Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Airbus A330
RR Trent 700
GE CF6
PW 4000
OJT B1 or B1/B2
DERICHEBOURG Atis aéronautique,
Parc Algorithmes, Immeuble Thalès – 17, Avenue Didier Daurat 31700 Blagnac
Tél. 05 34 60 61 40 -  05 34 60 61 50
DOC.FOR.49 ed1
Page 1 sur 51
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
TRAINEE
NAME:
Forename:
Licence number:
Experience on an aircraft with similar technology:
Signature:
YES
NO
Date :
/
/
ON JOB TRAINING
Type of training:
Type:
A 330 (RR Trent 700)
A 330 (GE CF6-80)
A 330 (PW 4000)
B1
Start date :
B2
/
B1/B2
/
End Date :
/
/
Performed at :
DERICHEBOURG ATIS AÉRONAUTIQUE
STAMP :
PRACTICAL ASSESSORS
Licence
number/Stamp
NAME
Signature
Date
Validation by Quality Department:
Date:
Name:
Signature:
Page 2 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
SUBJECT
The aim of this document is to record all the practical tasks performed by engineers within ATIS
Aviation, PART 145 FR.145.107 approved maintenance organisation, in order to comply with the
requirements of Appendix III of PART 66 to have the B1 or B2 or B1/B2 rating on A330
(RR/PW/GE)
Any task performed in the frame of this On Job Training (OJT) will have to be signed by the
trainee engineer and validated by assessors. This OJT will be performed under the responsibility of
one or more B1 or B2 or B1/B2 qualified engineers. (See “PRE-REQUISITE” on page 4/47)
After this training, the engineer will be able to:
- perform verifications of systems, engines, components and operational functions such as
specified in the maintenance manual,
- analyse all information in order to make decisions regarding trouble shooting and corrective
actions as per maintenance manual,
- describe the component replacement procedures specific to aircraft type.
DURATION
-
(1)
Engineer with B1 or B2 or B1/B2 rating and six month experience on an aircraft with a similar
technology: 70 hours(1),
- Engineer with B1 or B2 or B1/B2 rating and less than six month experience on an aircraft
with a similar technology: 140 hours(1),
- Engineer with no B1 or B2 or B1/B2 rating on an aircraft with a similar technology: four
months.
The 70/140 hours do not have to be necessarily performed in a row, but can be extended on a period adapted to
operational configuration (availability of aircraft, trainee and assessors).
CLASSIFICATION
Classifies the importance of a task for the completion of the practical training record.
Following classifications are used:
- Mandatory (M): This indicates that the related task is required for completion of the
practical training record.
- Optional (O):
This indicates that the related task is optional. It is recommended to
perform at least 70% of those tasks in each ATA chapter.
TASKS CODES
-
FOT: Functional Operational Test(*)
LOC: Location and identification of system components
MEL: Minimum Equipment List items requiring a maintenance procedure
RIA: Removal Installation Activation
OPC: Operational Check
SGH: Servicing Ground Handling
TSE: Trouble shooting Exercise
TVC: Carry out Thorough Visual Check
Page 3 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
-
(*)
TPR: Thorough Procedural review
If ground power or other applicable systems are unavailable a TPR will be carried out in place of a FOT.
SIGNING OFF THE TASKS
Part 66 Appendix 3 paragraph 2.2 requires that the practical training element must consist in the
performance of representative tasks and their assessment, in order to meet the following
objectives:
a) Ensure safe performance of maintenance, inspections and routine work according to the
maintenance manual and other relevant instructions and tasks as appropriate for the type
of aircraft, for example troubleshooting, repairs, adjustments, replacements, rigging and
functional checks such as engine run, etc, if required,
b) Correctly use all technical literature and documentation for the aircraft,
c) Correctly use specialist/special tooling and test equipment, perform removal and
replacement of components
The nominated trainer/assessor will sign off each task when satisfied that the trainee has attained
the demonstrable level of understanding that is required.
PRE-REQUISITE
The trainee must have participated and succeeded in a PART 147 theoretical type rating training
(T1/T2 training).
The assessors must have an experience of five years in the line maintenance and two years in the
qualification of type.
For any OJT, the assessors will have to make a request by email at the Quality Department for
validation of pre-requisit.
Page 4 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
B1/B2
Task
Code
M
M
M
B1
B1
B1
TVC
TVC
TVC
O
B1/B2
TPR
M
B1/B2
LOC
M
B1/B2
LOC
M
B1/B2
SGH
M
B1
SGH
Class
Date
Trainee's
signature
Instructor's
signature
ATA 05 - TIME LIMITS / MAINTENANCE CHECKS
05-001
05-002
05-003
05-00-00
05-50-00
05-51-11
05-004
05-51-18
Daily check
Weekly check
Walk around check
Inspection after lightning
strike
ATA 06 – DIMENSIONS and AREAS
06-001
06-20-00
Identify the major aircraft
zones
ATA 07 - LIFTING and SHORING
07-001
07-00-00
Main jacking/safety
procedures
ATA 08 – LEVELLING and WEIGHTING
08-001
08-21-00
Perform Quick Leveling
ATA 09 - TOWING and TAXIING
09-001
09-10-00
Towing points/ Limitation of
steering Angle
ATA 10 – PARKING/STORAGE
10-001
10-11-00
Parking procedures
M
B1/B2
SGH
10-002
10-20-00
Mooring of aircraft and kit
O
B&/B2
LOC
M
B1/B2
LOC
ATA 11 – PLACARDS and MARKINGS
11-001
11-21-52
Cabin door emergency
placards
Page 5 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Pressure Refuel with
Automatic Control from the
Panel 990VU
M
B1/B2
LOC
M
B1
FOT
M
B1
SGH
M
B1
SGH
O
B1/B2
SGH
O
B1
SGH
O
B1
TVC
O
B1
TVC
M
M
B2
B1/B2
FOT
SGH
M
B1/B2
TPR
Date
Trainee's
signature
Instructor's
signature
REMARKS :
ATA 12 - SERVICING
12-001
12-11-28
12-002
12-11-28
12-003
12-11-28
12-004
12-12-29
12-005
12-13-24
12-006
12-13-49
12-007
12-15-38
12-008
12-15-38
Gravity Servicing of the
APU Oil Reservoir
Fill the potable water
system using electrical
power
Fill the potable water
