N337AZ
Service difficulty reports · 67
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 = 'N337AZ' AND registry_match = 'registration' 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.
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 = 'N337AZ' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IXXA20261017102Window · fodFIRST OFFICER'S #2 WINDOW WILL NOT CLOSE. CLEANED DEBRIS FROM WINDOW TRACK. OPERATIONAL CHECK IAW B767 AMM 56-11-02 NOTED NO FAULTS. WINDOW LATCHED AND LOCKED.SDR IXX2026F00010Fitting · corrodedPICLE FORK CORR IN LEFT W/W AT INBD TOP AREA BY DRAIN CANISTERSDR IXXA20260929001Support Beam · corrodedBULK CARGO FLOOR SUPPORT BEAM STA 1417-1461 BL 0 HAS MULTIPLE LOCATIONS OF CORROSION. REFERENCE AMES WO N337AZ-44 NR 194024-0100-0142.SDR IXXA20260928001Skin · corrodedAREA FWD OF ALC, INTERNAL SKIN IS CORRODED BETWEEN STRINGERS 37L-38L APPROX STA 1087. REFERENCE AMES WO N337AZ-44 NR 194024-0100-0093.SDR IXXA20260927001Splice Plate · crackedNR 2 PYLON INBD AFT ATTACH ANGLE CRACKED. REMOVED & REPLACED NR 2 PYLON INBD AFT ATTACH ANGLE PER B767 SRM 51-40-02. REFERENCE AMES WO N337AZ-44 NR 194024-0400-0024.SDR IXXA20260822003Former · crackedLE NOSE FORMER AT LES 490 IS CRACKEDSDR IXXA20260822002Former · crackedLE NOSE FORMER AT #5 SLAT TAI DUCT IS CRACKEDSDR IXXA20260822001Attach Angle · crackedNR 2 PYLON OTBD AFT ATTACH ANGLE IS CRACKED.SDR IXXA2026081601Stiffener · crackedPANEL 447DB WEB STIFFENER IS CRACKEDSDR IXXA2026091601Skin Panel · delaminatedL/H UPPER SKIN PANEL OF L/H HORIZONTAL STABILIZER FROM STA 250-350 AT I/N END IS DELAMINATEDSDR IXXA202512107083Proximity Switch · inoperative"EMER DOOR" DESCRETE LIGHT COMES ON OCCASIONALY IN FLIGHT. NO EICAS MESSAGE DISPLAYED. PLACED ON DEFERRAL 68621 MINIMUM EQUIPMENT LIST ATI-52-71-01-01 CATEGORY C. DUE 18 DECEMBER 2025. SUPPLEMENTAL TO PREVIOUS REPORT IXXA20251207083 DATED 12/07/2025 AT KILN. ASDR IXXA2025120907083Light · false activationEMERGENCY DOOR DESCRETE LIGHT COMES ON OCCASIONALY IN FLIGHT. NO EICAS MESSAGE DISPLAYED. PLACED ON DEFERRAL 68621 MINIMUM EQUIPMENT LIST ATI-52-71-01-01 CATEGORY C.SDR IXXA2025101501Floor Support · corrodedCORROSION WAS FOUND ON A FORWARD CARGO BALLMAT FLOOR SUPPORT FITTING AT APPROXIMATELY STA 566 COMMON TO THE FITTING OF NUTPLATE STRAP. LOCATED, DRILLED AND INSTALLED NEW FORWARD CARGO SUPPORT IN ACCORDANCE WITH B767 SRM 51-40-02 AND B767 SRM 51-40-05.SDR IXXA2023081702Skin · crackedCRACK INDICATION NOTED DURING THE ACCOMPLISHMENT OF EO# ATI-07-767-6236, WINGLET STRINGER MODIFICATION OF L 9.5 OUTBOARD SEGMENT.SDR IXXA2023081701Skin · crackedCRACK INDICATION NOTED IN THE RIGHT WING SKIN