Popular Standards |
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AD 95-12-08 | MLG REAR HINGE PIN BUSH\AEROSPATIALE (SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE)\ATR72-101\ATR72-102\ATR72-201\ATR72 |
AD 95-12-09 | INSPECT HINGE FITTINGS OF NLG AFT DOOR\AIRBUS INDUSTRIE\A300 MODEL B4-103\A300 MODEL B4-203\A300 MODEL B4-2C\A300 MODE |
AD 95-12-10 | INSPECT ELECTRICAL CABLES IN DOOR\AIRBUS INDUSTRIE\A330-202\A330-223\A330-301\A330-321\A330-322\A330-323\A340-211\A340 |
AD 95-12-11 | INSPECT FUEL FLOW OF MAIN FUEL SUPPLY HOSE\AIRBUS INDUSTRIE\A340-211\A340-311 |
AD 95-12-12 | STICK SHAKERS\BOMBARDIER INC\DHC-8-100 SERIES |
AD 95-12-13 | ICING CONDITIONS\BRITISH AEROSPC (ENGLAND)\ATP |
AD 95-12-14 | REVERSE THRUST CONTROL\FOKKER SVCS\F.28 MARK 0100 |
AD 95-12-15 | PRESSURE SWITCH IN FUEL SYSTEM\JETSTREAM AIRCRFT LTD\JETSTREAM MODEL 4101 |
AD 95-12-16 | AIRPLANE ENGINE FIRE\MOONEY AIRCRFT CORP\M20R |
AD 95-12-17 | STRUCTURAL INTEGRITY OF THE OUTBOARD CHORDS\BOEING CO\737-100 SERIES\737-200 SERIES\737-200C SERIES |
AD 95-12-18 | FUEL SUPPLY LINE\FOKKER SVCS\F.28 MARK 0100 |
AD 95-12-20 | WING SLAT TRACK STOP PINS\AIRBUS INDUSTRIE\A330-301\A340-211\A340-212\A340-311\A340-312 |
AD 95-12-21 | INSTALL DOUBLER ON STRINGER 39\AIRBUS INDUSTRIE\A340-211\A340-311 |
AD 95-12-22 | THRUST REVERSER COWLS\AIRBUS INDUSTRIE\A340-211\A340-212\A340-311\A340-312 |
AD 95-12-23 | WING DAMAGE\TWIN COMMANDER AIRCRFT CORP\690C\695 |
AD 95-12-26 | FUEL LEAKAGE ONTO AN ENGINE\BOEING CO\747SP SERIES |
AD 95-12-27 | POSSIBILITY OF AN ALL- FLAPS-UP LANDING\BOEING CO\747-400 SERIES\747-400D SERIES\747-400F SERIES |
AD 95-13-01 | SEPARATION OF THE PASSENGER SEATS FROM THE SEAT TRACK\AIRBUS INDUSTRIE\A320 MODEL -111\A320 MODEL -211\A320 MODEL -212 |
AD 95-13-02 | VERTICAL STABILIZER\TWIN COMMANDER AIRCRFT CORP\685\690A\690B\690C\690D\690\695A\695 |
AD 95-13-03 | ELECTRICAL LANDING GEAR MOTOR\RAYTHEON AIRCRFT CO\100\200\200C\200CT\200T\99\99A\A100\A100-1\A200\A200C\A200CT\A99\B10 |
AD 95-13-05 | FAILURE OF STRUT\BOEING CO\747-100 SERIES\747-100B SUD SERIES\747-100B SERIES\747-200B SERIES\747-200C SERIES\747-200F |
AD 95-13-06 | FAILURE OF STRUT\BOEING CO\747-100 SERIES\747-100B SUD SERIES\747-100B SERIES\747-200B SERIES\747-200C SERIES\747-200F |
AD 95-13-07 | FAILURE OF STRUT\BOEING CO\747-100 SERIES\747-100B SUD SERIES\747-100B SERIES\747-200B SERIES\747-200C SERIES\747-200F |
AD 95-13-08 | AIRCRAFT HANDLING PROBLEMS\PRATT & WHITNEY CANADA INC\PT6A-67D |
AD 95-13-09 | ELEVATOR AND RUDDER HINGE SEPARATION\BURKHART GROB LUFT-UND\CLUB ASTIR IIB\G102 ASTIR CS\G103 TWIN ASTIR\SPEED ASTIR I |
AD 95-13-10 | VERTICAL FIN ATTACHMENT\AGUSTA S P A\A109A II\A109A\A109C |
AD 95-13-11 | REDUCED STRUCTURAL INTEGRITY OF THE WING FRONT SPAR\MCDONNELL DOUGLAS CORP\DC-10-10F\DC-10-10\DC-10-15\DC-10-30F (KC-1 |
AD 95-14-01 | CONTROL OF THE SAILPLANE\GLASER-DIRKS FLUGZEUGBAU GMBH\DG-100 |
AD 95-14-02 | INSTRUMENT AIR SYSTEM\RAYTHEON AIRCRFT CO\1900C\1900D\1900 |
AD 95-14-03 | CENTER TORQUE SHAFT\BRITISH AEROSPC AIRBUS LTD\BAC 1-11 200 SERIES\BAC 1-11 400 SERIES |
AD 95-14-04 | CENTER TORQUE SHAFT\BRITISH AEROSPC AIRBUS LTD\BAC 1-11 200 SERIES\BAC 1-11 400 SERIES |
AD 95-14-05 | DEGRADATION OF THE STRUCTURAL CAPABILITIES OF THE AIRPLANE\MITSUBISHI HEAVY IND LTD\YS-11A-200\YS-11A-300\YS-11A-500\Y |
AD 95-14-06 | TO ENSURE AIRPLANE SURVIVABILITY IN THE EVENT OF DAMAGE TO FULLY POWERED FLIGHT CONTROL SYSTEMS\MCDONNELL DOUGLAS CORP |
AD 95-14-07 | INSPECT FOR CRACKS IN HINGE PINS\AEROSPATIALE (SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE)\ATR72-101\ATR72-102\ATR72- |
AD 95-14-08 | PREVENT COLLAPSE OF THE NOSE LANDING GEAR\VICKERS-ARMSTRONGS (AIRCRFT LTD )\VISCOUNT 744\VISCOUNT 745D\VISCOUNT 810 |
AD 95-14-09 | FAILURE OF FUEL CROSSFLOW TUBE\LEARJET INC\60 |