system without electrical
power
12-009
12-010
12-24-34
12-34-24
Draining of the Standby
Static Pressure-Lines
Aircraft grounding
Pressure Refuel With
Manual Control
Procedure To Use The
Fuel Magnetic Level
Indicators
Hydraulic power Servicing
with a hand pump
Filling of the IDG with Oil
or Addition of Oil after
Level Check
ATA 20 – STANDARD PRACTICES - Airframe
20-001
20-28-00
Electrical bonding
Page 6 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
O
B1/B2
LOC
M
B1/B2
LOC
M
B1/B2
FOT
M
B1/B2
MEL
M
B1
FOT
O
B1/B2
LOC
O
M
M
B1/B2
B1/BS
B1
FOT
TVC
SGH
O
B1/B2
TSE
Date
Trainee's
signature
Instructor's
signature
REMARKS :
ATA 21 - AIR CONDITIONNING
21-001
21-00-00
21-002
21-00-00
21-003
21-26-00
21-004
21-26-02
21-005
21-31-00
21-006
21-52-00
21-007
21-008
21-009
21-63-00
21-63-17
21-31-66
21-010
21-30-00
Air conditioning system
controls & indication in
cockpit
Air conditioning general
localisation in cockpit
Operational Test of the
Avionics-Equipment
Ventilation System
Avionics Equipment
Ventilation Overboard
Valve
Operational Test of the
Pressure Control and
Monitoring
Air-condition pack
components
System Test of the Cockpit
and Cabin Temperature
Control
Cabin temp sensor
Safety valve filter
Pressure control and
monitoring, Fault Isol(TSM)
Page 7 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
M
O
M
B1/B2
B1
B2
TVC
LOC
LOC
O
B2
FOT
M
B2
FOT
M
B2
FOT
M
B1/B2
MEL
M
B1/B2
SGH
O
B2
FOT
O
M
B2
B2
SGH
TVC
Date
Trainee's
signature
Instructor's
signature
REMARKS :
ATA 22 - AUTO FLIGHT
22-001
22-002
22-003
22-00-00
22-00-00
22-00-00
22-004
22-10-00
22-005
22-10-00
22-006
22-30-00
22-007
22-30-02
22-008
22-70-00
22-009
22-70-00
22-010
22-011
22-70-00
22-70-00
AFS controls and
indications
AFS components
AFS components
Operational Test of True
North Reference Selection
Operational Test of AP
Eng and Lock Devices of
The Side Stick Controller
and Rudder Pedals
Operational Test of the
Autothrust Isolation from
Engine Control
Autothrust instinctive
disconnect
FM MCDU menu data
entry
Operational Test of BACKUP NAV Function
Crossloading of the FM
Data
Uploading of the FM Data
Page 8 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
B1/B2
Task
Code
O
O
B2
B2
FOT
RIA
BITE Test of the Auto
Flight System
M
B2
FOT
22-97-00
Test of the LAND CAT III
Capability
M
B2
FOT
22-81-00
FCU Fault Isolation(TSM)
O
B2
TSE
Item
ATA
Subject
22-012
22-013
22-70-00
22-81-12
Operational Test of the
MCDU 3 Transfer
Remove/Install FCU
22-014
22-96-00
22-015
22-016
Class
Date
Trainee's
signature
Instructor's
signature
REMARKS :
ATA 23- COMMUNICATION
23-001
23-00-00
23-002
23-00-00
Radio and cockpit
communications
components
Radio and cockpit
communications
components
M
B2
LOC
23-003
23-00-00
Cabin communications
systems components
O
B1
LOC
23-004
23-005
23-006
23-00-00
23-11-00
23-11-00
Cabin communications
systems components
HF System operational test
HF System operational test
M
O
M
B2
B1
B2
LOC
FOT
FOT
23-007
23-11-00
O
B2
FOT
23-008
23-12-00
M
B1/B2
FOT
23-009
23-12-00
O
B2
TSE
23-010
23-12-00
M
B2
FOT
23-011
23-12-01
O
B1/B2
MEL
Operational Test of the HF
System
VHF System operational
test
Failure or the VHF 1
reception
BITE Test of the VHF
System
VHF Communication
systems
O
B1
LOC
Page 9 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
23-012
23-28-00
23-013
23-32-00
23-014
23-015
23-33-34
23-33-71
23-016
Subject
Class
B1/B2
Task
Code
O
B1/B2
FOT
O
B2
SGH
O
O
B1/B2
B1/B2
RIA
FOT
23.36.51
SATCOM System
operationnal test
Change of the existing
Prerecorded
Announcement and
Boarding Music (PRAM)
Remove/Install PES
Controller
Bite test of PES Music
Landscape camera (if
installed)
M
B2
LOC
23-017
23-42-00
Cockpit to GRD crew call
system
M
B2
FOT
23-018
23-43-00
Cockpit to GRD crew call
system
O
B1
LOC
23-019
23-020
23-44-00
23-51-07
Service Interphone System
operational test
Radio PTT Switch
O
O
B1/B2
B2
FOT
MEL
23-021
23-51-17
Remove/Install Radio PTT
switch
O
B2
RIA
23-022
23-51-00
O
B2
FOT
23-023
23-51-00
M
B1/B2
FOT
23-024
23-71-00
Operational Test of the
Oxygen Mask Microphone
BITE Test of the Audio
System
Operational Test of the
CVR
O
B1
FOT
23-71-00
Operational Test of the
CVR and of the Recording
on all Four Channels
M
B2
FOT
23-026
23-027
23-028
23-029
23-71-00
23-73-00
23-73-00
23-73-00
Operational Test of the
CVR Recording Logic,
Including Timer Relay
PA System presentation
PA System operational test
Passengers call system
O
M
M
O
B2
B2
B1
B1/B2
FOT
TVC
FOT
LOC
23-030
23-73-00
Interface and Power - Up
Test of the CIDS
O
B1
FOT
M
B2
FOT
O
B1/B2
FOT
M
B1
FOT
23-025
23-031
23-73-00
23-032
23-73-00
Interface and Power - Up
Test of the CIDS
Operational test of Cabin /
Flight Crew interphone
system
23-73-00
Operational test of the
Emergency Evacuation
Signaling system
23-033
Date
Trainee's
signature
Instructor's
signature
Page 10 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Class
B1/B2
Task
Code
Operational test of
loudspeakers via MCDU
M
B1/B2
FOT
23-73-00
Operational test of cabin
SIGNS via MCDU
M
B1
FOT
23-036
23-73-00
FAP and PIM general
presentation
M
B2
TVC
23-037
23-73-00
Cabin layout and zone
programming
M
B2
SGH
23-038
23-51-00
AMU failure, Fault
Isolation(TSM)
M
B2
TSE
23-039
23-73-00
Operational test of the
EVAC function
M
B2
FOT
23-040
23-041
23-042
23-73-00
23-73-12
23-73-19
Operational Test of Cabin
LED Signs with the MCDU
Remove/Install the FAP
Remove/Install the CAM
M
O
O
B2
B2
B1/B2
FOT
TVC
RIA
23-043
23-73-34
Remove/Install the CIDS
Director
O
B2
RIA
23-044
23-73-46
Remove/Install DEU A
and/or DEU B
M
B1/B2
RIA
M
B2
FOT
M
B2
FOT
M
B1/B2
RIA
Item
ATA
23-034
23-73-00
23-035
23-045
23-81-00
23-046
23-81-00
23-047
23-81-13
Subject
Operational Test of the
Radio Management
Operational Test of the
Radio Navigation Back-up
Mode
Removal /Installation of the
RMP
Date
Trainee's
signature
Instructor's
signature
Page 11 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
B1/B2
Task
Code
O
B1
LOC
M
B2
LOC
Class
Date
Trainee's
signature
Instructor's
signature
REMARKS :
ATA 24 – ELECTRICAL POWER.
