|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
US-2009-26-06
|
|
2010-01-08
|
Engine Fuel & Control - Fuel Manifold Assemblies - Inspection
|
-
HONEYWELL INTERNATIONAL INC.
|
2010-02-11
|
|
|
US-2008-10-06R1
|
|
2010-01-08
|
Fuel - Fuel Tank Systems - Inspection
|
|
2010-01-22
|
|
|
2010-0005
|
|
2010-01-07
|
Landing Gear - Main Landing Gear Wheel Axle - Inspection / Modification
|
|
2010-01-21
|
|
|
US-2008-10-09R1
|
|
2010-01-07
|
Revision of Approved Maintenance Programme - Fuel Tank System Components - Revision/ Incorporation of New AWLs - CDCCL Requirements - Inspection/Repair
|
|
2010-01-15
|
|
|
2009-0230R1
|
|
2010-01-07
|
SUPERSEDED BY EASA AD 2010-0170-E
|
|
2010-01-21
|
|
|
2010-0007
|
|
2010-01-07
|
Fuselage – Frame 58 Butt Joint – Reinforcement
|
|
2010-01-21
|
|
|
US-2009-26-04
|
|
2010-01-06
|
Landing Gear - Main Landing Gear (MLG) Forward Trunnion Pins - Inspection/Lubrication/Overhauling
|
|
2010-02-01
|
|
|
US-2009-26-03
|
|
2010-01-06
|
Electrical Power - Static Inverter Resistor - Modification / Replacement
|
|
2010-02-01
|
|
|
US-2009-20-11
|
|
2010-01-06
|
[Correction] Fuel System Limitations and Inspections associated with Goodrich Corporation STC ST00127BO
|
-
BOEING
-
GOODRICH CORPORATION
|
2009-11-05
|
|
|
US-2009-26-17
|
|
2010-01-05
|
SUPERSEDED BY FAA AD 2012-19-03
|
|
2010-02-04
|
|
|
US-2009-26-12
|
|
2010-01-05
|
ENGINE COMPONENTS INC. - Cyllinder Assemblies - Inspection / Replacement
|
-
APPLIANCES
-
ATA 72 RECIPROCATING ENGINE
-
LYCOMING ENGINES
-
AEIO-320
-
AEIO-360
-
AEIO-540
-
AIO-320
-
HIO-360
-
HO-360
-
IO-320
-
IO-360
-
IO-540
-
LIO-320
-
LO-360
-
LTIO-540
-
LTO-360
-
O-320
-
O-360
-
O-540
-
TIO-540
-
TO-360
|
2010-02-04
|
|
|
2010-0002
|
|
2010-01-05
|
Stabilizers – Rudder Side Shell Skin – Inspection
|
|
2010-01-19
|
|
|
2010-0004
|
|
2010-01-05
|
SUPERSEDED BY EASA AD 2015-0211
|
-
SAFRAN HELICOPTER ENGINES
|
2010-01-19
|
|
|
US-2009-22-02
|
|
2010-01-04
|
Equpment / Furnishings - Rear Seat Frame - Inspection
|
-
AMERICAN CHAMPION AIRCRAFT CORP
|
2009-12-03
|
|
|
2010-0001-E
|
|
2010-01-04
|
SUPERSEDED BY EASA AD 2010-0202
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
2010-01-06
|
|
|
US-2009-24-11
|
|
2010-01-01
|
SUPERSEDED BY FAA AD 2010-01-04
|
|
2010-02-03
|
|
|
CF-2009-46
|
|
2009-12-23
|
Landing Gear Alternate Extension Access Panel – Potential Failure to Open
|
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
|
2010-01-07
|
|
|
CF-2009-45
|
|
2009-12-23
|
Aileron Terminal Quadrant Support Bracket Cracking
|
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
|
2010-01-07
|
|
|
2009-0279
|
|
2009-12-23
|
Canopy - Jettison Test / Repair
|
|
2010-01-06
|
|
|
US-2009-24-06
|
|
2009-12-22
|
NOT ADOPTED - SEE ATTACHED EASA DECISION - ANAC BRAZIL AD 2008-03-01R2
|
|
2009-12-17
|
|