AD 95-15-01 | OVER-WING ESCAPE SLIDE\BOEING CO\767-200 SERIES\767-300 SERIES\767-300F SERIES |
AD 95-15-02 | PREVENT FATIGUE CRACKING\VICKERS-ARMSTRONGS (AIRCRFT LTD )\VISCOUNT 744\VISCOUNT 745D\VISCOUNT 810 |
AD 95-15-03 | PREVENT FAILURE OF SIDE BRACE PINS\AEROSPATIALE (SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE)\ATR42-200\ATR42-300\ATR4 |
AD 95-15-04 | STRUCTURAL INTEGRITY OF THE WING LEADING EDGE SKIN AND WING ANTI-ICE FLUID DISTRIBUTION PANEL (TKS PANEL) INTERFACE JO |
AD 53-15-03 | PITCH CHANGE LINK SCREW\HARTZELL PROPELLER INC\HC-82XF-1 |
AD 53-16-01 | ELEVATOR TRIM TAB\BELLANCA INC\14-19-2\14-19-3A\14-19-3\14-19 |
AD 53-17-01 | CONTROL STICK BOOT\MOONEY MITE AIRCRFT CORP\M-18C 55\M-18C\M-18LA\M-18L |
AD 53-18-01 | GOODRICH WHEEL BEARING\CESSNA AIRCRFT CO\T-50 (ARMY AT-17, UC-78, NAVY JRC-1) |
AD 53-19-01 | GENERATOR COOLING FAN\MCDONNELL DOUGLAS CORP\C54-DC\C54A-DC\C54B-DC\C54D-DC\C54E-DC\C54G-DC\DC-4 |
AD 53-20-01 | HAMILTON STD. PROPELLOR PITCH STOP\MARTIN-MARIETTA CORP\202A\202 |
AD 53-21-01 | WING REAR SPAR ATTACHMENT BOLTS\DE HAVILLAND INC (CANADA)\DHC-2 MK.III\DHC-2 MK.II\DHC-2 MK.I |
AD 53-21-02 | HORIZONTAL STABILIZER STRUT\GRUMMAN AMERCN AVI CORP\G-21A (ARMY OA-9, NAVY JRF-1, -2, -3, -4, -5, AND |
AD 53-23-01 | NOSE LANDING GEAR CLUTCH PLATE\TRACOR FLIGHT SYSTEMS INC\240 SERIES\240-0\240-10\240-11\240-12\240-13\240-14\240-15\24 |
AD 53-23-02 | FUEL TANK FILLER NECK\DE HAVILLAND INC (CANADA)\DHC-2 MK.III\DHC-2 MK.II\DHC-2 MK.I |
AD 53-23-03 | LIFT STRUT FITTINGS\SKY ENTERPRISES INC\RC-3 |
AD 53-24-01 | STABILIZER STRUT TERMINALS\GRUMMAN AMERCN AVI CORP\G-21A (ARMY OA-9, NAVY JRF-1, -2, -3, -4, -5, AND |
AD 53-24-02 | TAIL ROTOR PITCH CHANGE ROD\HILLER AVI\UH-12A\UH-12B\UH-12 |
AD 53-24-03 | LADING GEAR BELLCRANK\MOONEY MITE AIRCRFT CORP\M-18L |
AD 53-24-04 | FUEL-HYDRAULIC LINES\PIPER AIRCRFT INC NEW\PA-18\PA-22 |
AD 53-25-01 | AILERON CONTROL SYSTEM\MCDONNELL DOUGLAS CORP\DC-6 |
AD 53-26-01 | IGNITION SWITCH\BRIGGS & STRATTON CORP\B-5 IGNITION SWITCHES |
AD 54-01-01 | MODEL 67000 REVERSE SOLENOID VALVES\HAMILTON STANDARD DIV\23250\23251\23260\232\24250\24260\242\34D50\34D51\34D60\34D\ |
AD 54-01-02 | LOW PITCH STOP LEVERS AND WEDGES\HAMILTON STANDARD DIV\23250\23251\23260\232\24250\24260\242\34D50\34D51\34D60\34D\34E |
AD 54-01-03 | FUEL STRAINER SCREEN\SIKORSKY AIRCRFT CORP\S-55 |
AD 54-02-01 | MAGNETO TIMING\TEXTRON LYCOMING AVCO CORP\O-290-D2 |
AD 54-02-02 | RIGGING OF WHEEL SKIS\FEDERAL SKI & ENGINEERING CORP\AWB-2500\AWB-2500A\AWB-2100 |
AD 54-04-01 | SPARK PLUGS\AC SPARK PLUG OF GENERAL MOTORS CORP\AC LA-87 SPARK PLUGS |
AD 54-05-02 | BLADE TIP FAILURE\SENSENICH PROPELLER MFG CO INC\M76A SERIES |
AD 54-06-01 | KIDDIE CO2 DISCHARGE VALVE\MCDONNELL DOUGLAS CORP\DC-6A\DC-6B\DC-6 |
AD 54-06-02 | WING SCARF SPLICE BUSHING\MARTIN-MARIETTA CORP\202 |
AD 54-08-01 | NOSE GEAR PISTON AND WORK ASSEMBLY\MARTIN-MARIETTA CORP\202A\202\404 |
AD 54-09-01 | CARBURETOR HOTSPOT HEATER ASSEMBLY\FAIRCHILD ENGINE DIV FAIRCHILD ENGINE & AIRPLANE CORP\6-440-C2 (L-440-1)\6-440-C3\6 |
AD 54-10-01 | PROPELLERS USING WEDGE INSERT TYPE LOW PITCH ASSEMBLIES\HAMILTON STANDARD DIV\23260\24260\34D50\34D51\34D60 |
AD 54-12-01 | LANDING GEAR OLEO DRAG STRUTS\MARTIN-MARIETTA CORP\404 |
AD 54-12-02 | VIBRATION STRESS\MCCAULEY PROPELLER SYSTEMS\D-1093\MAC20A (41D5926)\MAC20A |
AD 54-13-01 | STAR ASSEMBLY BOLT REPLACEMENT\SIKORSKY AIRCRFT CORP\S-55 |
AD 54-15-01 | CONTROL CABLE TURNBUCKLE THREADS\DE HAVILLAND INC (CANADA)\DHC-2 MK.III\DHC-2 MK.II\DHC-2 MK.I |
AD 54-16-01 | MAIN TRANSMISSION\SIKORSKY AIRCRFT CORP\S-55 |
AD 54-18-01 | WING-TO-FUSELAGE ATTACHMENT\NAVION AIRCRFT CO LTD\NAVION (ARMY L-17A)\NAVION A (ARMY L-17B AND L-17C)\NAVION B\NAVION |
AD 54-19-01 | BRAKE LINE COVER PLATE\PIPER AIRCRFT INC NEW\PA-18\PA-18-105 (SPECIAL)\PA-18-125 (ARMY L-21A)\PA-18-135\PA-18-150\PA-1 |
