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Investigation showed that the upper support of the NLG shock absorber was damaged
and the anti- rotation lugs were ruptured. This led the nose wheels to lose their
centered position reference normally ensured by the shock-absorber cams. The
BSCU had logged a steering system fault, because hydraulic power was not available
at the time of steering system checks, therefore the BSCU was not able to proceed
with the re-centering of the wheels.
To prevent reoccurrence of landings with the NLG turned 90 degrees, this AD
introduces operational procedures and maintenance actions.
James Coyne
Delegate of the Civil Aviation Safety Authority
23 November 2005
Maintenance Training
Organisation Exposition MTOE
Chapter 4.2.2
Page 7 of 46
Issue 2, Rev. 4 03.04.2006
APPROVED PART-147 AIRCRAFT TYPE MAINTENANCE TRAINING COURSE
Course Title Cat B1 Aircraft Type Maintenance Training Course
Airbus A318/A319/A320/A321 (CFM 56)
Course Code
Course Duration Total Duration:
Knowledge Training:
Practical Training
35 days
13 days
Target Population 􀁸 Students intending to acquire a variation of their Part-66 Cat
B1 Aircraft Maintenance Licence to include the Airbus
A318/A319/A320/A321 (CFM 56) aircraft type
Prerequisite 􀁸 Completion of the Part-66 Cat B1 basic training.
Exceptions may be granted by the Director of Technical
Training if the student’s prequalification is considered
sufficient to follow the type training course.
Objective 􀁸 provide approved Part-147 Cat B1 type training fulfilling the
applicable Part-66 requirements
􀁸 conduct Part-66 examination and practical assessment
Training Means
Knowledge
Training
(acc. ATA 104)
Lecture x Linear Video x
Manuals x Web Based Training
Instructor Led CBT x Student Paced CBT x
Computer Based
Simulations
x Simulators
Content See table next side
Examination/
Assessment
Knowledge examinations will be held at the conclusion of each
ATA chapter block, in general on a weekly basis, or as an
alternative at the end of the course.
Practical assessments will be held in the course of practical
training as defined by the practical training task list.
Maintenance Training
Organisation Exposition MTOE
Chapter 4.2.2
Page 8 of 46
Issue 2, Rev. 4 03.04.2006
APPROVED PART-147 AIRCRAFT TYPE MAINTENANCE TRAINING COURSE
Course Title Cat B1 Aircraft Type Maintenance Training Course
Airbus A318/A319/A320/A321 (CFM 56)
Training Duration
Module/ [hrs]
Sub-Module
Knowledge Practical
Intro 1 1
ATA 5..12 Aircraft General/ Publication 6 32
ATA 20 Standard Practices 1 2
ATA 21 Air-conditioning / Pressurization 11 6
ATA 22 Auto flight 3 1
ATA 23 Communication 4 2
ATA 24 Electrical Power 12 4
ATA 25 Equipment / Furnishing 4 5
ATA 26 Fire Protection 6 3
ATA 27 Flight Controls 23 6
ATA 28 Fuel 12 3
ATA 29 Hydraulic Power 10 3
ATA 30 Ice & Rain Protection 5 3
ATA 31 Instruments / Recording System 9 2
ATA 32 Landing Gear 12 6
ATA 33 Lights 6 3
ATA 34 Navigation 6 1,5
ATA 35 Oxygen 2 2
ATA 36 Pneumatics 6 1,5
ATA 38 Water / Waste 4 1,5
ATA 45 On Board Maintenance System - -
ATA 46 Information Systems 1 -
ATA 49 APU 6 3
ATA 51,53-
55, 57
Aircraft Structure 3 2
ATA 52 Doors 2 1,5
ATA 56 Windows 2
ATA 71..80 Power Plant 19 9
Aircraft visits 10
Test Examinations / Assessments 11
Total Hours 198 104
Airbus
Overhead Panel
Push-Button & Switching
Explanation
(For reference only)
A330 & A340
Overhead Panel Switches
23-Jan-07 For reference only
Airbus Overhead Panel Switches
21. AIR / PRESSURIZATION / VENTILATION
PACK 1
On – Pack flow control valve opens automatically except when;
- upstream press below min.
- compressor outlet overheat
- engine start sequence (Mode selector IGN, reopen after 30s if no
eng start.)
- any door is not closed and locked, a/c on gnd, an engine running.
- Onside engine fire Pb pressed
- ditching selected.
Note: On gnd, valves reopening is delayed 30s to avoid a supplementary pack closure cycle
during subsequent eng start. If there is no electrical power, the flow valves remain open and
permit NORM flow.
Off – Valve closes provided it is electrically supplied
Fault - Valve position disagree with Selector position
- Compressor outlet overheat
- Pack outlet overheat
PACK FLOW
NORM
LO HI LO- 80% (Less than 160 in Y and 200 total)
　
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