|
Number
|
Issued by
|
Issue date
|
Subject
|
Approval Holder / Type Designation
|
Effective date
|
Attachment |
|
US-2001-17-26R1
|
|
2002-01-29
|
SUPERSEDED BY FAA AD 2003-04-20
|
|
2001-10-03
|
|
|
CF-2002-10
|
|
2002-01-28
|
Intercompressor Case Fire
|
|
2002-03-01
|
|
|
CF-2002-08
|
|
2002-01-25
|
Fuselage Skin Panels Bonding Integrity Inspection
|
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
|
2002-02-22
|
|
|
US-2002-01-13
|
|
2002-01-25
|
Main Landing Gear Outer Cylinder Aft Trunnion - Inspection
|
|
2002-03-01
|
|
|
F-2001-446R1
|
|
2002-01-23
|
Ammeter circuit modification
|
|
2002-02-02
|
|
|
F-2002-046
|
|
2002-01-23
|
Flaps Control System Pushrod - Inspection / Replacement
|
|
2002-02-02
|
|
|
F-2002-044
|
|
2002-01-23
|
SIREN cargo hooks
|
-
AIRBUS HELICOPTERS
-
AS 350 / EC 130
-
SA/AS 365 / EC 155
|
2002-01-23
|
|
|
F-2001-501-001R1
|
|
2002-01-23
|
Hydraulic power - Hydraulic fluid
|
|
2002-02-02
|
|
|
F-1997-147-072R1
|
|
2002-01-23
|
Tail boom-to-aircraft structure junction attachment screws
|
|
2002-02-02
|
|
|
F-1997-146-054R1
|
|
2002-01-23
|
Tail boom-to-aircraft structure junction attachment screws
|
|
2002-02-02
|
|
|
F-2002-071-091
|
|
2002-01-23
|
Engines - High pressure oil pump - Pressure regulating valve (PRV)
|
|
2002-01-23
|
|
|
F-2002-043
|
|
2002-01-23
|
SUPERSEDED BY DGAC FRANCE AD F-2003-432
|
|
2002-01-23
|
|
|
US-2002-01-10
|
|
2002-01-22
|
Main Landing Gear Upper and Lower Torque Knees - Inspection / Replacement
|
-
TEXTRON AVIATION INC.
-
65 (Queen Air)
-
90 (King Air)
|
2002-02-22
|
|
|
US-2002-01-12
|
|
2002-01-22
|
High Pressure Turbine Interstage Seals - Removal from Service / Reduced Life Limit
|
|
2002-02-26
|
|
|
F-2002-077-040
|
|
2002-01-22
|
RVSM - Monitoring flight
|
|
2002-01-22
|
|
|
CF-2002-06
|
|
2002-01-21
|
Rudder Travel Limiter Actuators
|
|
2002-03-04
|
|
|
CF-2002-07
|
|
2002-01-21
|
Forward Engine Mount Assembly
|
-
DE HAVILLAND AIRCRAFT OF CANADA LTD.
|
2002-03-04
|
|
|
US-2002-01-04
|
|
2002-01-20
|
SUPERSEDED BY FAA AD 2004-09-34
|
|
2002-02-14
|
|
|
F-2002-032
|
|
2002-01-19
|
Fuselage - frame 35 reinforcement between stringer 30 and 31
|
|
2002-01-19
|
|
|
US-2001-25-51
|
|
2002-01-17
|
[Final Rule] Rotorcraft Flight manual - Revision -- Integrated Instrument Display System - Test
|
-
MD HELICOPTERS INC (MDHI)
|
2001-12-07
|
|