AD 54-19-02 | SERVO SAFETY CLIP\SIKORSKY AIRCRFT CORP\S-55 |
AD 54-20-01 | SAFETY BELT ASSEMBLIES\AIRCRFT BELT & TRIM CORP\LBM-1900 SAFETY BELTS |
AD 54-20-02 | SUPPORT ASSEMBLY CRACKS\SIKORSKY AIRCRFT CORP\S-55 |
AD 54-21-01 | FUEL PUMPS\AC SPARK PLUG OF GENERAL MOTORS CORP\AC DIAPHRAGM TYPE FUEL PUMPS |
AD 67-09-03 | FLAP JACK SCREW AND CARRIAGE ASSEMBLY\BRITISH AEROSPC AIRBUS LTD\BAC 1-11 400 SERIES |
AD 67-09-04 | CONTROL SURFACE LOCK\AG CAT CORP\G-164A\G-164 |
AD 67-10-01 | UPPER WING SKIN\BOEING CO\707-100 LONG BODY\707-100B LONG BODY\707-100B SHORT BODY\707-200\720 SERIES\720B SERIES |
AD 67-10-02 | ENGINE STUB ACCESS PANELS\BRITISH AEROSPC AIRBUS LTD\BAC 1-11 200 SERIES\BAC 1-11 400 SERIES |
AD 67-10-03 | FAILURE OF PROPELLER HINGES\DOWTY AEROSPC PROPELLERS\(C) R130/4-20-4/\(C) R148/4-20-4/\(C) R175/4-30-4/\(C) R186/4-30- |
AD 67-11-01 | FUEL PRESSURE GAUGE INSTRUMENT LINE\REVO INC\COLONIAL C-1\COLONIAL C-2\LAKE LA-4A\LAKE LA-4P\LAKE LA-4 |
AD 67-11-02 | CRACKS IN LOWER FUSELAGE EXTERIOR\MARYLAND AIR IND INC\F-27\F-27A\F-27B\F-27F\F-27G\F-27J\F-27M |
AD 67-11-03 | MAIN ROTOR GEAR DRIVE\SCHWEIZER AIRCRFT CORP\269A-1\269A\269B |
AD 67-11-04 | FUSELAGE MAIN FRAMES FORGING\LOCKHEED AIRCRFT CORP\188A\188C |
AD 67-11-05 | TAIL TRUSS REPLACEMENT\MOONEY AIRCRFT CORP\M20A\M20 |
AD 67-12-02 | NOSE LANDING GEAR\MARYLAND AIR IND INC\FH-227B\FH-227C\FH-227D\FH-227E\F-27\F-27A\F-27B\F-27F\F-27G\F-27J\F-27M\FH-227 |
AD 67-12-04 | RUDDER HORN ASSEMBLY\MARYLAND AIR IND INC\F-27\F-27A\F-27B\F-27F\F-27G\F-27J\F-27M\FH-227\FH-227B\FH-227C\FH-227D\FH-2 |
AD 67-12-05 | PULLEY FAIRLEADS\PILATUS AIRCRFT LTD\PC-6-H1\PC-6-H2\PC-6/350-H1\PC-6/350-H2\PC-6/350\PC-6/A-H1\PC-6/A-H2\PC-6/A\PC-6/ |
AD 67-12-06 | FUEL QUANTITY GAUGE SENDER UNITS\PIPER AIRCRFT INC NEW\PA-28-151\PA-28-161\PA-28-181\PA-28-140\PA-28-150\PA-28-160\PA- |
AD 67-13-02 | FUSELAGE INSPECTION\MCDONNELL DOUGLAS CORP\DC-6A\DC-6B\DC-6\DC-7B\DC-7C\DC-7 |
AD 67-13-03 | RUDDER CONTROL LEVER RIVETS\PILATUS AIRCRFT LTD\PC-6-H1\PC-6-H2\PC-6/350-H1\PC-6/350-H2\PC-6/350\PC-6/A-H1\PC-6/A-H2\P |
AD 67-14-01 | ROTOR BLADE MODIFICATION\AIR & SPACE AMERICA INC\18A |
AD 67-14-02 | LANDING GEAR SIDE STRUT\BOEING CO\727 SERIES\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES\727C SERIES |
AD 67-14-04 | FIN TOP ACTUATOR FITTING\BRITISH AEROSPC AIRBUS LTD\BAC 1-11 200 SERIES\BAC 1-11 400 SERIES |
AD 67-14-05 | NOSE GEAR STEERING CYLINDER GLAND NUT\BRITISH AEROSPC AIRBUS LTD\BAC 1-11 200 SERIES |
AD 67-14-06 | WING INSPECTION\MARTIN-MARIETTA CORP\202A\202\404 |
AD 67-14-07 | ENGINE EXHAUST SYSTEM\PIPER AIRCRFT INC NEW\PA-25-235 |
AD 67-14-08 | MAGNESIUM PITCH CHANGE REDUCTION GEAR HOUSING\RATIER-FOREST DIV DE FIGEAC\FH 76-1-05\FH 76-1-06\FH 76-1-07\FH 76-1-09\ |
AD 67-15-01 | STABILIZER LINK PIN\BRITISH AEROSPC AIRBUS LTD\BAC 1-11 200 SERIES\BAC 1-11 400 SERIES |
AD 67-15-02 | ELECTRICAL SYSTEM MODIFICATION\MARYLAND AIR IND INC\F-27\F-27A\F-27B\F-27F\F-27G\F-27J\F-27M\FH-227\FH-227B\FH-227C\FH |
AD 67-15-03 | INSPECTION OF THE OIL FILTER\ROLLS-ROYCE PLC\DART 525F,525,526,527,528-7E,528D-7E,529-7E,529-7H,529-8E,529-8H,529-8X,\ |
AD 67-15-04 | TAIL ROTOR GEAR BOX DRIVE SHAFT\EUROCOPTER FRANCE\SE 3130-ALOUETTE II |
AD 67-17-01 | FIXED SPLINE\PACIFIC PROPELLER INC\A6441FN-606 |
AD 67-17-02 | FLIGHT COMPARTMENT MODIFICATION\BRITISH AEROSPC AIRBUS LTD\BAC 1-11 200 SERIES\BAC 1-11 400 SERIES |
AD 67-17-03 | CRACKS IN SKIN OF STABILIZER\MARYLAND AIR IND INC\F-27\F-27A\F-27B\F-27F\F-27G\F-27J\F-27M\FH-227\FH-227B\FH-227C\FH-2 |
AD 67-17-06 | PYLON LOWER RING\SIKORSKY AIRCRFT CORP\S-55\S-55B\S-55C |
AD 67-18-02 | GALLEY SUPPLY BOXES\BOEING CO\707-100 LONG BODY\707-100B LONG BODY\707-100B SHORT BODY\707-200\707-300 SERIES\707-300B |
