N955AT
Service difficulty reports · 197
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 = 'N955AT' 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 = 'N955AT' 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 DALA2022032201861Not Reported · not reportedCRACKS (3 EA) ON INTERNAL DOUBLER, RH FRONT SPAR LOWER SIDE (IN REF SETTLEMENT AREA OF REFUEL ACCESS PANEL LATCHES). SUMMARY OF NRC 00079: INTERNAL DOUBLER, RH FRONT SPAR LOWER SIDE WAS REPAIRED PER ERA 598025-14 REV. ORIGINAL, PRI REV. 0 AND SRM 57- 40-01 REPSDR DALA2022032101830Not Reported · not reportedDENT ON CENTER FIXED FLAP VANE LOWER SKIN BTW XV2 283 TO XV2 279 (LH WING). SUMMARY OF NRC 00088: CENTER FIXED FLAP VANE LOWER SKIN BTW XV2 283 TO XV2 279 (LH WING) WAS REMOVED PER B717 AMM: 27-50-02-000- 802. DAMAGE AREA WAS REPAIR PER B717 S.R.M. 51-70-02-0GSDR DALA2022032101829Not Reported · not reportedCRACK ON EXTERNAL FUSELAGE SKIN STA Y=1040 LONG 14RH. SUMMARY OF NRC 00049: FUSELAGE SKIN STA Y=1040 LONG 14RH WAS REPAIRED PER ERA 597705-14 REV. ORIGINAL SECTION 1. PERMANENT REPAIR AND PRI REV. 0,1,2,3 AND 4. REPETITIVE INSPECTIONS WILL BE MONITORING UNDER SDR DALA2022032502002Skin · crackedREFERENCE ER/A 597705-14 FUSELAGE / SKIN / Y=1037, L-13R TO L- 14R / CRACKS, RESULTING IN A BOEING APPROVED RE-ENFORCING REPAIR . ACCOMPLISH SECTION II: REPETITIVE GENERAL VISUAL INSPECTION EVERY 24 MONTHS AFTER ACCOMPLISHMENT OF SECTION I: PERMANENT ASSOCIATESDR DALA2022031801805None · noneLIGHTNING STRIKE ON UPPER AREA OF OUTBD ELEVATOR TAB AT LH HORIZONTAL STABILIZER. SUMMARY OF NRC 00083: LH GEARED TAB WAS REMOVED AND SAME WAS INSTALLED PER B717 AMM 27-31-05. ALSO WAS REPAIRED PER B717 SRM 51-70-09-2R-5 AND SRM 51-70-09-0G. (LP #2160054)SDR DALA2022031701760None · noneCRACK ON ANGLE STA Y=1167 BTW LONG 2R AND 3R AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00152: ANGLE STA Y=1167 BTW LONG 2R AND 3R AT AFT ACCESSORY COMPARTMENT WAS REPLACED PER B717 PER ER/A 597825-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI REV 0 ANDSDR DALA2022032502001Frame · crackedER/A 597825-14, FUSELAGE / MAIN FRAME / CLIP AND ANGLE, STA. 1166, L1-L3R / CRACK AND TRAPPED FASTENER. SUBJECT REPAIR REQUIRES FOLLOW-ON REPETITIVE INSPECTIONS. ACCOMPLISH ER/A 597825-14, SECTION II INSPECTION WITHIN 3000 FLIGHT CYCLES AFTER SECTION I ACCOMPLSDR DALA2022031601717None · noneCORROSION ON ANGLE ON STA 1053 BTW LONG 28LH AND 28RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00261: ANGLE ON STA 1053 BTW LONG 28LH AND 28RH WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G AND DWG 9915561 REV. CG. (LP #2155703)SDR DALA2022031601716None · noneCORROSION ON INTERCOSTAL BTW 1022-1037 AND S30 C2. SUMMARY: INTERCOSTAL WAS REPLACED PER B-717 SRM 51-41-02-0G AND 51-41-05-0G PAR. 8. (LP #2155420)SDR DALA2022031401648None · noneCORROSION ON CHANNEL BTW STA 908 TO STA 927 AT AFT CARGO COMPARTMENT IN REF NRC 00187. SUMMARY OF