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hydraulic circuits and
electrical systems are
tested
- a third approach in
manual mode
Manual landing Ground spoiler activation
Auto brake accuracy
Ground spoiler activation
Auto brake accuracy
Taxi and
engine
shutdown
Taxi
Shutdown
- 43 -
APPENDIX 3
Checks performed on 27 November 2008
Flight Phases OFC Programme Checks performed
during flight on 27/11
Cabin
preparation
Cabin preparation
Cabin general
Flight
preparation
Flight preparation
Before engine start
Engine start
After engine start
Ground
Taxiing
Takeoff TOGA Max rated take off
Before take off
Thrust acquisition check
Takeoff
After lift off Auto flight systems
Landing gear retraction
Performed (initial climb)
Initial climb Auto throttle system Performed with EXPD
CLIMB
Climb to FL310
Climb to FL 310 Flight controls (normal law)
Auto flight systems
Systems (ECAM pages)
Communication systems
Navigation systems
Performed
Performed
(during climb towards
FL320)
Performed at
FL320 by New Zealand
pilot
Performed
FL280
Performed
(during climb towards
FL320)
Cruise at FL310 Engine parameters record
A/C trim
Performed FL320
Climb to FL390
– Mach 0.78
Air conditioning system
efficiency Cabin general
Cruise
Cruise at FL390
– Mach 0.78
APU start Performed
Descent to FL
140
Anti ice wing
MMO overspeed (prior to
FL250)
VMO overspeed (below
FL250)
Flight controls (alternate law)
Performed FL 390 (on
descent to FL200)
Performed on descent
(FL330)
Performed FL 200
Performed FL 120
Descent
Descent and
cruise at FL140
– Any suitable
A/C speed
ECS supply from the APU
bleed
Low speed – full configuration
Performed FL 120
Started at 4,080 ft.
- 44 -
Approach 1
(autoland)
Airplane general
ILS
Radio-altimeter
Auto callout
Automatic goaround
(at 1,000
ft AGL)
Auto flight systems
Landing gear emergency
Second
approach
(manual)
Airplane general
Flight controls
Approach and
landing
Manual landing Ground spoiler activation
Auto brake accuracy
Taxi and
engine
shutdown
Taxi
Shutdown
- 45 -
Appendix 4
Descriptions of flight at low speed – OFC document, SA CAM and ISATM manuals
- 46 -
Flight at low speed – SA CAM Manual
- 47 -
- 48 -
Flight at low speed – ISATM Manual
- 49 -
- 50 -
- 51 -
- 52 -
Appendix 5
FAA Document - SAFO 08 024
Bureau d’Enquêtes et d’Analyses
pour la sécurité de l’aviation civile
Zone Sud - Bâtiment 153
200 rue de Paris
Aéroport du Bourget
93352 Le Bourget Cedex - France
T : +33 1 49 92 72 00 - F : +33 1 49 92 72 03
www.bea.aero
DMC519
THE MAINTENANCE PROBLEM...
Modern aircraft, such as the AIRBUS A320, A330, A340, have
complicated electrical wiring systems containing many different
connectors, contacts and terminals, the repair of which require precision
tools.
It is not a cost effective use of the time of your technical staff to start
from scratch and try to become intimately knowledgeable about which
precision tools must be used to repair each electrical connector, contact
and terminal when DMC has already performed this task for the A320,
A330, A340.
AOG TIME CONSTRAINTS. Once the aircraft becomes inoperable because of a connector failure, it is imperative
to be able to replace the connector, contact or terminal as quickly as possible to avoid revenue loss due to AOG. The
DMC519 kit supplies your staff with both the information and the tools necessary to make this type of repair to the
A320, A330, A340 in the shortest time possible.
THE DMC SOLUTION...
TOOLING RESEARCH. DMC has already researched the wiring manual of the A320, A330, A340 and has identified
the most common tools required to maintain the electrical connectors in the A320, A330, A340. DMC has cross
referenced these tools to the connectors, contacts and
terminals, eliminating costly and time-consuming
research which would otherwise have to be
performed by your electrical technicians.
IMMEDIATE AVAILABILITY OF TOOLS
AND TECHNICAL INFORMATION. The
DMC519 kit contains all of the tooling to
　
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