AD 95-NM-230
Title: DEBONDING OF THE EDGES OF THE ACOUSTIC DAMPING FOILS\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 95-CE-62
Title: SEPARATION OF THE EXHAUST SYSTEM ENDPIPE FROM THE MUFFLER\HOAC AUSTRIA (FORMERLY HOFFMANN AIRCRAFT)\DV-20 'KATANA'
Organization: FAA
Status: Active
AD 95-NM-251
Title: EMERGENCY ELECTRICAL SYSTEM\BRITISH AEROSPACE\BAE-146-100A\BAE-146-200A\BAE-146-300A
Organization: FAA
Status: Active
AD 95-NM-167
Title: INADVERTENT DEPLOYMENT OF A THRUST REVERSER\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-1000A/HAWKER 1000
Organization: FAA
Status: Active
AD 95-NM-213
Title: STRUCTURAL INTEGRITY OF THE FUSELAGE\BRITISH AEROSPACE\AVRO 146-RJ70A\AVRO 146-RJ85A\AVRO 146-RJ100A
Organization: FAA
Status: Active
AD 95-NM-248
Title: BRAKE EFFECTIVENESS\LOCKHEED AIRCRFT CORP LOCKHEED-GEORGIA CO AND LOCKHEED-CALIF CO\382 SERIES
Organization: FAA
Status: Active
AD 95-NM-72
Title: LOSS OF HYDRAULIC SYSTEMS\DEHAVILLAND\DHC-8-100 SERIES\DHC-8-300
Organization: FAA
Status: Active
AD 95-CE-103
Title: STRUCTURAL FAILURE OF THE FUSELAGE AREA\AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD (FORMERLY GOVERNMENT AIRCRAFT FACTORIES)\N22B\N24A\N22S
Organization: FAA
Status: Active
AD 95-NM-247
Title: NOSE LANDING GEAR (NLG) DOOR\CANADAIR LTD\CL-600-2B16 (CL-601-3A)\CL-600-2B19
Organization: FAA
Status: Active
AD 95-NM-226
Title: FAILURE OF THE ESCAPE SLIDE TO DEPLOY\BOEING\747-100 SERIES\747-200 SERIES\747-300 SERIES
Organization: FAA
Status: Active
AD 95-NM-202
Title: STRUCTURAL CAPABILITY OF THE SKIN JOINT\GULFSTREAM AMERICAN & GULFSTREAM AEROSPACE\G-1159 SERIES (G-II)\G-1159A (G-III)\G-1159B SERIES (G-IIB)
Organization: FAA
Status: Active
AD 95-NM-106
Title: THE NUT OF THE FUEL CAP ASSEMBLY\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES\737 SERIES (T-43)
Organization: FAA
Status: Active
AD 95-NM-266
Title: INADVERTENT OPENING OF THE AIRSTAIR DOOR\DEHAVILLAND\DHC-8 SERIES
Organization: FAA
Status: Active
AD 95-NM-271
Title: FATIGUE-RELATED CRACKING IN THE REAR PRESSURE BULKHEAD\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 95-CE-21
Title: LANDING GEAR EMERGENCY EXTENSION AIR LINE\PIPER\PA-31T2
Organization: FAA
Status: Active
AD 95-ANE-57
Title: DEBRIS FROM THE TURBINE EXHAUST CASE (TEC)\PRATT & WHITNEY\JT9D-3\JT9D-7\JT9D-20\JT9D-59A\JT9D-70A\JT9D-7Q\JT9D-7R4\JT9D-7R4D\JT9D-7R4D1\JT9D-7R4E\JT9D-7R4E1\JT9D-7R4E4\JT9D-7R4G2\JT9D-7R4H1
Organization: FAA
Status: Active
AD 95-ANE-65
Title: STAGE 1 DISK OF THE HIGH PRESSURE COMPRESSOR ROTOR (HPCR)\CFM INTERNATIONAL\CFM 56-5
Organization: FAA
Status: Active
AD 95-CE-85
Title: FAILURE OF THE HINGE BRACKET ON THE HORIZONTAL STABILIZER\PILATUS AIRCRAFT LTD\PC-6
Organization: FAA
Status: Active
AD 95-CE-91
Title: VHF NAVIGATION RECEIVERS\ALLIED-SIGNAL AEROSPACE\VN-411B
Organization: FAA
Status: Active
AD 95-NM-166
Title: STRUCTURAL INTEGRITY OF THE ELEVATOR CONTROL CIRCUIT\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-1000A/HAWKER 1000
Organization: FAA
Status: Active
AD 95-NM-240
Title: AFT CORE COWL NOZZLE\LEARJET CORP\60
Organization: FAA
Status: Active
AD 95-CE-99
Title: INTERGRANULAR CORROSION\LUSCOMBE AIRCRAFT CORP (LARSEN) (SEE TEMCO FOR MODEL 11 SERIES)\8 SERIES
Organization: FAA
Status: Active
AD 95-NM-158
Title: STRUCTURAL INTEGRITY OF THE AIRPLANE\DEHAVILLAND\DHC-7 SERIES
Organization: FAA
Status: Active
AD 95-NM-264
Title: DISBONDING OF THE SKIN PANELS OF THE FUSELAGE\DEHAVILLAND\DHC-7 SERIES
Organization: FAA
Status: Active
AD 95-ANE-69-R2
Title: 14TH AND 15TH STAGE HPC DISK RUPTURE\PRATT & WHITNEY\JT9D-59A\JT9D-70A\JT9D-7Q\JT9D-7Q3\JT9D-7R4\JT9D-7R4D\JT9D-7R4D1\JT9D-7R4E\JT9D-7R4E1\JT9D-7R4E4\JT9D-7R4G2\JT9D-7R4H1
Organization: FAA
Status: Active
AD 95-CE-39
Title: RUDDER BEARING SUPPORT BRACKET\HB AIRCRAFT INDUSTRIES\HB-23/2400
Organization: FAA
Status: Active
AD 95-NM-165
Title: TKS METERING PUMP\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-800A/HAWKER 800\BAE 125-1000A/HAWKER 1000
Organization: FAA
Status: Active
AD 95-NM-241
Title: SLAT TRANSMISSION SYSTEM\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325
Organization: FAA
Status: Active
AD 95-CE-45
Title: PREVENT THE MAIN LANDING GEAR (MLG) FROM EXTENDING\PIPER\PA-31\PA-31-300\PA-31-325\PA-31-350\PA-31P\PA-31P-350\PA-31T\PA-31T1\PA-31T2\PA-31T3
Organization: FAA
Status: Active
AD 95-CE-56
Title: HYDRAULIC HOSE FAILURE\PIPER\PA-23\PA-23-160\PA-23-235\PA-23-250\PA-31\PA-31-300\PA-31-325\PA-31-350\PA-31P\PA-31P-350\PA-31T\PA-31T1\PA-31T2\PA-31T3\PA-42
Organization: FAA
Status: Active
AD 95-NM-263
Title: FATIGUE CRACKING\AIRBUS INDUSTRIE\A300-B2-1A\A300-B2-1C\A300-B2-203\A300-B4-103\A300-B4-203\A300-B4-2C\A300-B4-600R SERIES\A300-B4-620\A300-B4-622R\A300-B4-622
Organization: FAA
Status: Active
AD 95-CE-55
Title: LANDING GEAR SELECTOR CABLE FORWARD ATTACHMENT PIN ASSEMBLY\PIPER\PA-31\PA-31-325\PA-31-350\PA-31P\PA-31T
Organization: FAA
Status: Active
AD 95-CE-78
Title: EMERGENCY EXIT DOOR\INDUSTRIE AERONAUTICHE E MECCANICHE (SEE PIAGGIO)\P-180
Organization: FAA
Status: Active
AD 95-NM-109
Title: REDUCED STRUCTURAL INTEGRITY OF THE FUSELAGE, WING, AND VERTICAL STABILIZER\AIRBUS INDUSTRIE\A300-B2-1A\A300-B2-1C\A300-B2-203\A300-B4-103\A300-B4-203\A300-B4-2C\A300-B4-600R SERIES\A300-B4-620\A30...
Organization: FAA
Status: Active
AD 95-NM-175
Title: THRUST REVERSER\AIRBUS INDUSTRIE\A300-B4-103\A300-B4-203\A300-B4-2C\A300-B4-600R SERIES\A300-B4-620\A300-B4-622R\A300-B4-622\A310-200\A310-221\A310-222\A310-300
Organization: FAA
Status: Active
AD 95-NM-218
Title: DOOR 5 EVACUATION SLIDE/RAFT\BOEING\747-400 SERIES
Organization: FAA
Status: Active
AD 95-NM-237
Title: P-CLIPS\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233
Organization: FAA
Status: Active
AD 95-NM-267
Title: SHOCK ABSORBER SUB-ASSEMBLY\AIRBUS INDUSTRIE\A320-211\A320-212
Organization: FAA
Status: Active
AD 95-ANE-30
Title: PROPELLER HUB, BLADE, OR BLADE CLAMP FAILURE\HARTZELL PROPELLER INC\EHC-A3V SERIES\HC-B3T SERIES\HC-B4M SERIES\HC-B4T SERIES\HC-B5M SERIES\HARTZELL PROPELLER INC\EHC-A3V SERIES\HC-B3T SERIES\HC-B4M...
Organization: FAA
Status: Active
AD 95-NM-192
Title: WING RIB-TO-SKIN SUPPORT BRACKETS\EMPRESA BRASILEIRA DE AERONAUTICA S A\EMB-120 SERIES
Organization: FAA
Status: Active
AD 95-NM-211
Title: FAILURE OF THE PISTON ROD\MCDONNELL DOUGLAS CORPORATION\MD-11 SERIES
Organization: FAA
Status: Active
AD 95-NM-212
Title: INBOARD FLAP INBOARD TRACK\MCDONNELL DOUGLAS CORPORATION\DC-10-10\DC-10-10F\DC-10-15\DC-10-30\DC-10-30F (KC-10A)\DC-10-40\DC-10-40F\MD-11 SERIES
Organization: FAA
Status: Active
AD 95-NM-249
Title: PRESSURIZED FLOOR FITTING\AIRBUS INDUSTRIE\A320-111\A320-211\A320-231
Organization: FAA
Status: Active
AD 95-NM-268
Title: AIRSPEED LIMITATIONS PLACARD\DEHAVILLAND\DHC-8-301\DHC-8-311\DHC-8-315
Organization: FAA
Status: Active
AD 95-ANE-63
Title: ENGINE ELECTRICAL HARNESSES\CFM INTERNATIONAL\CFM 56-5
Organization: FAA
Status: Active
AD 95-CE-67
Title: WING SKIN AND REAR SPAR\SOCATA--GROUPE AEROSPATIALE (SEE MORANE-SAULNIER)\TBM 700
Organization: FAA
Status: Active
AD 95-NM-171
Title: BRAKE PISTONS\FOKKER-VFW B V\F.28 MARK 0070\F.28 MARK 0100
Organization: FAA
Status: Active
AD 95-NM-216
Title: STRUCTURAL INTEGRITY OF THE FUSELAGE\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233
Organization: FAA
Status: Active
AD 95-NM-221
Title: MAIN LANDING GEAR (MLG) PISTONS\MCDONNELL DOUGLAS CORPORATION\DC-9-81 (MD-81)\DC-9-82 (MD-82)\DC-9-83 (MD-83)\DC-9-87 (MD-87)\DC-9-80 (MD-80)\MD-88
Organization: FAA
Status: Active
AD 95-NM-228
Title: STRUCTURAL INTEGRITY OF THE AIRFRAME\AIRBUS INDUSTRIE\A300-600
Organization: FAA
Status: Active
AD 95-NM-253
Title: STRUCTURAL INTEGRITY OF THE AIRPLANE\FOKKER-VFW B V\F.27 MARK 100\F.27 MARK 200\F.27 MARK 300\F.27 MARK 400\F.27 MARK 500\F.27 MARK 600\F.27 MARK 700
Organization: FAA
Status: Active
AD 95-NM-255
Title: OUTFLOW/SAFETY VALVES\BEECH AIRCRAFT\400\400A\MU-300-10\2000\200 SERIES\B200\300 SERIES\B300
Organization: FAA
Status: Active
AD 95-SW-35
Title: ENGINE TURBINE\BELL HELICOPTER TEXTRON ***(SEE CA DEPT OF FORESTRY CONTNTL COPTERS GARLICK HAWKEYE ROTORWI\206L-1
Organization: FAA
Status: Active
AD 95-ANE-01
Title: PREVENT DISK FAILURE\TEXTRON LYCOMING (SEE AVCO)\AL-5512 SERIES
Organization: FAA
Status: Active
AD 95-ANE-64
Title: REMOVAL OF HIGH PRESSURE TURBINE ROTOR (HPTR) FRONT SHAFTS\CFM INTERNATIONAL\CFM 56-2
Organization: FAA
Status: Active
AD 95-ANE-68
Title: PREVENT AN HPT DISK RUPTURE\ALLIED-SIGNAL AEROSPACE\AUXILIARY POWER UNITS
Organization: FAA
Status: Active
AD 95-CE-84
Title: INBOARD AILERON HINGE BRACKET\PIPER\PA-31\PA-31-300\PA-31-325\PA-31-350\PA-31P-350\PA-31T3\PA-31P\PA-31T\PA-31T1\PA-31T2\PA-42\PA-42-720\PA-42-1000
Organization: FAA
Status: Active
AD 95-NM-151
Title: JUNCTION FITTING LUG OF THE HORIZONTAL STABILIZER\FOKKER-VFW B V\F.28 MARK 0070\F.28 MARK 1000\F.28 MARK 2000\F.28 MARK 3000\F.28 MARK 4000
Organization: FAA
Status: Active
AD 95-NM-152
Title: PREVENT INADVERTENT OPENING OF THE PASSENGER DOOR WHILE THE AIRPLANE IS IN FLIGHT\FOKKER-VFW B V\F.28 MARK 1000\F.28 MARK 2000\F.28 MARK 3000\F.28 MARK 4000
Organization: FAA
Status: Active
AD 95-NM-170
Title: ELEVATOR GUST LOCK HOUSING\FOKKER-VFW B V\F.28 MARK 0070\F.28 MARK 1000\F.28 MARK 2000\F.28 MARK 3000\F.28 MARK 4000
Organization: FAA
Status: Active
AD 95-NM-204
Title: PREVENT FATIGUE CRACKING\MCDONNELL DOUGLAS CORPORATION\DC-10-10\DC-10-10F\DC-10-15
Organization: FAA
Status: Active
AD 95-NM-208
Title: SLIDING WINDOW FRAMES\AIRBUS INDUSTRIE\A320-111\A320-211\A320-231
Organization: FAA
Status: Active
AD 95-NM-222
Title: PREVENT AN AIRPLANE FROM LANDING WITH ONE MAIN LANDING GEAR (MLG) PARTIALLY EXTENDED\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES
Organization: FAA
Status: Active
AD 95-NM-231
Title: BUS POWER CONTROL UNITS\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 95-NM-252
Title: FLIGHTCREW OXYGEN SYSTEM\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 95-ANE-19
Title: REMOVAL OF FAN DISKS\GENERAL ELECTRIC CO\CF34
Organization: FAA
Status: Active
AD 95-ANE-55
Title: PREVENT UNCONTAINED FAILURE OF THE FAN ROTOR DISK DUE TO FATIGUE CRACKING IN THE DOVETAIL SLOTS\ALLIEDSIGNAL\TFE 731-2\TFE 731-2A\TFE 731-3\TFE 731-3A\TFE 731-3AR\TFE 731-3B\TFE 731-3BR\TFE 731-3C\...
