N967AT
Service difficulty reports · 204
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 = 'N967AT' 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 = 'N967AT' 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 DALA2019082644954Slide · no testTHE R1 DOOR SLIDE FAILED THE DEPLOYMENT TEST PER AMDS CARD #2561-9002 FORECAST #95-0525-8-0121. MAINTENANCE REMOVED AND INSTALLED A NEW SERVICEABLE R1 DOOR SLIDE REF AMDS CARD #2561-9005. ICR HAS BEEN SUBMITTED USING DOC/WORKCARD #2560-9352 -95 (QC5126/376046)SDR DALA2019062703887Battery Pack · inoperativeTHE EXIT SIGN ABOVE THE AFT BULKHEAD DOOR IS INOPERATIVE (EMERGENCY LIGHT). MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY IAW B717 AMM 33-57-03. OPERATIONAL CHECK WAS GOOD. (LP #5759650)SDR DALA2018100205846Battery Pack · dischargedTHE FORWARD EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-235 REF AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #3914354)SDR DALA2018092005666Door Frame · corrodedCORROSION WAS FOUND ON THE FORWARD CARGO DOOR JAMB. REPLACED DOOR JAMB IN STEPS 1 THRU 5 REF SRM 53-20-15-2R PROC 6.SDR DALA2018091805643Mechanism · out of adjustTAILCONE RELEASE CAM MECHANISM IS CLOCKED WRONG. CHECKED CLOCKING AND ADJUSTED, REF BAC DWG 5961568 & AMM 53-52-03.SDR DALA2018082705270Lens · missingTHE FLIGHT ATTENDANT DISCOVERED THE OVERWING EXIT EMERGENCY SIGN COVER WAS MISSING. MAINTENANCE REPLACED THE LENS ASSEMBLY AND THE AIRCRAFT RETURNED TO SERVICE.SDR DALA2018052103460Power Supply · contaminatedTHE EMERGENCY EXIT LIGHTS WOULD NOT TURN OFF. MAINTENANCE FOUND THE POWER SUPPLY ABOVE THE AFT F/A SEAT TO BE SATURATED WITH WATER. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY IAW AMM 33-51. OPS CHECKED NORMAL.SDR DALA20180573103Battery Pack · malfunctionedUPPER AFT CABIN EXIT DOOR SIGN FLASHING WHEN IN ARM POSITION. MAINTENANCE REPLACED LIGHT POWER SUPPLY AND BATTERY ABOVE AFT DOOR CEILING PANEL IAW AMM 33-51. OPERATIONAL CHECK IS NOW NORMAL. AIRCRAFT OK FOR SERVICE.SDR DALA2018032601907Smoke Detector · false activationWHILE ON APPROACH FOR LANDING, THE FORWARD CARGO SMOKE INDICATION ILLUMINATED. THE QRH WAS COMPLIED WITH, DISCHARGED BOTH CARGO FIRE BOTTLES TO MAKE THE INDICATION EXTINGUISH. MAINTENANCE INSPECTED WIRE BUNDLES AND ALL COMPONENTS TESTED GOOD. THE CARGO SMOKE SDR DALA2017111308080Sign · detachedEMERGENCY EXIT SIGN COVER LOOSE. THE LIGHT WAS HANGING BY WIRES. SECURED THE EXIT SIGN.SDR DALA2017092507088Sign · looseCREW REPORTED THE CEILING EXIT SIGN AT ROW 1 WAS LOOSE. SECURED THE SIGN.SDR DALA2017082806424Light · intermittentAFT EMERGENCY EXIT SIGN FLICKERED. PERFORMED EMERGENCY EXIT LIGHT TEST IAW B717 AMM 33-51. NO FAULTS NOTED. OPERATION IS NORMAL.SDR DALA2017081106169Fire Warning · false activationTHE COCKPIT CREW RECEIVED A NR 1 ENGINE FIRE WARNING INDICATION WHILE IN CRUISE FLIGHT. IAW QRH, BOTH FIRE BOTTLES WERE DISCHARGED AND THE NR 1 ENGINE WAS SHUTDOWN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AT THE SCHEDULE DESTINATION. MAINTENANCE DID NOT SDR