N991AT
Service difficulty reports · 206
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 = 'N991AT' 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 = 'N991AT' 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 DALA2021081304664Web · damagedSUBFLOOR CUT FROM STATION 696 TO STATION 715. SUMMARY SEE NRC 063-0004:5310-01436-01D/002 00310: REPAIRED SUBFLOOR PER B717 SRM 53-00-55-2R-4 FIG 223. (LP #1909352)SDR DALA2021081804778Skin · damagedTHE AFT CARGO DOOR, FORWARD LOWER EDGE OF DOOR, SKIN IS KNIFE EDGE. THE DOOR WAS REPLACED ON NRC 144 AT C-2 CHECK IN ATLANTA. REPAIRED ON SHOP ORDER RO6476. (LP #1906584)SDR DALA2021080904511Bolt · damagedUPON INSPECTION OF SLANT PANEL HARDWARE, FOUND TOP INBOARD BOLT SPINNING ON RH SLANT PANEL IN WHEEL WELL. SUMMARY SEE NRC 001-0197:5300-2005/001 00121: REPLACED DOME NUTS REF B717 SRM 51-40-02. (LP #1902094)SDR DALA2021032201659Strut · damagedTHE LT MLG FIXED STRUT, OB FITTING HAS TOOLING DAMAGE. NRC 006-0003:3211-4003/010 00024: REWORKED AREA PER B717 CMM/OHM 57-40-1 PAGE 611.005 MATERIAL REMOVED TREATED AND PAINTED BLENDED AREA.SDR DALA2019080604583Threshold · corrodedNUMEROUS AREAS OF CORROSION WAS FOUND AT THE AFT CARGO THRESHOLD. REPLACED AFT CARGO DOOR THRESHOLD REF B717 SRM 53-20-15-2R.SDR DALA2019080504574Bushing · damagedHALF BUSHING GROOVED AT 4TH FROM O/B GEARED TAB HINGE, I/B LEG. REPLACED THE BUSHINGS.SDR DALA2019080904677Skin · damagedCOMPOSITE EXPOSED ON LEFT ELEVATOR ANTI-FLOAT TAB. REMOVED LT ELEVATOR GEARED TAB REF B717 AMM 27-31-05 TAB ASSY, GEARE OFF 92-5522-9-0007 00010. INSTALLED LT ELEVATOR GEARED TAB REF B717 AMM 27-31-05. NRC 132. TAB ASSY, GEAR ON 92-5522-9-0007 00129. (LP120205SDR DALA2019080904676Skin · damagedCOMPOSITE EXPOSED ON LEFT ELEVATOR CONTROL TAB. REMOVE LT ELEVATOR CONTROL TAB, ROUTED TO SHOP FOR REPAIR REF B717 AMM 27-31-04 TAB ASSY, CONTR OFF 95-5525-9-0003 09529. INSTALLED L/H ELEVATOR CONTROL TAB. REF B-717 AMM 27-31-04 TAB ASSY, ON 95-5525-9-0003 551SDR DALA2019080904675Skin · damagedCOMPOSITE EXPOSED ON RIGHT ELEVATOR CONTROL TAB. REMOVED RT ELEVATOR CONTROL TAB REF B717 AMM 27-31-04 TAB ASSY, CONTR OFF 95-5525-9-0002 09529. INSTALLED R/H ELEVATOR CONTROL TAB. REF B-717 AMM 27-31-04 TAB ASSY, CONTR ON 95-5525-9-0002 00268. (LP1202039)SDR DALA2018012200359Lens · damagedF/A REPORTED THAT THE AFT RIGHT EMERGENCY CEILING LIGHT LENS IS DAMAGED. MAINTENANCE REPLACED THE LIGHT ASSEMBLY IAW AMM 33-51. OPS CHECKED SATISFACTORY.SDR SWAA201710202Skin · delaminatedDURING UNSCHEDULED NON ROUTINE CHECK FOUND UPPER SURFACE TO BE DELAMINATED AND MISSING SECTION OF SPOILER SKIN.SDR DALA2017092207027Structure · corrodedCORROSION ON PRINTER ENCLOSURE IN THE COCKPIT. THE DAMAGED AREA FOR THE PRINTER ENCLOSURE WAS FABRICATED AND REPLACED IAW DWG 5991370, REV ORIGINAL, AND SRM 51-41-02.SDR DALA2017092106997Angle · crackedCRACKED ANGLE ON THE RH AFT ENGINE PYLON SUPPORT BULKHEAD BS 1022, LONGERON 7R. REPAIRED IAW ETI 17-17-164, REV ORIGINAL, AND ER/A 560925-14, REV ORIGINAL.SDR DALA2017091906959Skin · crackedCRACKED FUSELAGE SKIN BS 1022, BETWEEN LONGERONS 13R TO 14R. REPAIRED IAW ETI-17-17-148, REV 2, AND ER/A 560890-14, REV ORIGINAL.SDR DALA2017091906958Skin · crackedCRACKED FUSELAGE SKIN BS 1022, BETWEEN LONGERONS 13L TO 14L. REPAIRED IAW ETI-17-17-149, REV 2, AND ER/A 560891-14, REV ORIGINAL.SDR DALA2017091806931Longeron · crackedCRACKED LONGERON 3R, BS 1152. HFEC WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001. THE