Organization: FAA
Status: Active
AD 95-CE-44
Title: CRACKS IN THE PINTLE TO CYLINDER INTERFACE AREA\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\HP 137 MK.1\JETSTREAM SERIES 200\JETSTREAM MODEL 3101\JETSTREAM MODEL 3201
Organization: FAA
Status: Active
AD 95-CE-75
Title: TAILPLANE STABILIZER CENTER SECTION\AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD (FORMERLY GOVERNMENT AIRCRAFT FACTORIES)\N22B\N22S\N24A
Organization: FAA
Status: Active
AD 95-CE-94
Title: FAILURE OF NOSE LANDING GEAR (NLG)\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\HP 137 MK.1\JETSTREAM SERIES 200\JETSTREAM MODEL 3101\JETSTREAM MODEL 3201
Organization: FAA
Status: Active
AD 95-NM-199
Title: FATIGUE CRACKING IN THE SECONDARY PIVOT SUPPORT OF THE HORIZONTAL STABILIZER\MCDONNELL DOUGLAS CORPORATION\DC-10-10\DC-10-10F\DC-10-15\DC-10-30\DC-10-30F (KC-10A)\DC-10-40\DC-10-40F
Organization: FAA
Status: Active
AD 95-NM-203
Title: ROTARY ACTUATOR MOTORS\BOEING\767-200 SERIES\767-300 SERIES\767-300F SERIES
Organization: FAA
Status: Active
AD 95-NM-234
Title: ENGINE-DRIVEN GENERATOR\MCDONNELL DOUGLAS CORPORATION\MD-11 SERIES\DC-10-10\DC-10-10F\DC-10-15\DC-10-30\DC-10-30F (KC-10A)\DC-10-40\DC-10-40F
Organization: FAA
Status: Active
AD 95-NM-243
Title: PREVENT THE MOVEMENT OF BOTH POWER LEVERS AFT OF THE FLIGHT IDLE STOP DURING FLIGHT\SAAB-SCANIA AB\SF-340A\SAAB 340B SERIES
Organization: FAA
Status: Active
AD 95-NM-254
Title: PREVENT COLLAPSE OF THE NOSE LANDING GEAR\MCDONNELL DOUGLAS CORPORATION\DC-10-10\DC-10-10F\DC-10-15\DC-10-30\DC-10-30F (KC-10A)\DC-10-40\DC-10-40F\MD-11 SERIES
Organization: FAA
Status: Active
AD 95-CE-83
Title: COMBUSTION HEATERS\JANITROL AERO DIVISION (MIDLAND-ROSS CORP )\COMBUSTION HEATERS B1500\COMBUSTION HEATERS B2030\COMBUSTION HEATERS B3040\COMBUSTION HEATERS B4050
Organization: FAA
Status: Active
AD 95-CE-93
Title: FLAP AND AILERON CONTROL ROD FORK ENDS\AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD (FORMERLY GOVERNMENT AIRCRAFT FACTORIES)\N22B\N22S\N24A
Organization: FAA
Status: Active
AD 95-NM-150
Title: PREVENT FATIGUE-RELATED CRACKING\AIRBUS INDUSTRIE\A300-600
Organization: FAA
Status: Active
AD 95-NM-160
Title: CORROSION OF THE ANTENNA MOUNTING PLATES\BRITISH AEROSPACE\ATP SERIES
Organization: FAA
Status: Active
AD 95-NM-180
Title: LOSS OF FLIGHT CONTROLS\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-1000A/HAWKER 1000
Organization: FAA
Status: Active
AD 95-NM-197
Title: ELECTRICAL ARCING\LEARJET CORP\31\35A
Organization: FAA
Status: Active
AD 95-NM-198
Title: PREVENT COLLAPSE OF THE MAIN LANDING GEAR (MLG)\AIRBUS INDUSTRIE\A320-111\A320-211\A320-212\A320-231
Organization: FAA
Status: Active
AD 95-NM-256
Title: FAILURE OF THE OUTFLOW/SAFETY VALVES\INDUSTRIE AERONAUTICHE E MECCANICHE (SEE PIAGGIO)\P-180
Organization: FAA
Status: Active
AD 95-NM-161
Title: STRESS CORROSION CRACKING IN THE LONGITUDINAL LAP JOINTS OF THE FUSELAGE\AIRBUS INDUSTRIE\A300-B2-1A\A300-B2-1C\A300-B2-203\A300-B4-103\A300-B4-203\A300-B4-2C\A300-B4-600R SERIES\A300-B4-620\A300-B...
Organization: FAA
Status: Active
AD 95-CE-18
Title: ICING CONDITIONS\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 3101\JETSTREAM MODEL 3201
Organization: FAA
Status: Active
AD 95-NM-191
Title: CABIN SIDEWALL VENT BOX DIAPHRAGMS\MCDONNELL DOUGLAS CORPORATION\MD-11 SERIES
Organization: FAA
Status: Active
AD 95-NM-59
Title: STRUCTURAL INTEGRITY OF THE HORIZONTAL STABILIZER\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 95-NM-122
Title: PREVENT RESTRICTED CONTROL OF THE AILERONS\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-800A/HAWKER 800
Organization: FAA
Status: Active
AD 95-NM-188
Title: OXYGEN MASK LANYARDS\MCDONNELL DOUGLAS CORPORATION\DC-9-80\DC-9-81\DC-9-82\DC-9-83\DC-9-87\(MD-80) SERIES\MD-88\MD-90-30
Organization: FAA
Status: Active
AD 95-NM-224
Title: BRAKES\FOKKER-VFW B V\F.28 MARK 0070\F.28 MARK 0100
Organization: FAA
Status: Active
AD 95-CE-89
Title: PREVENT STRUCTURAL DAMAGE TO CABIN\BEECH AIRCRAFT\58P\58PA
Organization: FAA
Status: Active
AD 95-NM-121
Title: DEFORMATION OF THE NOSE RIB\SAAB-SCANIA AB\SF-340A\SAAB 340B SERIES
Organization: FAA
Status: Active
AD 95-NM-93
Title: OVERHEAD STORAGE HINGE BOLTS\BOEING\747-100 SERIES\747-200 SERIES\747-300 SERIES
Organization: FAA
Status: Active
AD 95-NM-110
Title: EMERGENCY LIGHTING SYSTEM\DEHAVILLAND\DHC-7 SERIES
Organization: FAA
Status: Active
AD 95-CE-79
Title: SPIGOT HOUSING ASSEMBLY\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\HP 137 MK.1\JETSTREAM SERIES 200\JETSTREAM MODEL 3101
Organization: FAA
Status: Active
AD 95-NM-145
Title: PREVENT FATIGUE CRACKING\MCDONNELL DOUGLAS CORPORATION\DC-9-10\DC-9-11\DC-9-12\DC-9-13\DC-9-14\DC-9-15\DC-9-15F\DC-9-21\DC-9-31\DC-9-32 (VC-9C)\DC-9-32F (C-9A, C-9B)\DC-9-33F\DC-9-34\DC-9-34F\DC-9-...
Organization: FAA
Status: Active
AD 95-NM-164
Title: STRUCTURAL INTEGRITY OF THE CARGO DOOR\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 95-NM-233
Title: LAVATORY WASTE RECEPTACLES\TRANSPORT CATEGORY AIRCRAFT\LAVATORY RECEPTACLES
Organization: FAA
Status: Active
AD 95-CE-54
Title: FAILURE OF THE NOSE LANDING GEAR (NLG)\BELLANCA INC MINNESOTA (SEE AERONCA F R A ENTERPRISES)\17-30\17-30A\17-31\17-31A\17-31TC\17-31ATC
Organization: FAA
Status: Active
AD 95-NM-22
Title: AUTOLAND SYSTEM\BOEING\747-100 SERIES\747-200 SERIES\747-300 SERIES\747SP
Organization: FAA
Status: Active
AD 95-NM-154
Title: PREVENT FUEL LEAKAGE AND POSSIBLE ENGINE FIRE\BOEING\767-200 SERIES\767-300 SERIES\767-300F SERIES
Organization: FAA
Status: Active
AD 95-NM-162
Title: PREVENT CHAFING OF THE FUEL LINE\BOEING\747-200 SERIES\747-300 SERIES\747-400 SERIES
Organization: FAA
Status: Active
AD 95-SW-32
Title: PILOT MISMANAGEMENT OF THE MAIN ROTOR (M/R) RPM\ROBINSON HELICOPTER COMPANY\R-44
Organization: FAA
Status: Active
AD 95-NM-146
Title: ICING CONDITIONS\AEROSPATIALE\ATR42 SERIES\ATR72 SERIES
Organization: FAA
Status: Active
AD 95-ANE-16
Title: POWER TURBINE ROTOR\ALLIEDSIGNAL\LTS101\LTP101
Organization: FAA
Status: Active
AD 95-ANE-12
Title: PREVENT A FUEL CONTROL FAILURE\ALLIEDSIGNAL\LTS101-600A-2\LTS101-600A-3
Organization: FAA
Status: Active
AD 95-ANE-66
Title: FAILURE OF CRITICAL COMPONENTS\HAMILTON STANDARD\14RF\14SF\6/5500/F-1
Organization: FAA
Status: Active
AD 95-ANE-03
Title: PREVENT PROPELLER BLADE TIP FATIGUE FAILURE\SENSENICH CORP\M76EMM\M7EMMS\76EM8\76EM8S()
Organization: FAA
Status: Active
AD 95-CE-61
Title: AIR FILTER GASKET FAILURE\BRACKETT AIRCRAFT SPECIALTIES INC\AIR FILTERS
Organization: FAA
Status: Active
AD 95-ANE-47
Title: FAN BLADE\CFM INTERNATIONAL\CFM 56-3
Organization: FAA
Status: Active
AD 95-ANE-45
Title: STEEL HIGH PRESSURE COMPRESSOR (HPC) DISK\PRATT & WHITNEY\TURBO WASP JT3D SERIES
Organization: FAA
Status: Active
AD 95-ANE-44
Title: FAILURE OF THE FAN DISK\CFM INTERNATIONAL\CFM 56-3
Organization: FAA
Status: Active
AD 95-ANE-41
Title: HPC STAGE 1 ROTOR DISK\GENERAL ELECTRIC CO\CF34
Organization: FAA
Status: Active
AD 95-ANE-37
Title: HIGH PRESSURE TURBINE (HPT) OR LOW PRESSURE TURBINE (LPT) FAILURE\PRATT & WHITNEY\PW2037
Organization: FAA
Status: Active
AD 95-SW-30
Title: PREVENT MAIN ROTOR (M/R) STALL OR MAST BUMPING\ROBINSON HELICOPTER COMPANY\R-44
Organization: FAA
Status: Active
AD 95-SW-29
Title: PREVENT MAIN ROTOR (M/R) STALL OR MAST BUMPING\ROBINSON HELICOPTER COMPANY\R-22 SERIES
Organization: FAA
Status: Active
AD 95-SW-27
Title: LOW-ROTOR RPM CAUTION LIGHT\ROBINSON HELICOPTER COMPANY\R-22 SERIES
Organization: FAA
Status: Active
AD 95-SW-26
Title: STRUCTURAL FAILURE OF TAILBOOM ASSEMBLY\BELL HELICPTR TEXTRON ***(SEE CA DEPT OF FORESTRY CONTNTL COPTERS GARLICK HAWKEYE ROTORWI\214ST
Organization: FAA
Status: Active
AD 95-SW-23
Title: PREVENT FAILURE OF THE SHEAVE\ROBINSON HELICOPTER COMPANY\R-22 SERIES
Organization: FAA
Status: Active
AD 95-SW-19
Title: PREVENT FAILURE OF THE HARDPOINT ASSEMBLY\MCDONNELL DOUGLAS HELICPTR (SEE SCHWEIZER AIRCRFT CORP )\369D\369E\369F\369FF\500N
Organization: FAA
Status: Active
AD 95-SW-14
Title: TESTING OF THE TANDEM HYDRAULIC SYSTEM\EUROCOPTER DEUTSCHLAND (FORMERLY MESSERSCHMITT-BOLKOW-BLOHM-GMBH)\BO-105\BO-105A\BO-105C SERIES\BO-105S SERIES\BO-105LS A-1
Organization: FAA
Status: Active
AD 95-SW-04
Title: CYCLIC PITCH CHANGE CONTROL ROD\EUROCOPTER FRANCE (FORMERLY AEROSPATIALE)\AS350B\AS350BA\AS350B1\AS350B2\AS350D\AS355E\AS355F\AS355F1\AS355F2\AS355N
Organization: FAA
Status: Active
AD 95-SW-01
Title: LEFT AND RIGHT FORWARD PASSENGER DOOR JETTISON SYSTEMS\EUROCOPTER FRANCE (FORMERLY AEROSPATIALE)\SA365N\SA365N1\SA365N2
Organization: FAA
Status: Active
AD 95-NM-56
Title: PREVENT CRACKING AND SUBSEQUENT FAILURE OF THE OUTFLOW/SAFETY VALVES\CESSNA\441\500\550\560
Organization: FAA
Status: Active
AD 95-CE-82
Title: FAILURE OF THE OPTIONAL BEECH ELECTRIC TRIM SYSTEM OR THE COLLINS AUTOPILOT SYSTEM\BEECH AIRCRAFT\C90A
Organization: FAA
Status: Active
AD 95-CE-51
Title: LANDING LIGHT SEAL\PIPER\PA-28-140\OPA-28-150\PA-28-160\PA-28-180
Organization: FAA
Status: Active
AD 95-CE-35
Title: PREVENT WATER IN THE FUEL TANKS\PIPER\PA-23\PA-23-150\PA-23-160\PA-23-235\PA-23-250
Organization: FAA
Status: Active
AD 95-CE-30
Title: ELEVATOR CONTROL SYSTEM\HB AIRCRAFT INDUSTRIES\HB-23/2400
Organization: FAA
Status: Active
AD 95-NM-275
Title: STRUCTURAL INTEGRITY OF THE FUSELAGE, HORIZONTAL STABILIZER, AND WINGS\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325
Organization: FAA
Status: Active
AD 95-NM-84
Title: ATTACHMENT CLIPS\AEROSPATIALE\ATR42 SERIES\ATR72 SERIES
Organization: FAA
Status: Active
AD 95-NM-172
Title: WING COLLECTOR TANKS\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 95-NM-155
Title: NOSE COWL\BOEING\737-200 SERIES (T-43)\737-200C SERIES (T-43)
Organization: FAA
Status: Active
AD 95-NM-141
Title: HYDRAULIC PIPE\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-1000A/HAWKER 1000
Organization: FAA
Status: Active
AD 95-NM-137
Title: PREVENT AN OUT-OF-TRIM CONDITION BETWEEN THE TRIMMABLE HORIZONTAL STABILIZER AND THE ELEVATOR\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325\A300-600
Organization: FAA
Status: Active
AD 95-NM-133
Title: HEAT DAMAGE AND MOISTURE CONTAMINATION TO THE FLEXIBLE CABLE\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPC )\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 95-NM-127
Title: PREVENT AUTOMATIC THRUST LEVER ADVANCE ON A SURGING ENGINE DURING TAKEOFF\MCDONNELL DOUGLAS CORP\DC-9-80\MD-88
Organization: FAA
Status: Active
AD 95-NM-124
Title: CONTROL RODS OF THE OUTBOARD LEADING EDGE SLAT OF THE WINGS\BOEING\767-200 SERIES\767-300 SERIES\767-300F SERIES
Organization: FAA
Status: Active
AD 95-NM-120
Title: LEAKAGE OF THE LAVATORY DRAIN SYSTEM\MCDONNELL DOUGLAS CORP\DC-10-10F\DC-10-10\DC-10-15\DC-10-30F (KC-10A)\DC-10-30\DC-10-40F\DC-10-40\MD-11F SERIES
Organization: FAA
Status: Active
AD 95-NM-118
