Thu, Dec 01, 2005
Applicability:
Model AS 332 helicopters versions C, C1, L, and L1, equipped with
plug doors.
Requirement: 1. Check for interference between
the step of the middle-rail stop assembly and the plug door
fitting, in accordance with paragraph 2.B. of Eurocopter AS 332
Alert Service Bulletin (ASB) No. 52.00.33 R1. If no interference is
evident, no further action is required.
2. In the case of plug doors where MOD 0725366 has not been
embodied, that are affected by interference indicated by wear
between the step of the rail of the stop assembly and the shaft of
the fitting: If there is interference, with or without shaft
rotation, comply with the instructions in paragraph 1.E.2.a.1. of
ASB No. 52.00.33 R1. In all cases, opening and closing the plug
door in flight is permitted only in an emergency in compliance with
the instructions of Note 3 in paragraph 2 of ASB No. 52.00.33 R1.
Affix a label to the immediate vicinity of the inner door handles,
indicating this restriction, in red text.
3. In the case of plug doors where MOD 0725366 has been embodied,
that are affected by interference indicated by wear between the
step of the rail of the stop assembly and the shaft of the fitting:
If there is interference, with or without shaft rotation, comply
with the instructions in paragraph 1.E.2.a.2. of ASB No. 52.00.33
R1.
Note: DGAC AD F-2004-142 R1 refers.
Compliance: 1. At the next ALF-check after 7
December 2005, unless already accomplished.
2. Before further flight, unless already accomplished.
3. Within the next 50 flight hours, and thereafter at intervals not
to exceed 50 flight hours.
This amendment becomes effective on 7 December 2005.
Background:
The manufacturer received a report of the loss of a right hand plug
door from an AS 332 L helicopter during in-flight door operation.
The aircraft was performing hover flight when a crew member
unlocked the door for aerial photography. The door was not found,
and an examination of the elements on the airframe revealed that
this event was caused by a hinge failure of the stop assembly of
the middle rail. Amendment 1 is issued in response to a revision of
the related DGAC AD, which introduces Revision 1 of the Requirement
document.
More News
Maximum Authorized Altitude A published altitude representing the maximum usable altitude or flight level for an airspace structure or route segment. It is the highest altitude on >[...]
Aero Linx: Soaring Safety Foundation (SSF) The Soaring Safety Foundation (SSF) is the Training and Safety arm of the Soaring Society of America (SSA). Our mission is to provide ins>[...]
From 2013 (YouTube Version): Dracula Lives On Through Kyle Franklin... and We're NOT Scared! ANN CEO and Editor-in-Chief, Jim Campbell speaks with Aerobatic and airshow master, Kyl>[...]
“For Montaer Aircraft it is a very prudent move to incorporate such reliable institution as Ocala Aviation, with the background of decades in training experience and aviation>[...]
Also: ForeFlight Upgrades, Cicare USA, Vittorazi Engines, EarthX We have a number of late-breaking news highlights from the 2024 Innovation Preview... which was PACKED with real ne>[...]