AD 00-CE-03
Title: CORRECT CHAFING DAMAGE AND CONSEQUENT LOSS OF ENGINE OIL CAUSED BY RUBBING PIPES\PILATUS AIRCRFT LTD\PC-12\PC-12/45
Organization: FAA
Status: Active
AD 00-CE-15
Title: CORRECT THE LACK OF A FIREWALL SEAL AND CONSEQUENT PROGRESSION OF FIRE AND SMOKE THROUGH THE FIREWALL PANEL INTO THE FLIGHT COMPARTMENT OR CABIN IN THE EVENT OF AN ENGINE COMPARTMENT FIRE\RAYTHEON\...
Organization: FAA
Status: Active
AD 00-NM-129
Title: PREVENT THE LOSS OF HYDRAULIC PRESSURE DUE TO FAILED HYDRAULIC TUBING\EMPRESA BRASILEIRA DE AERONAUTICA S A\EMB-145 SERIES
Organization: FAA
Status: Active
AD 00-NM-212
Title: PREVENT THE TURBINE AIR DISCHARGE DUCT OR WATER SEPARATOR OUTLET DUCT FROM DISCONNECTING FROM THE COLD AIR UNIT TURBINE OR FROM THE WATER SEPARATOR\RAYTHEON\BAE 125-800A\HAWKER 800 SERIES\HAWKER 80...
Organization: FAA
Status: Active
AD 00-CE-12
Title: DETECT, CORRECT, AND PREVENT FURTHER CRACKING IN THE RUDDER QUADRANT STRUCTURE CAUSED BY INCORRECTLY INSTALLED D-WASHERS\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPC )\JETSTREAM MODEL 3101\JETST...
Organization: FAA
Status: Active
AD 00-SW-14
Title: PREVENT FATIGUE CRACKING OF A BLADE, FAILURE OF A BLADE\EUROCOPTER FRANCE (FORMERLY AEROSPATIALE)\SA330F\SA330G\SA330J
Organization: FAA
Status: Active
AD 00-NM-18
Title: PREVENT FAILURE OF THE BEARING SUPPORT FITTING OF THE FORWARD TRUNNION\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES\727C
Organization: FAA
Status: Active
AD 00-NM-60
Title: PREVENT AN ASYMMETRIC BRAKING CONDITION AND A LONGER STOPPING DISTANCE DUE TO SUDDEN LOSS OF NORMAL BRAKING TO THE LEFT WHEEL\RAYTHEON\MU-300\MU-300-10\400\400A\400T
Organization: FAA
Status: Active
AD 00-SW-11
Title: PREVENT AN INACCURATE FUEL QUANTITY INDICATING SYSTEM READING, ENGINE FLAMEOUT DUE TO FUEL STARVATION, AND A SUBSEQUENT FORCED LANDING\BELL HELICPTR TEXTRON CANADA\430
Organization: FAA
Status: Active
AD 00-SW-22
Title: PREVENT LOSS OF ELECTRICAL POWER\BELL HELICPTR TEXTRON ***(SEE CA DEPT OF FORESTRY CONTNTL COPTERS GARLICK HAWKEYE ROTORWI\430
Organization: FAA
Status: Active
AD 00-CE-01
Title: PREVENT THE TAIL-FUSELAGE HINGE FAILING\AEROTECHNIK S R O\L 13 SEH VIVAT
Organization: FAA
Status: Active
AD 00-NM-52
Title: PREVENT ELECTRICAL ARCING BETWEEN THE OXYGEN TUBING AND AN ELECTRICAL SOURCE WHICH COULD RESULT IN AN OXYGEN FIRE\LEARJET CORP\60
Organization: FAA
Status: Active
AD 00-NM-03
Title: PREVENT THE INABILITY TO EXTEND THE NOSE LANDING GEAR\RAYTHEON\HAWKER 800XP SERIES\HAWKER 800A (U-125A)
Organization: FAA
Status: Active
AD 00-NM-46
Title: PREVENT CHAFING OF THE WIRE BUNDLE TO RELAY 'KT' ON PANEL 'JA'\RAYTHEON\HAWKER 800XP SERIES
Organization: FAA
Status: Active
AD 00-NM-63
Title: PREVENT JAMMING OF THE ROLL CONTROL SYSTEM (AILERONS AND SPOILERS)\CESSNA\750
Organization: FAA
Status: Active
AD 00-CE-28
Title: CORRECT POTENTIAL BRAKE SHUTTLE VALVE PROBLEMS, WHICH COULD CAUSE THE BRAKE ASSEMBLY TO DRAG AND OVERHEAT\FAIRCHILD AIRCRFT CORP\SA226-T\SA226-T(A)\SA226-T(B)\SA226-AT\SA226-TC\SA227-TT\SA227-TT(30...
Organization: FAA
Status: Active
AD 00-NM-48
Title: PREVENT THE FIRE WARNING FROM TERMINATING PREMATURELY\AIRBUS INDUSTRIE\A310-200\A310-200ADV\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325\A300-600
Organization: FAA
Status: Active
AD 00-NM-76
Title: PREVENT HIGH BEARING STRESS ON THE BUSHINGS IN THE FLAP FITTINGS\SAAB-SCANIA AB\SF-340A
Organization: FAA
Status: Active
AD 00-NM-134
Title: DETECT AND CORRECT FATIGUE CRACKING OF THE FRONT SPAR WEB OF THE WING\BOEING\747-100 SERIES\747-100B\747-100B SUD\747-200 SERIES\747-200B SERIES\747-200C SERIES\747-200F SERIES\747-300 SERIES\747-4...
