AD/A320/142 - Trust Reverser - Piston Rod Chrome Plating
Airworthiness Directive - AD/A320/142 - Trust Reverser - Piston Rod Chrome Plating
Airworthiness Directive - AD/A320/142 - Trust Reverser - Piston Rod Chrome Plating CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 11/2002,Aircraft above 5700 kg,Airbus Industrie A319, A320 and A321 Series Aeroplanes,Trust Reverser - Piston Rod Chrome Plating,142 DellaCa, Donna 2 1 2022-10-26T04:49:00Z 2022-10-26T04:50:00Z 1 258 1477 Office of Parliamentary Counsel 12 3 1732 16.0000
2006-09-22T00:00:00Z Toolkit http://www.activepdf.com 2022-10-26T00:00:00Z
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998) , PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE
OF
AIRWORTHINESS
DIRECTIVES
AIRWORTHINESS
DIRECTIVE
For the
reasons set
out in
the background
section, the
CASA delegate
whose signature
appears below
issues the
following Airworthiness
Directive (AD)
under
subregulation
39.1
(1)
of
CAR
1998.
The
AD
requires
that
the
action
set
out
in
the
requirement
section
(being
action
that
the
delegate
considers
necessary
to
correct
the
unsafe
condition)
be
taken
in
relation
to
the
aircraft
or
aeronautical
product
mentioned
in
the
applicability
section:
(a)
in
the
circumstances
mentioned
in
the
requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
Airbus
Industrie
A319,
A320
and
A321
Series
Aeroplanes
AD/A320/142 Trust
Reverser
-
Piston
Rod
Chrome
Plating 11/2002
Applicability: All
A319,
A320
and
A321
series
aeroplanes
as
identified
in
the
requirement
document.
Requirement: Action
per
DGAC
AD
2002- 337(B)R1.
Note:
DGAC
AD
2002-337(B)
R1
refers.
Compliance: Per
the
requirement
document
with
a
revised
effective
date
of
31
October
2002.
This
Airworthiness
Directive
becomes
effective
on
31
October
2002.
Background: Error during the repair and rigging of thrust reverser blocker door actuators has resulted
in
a
situation
of
potential
door
deployment in-
flight.
This
directive
mandates the replacement of affected actuators.
James
Coyne
Delegate
of
the
Civil
Aviation
Safety
Authority 24 September 2002
The
above
AD
is
notified
in
the
Commonwealth
of
Australia
Gazette
on
9
October
2002.
Page
1
of
1
Official source: https://www.legislation.gov.au/Details/F2006B01888