NRC 00258: CORROSION LEVEL 2, CHANNEL BTW STA 908 TO STA 927 WAS REPLACED CHANNEL PER B717 SRM 51-40-08-0G PAR 3. (LP #2154412)SDR DALA2022031401647None · noneCORROSION ON LONGERON SPLICE 30 BTW STA Y=889-908 AT AFT CARGO COMPARTMENT. SUMMARY 00238: CORROSION LEVEL 2, LONGERON SPLICE 30 BTW STA Y=889-908 AT AFT CARGO COMPARTMENT WAS REPLACED PER B-717 SRM 51- 41-05-0G AND 51-41-01-0G. (LP #2154356)SDR DALA2022031401644None · noneCORROSION ON SPLICE DOUBLER OF AFT DOOR JAMB AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00026: CORROSION LEVEL 2, SPLICE DOUBLER OF AFT DOOR JAMB AT FWD CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53- 20-15-2R-6. (LP #2151681)SDR DALA2022031001551None · noneCORROSION ON LONGERON CHANNEL 29LH AND STA 957 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00190: CORROSION LEVEL 2, CHANNEL REPAIR WAS REPLACED PER B-717 SRM 53-00-05-2R. AND SRM 51-41-05-0G. (LP #2151046)SDR DALA2022031001555None · noneCORROSION ON PRODUCTION DOUBLER ATTACHED ON FWD FACE OF AFT PRESSURE BULKHEAD, BTW LONG 29LH TO 29RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00262: CORROSION LEVEL 2, PRODUCTION DOUBLER WAS REPLACED PER B717 SRM 51-41-05-0G AND DRAWING 5910130 ITEM 61 REV. ETSDR DALA2022030901527None · noneCORROSION ON FWD PREVIOUS REPAIR DOUBLER AT FWD CARGO COMPARTMENT DOOR JAMB AREA. SUMMARY OF NRC 00192: CORROSION LEVEL 2, REPAIR DOUBLERS WERE REPLACED PER B717 SRM 53-20-15-2R-6 FIG. 201. (LP #2148640)SDR DALA2022030901525None · noneCORROSION ON SPLICE DOUBLER OF FWD DOOR JAMB AT AFT CARGO COMPATMENT. SUMMARY OF NRC 00028: CORROSION LEVEL 2, DOUBLERS REPAIR WAS REPLACED PER B-717 SRM 53-20-15-2R-7 REPAIR.7. (LP #2149003)SDR DALA2022030801496None · noneCRACK ON LONGERON 2RH STA Y=1133 AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00151: LONGERON 2RH STA Y=1133 AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #2147774)SDR DALA2022022301183None · noneSHIP 9514 - THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT TO A NORMAL SAFE LANDING BACK AT ATL. THIS WAS DUE TO AN "APU FIRE" INDICATION AT 26,000 FEET DURING CLIMB OUT. THE APU HAD BEEN OFF FOR MORE THAN 15 MINUTES BY THEN. THE CAPT RAN THE QRH APUSDR DALA2021112907292None · noneTHE TAIL COMPARTMENT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS PER B717 AMM 33-51-14. OPERATIONAL CHECK WAS GOOD. (LP #8347215)SDR DALA2021042202348Sensor · malfunctionedSHIP 9514 - THE FLIGHT CREW DECLARED AN EMERGENCY WHILE ON APPROACH DUE TO THE "PSEU FAIL" ILLUMINATING. THE CREW COMPLIED WITH QRH AND RESET THE GROUND PROXIMITY CIRCUIT BREAKER. IT WAS AN UNEVENTFUL LANDING AT NORMAL SPEED, BUT THEN THE "AGS FAIL", "SPOILER SDR DALA2020030601669Panel · missingDURING W/A NOTICED 2 CIRCULAR INSPECTION DISKS MISSING FROM RIGHT LOWER ELEVATOR SURFACE. LOG-PAGE UPDATED @ 04MAR20 2344 UTC 02 CORR BY ATL 04MAR20 ATA 5523 RII: N ENTR W INSTALLED INSP. PNLS. (LP #5106954)SDR