AD 67-18-03 | ENGINE MOUNT TRUSS\LOCKHEED MARTIN AERONTCL SYSTEMS\382B\382 |
AD 67-18-04 | LIFE VESTS\PAN AVION CO\PA-5 LIFE VESTS |
AD 67-18-05 | SEATS\TECO INC\603 SEATS |
AD 67-19-02 | HONEYCOMB DELAMINATION\BRITISH AEROSPC AIRBUS LTD\BAC 1-11 200 SERIES\BAC 1-11 400 SERIES |
AD 67-19-03 | FRONT SPAR WEB\BOMBARDIER INC\CL-44D4 |
AD 67-19-04 | ENGINE MOUNT\MARTIN-MARIETTA CORP\202A\202\404 |
AD 67-19-05 | OXYGEN CYLINDER MOUNTING CHANNELS\PIPER AIRCRFT INC NEW\PA-30 |
AD 67-20-01 | PROPELLER PITCH LOCK\PACIFIC PROPELLER INC\A6441FN-606 |
AD 75-03-05 | INFLIGHT SEPERATION OF THE EXTENSION SLEEVE\HAMILTON STANDARD DIV\54H60 |
AD 75-03-06 | CRACKS AND OPTICAL DISTORTION\MITSUBISHI HEAVY IND LTD\MU-2B-36A\MU-2B-26\MU-2B-26A\MU-2B-36 |
AD 75-03-07 | PASSENGER EVACUATION SYSTEM\LOCKHEED AIRCRFT CORP\L-1011-385-1-14\L-1011-385-1-15\L-1011-385-1 |
AD 75-04-02 | MAIN ROTOR SPINDLES\ORLANDO HELICPTR AIRWAYS INC\CH-19E\H-19A\H-19D\H-19G\HRS-1/CH-19\HRS-3/H-19B\UH-19D\SIKORSKY AIRC |
AD 75-04-03 | OXYGEN\MCDONNELL DOUGLAS CORP\DC-10-10F\DC-10-10\DC-10-30F (KC-10A)\DC-10-30\DC-10-40F\DC-10-40 |
AD 75-04-04 | OIL LINE SYSTEM\REGAL AIR INC\305A |
AD 75-04-05 | ENGINE FUEL PRESSURE SWITCHES\SABRELINER CORP\NA-265-20\NA-265-30\NA-265-40\NA-265-60\NA-265-65\NA-265-70\NA-265-80\NA |
AD 75-04-06 | PILOT-STATIC TUBING\BOEING CO\SERIES: 747-100,747-100B SUD,747-100B,747-200B,747-200C,747-200F,747-300,747-400\747-400 |
AD 75-04-07 | LIFE LIMIT - P/N 701810\PRATT & WHITNEY DIV\TURBO WASP JT3D-3B\TURBO WASP JT3D-3\TURBO WASP JT3D-7 |
AD 75-04-08 | HYDRAULIC SYSTEM ELECTRICAL WIRING\BOEING CO\737-100 SERIES\737-200 SERIES\737-200C SERIES\737-300 SERIES\737-400 SERI |
AD 75-04-09 | LANDING GEAR ACTUATOR\MOONEY AIRCRFT CORP\M20C\M20E\M20F |
AD 75-04-10 | HEATER OVERHEAT CONDITIONS\LOCKHEED AIRCRFT CORP\L-1011-385-1-14\L-1011-385-1-15\L-1011-385-1 |
AD 75-04-12 | MARKINGS ON TACHOMETER\AMERCN CHAMPION AIRCRFT CORP\8GCBC |
AD 75-05-04 | STROBE LIGHT FLASH TUBES\WHELEN ENGINEERING CO INC\A427 STROBE LIGHT FLASH TUBES |
AD 75-05-05 | MAIN WHEEL ASSEMBLY\GOODYEAR AEROSPC CORP\WHEEL ASSEMBLY |
AD 75-05-06 | FUEL MANIFOLD LEAKAGE\PRATT & WHITNEY DIV\JT8D-209\JT8D-217A\JT8D-217C\JT8D-217\JT8D-219\TURBO WASP JT8D-11,JT8D-15A,J |
AD 75-05-07 | MAGNETIC STABILIZER COMPASS\KING RADIO CORP\MODEL KCS-55 |
AD 75-05-09 | FUEL VALVE WIRE BUNDLES\BOEING CO\737-100 SERIES\737-200 SERIES\737-200C SERIES\737-300 SERIES\737-400 SERIES\737-500 |
AD 75-05-10 | SLIDE LATCH CABLE\BOEING CO\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES |
AD 75-05-11 | FLIGHT CREW WARNING\BOEING CO\747-100 SERIES\747-100B SUD SERIES\747-100B SERIES\747-200B SERIES\747-200C SERIES\747-2 |
AD 75-05-13 | TURBOFAN ENGINES\GENERAL ELECTRIC AIRCRFT ENGINES\CF700-2C\CF700-2D-2\CF700-2D |
AD 75-05-14 | ALTIMETER FAILURE\KOLLSMAN\B4545110001\B4545110011 |
AD 75-05-17 | AUXILIARY POWER UNITS\AIRESEARCH\GTCP660-4\GTCP660-4R |
AD 75-06-01 | REDUCTION GEARBOX DETERIORATION\PRATT & WHITNEY CANADA INC\PT6A-20A\PT6A-20B\PT6A-20\PT6A-27\PT6A-28\PT6A-34\PT6A-6/C2 |
AD 75-06-02 | CARGO CARRIERS\MD HELICPTR INC\369HE\369HM\369HS |
AD 75-06-03 | PITCH LINK ASSEMBLY\BELL HELICPTR TEXTRON\206A-1 (OH-58A)\206A\206B-1\206B |
AD 75-06-04 | FORWARD RUDDER CONTROL CABLE\PIPER AIRCRFT INC NEW\PA-31-350 |
AD 75-06-05 | FUSELAGE MAIN FRAMES\LOCKHEED-GEORGIA CORP\1329-23A\1329-23E\1329-25\1329-23D |
AD 75-06-07 | FORWARD PASSENGER DOORS\MCDONNELL DOUGLAS CORP\DC-10-10\DC-10-30F (KC-10A)\DC-10-30\DC-10-40 |
AD 75-06-08 | DC AND AC POWER\GULFSTREAM AEROSPC CORP\G-1159 |
AD 75-06-09 | ELEVATOR INBOARD HINGE SUPPORT\RAYTHEON AIRCRFT CO\60\A60 |
AD 75-06-10 | CABIN ROOF STRAPS\BELL HELICPTR TEXTRON\206A\206B |
AD 75-07-01 | HIGH FREQUENCY VIBRATION\BELL HELICPTR TEXTRON\212 |
AD 75-07-02 | AIR FILTER SEAL\CESSNA AIRCRFT CO\177A\177B\177RG\177\REIMS AVI S A\CESSNA F177RG |