COMMON TO THE INBOARD MOST HOLE AT WINGLET STRINGER L6.5 MODIFICATIONSDR IXXA2024081609Stringer · crackedCRACK FOUND RUNNING FROM THE 11 TO 5 O'CLOCK POSITION COMMON TO STRINGER L-6.5 BETWEEN WSTA 990.20 AND WSTA 1018.20 INBOARD AFT FASTENER AS MARKED.SDR IXXA2024081608Bulkhead · crackedSTA 1809.5 BULKHEAD RH FWD OUTER CHORD LOWER FWD FASTENER HAS CRACK EXTENDING FROM THE 3 O'CLOCK POSITION TO THE END OF THE PART AND UNDER ADJACENT STRUCTURE.SDR IXXA2024081607Skin · dentedAFT FUSELAGE, LOWER SKIN IS DENTED AT APPROX STA1790 BETWEEN STRINGERS 38R & 39RSDR IXXA2024081606Doubler · corrodedEXISTING REPAIR DOUBLER ON UPPER SURFACE OF HORIZONTAL STAB CENTER SECTION IS CORRODED. INSIDE TAIL COMPARTMENT AT APPROX STA1735 ON RH SIDE.SDR IXXA2024081605Seal · gougedCOCKPIT - #2 SLIDING WINDOW OPENING, LOWER FWD SEAL RETAINER TAB IS GOUGEDSDR IXXA2024081604Stabilizer · wornHORIZONTAL STAB FAIRING, 313BLX, HAS WEAR ON INNER SIDE.SDR IXXA2024081200001Fan Cowl · wornWEAR BEYOND LIMITS. LOWER FWD INNER EDGE WORN THROUGH EDGE PROTECTOR AND 1 PLY OF CARBON FIBER THAT MEASURED 16.75 INCHES X 1.2 INCHES.SDR IXXA20240807001Skin · delaminatedRIGHT WING, OUTBOARD FLAP, OUTBOARD LEADING EDGE SECTION IS DELAMINATED. POSSIBLE CAUSE UNDETERMINEDSDR IXXA20240816003Seal Depressor · crackedMCD CUTOUT FWD LOWER SEAL DEPRESSOR ATTACH FITTING IS CRACKEDSDR IXXA20240816002Retainer · gougedCOCKPIT CAPTAIN L2 WINDOW OPENING LOWER SEAL RETAINER STRUCTURE TAB IS GOUGEDSDR IXXA20240816001Sidewall Panel · damagedMAIN CABIN SIDEWALL #L4 IS DAMAGED. REFER TO HAECO WO 320007 NON ROUTINE 38783SDR IXXA20240816010Rib · crackedRIGHT WINGLET AFT ATTACH FRAME IS CRACKED INTERNAL JUST AFT OF UPPER AFT MOUNT BOLT. REF HAECO WO 320007 NON ROUTINE 38717SDR IXXA202408010004Retainer · gouged#2 ENG RH TR SEAL RETAINER FOUND GOUGED, CAUSE UNDETERMINED. ACCOMPLISHED BLENDOUT REPAIR MEASURING 0.750"W X 1.75"L X 0.018" DEEPSDR IXXA202408010003Mount Fitting · gouged#2 ENG RH TR FWD DEFLECTION LIMITER GOUGED, CAUSE UNDETERMINEDBLEAND OUT MEASURES 1.6"L X 0.096" DEPTHSDR IXXA202408010002Mount Fitting · gouged#1 ENGINE O/B T/R LOWER FWD DEFLECTION LIMITER FITTING WAS FOUND GOUGEDSDR IXXA2024080403Beam · chafed#1 PYLON AFT FAIRING ASSY, INBD LATCH BEAM CHAFED EDGE DAMAGE DUE TO CONTACT WITH BROKEN HOLD OPEN RODSDR IXXA2024080601Rib · gougedLEADING EDGE RIB AT OSS 494 ON LEFT WING IS GOUGED ON INBOARD SIDE, BLENDED OUT AREA MEASURE 2" X 1"SDR IXXA2024080404Keel · corrodedCORROSION FOUND ON RBL 9.50 KEEL CHORD UPPER SURFDACE , APPROXIMATELY AT BS 786SDR IXXA2024080402Longeron · chafed#1 PYLON PANEL 431AT INNER FWD STRUCTURAL CHANNELS (PN 313T2100-86 AND 