N.B. : SERVICING tasks please refer to ATA 12
24-001
24-00-00
24-002
24-00-00
Main electrical power
panels in flight
compartment
Main electrical power
panels in flight
compartment
Page 12 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
B1/B2
Task
Code
O
B1
LOC
Engine generators and
components
M
B2
LOC
Operational Test of the
IDG Disconnect and
Reconnect Function
M
B1/B2
TVC
M
B2
FOT
O
B1/B2
LOC
O
B1
LOC
M
B2
LOC
O
B1/B2
FOT
O
B2
FOT
M
B2
FOT
O
M
B1
B1/B2
FOT
FOT
M
M
B1/B2
B1/B2
LOC
LOC
O
M
B1
B1/B2
LOC
TVC
M
M
B1
B2
LOC
LOC
Item
ATA
24-003
24-00-00
Engine generators and
components
24-004
24-00-00
24-005
24-21-00
24-006
24-22-00
24-007
24-23-00
Operational Test of the
Side 1 and Side 2 Isolation
APU generator and
components
24-008
24-24-00
Emergency generator
components
24-009
24-24-00
24-010
24-24-00
24-011
24-25-00
Emergency generator
components
Operational Test of the
Emergency Generation
System
Operational Test of the AC
Essential Generation
Switching
24-28-00
Operational Test of Static
Inverter and DC ESS BUS
SUPPLY
24-012
24-013
24-014
24-28-00
24-29-00
24-015
24-016
24-30-00
24-32-00
24-017
24-018
24-38-00
24-38-34
24-019
24-020
24-40-00
24-40-00
24-021
24-41-00
24-022
24-023
Subject
Operational Test of Static
Inverter and DC ESS BUS
SUPPLY
BITE test or the ECMU
DC generation
components
TR unit reset
Batteries and Charge
Controllers components
BCL
External power
components
External power component
Class
M
B2
FOT
24-41-00
GCU/GAPCU or
GCU/GPCU system test
Energize aircraft electrical
circuits from external
power
M
B1/B2
SGH
24-41-00
Energise aircraft electrical
circuits from the APU
M
B1
FOT
Date
Trainee's
signature
Instructor's
signature
Page 13 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
24-024
24-41-00
24-025
24-42-00
24-026
24-22-02
24-027
24-028
24-24-00
24-21-51
Subject
Energise aircraft electrical
circuits from the APU
Energise the ground
service network
AC Generation IDG Oil
circuit
Failure of ECP, Fault
isolation(TSM)
IDG Removal/installation
B1/B2
Task
Code
O
B2
FOT
M
B1/B2
FOT
O
B1/B2
MEL
O
M
B1/B2
B1/B2
TSE
RIA
M
O
B1
B1/B2
FOT
LOC
O
O
B1/B2
B1/B2
SGH
LOC
Class
Date
Trainee's
signature
Instructor's
signature
REMARKS :
ATA 25 - EQUIPMENT AND FURNISHING
25-001
25-002
25-11-00
25-11-00
25-003
25-004
25-71-00
25-21-00
Crew seats operational test
ATTENDANT seats
Operation of the exterior
ladder
Seats components
Page 14 sur 51
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Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
25-005
25-21-00
25-006
25-23-41
25-007
25-008
25-009
25-010
25-011
25-23-44
31-18-71
25-34-51
25-35-00
25-40-00
25-012
25-013
25-50-00
25-62-00
25-014
25-015
25-016
25-62-41
25-62-42
25-65-00
25-017
25-65-20
25-018
25-74-00
Emergency Locator
Transmitter (ELT)
Lower deck mobile crew
rest room equipment(if
fitted)
25-019
25-27-36
Temperature setting panel
Passenger seats
Remove /Install Ceiling
panels
Remove /Install Dado
Panel
Remove /Install PSU
AIR CHILLER
Galley equipment
Lavatories
Cargo loading system
components
Slide bottle pressure check
Removal/Installation of
Escape Slide Raft on
passenger door
E/S slide emergency exit
ELT bite test
B1/B2
Task
Code
O
B1
SGH
M
B1/B2
RIA
M
O
O
M
M
B1
B1/B2
B1/B2
B1/B2
B1/B2
RIA
RIA
LOC
LOC
LOC
M
M
B1/B2
B1
LOC
LOC
O
O
M
B1
B1
B2
RIA
TVC
FOT
M
B1/B2
LOC
O
B1
LOC
O
B1/B2
RIA
O
B1
LOC
M
B2
LOC
Class
Date
Trainee's
signature
Instructor's
signature
REMARKS :
ATA 26 - FIRE PROTECTION.
26-001
26-00-00
26-002
26-00-00
Fire detection/
extinguishing. components
cockpit
Fire detection/
extinguishing. components
cockpit
Page 15 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
B1/B2
Task
Code
M
M
B1
B2
LOC
LOC
M
B1/B2
FOT
M
B1/B2
FOT
O
B1/B2
LOC
Item
ATA
Subject
Class
26-003
26-004
26-00-00
26-00-00
Engine fire detection loops
Engine fire detection loops
26-005
26-12-00
26-006
26-13-00
26-007
26-13-00
26-008
26-15-00
26-009
Engine fire and overheat
detection system
operational test
APU fire and overheat
detection system
operational test
O
B1/B2
LOC
26-15-00
APU fire detection and
extinguishing system
Avionic compartment
smoke detection system
components
Operational test of the
Avionics Compartment
Smoke-Detection through
the MCDU
M
B1/B2
FOT
26-010
26-16-00
Cargo compartment fire
extinguishing components
O
B1/B2
LOC
26-011
26-16-15
Removal/Installation of
Cargo Smoke Detector
M
B1/B2
RIA
M
B1/B2
FOT
M
B1
FOT
26-012
26-16-00
26-013
26-16-00
Operational check of
Cargo Compartment
Smoke Detection by PTT
Operational test of LowerDeck Cargo-Compartment
Smoke-Detection through
the MCDU
26-014
26-17-00
Lavatory fire extinguishing
components
O
B1
LOC
26-015
26-17-00
Operational check of
Lavatory Smoke Detection
System by MCDU
M
B1/B2
FOT
26-016
26-18-03
LDMCR Smoke detection
system
O
B1
MEL
26-017
26-21-41
Engine fire bottle weight
check
M
B1/B2
SGH
26-018
26-13-00
APU fire detection loop ‘A’
fault (TSM) Troubleshoot
M
B1/B2
TSE
Date
Trainee's
signature
Instructor's
signature
ATA 27 - FLIGHT CONTROLS
27-001
27-00-00
Flight control components
in cockpit
O
B1
LOC
27-002
27-00-00
Flight control components
in cockpit
M
B2
LOC
Page 16 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
B1/B2
Task
Code
O
B1
LOC
Operational test rudder
trim actuation
O
B2
FOT
27-26-00
Operational test of back-up
yaw damper (MCDU)
O
B2
FOT
27-44-00
Operational Test of the
Trimmable Horizontal
Stabiliser (THS) Actuator
M
B1
FOT
27-007
27-008
27-009
27-010
27-011
27-44-00
27-50-00
27-50-00
27-51-00
27-51-00
Operational Test of the
Trimmable Horizontal
Stabiliser (THS) Actuator
SFCC /WTB Reset
SFCC /WTB Reset
SFCC System test
SFCC System test
O
M
O
M
M
B2
B1
B2
B1
B2
FOT
FOT
FOT
FOT
FOT
27-012
27-54-00
O
B1
FOT
27-013
27-54-00
O
B2
FOT
27-014
27-015
27-016
27-017
27-64-00
27-64-01
27-93-34
27-93-34
O
M
M
O
B1
B1
B1
B2
LOC
MEL
RIA
RIA
27-018
27-96-00
M
B1
FOT
27-019
27-96-00
Operational test of Flap
and Slat System
Extending/ retracting
slat/flaps
Spoiler system
components
Spoiler
Remove/Instal FCPC
FCPC
Op Test of the Return to
Low Speed Config of the
Rudder and Pedals TravelLimitation Units
Op Test of the Return to
Low Speed Config of the
Rudder and Pedals TravelLimitation Units
O
B2
FOT
27-020
27-96-00
BITE Test of the EFCS
(SYSTEM TEST)
M
B1/B2
FOT
27-021
27-55-00
Flap position indicating,
Fault Isloation (TSM)
O
B1/B2
TSE
27-022
17-99-00
Electrical backup
O
B1/B2
SGH
Item
ATA
27-003
27-14-00
Ailerons and associated
systems
27-004
27-22-00
27-005
27-006
Subject
Class
Date
Trainee's
signature
Instructor's
signature
Page 17 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
REMARKS :
Page 18 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
B1/B2
Task
Code
O
B1
LOC
M
O
M
B2
B1
B1/B2
LOC
SGH
LOC
M
B1/B2
FOT
Class
Date
Trainee's
signature
Instructor's
signature
ATA 28 - FUEL
N.B. : For SERVICING tasks please refer to ATA 12
Fuel system components
in cockpit
28-001
28-00-00
28-002
28-003
28-004
28-00-00
28-28-00
28-21-00
28-005
28-25-00
Fuel system components
in cockpit
Pressure Defuel Procedure
All fuel boost pumps
Ground fuel transfer
procedure
28-006
28-25-00
Ground fuel transfer to the
trim tank
M
B1
FOT
28-007
28-21-51
Removal/Installation of
Fuel pump element
O
B1
TVC
28-008
28-26-53
M
B1
RIA
28-009
28-25-04
O
B1/B2
MEL
28-010
O
B1/B2
TSE
28-011
28-012
28-31-00
28-42-00810-887
28-00-00
O
M
B1/B2
B1/B2
TSE
SGH
28-013
28-42-22
O
B1/B2
RIA
Removal/Installation of
Fuel Inlet Valve Actuator
Refuel defuel system -Inlet
valve
Fuel Jettison fault
isolation(TSM)
Fuel Quantity incorrect,
temporarliy (TSM)
CDCCL procedures
Fuel Quantity indicator,
remove/refit.
