N962AX, cancelled May 13, 2015

Service difficulty reports · 60

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N962AX' AND deregistration_id = 'N962AX-2015-05-13'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ABXA070358Door Frame · gougedDOOR JAMB STA 200, LONGERON 15 RIGHT GOUGED. REPAIRED DOOR JAMB IAW DC9 SRM.Oct 8, 2007 · N962AX · Doug DC941 · Fuselage Main, StructureSDR ABXA070356Repair · crackedMAIN ENTRY DOOR FORWARD LOWER CORNER REPAIR CRACKED. REMOVED AND REPLACED REPAIR IAW DC9 SRM 52-01 FIG 4.Oct 8, 2007 · N962AX · Doug DC941 · Passenger/Crew DoorsSDR ABXA070357Angle · crackedMAIN ENTRY DOOR UPPER AFT CORNER, ANGLE CRACKED INSIDE LIGHTENING HOLE. REPAIRED MAIN ENTRY DOOR UPPER AFT ANGLE IAW DC9 SRM.Oct 8, 2007 · N962AX · Doug DC941 · Passenger/Crew DoorsSDR ABXA070355Fitting · crackedAFT LOWER CARGO DOOR BEAM END FITTING WAS CRACKED AFT END OF NR 2 BEAM. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.Oct 6, 2007 · N962AX · Doug DC941 · Cargo/Baggage DoorsSDR ABXA070354Cusp Web · crackedCUSP WEB CRACKED ON LEFT SIDE AT STA 980. REPAIRED CRACKED WEB IAW REA E-43520.Oct 5, 2007 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA070353Cusp Web · crackedCUSP WEB CRACKED AT STA 1022 - 1036. REPLACED CUSP WEB AS REQUIRED IAW DC9 SRM.Oct 5, 2007 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA070324Wheel · separatedAIRCRAFT BLOCKED IN WITH NR 4 MAIN TIRE FLAT. FOUND NR 4 WHEEL RIM SEPARATED. REPLACED NR 4 MAIN WHEEL ASSEMBLY, NR 4 BRAKE AND THE RIGHT MAIN LANDING GEAR PISTON AND AXLE ASSEMBLY IAW DC9 MM CHAPTER 32.Sep 28, 2007 · N962AX · Doug DC941 · Wheel/Ski/FloatSDR ABXA060024Torque Tube · damagedLANDING GEAR MALFUNCTION, GEAR DOOR OPEN LIGHT ILLUMINATED WITH GEAR HANDLE DOWN & 3 GREEN WHILE IN FLIGHT. LANDING GEAR WAS RECYCLED. REPLACED GEAR DOOR, TORQUE TUBE AND DOOR SEQUENCE DRIVE ARM IAW DC9 MM 32-11-03-2-02-1.Jan 12, 2006 · N962AX · Doug DC941 · Landing Gear Door Retract SectionSDR ABXA050258Cargo Track · corrodedFORWARD LOWER CARGO LEFT TRACK HAD EXFOLIATED CORROSION AT TWO ATTACH FASTENERS BETWEEN STA 218 AND 237. REPLACED BAD SECTION OF TRACK IAW DC-9 SSRM K05159 DRAWING.Oct 12, 2005 · N962AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA050261Bulkhead · crackedAFT PRESSURE BULKHEAD DOOR UPPER LT CORNER 13 DOUBLER HAD RADIAL CRACK EXTENDING FROM STOP DRILL. CRACK EXCEEDED APPLICABILITY AND CRACK REPAIR LIMITS FOR PREVIOUS J060088-1 ANGLE REPAIR. STOP DRILLED CRACKS AND REPAIRED IAW SRM.Oct 11, 2005 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA050257Intercostal · crackedAFT ASSY COMPARTMENT INTERCOSTAL BETWEEN FS 1114 AND FS 1133, LONGERON 17 RIGHT AND LONGERON 16 RIGHT HAD A CRACK ON BOTTOM FORWARD SIDE. FABRICATED AND INSTALLED REPAIR ANGLE AS REQUIRED IAW DC-9 SRM K05159 DRAWING.Oct 11, 2005 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA050260Skin · corrodedFUSELAGE SKIN BULGED AT STA 579, LONERON 30, EVIDENCE OF CORROSION INTERNAL. REMOVED INTERNAL CORRODED DOUBLER / INSTALLED NEW DOUBLER IAW SRM.Oct 10, 2005 · N962AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA050256Skin · crackedFUSELAGE CRACK