DALA2019060603430Light · damagedEMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: 604. MAINTENACE REINSTALLED THE CABIN SIDEWALL LIGHT LENS, (LT SIDE).SDR DALA2018121107129Battery Pack · inoperativeTHE L1 DOOR AND COCKPIT EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY FOR THE L1 DOOR AND COCKPIT EMERGENCY LIGHTS PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #4250450)SDR DALA2018111606643Battery Pack · inoperativeTHE OVERHEAD EMERGENCY EXIT SIGN FOR THE OVERWING EXITS WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-120 AND THE POWER SUPPLY REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4616688)SDR DALA2018032701946Battery Pack · inoperativeDURING AN EMERGENCY LIGHT TEST, THE R1 LIGHT DID NOT WORK. THE BATTERY PACK WAS REPLACED. A TEST WAS PERFORMED. TESTED OK IAW AMM 33-51-00 710-801.SDR DALA2018032101819Fire Bottle · unserviceableOUT OF LIMITS WEIGHT ON AFT/RT LAVATORY FIRE EXTINGUISHER CONTAINER. EXTINGUISHER ASSY WAS REMOVED AND A SERVICEABLE EXTINGUISHER ASSY WAS INSTALLED PER AMM 26-25-01.SDR DALA2018031801818Skin · wornWORN RT WING SLAT PANEL NR 1 LOWER SKIN STA XFS=145. WEAR ON RT WING SLAT WAS REPAIRED, AS A PERMANENT REPAIR PER ER/A 566779-14 REV ORIGINAL AND ETI-17-18-038 REV 3.SDR DALA2018031701757Vane · damagedDENTED AREA WAS FOUND DISBONDED. RT INBOARD FIXED FLAP VANE, LOWER SURFACE, DISBONDED AREA WAS REPAIRED IAW SRM 57-53-01-2R-1.SDR DALA2018031701754Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN BS 1133 BETWEEN STRINGERS 2L AND 3L. THE SKIN WAS REPAIRED IAW ER/A 566630-14AD, REV ORIG, AND ETI-17-18-029, REV 2.SDR DALA2018031701753Frame · crackedCRACKED FRAME BS 1037 BETWEEN LONGERONS 14L. THE FRAME WAS REPAIRED IAW ER/A 566736-14, REV ORIG.SDR DALA2018031701752Frame · crackedCRACKED FRAME, BS 1037, LONGERON 13R. THE FRAME WAS REPAIRED IAW ER/A 566676-14, REV ORIG, AND ETI-17-18-034, REV 1.SDR DALA2018031701751Frame Angle · crackedCRACKED FRAME ANGLE ON THE LT AFT LAVATORY AREA BS 1052, BETWEEN LONGERONS 18L AND 19L. THE FRAME ANGLE WAS REPLACED IAW DWG 9915561, REV CG, SRM 51-41-05-0G, AND 51-41-02-0G.SDR DALA2018031601848Skin · damagedDUE TO WEAR FOUND ON THE RT WING SLAT PANEL NR 1, LOWER SKIN, XFS 145, REMOVED AND REPLACED THE SLAT PANEL IAW AMM 27-80-01 AND ADJUSTED IAW AMM 27-80-01-830-802. RT WING NR 1 SLAT WAS REPAIRED IAW ER/A 566779-14, REV. ORIGINAL.SDR DALA2018031601736Cargo Track · corrodedCORROSION ON THE LT & RT CARGO TRACK BS 889 TO 1022. THE CARGO TRACKS WERE REPLACED IAW SRM 51-41-01-0G, AND 51-41-05-0G.SDR DALA2018031501733Frame · corrodedCORROSION ON FRAME, BS 954, BETWEEN LONGERONS 25 AND 28. THE FRAME WAS REPAIRED IAW SRM 51-41-05-0G, AND 53-20-07-2R-3-.SDR DALA2018031501711Skin · crackedAD 2016-09-05, AA 5530-01048: CRACKS ON REMOVABLE LEADING EDGE SKIN, STA ZFS=53 AT VERTICAL STABILIZER. REMOVABLE LEADING EDGE SKIN, STA ZFS=53 WAS REPAIRED PER SRM 55-30-01-2R-8.SDR DALA2018031501710Door