AD 75-07-03 | PLACARD FOR MACH TRIM SYSTEM\LOCKHEED AIRCRFT CORP\L-1011-385-1-14\L-1011-385-1-15\L-1011-385-1 |
AD 75-07-04 | RUDDER CONTROL BAR ASSYS\AMERCN GENERAL AIRCRFT HOLDING CO INC\AA-1A\AA-1B\AA-1\AA-5B\AA-5 |
AD 75-07-06 | SECOND STAGE TURBINE BLADES\ALLISON ENGINE CO INC\501-D22A |
AD 75-07-07 | EMERGENCY HATCH HANDLES\SIKORSKY AIRCRFT CORP\S-58A\S-58BT\S-58B\S-58C\S-58DT\S-58D\S-58ET\S-58E\S-58FT\S-58F\S-58G\S- |
AD 75-07-08 | TAIL ASSEMBLY\SIKORSKY AIRCRFT CORP\S-58A\S-58BT\S-58B\S-58C\S-58DT\S-58D\S-58ET\S-58E\S-58FT\S-58F\S-58G\S-58HT\S-58H |
AD 75-07-09 | ELECTRICAL SHOCK\MCDONNELL DOUGLAS CORP\DC-10-10F\DC-10-10\DC-10-30F (KC-10A)\DC-10-30\DC-10-40 |
AD 00-06-08 | PREVENT UNCOMMANDED MOVEMENT OF THE TRIMMABLE HORIZONTAL STABILIZER (THS)\AIRBUS INDUSTRIE\A330-301\A330-321\A330-322\ |
AD 00-06-09 | PREVENT UNEXPECTED POWER LOSS\TURBOMECA S A\ARRIEL 1A1\ARRIEL 1A2\ARRIEL 1A |
AD 00-06-10 | PREVENT SEPARATION OF THE TAIL BOOM AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER\BELL HELICPTR TEXTRON\407 |
AD 00-06-11 | PREVENT IN-FLIGHT ENGINE SHUTDOWN DUE TO ROLLER BEARING FAILURE FOLLOWING OIL CONTAMINATION\TURBOMECA S A\MAKILA 1A1\M |
AD 00-06-12 | PREVENT INJECTION WHEEL CRACKS\TURBOMECA S A\ARTOUSTE IIIB1\ARTOUSTE IIIB\ARTOUSTE IIID |
AD 00-06-13 | PREVENT FATIGUE CRACKING OF THE CORNERS OF THE DOOR FRAME AND THE CROSS BEAMS OF THE AFT CARGO DOOR\BOEING CO\737-200 |
AD 00-07-01 | PREVENT FAILURE OF THE NOSE LANDING GEAR (NLG) TO EXTEND AND LOCK DOWN PROPERLY\EMPRESA BRASILEIRA DE AERONAUTICA S A |
AD 00-07-03 | PREVENT CONTACT BETWEEN THE WIRE HARNESS AND THE FUEL LINE ASSEMBLY, WHICH COULD RESULT IN CHAFING OF THE WIRE HARNESS |
AD 00-07-05 | PREVENT CRACKING OF THE DIAGONAL BRACE OF THE NACELLE STRUT\BOEING CO\767-200 SERIES\767-300 SERIES\767-300F SERIES |
AD 00-07-06 | PREVENT FATIGUE CRACKING OF THE LOWER CORNERS OF THE DOOR FRAME AND CROSS BEAM OF THE FORWARD CARGO DOOR\BOEING CO\737 |
AD 00-07-08 | PREVENT BROKEN TIE RODS\BOEING CO\777-200 SERIES\777-300 SERIES |
AD 00-07-09 | PREVENT LOSS OF CONTROL OF THE AIRPLANE DURING TAKEOFF AND LANDING DUE TO LOOSE NUTS ON THE BOLTS OF THE INPUT CRANK A |
AD 00-07-10 | DETECT AND CORRECT CRACKED FIRE EXTINGUISHING TUBES IN THE ENGINE STRUTS\BOEING CO\747-200B SERIES\747-300 SERIES\747- |
AD 00-07-11 | PREVENT THE BRAKE HYDRAULIC FLUID FROM LEAKING BECAUSE OF THE BRAKE ASSEMBLY RODS CONTACTING THE BRAKE VALVE TUBING, W |
AD 00-07-12 | PREVENT DEGRADATION OF THE STRUCTURAL CAPABILITIES OF THE AFFECTED AIRPLANES\BOEING CO\727-100 SERIES\727-100C SERIES\ |
AD 00-07-13 | PREVENT CORRODED FUSE PINS\BOEING CO\757-200 SERIES\757-200PF SERIES |
AD 00-07-14 | PREVENT CHAFING OF THE PASSENGER SEAT WIRE ASSEMBLY AGAINST A BRACKET AT THE LOWER SIDEWALL PANEL DUE TO INSUFFICIENT |
AD 00-07-15 | PREVENT A DISPARITY BETWEEN THE RATINGS OF CERTAIN CIRCUIT BREAKERS AND THEIR ASSOCIATED ELECTRICAL CONNECTOR CONTACTS |
AD 00-07-16 | PREVENT ARCING FROM OCCURRING UNDER THE FORWARD CARGO COMPARTMENT FLOOR AS A RESULT OF DAMAGED EXTERNAL POWER FEEDER C |
AD 00-07-17 | ENSURE THAT THE UPPER MAIN CIRCUIT BREAKER PANEL OPENS FULLY\MCDONNELL DOUGLAS CORP\MD-11F\MD-11 |
AD 00-07-19 | PREVENT CHAFING AND DAMAGE TO EXTERNAL GROUND POWER FEEDER CABLES\MCDONNELL DOUGLAS CORP\MD-11F\MD-11 |
AD 00-07-20 | PREVENT ARCING AND OVERHEATING OF TERMINALS AND CONSEQUENT SMOKE AND FIRE IN THE FORWARD CARGO COMPARTMENT\MCDONNELL D |
AD 00-07-21 | PREVENT WIRE CHAFING OF THE CONTROL PANEL OF THE AUXILIARY POWER UNIT (APU)\MCDONNELL DOUGLAS CORP\MD-11F\MD-11 |
AD 00-07-23 | PREVENT A FAILURE OF THE THUNDERSTORM LIGHTS IN THE COCKPIT AFTER LOSS OF ALL GENERATED ELECTRICAL POWER\BOMBARDIER IN |
AD 00-07-24 | ENSURE ADEQUATE ELECTRICAL BONDING BETWEEN THE HORIZONTAL AND VERTICAL STABILIZERS\FOKKER SVCS\F.28 MARK 0070\F.28 MAR |
