|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
US-90-25-05R1
|
|
2008-02-14
|
[Correction] Corrosion Prevention and Control Program - Implementation
|
|
2008-01-22
|
|
|
CF-2008-07
|
|
2008-02-14
|
Fuel System Safety - Introduction of Critical Design Configuration Control Limitations
|
|
2008-02-15
|
|
|
CF-2008-09
|
|
2008-02-14
|
Air-Driven Generator - Internal Wiring
|
|
2008-02-18
|
|
|
CF-2008-10
|
|
2008-02-14
|
Air-Driven Generator - Internal Wiring
|
|
2008-02-19
|
|
|
2008-10
|
|
2008-02-14
|
Airbus A318/A319/A320/A321 Standard Operating Procedures - Ground Spoilers do not Deploy Automatically After Landing
|
-
Safety Information Bulletin
|
|
|
|
2008-0029
|
|
2008-02-14
|
Equipment/Furnishings - Pilot’s Operating Handbook procedure for crew and front passenger seats - Modification
|
|
2008-02-28
|
|
|
2008-0027-E
|
|
2008-02-13
|
SUPERSEDED BY EASA EMERGENCY AD 2008-0056-E
|
-
CONTINENTAL AEROSPACE TECHNOLOGIES, GmbH
|
2008-02-15
|
|
|
2008-0028-E
|
|
2008-02-13
|
Stabilizers – Vertical Fin Spar - Inspection
|
-
TECNAM, Costruzioni Aeronautiche
|
2008-02-15
|
|
|
2008-0026
|
|
2008-02-12
|
SUPERSEDED BY EASA AD 2013-0268 AND EASA AD 2013-0269
|
|
2008-02-26
|
|
|
US-2008-03-20
|
|
2008-02-11
|
Forward RH Side Door Slide Compartment Door Mounted Escape System - Modification
|
|
2008-03-17
|
|
|
US-2008-03-16
|
|
2008-02-08
|
Rudder and Aileron Interconnecting Components - Inspection / Replacement
|
-
CIRRUS DESIGN CORPORATION
|
2008-03-11
|
|
|
2008-08
|
|
2008-02-07
|
Failure of Fuel Filler Cap, resulting in Fuel Contamination
|
-
Safety Information Bulletin
|
|
|
|
US-2007-23-12
|
|
2008-02-06
|
[Correction] Fuel System Installation Configuration - Survey / Repair / Modification
|
|
2008-01-10
|
|
|
US-2008-02-13
|
|
2008-02-06
|
Fuselage Crown Skin - Inspection / Repair
|
|
2008-02-28
|
|
|
2008-06
|
|
2008-02-06
|
WITHDRAWN - FAA SAIB TRANSFERRED TO EASA SUP WEBPAGE
|
-
Safety Information Bulletin
|
|
|
|
2008-09
|
|
2008-02-06
|
Embraer EMB-135 and EMB-145 Aeroplanes - Mechanical Gust Lock System
|
-
Safety Information Bulletin
|
|
|
|
2008-0023
|
|
2008-02-06
|
SUPERSEDED BY EASA AD 2009-0102
|
|
2008-02-20
|
|
|
US-2008-02-19
|
|
2008-02-05
|
High Pressure Turbine Rotor assemblies - Identification / Removal from Service
|
-
HONEYWELL INTERNATIONAL INC.
-
TFE731
-
TFE731-20/-40/-50/-60
|
2008-03-06
|
|
|
US-2008-03-02
|
|
2008-02-01
|
SUPERSEDED BY FAA AD 2012-02-02
|
|
2008-03-06
|
|
|
DCA-750XL-4A
|
|
2008-01-31
|
Fuselage – Frame 384 Rivets – Inspection / Replacement
|
|
2008-01-31
|
|