AD/A109/49 - Battery Bus Circuit Breaker
Airworthiness Directive - AD/A109/49 - Battery Bus Circuit Breaker
Airworthiness Directive - AD/A109/49 - Battery Bus Circuit Breaker CASA Airworthiness Directive Jurisdiction:Commonwealth of Australia;CorporateName:Civil Aviation Safety Authority; Issue 3/2004,Rotorcraft,Agusta A109 Series Helicopters,Battery Bus Circuit Breaker,49 DellaCa, Donna 2 1 2022-10-25T22:29:00Z 2022-10-25T22:30:00Z 1 307 1754 Office of Parliamentary Counsel 14 4 2057 16.0000
2006-09-21T00:00:00Z Toolkit http://www.activepdf.com 2022-10-25T00:00:00Z
COMMONWEALTH OF AUSTRALIA (Civil
Aviation
Safety
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 CASR 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.
Agusta
A109
Series
Helicopters
AD/A109/49 Battery
Bus
Circuit
Breaker 3/2004
Applicability: A109E
series
helicopters
as
follows:
All
serial
numbers
(S/N)
up
to
and
including
11077
that
have
kits
part
number 109-0812-04-101, or -103, or -107, or -109 installed, and
b.
S/N
11078
up
to
and
including
11122.
Requirement: Modify
the
emergency
electrical
bus
in
accordance
with
Agusta
Mandatory
Bollettino Tecnico 109EP-39 dated 25 November 2003.
Note:
ENAC
AD
2003-384
refers.
Compliance: No
later
than
31
March
2004.
This
Airworthiness
Directive
becomes
effective
on
18
March
2004.
Background: The Italian Ente Nazionale per l’Aviazone Civile has advised that Agusta, whilst carrying out an investigation into the emergency busses of the A109E helicopter, discovered that in the event of a double generator failure the 25 Amp “BATT BUS” circuit breaker could trip.
This Directive requires the modification of the emergency electrical
bus
installation
by
the
replacement
of
the
“BATT
BUS”
circuit
breaker
with a 35 Amp rated circuit breaker.
James
Coyne
Delegate
of
the
Civil
Aviation
Safety
Authority 4 February 2004
The
above
AD
is
notified
in
the
Commonwealth
of
Australia
Gazette
on
25
February
2004.
Page
1
of
1
Official source: https://www.legislation.gov.au/Details/F2006B01833