N952AX, cancelled Apr 4, 2018

Service difficulty reports · 91

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 = 'N952AX' AND deregistration_id = 'N952AX-2018-04-04'
  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 ABXA080250Bolt · looseNR 1 MLG TIRE REQUIRED CHANGE PER PEA 34100014-001. REMOVED AND REPLACED NR 1 MLG TIRE ASSY IAW DC9 AMM 32-40-01-2. WHEEL BOLTS LOOSE. INSPECTED, REPAIRED IAW ABX SPEC WORKSHEET BS421B DATED 12-21-07 AND THE ABX WHEEL AND TIRE MANUAL, REV 17.Sep 29, 2008 · N952AX · Doug DC941 · Wheel/Ski/FloatSDR ABXA080217Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK IAW DC9 MM. OPS CHECKED GOOD. (S)Aug 12, 2008 · N952AX · Doug DC941 · Emergency LightingSDR ABXA080157Uplock Switch · malfunctionedSTA SWF, CPM GEAR RETRACTION, AFTER TAKEOFF, LEFT "GEAR UNSAFE" LIGHT REMAINED ILLUMINATED. CYCLED GEAR AND NOTED THAT LEFT HEAR DOWN "GREEN LIGHT" ILLUMINATED WITHOUT DELAY. "NO CYCLE TIME" UPON RETRACTION ALL INDICATIONS WERE NORMAL. DEFERRED CLEARED DI 6Jun 12, 2008 · N952AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA070413Frame · corrodedFORWARD LOWER CARGO FRAME AT STATION 579 WAS CORRODED AT LONGERON 30. REPAIRED FRAME IN ACCORDANCE WITH DC9 SRM 53-03.Oct 29, 2007 · N952AX · Doug DC941 · Fuselage Main, FrameSDR ABXA070412Bracket · corrodedSPOILER CONTROL TORQUE TUBE BRACKET CORRODED. REMOVED AND REPLACED SPOILER TORQUE TUBE BRACKET IN ACCORDANCE WITH DC9 MAINTENANCE MANUAL 20-16-00-2-0001.Oct 22, 2007 · N952AX · Doug DC941 · SpoilersSDR ABXA070409Longeron · crackedLONGERON 17 LEFT CRACKED AT FRAME ATTACH POINTS AT STATION 1041 AND 1056. REMOVED AND REPLACED LONGERON SECTION IN ACCORDANCE WITH DC9 SRM.Oct 20, 2007 · N952AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA070408Longeron · crackedLONGERON 16 RIGHT CRACKED AT UPPER FRAME ATTACH HOLE AT STATION 1041. REMOVED AND REPLACED SECTION IN ACCORDANCE WITH DC9 SRM 53-02.Oct 20, 2007 · N952AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA070405Gusset · crackedFS 206.00, LONGERON 16 LEFT GUSSET CRACKED. REMOVED AND REPLACED GUSSET IN ACCORDANCE WITH DC9 SRM.Oct 20, 2007 · N952AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA070411Floorbeam · corrodedFLOORBEAM AT STATION 1011 LOWER FORWARD FLANGE CORRODED AT APPROXIMATELY RIGHT BUTT LINE 15 UNDER NUT PLATES. REPAIRED FLOORBEAM IN ACCORDANCE WITH DC9 SSRM K07411.Oct 20, 2007 · N952AX · Doug DC941 · Fuselage Main, Floor BeamSDR ABXA070407Attach Angle · crackedLOWER PYLON LEADING EDGE ATTACH ANGLE CRACKED. REMOVED AND REPLACED FORWARD SECTION OF PYLON LOWER ATTACH ANGLE IN ACCORDANCE WITH DC9 SRM 54-04.Oct 20, 2007 · N952AX · Doug DC941 · Nacelle/Pylon, Attach FittingsSDR ABXA070406Gusset · crackedFS 206.00, APPROXIMATE LONGERON 11 LEFT, GUSSET CRACKED. REMOVED AND REPLACED GUSSET IN ACCORDANCE WITH DC9 SRM.Oct 20, 2007 · N952AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA070410Seat Track · corrodedSEAT TRACK CORRODED AT LEFT BUTT LINE 9.88, STATION 996-1021. REMOVED AND REPLACED TRACK IN ACCORDANCE WITH DC9 SRM 51-30-5 AND 51-30-1.Oct 20, 2007 · N952AX · Doug DC941 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA070401Frame · corrodedFORWARD LOWER