Organization: FAA
Status: Active
AD 00-NM-121
Title: PREVENT OVERHEATING OF THE WIRE BETWEEN CERTAIN CIRCUIT BREAKERS, WHICH COULD RESULT IN SMOKE EMISSIONS IN THE COCKPIT\EMPRESA BRASILEIRA DE AERONAUTICA S A\EMB-120 SERIES
Organization: FAA
Status: Active
AD 00-NM-35
Title: PREVENT DAMAGED ELECTRICAL WIRES OR DAMAGED DOOR ACTUATION CABLES DUE TO CHAFING BY THE CABLES DURING OPERATION OF THE FORWARD PASSENGER DOOR\MCDONNELL DOUGLAS CORP\MD-11 SERIES
Organization: FAA
Status: Active
AD 00-NM-38
Title: PREVENT OVERHEATING OF THE ELECTRICAL PINS INSIDE THE CARGO CONTROL UNITS (CCU)\MCDONNELL DOUGLAS CORP\MD-11 SERIES
Organization: FAA
Status: Active
AD 00-NM-28
Title: PREVENT SMOKE AND FIRE IN THE FORWARD CARGO COMPARTMENT\MCDONNELL DOUGLAS CORP\MD-11 SERIES
Organization: FAA
Status: Active
AD 00-NM-36
Title: PREVENT ELECTRICAL ARCING AND/OR HEAT DAMAGED WIRES DUE TO IMPROPER WIRE INSTALLATIONS DURING MANUFACTURE AND/OR MAINTENANCE OF THE AIRPLANE\MCDONNELL DOUGLAS CORP\MD-11 SERIES
Organization: FAA
Status: Active
AD 00-NM-37
Title: PREVENT FIRE AND SMOKE IN CERTAIN WIRE BUNDLES THAT ARE ROUTED TO AND FROM THE MAIN AVIONICS COMPARTMENT OR CENTER ACCESSORY COMPARTMENT\MCDONNELL DOUGLAS CORP\MD-11 SERIES
Organization: FAA
Status: Active
AD 00-NM-34
Title: PREVENT ARCING AND HEAT DAMAGE TO THE ATTACHMENT POINTS OF THE MAIN EXTERNAL AND GALLEY POWER RECEPTACLE GROUND WIRE, INSULATION BLANKETS OUTBOARD AND AFT OF THE RECEPTACLE AREA, AND ADJACENT POWER...
Organization: FAA
Status: Active
AD 00-NM-179
Title: PREVENT CORROSION FROM DEVELOPING ON THE UNDERSIDE OF THE TOP SKIN OF THE CENTER WING\BRITISH AEROSPC\BAE 146 SERIES\AVRO 146-RJ SERIES
Organization: FAA
Status: Active
AD 00-NM-29
Title: PREVENT INSUFFICIENT CLEARANCE AND CONTACT BETWEEN THE B7-28 BUS AND AN ADJACENT PANEL\MCDONNELL DOUGLAS CORP\MD-11 SERIES\MD-11F SERIES
Organization: FAA
Status: Active
AD 00-NM-31
Title: DETECT DISCREPANCIES THAT INCLUDE BUT ARE NOT LIMITED TO FRAYED, CHAFED, OR NICKED WIRES AND WIRE INSULATION\MCDONNELL DOUGLAS CORP\MD-11 SERIES\MD-11F SERIES
Organization: FAA
Status: Active
AD 00-NM-32
Title: PREVENT ELECTRICAL SHORTING OF THE BRAKE COILS OF THE AUTO THROTTLE SERVO (ATS) OR ELEVATOR LOAD FEEL (ELF)/FLAP LIMITER (FL) DUPLEX ACTUATOR\MCDONNELL DOUGLAS CORP\MD-11 SERIES\MD-11F SERIES
Organization: FAA
Status: Active
AD 00-NM-33
Title: PREVENT ARCING AND SPARKING DAMAGE TO THE POWER FEEDER CABLES, TERMINAL STRIPS, AND ADJACENT STRUCTURE\MCDONNELL DOUGLAS CORP\MD-11 SERIES
Organization: FAA
Status: Active
AD 00-NM-17
Title: PREVENT ELECTROMAGNETIC INTERFERENCE WITH THE ANTI-SKID CONTROL SYSTEM\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 00-NM-133
Title: PREVENT RUPTURE OF THE HYDRAULIC LINE AND LOSS OF HYDRAULIC PRESSURE DUE TO CHAFING\EMPRESA BRASILEIRA DE AERONAUTICA S A\EMB-120 SERIES
Organization: FAA
Status: Active
AD 00-SW-24
Title: PREVENT A HORIZONTAL STABILIZER SLAT (SLAT) FROM SEPARATING, IMPACT WITH A MAIN OR TAIL ROTOR BLADE, AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER\BELL HELICPTR TEXTRON CANADA\407
Organization: FAA
Status: Active
AD 00-NM-130
Title: PREVENT DETERIORATION AND DEFORMATION OF THE MASS-BALANCE WEIGHTS OF THE AILERON\EMPRESA BRASILEIRA DE AERONAUTICA S A\EMB-120 SERIES
Organization: FAA
Status: Active
AD 00-CE-09-1
Title: DETECT AND CORRECT CRACKS IN THE WING SPAR ASSEMBLIES\RAYTHEON\45 (YT-34)\A45 (T34A, B45)\D45 (T-34B)
Organization: FAA
Status: Active
AD 00-NM-04
Title: PREVENT FAILURE OF THE FRONT SPAR ATTACHMENT AND UPPER CAP OF THE ENGINE PYLONS DUE TO FATIGUE CRACKING\MCDONNELL DOUGLAS CORP\DC-9-10\DC-9-20\DC-9-30\DC-9-40\DC-9-50\C-9 (MILITARY) SERIES
Organization: FAA
Status: Active
AD 00-NM-202
Title: PREVENT BREAKAGE OF THE POWER CONTROL CABLE ASSEMBLIES DUE TO THE INFLEXIBLE CONSTRUCTION OF THE CABLE\SHORT BROTHERS\SD3-60 SHERPA SERIES
Organization: FAA
Status: Active
AD 00-NM-10
Title: PREVENT THE CONTROL LINK OF THE AILERON AUTOPILOT SERVO FROM BEING DRIVEN OVERCENTER\ISRAEL AIRCRFT IND LTD\ASTRA SPX SERIES\1125 WESTWIND ASTRA SERIES
Organization: FAA
Status: Active
AD 00-NM-146
Title: PREVENT CHAFING OF WIRE BUNDLES IN TWO JUNCTION BOXES IN THE MAIN WHEEL WELL\BOEING\737-100 SERIES\737-200 SERIES\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 00-NM-132
Title: PREVENT THE AIRPLANE FROM DEPARTING THE RUNWAY AT HIGH SPEEDS DURING LANDING DUE TO BENDING AND DAMAGE TO THE SQUAT SWITCH ASSEMBLY OF THE NOSE LANDING GEAR\LEARJET CORP\45 SERIES
Organization: FAA
Status: Active
AD 00-NM-07
Title: PREVENT CRACKING OF THE HYDRAULIC LINES\DORNIER-WERKE G M B H\328-300 SERIES
Organization: FAA
Status: Active
AD 00-NM-62
Title: DETECT AND CORRECT EXCESS BACKLASH OF THE SPHERICAL BEARING OF THE ACTIVE AILERON SERVO-CONTROLS\AIRBUS INDUSTRIE\A330-301 SERIES\A330-321 SERIES\A330-322 SERIES\A330-341 SERIES\A330-342 SERIES\A34...