REMARKS :
Page 19 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
B1/B2
Task
Code
M
M
M
B1/B2
B1
B2
LOC
SGH
SGH
M
B1/B2
LOC
Class
Date
Trainee's
signature
Instructor's
signature
ATA 29 - HYDRAULIC POWER
N.B. : For SERVICING tasks please refer to ATA 12
29-001
29-002
29-003
29-00-00
29-00-00
29-00-00
29-004
29-00-00
Hydraulic power panels
cockpit
Maintenance panel
Maintenance panel
Engine Hydraulic
Components
29-005
29-00-00
Pressurise the green (blue
,yellow)hydraulic system
with electric pump
M
B1
SGH
29-006
29-11-00
Green system ground
service panel
M
B1/B2
LOC
29-007
29-12-00
Blue system ground
service panel
M
B1/B2
LOC
29-008
29-13-00
Yellow system ground
service panel
M
B1/B2
LOC
29-009
29-24-00
O
B1
FOT
29-010
29-30-02
Operational test of the RAT
Extension and retraction
Indication reservoir
quantity on ECAM Hyd
page
O
B1/B2
MEL
29-011
29-31-11
Hyd tank Air Pressure
switch, remove/install
M
B1/B2
RIA
29-012
29-22-51
Blue system electric pump,
remove/install
O
B1
RIA
29-013
29-11-00810-813
Green hydraulic quantity
transmitter, (TSM)
O
B1/B2
TSE
29-014
29-22-00810-802
Overheat of Blue electric
pump, (TSM)
O
B1
TSE
REMARKS :
Page 20 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
ATA 30 - ICE AND RAIN PROTECTION
30-001
30-00-00
Anti ice system
components in cockpit
O
B1
LOC
30-002
30-00-00
Anti ice system
components in cockpit
M
B2
LOC
30-003
30-11-00
Wing anti ice components
on wing
M
B1/B2
LOC
30-004
30-005
30-006
30-007
30-008
30-009
30-010
30-11-01
30-31-00
30-31-00
30-40-00
30-40-00
30-42-34
30-21-01
30-11-00710-801
30-11-00790-801
30-81-00830-801
Wing ice protection anti ice
Control valve
Probe heat components
Probe heat components
Window heat components
Window heat components
Remove/Install WHC
Engine anti ice valve
Operational test of wing
anti-ice system
Leak check, anti-ice ducts
and connections
Loss of ice detectors
(TSM) fault isolation
M
O
M
O
M
M
M
B1
B1
B2
B1
B2
B1/B2
B1/B2
MEL
LOC
LOC
LOC
LOC
RIA
MEL
M
B1/B2
FOT
O
B1
SGH
O
B1/B2
TSE
30-010
30-011
30-012
REMARKS :
Page 21 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
ATA 31 - INDICATING/RECORDING
31-00-00
Indicating/recording
System components and
indication in cockpit
O
B1
LOC
31-002
31-003
31-004
31-005
31-006
31-00-00
31-21-00
31-36-00
31-36-52
31-50-00
Indicating/recording
System components and
indication in cockpit
Procedure to Set the Clock
ACMS general operation
DAR Servicing
FWS System test
M
M
M
M
M
B2
B1/B2
B1/B2
B2
B1/B2
LOC
SGH
SGH
SGH
FOT
31-007
31-008
31-009
31-50-00
31-60-00
31-60-00
O
M
M
B2
B1/B2
B2
FOT
FOT
SGH
31-010
31-011
31-63-22
31-63-22
M
O
B1/B2
B2
RIA
SGH
31-012
31-68-01
31-56-00810-804
O
B1/B2
MEL
M
B1/B2
TSE
31-001
31-013
Operational Test of the
ECAM Control Panel
DMC system test
EIS start/ stop procedure
Removal/Installation of
Display Unit
DU Cleaning Procedure
ECAM DMC switching
selector
Loss of ECAM control
panel (TSM)
REMARKS :
Page 22 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
B1/B2
Task
Code
O
B1
LOC
M
B2
LOC
O
B1/B2
LOC
O
B1/B2
LOC
M
B1
SGH
O
B1/B2
SGH
M
B1/B2
RIA
O
B1
LOC
M
B1
FOT
M
B1/B2
FOT
M
O
B1
B1
FOT
MEL
O
O
B1/B2
B1:B2
TSE
MEL
Class
Date
Trainee's
signature
Instructor's
signature
ATA 32 - LANDING GEAR
N.B : For SERVICING tasks please refer to ATA 12
32-001
32-00-00
32-002
32-00-00
32-003
32-10-00
32-004
32-20-00
32-005
32-00-00
32-006
32-40-00
32-007
32-42-57
32-008
32-42-00
32-009
32-46-00
32-010
32-69-00
32-011
32-012
32-31-00
32-42-02
32-013
32-014
32-61-00810-803
32-31-01
System components and
control in the cockpit
System components and
control in the cockpit
MLG and doors
components
NLG and doors
components
Gear doors ground
opening/ closing
Wheels and brakes
components
Remove/Install Wheel
Speed Tachometer
Brakes system
components (normal, alt,
parking)
BITE Test of the BSCU
and its Related Systems
Simulation of flight ,when
the aircraft is on the
ground
Normal Extension and
Retraction System test
Green brake system
Nose landing gear shows
false uplock
condition(TSM)
LGCIU inop
REMARKS :
Page 23 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
O
B1/B2
TVC
M
M
M
B2
B1
B2
RIA
FOT
FOT
O
B1
LOC
M
B2
LOC
Date
Trainee's
signature
Instructor's
signature
ATA 33 - LIGHTS
33-001
33-10-00
33-002
33-003
33-004
33-10-00
33-14-00
33-14-00
33-005
33-14-00
33-006
33-14-00
Cockpit light operation
Bulb/ LED and push button
body
Operational test of Lights
Annunciator lights test
Annunciator lights spare
bulbs
Annunciator lights spare
bulbs
33-007
33-20-00
Cabin general illumination
operation
O
B1/B2
TVC
33-008
33-21-11
Removal/Instal of Ballast
Unit with Lamp-holder
M
B1/B2
RIA
33-009
33-24-00
Operational test of lavatory
lighting
O
B1/B2
FOT
33-010
33-25-00
33-011
M
B1
FOT
33-25-00
Passenger Reading Lights
System test
Bite test of Passenger
reading lights and cabin
attendant lights
M
B1/B2
FOT
33-012
33-25-00
Test of Passenger Reading
lights and Cabin Attendant
Lights
M
B2
FOT
33-013
33-30-00
O
B1/B2
TVC
33-014
33-50-00
M
B1/B2
LOC
33-015
33-51-00
M
B1/B2
FOT
33-016
33-51-00
M
B1/B2
FOT
33-017
33-51-00
EMER LIGHT SYS
operational test from FAP
Localised system test of
the Emergency Power
Supply Unit
M
B1/B2
FOT
33-018
33-51-00
EPSU load-programming
procedure (teach in)
O
B1
SGH
M
B2
SGH
M
