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  Safety Publications Tool

List of Mandatory Continuing Airworthiness Information

Displaying records 12421 to 12440 out of a total of 18179 publications.

Number Issued by Issue date Sorted in descending order Subject Approval Holder / Type Designation Effective date Attachment
F-1999-511-297R2
FR
 2002-11-23 Fuselage - Articulated seat and dummy tracks
  • AIRBUS S.A.S.
    • A300
    • A300-600
    • A300-600ST (Beluga)
    • A310
2002-11-23
F-2001-265R2
FR
 2002-11-23 Navigation - Pitot probes.
  • AIRBUS S.A.S.
    • A300
    • A300-600
    • A310
2002-11-23
F-2002-554
FR
 2002-11-23 Electrical power Replacement of TRU installed in position 2 (1PU2)
  • AIRBUS S.A.S.
    • A319
    • A320
    • A321
2002-11-23
US-2002-22-12
US
 2002-11-22 [Correction] TITEFLEX CORPORATION - High-Pressure and Medium-Pressure Fuel Hoses - Inspection / Replacement
  • APPLIANCES
    • ATA 28 FUEL SYSTEM
    • ATA 73 ENGINE FUEL & CONTROL
2002-12-13
US-2002-23-02
US
 2002-11-20 Time Limits / Maintenance Checks - Airworthiness Limitations Section / Maintenance Program - Revision
  • GENERAL ELECTRIC
    • CF34-8
2002-12-26
US-2002-23-03
US
 2002-11-20 Main Rotor Drive - Longitudinal Drive Link / Non-Rotating Swashplate - Inspection / Repair / Modification
  • MD HELICOPTERS INC (MDHI)
    • MD900
2002-12-26
US-2002-23-05
US
 2002-11-20 Electrical Power - Circuit Breakers - Replacement
  • TEXTRON AVIATION INC.
    • 750 (Citation X)
2002-12-26
US-2002-23-11
US
 2002-11-20 Flight Controls - Elevator Balance Weight Attachment Screws - Inspection
  • TEXTRON AVIATION INC.
    • 100 (King Air)
    • 1900 (Airliner)
    • 200 (Super King Air)
    • 300 (Super King Air)
    • 90 (King Air)
2003-01-10
CF-2002-47
CA
 2002-11-18 Inspection of Turbine Exhaust Duct
  • PRATT & WHITNEY CANADA
    • PT6A-100
    • PT6A-11/15
    • PT6A-20
    • PT6A-30
    • PT6A-6
2002-12-30
US-2002-23-06
US
 2002-11-14 SUPERSEDED BY FAA AD 2004-05-24
  • LYCOMING ENGINES
    • AEIO-540
    • IO-540
    • LTIO-540
    • O-540
    • TIO-540
2002-11-19
D-2002-355
DE
 2002-11-14 Correction of Airplane Flight Manual (AFM) Performance
  • DEUTSCHE AIRCRAFT GmbH
    • Dornier 328
2002-11-14
F-2002-550
FR
 2002-11-13 MGB - Aft suspension bars
  • AIRBUS HELICOPTERS
    • SA 330 / AS 332 / EC 225
2002-11-23
F-1997-026-005R3
FR
 2002-11-13 Main rotor blade vibration damper
  • AIRBUS HELICOPTERS
    • SA 330 / AS 332 / EC 225
2002-11-23
F-2002-569
FR
 2002-11-13 Structure - Tank skin reinforcement.
  • DASSAULT AVIATION
    • Mystère-Falcon 50
    • Mystère-Falcon 900
2002-11-23
US-2002-22-17
US
 2002-11-12 SUPERSEDED BY FAA AD 2004-17-01
  • TEXTRON AVIATION INC.
    • 208 (Caravan I)
2002-12-31
F-2002-528
FR
 2002-11-09 Fuselage - Reinforcement of the structure between frames 40.3 and 45
  • AIRBUS S.A.S.
    • A330
2002-11-09
F-2002-415R2
FR
 2002-11-09 SUPERSEDED BY EASA AD 2010-0193
  • AIRBUS S.A.S.
    • A340
2002-11-09
F-2001-359R3
FR
 2002-11-09 Emergency door 3 type I (LH & RH) - Escape slide parachute pin
  • AIRBUS S.A.S.
    • A330
2002-11-09
F-2002-531
FR
 2002-11-09 Wing inspection of rear spar between ribs 1 and 2
  • AIRBUS S.A.S.
    • A320
2002-11-09
US-2002-22-14
US
 2002-11-08 Main Rotor - Tension-Torsion Straps - Retirement (Life) Limit
  • BELL TEXTRON INC. (BTI)
    • 204B
    • 205
    • 212
  • McDermott 214 Holdings, LLC
    • 214
2002-12-13