Frame · corrodedCORROSION ON L1 DOOR JAMB WEB BTW STA Y=200-207 BTW LONG 17L TO 18L AT CPAX. CORROSION LEVEL 2, L1 DOOR JAMB WEB BTW STA Y=200-207 BTW LONG 17L TO 18L AT CPAX WAS REPAIRED PER ER/A 566681-14 REV ORIGINAL AND ETI-17-18-035 REV 1.SDR DALA2022030901528None · noneFAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY C-CHECK OR 24 MONTHS WHICHEVER OCCURS FIRST PER ERA 566676-14. DISPLACED LAV TO GAIN ACCESS TO INSPECTION AREA. PERFORMED VISUAL REPETITIVE INSPESDR DALA2018031401686Frame Angle · corrodedCORROSION ON THE FRAME ANGLE, BS 908, BETWEEN LONGERONS 29 AND 30R, THE FRAME ANGLE WAS REPAIRED IAW SRM 53-00-06-2R-2, REPAIR 2, 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018031401685Stiffener · crackedCRACKED VERTICAL STIFFENER BS 813 TO 816, BL 0, FWD BULKHEAD AFT FACE. THE STIFFENER WAS REPAIRED IAW SRM 53-00-00-2R, FIG-201, SHEET 1.SDR DALA2018031301628Access Panel · crackedCRACKED RT WING LOWER ACCESS PANEL AT THE TRAILING EDGE AREA XRS 150. THE ACCESS PANEL WAS REPAIRED SRM 57-50-01-2R, 51-41-01 0G, AND 51-41-05-0G.SDR DALA2018031301627Cap · crackedCRACKED CAP BS 1022, LONGERON 7R AND 7L. THE CAP WAS REPAIRED IAW ETI 17-18-026, REV 1, AND ER/A 566634-14, REV ORIGINAL.SDR DALA2018031101608Floor Panel · delaminatedDELAMINATION ON FLOOR PANELS #211ANF, 221WF, 222GF, 222TF, 222AAF, 222AMF, 222AEF, 222AHF, 222AVF, 222ATF, AND 222DF AT PAX CABIN. NRC 00508: FLOOR PANELS #222AAF, 221WF, 222GF, 211ANF, 222AHF, 222AEF, 222AVF, AND 222ATF WERE FABRICATED, REPLACED, AND IDENTIFISDR DALA2018031101605Floor Panel · crackedCRACKS ON FLOOR PANELS #221CF, 221BF, 222ARF, 222AMF, 223JF, AND FLOOR PANEL P/N SP95530011-3 AT PAX CAB (CPAX). NRC 00506: FLOOR PANELS #221CF, 221BF, 22AMF, 223JF, AND SP95530011-3 WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50-2R FLOOR PANSDR DALA2018031101604Pan · crackedCRACKS ON THE LT FWD OVERWING EMERGENCY EXIT DOOR FRAME PAN UPPER AREA. THE PAN WAS REPIARED IAW SRM 53-20-15-2R-8.SDR DALA2022030901529None · nonePERMANENT REPAIR WAS PERFORMED ON EXTERNAL SKIN PER B-717 SRM 53-02-01-2R-1 FIG. 202 SHEET 1. VISUAL INSPECTION WAS PERFORMED PER B717 SRM 53-02-01-2R PROCEDURE 1 PAR. 6A AND NO FUTHER DAMAGE FOUND. REPETITIVE 8000 CYCLES INSPECTION PER B717 SRM 53-02-01-2R-1 SDR DALA2018031001601Door Frame · crackedCRACKS ON THE RT FWD OVERWING EMERGENCY EXIT DOOR FRAME PAN UPPER AREA. REPAIRED IAW SRM 53-20-15-2R-8.SDR DALA2018031001600Fitting · crackedCRACKED AFT VENTRAL DOOR FRAME LT FITTING BS 1064, LBL 14.5, Z=37. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018031001599Fitting · crackedCRACKED FITTING BS 665, LONGERON 24 OF AFT BULKHEAD IN THE FWD CARGO BAY. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018031001591Skin · dentedDENT ON FUSELAGE SKIN BETWEEN BS 275 - 294, LONGERON 18L TO 19L. REPAIRED IAW SRM 53-20-01-2R, PROCEDURE 5, FIG 202,
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