AD 00-07-25 | PREVENT INTERFERENCE AND CHAFING BETWEEN THE ALTERNATOR POWER FEEDER CABLES AND ADJACENT STRUCTURE, WHICH COULD RESULT |
AD 00-07-27 | PREVENT LOSS OF THE MAIN SOURCES OF ATTITUDE DATA, CONSEQUENT HIGH PILOT WORKLOAD, AND A SIGNIFICANT INCREASE IN THE L |
AD 00-07-51 | PREVENT LOSS OF ALL ALTITUDE INFORMATION AND SUBSEQUENT ESSENTIAL NAVIGATION DATA FOR CONTINUED SAFE FLIGHT AND LANDIN |
AD 00-08-01 | PREVENT CRACK INITIATION AND PROPAGATION LEADING TO TURBINE DISK FAILURE\ROLLS-ROYCE PLC\TAY 650-15 |
AD 00-08-02 | PREVENT FAILURE OF THE MAIN TRANSMISSION, LOSS OF ROTOR DRIVE, AND SUBSEQUENT LOSS OF CONTROL OF THE HELICOPTER\AGUSTA |
AD 00-08-04 | PREVENT SPRAG CLUTCH FAILURE, LOSS OF MAIN ROTOR RPM DURING AUTOROTATION, AND SUBSEQUENT LOSS OF CONTROL OF THE HELICO |
AD 00-08-05 | PREVENT FAILURE OF A MAIN ROTOR PITCH CONTROL LINK ROD-END SPHERICAL BEARING, INCREASED VIBRATION LEVEL, AND SUBSEQUEN |
AD 00-08-06 | PREVENT LOSS OF ELECTRICAL CONTINUITY\EUROCOPTER FRANCE\SA-366G1 |
AD 00-08-07 | PREVENT AN ENGINE FIRE FROM MOVING TO THE FUSELAGE AND TO THE LINES THAT CARRY FLAMMABLE FLUID THAT ARE LOCATED INBOAR |
AD 00-08-08 | PREVENT FAILURE OF THE KEEL BEAM STRUCTURE\BOEING CO\737-600 SERIES\737-700 SERIES\737-800 SERIES |
AD 00-08-09 | PREVENT SPRAG CLUTCH FAILURE, LOSS OF MAIN ROTOR RPM DURING AUTOROTATION, AND SUBSEQUENT LOSS OF CONTROL OF THE HELICO |
AD 00-08-10 | PREVENT CRITICAL LIFE-LIMITED ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DA |
AD 00-08-11 | PREVENT CRITICAL LIFE-LIMITED ROTATING ENGINE PART FAILURE\GENERAL ELECTRIC AIRCRFT ENGINES\CF6-45A\CF6-45A2\CF6-50A\C |
AD 00-08-13 | PROVIDE THE FLIGHT CREW WITH PROCEDURES TO DETECT AN UNCOMMANDED BRAKE APPLICATION CONDITION DURING TAXI AND TAKEOFF, |
AD 00-08-15 | PREVENT FATIGUE CRACKING OF THE UPPER WING SKIN\BOEING CO\777-200 SERIES\777-300 SERIES |
AD 51-02-02 | ASBESTOS CLOTH REMOVAL\SWIFT MUSEUM FOUNDT INC\GC-1A\GC-1B |
AD 51-03-01 | FUEL LINE REWORK\MOONEY MITE AIRCRFT CORP\M-18C 55\M-18C\M-18LA\M-18L |
AD 51-03-02 | LANDING GEAR CRANKSHAFTS\MARTIN-MARIETTA CORP\202A\202 |
AD 51-04-01 | FUEL VENT LINE CHECK VALVE\MARTIN-MARIETTA CORP\202 |
AD 51-04-02 | CYLINDER HOLDDOWN STUDS\WRIGHT AERONTCL DIV CURTISS-WRIGHT CORP\CYCLONE R-1820F-2A,R-1820F-3A,R-1820F-55,R-1820F-56,R- |
AD 51-07-01 | THROTTLE HOUSING\NAVION AIRCRFT CO LTD\NAVION (ARMY L-17A)\NAVION A (ARMY L-17B AND L-17C)\NAVION B\NAVION D\NAVION E\ |
AD 51-08-03 | STABILIZER SPAR ATTACHMENT\SWIFT MUSEUM FOUNDT INC\GC-1A\GC-1B |
AD 51-09-01 | POWER MEASUREMENT VALUES\PRATT & WHITNEY DIV\WASP MAJOR B5\WASP MAJOR TSB3-G |
AD 51-09-02 | HINGE BRACKETS AND BOLTS\MCDONNELL DOUGLAS CORP\C54-DC\C54A-DC\C54B-DC\C54D-DC\C54E-DC\C54G-DC\DC-4 |
AD 51-10-01 | WING FLAP OPERATING LINK\MCDONNELL DOUGLAS CORP\DC-6 |
AD 51-10-02 | CONTROL CABLE INSPECTION\LUSCOMBE DON AVI HISTORY FOUNDT INC\8A\8B\8C\8D\8E\8F\8\T-8F |
AD 51-10-04 | COWL MOUNTING CHANNELS\CESSNA AIRCRFT CO\190 |
AD 51-10-05 | FUSELAGE REINFORCEMENT REWORK\SWIFT MUSEUM FOUNDT INC\GC-1A\GC-1B |
AD 51-11-01 | MODIFICATION BOARD ITEMS\MARTIN-MARIETTA CORP\202A\202 |
AD 51-11-02 | ELEVATOR SPAR\CESSNA AIRCRFT CO\190\195 |
AD 51-11-04 | LANDING GEAR REWORK\SWIFT MUSEUM FOUNDT INC\GC-1A\GC-1B |
AD 51-13-01 | WING TOP COVER SPLICE ANGLES\MARTIN-MARIETTA CORP\202A\202 |
AD 51-14-01 | FUEL BOOSTER PUMP REMOVAL\RAYTHEON AIRCRFT CO\35-33\35-A33\35-B33\35-C33A\35-C33\35R\35\A35 |
AD 51-15-02 | CRANKCASES\WYTWORNIA SPRZETU KOMUNIKACYJNEGO\6A4-165-B3 |
AD 51-16-01 | TRIM TAB MODIFICATION\BELLANCA AIRCRFT\14-13-2\14-13 |
AD 51-16-02 | ELEVATOR TRIM TAB\BELLANCA INC\14-19 |
AD 51-18-01 | RUDDER TORQUE TUBE\CESSNA AIRCRFT CO\T-50 (ARMY AT-17, UC-78, NAVY JRC-1) |
AD 51-19-02 | OIL RADIATOR HOSE\PIPER AIRCRFT INC NEW\PA-18\PA-20\PA-22 |