Organization: FAA
Status: Active
AD 00-CE-29
Title: CORRECT SUBSTANDARD QUALITY COCKPIT VOICE RECORDINGS CAUSED BY THE CONFIGURATION OF THE PRESENT CVR SYSTEM, WHICH COULD AFFECT AIR SAFETY IF IMPORTANT INFORMATION THAT THE CVR PROVIDES IS NOT AVAIL...
Organization: FAA
Status: Active
AD 00-NM-104
Title: PREVENT A SUDDEN CHANGE IN PITCH DUE TO AN OUT-OF-TRIM CONDITION COMBINED WITH AN AUTOPILOT DISCONNECT\AIRBUS INDUSTRIE\A300-B2-203\A300-B4-203\A300-600\A300-600R\A310-200\A310-200ADV\A310-221\A310...
Organization: FAA
Status: Active
AD 00-NM-107
Title: PREVENT A SEVERE ASYMMETRIC THRUST CONDITION DURING FLIGHT WHICH COULD RESULT IN LOSS OF CONTROL OF THE AIRPLANE\BOEING\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 00-NM-127
Title: PREVENT INCAPACITATION OF THE FLIGHTCREW AND CONSEQUENT LOSS OF CONTROL OF THE AIRPLANE DUE TO DELAYS IN DONNING OXYGEN MASKS IN RESPONSE TO THE ACTIVATION OF THE CABIN ALTITUDE WARNING HORN\LEARJE...
Organization: FAA
Status: Active
AD 00-SW-03
Title: PREVENT DAMAGE TO THE LONGITUDINAL DRIVE LINK\MCDONNELL DOUGLAS HELICPTR (SEE SCHWEIZER AIRCRFT CORP )\MD-900
Organization: FAA
Status: Active
AD 00-NM-12
Title: PREVENT THE DISPLAY OF INCORRECT ENGINE LIMITATIONS, WHICH COULD RESULT IN AN OVERSPEED OF THE PROPELLERS AND POTENTIAL FOR BLADE FAILURE\SHORT BROTHERS\SD3-60
Organization: FAA
Status: Active
AD 00-SW-10
Title: PREVENT THE TAIL ROTOR BLADES FROM STRIKING THE TAILBOOM\BELL HELICPTR TEXTRON CANADA\407
Organization: FAA
Status: Active
AD 00-NM-105
Title: PREVENT CRACKING OF THE CENTER SECTION OF THE FUSELAGE\AIRBUS INDUSTRIE\A300-600\A300-600R
Organization: FAA
Status: Active
AD 00-NM-100
Title: PREVENT OPENING OF THE CARGO DOOR WHILE THE AIRPLANE IS IN FLIGHT\MCDONNELL DOUGLAS CORP\DC-8-63F\DC-8-62F\DC-8-71F\DC-8-72F\DC-8-73F
Organization: FAA
Status: Active
AD 00-NM-91
Title: PREVENT DAMAGE TO THE 90-MINUTE AUXILIARY POWER UNIT (APU) STANDBY POWER FEEDER CABLE\BOEING\767-200 SERIES\767-200ER SERIES\767-300 SERIES\767-300ER SERIES\767-300F SERIES\767-400ER SERIES
Organization: FAA
Status: Active
AD 00-CE-09
Title: DETECT AND CORRECT CRACKS IN THE WING SPAR ASSEMBLIES AND ASSURE THE OPERATIONAL SAFETY OF THE ABOVE-REFERENCED AIRPLANES\RAYTHEON\45 (YT-34)\A45 (T34A, B45)\D45 (T-34B)
Organization: FAA
Status: Active
AD 00-NM-50
Title: PREVENT IN-FLIGHT LOSS OF INBOARD AND OUTBOARD FLAP ASSEMBLIES DUE TO FAILURE OF H-11 ATTACHING BOLTS\MCDONNELL DOUGLAS CORP\DC-10-10\DC-10-15\DC-10-30\DC-10-30F (KC-10A)\DC-10-40
Organization: FAA
Status: Active
AD 00-NM-103
Title: PREVENT CRACKING OR BREAKING OF THE DOOR HANDLE MOUNTING HUB\BOEING\737-200 SERIES\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 00-NM-90
Title: PREVENT UNUSUAL HANDLING CHARACTERISTICS AND CONSEQUENT REDUCED CONTROLLABILITY DURING GROUND OPERATIONS DUE TO INCORRECT METHODS OF WEIGHING AND BALANCING THE AIRPLANE\BOMBARDIER INC (FORMERLY CAN...
Organization: FAA
Status: Active
AD 00-NM-69
Title: PREVENT UNWANTED DEPLOYMENT OF A THRUST REVERSER\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\KC-10
Organization: FAA
Status: Active
AD 00-SW-05
Title: PREVENT FAILURE OF A MAIN ROTOR BLADE DUE TO CORROSION ON THE INTERNAL SURFACE OF THE SPAR AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER\AGUSTA S P A (FORMERLY SIAI MARCHETTI S P A AGUSTA CONSTR...
Organization: FAA
Status: Active
AD 00-NM-56
Title: PREVENT FAILURE OF THE OVERWING EMERGENCY EXITS TO OPEN\DASSAULT AVI PARIS FRANCE (SEE AVIONS MARCEL DASSAULT A M D )\FALCON 2000\MYSTERE-FALCON 20\MYSTERE-FALCON 200\MYSTERE-FALCON 50\MYSTERE-FALC...