B1/B2
RIA
M
B1/B2
TSE
33-019
33-51-00
33-020
33-51-38
33-42-00810-801
33-021
Cargo and services lights
operation
Emergency lights
components
Operational check of the
Emergency Light via
MCDU
EPSU load-programming
procedure (teach in)
Removal/Installation of
EPSU battery
Left landing light inop
(TSM) Fault isolation
Page 24 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
REMARKS :
Page 25 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
B1/B2
Task
Code
O
B1
LOC
M
M
M
O
B2
B1/B2
B1/B2
B1/B2
LOC
SGH
SGH
MEL
O
B1/B2
TSE
O
B2
SGH
M
B2
TVC
M
M
O
M
B2
B1
B2
B2
TVC
TVC
RIA
TVC
M
O
B2
B2
FOT
FOT
O
O
B2
B2
LOC
FOT
O
M
B2
B1/B2
FOT
FOT
O
B1/B2
FOT
O
M
O
O
M
M
O
M
B2
B1
B2
B1/B2
B2
B2
B1
B2
FOT
FOT
FOT
FOT
FOT
MEL
FOT
FOT
O
B1
FOT
Class
Date
Trainee's
signature
Instructor's
signature
ATA 34- NAVIGATION
34-001
34-00-00
34-002
34-003
34-004
34-005
34-00-00
34-10-00
34-10-00
34-10-01
Navigation system
components
Navigation system
components
ADIRS start procedure
IRS align procedure
ADIRS
34-006
34-11-00
34-007
34-11-00
34-008
34-11-00
34-009
34-010
34-011
34-012
34-11-00
34-12-34
34-12-34
34-12-34
34-013
34-014
34-13-00
34-13-00
34-015
34-016
34-13-00
34-13-00
Detection of a discrepancy
of the left and right static
pressure on ADIRU 1
Draining and Flushing of
the Standby Static and
Standby Total Pressure
Lines
ATT/ HDG switching
operation
Air data switching
operation
ADIRU
ADIRU
ADIRS Removal Criteria
ALT/CAS dynamic slew
test
AOA SENSOR TEST
VMO/MMO Selector
Switch
ADR interface test
34-017
34-018
34-22-25
34-36-00
Bite test of the ISIS
indicator (if installed)
MMR System test
34-019
34-36-00
34-020
34-021
34-022
34-023
34-024
34-025
34-026
34-027
34-36-00
34-41-00
34-41-00
34-42-00
34-42-00
34-42-01
34-43-00
34-43-00
34-028
34-48-00
Operationnel Test of GPS
Function
Operational Test of ILS
Function
Weather radar system test
Weather radar system test
R.A system test
Radio altimeter ramp test
Radio altimeter
TCAS system test
TCAS system test
GPWC or EGPWC system
test
Page 26 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
B1/B2
Task
Code
M
B2
FOT
O
B2
TVC
O
M
M
O
B2
B2
B2
B1/B2
FOT
FOT
FOT
FOT
O
B2
FOT
O
B1
FOT
M
B2
FOT
M
B2
TSE
Item
ATA
Subject
Class
34-029
34-48-00
GPWC or EGPWC system
test
34-030
34-48-00
34-031
34-032
34-033
34-034
34-48-00
34-51-00
34-52-00
34-53-00
34-035
34-53-00
34-036
34-55-00
34-037
34-55-00
34-038
34-41-00810-803
Uploading of the Enhanced
GPWC Data-Base
GPWS ground vocabulary
test
DME System test
BITE test of the ATC
ADF system test
Operational Test of the
ADF
VOR/MARKER /DME
System test
VOR/MARKER System
test
Failure of weather radar
antenna(TSM) fault
isolation
Date
Trainee's
signature
Instructor's
signature
REMARKS :
Page 27 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
ATA 35 OXYGEN
35-001
35-00-00
Flight compartment oxygen
system components
O
B1
LOC
35-002
35-003
35-00-00
35-12-00
Flight compartment oxygen
system components
Crew oxygen system
M
O
B2
B1/B2
LOC
LOC
35-004
35-21-00
Cabin oxygen system
components
O
B1/B2
LOC
35-005
35-21-42
O
B1
RIA
35-006
35-22-00
O
B1
FOT
35-007
35-31-52
M
B1
TVC
35-008
35-32-00
Remove/Install Generator
Emergency Oxygen
Check Oxygen Container
Opening and Vent
Function of Bleed/Vent
Valve
Visual check of the Tamper
Seal/Serviceability
Indicator on the Protective
Breathing Eqpt
Portable oxygen
equipment
O
B1
LOC
35-009
35-13-01
Crew oxygen -control and
indicating
O
B1
MEL
35-010
35-00-00860-801
Precautions when working
with Oxygen
M
B1/B2
SGH
REMARKS :
Page 28 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
ATA 36 - PNEUMATIC
O
B1
LOC
36-00-00
System components in
cockpit
System components in
cockpit
M
B2
LOC
36-003
36-11-00
Engine bleed system
components
M
B1
LOC
36-004
36-005
36-006
36-11-00
36-11-00
36-11-06
Engine bleed system
components
BITE Test of the BMC
IP Check valve
O
M
O
B1
B1/B2
B1
LOC
FOT
MEL
36-007
36-11-15
Remove/Install Bleed
Pressure Transducer 9HA
M
B1/B2
RIA
O
O
B1/B2
B1/B2
FOT
TSE
M
B1/B2
SGH
36-001
36-00-00
36-002
36-008
36-009
36-12-00
36-22-00
36-010
36-21-00
Operational Test of the
APU Bleed-Air Supply and
Crossbleed System
APU leak detection
Pressure and temperature
monitoring
REMARKS :
Page 29 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
ATA 38 - WATER:WASTE SYSTEM
N.B : For SERVICING tasks please refer to ATA 12
38-001
38-00-00
CIDS water/ waste page
on FAP
O
B2
LOC
38-002
38-10-00
Potable/waste water
system components
O
B1
LOC
38-003
38-12-00
Potable water heater
functional test
O
B1/B2
FOT
38-004
38-005
38-12-00
38-14-00
M
O
B1
B1/B2
SGH
LOC
38-006
38-31-00
Isolation Toilet and Water
Heater with Shut of Valve
Drain water system
Operational test of the
VSC
M
B1/B2
FOT
38-007
38-31-00
Functional test of the Toilet
Assemblies
M
B1
FOT
38-008
38-009
38-31-41
38-32-00
O
O
B1
B1/B2
SGH
LOC
38-010
38-32-41
O
B1
RIA
38-011
38-41-00
O
B1/B2
LOC
Potable servicing for
normal and ice conditions
Potable water drainage
Removal/Instalation of
Drain Valve
Air supply system
components
REMARKS :
Page 30 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
ATA 45 - ONBOARD MAINTENANCE SYSTEMS
45-001
45-002
45-003
45-004
45-005
45-00-00
45-10-00
45-10-00
45-10-00
45-10-00
CMS Components
CMS Components
CMS general operation