AT STA. 1087, LONGERON 2 LEFT. REPAIRED AREA IAW DC-9 SRM 53-01.Oct 10, 2005 · N962AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA040377Pressure Panel · leakingDESCENDING, PASSING FL 180, AUTOPILOT WITH HEADING MODE ENGAGED, NOTICED A/C DRIFTED 20 DEGREES LT OF COURSE WITH NOSE DOWN, SWITCHED TO TURN KNOB, A/C WOULD NOT RESPOND. DISENGAGED AUTOPILOT, YOKE STILL IN LT/FWD POSITION. WENT TO ROLL WINGS LEVEL BUT YOKE JANov 12, 2004 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA040183Link · damagedAIRCRAFT VIBRATES AT 320 KTS AT LOW ALTITUDE CLIMB AND CRUISE REGARDLESS OF POWER SETTINGS. REPLACED RT WING TO STRUCTURE TRAILING LINKS AND HARDWARE DUE TO EXCESSIVE MOVEMENT IAW MM 20-10, 20-15 & 20-16.May 11, 2004 · N962AX · Doug DC941 · Aerodynamic FairingsSDR ABXA040059Stiffener · crackedAFT PRESSURE BULKHEAD FORWARD RIGHT STIFFENER, 4TH FROM TOP, WAS CRACKED AT TEE. REPAIRED AREA IAW DC-9 SSRM K05159.Jan 28, 2004 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA020353Link · crackedNR 1 ENGINE UPPER RIGHT LINK THRUST REVERSER CRACKED. REPLACED IAW MM.Dec 6, 2002 · N962AX · Doug DC941 · Engine Thrust ReverserSDR ABXA020036Stringer · crackedRIGHT STAB. INTERIOR #2 UPPER STRINGER, WAS CRACKED AT XHS 204.1, APPROXIMATELY 1.5" INBOARD TO OUTBOARD OF RIB. REPAIRED #2 STRINGER IAW DC-9 SRM 55-02.Jun 5, 2002 · N962AX · Doug DC941 · Horizontal Stabilizer, Spar/RibSDR ABXA020035Stringer · crackedRIGHT STAB. INTERIOR, #3 UPPER STRINGER, WAS CRACKED AT XHS 158, 1" INBOARD TO OUTBOARD OF RIB. REPAIRED #3 STRINGER IAW DC-9 SRM 55-02.Jun 5, 2002 · N962AX · Doug DC941 · Horizontal Stabilizer, Spar/RibSDR ABXA000298Control Box · failedON TAKEOFF, THE GREEN NOSE LANDING GEAR LIGHT WAS OUT WITH THE GEAR IN THE DOWN POSITION. THE RED NOSE GEAR UNSAFE LIGHT WAS ILLUMINATED WITH THE GEAR HANDLE UP. RECYCLED THE GEAR AND ACCOMPLISHED ABNORMAL PROCEDURES. THE UNSAFE LIGHT EXTINGUISHED. REPLACEJun 12, 2000 · N962AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA000112Control · failedLEFT MAIN GEAR INDICATED UNSAFE POSITION ON GEAR EXTENSION. MAIN GEAR DOWNLOCK SWITCH INDICATES GREEN. GEAR WARNING HORN COULD NOT BE SILENCED. PULLED P26 AND SILENCED HORN. LANDING UNEVENTFUL. CREW RECYCLED GEAR. RERACKED PROX CONTROL BOX. OPS CHECKED Feb 18, 2000 · N962AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA9900830Power Supply · dischargedEMERGENCY LIGHTS INOPERATIVE INTERMITTENTLY. REPLACED EMERGENCY LIGHT POWER SUPPLY.Dec 6, 1999 · N962AX · Doug DC941 · Emergency LightingSDR ABXA9701363Skin · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE CENTER WING TANK LOWER KEEL DOUBLER HAD NUMEROUS CORROSION BLENDOUTS BEYOND SRM LIMITS. REPAIRED CENTER WING LOWER KEEL DOUBLER IAW ABX REA D957-19608-MR.Jul 31, 1997 · N962AX · Doug DC941 · Wing, Plate/SkinSDR ABXA9701362Longeron · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND LONGERON 25 LEFT TEE ANGLE CORRODED AT FS 1152. REPAIRED LONGERON 25 IAW ABX REA D953-20348-MR.Jul 31, 1997 · N962AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA9701392Fitting · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND KEEL FITTING