AD 51-19-04 | MODIFICATION BOARD ITEMS\MARTIN-MARIETTA CORP\202A\202 |
AD 51-20-02 | MODIFICATION BOARD ITEMS\MARTIN-MARIETTA CORP\202A\202 |
AD 51-20-03 | COLLECTIVE PITCH BALLAST SYSTEM BRACKET\HILLER AVI\UH-12A\UH-12 |
AD 51-21-01 | RUDDER RIB FLANGES\CESSNA AIRCRFT CO\120\140 |
AD 51-21-02 | AILERON HINGE BRACKETS\PIPER AIRCRFT INC NEW\PA-12 |
AD 51-21-03 | RUDDER BELLCRANK\LUSCOMBE AIRCRFT CORP\11A |
AD 51-22-01 | GEAR SHAFT REPLACEMENT\SIKORSKY AIRCRFT CORP\S-51 |
AD 51-23-03 | BATTERY BOX INSULATION\PIPER AIRCRFT INC NEW\PA-16\PA-20\PA-22 |
AD 51-23-04 | ROTOR LINK ASSEMBLIES\SIKORSKY AIRCRFT CORP\S-51 |
AD 51-24-01 | EXHAUST VALVE SEATS\TEXTRON LYCOMING AVCO CORP\GO-435-C2 |
AD 51-24-02 | FIN INSPECTION\MARTIN-MARIETTA CORP\202 |
AD 51-25-01 | HORIZONTAL STABILIZER\CESSNA AIRCRFT CO\T-50 (ARMY AT-17, UC-78, NAVY JRC-1) |
AD 51-25-02 | CIRCUIT BREAKER COVER\MARTIN-MARIETTA CORP\202A\202 |
AD 51-26-01 | TAIL ROTOR REINFORCEMENT\BELL HELICPTR TEXTRON\47B\47B3\47D\47D1 |
AD 51-26-02 | AUTOMATIC PILOT SERVO CLUTCHES\LEAR INC\L-2 SERIES AUTOMATIC PILOTS |
AD 51-26-03 | DEFLATED HYDRAULIC VALVE LIFTERS\TELEDYNE CONTNTL MOTORS\E185-1\E185-10\E185-11\E185-2\E185-3\E185-5\E185-8\E185-9 |
AD 51-27-01 | ENGINE MOUNT REPLACEMENT\BELL HELICPTR TEXTRON\47B\47B3\47D\47D1\47E\47G\47G-2\47G-2A\47G-2A-1\47G-3\47G-3B\47G-3B-1\4 |
AD 72-10-04 | LANDING GEAR SYSTEM\RAYTHEON AIRCRFT CO\99A\99\A99A\A99\B99 |
AD 72-11-01 | POSSIBLE FIRE FROM FUEL VAPOR\PIPER AIRCRFT INC NEW\PA-23-235\PA-23-250 (NAVY UO-1)\PA-E23-250 |
AD 72-11-03 | ENGINE FUEL STARVATION\GRUMMAN AMERCN AVI CORP\G-21A (ARMY OA-9, NAVY JRF-1, -2, -3, -4, -5, AND\G-21 |
AD 72-11-04 | FAILURE TAIL ROTOR DRIVE PINS\ENSTROM HELICPTR CORP\F-28A |
AD 72-11-05 | AUXILIARY FUEL CELL LEAKS\CESSNA AIRCRFT CO\411A\411\421A\421B\421C\421 |
AD 72-12-01 | MAIN GEAR DOWNLOCK SHAFT\BOEING CO\727 SERIES\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES\727C SERIE |
AD 72-12-03 | FAILURE OF AIR BOTTLES\DE HAVILLAND AIRCRFT CO LTD (ENGLAND)\D H 104 DOVE SERIES 1A,2A,5A,5BA,6A,6BA,7AXC,7A,8AXC,8A |
AD 72-12-04 | SUPPORT OF FUEL LINES\CESSNA AIRCRFT CO\401A\401B\401\402A\402B\402C\402 |
AD 72-12-05 | LANDING GEAR JACK ASSEMBLIES\DE HAVILLAND AIRCRFT CO LTD (ENGLAND)\D.H.114 HERON SERIES 2A\D.H.114 HERON SERIES 2DA\D. |
AD 72-13-02 | MAIN LANDING GEAR BEAMS\GENERAL DYNAMICS CORP\22M\22 |
AD 72-13-03 | FUEL BOOST PUMP CIRCUIT\BELLANCA INC\17-30 |
AD 72-13-07 | DRIVE SHAFT ASSEMBLIES\HILLER AVI\1100\FH-1100 |
AD 72-13-08 | MAIN ROTOR BLADES\HILLER AVI\UH-12L4\UH-12L\ROGERSON HILLER CORP\UH-12E-L |
AD 72-14-01 | FAILURE OF PROPELLER BLADE\DOWTY AEROSPC PROPELLERS\(C) R.209/4-40-4.5\(C) R.245/4-40-4.5\(C) R.259/4-40-4.5\(C) R130/ |
AD 72-14-02 | FUEL OR FUMES IN WINGS OR CABIN\AERMACCHI S P A\S.205 - 18/F\S.205 - 18/R\S.205 - 20/F\S.205 - 20/R\S.205 - 22/R\S.208 |
AD 72-14-03 | FAILURES OF FLAP CHAINS\VICKERS-ARMSTRONGS (AIRCRFT LTD )\VISCOUNT 744\VISCOUNT 745D\VISCOUNT 810 |
AD 72-14-04 | MAIN GEAR DOOR TORQUE TUBE\SABRELINER CORP\NA-265-20\NA-265-30\NA-265-40\NA-265-60\NA-265 |
AD 72-14-05 | ENGINE EXHAUST SYSTEM STACKS\PIPER AIRCRFT INC NEW\PA-23-250 (NAVY UO-1)\PA-E23-250 |
AD 72-14-06 | FIRST STAGE (LOW PRESSURE) IMPELLERS\ROLLS-ROYCE PLC\DART 542-10J\DART 542-10K\DART 542-10\DART 542-4K\DART 542-4 |
AD 72-14-07 | BOLTS IN STABILATOR HINGE FITTINGS\PIPER AIRCRFT INC NEW\PA-28-140\PA-28-150\PA-28-151\PA-28-160\PA-28-161\PA-28-180\P |
AD 72-15-01 | WING TO FUSELAGE ATTACH BOLTS\DE HAVILLAND AIRCRFT CO LTD (ENGLAND)\D.H.114 HERON SERIES 2A\D.H.114 HERON SERIES 2DA\D |
AD 72-15-02 | ALTERNATOR COOLING FANS\PRESTOLITE CO\ALTERNATOR COOLING FANS |
AD 72-15-03 | SPOILER ACUTUATOR BOLTS\LEARJET INC\24A\24B-A\24B\24C\24D-A\24D\24E\24F-A\24F\24\25A\25B\25C\25D\25F\25 |