Title: PREVENT FAILURE OF THE HORIZONTAL STABILIZER PRIMARY TRIM MOTOR\MCDONNELL DOUGLAS CORP\DC-9-80
Organization: FAA
Status: Active
AD 95-NM-117
Title: ELECTRICAL/ELECTRONICS (E/E) EQUIPMENT BAY\BOEING\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 95-NM-111
Title: LEAKAGE OF THE LAVATORY DRAIN SYSTEM OR FLUSH/FILL SYSTEMS\BOEING\737-100 SERIES\737-200 SERIES (T-43)\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 95-NM-108
Title: PYLON TRUSS FITTING\MCDONNELL DOUGLAS CORP\DC-10-10\DC-10-15\DC-10-30\DC-10-30F (KC-10A)
Organization: FAA
Status: Active
AD 95-NM-99
Title: MAIN LANDING GEAR (MLG) DOWNLOCK ACTUATOR\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 95-NM-98
Title: PREVENT FRACTURING OF THE COUPLING NUT\BOEING\747-400 SERIES
Organization: FAA
Status: Active
AD 95-NM-91
Title: INTEGRITY OF THE MAIN LANDING GEAR (MLG)\MCDONNELL DOUGLAS CORP\DC-9-80\DC-9-81\DC-9-82\DC-9-83\DC-9-87\(MD-80) SERIES\MD-88
Organization: FAA
Status: Active
AD 95-NM-90
Title: UPPER SAFETY LOCKING PIN ON THE PASSENGER DOOR\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233
Organization: FAA
Status: Active
AD 95-NM-89
Title: FIRE WALL\AIRBUS INDUSTRIE\A320-231
Organization: FAA
Status: Active
AD 95-NM-87
Title: MAIN LANDING GEAR (MLG) DOWNLOCK-ACTUATORS\FOKKER-VFW B V\F.28 MARK 0100\F.28 MARK 1000\F.28 MARK 2000\F.28 MARK 3000\F.28 MARK 4000
Organization: FAA
Status: Active
AD 95-NM-83
Title: EMERGENCY EVACUATION SLIDE RAFTS\BOEING\747SP
Organization: FAA
Status: Active
AD 95-NM-79
Title: PROP BRAKE WARNING SYSTEM\SAAB-SCANIA AB\SF-340A\SAAB 340B SERIES
Organization: FAA
Status: Active
AD 95-NM-78
Title: PREVENT REDUCED STRUCTURAL INTEGRITY OF THE HORIZONTAL STABILIZER CUTOUT LONGERON\AIRBUS INDUSTRIE\A300-600
Organization: FAA
Status: Active
AD 95-NM-77
Title: BRAKING/STEERING CONTROL UNIT (BSCU) SYSTEMS\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233
Organization: FAA
Status: Active
AD 95-NM-76
Title: STANDBY INSTRUMENT LIGHTING SYSTEM\BEECH AIRCRAFT\400
Organization: FAA
Status: Active
AD 95-NM-75
Title: PREVENT REDUCED CONTROLABILITY OF THE AIRPLANE AFTER TAKEOFF\BEECH AIRCRAFT\400A
Organization: FAA
Status: Active
AD 95-NM-71
Title: INSPECT OVERWING FAIRINGS\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPC )\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 95-NM-70
Title: PREVENT ELECTRICAL ARCING AND SUBSEQUENT LOSS OF THE ASSOCIATED ELECTRICAL SYSTEM\FOKKER-VFW B V\F.27 MARK 050\F.28 MARK 0100
Organization: FAA
Status: Active
AD 95-NM-58
Title: ENSURE STRUCTURAL INTEGRITY OF THE HORIZONTAL STABILIZER\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 95-NM-53
Title: PREVENT THE INABILITY TO SHUT OFF THE SUPPLY OF FUEL IN THE EVENT OF AN ENGINE FIRE\BOEING\747-400 SERIES
Organization: FAA
Status: Active
AD 95-NM-47
Title: PREVENT REDUCED STRUCTURAL INTEGRITY OF THE WING\MCDONNELL DOUGLAS CORP\DC-10-10\DC-10-15\DC-10-30\DC-10-40
Organization: FAA
Status: Active
AD 95-NM-43
Title: INCORRECT FAULT DISPLAYS IN THE COCKPIT\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-800A/HAWKER 800\BAE 125-1000A/HAWKER 1000
Organization: FAA
Status: Active
AD 95-CE-47
Title: TAILPLANE MAIN RIB FORWARD FLANGES\DEHAVILLAND\DHC-3 (U-1A) (OTTER)
Organization: FAA
Status: Active
AD 95-CE-40
Title: PREVENT FAILURE OF THE FLIGHT CONTROL SYSTEM\FAIRCHILD AIRCRFT CORP\SA226-T\SA226-T(B)\SA226-AT\SA226-TC\SA227-TT\SA227-AT\SA227-AC
Organization: FAA
Status: Active
AD 95-CE-32
Title: PREVENT MAIN LANDING GEAR COLLAPSE\BEECH AIRCRAFT\200 (A100-1) (RU-21J)\200C\200T\A200 (C-12A) (C-12C)\F90\99\99A\A99A\B99\C99\100\A100\B100\200 SERIES\B200\200T\B200T\200C\B200C\200CT\B200CT\65-A9...
Organization: FAA
Status: Active
AD 95-CE-26
Title: FORWARD LOWER EDGE WING SKIN STRUCTURE\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPC )\JETSTREAM MODEL 3201
Organization: FAA
Status: Active
AD 95-CE-13
Title: LEFT HAND (LH) AND RIGHT HAND (RH) ESSENTIAL BUS\FAIRCHILD AIRCRFT CORP\SA226-T\SA226-AT\SA226-TC\SA226-T(B)\SA227-AC\SA227-AT\SA227-BC\SA227-TT\SA227-CC\SA227-DC
Organization: FAA
Status: Active
AD 95-CE-10
Title: FAILURE OF THE NOSE LANDING GEAR (NLG)\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPC )\JETSTREAM MODEL 3201\JETSTREAM MODEL 3101\JETSTREAM SERIES 200\HP 137 MK.1
Organization: FAA
Status: Active
AD 95-NM-142
Title: AUXILIARY POWER UNIT (APU)\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-800A/HAWKER 800
Organization: FAA
Status: Active
AD 95-NM-177
Title: OVERFREQUENCY CONDITION OF THE GENERATOR\MCDONNELL DOUGLAS CORPORATION\DC-10-10\DC-10-10F\DC-10-15\DC-10-30\DC-10-30F (KC-10A)\DC-10-40\DC-10-40F
Organization: FAA
Status: Active
AD 95-NM-136
Title: RUDDER DAMPER\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-CE-69-1
Title: DETECT AND CORRECT CRACKED MAIN LANDING GEAR (MLG) INBOARD DOOR HINGE ASSEMBLIES\PIPER\PA-31\PA-31-300\PA-31-325\PA-31-350\PA-31P\PA-31P-350\PA-31T\PA-31T1\PA-31T2\PA-31T3
Organization: FAA
Status: Active
AD 96-NM-92-A
Title: PREVENT THE LOSS OF THE ESCAPE SLIDES DURING FLIGHT\AIRBUS INDUSTRIE\A319-131\A319-132\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233
Organization: FAA
Status: Active
AD 96-NM-194-A
Title: PREVENT INADVERTENT AND UNCOMMANDED RUDDER TRIM ACTIVATION\AIRBUS INDUSTRIE\A300-600\A310-200\A310-200ADV\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325
Organization: FAA
Status: Active
AD 96-NM-226
Title: PREVENT INADEQUATE LIGHTING AND CUEING OF THE EMERGENCY FLOOR PATH LIGHTING SYSTEM\BOEING\737-200 SERIES (T-43)
Organization: FAA
Status: Active
AD 96-NM-110-A
Title: PREVENT FAILURE OF THE PILOT'S CONTROL CABLES FOR THE AUTOPILOT, ELEVATOR, RUDDER, AILERON, AND ENGINE\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-NM-214-A
Title: PREVENT FATIGUE CRACKING IN THE STRUCTURE THAT ATTACHES THE FLAP NACELLE FAIRING TO THE WING FLAPS\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPC )\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 96-NM-66
Title: PREVENT CONTAMINATION OF THE ENGINE ACCESSORY GEARBOX OIL WITH HYDRAULIC FLUID\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325\A300-600
Organization: FAA
Status: Active
AD 96-ANE-02-A
Title: PREVENT FAN BLADE FAILURE\PRATT & WHITNEY\JT8D-209\JT8D-217\JT8D-217A\JT8D-217C\JT8D-219
Organization: FAA
Status: Active
AD 96-ANE-36
Title: PREVENT A STAGE 4 LOW PRESSURE TURBINE (LPT) ROTOR FAILURE\TEXTRON LYCOMING (SEE AVCO)\ALF-502 SERIES\LF507 SERIES
Organization: FAA
Status: Active
AD 96-CE-60-A
Title: PREVENT MOISTURE FROM ACCUMULATING AND FREEZING IN THE AIRSTAIR DOOR HANDLE AND LATCH HOUSING\BEECH AIRCRFT\1900\1900C (C-12J)\1900D
Organization: FAA
Status: Active
AD 96-NM-227
Title: PREVENT FAILURE OF THE ATTACHMENT BOLTS ON THE FORWARD AND AFT FLANGES OF THE NO. 4 BANJO FITTING AND THE PYLON CARRY-THROUGH CAP DUE TO FATIGUE CRACKING\MCDONNELL DOUGLAS CORP\MD-11 SERIES
Organization: FAA
Status: Active
AD 96-NM-113-R1
Title: PREVENT REDUCED STRUCTURAL INTEGRITY OF THE LOWER PART OF THE MAIN LANDING GEAR (MLG) FAIRING\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-CE-23-R1
Title: TO PREVENT POSSIBLE IN-FLIGHT SEPARATION OF THE WING FROM THE AIRPLANE CAUSED BY A CRACKED AFT LOWER FUSELAGE WING ATTACH FITTING\WHITE INTNL LTD (FORMERLY AVIAT FORMERLY CHRISTEN IND )\S-1S\S-1T\S...
Organization: FAA
Status: Active
AD 96-CE-09-R1
Title: PREVENT MAIN LANDING GEAR (MLG) COLLAPSE CAUSED BY MAIN GEAR SIDEBRACE STUD CRACKS\PIPER\PA-24\PA-24-250\PA-24-260\PA-24-400\PA-30\PA-39\PA-28R-180\PA-28R-200\PA-28R-201\PA-28R-201T\PA-32R-300\PA-3...
Organization: FAA
Status: Active
AD 96-NM-171-R1
Title: R1 LOSS OF CONTROL OF THE CABIN PRESSURIZATION SYSTEM\BOEING\747-400 SERIES\747-400D\747-400F
Organization: FAA
Status: Active
AD 96-NM-103
Title: TRICKLING OF WATER INTO THE AVIONICS COMPARTMENT\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233
Organization: FAA
Status: Active
AD 96-NM-248
Title: FATIGUE CRACKING AND CORROSION AROUND AND UNDER CHAFING PLATES OF THE WING ROOT BETWEEN FUSELAGE FRAMES (FR) 36 AND FR 39\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310...
Organization: FAA
Status: Active
AD 96-NM-194-R1
Title: INADVERTENT AND UNCOMMANDED RUDDER TRIM ACTIVATION\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325\A300-600
Organization: FAA
Status: Active
AD 96-NM-186
Title: FATIGUE CRACKING IN THE LAPJOINT BELOW THE CHINE LINE AT CERTAIN FUSELAGE STATIONS\FOKKER-VFW B V\F.27 MARK 100\F.27 MARK 200\F.27 MARK 300\F.27 MARK 400\F.27 MARK 500\F.27 MARK 600\F.27 MARK 700
Organization: FAA
Status: Active
AD 96-SW-22
Title: DETECT CRACKS THAT REDUCE THE STRENGTH OF THE MAIN GEARBOX STRUT ATTACHMENT AND COULD RESULT IN FAILURE OF THE MAIN GEARBOX MOUNTING, AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER\EUROCOPTER FRA...
Organization: FAA
Status: Active
AD 96-NM-184
Title: DETECT AND CORRECT REDUCED STRUCTURAL INTEGRITY OF THE WING-FUSELAGE SUPPORT AND FUSELAGE PRESSURE VESSEL RESULTING FROM STRUCTURAL FATIGUE CRACKING IN THE TRANSITION AND PICK-UP ANGLES\AIRBUS INDU...
Organization: FAA
Status: Active
AD 96-NM-232
Title: PREVENT INABILITY TO OPEN THE NUMBER 1, 2, OR 4 PASSENGER DOOR AND TO USE THE ESCAPE SLIDE AT THAT DOOR DURING AN EMERGENCY EVACUATION OF THE AIRPLANE\BOEING\757-200 SERIES
Organization: FAA
Status: Active
AD 96-NM-12-R1
Title: PREVENT THE FAILURE OF THE ACTUATORS USED TO DEPLOY THE RAM AIR TURBINE (RAT)\BOEING\757-200 SERIES\757-200CB SERIES\757-200PF SERIES
Organization: FAA
Status: Active
AD 96-NM-187
Title: PREVENT FAILURE OF THE THRUST REVERSER CONTROL CABLES\BRITISH AEROSPACE\1-11 200 SERIES\1-11 400 SERIES
Organization: FAA
Status: Active
AD 96-NM-189
Title: FAILURE OF THE TORQUE TUBES\BRITISH AEROSPACE\ATP SERIES
Organization: FAA
Status: Active
AD 96-NM-274
Title: LEAKS IN HIGH PRESSURE OXYGEN HOSE ASSEMBLIES\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\DH 125-400A\BH 125-400A\BH.125-600A\HS.125-600A\HS.125-700A\BAE 125-800A/HAWKER 800\HA...
Organization: FAA
Status: Active
AD 96-NM-230
Title: FATIGUE CRACKING AT THE JUNCTION OF THE BAGGAGE FLOOR AND FRAME 35\DASSAULT AVIATION PARIS FRANCE (SEE AVIONS MARCEL DASSAULT A M D )\MYSTERE-FALCON 50
Organization: FAA
Status: Active
AD 96-NM-59
Title: BEARING FAILURE\LOCKHEED AIRCRAFT CORP LOCKHEED-GEORGIA COMPANY AND LOCKHEED-CALIFORNIA COMPANY\L-1011 SERIES
Organization: FAA
Status: Active
AD 96-NM-220
Title: DAMAGE TO THE HYDRAULIC TUBES AND ELECTRICAL HARNESSES\SAAB-SCANIA AB\2000
Organization: FAA
Status: Active
AD 96-NM-119
Title: STRUCTURAL DAMAGE TO THE HORIZONTAL OR VERTICAL STABILIZER\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-CE-25-A
Title: FAILURE OF THE MAIN LANDING GEAR\PILATUS BRITTEN-NORMAN LTD (SEE BRITTEN-NORMAN)\BN-2\BN-2A\BN-2A-3\BN-2A-6\BN-2A-8\BN-2A-2\BN-2A-9\BN-2A-20\BN-2A-21\BN-2A-26\BN-2A-27\BN-2B-20\BN-2B-21\BN-2B-26\BN...