AT FS 737 CRACKED. REPLACED KEEL FITTING AT FS 737 IAW DC-9 SRM CHAPTER 51-30-1, 51-30-2 AND 51-30-5.Jul 10, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701385Bracket · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE SLAT CONTROL VALVE PULLEY BRACKET CORRODED AT FS 675. REPLACED SLAT CABLE PULLEY BRACKET AND RIGGED SLAT CONTROL SYSTEM IAW DC-9 MAINTENANCE MANUAL CHAPTER 27-80-2.Jul 9, 1997 · N962AX · Doug DC941 · Leading Edge Slat Control SystemSDR ABXA9701383Jamb · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT MAIN LANDING GEAR DOOR FORWARD JAMB CRACKED AT UPLOCK SWITCH. REPAIRED DOOR JAMB IAW ABX REA D953-20150.Jul 9, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701384Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT ENGINE PYLON UPPER BEAVERTAIL FITTING CORRODED. REMOVED AND REPLACED LEFT BEAVERTAIL FITTING AND REPAIRED AREA IAW ABX REA D954-20135-MR AND DC-9 SRM CHAPTER 51-30-5.Jul 8, 1997 · N962AX · Doug DC941 · Nacelle/Pylon, Attach FittingsSDR ABXA9701387Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT ENGINE PYLON LOWER BEAVERTAIL FITTING CORRODED. REPAIRED LEFT LOWER BEAVERTAIL IAW ABX REA D954-20074 AND DC-9 SRM CHAPTER 53-04, FIGURE 13.Jul 1, 1997 · N962AX · Doug DC941 · Nacelle/Pylon, Attach FittingsSDR ABXA9701386Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT ENGINE PYLON LOWER BEAVERTAIL FITTING CORRODED. REPAIRED RIGHT PYLON LOWER BEAVERTAIL IAW ABX REA D954-19607-MR.Jul 1, 1997 · N962AX · Doug DC941 · Nacelle/Pylon, Attach FittingsSDR ABXA9701388Bracket · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT LATERAL CONTROL MIXER BRACKET CRACKED AND CORRODED. REPLACED LEFT LATERAL CONTROL MIXER BRACKET IAW DC-9 MAINTENANCE MANUAL CHAPTERS 20-16-0 AND 27-61-4.Jun 27, 1997 · N962AX · Doug DC941 · Aileron Control SystemSDR ABXA9701361Fitting · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT PYLON UPPER BEAVERTAIL EXCESSIVELY CORRODED. REPAIRED RIGHT UPPER BEAVERTAIL IAW ABX REA D954-19607-MR.Jun 27, 1997 · N962AX · Doug DC941 · Nacelle/Pylon StructureSDR ABXA9701389Rib · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT WING NR 2 SLAT TRACK INBOARD RIB CRACKED AT AFT LOWER FLANGE. REPLACED NR 2 RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jun 24, 1997 · N962AX · Doug DC941 · Wing, Rib/BulkheadSDR ABXA9701376Skin · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND TWO FUSELAGE SKIN CRACKS AT RIVETS AT FS58 ON LEFT HAND SIDE. REPAIRED IAW DC-9 SRM CHAPTER 53-01.Jun 23, 1997 · N962AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA9701391Rib · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LEFT WING LEADING EDGE RIB AT STATION XIS 136 CORRODED. REPLACED WING LEADING EDGE RIB AT XIS 136 IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jun 19, 1997 · N962AX · Doug DC941 · Wing, Rib/BulkheadSDR ABXA9701390Bulkhead Jamb · crackedWHILE COMPLYING WITH VISUAL INSPECTION OF THE AFT PRESSURE BULKHEAD IAW AD 85-01-02 PER SB 53-137, FOUND THE BULKHEAD DOOR JAMB CRACKED JUST BELOW THE UPPER LEFT CORNER OF DOOR CUTOUT. REPLACED CRACKED DOUBLER IAW DC-9 SRM CHAPTER 51-30-5.Jun 18, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701382Jamb · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE RIGHT VENTRAL DOOR JAMB FRAME CORRODED FROM FS 1133 TO FS 1163. REPLACED THE UPPER JAMB CAP AND DOOR STOP FITTINGS IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jun 17, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701381Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 9 LEFT. REMOVED AND REPLACED CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 17, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701379Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 9 RIGHT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1.Jun 16, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701378Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD LATERAL STIFFENER CRACKED AT LONGERON 7R. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 16, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701364Former · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND A FRAME FITTING CRACKED AT FS 675 JUST INBOARD OF LEFT CANTED KEEL. REPAIRED FRAME FITTING IAW DC-9 SRM CHAPTER 53-03, FIGURE 12.Jun 16, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701380Slat · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE NR 1 LEFT SLAT CORRODED AT CENTER ATTACH FITTING. REPLACED NR 1 LEFT SLAT IAW DC-9 MAINTENANCE MANUAL, CHAPTER 27-80-1.Jun 13, 1997 · N962AX · Doug DC941 · Leading Edge DevicesSDR ABXA9701360Keelbeam · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE KEEL BEAM HAD EXCESSIVE CORROSION BLENDOUTS AT FS665.0. REPAIRED KEEL BEAM IAW ABX REA D953-19727-MR.Jun 13, 1997 · N962AX · Doug DC941 · Fuselage Main, KeelSDR ABXA9701377Bulkhead Skin · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD DOOR JAMB CRACKED ON RIGHT SIDE. REPAIRED DOOR JAMB IAW DC-9 SRM CHAPTER 53-05.Jun 12, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701374Bracket · corrodedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE LOWER RUDDER HINGE BRACKET CORRODED. REPLACED HINGE BRACKET IAW DC-9 MM 20-16-0.Jun 12, 1997 · N962AX · Doug DC941 · Vertical StabilizerSDR ABXA9701373Former · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND A FORMER CRACKED AT FS660 IN RIGHT CANTED KEEL AREA. REPLACED FORMER AND CLIP IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Jun 12, 1997 · N962AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA9701370Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 12 RIGHT. REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701369Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 14 RIGHT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701368Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 14 LEFT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, BulkheadSDR ABXA9701367Bulkhead Clip · crackedWHILE COMPLYING WITH 'D' INSPECTION, FOUND THE AFT PRESSURE BULKHEAD FORWARD LATERAL STIFFENER END CLIP CRACKED AT LONGERON 15 LEFT. REMOVED AND REPLACED END CLIP IAW DC-9 SRM CHAPTERS 51-30-1 AND 51-30-5.Jun 10, 1997 · N962AX · Doug DC941 · Fuselage Main, Bulkhead
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