AD/A109/30 - Gleason Crown Inspection
Airworthiness Directive - AD/A109/30 - Gleason Crown Inspection
Airworthiness Directive - AD/A109/30 - Gleason Crown Inspection CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 8/1999,Rotorcraft,Agusta A109 Series Helicopters,Gleason Crown Inspection,30 DellaCa, Donna 2 0 2022-10-21T00:24:00Z 2022-10-21T00:24:00Z 1 266 1519 Office of Parliamentary Counsel 12 3 1782 16.0000
2006-09-21T00:00:00Z Toolkit http://www.activepdf.com 2022-10-21T00:00:00Z
COMMONWEALTH OF AUSTRALIA (Civil
Aviation
Regulations
1998) ,
PART
39
-
105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE
OF
AIRWORTHINESS
DIRECTIVES
Agusta
A109
Series
Helicopters
AD/A109/30 Gleason Crown Inspection 8/99
DM
Applicability: A109A,
A109AII
and
A109C
helicopters,
fitted
with
main
transmission
and
Gleason Crown identified in Agusta Service Bulletin No. 109-109 dated 03 June 1999 and which have accumulated between 300 and 900 operating hours.
Requirement: 1.
Perform the aural inspection of the main gearbox in accordance with the instructions
contained
in
Part
I
of
Agusta
Service
Bulletin
No.
109-109
dated
03 June 1999.
Note:
The
word
“auscultate”
in
the
Agusta
SB
means
“to
listen
to
using
a
stethoscope”.
2.
Perform the non destructive test of the Gleason Crown (installed in the main transmission)
in
accordance
with
the
instructions
contained
in
Part
II
of
Agusta Service Bulletin No. 109-109 dated 03 June 1999.
Replace Gleason Crown as required by Agusta Service Bulletin No. 109-109.
3.
Repeat
the
test
at
2
above.
Note:
RAI
AD
99-267
dated
10
June
1999
refers.
Compliance: 1.
Before
next
flight
after
the
effective
date
of
this
Directive.
2.
Not
later
than
50
operating
hours
following
the
effective
date
of
this
Directive.
3.
Every
three
hundred
operating
hours
up
to
and
including
nine
hundred
operating
hours.
This
Airworthiness
Directive
becomes
effective
on
14
July
1999.
Background: One case of a cracked Gleason Crown on an Agusta A109C helicopter has been discovered following an investigation into a reported unusual noise from the main rotor transmission system.
This directive introduces a regular aural inspection and Non
Destructive
test
to
monitor
for
the
presence
of
cracks
in
the
Gleason
Crown
of certain helicopters and certain transmissions.
Official source: https://www.legislation.gov.au/Details/F2006B01816