Organization: FAA
Status: Active
AD 96-NM-211
Title: FAILURE OF THE MAIN LANDING GEAR\SAAB-SCANIA AB\2000
Organization: FAA
Status: Active
AD 96-NM-229
Title: AUXILIARY POWER UNIT (APU) FAILURE\SAAB-SCANIA AB\2000
Organization: FAA
Status: Active
AD 96-CE-58
Title: ASYMMETRICAL FLAP DEFLECTION\FAIRCHILD AIRCRAFT CORPORATION\SA226-TC\SA226-T\SA226-T(B)\SA226-AT
Organization: FAA
Status: Active
AD 96-NM-206
Title: ENSURE THAT A WASHER BETWEEN THE BOLT HEAD AND BUSHING IS INSTALLED IN THE RESTRAINT ANCHOR CONFIGURATION OF THE DOUBLE FLIGHT ATTENDANTS SEATS THAT ARE WALL MOUNTED\BOEING\767-200 SERIES\767-300 S...
Organization: FAA
Status: Active
AD 96-NM-263
Title: CONTINUED STRUCTURAL INTEGRITY OF THE TOTAL BOEING MODEL 727 FLEET\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES
Organization: FAA
Status: Active
AD 96-NM-213
Title: SHORT CIRCUITING BETWEEN THE FLOORMAT HEATER AND THE FLOOR PANEL\SAAB-SCANIA AB\2000
Organization: FAA
Status: Active
AD 96-CE-68
Title: FAILURE OF THE CARGO DOOR IN FLIGHT WHICH COULD CAUSE DECOMPRESSION INJURIES TO PASSENGERS AND SUBSTANTIAL STRUCTURAL DAMAGE TO THE AIRPLANE\FAIRCHILD AIRCRAFT CORPORATION\SA226-AT\SA226-TC\SA227-A...
Organization: FAA
Status: Active
AD 96-NM-271
Title: PREVENTION OF DIRECT CURRENT (DC) POWER DISTRIBUTION SYSTEM FROM SHORT CIRCUITING\BOMBARDIER INC (FORMERLY CANADAIR LTD)\CL-600-2B19
Organization: FAA
Status: Active
AD 96-NM-174
Title: CORROSION IN THE REAR CARGO DOOR\FOKKER-VFW B V\F.28 MARK 1000\F.28 MARK 2000\F.28 MARK 3000\F.28 MARK 4000
Organization: FAA
Status: Active
AD 96-CE-54
Title: THE NOSE LANDING GEAR (NLG)\TWIN COMMANDER AIRCRAFT CORP (FORMERLY GULFSTREAM)\500-S\500-U\680-F\680-V\690\690-A\690-B\690-C\690-D\695\695-A
Organization: FAA
Status: Active
AD 96-NM-256
Title: FRETTING AT THE DIAGONAL TRUSS TO WEB JOINT OF THE ELEVATOR, AND CRACKING IN THE CAP FILLET RADIUS ADJACENT TO THE JOINT\LOCKHEED AIRCRAFT CORP LOCKHEED-GEORGIA COMPANY AND LOCKHEED-CALIFORNIA COMP...
Organization: FAA
Status: Active
AD 96-NM-214
Title: FATIGUE CRACKING IN THE STRUCTURE\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 96-NM-212
Title: UNCOMMANDED MOVEMENT OF THE RIGHT-HAND ELEVATOR TRIM-TAB TO A MAXIMUM DEFLECTION POSITION\SAAB-SCANIA AB\SF-340A
Organization: FAA
Status: Active
AD 96-NM-167
Title: FALSE FIRE WARNING INPUTS OF THE ENGINES AND AUXILIARY POWER UNIT (APU)\SAAB-SCANIA AB\2000
Organization: FAA
Status: Active
AD 96-NM-170
Title: FATIGUE CRACKING\AIRBUS INDUSTRIE\A300-600
Organization: FAA
Status: Active
AD 96-NM-221
Title: LOSS OF THE INTEGRATED HYDRAULIC PACKAGE (IHP) FUNCTION\SAAB-SCANIA AB\2000
Organization: FAA
Status: Active
AD 96-NM-245
Title: FATIGUE CRACKING IN THE INTERNAL SKIN DOUBLERS\BOEING\747-100 SERIES\747-100B\747-200 SERIES\747-200B SERIES\747-200C SERIES\747-200F SERIES\747-300 SERIES\747-400 SERIES\747-400D\747-400F\747SP\74...
Organization: FAA
Status: Active
AD 96-CE-53
Title: CRACKS IN THE UPPER RUDDER HINGE BRACKET\PIPER\PA-38-112
Organization: FAA
Status: Active
AD 96-NM-228
Title: OVERBIAS OR OVERBALANCE OF THE RUDDER\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-800A/HAWKER 800\HAWKER 800XP SERIES
Organization: FAA
Status: Active
AD 96-NM-270
Title: FAILURES OF THE ELECTRICAL CONNECTORS\MCDONNELL DOUGLAS CORPORATION\DC-9-80
Organization: FAA
Status: Active
AD 96-NM-222
Title: CHAFING OF WIRE BUNDLES\BOEING\757-200 SERIES\757-200CB SERIES\757-200PF SERIES
Organization: FAA
Status: Active
AD 96-NM-282
Title: LOSS OF AIRPLANE CONTROLLABILITY OR ENGINE OVERSPEED\FRAKES AVIATION (FORMERLY GULFSTREAM AMERICAN)\G-73
Organization: FAA
Status: Active
AD 96-NM-257
Title: RUPTURE OF THE REAR SPAR\LOCKHEED AIRCRAFT CORP LOCKHEED-GEORGIA COMPANY AND LOCKHEED-CALIFORNIA COMPANY\L-1011-385 SERIES
Organization: FAA
Status: Active
AD 96-NM-194
Title: UNCOMMANDED ACTIVATION OF THE RUDDER TRIM\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325\A300-600
Organization: FAA
Status: Active
AD 96-NM-182
Title: FATIGUE CRACKING OF THE FUSELAGE OUTER SKIN\AIRBUS INDUSTRIE\A300-600
Organization: FAA
Status: Active
AD 96-NM-178
Title: UNCOMMANDED APPLICATION OF THE BRAKES DURING LANDING\BRITISH AEROSPACE\ATP SERIES
Organization: FAA
Status: Active
AD 96-NM-172
Title: CRACKING IN THE AFT MOUNT BEAM ASSEMBLY OF THE ENGINE\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325\A300-600
Organization: FAA
Status: Active
AD 96-NM-171
Title: LOSS OF CONTROL OF THE CABIN PRESSURIZATION SYSTEM\BOEING\747-400 SERIES
Organization: FAA
Status: Active
AD 96-NM-165
Title: BROKEN OR DEFORMED THRUST REVERSER CONTROL LEVER SPRINGS\AIRBUS INDUSTRIE\A300-B2-1A\A300-B2-1C\A300-B2-203\A300-B4-103\A300-B4-203\A300-B4-2C\A300-B4-600R SERIES\A300-B4-620\A300-B4-622R\A300-B4-622
Organization: FAA
Status: Active
AD 96-NM-130
Title: INCORRECT WIRING OF THE WIRE HARNESS INSTALLATION TO THE FIRE EXTINGUISHER CARTRIDGES IN THE ENGINE NACELLES\SAAB-SCANIA AB\SF-340A\SAAB 340B SERIES
Organization: FAA
Status: Active
AD 96-NM-113
Title: REDUCED STRUCTURAL INTEGRITY OF THE LOWER PART OF THE MLG FAIRING\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-NM-110
Title: CHAFING OF VARIOUS CONTROL CABLES\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-NM-31-R1
Title: IMPROPER FUNCTIONING OF A CERTAIN ACTUATOR\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES\737 SERIES (T-43)
Organization: FAA
Status: Active
AD 96-CE-51
Title: LOSS OF ENGINE POWER AND FUEL DEPLETION DURING FLIGHT\MOONEY AIRCRAFT CORPORATION (SEE UNIVAIR)\M20F\M20J\M20L
Organization: FAA
Status: Active
AD 96-NM-193
Title: CORROSION OR CRACKING OF MLG A-FRAME FITTINGS\BRITISH AEROSPACE\1-11 200 SERIES\1-11 400 SERIES
Organization: FAA
Status: Active
AD 96-NM-73
Title: SPREAD OF FIRE THROUGH THE ZONES OF EACH NACELLE\DEHAVILLAND\DHC-8-100 SERIES\DHC-8-300
Organization: FAA
Status: Active
AD 96-NM-152-R1
Title: FAILURE OF THE WHEEL FLANGES\BOEING\737-100 SERIES\737-200 SERIES (T-43)
Organization: FAA
Status: Active
AD 96-NM-219
Title: ACCUMULATION OF SLUSH IN THE MAIN LANDING GEAR (MLG) BAY AREAS\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-NM-177
Title: PROPER SWITCHES INSTALLED ON THE FIRE HANDLE PANEL OF THE FIRE HANDLE ASSEMBLY\SAAB-SCANIA AB\SAAB 340B SERIES
Organization: FAA
Status: Active
AD 96-NM-115
Title: FAILURE OF THE CABLE TENSION REGULATOR ON BOTH THE LEFT AND RIGHT ELEVATORS\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-CE-66
Title: FAILURE OF A MLG WHEEL AXLE/PISTON TUBE ASSEMBLY\EMPRESA BRASILEIRA DE AERONAUTICA S A\EMBRAER EMB-110P1\EMBRAER EMB-110P2
Organization: FAA
Status: Active
AD 96-NM-203
Title: FATIGUE CRACKS IN THE SKIN AND LONGERONS OF THE FUSELAGE\MCDONNELL DOUGLAS CORPORATION\DC-9-10\DC-9-20\DC-9-30\DC-9-40\DC-9-50\DC-9-81\DC-9-82\DC-9-83\DC-9-87\MD-88\C-9 (MILITARY) SERIES
Organization: FAA
Status: Active
AD 96-NM-201
Title: ENSURE CONTINUED STRUCTURAL INTEGRITY OF THESE AIRPLANES\MCDONNELL DOUGLAS CORPORATION\MD-90-30
Organization: FAA
Status: Active
AD 96-NM-120
Title: LOSS OF HYDRAULIC DAMPING IN THE MAIN LANDING GEAR\CONSTRUCCIONES AERONAUTICAS S A (CASA)\C-212 SERIES
Organization: FAA
Status: Active
AD 96-CE-25
Title: FAILURE OF THE MAIN LANDING GEAR\PILATUS BRITTEN-NORMAN LTD (SEE BRITTEN-NORMAN)\BN-2\BN-2A\BN-2A SERIES\BN-2B SERIES\BN-2T
Organization: FAA
Status: Active
AD 96-CE-23
Title: POSSIBLE IN-FLIGHT SEPARATION OF THE WING FROM THE AIRPLANE\WHITE INTERNATIONAL LTD (FORMERLY AVIAT FORMERLY CHRISTEN IND )\S-1S\S-1T\S-2\S-2A\S-2S\S-2B
Organization: FAA
Status: Active
AD 96-CE-17
Title: FAILURE OF THE UPPER MOUNTING BRACKETS ON BOTH WING MOUNTED ENGINES\PILATUS BRITTEN-NORMAN LTD (SEE BRITTEN-NORMAN)\BN-2\BN-2T\BN-2A\BN-2B SERIES
Organization: FAA
Status: Active
AD 96-NM-126
Title: FATIGUE CRACKING IN THE AREA OF THE CENTER WING-TO-FUSELAGE ATTACHMENT FITTING\CONSTRUCCIONES AERONAUTICAS S A (CASA)\CN-235 SERIES
Organization: FAA
Status: Active
AD 96-CE-24
Title: FAILURE OF THE LEFT-HAND (LH) RUDDER BAR ASSEMBLY\BRITTEN-NORMAN LTD (SEE ALSO PILATUS BRITTEN-NORMAN)\BN-2A MARK III\PILATUS BRITTEN-NORMAN LTD (SEE BRITTEN-NORMAN)\BN-2A
Organization: FAA
Status: Active
AD 96-NM-283
Title: CHAFING OF THE WIRE BUNDLES ADJACENT TO THE DISCONNECT PANEL BRACKET ASSEMBLY\MCDONNELL DOUGLAS CORPORATION\MD-11 SERIES
Organization: FAA
Status: Active
AD 96-NM-278
Title: CRACKING OF THE SUPPORT BRACKETS IN THE REFUEL AND FUEL TRANSFER LINES\MCDONNELL DOUGLAS CORPORATION\MD-11 SERIES
Organization: FAA
Status: Active
AD 96-NM-272
Title: FATIGUE CRACKING IN THE FUSELAGE SKIN OR DOUBLER AT THE CORNERS OF THE UPPER CARGO DOORJAMB\MCDONNELL DOUGLAS CORPORATION\DC-9-10\DC-9-15\DC-9-30\C-9 (MILITARY) SERIES
Organization: FAA
Status: Active
AD 96-NM-210
Title: UNCOMMANDED NOSE-DOWN PITCH AT CERTAIN DLAP SETTINGS DURING ICING CONDITIONS\MITSUBISHI AIRCRFT INTNL AND MITSUBISHI HEAVY IND\MU-300
Organization: FAA
Status: Active
AD 96-NM-209
Title: UNCOMMANDED NOSE-DOWN PITCH AT CERTAIN FLAP SETTINGS DURING ICING CONDITIONS\BEECH AIRCRAFT\400\400T\MU-300-10\400A
Organization: FAA
Status: Active
AD 96-NM-196
Title: FATIGUE CRACKING OF THE MAIN ENTRY DOOR FRAME PRESSING AREA\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\DH 125-1A\DH 125-3A
Organization: FAA
Status: Active
AD 96-NM-190
Title: SCORING OF THE UPPER FUSELAGE SKIN\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\DH 125-1A\DH 125-3A\DH 125-400A
Organization: FAA
Status: Active
AD 96-NM-144
Title: IN-FLIGHT UNCOMMANDED ACTIVATION OF THE PROPELLER BRAKE SYSTEM\CONSTRUCCIONES AERONAUTICAS S A (CASA)\CN-235 SERIES\CN-235-100\CN-235-200
Organization: FAA
Status: Active
AD 96-NM-141
Title: INADVERTENT OPENING OF THE PASSENGER/CREW DOOR DURING UNPRESSURIZED FLIGHT\AEROSPATIALE\ATR42 SERIES\ATR72 SERIES
Organization: FAA
Status: Active
AD 96-NM-138
Title: FATIGUE-RELATED CRACKING IN THE GUIDE HOOKS OF THE CARGO DOOR\CONSTRUCCIONES AERONAUTICAS S A (CASA)\CN-235 SERIES
Organization: FAA
Status: Active
AD 96-NM-106
Title: FATIGUE CRACKING IN THE AREA WHERE THE CENTER FUSELAGE JOINS THE WING\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233
Organization: FAA
Status: Active
AD 96-NM-96
Title: MOVEMENT OF THE SUPPORT BEAM ATTACHED TO THE FUSELAGE FRAME AT STATION 452.00\ISRAEL AIRCRAFT INDUSTRIES LTD\1125 WESTWIND ASTRA SERIES
Organization: FAA
Status: Active
AD 96-NM-64
Title: CLOGGING OF THE HYDRAULIC PUMP DRAIN SYSTEM\AIRBUS INDUSTRIE\A300-B4-103\A300-B4-203\A300-B4-2C\A300-B4-600R SERIES\A300-B4-620\A300-B4-622\A300-B4-622R\A300-C4-620\A310-221\A310-222\A310-322\A310-...