Organization: FAA
Status: Active
AD 00-NM-25
Title: PREVENT FALSE WARNING OF A HOT ENGINE EXHAUST TAILPIPE AND INTERMITTENT SIGNAL FAILURE\SAAB-SCANIA AB\SF-340A\SAAB 340B SERIES
Organization: FAA
Status: Active
AD 00-NM-77
Title: PREVENT FRACTURE OF THE LEAD SCREW OF THE POSITION 1 FLAP SCREW JACK\AIRBUS INDUSTRIE\A310-200\A310-200ADV\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325
Organization: FAA
Status: Active
AD 00-NM-49
Title: PREVENT OPENING OF THE CARGO DOOR WHILE THE AIRPLANE IS IN FLIGHT\MCDONNELL DOUGLAS CORP
Organization: FAA
Status: Active
AD 00-NM-66
Title: PREVENT AN INOPERATIVE BACKUP FLIGHT IDLE STOP SYSTEM\EMPRESA BRASILEIRA DE AERONAUTICA S A\EMB-120 SERIES
Organization: FAA
Status: Active
AD 00-NM-64
Title: DETECT AND CORRECT EXCESSIVE PLAY OF THE EYE-END OF THE PISTON ROD OF THE ELEVATOR SERVO-CONTROLS\AIRBUS INDUSTRIE\A330-301 SERIES\A330-321 SERIES\A330-322 SERIES\A330-341 SERIES\A330-342 SERIES\A3...
Organization: FAA
Status: Active
AD 00-NM-27
Title: DETECT CORROSION OF THE LOWER SURFACE OF THE WING CENTER SECTION AND THE SURROUNDING AREA\BOEING\727-100 SERIES
Organization: FAA
Status: Active
AD 00-CE-20
Title: INFORMATION NECESSARY TO ACTIVATE THE PNEUMATIC WING AND TAIL DEICING BOOTS AT THE FIRST SIGNS OF ICE ACCUMULATION IS CRITICAL FOR FLIGHT IN ICING CONDITIONS\PIPER\PA-42\PA-42-720\PA-42-720R\PA-42-...
Organization: FAA
Status: Active
AD 00-NM-22
Title: PREVENT AN INADVERTENT INCREASE IN THRUST\AIRBUS INDUSTRIE\A320-232\A320-233
Organization: FAA
Status: Active
AD 00-NM-23
Title: PREVENT FALSE SMOKE WARNINGS FROM THE CARGO COMPARTMENT SMOKE DETECTORS, WHICH COULD RESULT IN ABORTED TAKEOFFS, DIVERSIONS OF FLIGHT ROUTES, AND EMERGENCY EVACUATION OF FLIGHT CREW AND PASSENGERS\...
Organization: FAA
Status: Active
AD 00-NE-04
Title: PREVENT RADIAL DRIVE STEADY BEARING FAILURE\ROLLS-ROYCE LTD\RB-211-535C\RB-211-535E4\RB-211-535E4B\BOEING\757-200 SERIES\757-200CB SERIES\757-200PF SERIES\757-300 SERIES\TUPOLEV\204 SERIES
Organization: FAA
Status: Active
AD 00-CE-02
Title: PREVENT CHAFING BETWEEN THE WING FUEL QUANTITY WIRING HARNESS AND THE INTERNAL WING HARNESS SUPPORTS AT EACH WING RIB LOCATION\RAYTHEON\1900C (C-12J)\1900D\1900C
Organization: FAA
Status: Active
AD 00-NM-55
Title: PREVENT IGNITION SOURCES AND CONSEQUENT FIRE/EXPLOSION IN THE FUEL TANK\AIRBUS INDUSTRIE\A319-131\A319-132\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232\A320-233\A321-100\A321-111\...
Organization: FAA
Status: Active
AD 00-NM-02
Title: PREVENT CRACKING OF THE NLG MAIN FITTING, WHICH COULD LEAD TO COLLAPSE OF THE NLG DURING TAKEOFF AND LANDING, AND POSSIBLE INJURY TO THE FLIGHTCREW AND PASSENGERS\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 00-NM-06
Title: PREVENT FAILURE OF THE SHOULDER HARNESS\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\F.28 MARK 0070\F.28 MARK 0100\...
Organization: FAA
Status: Active
AD 00-NM-01
Title: PREVENT OPENING OF THE CARGO DOOR WHILE THE AIRPLANE IS IN FLIGHT\MCDONNELL DOUGLAS CORP\DC-8-61F\DC-8-62F\DC-8-63F\DC-8-71F\DC-8-72F\DC-8-73F\DC-8F-54\DC-8F-55
Organization: FAA
Status: Active
AD 84-CE-18
Title: FAILURE OF THE UPPER MOUNTING BRACKETS ON BOTH WING MOUNTED ENGINES\PILATUS BRITTEN-NORMAN LTD (SEE BRITTEN-NORMAN)\BN-2T MK III
Organization: FAA
Status: Active
AD 86-CE-23-A
Title: FAILURE OF THE MAIN LANDING GEAR CAUSED BY CRACKS IN THE TORQUE LINK ASSEMBLY AREA\PILATUS BRITTEN-NORMAN LTD (SEE BRITTEN-NORMAN)\BN-2A MARK III\BN-2A MARK III-2\BN-2A MARK III-3
Organization: FAA
Status: Active
AD 86-CE-23
Title: FAILURE OF THE MAIN LANDING GEAR\BRITTEN-NORMAN LTD (SEE ALSO PILATUS BRITTEN-NORMAN)\BN-2A MARK III\BN-2A MARK III-2\BN-2A MARK III-3
Organization: FAA
Status: Active
AD 89-ANE-44
Title: DETECT PROPELLER HUB CRACKS\HARTZELL PROPELLER INC\( )HC-( )2Y( )-( )\PIPER\PA-32-260\PA-32-300\PA-32-301T\PA-32-301\PA-32\TEXTRON LYCOMING (SEE AVCO)\540 SERIES\PILATUS BRITTEN-NORMAN LTD (SEE BRI...
