Guide Vanes
5. Inlet Guide Vanes ( Stg. 1 LPC Stator )
6. Vent Air Outlet Overboard ( Breather )
7. Starter
8. Relay Box
9. P2 Sense Line
10. ACOC Modulating Valve
11. Main Gearbox
12. Starter Valve
13. Bleed Valve Solenoids
14. EEC Pressure Probe Connections
15. Starter Duct
16. ACOC, Air Cooled Air Cooler
17. Generator Cable
18. EEC Harness
19. Data Entry Plug ( Programming Plug )
20. P5 Pressure Connection
21. P2 Pressure Connection
22. P12.5 Pressure Connection
23. P25 Pressure Connection
24. PB Pressure Connection
25. PAMB Pressure Connection
26. ACOC Bypass Valve
27. HMS Oil Temperature Sensor
28. ACOC Modulating Valve Actuator andServo Valve
29. A/C High Stage Bleed Valve Solenoid
30. Stage 7A Bleed Valve Solenoid
31. Stage 7C Bleed Valve Solenoid
32. Stage 7B Bleed Valve Solenoid
33. Stage 10 Bleed Valve Solenoid
34. Make Up Air Valve Solenoid
35. No. 4 Bearing Scavenge and BreatherLine
36. No. 4 Bearing Scavenge Valve
37. Aft Engine Mount
38. HPT Stg. 2 Cooling Air
39. Stage 10 Handling Bleed Valve
40. Stage 7 A Handling Bleed Valve
41. Turbine Exhaust Case TEC
42. LPT Case
43. HPT Case
44. Diffuser Case
45. Ignition Exiter Unit A + B
46. ACAC Outlet Duct
47. LPT Case Cooling ( ACC Active ClearanceControl )
48. Stage 7 B Handling Bleed Valve
49. LPT Case Cooling Manifold
50. Borescope Plug NGV Stage 1 HPT
51. Make Up Air (HPT Stage 2 Rotor Cooling)
52. HPT Stage 2 Cooling Air
53. Ignitor Plug A
54. LPT ACC Valve (Active Clearance Control)
55. HPT ACC Valve
56. Fuel Distribution Valve
57. ACC Valve Actuator
58. BSBV Actuator ( Booster Stage BleedValve )
59. HPT Case Cooling Manifold
60. Buffer Air No. 4 Bearing Compartment
61. Ignition Lead, System B
62. Fuel Spray Nozzle No. 7
63. ACC Actuator Electrical Connector
64. ACC Actuation Rod
65. Scavenge Oil No. 4 Bearing
66. Fire Detection Loop
67. EGT Probe
68. EGT Harness
69. EGT Junction Box
70. Pressure Oil No. 5 Bearing
71. HPT Case Cooling Manifold
72. Stage 7 LPT Blades
73. No. 5 Bearing Compartment Cover
74. Scavenge Oil Line No. 5 Bearing
75. Pressure Oil Line No. 5 Bearing
76. TEC Strut with P4.9 Probe
Nur
zur
Sch
ulun
g
LTM
V2500-A5
LIST OF COMPONENTSLOCATION TRAINING MANUAL
ENGINE
HAM US/F FL 01. 2001Page: 2
77. Fuel Supply Line
78. Low Oil Pressure Switch
79. Oil Pressure Transmitter
80. Fuel Diverter and Return Valve
81. Fuel Cooled Oil Cooler
82. Hydraulic Pump Suction Line
83. Hydraulic Pump Pressure Line
84. Scavenge Filter Diff. Press. Switch
85. Fuel Filter
86. Hydraulic Pump Case Drain Filter
87. Oil Tank
88. Scavenge Oil Filter
89. HPC Stage 7 C Handling Bleed Valve
90. Scavenge Oil Line No. 5 Bearing
91. HPT Stage 2 Cooling Air
92. Hydraulic Pump
93. Pressure Oil Filter ( and Pump )
94. Oil Tank Remote Fill Connectors
95. Hydraulic Pump Pad
96. EEC Dedicated Alternator
97. Abradable Lining
98. Annulus Filler
99. HPC Rear Outer Case
100. HPC Front Case
101. IDG Oil Cooler
102. VSV Actuator
103. Pneumatic Air Duct Stage 7 (Aircraft)
104. ACAC, Air Cooled Air Cooler
105. Pneumatic Air Duct Stage 10 (Aircraft)
106. BSBV Master Actuator
107. FMU, Fuel Metering Unit
108. Common Scavenge Oil Return Line
109. Magnetic Chip Detector (Master)
110. Scavenge Oil Filter Diff. Press. Line
111. Scav. Oil Temperature Sensor
112. Fuel Flow Transmitter
113. Angle Gearbox
114. Retract and Extend Line to Slave Actuator
115. HP Fuel Supply
116. BSBV Feedback Signal
117. LP Fuel Return
118. BSBV Command Signal
119. VSV Actuator LVDT with Feedback Signal
120. BSBV Air Outlet
121. VSV Actuator Torque Motor with Command Signal
122. VSV Crankshaft
123. VSV Actuation Lever Stage 5
124. Main Fuel Line ( Metered Fuel )
125. Fuel Nozzle Supply Line
126. ACC Valve Gearbox
127. Buffer Air to/from ACAC
128. P4.9 Probe
129. Buffer Air to No. 4 Bearing Compartment
130. Fuel Spray Nozzle
131. Combustion Chamber Locating Pin
132. Borescope Plug HPT Stage 2
133. Oil Tank Filler Cap
134. Oil Quantity Transmitter
135. Oil Level Sight Glass
136. Anti Syphon Line
137. HP Fuel Pump Inlet (from FCOC)
138. FMU Spill Flow to FD&RV
139. Engine Fuel Pump
140. Scavenge Oil Pump
141. Scavenge Oil Line Left Gearbox Compart-ment
142. Scavenge Oil Line Right Gearbox Com-partment
143. Magnetic Chip Detector (Angle Gearbox)
144. Cooling Air to EEC Dedicated Generator
145. Pressure Signal to No. 4 Bearing Sca-venge Valve
146. No. 4 Bearing Vent Pressure Transmitter