CMS manual switching
CMC System test
O
M
M
M
M
B1
B2
B1/B2
B2
B1/B2
LOC
LOC
TVC
TVC
FOT
45-006
45-10-00
Operational Test of the
Automatic Switching
O
B2
FOT
45-20-00
45-41-22
Uploading procedure with
MDDU including FMGEC
Printer servicing
O
M
B1
B1/B2
SGH
SGH
M
M
B1
B2
FOT
FOT
M
B2
FOT
O
B2
FOT
M
B2
TVC
45-007
45-008
ATA 46 - INFORMATION SYSTEMS
46-001
46-002
46-21-00
46-21-00
46-003
46-21-00
46-004
46-21-00
46-005
46-21-00
46-006
46-21-00
46-007
Bite Test ATIMS
Bite Test ATSU by CMS
VHF 3 Link Test of the
ATSU
SATCOM Link Test of the
ATSU
O
B2
TVC
46-21-00
Initialisation Procedure of
the ATSU Router
Uploading of the ATSU
Software with the
Multipurpose Disk Drive
Unit (MDDU)
Procedure to Get Access
to the DSP USERDEFINED Pages
M
B2
TVC
46-008
46-21-21
DCDU, removal/installation
O
B2
RIA
46-009
46-21-00
Failure of ATSU(TSM)
O
B2
TSE
REMARKS :
Page 31 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
ATA 49 - APU
N.B : For SERVICING tasks please refer to ATA 12
49-001
49-00-00
49-002
49-003
49-00-00
49-16-01
49-41-00810-805
49-00-00710-801
49-004
49-005
APU system components
in cockpit
O
B1/B2
LOC
APU start, operation and
shut down procedures
Air intake flap
O
O
B1
B1
FOT
MEL
APU ignitor fault(TSM)
M
B1/B2
TSE
Funtional test
M
B&/B2
SGH
REMARKS :
Page 32 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
M
B1/B2
SGH
M
B1
SGH
M
B1
FOT
M
B1/B2
LOC
M
B1/B2
FOT
O
B1/B2
MEL
Date
Trainee's
signature
Instructor's
signature
ATA 52 - DOORS
52-001
52-10-00
52-002
52-30-00
52-003
52-30-00
52-004
52-30-00
52-005
52-71-00
52-006
52-71-01
Passengers doors
operation
FWD/AFT cargo door
opening and closing with
elec.hyd.pump
FWD/AFT cargo door
opening and closing with
hand pump
Cargo door locking
mechanism
BITE Test of the Proximity
Switch Control Unit
Door and escape slide
control system -Proximity
switches
ATA 53 - FUSELAGE
53-001
53-10-00
Opening / Closing of the
Radome
O
B1/B2
SGH
53-002
53-11-00210-801
General inspection of NLG
stucture
O
B1
LOC
M
B1
LOC
ATA 54 - NACELLE / PYLONS
54-001
54-50-00
Pylon Pressure relief
Doors
ATA 55- STABILIZERS
55-001
55-41-00
Rudder main structure
O
B1
LOC
ATA 56 - WINDOWS
56-001
56-10-00
Windshield Panels
M
B1
LOC
56-002
56-12-00
Cockpit sliding window
operating mechanism
M
B1
SGH
56-003
30-42-00810-817
Loss of windshield heater
monitoring(TSM)
M
B1/B2
TSE
Pressure relief Panels
O
B1
LOC
ATA 57 - WINGS
57-001
57-00-00
Page 33 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
REMARKS :
Page 34 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
ATA 71 - POWER PLANT (RR Trent 772B-60)
71-001
71-13-00
Opening /Closing of the
Fan Cowls doors
M
B1/B2
SGH
71-002
78-36-00
Opening /Closing of the
Thrust Reverser Doors
M
B1
SGH
71-003
71-10-00
Visual Inspection of the Air
Inlet Cowl
O
B1
TVC
71-004
71-005
71-006
71-007
71-00-00
71-00-00
71-00-00
71-71-00
Engine Controls and
Indications in the Cockpit
DRY MOTORING CHECK
WET MOTORING CHECK
Engine drain module
M
M
O
O
B1/B2
B1
B1
B1
LOC
FOT
TVC
LOC
M
B1
TVC
O
B1
TVC
M
B1/B2
LOC
ATA 72 – ENGINE (RR Trent 772B-60)
72-001
72-21-00
72-002
72-00-00
Visual inspection of Fan
Blades and Spinner
Visual inspection of visible
area of engine inlet/fan
outlet
72-003
72-60-00
Accessory drive gearbox
REMARKS :
Page 35 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
ATA 73- ENGINE FUEL AND CONTROL (RR Trent 772B-60)
Engine fuel control
components
ECU components
FADEC System Test
73-001
73-002
73-003
73-00-00
73-20-00
73-21-00
M
M
M
B1/B2
B2
B1/B2
LOC
LOC
FOT
73-004
73-21-00
73-005
73-006
73-21-00
73-21-00
73-008
73-21-00
MCDU FADEC non
motoring test
MCDU FADEC motoring
test
FADEC Sensors
FADEC Specific data
Menu
M
B1
FOT
M
M
B1
B2
FOT
LOC
M
B2
TVC
73-009
73-21-00
Reading of the Scheduled
Maint Report
M
B2
TVC
Failure or the HP fuel shutoff valve in OPEN position
on engine 1
73-010
73-21-51
O
B1/B2
TSE
73-011
73-012
73-013
73-25-00
73-25-02
73-25-34
M
O
M
B1
B2
B1
MEL
MEL
FOT
73-014
73-015
73-25-34
73-25-34
M
M
B1
B2
FOT
FOT
73-016
73-017
73-25-34
73-30-00
O
M
B2
B1
TVC
MEL
73-018
73-21-13
O
B1/B2
RIA
Engine short time limited
dispatch items
EIVMU
MCDU EIVMU system test
EIVMU specific data read
out
Bite Test of the EIVMU
Read the MAX FLIGHT
VIBRATION Data
Fuel Filter clog indication
Fuel temperature
thermocouple remve/install
REMARKS :
Page 36 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
M
O
M
M
B1/B2
B1
B1
B1/B2
FOT
SGH
MEL
LOC
M
B1/B2
LOC
O
B1
TVC
Date
Trainee's
signature
Instructor's
signature
ATA 74 - IGNITION (RR Trent 772B-60)
74-001
74-002
74-003
74-004
74-00-00
74-21-51
74-31-00
74-11-34
Ignition system
components
Igniter Plug
Ignition Indicating System
Ignition units
ATA 75- AIR (RR Trent 772B-60)
75-001
75-00-00
75-002
75-31-00
Air system components
Adjustement/Test of the
Variable Bleed Valve
System
75-003
75-33-00
Variable Stator Vane
Actuator/Sensor
O
B1
RIA
75-004
75-41-00810-833
High nacelle temp trend on
engine(TSM)
O
B1
TSE
ATA76 – ENGINES CONTROLS (RR Trent 772B-60)
76-001
76-10-00
Engine controls in the
cockpit
M
B1/B2
LOC
76-002
76-11-00
Adjustement and Rigging
of the mechanical linkage
O
B1
SGH
76-003
76-11-19
Throttle Control Unit and
Mechanical Box
M
B1
FOT
76-004
76-11-00810-864
Engine throttle levers too
tight or too loose(TSM)
O
B1