CRACKS WERE CONFIRMED ON THE LONGERON. TRIMMED OUT AND NO CRACKS WERE FOUND NDT SPM 06-10-01.001. LONGERON WAS REPAIRED IAW SRM 53-00-05, REP 2.SDR DALA2017091606927Frame Angle · corrodedCORROSION ON FRAME ANGLE BS 927, BETWEEN LONGERONS 29L - 30L IN THE AFT CARGO BAY. REPAIRED IAW SRM 53-00-06-2R, REP 2.SDR DALA2017091606926Fitting · crackedCRACK ON MAIN FRAME WING TO FUSELAGE FITTING BS 661, LONGERON 22L. REPAIRED IAW ETI-17-17-155, REV ORIGINAL, AND ER/A 560940-14, REV ORIGINAL.SDR DALA2017091606925Door Frame · corrodedCORROSION ON DOOR FRAME WEB BS 200, LONGERON 18L. A REPAIR WAS ACCOMPLISHED IAW ETI-17-17-160, REV 3, AND ER/A 560920-14, REV ORIGINAL.SDR DALA2017091506902Fitting · crackedCRACKED VERTICAL FITTING BS 663 RBL 22 Z=-12, THE FITTING WAS REPLACED IAW DWG 9910009-123, REV BB, AND SRM 51-41-05. LEAK CHECKED IAW AMM 28-00-00, NO LEAKS FOUND.SDR DALA2017091506903Longeron · crackedCRACKED LONGERON 2R, BS 1133. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, PROCEDURE 2. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.SDR DALA2017091506899Tab · wornWEAR ON UPPER CORNER AT RUDDER TAB. THE RUDDER TAB WAS REPAIRED IAW SRM 55-41-01-2R-1, REPAIR 1, AND JIC 5464417.SDR DALA2017091406880Tab · stuckDURING RUDDER INSTALLATION, RUDDER CONTROL TAB WAS STRUCK ON RT SIDE.SDR DALA2017091306858Tab · debondedDEBONDED AILERON TRIM TAB UPPER SURFACE XAT=12 ON THE LT WING. TRIM TAB WAS REPAIRED IAW SRM 51-70-02-2R-3, REPAIR 3.SDR DALA2017091206828Doubler · corrodedEXFOLIATED CORROSION ON PRODUCTION DOUBLER P/N 9915561-73 OF AFT PRESSURE BULKHEAD LWR AREA. CORROSION LEVEL 2. PRODUCTION DOUBLER P/N 9915561-73 WAS REPLACED PER SRM 51-41-02 AND SRM 51-41-05.SDR DALA2017091006819Frame Angle · crackedCRACKED FRAME ANGLE BS 1022 BETWEEN LONGERONS 16 - 17L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02 AND SRM 51-41-05.SDR DALA2017091006812Floor Panel · crackedCRACKED COCKPIT FLOOR PANEL 211ANF. A NEW FLOOR PANEL WAS FABRICATED IAW SRM 53-20-50-2R, REP 3, AND INSTALLED IAW CARD 2040-0058.SDR DALA2017091006810Cusp Web · crackedCRACKED CUSP WEB BS 889 TO 908, BETWEEN LBL 56 AND 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 2R-4, FIG 226.SDR DALA2017090906797Frame · crackedCRACKED RH FRAMES STA Y=679, Y=694, AND Y=715 AT CANTED KEEL AREA. (FUS). NRC 00364: FRAMES WERE REPAIRED PER B717-200 SRM 51-70-11-2R. CRACKS WERE FOUND WITH FOLLOW DIMENTIONS: STA Y=679 1) 2.350", 2) 2.500"; STA Y=694 1) 2.750"; STA Y= 715 1) 1.650", 2) 0.75SDR DALA2017090906796Frame · crackedCRACKED LH FRAMES STA Y=679, Y=694, AND Y=715 AT CANTED KEEL AREA. (FUS). NRC 00365: FRAMES WERE REPAIRED PER B717-200 SRM 51-70-11-2R. CRACKS WERE FOUND WITH FOLLOW DIMENTIONS: STA Y=679 1) 2.350"; STA Y=694 1) 1.370", 2) 1.350", 3) 0.800"; STA Y= 715 1) 0.7SDR DALA2017090906804Cusp Web · crackedCRACKED CUSP WEB BS 674, LBL 44. THE CUSP WEB WAS REPLACED IAW SRM 53-00-55-2R-4, FIG 226.SDR DALA2017090906803Frame Angle · crackedCRACKED FRAME ANGLE BS 1022 BETWEEN LONGERON 13 - 14R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243 REV JS, SRM 51-41-05, AND SRM 51-41-02.SDR DALA2017090906802Frame Angle · crackedCRACKED LT ANGLE AT BS 1022, BETWEEN LONGERONS 13 & 14L. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JV, SRM 51-41-02-0G, AND SRM 51-41-02-0G.SDR DALA2017090806792Angle · corrodedCORROSION ON THE ANGLE OF THE RT CONSOLE FROM BS 137 TO 157 BETWEEN RBL 44 TO 54. NEW ANGLE WAS REPLACED PER B-717-200 DWG #9936533 REV. CM, SRM 51-41-01 AND SRM 51-41-02. (LP #0203440)SDR DALA2017090806789Door Frame · crackedCRACK ON THE RT NLG DOOR FRAME. NLG DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R, REP 2.SDR DALA2017090806788Door Frame · crackedCRACK ON Y=42 LT SIDE OF NLG DOOR FRAME. THE NLG DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R, REP 2.SDR DALA2017090706702Fitting · crackedCRACKED LEFT FITTING BS 1063, LBL 17, Z=20. IN THE AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR FRAME. A NEW FITTING WAS INSTALLED IAW SRM 51-41-05, 51-41-02, AND 51-40-08.SDR DALA2017090706701Hinge · wornFREE PLAY ON BOTH HINGES AT FWD CARGO DOOR. THE FWD & AFT HINGES WERE REPAIRED IAW ER/A 559577-14MA, REV ORIGINAL.SDR DALA2017090706700Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PLATES #520CT AND 620CT (AMDS 5720-2001) (AI) (AD). NRC 00472: THE UPPER WING ACCESS DOOR 520CT AND 620CT WERE REPLACED PER B-717 SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION III AND PART NUMBERS WERE VERIFIED PER B-717 AIPC 57-22-01-01SDR DALA2017090706693Access Panel · damagedELONGATED HOLES ON FUEL TANK ACCESS PLATES #520CB, 520FT, AND 520EB (AI). NRC 00471: FUEL ACCESS PLATES #520CB, 520FT, AND 520EB WERE REPAIRED PER B-717 SRM 57-10-01 REPAIR 2 PAR. 5 CONDITION II. (LP #0201639)SDR DALA2017090706699Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL 620DT OUT OF ALLOWABLE LIMITS, THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, PAR 5, REPAIR 2.SDR DALA2017090706698Angle · crackedCRACKED INTERNAL ANGLE ON UPPER AFT AND FWD CORNER OF THE RT AFT EMERGENCY EXIT DOOR. REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9957735, REV G.SDR DALA2017090706697Angle · crackedCRACKED INTERNAL ANGLE. UPPER AFT CORNER AT THE RT FWD EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9957735, REV. G.SDR DALA2017090706695Angle · crackedCRACKED INTERNAL ANGLE, UPPER FWD CORNER AT THE LT AFT & LT FWD EMERGENCY EXIT DOORS THE ANGLES WERE REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9957735, REV G.SDR DALA2017090706692Pan · crackedCRACK ON INNER PAN BETWEEN BEAMS 1 AND 2 AFT EDGE AT FWD CARGO COMPARTMENT DOOR. HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM PART 6, 06-10-01.001 AND ONE CRACK WAS DELIMTED OF 2.000" LENGHT. REPARIED IAW SRM 52-30-02-2R-4. FIGURE 201.SDR DALA2017090706691Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PLATE 620JB. THE ACCESS PANEL WAS REPLACED.SDR DALA2017090606644Fitting · crackedCRACKED FITTING, BS 715, RBL 44, Z=-8. THE FITTING WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND 51-40-08.SDR DALA2017090606643Doubler · damagedWEAR ON DOUBLER AT FLIGHT ATTENDANT SEAT ENCLOSURE OF AFT VENTRAL DOOR. THE WEAR WAS BLENDED IAW SRM 52-10-02-1A-2. NDT WAS ACCOMPLISHED IAW SPM 04-00-07, PAR 5, FIG 3, SHEET 1 AND 2, FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02-1A-2. REPAIRED IAW SRM 52-10SDR DALA2017090306565Channel · crackedCRACKED CHANNELS ON FLOOR PANELS #221NF, 221SF, 221TF, 221XF, 222AQF, 222EF, 222SF, 222AF, 222XF, AND 222AFF AT CABIN PAX (CPAX). NRC 00338: HFEC INSPECTION WAS ACCOMPLISHED ON CHANNELS ON FLOOR PANELS #221NF, 221TF, 221XF, 222AQF, AND 222SF AND NO CRACKS WERESDR DALA2017090406569Beam · crackedCRACKED BEAM 1 ON AFT EDGE BS 200 ON THE L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, REPAIR 7, FIG .201.
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