CARGO AFT SIDE AND LOWER LEG OF FRAME CORRODED FS 598 AT LONGERON 30. BLENDED AREA IN ACCORDANCE WITH DC9 SRM.Oct 19, 2007 · N952AX · Doug DC941 · Fuselage Main, FrameSDR ABXA070402Support Angle · crackedLEFT MAIN LANDING GEAR DOOR ACTUATOR SUPPORT ANGLE CRACKED FORWARD SIDE. REMOVED AND REPLACED IN ACCORDANCE WITH DC9 SRM.Oct 19, 2007 · N952AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA070400Support · crackedRIGHT INBOARD SPOILER TORSION BAR CENTER SUPPORT CRACKED IN THREE (3) PLACES. REPLACED SUPPORT ASSEMBLY IN ACCORDANCE WITH DC9 SRM 51-30-5.Oct 19, 2007 · N952AX · Doug DC941 · SpoilersSDR ABXA070403Longeron · crackedLONGERON 4 LEFT CRACKED AT FRAME ATTACH POINTS AT STATION 160. SPLICED IN NEW LONGERON IN ACCORDANCE WITH DC9 SRM.Oct 19, 2007 · N952AX · Doug DC941 · Fuselage Main, Longeron/StringerSDR ABXA070399Attach Fitting · crackedLEFT WING OUTBOARD SPOILER, OUTBOARD SPOILER ATTACH FITTING CRACKED. REMOVED AND REPLACED FITTING IN ACCORDANCE WITH DC9 SRM.Oct 19, 2007 · N952AX · Doug DC941 · SpoilersSDR ABXA070404Counterbalance · corrodedRIGHT ELEVATOR COUNTERBALANCE HEIGHT RUSTY IN SEVERAL AREAS. REPAIRED AREA IN ACCORDANCE WITH REA D955-56583.Oct 12, 2007 · N952AX · Doug DC941 · Elevator StructureSDR ABXA070090Battery · dischargedEMERGENCY LIGHTS WOULD NOT STAY ON. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW MM 33-53-00.Apr 7, 2007 · N952AX · Doug DC941 · Emergency LightingSDR ABXA060280Control Box · defectiveRT MAIN GEAR UNSAFE LIGHT WITH ASSOCIATED RT LANDING GEAR GREEN LIGHT. ALTERNATE MAIN GEAR INDICATION OPERATES NORMAL. REPLACED PROXIMITY SWITCH CONTROL BOX IAW MM 32-60-01-2.Oct 13, 2006 · N952AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA060080Duct · looseWHEN PRESSURIZATION WAS SET AT TOP OF DESCENT AND POWER WAS PULLED BACK (1.3 EPR), THE CABIN BEGAN TO CLIMB AT 300 FPM. CABIN ALTITUDE REACHED 10,000 FT AND CREW TOOK OVER PRESSURIZATION MANUALLY. CREW WENT ON OXYGEN. FOUND COLD AIR DUCT LOOSE AT WATER SEPAFeb 8, 2006 · N952AX · Doug DC941 · Air Distribution SystemSDR ABXA050269Stop Fitting · crackedAFT P DOME DOOR JAMB UPPER RIGHT DOOR STOP FITTING CRACKED. REMOVED AND REPLACED AFT P DOME DOOR JAMB UPPER RIGHT DOOR STOP FITTING IAW DC-9 SRM 51-30-1, 51-30-2 AND 51-30-5.Oct 23, 2005 · N952AX · Doug DC941 · Fuselage Main, StructureSDR ABXA050266Fitting · corrodedEND FITTING CORRODED JUST INBOARD OF LONGERON 29 RIGHT IN KEEL BEAM AREA LOWER WING CENTER SECTION FS 649. REMOVED AND REPLACED END FITTING IAW DC-9 SRM 51-30-5.Oct 20, 2005 · N952AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050268Keelbeam · crackedEND FITTING SIDE SUPPORT CRACKED ON LEFT SIDE OF KEEL BEAM CENTER SUPPORT LONGERON 30, FS 646 APPROXIMATELY. REMOVED AND REPLACED END FITTING AT STA 646, LONGERON 30 IAW DC-9 SRM 51-30-5.Oct 20, 2005 · N952AX · Doug DC941 · Fuselage Main, KeelSDR ABXA050267Fitting · corrodedEND FITTING CORRODED LONGERON 29 LEFT APPROXIMATELY STA FS 649, LOWER WING CENTER SECTION IN KEEL BEAM AREA. REMOVED AND REPLACED LONGERON END FITTING IAW DC-9 SRM 51-30-5.Oct 20, 2005 · N952AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050265Shear Tie · crackedSHEAR TIE CRACKED AT STA 1021 BETWEEN