Organization: FAA
Status: Active
ad 89-ANE-05
Title: A NO. 3 BEARING FAILURE AND SUBSEQUENT INFLIGHT ENGINE SHUTDOWN\CFM INTERNATIONAL\CFM56-2\CFM56-3\CFM56-3B\CFM56-3C\CFM56-5
Organization: FAA
Status: Active
AD 90-CE-65
Title: FAILURE OF THE ELEVATOR BUNGEE SPRING\PIPER\PA-31\PA-31-300\PA-31-325\PA-31-350\PA-31P
Organization: FAA
Status: Active
AD 90-CE-28
Title: FAILURE OF THE ENGINE MOUNT BEAM CAUSED BY FATIGUE CRACKS\CESSNA\402C\414A
Organization: FAA
Status: Active
AD 90-CE-61
Title: HORIZONTAL STABILIZER AND THE AFT FUSELAGE ATTACHMENT\PIPER\PA-31T\PA-31T1\PA-31T2\PA-31T3
Organization: FAA
Status: Active
AD 90-CE-60
Title: FUSELAGE STATION BULKHEAD\PIPER\PA-31\PA-31-300\PA-31-325\PA-31-350
Organization: FAA
Status: Active
AD 90-CE-59
Title: MAIN LANDING GEAR (MLG) DOOR\PIPER\PA-31\PA-31-325\PA-31-350\PA-31P\PA-31T1\PA-31T
Organization: FAA
Status: Active
AD 91-CE-87
Title: CRACKED ELEVATOR, FLAP, AILERON, ELEVATOR TRIM, ELEVATOR/FLAP INTERCONNECT, AND RUDDER CONTROL RODS\DEHAVILLAND\DHC-6-1\DHC-6-100\DHC-6-200\DHC-6-300
Organization: FAA
Status: Active
AD 91-CE-45
Title: FUSELAGE SIDE FRAME FLANGES\DEHAVILLAND\DHC-6-1\DHC-6-100\DHC-6-200\DHC-6-300
Organization: FAA
Status: Active
AD 92-ANE-23
Title: PREVENT AN UNCONTAINED FAILURE OF THE SIXTH STAGE LOW PRESSURE TURBINE (LPT) INNER AIRSEAL\PRATT & WHITNEY\JT9D-59A\JT9D-70A\JT9D-7Q\JT9D-7Q3
Organization: FAA
Status: Active
AD 92-CE-46
Title: LOSS OF THE AIRPLANE'S INTERNAL POWER CONNECTION TO THE AUTO-IGNITION SYSTEM\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 3101\JETSTREAM MODEL 3201
Organization: FAA
Status: Active
AD 92-CE-25
Title: NOSE LANDING GEAR FAILURE\AVIONS PIERRE ROBIN\R2160
Organization: FAA
Status: Active
AD 92-CE-41
Title: QUICK CONNECTORS BECOMING INADVERTENTLY DISCONNECTED\LOUIS L'HOTELLIER S A\BALL AND SWIVAL JOINT QUICK CONNECTORS
Organization: FAA
Status: Active
AD 92-NM-71
Title: PREVENT REDUCED STRUCTURAL CAPABILITY OF THE WING AND FUEL LEAKAGE\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 93-CE-45
Title: FAILURE OF THE WING STRUTS\DEHAVILLAND\DHC-6-1\DHC-6-100\DHC-6-200\DHC-6-300
Organization: FAA
Status: Active
AD 93-NM-194
Title: FAILURE OF THE UPPER DRAG STRUT TRUNNION FITTINGS OF THE NOSE LANDING GEAR\DEHAVILLAND\DHC-8 SERIES
Organization: FAA
Status: Active
AD 93-NM-193
Title: FAILURE OF THE MLG WHEEL AXLE\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 93-ANE-79
Title: CCOC FLANGE CRACKS\PRATT & WHITNEY\JT8D-1\JT8D-1A\JT8D-1B\JT8D-7\JT8D-7A\JT8D-9\JT8D-9A\JT8D-11\JT8D-15\JT8D-15A\JT8D-17\JT8D-17A\JT8D-17AR\JT8D-17R
Organization: FAA
Status: Active
AD 93-CE-54
Title: ENGINE OIL FILTER ADAPTERS ASSEMBLIES\CESSNA AIRCRAFT COMPANY\ENGINE OIL FILTER ADAPTERS ASSEMBLIES
Organization: FAA
Status: Active
AD 93-ANE-07
Title: INSPECT RIVETED OR SNAP RING IMPULSE COUPLING ASSEMBLIES\TELEDYNE CONTINENTAL MOTORS\S-20\S-1200\D-2000\D-3000
Organization: FAA
Status: Active
AD 93-ANE-08
Title: PREVENT CRANKSHAFT FAILURE AND SUBSEQUENT ENGINE FAILURE\TELEDYNE CONTINENTAL MOTORS\I0-360\TSI0-360\LTSI0-360\I0-520\TSI0-520
Organization: FAA
Status: Active
AD 93-CE-02
Title: PREVENT CANOPY FRAME FAILURE AND EMERGENCY CANOPY DEPLOYMENT FAILURE\GLASFLUGEL\MOSQUITO
Organization: FAA
Status: Active
AD 93-NM-125
Title: PREVENT RUPTURE OF THE UNIVERSAL JOINTS\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325
Organization: FAA
Status: Active
AD 94-SW-23-R1
Title: FATIGUE FAILURE OF THE PILLOW BLOCK BEARING BOLTS (BEARING BOLTS)\BELL HELICPTR TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\214B\214B-1
Organization: FAA
Status: Active
AD 94-NM-117
Title: CLEARLY VISIBLE 'EXIT' SIGNS FOR THE OVERWING EMERGENCY EXIT DURING AN EVACUATION\FOKKER-VFW B V\F.28 MARK 0100
Organization: FAA
Status: Active
AD 94-NM-94
Title: JAMMING OF THE PASSENGER/CREW DOOR\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 94-SW-26
Title: FATIGUE FAILURE OF THE CARRIER\BELL HELICOPTER TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\214B\214B-1\214ST
Organization: FAA
Status: Active
AD 94-ANE-44-R
Title: CRANKSHAFT FAILURE\TEXTRON LYCOMING (SEE AVCO)\320 SERIES\360 SERIES
Organization: FAA
Status: Active
AD 94-SW-28
Title: FATIGUE FAILURE OF THE BEARING BOLTS\BELL HELICOPTER TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\214ST
Organization: FAA
Status: Active
AD 94-SW-29
Title: FATIGUE FAILURE OF THE TRUNNION\BELL HELICOPTER TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\214B\214B-1\214ST
Organization: FAA
Status: Active
AD 94-SW-20
Title: FATIGUE FAILURE OF THE MAST AND SPLINE PLATE\BELL HELICOPTER TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\412\412EP
Organization: FAA
Status: Active
AD 94-SW-25
Title: FATIGUE FAILURE OF THE MAST\BELL HELICOPTER TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\214ST
Organization: FAA
Status: Active
AD 94-SW-24
Title: FATIGUE FAILURE OF THE SPIDER\BELL HELICOPTER TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\214B\214B-1
Organization: FAA
Status: Active
AD 94-CE-34
Title: MLG FAILURE BECAUSE OF A CRACKED 'A' FRAME ASSEMBLY\BEECH AIRCRAFT\76
Organization: FAA
Status: Active
AD 94-NM-222
Title: WATER IN 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 94-SW-17
Title: FAILURE OF THE MAIN ROTOR THRUST BEARING\SCHWEIZER AIRCRFT CORP (SEE MCDONNELL DOUG HELI )\269A\269A-1\269B\269 SERIES (TH-55A)\MCDONNELL DOUGLAS HELICPTR (SEE SCHWEIZER AIRCRFT CORP )\269A\269A-1\...