Organization: FAA
Status: Active
AD 96-CE-56
Title: FATIGUE CRACKS IN THE RUDDER TORQUE TUBE BOTTOM FLANGE\INDUSTRIE AERONAUTICHE E MECCANICHE (SEE PIAGGIO)\P-180
Organization: FAA
Status: Active
AD 96-CE-47
Title: IN-FLIGHT VERTICAL FIN STRUCTURAL FAILURE OF THE FRONT SPAR ATTACHMENTS\AIR TRACTOR INC\AT-301\AT-401\AT-302\AT-400\AT-400A\AT-402\AT-501\AT-502
Organization: FAA
Status: Active
AD 96-CE-40
Title: FAILURE OF THE LANDING GEAR LEGS\BURKHART GROB LUFT-UND RAUMFAHRT (FORMERLY GROB-WERKE GMBH & CO )\G109\G109B
Organization: FAA
Status: Active
AD 96-ANE-38
Title: OVERSPEED OF THE AFT FAN DISK\GENERAL ELECTRIC CO\CF700 SERIES
Organization: FAA
Status: Active
AD 96-ANE-24
Title: OIL SCAVENGE PUMP SNAP RING FAILURE\ALLIED-SIGNAL AEROSPACE\OIL SCAVENGE PUMPS\RAJAY CORP\OIL SCAVENGE PUMPS\TELEDYNE CONTINENTAL MOTORS\IO-470 SERIES\TSIO-520 SERIES\TEXTRON LYCOMING (SEE AVCO)\O-...
Organization: FAA
Status: Active
AD 96-SW-21
Title: FAILURE OF ESSENTIAL ELECTRICAL EQUIPMENT\EUROCOPTER DEUTSCHLAND (FORMERLY MESSERSCHMITT-BOLKOW-BLOHM-GMBH)\BO-105C SERIES\BO-105S SERIES
Organization: FAA
Status: Active
AD 96-NM-252
Title: SEVERELY REDUCED CONTROLLABILITY OF THE AIRPLANE DURING APPROACH\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233\A321-100\A321-111\A321-112\A321-131
Organization: FAA
Status: Active
AD 96-NM-188
Title: CRACKING OF THE ENGINE MOUNTING LUGS\BRITISH AEROSPACE\1-11 200 SERIES\1-11 400 SERIES
Organization: FAA
Status: Active
AD 96-NM-180
Title: INADEQUATE VENTING OF CABIN PRESSURE IN THE EVENT OF RAPID DECOMPRESSION\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-1000A/HAWKER 1000
Organization: FAA
Status: Active
AD 96-NM-168
Title: CRACKING IN FRAME 179 OF THE FUSELAGE\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 96-CE-62
Title: TRIM SYSTEM MALFUNCTION\INDUSTRIE AERONAUTICHE E MECCANICHE (SEE PIAGGIO)\P-180
Organization: FAA
Status: Active
AD 96-SW-23
Title: FAILURE OF THE CLUTCH AND LOSS OF POWER TO THE MAIN ROTOR\EUROCOPTER DEUTSCHLAND (FORMERLY MESSERSCHMITT-BOLKOW-BLOHM-GMBH)\BK117A-1\BK117A-3\BK117A-4\BK117B-1\BK117B-2
Organization: FAA
Status: Active
AD 96-NM-260
Title: HIGH FUEL PRESSURE IN COMPONENTS BETWEEN THE FUEL SHUTOFF SPAR VALVE AND THE ENGINE FUEL SHUTOFF VALVE\BOEING\747-100 SERIES\747-200 SERIES\747-300 SERIES\747-400 SERIES
Organization: FAA
Status: Active
AD 96-NM-137
Title: LOSS OF CONTROL OF THE ELEVATOR AND/OR RUDDER\CONSTRUCCIONES AERONAUTICAS S A (CASA)\CN-235 SERIES
Organization: FAA
Status: Active
AD 96-NM-123
Title: PROBLEMS ASSOCIATED WITH CORROSION DAMAGE\CONSTRUCCIONES AERONAUTICAS S A (CASA)\C-212
Organization: FAA
Status: Active
AD 96-NM-108
Title: FAILURE OF LUGS AND/OR PINS\CANADAIR LTD\CL-600-2B19
Organization: FAA
Status: Active
AD 96-SW-30
Title: POSSIBLE HEAT ACCUMULATION\MCDONNELL DOUGLAS HELICOPTER (SEE SCHWEIZER AIRCRAFT CORPORATION)\MD-900
Organization: FAA
Status: Active
AD 96-NM-244
Title: FATIGUE CRACKING\MCDONNELL DOUGLAS CORPORATION\DC-9-10\DC-9-20\DC-9-30\DC-9-40\DC-9-50\C-9 (MILITARY) SERIES
Organization: FAA
Status: Active
AD 96-NM-175
Title: EXTINGUISHING AGENT IS PROPERLY DISTRIBUTED WITHIN THE BAGGAGE BAYS AND PORTABLE EXTINGUISHERS OPERATE PROPERLY\SHORT BROTHERS\SD3-30\SD3-60
Organization: FAA
Status: Active
AD 96-NM-169
Title: CHAFING OF WIRE BUNDLES\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325
Organization: FAA
Status: Active
AD 96-NM-127
Title: CENTER WING ATTACHMENT RODS FAILING\CONSTRUCCIONES AERONAUTICAS S A (CASA)\CN-235 SERIES
Organization: FAA
Status: Active
AD 96-NM-44
Title: DETECTING CORROSION BEHIND THE SCUFF PLATES AT EXIT AND CARGO DOORS\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325
Organization: FAA
Status: Active
AD 96-NM-43
Title: DETECTING CORROSION BEHIND THE SCUFF PLATES AT EXIT AND CARGO DOORS\AIRBUS INDUSTRIE\A300-600\A300-B2-1A\A300-B2-1C\A300-B2-203\A300-B2K-3C\A300-B4-103\A300-B4-203\A300-B4-2C\A300-B4-600R SERIES\A3...
Organization: FAA
Status: Active
AD 96-NM-42
Title: DETECTING CORROSION BEHIND THE SCUFF PLATES AT EXIT AND CARGO DOORS\AIRBUS INDUSTRIE\A300-600
Organization: FAA
Status: Active
AD 96-CE-65
Title: FAILURE OF THE FLIGHT CONTROL SYSTEM\FAIRCHILD AIRCRAFT CORPORATION\SA226-T\SA226-T(B)\SA226-AT\SA226-TC\SA227-TT\SA227-AT\SA227-AC\SA227-BC
Organization: FAA
Status: Active
AD 96-CE-60
Title: MOISTURE ACCUMULATING AND FREEZING IN THE AIRSTAIR DOOR HANDLE AND LATCH HOUSING\BEECH AIRCRAFT\1900\1900C (C-12J)\1900D
Organization: FAA
Status: Active
AD 96-CE-37
Title: LOSS OF THE SAILPLANE ENGINE PROPELLER\BURKHART GROB LUFT-UND RAUMFAHRT (FORMERLY GROB-WERKE GMBH & CO )\G103 C TWIN III SL
Organization: FAA
Status: Active
AD 96-NM-105
Title: FATIGUE CRACKING IN THE RIB FLANGE\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233
Organization: FAA
Status: Active
AD 96-NM-269
Title: FAILURES OF THE EMERGENCY DC/AC BUS POWER SUPPLY\FOKKER-VFW B V\F.28 MARK 0070\F.28 MARK 0100
Organization: FAA
Status: Active
AD 96-NM-239
Title: SHORT CIRCUITING OF SWITCHES IN THE CABIN ATTENDANT'S PANEL\BOEING\747-100 SERIES\747-200 SERIES\747-300 SERIES
Organization: FAA
Status: Active
AD 96-NM-185
Title: FATIGUE CRACKING IN THE VERTICAL STABILIZER\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 96-NM-92
Title: LOSS OF THE OFF-WING EMERGENCY EVACUATION SLIDES ('ESCAPE SLIDES') DURING FLIGHT\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233
Organization: FAA
Status: Active
AD 96-NM-60
Title: FAILURE OF THE FLAP TRANSMISSION SHAFT\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325
Organization: FAA
Status: Active
AD 96-SW-32
Title: CRACKS IN THE HEAD AREA OF THE OUTBOARD TENSION-TORSION (T-T) BAR PIN\HILLER AVIATION (SEE ROGERSON HILLER)\UH-12A (HTE-1, H-23A)\UH-12B (HTE-2, H-23B, H-23C)\UH-12C\UH-12D (UH-23D)\UH-12E
Organization: FAA
Status: Active
AD 96-NM-100
Title: ENGAGING THE STANDBY ELEVATOR CONTROL SYSTEM\BRITISH AEROSPACE\ATP SERIES
Organization: FAA
Status: Active
AD 96-ANE-35
Title: FRACTURE OF THE HIGH PRESSURE TURBINE (HPT) SHAFT\PRATT & WHITNEY\JT8D-209\JT8D-217\JT8D-217A\JT8D-217C\JT8D-219
Organization: FAA
Status: Active
AD 96-ANE-32
Title: 4TH STAGE LPT BLADE FAILURE\PRATT & WHITNEY\JT8D-1\JT8D-1A\JT8D-1B\JT8D-7\JT8D-7A\JT8D-7B\JT8D-9\JT8D-9A\JT8D-11\JT8D-15\JT8D-17\JT8D-17R
Organization: FAA
Status: Active
AD 96-NM-117
Title: FAILURE OF THE ANCHOR POINT FASTENERS ON THE SEAT RESTRAINING SYSTEMS\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-NM-116
Title: FAILURE OF THE DIAGONAL BRACES THAT CONNECT THE LEFT AND RIGHT WINGS TO THE FUSELAGE\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-NM-236
Title: DISCONNECT UNIT FROM OPENING INADVERTENTLY\SAAB-SCANIA AB\2000
Organization: FAA
Status: Active
AD 96-CE-57
Title: STRUCTURAL FAILURE OF THE HORIZONTAL STABILIZER CAUSED BY FATIGUE CRACKS\AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD (FORMERLY GOVERNMENT AIRCRAFT FACTORIES)\N22B\N22S\N24A
Organization: FAA
Status: Active
AD 96-CE-35
Title: CRACKS IN THE AILERON OPERATING LEVER'S ACTUATING SHAFT WELDED SEAMS\GLASFLUGEL\STANDARD 'LIBELLE'\STANDARD LIBELLE 201B
Organization: FAA
Status: Active
AD 96-NM-131
Title: FAILURE OF THE FRONT BULKHEAD OF THE AFT MAIN BAGGAGE BAY AND THE DOORS OF THE AFT RIGHT STOWAGE COMPARTMENT DURING EMERGENCY LANDING DYNAMIC CONDITIONS\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AER...
Organization: FAA
Status: Active
AD 96-NM-118
Title: LOOSENING OR LOSS OF THE ATTACHMENT SCREWS\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-NM-114
Title: FAILURE OF THE NO. 2 PRIMARY FLIGHT AND MULTIPLE FUNCTION DISPLAYS OR THE AUTOPILOT/YAW DAMPER SERVOS DURING TAKEOFF AND LANDING\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-NM-65
Title: DISBONDING\AIRBUS INDUSTRIE\A300-600\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325
Organization: FAA
Status: Active
AD 96-SW-27
Title: SELF-ACTIVATION OF THE VALVES\BELL HELICOPTER TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\214ST
Organization: FAA
Status: Active
AD 96-NM-218
Title: THE POSSIBILITY OF AN IN-FLIGHT OR GROUND FIRE\MCDONNELL DOUGLAS CORPORATION\MD-11 SERIES\MD-11F SERIES
Organization: FAA
Status: Active
AD 96-NM-97
Title: OVERHEATING OF THE ELECTRICAL GROUND POSTS\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 96-NM-71
Title: LEAKAGE OF FUEL INTO THE FORWARD CARGO BAY\BOEING\747-200 SERIES\747-300 SERIES\747-400 SERIES
Organization: FAA
Status: Active
AD 96-NM-52
Title: CORROSION AND CONSEQUENT FATIGUE CRACKING OF THE UPPER DECK FLOOR BEAM AT STATION 980\BOEING\747-300 SERIES\747-400 SERIES
Organization: FAA
Status: Active
AD 96-ANE-25
Title: N2 ACCESSORY DRIVE ASSEMBLY DISENGAGEMENT\TEXTRON LYCOMING (SEE AVCO)\T5311A\T5311B\T5313B\T5317 SERIES\T53
Organization: FAA
Status: Active
AD 96-NM-89
Title: SETTINGS FOR THE RUDDER PEDALS RESTRICTING THE FLIGHT CREW IN ITS ABILITY TO MOVE THE RUDDER TO ITS MAXIMUM CERTIFIED DEFLECTION\CONSTRUCCIONES AERONAUTICAS S A (CASA)\C-212 SERIES
Organization: FAA
Status: Active
AD 96-NM-86
Title: FATIGUE CRACKING OF THE DRAG BRACE OF THE LEFT AND RIGHT MLG\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 96-CE-44
Title: FAILURE OF THE RUDDERVATOR DIFFERENTIAL TAIL CONTROL ROD ASSEMBLY\BEECH AIRCRAFT\35\A35\B35\C35\D35\E35\F35\G35\H35\J35\K35\M35\N35\P35\35R\S35\V35\V35-TC\V35A\V35A-TC\V35B\V35B-TC
Organization: FAA
Status: Active
AD 96-NM-154
Title: FAILURE OF THE LOWER BOLTS THAT JOIN THE DOG-LINKS TO THE PISTON OF THE HORIZONTAL STABILIZER CONTROL UNIT (HSCU)\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 96-ANE-26
Title: CRACKING OF THE FUEL MANIFOLD ASSEMBLY\TEXTRON LYCOMING (SEE AVCO)\ALF502 SERIES\LF507 SERIES
Organization: FAA
Status: Active
AD 96-NM-107
Title: FATIGUE CRACKING OF THE REAR PRESSURE BULKHEAD\AIRBUS INDUSTRIE\A300-600\A300-B2-1A\A300-B2-1C\A300-B2-203\A300-B2K-3C\A300-B4-103\A300-B4-203\A300-B4-2C\A300-B4-600R SERIES\A300-B4-620\A300-B4-622...