LONGERON 15 RIGHT AND LONGERON 16 RIGHT. REMOVED AND REPLACED SHEAR TIE IAW DC-9 SRM 51-30-5 AND 51-30-2.Oct 19, 2005 · N952AX · Doug DC941 · Fuselage Internal Mounting StructureSDR ABXA050264Attach Bracket · crackedATTACH BRACKET ON AFT SIDE OF PYLON BULKHEAD AT LONGERON 17 RIGHT WAS CRACKED. REMOVED AND REPLACED BRACKET IAW DC9 SRM 51-30-2.Oct 19, 2005 · N952AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA050203Control Box · defectiveGEAR DOOR OPEN LIGHT ILLUMINATED IN FLIGHT. INSPECTED AIRCRAFT MAIN LANDING GEAR DOOR UPLATCHES AND MECHANISMS IAW DC-9 AMM 32-60-03-2. ALL OKAY, NO DEFECTS NOTED. INSPECTED PROX SENSORS FOR POSITIONING AND ATTACHMENT, NO DEFECTS NOTED. REMOVED AND REPLACEAug 24, 2005 · N952AX · Doug DC941 · Landing Gear Position and WarningSDR ABXA040097Skin · crackedFUSELAGE SKIN CRACKED AT LEFT AFT NOSE LANDING GEAR DOOR AFT HINGE. REPAIRED LEFT SKIN CRACK IAW DC-9 SRM 53-05.Mar 10, 2004 · N952AX · Doug DC941 · Fuselage Main, Plate/SkinSDR ABXA040106Support · crackedLEFT OUTBOARD SPOILER OUTBOARD SUPPORT TEE WAS CRACKED. REPLACED SUPPORT TEE IAW DC-9 SRM 51-30-2 AND 51-30-5.Mar 3, 2004 · N952AX · Doug DC941 · SpoilersSDR ABXA040102Bracket · corrodedLEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 446 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5.Mar 2, 2004 · N952AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA040100Bracket · corrodedLEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 541 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5.Mar 2, 2004 · N952AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA040101Bracket · corrodedLEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD CARGO AT FS 484 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5.Mar 2, 2004 · N952AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA040105Bracket · corrodedLEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 237 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED BRACKET IAW DC-9 SRM 51-30-5.Mar 2, 2004 · N952AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA040104Support · corrodedLEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 365 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED ATTACH BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-5.Mar 2, 2004 · N952AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA040103Support · corrodedLEVEL 2 CORROSION ON LOWER SIDE OF SEAT TRACK ATTACH BRACKET IN FORWARD LOWER CARGO AT FS 427 BETWEEN LONGERON 27 RIGHT AND 28 RIGHT. REPLACED ATTACH BRACKET IAW DC-9 SRM 51-30-1 AND 51-30-5.Mar 2, 2004 · N952AX · Doug DC941 · Fuselage Miscellaneous StructureSDR ABXA040099Spar · corrodedANGLE EXFOLIATED AND BULGED UPPER AFT FLANGE OF REAR SPAR UPPER TEE JUST OUTBOARD OF TRUNNION. REPLACED TEE ANGLE XRS 111.00 LEFT WING IAW DC-9 SRM.Mar 1, 2004 · N952AX · Doug DC941 · Wing SparSDR ABXA040098Fitting · corrodedAFT ACCESSORY LONGERON 11 RIGHT END FITTING EXFOLIATED JUST FORWARD OF CANTED FRAME. REPLACED LONGERON 11 RIGHT END FITTING IAW DC-9 SRM 51-30-5.Mar 1, 2004 · N952AX · Doug DC941 · Fuselage Main, Attach FittingsSDR ABXA030445Window · stiffCAPTAIN'S CLEARVIEW WINDOW WOULD NOT OPEN. MAINTENANCE OPS CHECKED