DALA2017070205123Unknown · malfunctionedAFT EXIT SIGN ILLUMINATED WHILE EMERG LIGHT SWITCH IN ARM POSITION. PERFORMED EMERGENCY LIGHTS TEST PER AMM 33-51. CYCLED EMERGENCY LIGHTS SWITCH SEVERAL TIMES. AFT EXIT SIGN DID NOT ILLUMINATE IN THE ARMED POSITION. SYSTEM CHECKS GOOD. A/C OK FOR SVC.SDR DALA2017040302708Lens · missingEMERGENCY LIGHT LENS MISSING, IN THE OVERHEAD ABOVE ROW 1. REPLACED THE LENS, CHECKED GOOD.SDR DALA2016102407497Skin · crackedCRACKED FUSELAGE SKIN Y=1076 LONG 14 RT. REPAIR WAS ACCOMPLISHED PER ETI-17-16-123 REV 1 & ER/A 550326-14 REV ORIGINAL. LEAK TEST OF AIR CONDITION PNEUMATIC DUCT WAS ACCOMPLISHED PER AMM 21-00-00 790-801 AND NO LEAKS WERE FOUND. ACCOMPLISH SECTION II REPETISDR DALA2016102307458Skin · damagedDISTRESS AT VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE. BHEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND IAW DWG SG 95550001 REV.B, BUSHINGS WERE FABRICATED AND INSTALLED IAW DPS 4.710-3 AND DWG SG95550001 REV. B.SDR DALA2016102307456Skin · crackedCRACKED SLAT PANEL NR 2 INBD FACE XOS 238 RT WING. THE SLAT PANEL WAS REMOVED IAW AMM 27-80-01 000-806, HFEC INSPECTION WAS ACCOMPLISHED AND ONE CRACK WAS FOUND IAW NDT SPM 06-10-01. THE SLAT PANEL WAS REPAIRED IAW SRM 57-00-00 FIG. 201 AND INSTALLED IAW AMMSDR DALA2016102107422Door Frame · crackedCRACK ON DOOR JAMB STA Y=954 AT AFT CARGO COMPARTMENT C2 (SM) (S/N 00135). DOOR JAMB WAS REPLACE PER SRM 51-41-02 AND 51-41-05. PERFORM DECAL VISUAL INSPECTION EVERY C CHECK PER TOPP 30-10-70 PAR I PG 14.SDR DALA2016102107421Longeron · crackedCRACKED LONGERON 2R ON STA 1133 AT AFT ACCESSORIES AREA. LONGERON SECTION WAS REPLACED PER SRM 51-41-05, 51-40-08, 51-10-04 PAR 15 AND 21, AND SRM 51-41-01.SDR DALA2016102107420Pan · crackedCRACK ON LOWER FWD CORNER AT AFT CARGO COMPARTMENT DOOR PAN. REPAIR WAS ACCOMPLISHED PER ER/A 550336-14 REV ORIGINAL AND ETI-17-16-127 REV 3.SDR DALA2016102007385Frame · crackedCRACKED FRAME ANGLE ON BULKHEAD PYLON SUPPORT AT BS 1022 LONGERON 7L. REPAIRED IAW ETI-17-16-130 REV. ORIGINAL AND ER/A 550341-14 REV. ORIGINAL.SDR DALA2016101907359Cusp Web · corrodedCORROSION ON THE RT CUSP WEB BS 550. DAMAGED AREA WAS TRIMMED OUT IAW SRM 53-00-55. HFEC INSPECTION WAS ACCOMPLISHED AFTER TRIM OUT AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01. REPAIRED IAW SRM 53-00-55 FIG. 215, 51-10-4 PAR 15, 21, 51-41-02, AND 51-10-04 SDR DALA2017010500102Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB ON STA Y=550 IN REF CARD 00393. CRACK WAS FOUND WITH NEXT DIMENSION L=.320" DAMAGED AREA WAS TRIMMED OUT PER SRM 53-00-55. HFEC INSPECTION WAS ACCOMPLISHED ON RT CUSP WEB ON STA Y=550 AFTER TRIM OUT AND NO CRACKS WERE FOUND PSDR DALA2016101807332Longeron · corrodedCORROSION OUT OF LIMITS ON LONGERON 30 BTW STA Y= 974 TO 1005 AT AFT CARGO COMPARTMENT. LONGERON 30 BTW STA Y=974 TO Y=1005 WAS REPAIRED PER SRM 53-00-05 FIG 201 REPAIR 3.SDR DALA2016101807331Access Panel · corrodedEXCESSIVE CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 620CB AND 620AT AT RT WING. PLATES 