TSE
ATA 77 - ENGINE INDICATING (RR Trent 772B-60)
77-001
77-00-00
Engine indicating systems/
ECAM, panel
M
B1/B2
LOC
77-002
77-10-00
Engine indicating systems
components on eng
M
B1/B2
LOC
REMARKS :
Page 37 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
O
B1/B2
LOC
M
B1
MEL
M
B1
FOT
M
B1
SGH
O
B1
TVC
Date
Trainee's
signature
Instructor's
signature
ATA 78 - Exhaust (RR Trent 772B-60)
Thrust reverser system
components
78-001
78-00-00
78-002
78-30-00
78-003
78-31-00
78-004
78-32-41
Thrust Reverser
Deactivate/Reavtivate
Operational Test of the
Thrust Reverser System
Via MCDU
Manual
Deployment/stowing of the
Pivoting Doors
78-005
78-32-44
Adjustement of the Thrust
Reverser Door Latches
ATA 79 – OIL (RR Trent 772B-60)
79-001
79-00-00
Visual Inspection of the Oil
System components
M
B1/B2
LOC
79-002
79-003
79-004
79-00-00
79-22-45
79-31-00
Check Master Magnetic
Chip Detector for particles
Check Scavenge Screens
Oil Quantity Indication
O
O
M
B1
B1
B1
SGH
RIA
LOC
O
B1
LOC
M
B1
SGH
O
B1
TVC
M
B1
MEL
O
B1
TSE
ATA 80– STARTING (RR Trent 772B-60)
80-001
80-00-00
80-002
80-11-00
80-003
80-11-10
80-004
80-11-01
80-005
80-11-00810-841
Starting system
components
Manual operation of the
Starter Shut-Off Valve
Check Starter Magnetic
Chip Detector and Oil
Level
Manual Start procedure
Starter control valve does
not move to the correct
position(TSM)
Page 38 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee's
signature
Instructor's
signature
REMARKS :
Page 39 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
ATA 71 - POWER PLANT (GE CF6)
71-001
71-13-41
Opening /Closing of the
Fan Cowls doors
M
B1/B2
SGH
71-002
78-36-00
Opening /Closing of the
Thrust Reverser Doors
M
B1
SGH
71-003
71-11-00
Visual Inspection of the Air
Inlet Cowl
O
B1
TVC
71-004
71-005
71-006
71-007
71-00-00
71-00-00
71-00-00
71-70-00
Engine Controls and
Indications in the Cockpit
DRY MOTORING CHECK
WET MOTORING CHECK
Engine drain module
M
M
O
O
B1/B2
B1
B1
B1
LOC
FOT
TVC
LOC
M
B1
TVC
O
B1
TVC
M
B1/B2
LOC
ATA 72 – ENGINE (GE CF6)
72-001
72-20-00
72-002
72-00-00
Visual inspection of Fan
Blades and Spinner
Visual inspection of visible
area of engine inlet/fan
outlet
72-003
72-60-00
Accessory drive gearbox
REMARKS :
DERICHEBOURG Atis aéronautique,
Parc Algorithmes, Immeuble Thalès – 17, Avenue Didier Daurat 31700 Blagnac
Tél. 05 34 60 61 40 -  05 34 60 61 50
DOC.FOR.49 ed1
Page 40 sur 51
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee’s
signature
Instructor’s
signature
73-00-00 - ENGINE FUEL AND CONTROL (GE CF6)
Engine fuel control
components
ECU components
FADEC System Test
73-001
73-002
73-003
73-00-00
73-20-00
73-21-00
M
M
M
B1/B2
B2
B1/B2
LOC
LOC
FOT
73-004
73-21-00
73-005
73-006
73-21-00
73-21-00
73-008
73-21-00
MCDU FADEC non
motoring test
MCDU FADEC motoring
test
FADEC Sensors
FADEC Specific data
Menu
M
B1
FOT
M
M
B1
B2
FOT
LOC
M
B2
TVC
73-009
73-21-00
Reading of the Scheduled
Maint Report
M
B2
TVC
Failure or the HP fuel shutoff valve in OPEN position
on engine 1
73-010
73-21-51
O
B2
TSE
73-011
73-012
73-013
73-25-00
73-25-02
73-25-34
M
O
M
B1
B2
B1
MEL
MEL
FOT
73-014
73-015
73-25-34
73-25-34
M
M
B1
B2
FOT
FOT
73-016
73-017
73-25-34
73-30-00
O
M
B2
B1
TVC
MEL
73-018
73-11-11
O
B1/B2
RIA
Engine short time limited
dispatch items
EIVMU
MCDU EIVMU system test
EIVMU specific data read
out
Bite Test of the EIVMU
Read the MAX FLIGHT
VIBRATION Data
Fuel Filter clog indication
Fuel temperature
thermocoule remove/install
REMARKS :
Page 41 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
M
O
M
M
B1
B1
B1
B1/B2
FOT
SGH
MEL
LOC
M
B1
LOC
O
B1
TVC
Date
Trainee’s
signature
Instructor’s
signature
74-00-00 - IGNITION (GE CF6)
74-001
74-002
74-003
74-004
74-00-00
74-21-51
74-31-00
74-11-51
Ignition system components
Igniter Plug
Ignition Indicating System
Ignition Units
75-00-00 - AIR (GE CF6)
75-001
75-002
75-00-00 Air system components
Adjustement/Test of the
Variable Bleed Valve
75-31-00 System
75-003
Variable Stator Vane
75-32-00 Actuator/Sensor
O
B1
TVC
75-004
75-41-00- High nacelle temp trend on
810-819 engine (TSM)
O
B1
TSE
76-00-00 - ENGINES CONTROLS (GE CF6)
76-001
Engine controls in the
76-10-00 cockpit
M
B1/B2
LOC
76-002
Adjustement and Rigging of
76-11-00 the mechanical linkage
O
B1
SGH
76-003
Throttle Control Unit and
76-11-19 Mechanical Box
M
B1
FOT
76-004
76-11-00- Engine throttle levers too
810-866 tight or too loose(TSM)
O
B1
TSE
77-00-00 - ENGINE INDICATING (GE CF6)
77-001
Engine indicating systems/
77-00-00 ECAM, panel
M
B1/B2
LOC
77-002
Engine indicating systems
77-10-00 components on eng
M
B1/B2
LOC
REMARKS :
Page 42 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
B1/B2
Task
Code
O
B1
LOC
M
B1
MEL
M
B1
FOT
M
B1
SGH
O
B1
TVC
Class
Date
Trainee’s
signature
Instructor’s
signature
78-00-00 - EXHAUST(GE CF6)
Thrust reverser system
components
78-001
78-00-00
78-002
78-30-00
78-003
78-31-00
78-004
78-32-65
Thrust Reverser
Deactivate/Reavtivate
Operational Test of the
Thrust Reverser System
Via MCDU
Manual
Deployment/stowing of the
Pivoting Doors
78-005
78-32-49
Adjustement of the Thrust
Reverser Door Latches
79-00-00 - OIL(GE CF6)
79-001
79-00-00
Visual Inspection of the Oil
System components
O
B1
TVC
79-002
79-003
79-004
79-21-11
79-21-41
