AD/A320/46 Amdt 4 - Inboard Flap Trunnion
Airworthiness Directive - AD/A320/46 Amdt 4 - Inboard Flap Trunnion
Airworthiness Directive - AD/A320/46 Amdt 4 - Inboard Flap Trunnion CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 11/1999,Aircraft above 5700 kg,Airbus Industrie A319, A320 and A321 Series Aeroplanes,Inboard Flap Trunnion,46 Amdt 4 DellaCa, Donna 2 0 2022-10-27T03:33:00Z 2022-10-27T03:34:00Z 1 276 1579 Office of Parliamentary Counsel 13 3 1852 16.0000
2006-09-22T00:00:00Z Toolkit http://www.activepdf.com 2022-10-27T00:00:00Z
COMMONWEALTH OF AUSTRALIA (Civil
Aviation
Regulations
1998) ,
PART
39
-
105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE
OF
AIRWORTHINESS
DIRECTIVES
Airbus
Industrie
A319,
A320
and
A321
Series
Aeroplanes
AD/A320/46
Amdt
4
Inboard
Flap
Trunnion 11/99
Applicability: A319,
A320,
and
A321
aircraft,
all
models
and
serial
numbers;
without
Airbus Industrie modification 26495 installed at production or Service Bulletin
A320-27-1117
incorporated.
Requirement: Action
in
accordance
with
the
technical
requirements
of
DGAC
AD 1996-271-092 (B) R3.
Note:
Airbus
Industrie
Service
Bulletins
A320-27-1066
Revision
5,
-1050,
-1097 Revision 2, -1108 Revision 3, and -1117 refer.
Compliance: As
specified
in
the
Requirement
document
for
the
initial
and
repetitive
inspection
requirements.
This
Amendment
becomes
effective
on
4
November
1999.
Background: An operator reported wear marks 0.118 inches deep in the inboard flap attachment trunnion caused by chafing of the sliding panel drive chain.
This could lead to rupture of the trunnion primary load path and subsequently adversely influence the fatigue
life
of
the
secondary
load
path.
Inspection
of
the
trunnion
will
ensure
that
the critical depth is not reached.
Amendment
1
amended
the
applicability,
and
included
inspections
for
all
mod.
states across the various aircraft.
Amendment 2 reflected a revision of the DGAC AD which introduced revised requirement documents.
Amendment 3 clarified
applicability.
Amendment
4
is
issued
in
response
to
a
new
DGAC
AD
which
introduces
revisions of the related service bulletins and clarifies compliance requirements.
Amendment 3 of this Airworthiness Directive became effective on 17 June 1999. Amendment 2 of this Airworthiness Directive became effective on 1 January 1998. The
original
issue
of
this
Airworthiness
Directive
became
effective
on
27
April
1995.
Official source: https://www.legislation.gov.au/Details/F2006B01936