620AT AND 620CB WERE REWORKED AND WERE FOUND OUT LIMITS, THEREFORE FUEL ACCESS PLATES WERE REPLACED AND THE APPLICABILITY WAS VERIFIED PER IPC 57-22-01-01 AND 57-23-01-SDR DALA2016101807330Door Frame · crackedCRACKED RT NLG DOOR JAMB. (00434) LENGTH ORIGINAL CRACK LONG 1.300" AND WIDTH 0.750". DAMAGED AREA WAS REMOVED, CUT WAS CHECKED PER HFEC INSP, AND NO CRACKS FOUND. AREA WAS REPAIRED PER SRM 53-10-14 FIG 201 REPAIR 2.SDR DALA2016101807329Door Frame · crackedCRACKED LT NLG DOOR JAMB (00435). LENGTH ORIGINAL CRACK LONG 1.125" AND WIDTH 0.750", DAMAGED AREA WAS REMOVED, CUT WAS CHECKED PER HFEC INSP, AND NO CRACKS FOUND. AREA WAS REPAIRED PER SRM 53-10-14 FIG 201 REPAIR 2.SDR DALA2016101807328Cusp Web · crackedEXCESSIVE CORROSION ON RT CUSP WEB ON STA Y=550 IN REF CARD 00393. CRACK WAS FOUND WITH NEXT DIMENSION L=.320" DAMAGED AREA WAS TRIMMED OUT PER SRM 53-00-55. HFEC INSPECTION WAS ACCOMPLISHED ON RT CUSP WEB ON STA Y=550 AFTER TRIM OUT AND NO CRACKS WERE FOUNDSDR DALA2016101607262Cusp Web · crackedCRACK ON CUSP WEB BS 663 BTW LBL 54 TO 60. HFEC WAS ACCOMPLISHED AND A CRACK WAS CONFIRMED OF 1.900" LENGTH IAW NDT SPM 06-10-01 .001: THE CRACK WAS STOPPED DRILL IAW SRM 51-00-07 PAR 5. HFEC WAS ACCOMPLISHED IAW NDT SPM 06-10-01 .001 AND NO CRACKS WERE FOUNDSDR DALA2016101607261Frame · crackedCRACKED FRAME 907 BETWEEN LONGERONS 26-28R, REPAIRED IAW SRM 51-41-02 AND 51-41-05.SDR DALA2016101607260Channel · crackedCRACKED RT MLG DOOR FRAME CHANNEL AT BS 757. THE CHANNEL WAS REPLACED IAW SRM 51-41-02 AND 51-41-05.SDR DALA2016101407266Cusp Web · crackedCRACK FOUND ON THE RT CUSP WEB BS 365 X45. HFEC INSPECTION WAS ACCOMPLISHED ON THE CUSP WEB AND A CRACK WAS CONFIRMED IAW NDT SPM 06-10-01 .001. THE DAMAGE WAS REMOVED PER B-717 SRM 55-00-55 REPAIR 4 AND ANOTHER HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKSDR DALA2016101407230Angle · crackedCRACK ON BULKHEAD ANGLE BS 1022 BETWEEN LONGERONS 13-14R. A NEW ANGLE WAS MANUFACTURED IAW DRAWING 9912243-198 AND SRM 51-20-09, TREATED AND PAINTED IAW SRM 51-10-04 PAR 21 AND 15, AND INSTALLED IAW SRM 51-41-02 AND 51-41-05.SDR DALA2016101407229Angle · crackedCRACK ON BULKHEAD ANGLE BS 1022 BETWEEN LONGERONS 16-17L. A NEW FRAME ANGLE WAS MANUFACTURED IAW DRAWING 9912243-189 AND SRM 51-20-09. TREATED AND PAINTED IAW SRM 51-10-04 PAR 15 AND 21, AND INSTALLED IAW SRM 51-41-05.SDR DALA2016101307188Longeron Splice · corrodedCORROSION ON LONGERON SPLICE 18R, BS 898. THE SPLICE WAS REMOVED IAW SRM 51-41-05. SPLICE WAS FABRICATED IAW SRM 53-20-01 FIG 1 AND 51-20-09. THE SPLICE AND AREA WAS TREATED AND PAINTED IAW SRM 51-10-04 PAR. 15/21. THE SPLICE WAS INSTALLED IAW SRM 51-41-0SDR DALA2016101307187Pan · crackedCRACK ON PAN BS 427 BETWEEN BEAM 1 AND BEAM 2 AT FWD CARGO DOOR. HFEC INSPECTION WAS ACCOMPLISHED AND CRACKS WERE FOUND IAW NDT SPM 06-10-01 .001. CRACKS ON PAN WERE STOP DRILLED IAW SRM 52-30-02 FIG 201, HFEC WAS ACCOMPLISHED ON PAN AND NO CRACKS WERE FOUNSDR DALA2016101307186Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB BS 455. DAMAGE WAS REMOVED, A REPAIR WAS MANUFACTURED, AND INSTALLED IAW SRM 53-00-55 REPAIR 4. HFEC WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001 AND NO CRACKS WERE FOUND AFTER CUT OUT.SDR DALA2016101307185Support · crackedCRACKED SUPPORT UNDER SEAT TRACK X 44.5 ON BS 715. THE SUPPORT WAS REPLACED IAW DWG 9923417 REV. B AND SRM 51-41-05.SDR DALA2016101307184Access Panel · corrodedEXCESIVE CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 520CB LT WING. THE ACCESS PANEL WAS DETERMINED TO BE OUT OF LIMITS AND WAS REPLACED IAW SRM 57-10-01 PAR. 5.SDR DALA2016101207172Access Panel · damagedELONGATED HOLES ON FUEL ACCESS PANEL 141AR ON THE RT WING. THE ACCESS PANEL WAS REWORKED IAW SRM 57-10-01 CONDITION II AND FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 57-10-01.SDR DALA2016101207171Seat Track · crackedCRACKED SUPPORT UNDER SEAT TRACK X -44.5 AT BS 715. THE SUPPORT WAS REMOVED IAW SRM 51-41-05 AND 51-41-02. A NEW SUPPORT WAS DRILLED IAW DWG 9923417 REV. B AND SRM 51-40-08. TREATED AND PAINTED IAW SRM 51-10-04 PAR. 21 AND 15. AND INSTALLED IAW DWG 9923417SDR DALA2016101207170Cusp Web · corrodedPUNCTURE ON LT CUSP WEB BS 294 BETWEEN X 44 TO 54. DAMAGE WAS REMOVED, HFEC INSPECTION ACCOMPLISHED, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01 .001. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-55 AND SRM 51-41-02.SDR DALA2016101207169Cusp Web · corrodedEXCESSIVE CORROSION ON LT CUSP WEB BS 856. DAMAGE WAS REMOVED, DOUBLER FABRICATED, AND INSTALLED IAW SRM 53-00-55 AND 51-41-02, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001.SDR DALA2016101207168Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB ON BS 513. DAMAGE ON AREA WAS TRIMMED OUT IAW SRM 53-00-55. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIR FABRICATED IAW SRM 53-00-55 REPAIR 4 FIG. 215 AND INSTALLED IAW SRM 51-4SDR DALA2016101107154Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB ON BS 489 IAW CARD 00393. DAMAGE WAS REMOVED IAW SRM 53-00-55 FIG. 215. HFEC INSPECTION WAS ACCOMPLISHED AFTER TRIM OUT AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIR FABRICATED IAW SRM 53-00-55. REPAIR INSTALLEDSDR DALA2016101107153Cusp Web · crackedCRACK ON RT CUSP WEB BS 218 X=45 AT CABIN PAX RH. CRACK WAS STOP DRILL IAW SRM 53-00-55 REPAIR 4, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001, NO CRACKS WERE FOUND AFTER STOP DRILL. REPAIR DOUBLER WAS FABRICATED IAW SRM 53-00-55. AREA DRILLED WSDR DALA2016101007119Access Panel · damagedELONGATED HOLES ON FUEL ACCESS PANEL 141AL ON THE LT WING. THE FUEL ACCESS PANEL WAS REPAIRED SRM 57-10-01 CONDITION II.SDR DALA2016101007118Frame · crackedCRACKED FRAME ANGEL BS 1116 BETWEEN LONGERONS 15 -16 BOTH SIDES. THE ANGLS WERE REPLACED IAW SRM 51-41-05.SDR DALA2016110208155Floorbeam · corrodedSEVERAL CORROSION POINTS ON FLOORBEAM BS 200 FROM X-13 TO X-44 . CORROSION WAS REMOVED IAW SRM 51-10-04 PAR 26, THE FLOORBEAM WAS REPAIRED IAW SRM 51-41-02. AND 51-41-05.
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