Organization: FAA
Status: Active
AD 94-CE-22
Title: ACRYLIC CABIN OR COCKPIT SIDE WINDOWS\FAIRCHILD AIRCRAFT CORPORATION\SA26-T\SA26-AT\SA226-T\SA226-T(B)\SA226-AT\SA226-TC\SA227-AT\SA227-AC\SA227-BC\SA227-TT
Organization: FAA
Status: Active
AD 94-ANE-44
Title: PREVENT CRANKSHAFT FAILURE\TEXTRON LYCOMING (SEE AVCO)\O-235 SERIES\O-290 SERIES\O-320 SERIES\O-360 SERIES
Organization: FAA
Status: Active
AD 94-NM-89
Title: STRUCTURAL CAPABILITY OF THE AIRPLANE FUSELAGE\DEHAVILLAND\DHC-8-100 SERIES\DHC-8-300
Organization: FAA
Status: Active
AD 94-NM-195
Title: STRUCTURAL INTEGRITY OF THE AIRPLANE\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...
Organization: FAA
Status: Active
AD 94-NM-245
Title: PREVENT STIFF OPERATION OF THE ELEVATOR CONTROL\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325\A300-600
Organization: FAA
Status: Active
AD 94-NM-246
Title: STRUCTURAL CAPABILITY OF THE AIRPLANE\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-B4-622R\A300-B4...
Organization: FAA
Status: Active
AD 94-NM-102
Title: STRUCTURAL INTEGRITY OF THE AIRPLANE\AIRBUS INDUSTRIE\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-B4-622R\A300-B4-622
Organization: FAA
Status: Active
AD 94-ANE-44-A
Title: PREVENT CRANKSHAFT FAILURE\TEXTRON LYCOMING (SEE AVCO)\235 SERIES\290 SERIES\320 SERIES\360 SERIES
Organization: FAA
Status: Active
AD 94-ANE-51
Title: LOW PRESSURE TURBINE (LPT) VANE FAILURES\PRATT & WHITNEY\JT9D-7R4\JT9D-7R4D\JT9D-7R4D1\JT9D-7R4E\JT9D-7R4E1\JT9D-7R4E4\JT9D-7R4G2\JT9D-7R4H1
Organization: FAA
Status: Active
AD 94-ANE-49
Title: COMPRESSOR ROTOR PART CRACKING\PRATT & WHITNEY\JFTD12A\T73 SERIES
Organization: FAA
Status: Active
AD 94-SW-16
Title: PREVENT FAILURE OF THE MAIN TRANSMISSION INPUT DRIVESHAFT ASSEMBLY (DRIVESHAFT)\BELL HELICOPTER TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\206A\206B (OH-58B)
Organization: FAA
Status: Active
AD 94-NM-238
Title: REAR PASSENGER DOOR APERTURE\BRITISH AEROSPACE\ATP SERIES
Organization: FAA
Status: Active
AD 94-NM-226
Title: INBOARD ELEVATOR POWER CONTROL PACKAGES (PCP)\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 94-NM-244
Title: STRUCTURAL INTEGRITY OF THE AIRPLANE\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
Organization: FAA
Status: Active
AD 94-NM-237
Title: UNCOMMANDED EXTENSION OF THE LIFT SPOILER\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPC )\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 94-NM-212
Title: POWER CONTROL LEVERS\BRITISH AEROSPACE\ATP SERIES
Organization: FAA
Status: Active
AD 94-NM-196
Title: CARGO FIRE EXTINGUISHING SYSTEM\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325\A300-600
Organization: FAA
Status: Active
AD 94-NM-179
Title: PREVENT EXCESSIVE FREE PLAY OF THE ELEVATOR CONTROL TAB AND POSSIBLE TAB FLUTTER\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES
Organization: FAA
Status: Active
AD 94-NM-164
Title: COCKPIT FRAME AND ADJACENT FUSELAGE STRUCTURE\BRITISH AEROSPACE\1-11 200 SERIES\1-11 400 SERIES
Organization: FAA
Status: Active
AD 95-CE-91-A
Title: PREVENT VHF NAVIGATION RECEIVER INTERFERENCE FROM FREQUENCY MODULATION (FM) RADIO STATION BROADCAST FREQUENCIES\ALLIEDSIGNAL INC\VN 411B
Organization: FAA
Status: Active
ad 95-nm-150-A
Title: DETECT AND CORRECT FATIGUE CRACKING ON THE FORWARD FITTINGS IN THE RADIUS OF FRAME 40 ADJACENT TO THE TENSION BOLTS IN THE CENTER SECTION OF THE WINGS\AIRBUS INDUSTRIE\A300-600
Organization: FAA
Status: Active
AD 95-CE-65
Title: DETECT AND CORRECT CRACKS IN A FLAP CARRIAGE\SOCATA--GROUPE AEROSPATIALE (SEE MORANE-SAULNIER)\TBM 700
Organization: FAA
Status: Active
AD 95-ANE-57-A
Title: PREVENT RELEASE OF UNCONTAINED DEBRIS FROM THE TURBINE EXHAUST CASE (TEC) FOLLOWING AN INTERNAL ENGINE FAILURE\PRATT & WHITNEY\JT9D-3\JT9D-7\JT9D-20\JT9D-59A\JT9D-70A\JT9D-7Q\JT9D-7R4
Organization: FAA
Status: Active
ad 95-ce-49
Title: DETECT AND CORRECT LOOSE FORWARD ELEVATOR MOUNTING BRACKETS,\ROLLADEN SCHNEIDER OHG\LS3-A\LS 4\LS 4A
Organization: FAA
Status: Active
AD 95-NM-275-A
Title: PREVENT REDUCED STRUCTURAL INTEGRITY OF THE FUSELAGE\AIRBUS INDUSTRIE\A310-200\A310-221\A310-222\A310-300\A310-322\A310-324\A310-325