Organization: FAA
Status: Active
AD 96-NM-124
Title: IN-CABIN INFLATION OF THE EVACUATION SLIDES\MCDONNELL DOUGLAS CORPORATION\DC-9-10\DC-9-20\DC-9-30\DC-9-40\DC-9-50\DC-9-81\DC-9-82\DC-9-83\DC-9-87\MD-88
Organization: FAA
Status: Active
AD 96-CE-19
Title: CORROSION IN THE ELEVATOR CAUSED BY WATER ENTERING THE ELEVATOR CONTROL ROD\SCHEMPP-HIRTH KG (SEE GROB-WERKE)\STANDARD CIRRUS\NIMBUS-2\NIMBUS-2B\MINI-NIMBUS HS-7\MINI-NIMBUS B\DISCUS A\DISCUS B
Organization: FAA
Status: Active
AD 96-SW-05
Title: FAILURE OF THE RING GEAR, LOSS OF DRIVE TO THE MAIN ROTOR GEARBOX, AND A SUBSEQUENT FORCED LANDING\SCHWEIZER AIRCRAFT CORP (SEE MCDONNELL DOUG HELI )\269A\269A-1\269B\269C\TH-55A
Organization: FAA
Status: Active
AD 96-NM-32
Title: FATIGUE CRACKING IN DRAG STAY UNIT OF THE MAIN LANDING GEAR (MLG)\FOKKER-VFW B V\F.27 MARK 050\F.27 MARK 100\F.27 MARK 200\F.27 MARK 300\F.27 MARK 400\F.27 MARK 600\F.27 MARK 700
Organization: FAA
Status: Active
AD 96-NM-202
Title: ELECTRICAL ARCING AND CONSEQUENT FIRE HAZARD\LEARJET CORP\31\35A
Organization: FAA
Status: Active
AD 96-NM-85
Title: FAILURE DURING EMERGENCY LANDING DYNAMIC CONDITIONS OF THE INTERCOSTAL THAT ATTACHES THE THIRD CREW MEMBER SEAT ('THIRD CREW SEAT') TO THE FLOOR STRUCTURE IN THE FLIGHT COMPARTMENT\JETSTREAM AIRCRA...
Organization: FAA
Status: Active
AD 96-NM-233
Title: PREVENTION OF FLAME, FUEL, AND VAPOR FROM ENTERING COMPARTMENTS BEHIND THE FIREZONE COMPARTMENT OF THE NACELLE OF THE LEFT AND RIGHT ENGINES\SAAB-SCANIA AB\2000
Organization: FAA
Status: Active
AD 96-CE-45
Title: INABILITY OF BOTH ENGINES TO UTILIZE THE ENTIRE FUEL SUPPLY\MITSUBISHI AIRCRFT INTNL AND MITSUBISHI HEAVY IND\MU-2B\MU-2B-10\MU-2B-15\MU-2B-20\MU-2B-30
Organization: FAA
Status: Active
AD 96-SW-10
Title: LOSS OF THE ABRASION STRIP FROM THE MAIN ROTOR BLADE\SCHWEIZER AIRCRAFT CORP (SEE MCDONNELL DOUG HELI )\269A\269A-1\269B\269C\TH-55A SERIES\MCDONNELL DOUGLAS HELICOPTER (SEE SCHWEIZER AIRCRAFT CORP...
Organization: FAA
Status: Active
AD 96-SW-17
Title: FAILURE OF THE STEEL SWASHPLATE SUPPORT ASSEMBLY\BELL HELICOPTER TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\412
Organization: FAA
Status: Active
AD 96-NM-243
Title: OVERHEAT FAILURE OF THE FLIGHT CONTROL COMPUTER (FCC)\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 96-NM-76
Title: STRUCTURAL DEGRADATION OF THE NOSE LANDING GEAR (NLG)\CONSTRUCCIONES AERONAUTICAS S A (CASA)\CN-235 SERIES
Organization: FAA
Status: Active
AD 96-NM-93
Title: STRUCTURAL DAMAGE TO THE TAIL SECTION\AIRBUS INDUSTRIE\A320-111\A320-211\A320-212\A320-231
Organization: FAA
Status: Active
AD 96-NM-11
Title: LOSS OF THE STANDBY EMERGENCY GENERATION SYSTEM\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233
Organization: FAA
Status: Active
AD 96-CE-27
Title: SEPARATION OF THE STABILONS FROM THE AIRPLANE\BEECH AIRCRAFT\1900D\BEECH AIRCRAFT\1900D
Organization: FAA
Status: Active
AD 96-CE-38
Title: SAILPLANE FLUTTER\GLASFLUGEL\H-301 'LIBELLE'\H301B 'LIBELLE'\STANDARD 'LIBELLE'\STANDARD LIBELLE 201B\CLUB LIBELLE 205\KESTREL
Organization: FAA
Status: Active
AD 96-NM-242
Title: FAILURE OF THE GPWS EQUIPMENT\AIRTELL INTERNATIONAL INC\CENTAURUS MODEL C3-100\AIRTELL INTERNATIONAL INC\CENTAURUS MODEL C3-100
Organization: FAA
Status: Active
AD 96-NM-51
Title: PREVENTION OF THE LEFT AND RIGHT ELEVATORS FROM OSCILLATING OR FLUTTERING\BRITISH AEROSPACE\BAE-146\AVRO 146-RJ SERIES
Organization: FAA
Status: Active
AD 96-NM-26
Title: FAILURE OF THE MAIN FITTING\BRITISH AEROSPACE\BAE-146\AVRO 146-RJ SERIES
Organization: FAA
Status: Active
AD 96-CE-48
Title: FATIGUE FAILURE OF A TAIL LANDING GEAR SPRING\AIR TRACTOR INC\AT-802\AT-802A
Organization: FAA
Status: Active
AD 96-NM-163
Title: THE POTENTIAL FOR A FIRE IN THE PASSENGER COMPARTMENT RESULTING FROM FAILURE OF THE FLUORESCENT LIGHT BALLAST OF THE CABIN SIDEWALL\TRANSPORT CATEGORY AIRCRFT\DAY-RAY PRODUCTS
Organization: FAA
Status: Active
AD 96-ANE-33
Title: FRONT COMPRESSOR FRONT HUB (FAN HUB)\PRATT & WHITNEY\JT8D-209\JT8D-217\JT8D-217C\JT8D-219
Organization: FAA
Status: Active
AD 96-ANE-13
Title: NON-RESPONSIVE POWER LEVER AND LACK OF CONTROL OF ENGINE POWER\GARRETT TURBINE ENGINE CO (SEE AIRESEARCH ALLIED SIGNAL)\TPE 331 SERIES (OLDER AD'S FOR THIS MODEL UNDER AIRESEARCH)
Organization: FAA
Status: Active
AD 96-NM-78
Title: INSTALLATION OF MANUAL EXTENSION GEARBOX ASSEMBLIES THAT DO NOT CONTAIN REQUIRED GEARBOX HOUSINGS/HOUSING ASSEMBLIES\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES
Organization: FAA
Status: Active
AD 96-NM-67
Title: STICKING CONDITIONS IN THE RUDDER TRIM SWITCH\BOEING\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 96-SW-04
Title: FAILURE OF THE PLATE DUE TO FATIGUE CRACKING\SIKORSKY AIRCRFT DIV OF UNITED AIRCRFT CORP\S-64E
Organization: FAA
Status: Active
AD 96-CE-29
Title: THE FAILURE OF THE NOSE WHEEL\PIPER\PA-31\PA-31-325\PA-31-350\PA-31P
Organization: FAA
Status: Active
AD 96-NM-79
Title: IMPROPER GROUNDING OF THE HOUSING OF THE LAVATORY PUMP AND FILTER ASSEMBLY\FOKKER-VFW B V\F.28 MARK 0100\F.27 MARK 050
Organization: FAA
Status: Active
AD 96-NM-160
Title: FIRE HAZARD AS A RESULT OF BURNING AND ARCING OF THE CONNECTOR CONTACTS OF THE POWER FEEDER CABLE OF THE AUXILIARY POWER UNIT (APU) GENERATOR\MCDONNELL DOUGLAS CORP\MD-11 SERIES
Organization: FAA
Status: Active
AD 96-NM-158
Title: LOSS OF ROLLER ATTACH NUTS AND THE FLAP ROLLER\BEECH AIRCRAFT\400A\400T
Organization: FAA
Status: Active
AD 96-NM-70
Title: INCORRECT ROUTING AND INCORRECT TENSION OF THE FLIGHT CONTROL LOCK CABLES AND ELEVATOR CONTROL CABLES\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 96-NM-217
Title: CONTROL THE AIRPLANE MANUALLY IF THE AUTOPILOT OR AUTOTHROTTLE FUNCTION FAILS TO DISENGAGE\MCDONNELL DOUGLAS CORP\DC-9-81\(MD-80) SERIES\DC-9-82\DC-9-83\DC-9-87\MD-88
Organization: FAA
Status: Active
AD 96-CE-43
Title: WING SKIN DE-BONDING OR WARPING OF THE CABIN WINDOWS\BEECH AIRCRAFT\1900D
Organization: FAA
Status: Active
AD 96-ANE-06
Title: GGT STAGE 2 FORWARD COOLING PLATE FAILURE\GENERAL ELECTRIC CO\CT7
Organization: FAA
Status: Active
AD 96-NM-121
Title: HONEYWELL STANDARD WINDSHEAR DETECTION SYSTEMS (WSS)\BOEING\727-200 SERIES\MCDONNELL DOUGLAS CORP\MD-11 SERIES\BRITISH AEROSPACE\AVRO 146-RJ70A\AVRO 146-RJ85A\AVRO 146-RJ100A
Organization: FAA
Status: Active
AD 96-NM-95
Title: EMERGENCY INTERNAL RELEASE SYSTEM OF THE TAILCONE\MCDONNELL DOUGLAS CORP\DC-9-10\DC-9-11\DC-9-12\DC-9-13\DC-9-14\DC-9-15\DC-9-15F\DC-9-21\DC-9-31\DC-9-32 (VC-9C)\DC-9-32F (C-9A, C-9B)\DC-9-33F\DC-9...
Organization: FAA
Status: Active
AD 96-NM-156
Title: REDUCED CONTROLLABILITY OF THE AIRPLANE\BOEING\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 96-NM-58
Title: CABIN CEILING LIGHTING SYSTEM\DEHAVILLAND\DHC-8-102\DHC-8-103\DHC-8-301
Organization: FAA
Status: Active
AD 96-NM-88
Title: TORQUE TUBE OF THE LEFT-HAND ELEVATOR\FOKKER-VFW B V\F.27 MARK 100\F.27 MARK 200\F.27 MARK 300\F.27 MARK 400\F.27 MARK 500\F.27 MARK 600\F.27 MARK 700
Organization: FAA
Status: Active
AD 96-SW-06
Title: SEPARATION OF THE CONTROL ROTOR BLADE ASSEMBLY\HILLER AVI (SEE ROGERSON HILLER)\UH-12\UH-12A (HTE-1, H-23A)\UH-12B (HTE-2, H-23B, H23C)\UH-12C\UH-12D (UH-23D)\CH-112\ROGERSON HILLER (SEE HILLER)\UH...
Organization: FAA
Status: Active
AD 96-NM-164
Title: RAT FROM BREAKING AWAY FROM ITS SUPPORT LEG\AIRBUS INDUSTRIE\A320-111\A320-211\A320-212\A320-214\A320-231\A320-232
Organization: FAA
Status: Active
AD 96-SW-03
Title: FATIGUE FAILURE OF THE TAIL ROTOR SLIDER (SLIDER)\BELL HELICPTR TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\HH-1K\TH-1F\TH-1L\UH-1A\UH-1B\UH-1E\UH-1F\UH-1H\UH-1L...
Organization: FAA
Status: Active
AD 96-NM-69
Title: LOSS OF BRAKE EFFECTIVENESS\SAAB-SCANIA AB\SF-340A
Organization: FAA
Status: Active
AD 96-NM-136
Title: ENGINE FIRE\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPC CORP )\BAE 125-800A/HAWKER 800\HAWKER 800XP SERIES
Organization: FAA
Status: Active
AD 96-NM-173
Title: EXCESSIVE WEAR OF THE AILERON PUSH-PULL TUBE\ISRAEL AIRCRFT IND LTD\1123 SERIES\1124 SERIES\1124A
Organization: FAA
Status: Active
AD 96-NM-29
Title: INBOARD FLAP TRUNNION\AIRBUS INDUSTRIE\A320-111\A320-211\A320-212\A320-231\A320-232
Organization: FAA
Status: Active
AD 96-SW-15
Title: MAIN ROTOR (M/R) STALL\ROBINSON HELICPTR CO\R-44
Organization: FAA
Status: Active
AD 96-SW-14
Title: MAIN ROTOR (M/R) STALL\ROBINSON HELICPTR CO\R-22 SERIES
Organization: FAA
Status: Active
AD 96-NM-125
Title: RUNAWAY OF THE AUTOTHROTTLE DURING FLIGHT OR GROUND OPERATIONS\BOEING\757-200 SERIES\757-200CB SERIES\757-200PF SERIES
Organization: FAA
Status: Active
AD 96-NM-135
Title: STRUCTURAL INTEGRITY OF THE NUMBER 4 BANJO FITTING\MCDONNELL DOUGLAS CORP\DC-10-10\DC-10-30\DC-10-30F (KC-10A)\DC-10-40\DC-10-40F
Organization: FAA
Status: Active
AD 96-NM-153
Title: AILERON CONTROL SYSTEM\BOEING\737 SERIES (T-43)
Organization: FAA
Status: Active
AD 96-NM-152
Title: FAILURE OF THE WHEEL FLANGES\BOEING\737-100 SERIES\737-200 SERIES (T-43)
Organization: FAA
Status: Active
AD 96-NM-151
Title: YAW DAMPER SYSTEM\BOEING\737-100 SERIES\737-200 SERIES (T-43)\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 96-NM-150
Title: REDUCED RATE OF MOVEMENT OF THE ELEVATOR, AILERON, OR RUDDER\BOEING\737-100 SERIES\737-200 SERIES (T-43)\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 96-NM-149
Title: CORROSION IN THE BEARINGS, CABLES, ELECTRICAL CONNECTORS\BOEING\737 SERIES (T-43)
Organization: FAA
Status: Active
AD 96-NM-148
Title: FATIGUE CRACKING OF THE PULLEY BRACKETS\BOEING\737-300 SERIES
Organization: FAA
Status: Active
AD 96-NM-147
Title: RUDDER PEDAL\BOEING\737-100 SERIES\737-200 SERIES (T-43)\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 96-NM-146
Title: REDUCED ROLL AND/OR PITCH RATE CONTROL OF THE AILERON\BOEING\737 SERIES (T-43)
Organization: FAA
Status: Active
AD 96-NM-145
Title: LATERAL CONTROL SYSTEM TRANSFER MECHANISM\BOEING\737-100 SERIES\737-200 SERIES (T-43)
Organization: FAA
Status: Active
AD 96-NM-80
Title: IMPACT OVERLOAD AND CONSEQUENT CRACKING OF THE SUBJECT PARTS\FOKKER-VFW B V\F.27 MARK 100\F.27 MARK 200\F.27 MARK 300\F.27 MARK 400\F.27 MARK 500\F.27 MARK 600\F.27 MARK 700
Organization: FAA
Status: Active
AD 96-NM-48
Title: LOCK JACK ASSEMBLIES OF THE MAIN LANDING GEAR (MLG)\BRITISH AEROSPACE\BAE-146\AVRO 146-RJ SERIES
Organization: FAA
Status: Active
AD 96-NM-53
Title: REAR SPAR LOWER CAP OF THE WING\MCDONNELL DOUGLAS CORP\DC-9-80\DC-9-81\DC-9-82\DC-9-83\DC-9-87\(MD-80) SERIES\MD-88
Organization: FAA
Status: Active
AD 96-NM-47
Title: SHROUD BOX ATTACHMENT LUG\AIRBUS INDUSTRIE\A320-111\A320-211\A320-212\A320-231
Organization: FAA
Status: Active
AD 96-NM-40
Title: REDUCED CONTROLLABILITY OF THE AIRPLANE\BRITISH AEROSPACE\BAE-146\AVRO 146-RJ SERIES
Organization: FAA
Status: Active
AD 96-CE-33
Title: LOSS OF ELECTRICAL POWER\PILATUS BRITTEN-NORMAN LTD (SEE BRITTEN-NORMAN)\BN-2\BN-2A SERIES\BN-2B SERIES
Organization: FAA
Status: Active
AD 96-NM-140
Title: UNCOUPLING OF THE ELEVATORS\AEROSPATIALE\ATR72-100 SERIES\ATR72-200 SERIES
Organization: FAA
Status: Active
AD 96-NM-57
Title: FUEL LEAKAGE\BOEING\747-100 SERIES\747-100B\747-200 SERIES\747-200B SERIES\747-200C SERIES\747-200F SERIES\747-300 SERIES\747-400 SERIES\747-400D\747-400F\747SP\747SR\747-E4B\757-200 SERIES\757-200...