AD 72-15-04 | FLAME PROPAGATION IN ENGINE FIRE ZONE\BOMBARDIER INC\CL-215-1A10 |
AD 72-16-02 | VOLPAR NOSE GEAR FORK\RAYTHEON AIRCRFT CO\3NM\3N\3TM\C-45G\C-45H\D18C\D18S\E18S-9700\E18S\G18S\H18\JRB-6\RC-45J\TC-45G |
AD 72-16-03 | STAGE 2 HIGH PRESSURE TURBINE DISCS\GENERAL ELECTRIC AIRCRFT ENGINES\CF6-6D1\CF6-6D |
AD 72-16-04 | CRACKS IN NOSE GEAR DRAG LINK\AERMACCHI S P A\S.205 - 18/R\S.205 - 20/R\S.205 - 22/R |
AD 72-16-06 | ELECTRICAL FEEDER WIRE GAGE\CARSON HELICPTRS INC\S-61L\SIKORSKY AIRCRFT CORP\S-61A\S-61L\S-61N\S-61R |
AD 72-16-07 | WING MAIN SPAR PICKUP FITTINGS\DE HAVILLAND AIRCRFT CO LTD (ENGLAND)\D H 104 DOVE SERIES 1A,2A,5A,5BA,6A,6BA,7AXC,7A,8 |
AD 72-16-08 | CRACKS IN SLEEVES GEAR BOX OIL LINE\EUROCOPTER FRANCE\SA 3180-ALOUETTE ASTAZOU\SA 318B-ALOUETTE ASTAZOU\SA 318C-ALOUET |
AD 72-16-09 | TAIL ROTOR INPUT GEAR SHAFT ASSEMBLY\MD HELICPTR INC\369A\369HE\369HM\369HS\369H |
AD 72-16-10 | AFT TRANSMISSION RING\BOEING DEFENSE & SPACE GROUP\107-II |
AD 72-17-01 | INDUCTION AIR BOX VALVE\PIPER AIRCRFT INC NEW\PA-34-200 |
AD 72-17-05 | ELECTRIC TRIM SWITCH\PIPER AIRCRFT INC NEW\PA-28-180\PA-28-235\PA-28R-180\PA-28R-200\PA-32-260\PA-32-300 |
AD 72-18-01 | FUEL SELECTOR VALVE WARNING LIGHT\RAYTHEON AIRCRFT CO\35\A35\B35\C35 |
AD 72-18-03 | CORROSION OF RUDDER & ELEVATOR CABLES\AMERCN CHAMPION AIRCRFT CORP\7GCAA\7GCBC\7KCAB\8KCAB |
AD 72-18-04 | VNE LIMITATIONS\MD HELICPTR INC\369HE\369HM\369HS\369H |
AD 72-18-06 | STABILATOR TIP BALANCE WEIGHTS\PIPER AIRCRFT INC NEW\PA-34-200 |
AD 72-18-09 | CONTROL RODS AND ELECTRICAL SYSTEMS\VICKERS-ARMSTRONGS (AIRCRFT LTD )\VISCOUNT 744\VISCOUNT 745D\VISCOUNT 810 |
AD 72-19-01 | MAIN ROTOR RETENTION STRAPS\BELL HELICPTR TEXTRON\206A-1 (OH-58A)\206A\206B-1\206B |
AD 77-17-06 | AUXILIARY POWER UNITS\AIRESEARCH\TSCP700-4B\TSCP700-5 |
AD 77-17-08 | FUEL REGULATOR P1 MULTIPLIER LEVER\ALLIEDSIGNAL INC\T5307A\T5309A\T5309B\T5309C\T5311A\T5311B\T5313A\T5313B\T5317A\T53 |
AD 77-17-11 | REAR SPAR LOWER CAP\TRANSCONTNTL AND WESTERN AIR INC\ARMY B-17F\ARMY B-17G |
AD 77-17-12 | WING SPAR CHORD SPLICE JOINTS\MARTIN-MARIETTA CORP\404 |
AD 77-17-13 | NOSE LANDING GEAR DOORS\BOMBARDIER INC\CL-215-1A10\CL-215-6B11 (CL-215T VARIANT)\CL-215-6B11 (CL-415 VARIANT) |
AD 77-18-01 | ENGINE OIL COOLER\MOONEY AIRCRFT CORP\M20E\M20F\M20J |
AD 77-18-04 | CABIN PRESSURIZATION\RAYTHEON AIRCRFT CO\200T\200\A100\B100\C90\E90 |
AD 77-18-05 | VARIABLE AUTHORITY STEERING SYSTEM\FAIRCHILD AIRCRFT CORP\SA226-AT\SA226-TC\SA226-T |
AD 77-18-06 | HORIZONTAL STABILIZER\BOEING CO\727 SERIES\727-100 SERIES\727-100C SERIES\727-200 SERIES\727-200F SERIES\727C SERIES |
AD 77-18-07 | JAMMED ELEVATOR DRIVE\LOCKHEED AIRCRFT CORP\L-1011-385-1-14\L-1011-385-1-15\L-1011-385-1\L-1011-385-3 |
AD 77-19-02 | CABIN DOOR LOCKING MECHANISM\LEARJET INC\23\24A\24B-A\24B\24C\24D-A\24D\24E\24F-A\24F\24\25A\25B\25C\25D\25F\25 |
AD 77-19-03 | MAIN ROTOR RETENSION STRAPS\MD HELICPTR INC\369D |
AD 77-19-05 | FLYING WIRE TERMINALS\AG CAT CORP\G-164A\G-164B (WITH 73 INCH WING GAP)\G-164B-15T\G-164B-20T\G-164B-34T\G-164B |
AD 77-19-06 | AILERON CABLES\PIPER AIRCRFT INC NEW\PA-31-300\PA-31-325\PA-31-350\PA-31 |
AD 77-19-07 | CONTROL COLUMN ASSEMBLY\RAYTHEON AIRCRFT CO\18A\18D\18S (ARMY C-45C)\A18A\A18D\B18S (ARMY F-2)\C18S\D18C\D18S\E18S-970 |
AD 77-20-02 | TAIL ROTOR SPINDLE\ENSTROM HELICPTR CORP\280\28OC\F-28A\F-28C\F-28 |
AD 77-20-06 | WING STRUT CORROSION\PILATUS AIRCRFT LTD\PC-6-H1\PC-6-H2\PC-6/350-H1\PC-6/350-H2\PC-6/350\PC-6/A-H1\PC-6/A-H2\PC-6/A\P |
AD 77-21-01 | TAIL ROTOR GEAR BOXES\BELL HELICPTR TEXTRON\47B\47B3\47D\47D1\47E\47G\47G-2\47G-2A\47G-2A-1\47G-3\47G-3B\47G-3B-1\47G- |
AD 77-21-02 | FUEL TANKS\AEROSPATIALE (SOCIETE NATIONALE INDUSTRIELLE AEROSPATIALE)\NORD 262A SERIES |
AD 77-21-03 | RUDDER SPAR CRACKS\PIPER AIRCRFT INC NEW\PA-36-285 |
