|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
CE-11-49
|
|
2011-09-01
|
Air Tractor, Inc. AT-802, AT-802A Elevator Tab Control System
|
-
Safety Information Bulletin
|
|
|
|
AV-06-2011
|
|
2011-09-01
|
SUPERSEDED BY ANAC Flight Alert (FA) No. 24/2012
|
-
Safety Information Bulletin
|
|
|
|
2011-0166
|
|
2011-09-01
|
SUPERSEDED BY EASA AD 2012-0177
|
|
2011-09-15
|
|
|
2011-0165
|
|
2011-09-01
|
SUPERSEDED BY EASA AD 2014-0205
|
|
2011-09-15
|
|
|
CF-2011-33
|
|
2011-09-01
|
Engine Support Beam – Cracking on the Upper and Lower Web
|
|
2011-08-31
|
|
|
2010-0112R1
|
|
2011-08-31
|
Oxygen System – Passenger Oxygen Masks - Identification /
Modification / Replacement
|
|
2011-08-31
|
|
|
2011-0162
|
|
2011-08-30
|
Electrical Power – Generator Relay After Junction Box – Modification
|
-
AIRBUS HELICOPTERS DEUTSCHLAND
|
2011-09-06
|
|
|
2011-0163
|
|
2011-08-30
|
SUPERSEDED BY EASA AD 2015-0232
|
|
2011-09-13
|
|
|
US-2011-16-02
|
|
2011-08-30
|
Ice and Rain Protection - Airplane Flight Manual (AFM) - Revision
|
|
2011-08-30
|
|
|
US-2011-17-11
|
|
2011-08-29
|
Wings - Lower Rear Spar Cap - Inspection
|
|
2011-09-26
|
|
|
CF-2011-34
|
|
2011-08-26
|
Ice Protection System – Failure of the Timer and Monitor Unit
|
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
|
2011-08-31
|
|
|
2011-0161
|
|
2011-08-26
|
Electric and Electronic Common Installation – Right Hand (RH) Wing Wiring in Zone 675 - Modification
|
-
AIRBUS S.A.S.
-
A300-600
-
A300-600ST (Beluga)
|
2011-09-09
|
|
|
2011-0158
|
|
2011-08-26
|
Fuel – Fuel-Balance Transfer System – Deactivation
|
|
2011-09-09
|
|
|
2011-0159
|
|
2011-08-26
|
SUPERSEDED BY EASA AD 2019-0224
|
|
2011-09-09
|
|
|
2011-0156-E
|
|
2011-08-25
|
SUPERSEDED BY EASA AD 2012-0030
|
-
LEONARDO S.p.A. HELICOPTERS
|
2011-08-25
|
|
|
2011-0157
|
|
2011-08-25
|
SUPERSEDED BY EASA AD 2012-0049
|
|
2011-09-08
|
|
|
US-2011-18-02
|
|
2011-08-24
|
Rotor - Fan Rotor Spinner Support - Removal
|
|
2011-09-26
|
|
|
2011-0152-E
|
|
2011-08-18
|
SUPERSEDED BY EASA AD 2014-0232
|
-
CONTINENTAL AEROSPACE TECHNOLOGIES, GmbH
|
2011-08-22
|
|
|
CF-2011-32
|
|
2011-08-18
|
Rudder Control - Excessive Wear on the Brake Pedal Bellcrank
|
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
|
2011-08-29
|
|
|
CF-2011-31
|
|
2011-08-18
|
Incorrect Heat Treatment of Pushrod Assembly
|
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
|
2011-08-31
|
|