79-31-00
Check Master Magnetic
Chip Detector for particles
Check Scavenge Screens
Oil Quantity Indication
O
O
M
B1
B1
B1
TVC
TVC
LOC
O
B1
LOC
M
B1
SGH
O
B1
TVC
M
B1
MEL
O
B1
TSE
80-00-00 - STARTING(GE CF6)
80-001
80-00-00
80-002
80-11-20
80-003
80-11-41
80-004
80-11-01
80-005
80-11-00810-813
Starting system
components
Manual operation of the
Starter Shut-Off Valve
Check Starter Magnetic
Chip Detector and Oil
Level
Manual Start procedure
Starter control valve does
not move to the correct
position(TSM)
Page 43 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
REMARKS :
Page 44 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee’s
signature
Instructor’s
signature
71-00-00 - POWER PLANT (PW 4000)
71-001
71-13-00
Opening /Closing of the
Fan Cowls doors
M
B1
SGH
71-002
78-36-00
Opening /Closing of the
Thrust Reverser Doors
M
B1
SGH
71-003
71-11-00
Visual Inspection of the Air
Inlet Cowl
O
B1
TVC
71-004
71-005
71-006
71-007
71-00-00
71-00-00
71-00-00
71-00-00
Engine Controls and
Indications in the Cockpit
DRY MOTORING CHECK
WET MOTORING CHECK
Engine drain module
M
M
O
O
B1
B1
B1
B1
LOC
FOT
TVC
LOC
M
B1
TVC
O
B1
TVC
M
B1/B2
LOC
72-00-00 - ENGINE(PW 4000)
72-001
72-33-00
72-002
72-00-00
Visual inspection of Fan
Blades and Spinner
Visual inspection of visible
area of engine inlet/fan
outlet
72-003
72-60-00
Accessory drive gearbox
REMARKS :
Page 45 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
Date
Trainee’s
signature
Instructor’s
signature
73-00-00 - ENGINE FUEL AND CONTROL (PW 4000)
Engine fuel control
components
ECU components
FADEC System Test
73-001
73-002
73-003
73-00-00
73-20-00
73-21-00
M
M
M
B1/B2
B2
B1/B2
LOC
LOC
FOT
73-004
73-21-00
73-005
73-006
73-21-00
73-21-00
73-008
73-21-00
MCDU FADEC non
motoring test
MCDU FADEC motoring
test
FADEC Sensors
FADEC Specific data
Menu
M
B1
FOT
M
M
B1
B2
FOT
LOC
M
B2
TVC
73-009
73-21-00
Reading of the Scheduled
Maint Report
M
B2
TVC
Failure or the HP fuel shutoff valve in OPEN position
on engine 1
73-010
73-21-51
O
B2
TSE
73-011
73-012
73-013
73-25-00
73-25-02
73-25-34
M
O
M
B1
B2
B1
MEL
MEL
FOT
73-014
73-015
73-25-34
73-25-34
M
M
B1
B2
FOT
FOT
73-016
73-017
73-25-34
73-30-00
O
M
B2
B1
TVC
MEL
73-018
73-32-11
O
B1/B2
RIA
Engine short time limited
dispatch items
EIVMU
MCDU EIVMU system test
EIVMU specific data read
out
Bite Test of the EIVMU
Read the MAX FLIGHT
VIBRATION Data
Fuel Filter clog indication
Fuel temperature
thermocouple remve/install
REMARKS :
Page 46 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
Class
B1/B2
Task
Code
M
O
M
M
B1
B1
B1
B1/B2
FOT
SGH
MEL
LOC
M
B1
LOC
Date
Trainee’s
signature
Instructor’s
signature
74-00-00 - IGNITION (PW 4000)
74-001
74-002
74-003
74-004
74-00-00
74-21-00
74-31-00
74-11-00
Ignition system
components
Igniter Plug
Ignition Indicating System
Ignition units
75-00-00 - AIR
75-001
75-00-00
75-002
75-31-00
Air system components
Adjustement/Test of the
Variable Bleed Valve
System
O
B1
TVC
75-003
75-31-12
Variable Stator Vane
Actuator/Sensor
O
B1
TVC
75-004
75-41-00810-825
High nacelle temp trend on
engine(TSM)
O
B1
TSE
76-00-00 - ENGINES CONTROLS (PW 4000)
76-001
76-10-00
Engine controls in the
cockpit
M
B1/B2
LOC
76-002
76-11-00
Adjustement and Rigging
of the mechanical linkage
O
B1
SGH
76-003
76-11-19
Throttle Control Unit and
Mechanical Box
M
B1
FOT
76-004
76-11-00810-867
Engine throttle levers too
tight or too loose(TSM)
O
B1
TSE
77-00-00 - ENGINE INDICATING (PW 4000)
77-001
77-00-00
Engine indicating systems/
ECAM, panel
M
B1/B2
LOC
77-002
77-10-00
Engine indicating systems
components on eng
M
B1/B2
LOC
REMARKS :
Page 47 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
Item
ATA
Subject
B1/B2
Task
Code
O
B1
LOC
M
B1
MEL
M
B1
FOT
M
B1
SGH
O
B1
TVC
Class
Date
Trainee’s
signature
Instructor’s
signature
78-00-00 - EXHAUST(PW 4000)
Thrust reverser system
components
78-001
78-00-00
78-002
78-30-00
78-003
78-31-00
78-004
78-32-00
Thrust Reverser
Deactivate/Reavtivate
Operational Test of the
Thrust Reverser System
Via MCDU
Manual
Deployment/stowing of the
Pivoting Doors
78-32-32
Adjustement of the Thrust
Reverser Door Latches
78-005
79-00-00 - OIL(PW 4000)
79-001
79-00-00
Visual Inspection of the Oil
System components
O
B1
TVC
79-002
79-003
79-004
79-21-11
79-22-00
79-31-00
Check Master Magnetic
Chip Detector for particles
Check Scavenge Screens
Oil Quantity Indication
O
O
M
B1
B1
B1
TVC
TVC
LOC
O
B1
LOC
M
B1
SGH
O
B1
TVC
M
B1
MEL
O
B1
TSE
80-00-00 - STARTING(PW 4000)
80-001
80-00-00
80-002
80-11-20
80-003
80-11-18
80-004
80-11-01
80-005
80-11-00810-823
Starting system
components
Manual operation of the
Starter Shut-Off Valve
Check Starter Magnetic
Chip Detector and Oil
Level
Manual Start procedure
Starter control valve does
not move to the correct
position(TSM)
Page 48 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
REMARKS :
Page 49 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
ADDITIONAL PRACTICAL EXPERIENCE
ATA
reference
Work experience
Date
Trainee’s
signature
Assessor’s
signature
Page 50 sur 51
DOC.FOR.49 ed1
Airbus A330 RR/GE/PW
MAINTENANCE PRACTICE TRAINING MANUAL
B1 or B1/B2
ADDITIONAL PRACTICAL EXPERIENCE
ATA
reference
Work experience
Date
Trainee’s
signature
Assessor’s
signature
Page 51 sur 51
DOC.FOR.49 ed1