WINDOW ON GROUND. OPS CHECKED GOOD IAW DC9 MM 56-10-03.Nov 18, 2003 · N952AX · Doug DC941 · Flight Compartment WindowsSDR ABXA030107Bracket · brokenSLAT DISAGREEMENT LIGHT ILLUMINATED UPON SLAT EXTENSION. FLIGHT CREW VERIFIED THROUGH FLIGHT CONTROLS THAT THERE WAS AN ASSYMETRY PROBLEM. FLIGHT CREW RETRACTED SLATS AND MADE A NO SLAT LANDING. FOUND AT ILN, #1 AND #2 SLAT PULLEY BRACKETS BROKEN, AND 3 EACH LMar 5, 2003 · N952AX · Doug DC941 · Leading Edge Slat Control SystemSDR ABXA030106Support · brokenSLAT DISAGREEMENT LIGHT ILLUMINATED UPON SLAT EXTENSION. FLIGHT CREW VERIFIED THROUGH FLIGHT CONTROLS THAT THERE WAS AN ASSYMETRY PROBLEM. FLIGHT CREW RETRACTED SLATS AND MADE A NO SLAT LANDING. FOUND AT ILN, NR 1 AND NR 2 SLAT PULLEY BRACKETS BROKEN AND 3 EACMar 5, 2003 · N952AX · Doug DC941 · Leading Edge Slat Control SystemSDR ABXA020307Controller · malfunctionedELEVATOR OSCILLATES VIOLENTLY WHEN AUTO PILOT WAS ENGAGED. COULD NOT DUPLICATE. REPLACED THE AUTO PILOT CONTROLLER IAW DC9 M.M. 22-10-00-5. AUTO PILOT SYSTEM OPS CHECK GOOD.Nov 8, 2002 · N952AX · Doug DC941 · Autopilot SystemSDR ABXA020173Spar · crackedUNREPAIRED CRACKS NOTED ON LEFT ELEVATOR FRONT SPAR .625 INCH LONG AT XE 174.5 AND .75 INCH AT XE 172.5. INSTALLED NEW ELEVATOR IAW DC-9 MM.Jul 24, 2002 · N952AX · Doug DC941 · Elevator, Spar/RibSDR ABXA020172Angle · crackedLOWER RIGHT PYLON ATTACH ANGLE WAS CRACKED AT STATION 1072. INSTALLED SECTION OF ATTACH ANGLE IAW DC-9 SRM 54-04.Jul 24, 2002 · N952AX · Doug DC941 · Fuselage Structure (General)SDR ABXA020171Bracket · corrodedSPOILER - ACTUATOR MIXER BRACKET WAS CORRODED AND PITTED IN NUMEROUS PLACES. REPLACED MIXER BRACKET IAW DC-9 MM.Jul 23, 2002 · N952AX · Doug DC941 · Drag Control ActuatorSDR ABXA020170Door · chafedLEFT MAIN LANDING GEAR OUTBOARD DOOR CHAFED ON INNER FORWARD LIP AND UNDER ARTICULATING DOOR COUNTER BALANCE ARM. REPLACED THE LEFT MAIN LANDING GEAR OUTBOARD DOOR AIW DC-9 MM.Jul 23, 2002 · N952AX · Doug DC941 · Landing Gear DoorsSDR ABXA010703Battery Pack · dischargedEMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED THE EMERGENCY EVACUATION LIGHTS BATTERY PACK IAW DC-9 MM 33-53-02.Feb 6, 2002 · N952AX · Doug DC941 · Emergency LightingSDR ABXA010657Battery · dischargedEMERGENCY LIGHTS FAILED TEST. REPLACED THE EMERGENCY LIGHT BATTERIES IAW DC-9 MM 33-53-02-4-001. OPS CHECKED GOOD IAW DC-9 MM 33-53-00.Dec 30, 2001 · N952AX · Doug DC941 · Emergency LightingSDR ABXA010656Fire Warning · malfunctionedLOOP-A LEFT ENGINE LIGHT ILLUMINATED DURING DESCENT. PERFORMED ABNORMAL CHECKLIST AND REMAINED ON LOOP-B. INSPECTED LOOP FOR DEFECTS, NONE FOUND. CHECKED CONTINUITY OF LOOP, ALL OK. CLEANED CONNECTOR FROM WATER/OIL SOAKAGE. OPS CHECKED GOOD IAW DC-9 AMM CDec 28, 2001 · N952AX · Doug DC941 · Fire DetectionSDR ABXA010464Window · openOUT OF 2500 FT AGL, THE CAPTAIN'S CLEAR VIEW WINDOW OPENED AND DUMPED PRESSURIZATION. CHECKED AND INSPECTED CAPTAIN'S CLEAR VIEW WINDOW PER DC9 AMM 56-10-03. PRESSURIZED AIRCRAFT TO 3 PSI. NO LEAKS NOTED. CHECKED CLEARANCES OF THE LOWER AFT HOOK AND FITTINSep 5, 2001 · N952AX · Doug DC941 · Flight Compartment Windows
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