Organization: FAA
Status: Active
ad 95-CE-64
Title: TO PREVENT CRACKS IN THE MAIN LANDING GEAR (MLG) ATTACHMENT BEARING\SOCATA--GROUPE AEROSPATIALE (SEE MORANE-SAULNIER)\TB20\TB21
Organization: FAA
Status: Active
AD 95-CE-72
Title: PREVENT STRUCTURAL FAILURE OF THE WING FRONT ATTACHMENTS CAUSED BY FATIGUE CRACKING\SOCATA--GROUPE AEROSPATIALE (SEE MORANE-SAULNIER)\TB9\TB10
Organization: FAA
Status: Active
AD 95-CE-51-R1
Title: PREVENT THE LANDING LIGHT SEAL FROM LODGING IN THE CARBURETOR\PIPER\PA-28-140\PA-28-150\PA-28-160\PA-28-180
Organization: FAA
Status: Active
AD 95-CE-53-R1
Title: R1 STRUCTURAL FAILURE OF THE MLG CAUSED BY FATIGUE CRACKING\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPC )\HP 137 MK.1\JETSTREAM MODEL 3101\JETSTREAM SERIES 200
Organization: FAA
Status: Active
AD 95-CE-35-R1
Title: ELIMINATING WATER IN THE FUEL TANKS\PIPER\PA-23\PA-23-160\PA-23-235\PA-23-250
Organization: FAA
Status: Active
ad 95-CE-70
Title: TO PREVENT MAIN LANDING GEAR (MLG) FAILURE CAUSED BY CRACKS IN THE SUPPORT RIBS, WHICH COULD RESULT IN LOSS OF CONTROL OF THE AIRPLANE DURING LANDING OPERATIONS\SOCATA--GROUPE AEROSPATIALE (SEE MOR...
Organization: FAA
Status: Active
ad 95-ANE-69-R1
Title: PREVENT 14TH AND 15TH STAGE HPC DISK RUPTURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRCRAFT\PRATT & WHITNEY\JT9D-59A\JT9D-70A\JT9D-7Q\JT9D-7Q3\JT9D-7R4
Organization: FAA
Status: Active
AD 95-CE-71
Title: STRUCTURAL FAILURE OF THE REAR WING ATTACHMENT FITTINGS CAUSED BY CRACKS IN THIS AREA\SOCATA--GROUPE AEROSPATIALE (SEE MORANE-SAULNIER)\TB10\TB200
Organization: FAA
Status: Active
ad 95-ane-38-4
Title: PREVENT DIFFUSER CASE ASSEMBLY RUPTURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE, ENGINE FIRE, AND DAMAGE TO THE AIRCRAFT\PRATT & WHITNEY\JT9D-7R4
Organization: FAA
Status: Active
AD 95-NM-111-R1
Title: ENGINE DAMAGE, AIRFRAME DAMAGE, AND/OR HAZARD TO PERSONS OR PROPERTY ON THE GROUND AS A RESULT OF 'BLUE ICE'\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-140
Title: CORRECT CORROSION ON THE REAR SPARS OF THE WINGS\AEROSPATIALE\ATR42-200 SERIES\ATR42-300 SERIES\ATR42-320 SERIES
Organization: FAA
Status: Active
ad 95-NM-182
Title: PREVENT DISCONNECT OF THE ANTI-SKID CONTROL UNIT (ASCU) OF THE AIRCRAFT BRAKING SYSTEM AND REVERSION TO MANUAL BRAKING DURING OPERATION ON RUNWAYS CONTAMINATED BY STANDING WATER, SLUSH, OR WET SNOW...
Organization: FAA
Status: Active
AD 95-NM-200
Title: CRACK FORMATION IN THE SEALING ANGLES\AIRBUS INDUSTRIE\A300-600
Organization: FAA
Status: Active
AD 95-CE-53
Title: STRUCTURAL FAILURE OF THE MLG\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\HP 137 MK.1\JETSTREAM SERIES 200\JETSTREAM MODEL 3101
Organization: FAA
Status: Active
AD 95-NM-216-R1
Title: REDUCED STRUCTURAL INTEGRITY OF THE FUSELAGE AND RESTRICTED OPERATION OF THE MAIN LANDING GEAR (MLG) FREE-FALL SYSTEM\AIRBUS INDUSTRIE\A320-111\A320-200\A320-211\A320-212\A320-214\A320-231\A320-232...
Organization: FAA
Status: Active
AD 95-NM-29
Title: ICING OF THE NO. 1 PITOT TUBE\FOKKER-VFW B V\F.28 MARK 0070\F.28 MARK 0100
Organization: FAA
Status: Active
AD 95-NM-143
Title: REDUCED CONTROLLABILITY OF THE AIRPLANE\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 95-NM-215
Title: FATIGUE CRACKING\BOEING\737-100 SERIES\737-200 SERIES (T-43)
Organization: FAA
Status: Active
AD 95-NM-207
Title: ADVERSELY AFFECTED OPERATION OF THE FUSE\BOEING\737-300 SERIES\737-400 SERIES\737-500 SERIES
Organization: FAA
Status: Active
AD 95-CE-96
Title: AN ASYMMETRICAL AIRBRAKE DEPLOYMENT CAUSING AN UNCONTROLLABLE ROLL AND POSSIBLE LOSS OF CONTROL OF THE SAILPLANE\BURKHART GROB LUFT-UND RAUMFAHRT (FORMERLY GROB-WERKE GMBH & CO )\G103 TWIN ASTIR
Organization: FAA
Status: Active
AD 95-CE-31
Title: FAILURE OF THE PILOT'S AND CO-PILOT'S CONTROL WHEELS\AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD (FORMERLY GOVERNMENT AIRCRAFT FACTORIES)\N22S\N22B\N24A
Organization: FAA
Status: Active
AD 95-CE-44-R1
Title: FAILURE OF THE MLG CAUSED BY 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 MODE...