Organization: FAA
Status: Active
AD 96-NM-139
Title: SEPARATION OF THE RAM AIR INLET DUCT FROM THE AIRPLANE\BRITISH AEROSPACE\ATP SERIES
Organization: FAA
Status: Active
AD 96-NM-41
Title: LINK SUBASSEMBLY OF THE MAIN LANDING GEAR (MLG)\BRITISH AEROSPACE\BAE 146 SERIES
Organization: FAA
Status: Active
AD 96-ANE-15
Title: TURBINE SHROUD FRAGMENTS\ALLIED-SIGNAL AEROSPC\AUXILIARY POWER UNITS
Organization: FAA
Status: Active
AD 96-CE-28
Title: OUTFLOW/SAFETY VALVE CRACKING AND SUBSEQUENT FAILURE\INDUSTRIE AERONAUTICHE E MECCANICHE (SEE PIAGGIO)\P-180
Organization: FAA
Status: Active
AD 96-NM-68
Title: DECOMPRESSION PANEL\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM SERIES 4100
Organization: FAA
Status: Active
AD 96-NM-12
Title: FAILURE OF THE RAM AIR TURBINE (RAT)\BOEING\757-200 SERIES\757-200CB SERIES\757-200PF SERIES
Organization: FAA
Status: Active
AD 96-NM-142
Title: STRINGERS OF THE LOWER SKIN OF THE WINGS\FOKKER-VFW B V\F.27 MARK 100\F.27 MARK 200\F.27 MARK 300\F.27 MARK 400\F.27 MARK 500\F.27 MARK 600\F.27 MARK 700
Organization: FAA
Status: Active
AD 96-NM-07
Title: STRUCTURAL INTEGRITY OF THE VERTICAL FIN\SHORT BROTHERS\SD3-30\SD3-SHERPA SERIES
Organization: FAA
Status: Active
AD 96-NM-38
Title: NOSE WHEEL STEERING SYSTEM\FOKKER-VFW B V\F.27 MARK 050\F.27 MARK 100\F.27 MARK 200\F.27 MARK 300\F.27 MARK 400\F.27 MARK 500\F.27 MARK 600\F.27 MARK 700
Organization: FAA
Status: Active
AD 96-NM-09
Title: STRESS CORROSION OR CRACKING OF THE GLAND\SHORT BROTHERS\SD3-60\SD3-SHERPA SERIES
Organization: FAA
Status: Active
AD 96-NM-28
Title: LOOSE OR MISSING RIVETS AT THE RIB-TO-STRINGER CONNECTIONS\FOKKER-VFW B V\F.27 MARK 100\F.27 MARK 200\F.27 MARK 300\F.27 MARK 400\F.27 MARK 500\F.27 MARK 600\F.27 MARK 700
Organization: FAA
Status: Active
AD 96-CE-30
Title: CLOGGED FUEL FILTER AND CONTAMINATED FUEL FILTER BY-PASS VALVE\BEECH AIRCRAFT\1900C (C-12J)\1900D\2000
Organization: FAA
Status: Active
AD 96-NM-08
Title: FLAP HYDRAULIC UNITS\SHORT BROTHERS\SD3-30\SD3-60\SD3-SHERPA SERIES
Organization: FAA
Status: Active
AD 96-NM-122
Title: ICING CONDITIONS\SHORT BROTHERS\SD3-60\SD3-SHERPA SERIES
Organization: FAA
Status: Active
AD 96-NM-24
Title: WING ENGINE PYLON\MCDONNELL DOUGLAS CORP\DC-10-15
Organization: FAA
Status: Active
AD 96-NM-10
Title: STRUCTURAL INTEGRITY OF FRAME 47\AIRBUS INDUSTRIE\A300-600
Organization: FAA
Status: Active
AD 96-ANE-08
Title: LOW PRESSURE TURBINE (LPT) SEAL PLATE\ALLIEDSIGNAL\TFE 731-2A\TFE 731-3C\TFE 731-3CR
Organization: FAA
Status: Active
AD 96-NM-91
Title: COLLAPSE OF THE MAIN LANDING GEAR (MLG)\MCDONNELL DOUGLAS CORP\DC-9-10\DC-9-11\DC-9-12\DC-9-13\DC-9-14\DC-9-15\DC-9-15F\DC-9-21\DC-9-31\DC-9-32 (VC-9C)\DC-9-32F (C-9A, C-9B)\DC-9-33F\DC-9-34\DC-9-3...
Organization: FAA
Status: Active
AD 96-ANE-09
Title: COMPRESSOR STALL\ROLLS-ROYCE LTD\RB-211-535E4\RB-211-535E4B
Organization: FAA
Status: Active
AD 96-NM-06
Title: OVERLOAD OF THE STATIC INVERTER\BOEING\737-100 SERIES\737-200 SERIES (T-43)
Organization: FAA
Status: Active
AD 96-NM-81
Title: TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEMS (TCAS)\ALLIED-SIGNAL AEROSPC\TCAS II
Organization: FAA
Status: Active
AD 96-NM-54
Title: FUEL HOSE ASSEMBLY ON THE AUXILIARY POWER UNIT (APU)\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-1000A/HAWKER 1000
Organization: FAA
Status: Active
AD 96-NM-25
Title: COLLAPSE OF THE MAIN LANDING GEAR (MLG)\BOEING\767-200 SERIES\767-300 SERIES\767-300F SERIES
Organization: FAA
Status: Active
AD 96-ANE-02
Title: FAN BLADE FAILURE\PRATT & WHITNEY\JT8D-209\JT8D-217\JT8D-217A\JT8D-217C\JT8D-219
Organization: FAA
Status: Active
AD 96-CE-16
Title: AILERON MASS BALANCE ATTACHMENT\PILATUS BRITTEN-NORMAN LTD (SEE BRITTEN-NORMAN)\BN-2\BN-2A SERIES\BN-2A MARK III
Organization: FAA
Status: Active
AD 96-NM-63
Title: LATERAL CONTROL CHARACTERISTICS\LEARJET CORP\35\35A\36\36A
Organization: FAA
Status: Active
AD 96-NM-90
Title: STRESS CORROSION CRACKING OF THE LOWER WING PLANKS\GULFSTREAM AMERICAN & GULFSTREAM AEROSPACE\G-1159 SERIES (G-II)\G-1159A (G-III)\G-1159B SERIES (G-IIB)
Organization: FAA
Status: Active
AD 96-NM-36
Title: FAILURE OF HYDRAULIC FUSE\BOEING\737-100 SERIES\737-200 SERIES (T-43)\747-100 SERIES\747-200 SERIES\747-300 SERIES\747SP
Organization: FAA
Status: Active
AD 96-NM-49
Title: UNCOMMANDED RETRACTION OF THE LANDING GEAR\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 96-CE-09
Title: MAIN LANDING GEAR (MLG) SIDE BRACE STUD CRACKS\PIPER\PA-24\PA-24-250\PA-24-260\PA-24-400\PA-30\PA-39
Organization: FAA
Status: Active
AD 96-NM-39
Title: TRUNNION BOLTS\MCDONNELL DOUGLAS CORP\DC-10-10\DC-10-10F\DC-10-15
Organization: FAA
Status: Active
AD 96-NM-31
Title: FUEL SYSTEM CROSSFEED VALVE\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES\737 SERIES (T-43)
Organization: FAA
Status: Active
AD 96-NM-04
Title: FAILURE OF HYDRAULIC SYSTEM\BOEING\737-100 SERIES\737-200 SERIES (T-43)
Organization: FAA
Status: Active
AD 96-NM-35
Title: THRUST DECAY CHARACTERISTICS\LOCKHEED AIRCRFT CORP LOCKHEED-GEORGIA CO & LOCKHEED-CALIF CO\382 SERIES\382E\382G
Organization: FAA
Status: Active
AD 96-NM-19
Title: ICING CONDITIONS\EMPRESA BRASILEIRA DE AERONAUTICA S A\EMB-120 SERIES
Organization: FAA
Status: Active
AD 96-CE-01
Title: ICING CONDITIONS\DEHAVILLAND\DHC-6 SERIES (TWIN OTTER)
Organization: FAA
Status: Active
AD 96-CE-02
Title: ICING CONDITIONS\EMPRESA BRASILEIRA DE AERONAUTICA S A\EMB-110P1\EMB-110P2
Organization: FAA
Status: Active
AD 96-CE-03
Title: ICING CONDITIONS\BEECH AIRCRAFT\99 SERIES\99A\A99A\B99\C99\B200\B200C\1900\1900C (C-12J)\1900D
Organization: FAA
Status: Active
AD 96-CE-04
Title: ICING CONDITIONS\DORNIER-WERKE G M B H\DO 228-100\DO 228-101\DO 228-200\DO 228-201\DO 228-202\DO 228-212
Organization: FAA
Status: Active
AD 96-CE-05
Title: ICING CONDITIONS\CESSNA\208\208B
Organization: FAA
Status: Active
AD 96-CE-06
Title: ICING CONDITIONS\FAIRCHILD AIRCRFT CORP\SA226-T\SA226-T(B)\SA226-AT\SA226-TC\SA227-TT\SA227-AT\SA227-AC\SA227-BC\SA227-CC\SA227-DC
Organization: FAA
Status: Active
AD 96-NM-13
Title: ICING CONDITIONS\BRITISH AEROSPACE\ATP SERIES
Organization: FAA
Status: Active
AD 96-NM-14
Title: ICING CONDITIONS\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 96-NM-15
Title: ICING CONDITIONS\BRITISH AEROSPACE\HS 748 SERIES 2A\HS 748 SERIES 2B
Organization: FAA
Status: Active
AD 96-NM-16
Title: ICING CONDITIONS\SAAB-SCANIA AB\SF-340A\SAAB 340B SERIES\2000
Organization: FAA
Status: Active
AD 96-NM-17
Title: ICING CONDITIONS\CONSTRUCCIONES AERONAUTICAS S A (CASA)\C-212 SERIES\CN-235 SERIES
Organization: FAA
Status: Active
AD 96-NM-18
Title: ICING CONDITIONS\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
AD 96-NM-20
Title: ICING CONDITIONS\DEHAVILLAND\DHC-7 SERIES\DHC-8 SERIES
Organization: FAA
Status: Active
AD 96-NM-21
Title: ICING CONDITIONS\FOKKER-VFW B V\F.27 MARK 050\F.27 MARK 100\F.27 MARK 200\F.27 MARK 300\F.27 MARK 400\F.27 MARK 500\F.27 MARK 600\F.27 MARK 700
Organization: FAA
Status: Active
AD 97-NM-201
Title: ENSURE CONTINUED STRUCTURAL INTEGRITY OF THESE AIRPLANES (DORNIER LUFTFAHRT GMBH MODEL 328-100 SERIES)\SHORT BROTHERS\SD3-30\SD3-60\SD3-SHERPA SERIES\DORNIER-WERKE G M B H\328-100 SERIES
Organization: FAA
Status: Active
AD 97-NM-273-R1
Title: R1 ENSURE CONTINUED STRUCTURAL INTEGRITY OF THESE AIRPLANES (ATR72 SERIES)\AEROSPATIALE\ATR72-101\ATR72-102\ATR72-201\ATR72-202\ATR72-211\ATR72-212\ATR72-212A
Organization: FAA
Status: Active
AD 97-NM-184
Title: PREVENT RAPID DECOMPRESSION OF THE AIRPLANE DUE TO BONDING DELAMINATION AND CRACKING OF THE FUSELAGE\AIRBUS INDUSTRIE\A300-B2-1A\A300-B2-1C\A300-B2-203\A300-B2K-3C\A300-B4-103\A300-B4-203\A300-B4-2...
Organization: FAA
Status: Active
AD 97-NM-260
Title: MINIMIZE CONTAMINATION OF THE SWITCH CONTACTS AND CONSEQUENT FAILURE OF THE SWITCHES, WHICH, IF NOT CORRECTED, COULD RESULT IN INABILITY OF THE FLIGHT CREW TO ACTIVATE THE CARGO FIRE EXTINGUISHING,...
Organization: FAA
Status: Active
AD 97-ANE-44
Title: PREVENT FRONT PYLON MOUNT BOLT AND PRIMARY MOUNT THRUST LOAD PATH FAILURE\PRATT & WHITNEY\PW4164\PW4168 SERIES\PW4168A\AIRBUS INDUSTRIE\A330-301 SERIES\A330-321 SERIES\A330-322 SERIES\A330-341 SERI...
Organization: FAA
Status: Active
AD 97-NM-88
Title: DETECT AND CORRECT FATIGUE CRACKING OF THE LONGERON SPLICE FITTINGS AT STRINGER 11\BOEING\747-100 SERIES\747-200 SERIES\747-300 SERIES\747SP\747SR
Organization: FAA
Status: Active
AD 97-NM-235
Title: PREVENT STRUCTURAL FAILURE OF THE MAIN DECK CARGO DOOR HINGE OR FAILURE OF THE CARGO DOOR SYSTEM\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES
Organization: FAA
Status: Active
AD 97-NM-234
Title: PREVENT STRUCTURAL FAILURE OF THE MAIN DECK CARGO DOOR HINGE OR FAILURE OF THE CARGO DOOR SYSTEMS\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES
Organization: FAA
Status: Active
AD 97-NM-233
Title: PREVENT STRUCTURAL FAILURE OF THE MAIN DECK CARGO DOOR HINGE OR FAILURE OF THE CARGO DOOR SYSTEM\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES
Organization: FAA
Status: Active
AD 97-NM-232
Title: PREVENT STRUCTURAL FAILURE OF THE MAIN DECK CARGO DOOR HINGE OR FAILURE OF THE CARGO DOOR SYSTEM\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES
Organization: FAA
Status: Active
AD 97-CE-99
Title: DETECT AND CORRECT MIGRATION OF THE WING ATTACHMENT BUSHES IN THE FUSELAGE FRONT AND REAR SPAR FRAMES\SHORT BROTHERS\SC-7 SERIES 2\SC-7 SERIES 3
Organization: FAA
Status: Active
AD 97-NM-323
Title: PREVENT FATIGUE CRACKS OF THE FRONT SPAR WEB OF THE CENTER SECTION OF THE WINGS\BOEING\727 SERIES
Organization: FAA
Status: Active
AD 97-NM-270
Title: ENSURE CONTINUED STRUCTURAL INTEGRITY OF THESE AIRPLANES (ATR42 SERIES)\AEROSPATIALE\ATR42 SERIES
Organization: FAA
Status: Active
AD 97-NM-273
Title: ENSURE CONTINUED STRUCTURAL INTEGRITY OF THESE AIRPLANES\AEROSPATIALE\ATR72 SERIES
Organization: FAA
Status: Active
AD 97-CE-67
Title: DETECT AND CORRECT CRACKS AND CORROSION IN THE EXHAUST SYSTEM\CESSNA\T310P\T310Q\T310R\320\320-1\320A\320B\320C\320D\320E\320F\335\340\340A\321 (NAVY OE-2)\401\401A\401B\402\402A\402B\402C\404\411\...
