|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
US-2002-05-05
|
|
2002-03-13
|
SUPERSEDED BY FAA AD 2002-24-08
|
-
CIRRUS DESIGN CORPORATION
|
2002-03-19
|
|
|
CF-2002-19
|
|
2002-03-11
|
SUPERSEDED BY TRANSPORT CANADA AD CF-2003-01
|
|
2002-03-11
|
|
|
US-2002-05-03
|
|
2002-03-08
|
Time Limits / Maintenance Checks - Critical Life-Limited Parts - Inspection
|
|
2002-04-12
|
|
|
US-2002-05-51
|
|
2002-03-07
|
SUPERSEDED BY FAA AD 2002-15-03
|
|
2002-03-07
|
|
|
D-2002-015-2
|
|
2002-03-07
|
Landing gear - Inspection/Check of several Landing Gear Bolts
|
|
2002-03-07
|
|
|
D-2002-014-2
|
|
2002-03-07
|
Landing gear - Inspection/Check of several Landing Gear Bolts
|
|
2002-03-07
|
|
|
D-2002-050
|
|
2002-03-07
|
Electrical power - Fuel pump wiring check inside the feeder tank
|
|
2002-03-07
|
|
|
D-2002-049
|
|
2002-03-07
|
Electrical power - Fuel pump wiring check inside the feeder tank
|
|
2002-03-07
|
|
|
F-2002-127
|
|
2002-03-06
|
Engine - Centrifugal Impeller - Modification
|
-
SAFRAN HELICOPTER ENGINES
|
2002-03-16
|
|
|
US-2002-03-08
|
|
2002-03-06
|
SUPERSEDED BY FAA AD 2005-25-09
|
-
PRATT & WHITNEY
-
PW4000
-
PW4070
-
PW4080
-
PW4090
-
PW4100
|
2002-04-16
|
|
|
F-1999-265-117R2
|
|
2002-03-06
|
Thrust Reversers Locking
|
|
2002-03-16
|
|
|
CF-2002-16
|
|
2002-03-04
|
Magnetic Brake
|
-
BELL TEXTRON CANADA LTD (BTCL)
|
2002-03-15
|
|
|
CF-2002-17
|
|
2002-03-04
|
Magnetic Brake
|
-
BELL TEXTRON CANADA LTD (BTCL)
|
2002-03-15
|
|
|
SE-1-173
|
|
2002-03-04
|
Landing Gear - Installation of New Retract Actuator Bracket Attachment Bolt.
|
|
2002-03-04
|
|
|
US-2002-04-08
|
|
2002-03-01
|
Equipment / Furnishings - Rudder Pedal Housing Upper Cover Assembly - Inspection
|
|
2002-04-05
|
|
|
US-2002-05-01
|
|
2002-03-01
|
Outboard Nacelle Struts Aft Torque Bulkhead Vertical Chords - Inspection / Modification
|
|
2002-03-18
|
|
|
G-001-03-2002
|
|
2002-03-01
|
Fuel - Quantity indication - Installation of a new harness in the fuel tank and an inspection of the cable to the fuel boost pump (left and right).
|
-
BAE SYSTEMS (OPERATIONS) LTD
|
2002-03-01
|
|
|
US-2002-04-06
|
|
2002-02-25
|
Wings - Rear Spar Upper Chord - Inspection
|
|
2002-04-01
|
|
|
US-2002-04-01
|
|
2002-02-21
|
Nose Landing Gear Upper Lock Link Assembly - Inspection / Modification
|
|
2002-03-28
|
|
|
CF-2002-15
|
|
2002-02-20
|
Rudder Trim Switch Wiring
|
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
|
2002-03-15
|
|