313T2100-82) ARE CHAFED ON THE FWD ENDSSDR IXXA2024080401Fairing · damagedR/H STAB FAIRING #314CRX FOUND TO HAVE 2EA PUNCTURES IN INNER SKINSDR IXXA20240801001Support Beam · chafedR/H AFT MLG SUPPORT BEAM FWD EDGE OF THE LOWER FREE FLANGE HAS CHAFING DAMAGE DUE TO CONTACT WITH LOWER BULB SEAL ATTACH ANGLE APPROX 30" OTBD OF THE INBD END OF BEAMSDR IXXA2024073102Skin · crackedCRACK FOUND IN FORWARD ENTRY DOOR AFT LOWER CORNER FUSELAGE SKIN EXTENDING FROM FASTENER IN 10 O'CLOCK POSITIONSDR IXXA202407310001Skin · crackedCRACK FOUND IN SKIN OF FORWARD SERVICE DOOR AFT LOWER CORNER EXTENDING OUT FROM FASTENER IN 2 O'CLOCK AND 8 O'CLOCK POSITIONSDR IXXA2024080303Panel · erodedL.WING L/E PANEL 511CB ERRODED ON THE ERROSION STRIP EDGESDR IXXA2024080300003Panel · crackedL.WING L/E PANEL 511BB CRACKED AT FASTENER HOLE ON AFT SURFACE AND DELAMINATION ON FWD EDGESDR IXXA20231013069Unknown · unknownLINE MAINTENANCE REPORTED, DESCENT DEVICE HARNESS BAG TORN. REMOVED AND REPLACED EMERGENCY EQUIPMENT BAG. NO ADDITIONAL FAULTS NOTED.SDR IXXA20230919064Unknown · unknownON CLIMB AT 7,000 FT CREW REPORTED FLIGHT CONTROL MALFUNCTION. IN BOTH AUTOPILOT AND MANUAL MODE FLIGHT CONTROLS UNRESPONSIVE. CREW DIVERTED TO KRIV WITH AN EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL AND NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL THESDR IXXA20230919063Unknown · unknownON CLIMB AT 7,000 FT CREW REPORTED FLIGHT CONTROL MALFUNCTION. IN BOTH AUTOPILOT AND MANUAL MODE FLIGHT CONTROLS UNRESPONSIVE. CREW DIVERTED TO KRIV WITH AN EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL AND NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL THESDR IXXA202309011056Unknown · unknownON CLIMB AT 7,000 FT CREW REPORTED FLIGHT CONTROL MALFUNCTION. IN BOTH AUTOPILOT AND MANUAL MODE FLIGHT CONTROLS UNRESPONSIVE. CREW DIVERTED TO KRIV WITH AN EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL AND NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL, THSDR IXXA20230703040Unknown · unknownPOST FLIGHT, LINE MAINTENANCE IDENTIFIED FLIGHT DECK LIGHT OVERHEAD LIGHT WILL NOT ILLUMINATE ON EMERGENCY LIGHT TEST. ALTERNATIVELY, LIGHT WILL ILLUMINATE ON OVERRIDE FUNCTION. IAW B767 AMM 33-51-03, REMOVED AND REPLACED EMERGENCY LIGHT OVERHEAD LIGHT. OPERATSDR IXXA20221123148Unknown · smokeDURING GROUND LOADING, CREW REPORTED SMOKE IN FLIGHT DECK. WORK IN PROGRESS.SDR IXXA2022092110None · wornRW SHEAR TUBE WORNSDR IXXA2022092109Torque Tube · wornRW MAIN TORQUE TUBE WORNSDR IXXA2022092108None · wornRW FLAP SPLINE BUSHING WORNSDR IXXA2022092107None · wornRW FLAP COLLAR FITTING WORN
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