Organization: FAA
Status: Active
AD 95-CE-98
Title: STRUCTURAL FAILURE OF THE FRONT SPAR CAUSED BY CRACKS IN THE STUB WING UPPER FRONT SPAR CAP FLANGES\AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD (FORMERLY GOVERNMENT AIRCRAFT FACTORIES)\N22B\N22S\N24A
Organization: FAA
Status: Active
AD 95-CE-95
Title: FAILURE OF THE ELEVATOR CONTROL LEVER\GROB-WERKE GMBH & CO (SEE SCHEMPP-HIRTH BURKHART GROB LUFT-UND RAUMFAHRT)\G102 ASTIR CS
Organization: FAA
Status: Active
AD 95-CE-100
Title: CRACKING IN THE UPPER FIN AND HORIZONTAL STABILIZER ATTACHMENT FITTINGS\AEROSPACE TECHNOLOGIES OF AUSTRALIA PTY LTD (FORMERLY GOVERNMENT AIRCRAFT FACTORIES)\N22B\N22S\N24A
Organization: FAA
Status: Active
AD 95-CE-89-R1
Title: STRUCTURAL CRACKING TO THE CABIN CAUSED BY MISSING RIVETS\BEECH AIRCRAFT\58P\58PA
Organization: FAA
Status: Active
AD 95-NM-234-R1
Title: WRONG ENGINE-DRIVEN GENERATOR BEING SHUT DOWN UNNECESSARILY IN THE EVENT OF AN ENGINE FIRE WARNING\MCDONNELL DOUGLAS CORPORATION\MD-11 SERIES
Organization: FAA
Status: Active
AD 95-SW-36
Title: FATIGUE FAILURE OF THE MAST OR TRUNNION\BELL HELICOPTER TEXTRON ***(SEE CA DEPT OF FORESTRY CONTINENTAL COPTERS GARLICK HAWKEYE ROTORWI\206L\206L-1\206L-3\206L-4
Organization: FAA
Status: Active
AD 95-ANE-56
Title: ENGINE COMBUSTOR LINER DETERIORATION\ROLLS-ROYCE LIMITED\RB.211-524G\RB.211-524H
Organization: FAA
Status: Active
AD 95-NM-160-R1
Title: CORROSION OF THE ANTENNA MOUNTING REINFORCING PLATES AND SURROUNDING SKIN\BRITISH AEROSPACE\ATP SERIES
Organization: FAA
Status: Active
AD 95-NM-94
Title: SEPARATION OF THE LOWER COWLING FROM THE AIRPLANE\FOKKER-VFW B V\F.28 MARK 0100\F.28 MARK 0070
Organization: FAA
Status: Active
AD 95-CE-34
Title: FAILURE OF BOTH GENERATORS DURING CRITICAL PHASES OF FLIGHT\FAIRCHILD AIRCRAFT CORPORATION\SA226-T\SA226-T(B)\SA226-AT\SA226-TC\SA227-TT\SA227-AT\SA227-AC
Organization: FAA
Status: Active
AD 95-NM-271A
Title: FATIGUE-RELATED CRACKING IN THE REAR PRESSURE BULKHEAD\JETSTREAM AIRCRAFT LTD (FORMERLY BRITISH AEROSPACE)\JETSTREAM MODEL 4101
Organization: FAA
Status: Active
AD 95-NM-142-R1
Title: HEAT DAMAGE TO THE FUEL FEED HOSE ASSEMBLIES OF THE AUXILIARY POWER UNIT (APU)\RAYTHEON CORPORATE JETS (FORMERLY BRITISH AEROSPACE CORPORATION)\BAE 125-800A/HAWKER 800
Organization: FAA
Status: Active
AD 95-CE-10-R1
Title: FAILURE OF THE NOSE LANDING GEAR (NLG)\JETSTREAM AIRCRFT LTD (FORMERLY BRITISH AEROSPACE)\HP 137 MK.1\JETSTREAM SERIES 200\JETSTREAM MODEL 3101\JETSTREAM MODEL 3201
Organization: FAA
Status: Active
AD 95-NM-265
Title: DEGRADATION OF THE STRUCTURAL CAPABILITY OF THE FUSELAGE AND SUDDEN LOSS OF CABIN PRESSURE\DEHAVILLAND\DHC-7 SERIES
Organization: FAA
Status: Active
AD 95-SW-34
Title: FAILURE OF THE MAIN GEARBOX SECOND STAGE LOWER PLANETARY PLATE (PLATE) DUE TO FATIGUE CRACKING\SIKORSKY AIRCRFT DIV OF UNITED AIRCRFT CORP\S-64F (CH-54B)
Organization: FAA
Status: Active
AD 95-NM-223
Title: FAILURE OF THE MAIN LANDING GEAR (MLG) TO EXTEND FOR LANDING AND SUBSEQUENT DAMAGE TO THE AIRPLANE\BOEING\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES
Organization: FAA
Status: Active
AD 95-NM-176
Title: ELECTRICAL SHORT CIRCUITING\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-201
Title: HIGH BEARING STRESS ON THE BUSHINGS IN THE FLAP FITTINGS\SAAB-SCANIA AB\SF-340A
Organization: FAA
Status: Active
AD 95-NM-257
Title: ENSURE THAT THE EMERGENCY LIGHTS ILLUMINATE WHEN NEEDED\DEHAVILLAND\DHC-7 SERIES
Organization: FAA
Status: Active
AD 95-CE-03
Title: VIBRATION OF THE RUDDER\BURKHART GROB LUFT-UND RAUMFAHRT (FORMERLY GROB-WERKE GMBH & CO )\G109
Organization: FAA
Status: Active
AD 95-NM-163
Title: UNDETECTED CRACKING OF THE FRAMES AND SKIN PANELS OF THE FUSELAGE\DEHAVILLAND\DHC-8-102\DHC-8-103
Organization: FAA
Status: Active
AD 95-NM-232
Title: MAIN HYDRAULIC POWER SUPPLY\DORNIER-WERKE G M B H\DO 328-100
Organization: FAA
Status: Active
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


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