Organization: FAA
Status: Active
AD 97-NM-58
Title: PREVENT DAMAGE TO CERTAIN HYDRAULIC SYSTEM COMPONENTS IN THE NUMBER 2 ENGINE NACELLE\DEHAVILLAND\DHC-8-100 SERIES\DHC-8-300
Organization: FAA
Status: Active
AD 97-SW-06
Title: LOSS OF THE COMMON GROUND OF THE TWO TRANSFORMER-RECTIFIERS\EUROCOPTER FRANCE (FORMERLY AEROSPATIALE)\SA330F\SA330G\SA330J
Organization: FAA
Status: Active
AD 97-CE-103
Title: OPERATOR USING INACCURATE WEIGHT AND BALANCE INFORMATION PROVIDED IN THE SAILPLANE FLIGHT MANUAL (SFM)\ALEXANDER SCHLEICHER\ASK 21
Organization: FAA
Status: Active
AD 97-NM-133
Title: PREVENT A REDUCED RATE OF MOVEMENT OF THE ELEVATOR, AILERON, OR RUDDER\BOEING\737-100 SERIES\737-200 SERIES (T-43)\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 97-NM-151
Title: EXCESSIVE WEAR ON THE AILERON CONTROL CABLES, CABLE GUIDES, AND CABLE PULLEYS LOCATED AT THE REAR WING SPARS\SAAB-SCANIA AB\2000 SERIES
Organization: FAA
Status: Active
AD 97-SW-59
Title: PREVENT FAILURE OF THE PLATE DUE TO FATIGUE CRACKING\SIKORSKY AIRCRFT DIV OF UNITED AIRCRFT CORP\CH-54B
Organization: FAA
Status: Active
AD 97-NM-276
Title: ENSURE CONTINUED STRUCTURAL INTEGRITY\BOEING\767-200 SERIES\767-300 SERIES
Organization: FAA
Status: Active
AD 97-ANE-36
Title: PREVENT PROPELLER HUB CRACKS\MT-PROPELLER ENTWICKLUNG GMBH\MTV-3-B-C/L250-21
Organization: FAA
Status: Active
AD 97-CE-32
Title: FAILURE OF THE ELEVATOR SPAR CAUSED BY FATIGUE CRACKING\PIPER\PA-31\PA-31-300\PA-31-325\PA-31-350\PA-31P-350
Organization: FAA
Status: Active
AD 97-CE-07
Title: PREVENT DEVIATION FROM AN INTENDED FLIGHT PATH DURING A NON-PRECISION APPROACH CAUSED BY INACCURATE INFORMATION FROM THE GPS FLIGHT MANAGEMENT SYSTEM\ALLIEDSIGNAL AVIONICS INC\GNS-XLS\GNS-XL
Organization: FAA
Status: Active
AD 97-NM-195
Title: PREVENT FATIGUE-RELATED CRACKING IN THE SHEAR CLEATS OF THE ROLLER GUIDE STRUCTURAL SUPPORT OF THE PASSENGER DOOR\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPC )\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 97-SW-41
Title: PREVENT FAILURE OF THE SPINDLES OR PINS THAT COULD RESULT IN LOSS OF A MAIN ROTOR BLADE\EUROCOPTER FRANCE (FORMERLY AEROSPATIALE)\AS332C\AS332L\AS332L1
Organization: FAA
Status: Active
AD 97-CE-10
Title: PREVENT LOSS OF AIRPLANE CONTROL OR ENGINE OVERSPEED WITH CONSEQUENT LOSS OF ENGINE POWER CAUSED BY THE POWER LEVERS BEING POSITIONED AFT OF THE FLIGHT IDLE STOP WHILE THE AIRPLANE IS IN FLIGHT\DEH...
Organization: FAA
Status: Active
AD 97-NM-153-R1
Title: PREVENT CRACKS IN THE CENTER WING BOX ANGLE FITTING\AIRBUS INDUSTRIE\A300-600
Organization: FAA
Status: Active
AD 97-CE-152
Title: PREVENT FAILURE OF THE HORIZONTAL STABILIZER REAR SPAR CAUSED BY CRACKS AT THE ELEVATOR OUTBOARD HINGE ATTACHMENT\PIPER\PA-31\PA-31-300\PA-31-325\PA-31-350\PA-31P-350
Organization: FAA
Status: Active
AD 97-CE-137
Title: PREVENT THE STABILIZER FROM DETACHING AT THE FORWARD STABILIZER ATTACH FLANGES\DORNIER-WERKE G M B H\DO 27 Q-6
Organization: FAA
Status: Active
AD 97-CE-122
Title: DETECT AND CORRECT CRACKS IN THE BRAKE TORQUE TUBE ASSEMBLIES\BRITISH AEROSPC\B.121 SERIES 1\B.121 SERIES 2\B.121 SERIES 3
Organization: FAA
Status: Active
AD 97-NM-315
Title: DETECT AND CORRECT CRACKING OF THE BULKHEAD WEB AND CAP\LOCKHEED AIRCRFT CORP LOCKHEED-GEORGIA CO AND LOCKHEED-CALIF CO\L-1011-385 SERIES
Organization: FAA
Status: Active
AD 97-NM-129
Title: PREVENT CRACKING OF THE OUTER LINKS OF THE SIDE STAYS OF THE MAIN LANDING GEAR (MLG)\BRITISH AEROSPC\BAE 146 SERIES\AVRO 146-RJ SERIES
Organization: FAA
Status: Active
AD 97-CE-83
Title: PREVENT ELECTROMAGNETIC INTERFERENCE (EMI) ON THE ENGINE ELECTRONIC MODULE\HOAC AUSTRIA (FORMERLY HOFFMANN AIRCRAFT)\DV-20 KATANA
Organization: FAA
Status: Active
AD 97-CE-16
Title: PREVENT JAMMING OF THE ELEVATOR TRIM TAB ACTUATOR CAUSED BY ICE FORMATIONS\BEECH AIRCRFT\B300\B300C
Organization: FAA
Status: Active
AD 97-CE-139
Title: DETECT AND CORRECT FATIGUE CRACKING OF THE WING UPPER SPAR CAP\AEROSTAR AIRCRFT CORP (FORMERLY PIPER TED SMITH)\PA-60-600 (AEROSTAR 600)\PA-60-601P (AEROSTAR 601P)\PA-60-700P (AEROSTAR 700P)\PA-60-...
Organization: FAA
Status: Active
AD 97-CE-153
Title: HELP PREVENT PASSENGERS AND CREW FROM NOT BEING ABLE TO OPEN THE EMERGENCY EXIT DOORS DURING AN AIRPLANE EMERGENCY\BEECH AIRCRFT\1900\1900C (C-12J)\1900D
Organization: FAA
Status: Active
AD 97-NM-192
Title: PREVENT FATIGUE CRACKING OF THE UPPER FRAME FLANGES\AIRBUS INDUSTRIE\A320 SERIES
Organization: FAA
Status: Active
AD 97-NM-04-R1
Title: PREVENT FAILURE OF THE ALTERNATE RELEASE MECHANISM OF THE FLIGHT COMPARTMENT DOOR\DEHAVILLAND\DHC-8-100 SERIES\DHC-8-200\DHC-8-300
Organization: FAA
Status: Active
AD 97-NM-53
Title: PREVENT CORROSION OF THE FORWARD TRUNNION JOINT OF THE MAIN LANDING GEAR (MLG)\BOEING\767-200 SERIES\767-300 SERIES\767-300F SERIES
Organization: FAA
Status: Active
AD 97-NM-87
Title: DETECT AND CORRECT FATIGUE CRACKING OF CERTAIN LOWER LOBE FUSELAGE FRAMES\BOEING\747-100 SERIES\747-200 SERIES\747-300 SERIES
Organization: FAA
Status: Active
AD 97-NM-241
Title: PREVENT FAILURE OF THE BRAKE HOUSING IN THE TORQUE ROD REGION\BOEING\767-200 SERIES\767-300 SERIES\767-300F SERIES
Organization: FAA
Status: Active
AD 97-NM-339
Title: TO PREVENT INABILITY OF THE MAIN ENTRANCE DOOR TO OPEN\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPC )\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 97-NM-292
Title: TO PREVENT COLLAPSE OF THE MAIN LANDING GEAR (MLG) DUE TO FRACTURING OF THE SHOCK STRUT CYLINDER\MCDONNELL DOUGLAS CORP\DC-9-81\DC-9-82\DC-9-83\DC-9-87\MD-88
Organization: FAA
Status: Active
AD 97-NM-107
Title: PREVENT OBSTRUCTIONS IN THE AIR EXTRACTION SYSTEM OF THE LAVATORY\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325\A300-600\A320-111\A320-200\A320-211\A320-212\A320-2...
Organization: FAA
Status: Active
AD 97-NM-106-R1
Title: DETECT AND CORRECT CORROSION AND/OR WEAR OF THE TOP AND BOTTOM SHEAR DECKS OF THE LEFT AND RIGHT STUB WINGS\SHORT BROTHERS\SD3-60\SD3-60 SHERPA SERIES
Organization: FAA
Status: Active
AD 97-NM-42
Title: PREVENT PITCH-UP OF THE AIRPLANE DUE TO ACTIVATION OF THE SPOILERS DURING AN AUTOMATIC LANDING\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233
Organization: FAA
Status: Active
AD 97-NM-227
Title: DETECT AND CORRECT FATIGUE CRACKING BETWEEN THE UPPER AND LOWER SILLS OF THE NUMBER 1 CARGO DOOR\BOEING\727-200 SERIES
Organization: FAA
Status: Active
AD 97-NM-51
Title: DETECT AND CORRECT CRACKING AND CORROSION OF THE FUSE PINS\BOEING\767-200 SERIES\767-300 SERIES\767-300F SERIES
Organization: FAA
Status: Active
AD 97-NM-159
Title: PREVENT FATIGUE CRACKING OF CERTAIN FASTENER HOLES ON THE OUTER FRAMES OF THE FUSELAGE\AIRBUS INDUSTRIE\A320-111\A320-211\A320-231
Organization: FAA
Status: Active
AD 97-NM-144
Title: PREVENT NAV/COM RADIOS FROM SIMULTANEOUSLY CHANGING TUNED FREQUENCIES AND TRANSPONDER CODES\SAAB-SCANIA AB\2000
Organization: FAA
Status: Active
AD 97-NM-92
Title: DETECT AND CORRECT FATIGUE CRACKING IN THE MANHOLE DOUBLERS OF THE LOWER WING PANELS\MITSUBISHI AIRCRFT INTNL AND MITSUBISHI HEAVY IND\YS-11
Organization: FAA
Status: Active
AD 97-NM-185
Title: PREVENT FATIGUE CRACKING OF THE SPRING BEAM\BOEING\747-100 SERIES\747-100B\747-200 SERIES\747-200B SERIES\747-200C SERIES\747-200F SERIES\747-300 SERIES\747-400 SERIES\747-400D\747-400F\747SP\747SR...
Organization: FAA
Status: Active
AD 97-CE-138
Title: TO PREVENT ONE OR BOTH WHEEL SKIS FROM ROTATING INTO A NOSE-DOWN POSITION DURING FLIGHT\CESSNA\180\180A\180B\180C\180D\180E\180F\180G\180H\180J\180K\185\185A\185B\185C\185D\185E\A185E\A185F
Organization: FAA
Status: Active
AD 97-ANE-53
Title: PREVENT HIGH PRESSURE COMPRESSOR (HPC) SURGE\PRATT & WHITNEY\PW4152\PW4056\PW4156\PW4256\PW4052\PW4158\PW4060\PW4160\PW4460\PW4050\PW4060A\PW4156A\PW4062\PW4462\PW4060C\PW4650
Organization: FAA
Status: Active
AD 97-ANE-58
Title: PREVENT CYLINDER HEAD CRACKING\PRATT & WHITNEY\R-1340
Organization: FAA
Status: Active
AD 97-SW-64
Title: TO PREVENT VIBRATIONS CAUSED BY DISBONDING OF THE CENTER SECTION OF A FREQUENCY ADAPTER FROM THE ELASTOMER ON THE MAIN ROTOR HEAD AND SUBSEQUENT REDUCED CONTROLLABILITY OF THE HELICOPTER\EUROCOPTER...
Organization: FAA
Status: Active
AD 97-SW-61
Title: TO PREVENT FAILURE OF THE SPLINE TEETH IN EACH INPUT SHAFT COUPLING ASSEMBLY (COUPLING ASSEMBLY), LOSS OF DRIVE TO THE MAIN ROTOR SYSTEM\MCDONNELL DOUGLAS HELICPTR (SEE SCHWEIZER AIRCRFT CORP )\369...
Organization: FAA
Status: Active
AD 97-SW-55
Title: TO PREVENT MAIN ROTOR PITCH CHANGE LINK SPHERICAL BEARING AXIAL PLAY DUE TO WEAR\AGUSTA S P A (FORMERLY SIAI MARCHETTI S P A AGUSTA CONSTRUZIONI AERONAUTICHE GIOVANNI) (SEE SIA\A109C\A109K2
Organization: FAA
Status: Active
AD 97-NM-325
Title: PREVENT ENGINE DAMAGE, AIRFRAME DAMAGE, AND/OR HAZARD TO PERSONS OR PROPERTY ON THE GROUND AS A RESULT OF 'BLUE ICE'\BOEING\747-100 SERIES\747-200 SERIES\747-300 SERIES\747SP\747-400F
Organization: FAA
Status: Active
AD 97-NM-258
Title: PREVENT A POTENTIAL FIRE HAZARD OR THE POSSIBLE LOSS OF ELEVATOR CONTROL SYSTEM REDUNDANCY\MCDONNELL DOUGLAS CORP\MD-90-30
Organization: FAA
Status: Active
AD 97-NM-187
Title: TO PREVENT A DEFECTIVE LIGHT BULB FROM CAUSING A SHORT CIRCUIT THAT EMITS SMOKE AND FUMES INTO THE COCKPIT, OR CAUSING DAMAGE TO THE CIRCUIT CARDS AND VARIOUS COMPONENTS\DORNIER-WERKE G M B H\DO 32...
Organization: FAA
Status: Active
AD 97-NM-186-A
Title: PREVENT POSSIBLE SEPARATION OF THE ENGINE FROM THE AIRPLANE IN THE EVENT OF A PRIMARY THRUST LINKAGE FAILURE\BOEING\767-200 SERIES\767-300 SERIES\767-300F SERIES
Organization: FAA
Status: Active


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