N977AT
Service difficulty reports · 159
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 = 'N977AT' 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 = 'N977AT' 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 DALA2024022202463Door Frame · corrodedCORROSION AFT PREVIOUS REPAIR DOUBLER ON FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00195: CORROSION LEVEL 2. NEW DOUBLER ON FWD CARGO COMPARTMENT DOOR JAMB WAS FABRICATED PER B717 SRM 53-20-15-2R PROCEDURE 6 REPAIR 6 AND REPLACED PER SRM 51-41-02-0G AND SDR DALA2024022002327Doubler · corrodedCORROSION ON FWD PREVIOUS REPAIR DOUBLER ON AFT CARGO COMPARTMENT DOOR JAMB PAN. SUMMARY OF NRC 00137: CORROSION LEVEL 2. FWD PREVIOUS REPAIR DOUBLERS ON AFT CARGO COMPARTMENT DOOR JAMB PAN WERE REPLACED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. PERFORM GSDR DALA2024022002325Frame · crackedA.D. CRACK OF 0.100 IN ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 LH (REF CARD 5310-01436-04B). SUMMARY OF NRC 00265: CRACK OF 0.100 IN ON UPPER RADIUS OF THE FRAME TAB ON THE OVERWING FRAME AT STA Y=674.000 LH WAS REPAIRED PER AMDSDR DALA2023062305085Unknown · unknownFIRST CLASS CEILING EXIT SIGN COVER IS MISSING. MAINTAINANCE REPLACED THE COVER AS REQUIRED. AIRCRAFT IS OK FOR SERVICE. (LP #4730934)SDR DALA2023060904690Unknown · unknownCRACK INDICATION ON L/H VERT STAB ON HOLE 5 FROM BOTTOM -MARKED-. CONFIRMED CRACK IS IN SKIN LAYER ONLY QC5253. REMOVED LEADING EDGE VERTICAL STAB REF. B717, AMM 55-32-01. C/W ERA 609501-14AD REV ORIGINAL PERMANENT REPAIR SECTION I QC5270. REINSTALLED LEADING SDR DALA2023060904689Unknown · unknownCRACK INDICATION ON L/H VERT STAB ON HOLES 5 FROM BOTTOM -MARKED-. C/W PRI 609501-14AD REV 0 AND 1 QC 5270. C/W PRI 609501-14AD REV 2 QC 5270. FINAL ERA 609501-14AD REV ORIGINAL MATCHES ALL STEPS OF PRI 609501-14AD REV 0, 1, AND 2 QC 5270. ASSOCIATED ER/A 14-6SDR DALA2022011800324Longeron · corrodedCORROSION AT LONGERON 30 BETWEEN STA 904 AND STA 927. SUMMARY SEE NRC 088-0008:5331-2001/007 00377: REPLACED LONGERON 30 BETWEEN STA 904 AND STA 927 PER B717 SRM 51-40-02. CORROSION LEVEL:2 . (LP #2086514)SDR DALA2022011400280None · noneCORROSION STA 927 TO 946 AT LONGERON 30 AND SPLICE. SUMMARY SEE NRC 088-0008:5331-2001/011 00381: REMOVED CORROSION AND CHECKED LIMITS STA 927 TO 946 LONGERON 30 PER B717 SRM 53-00-00. REPLACED SPLICED PER B717 SRM 53-20-05-2R. (LP #2085655)SDR DALA2022011300256None · noneTHE IDG FEEDER HARNESS IS ROUTED TOO CLOSE TO THE #2 ENGINE FUEL LINE, AS INDICATED IN WORK CARD 0571-9202. THERE MUST BE A 0.39" MIN DISTANCE. SUMMARY SEE NRC 110-0001:0571-9202/010 00370: ROUTED IDG FEEDER HARNESS AS PER AMDS CARD 0571-9202. (LP #2083609)SDR DALA2021091605522Cable · frayedDURING 1L SLIDE REPLACEMENT, THE LANYARD CABLE ASSEMBLY WAS FOUND TO BE FRAYED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE INSTALLED A SERVICEABLE LANYARD PER AMDS 2561.9004. THE AIRSDR DALA2021091405452Door Sill · damagedTHE AFT CARGO DOOR SILL IS DAMAGED ON THE RIGHT HAND SIDE. MAINTENANCE REPLACED THE SILL PER B717 SRM 51-40. (LP #8103207)SDR DALA2019052303142Frame · crackedRIGHT SIDE FRAME 715 SHOWS SIGNS OF A CRACK IN RADIUS WITH NDT TESTING PER 5310-01436-01C. NRC 044-0003:5310-01436-01C/001 00033: REPLACED OW FRAME AT STA 715 RT SIDE PER AMDS 5310-01436-03B. (LP #1086614)SDR DALA2018051503372Gasper Fan · odorTHE FLIGHT WAS DIVERTED TO RDU DUE TO A REPORTED ELECTRICAL ODOR IN THE FIRST CLASS AREA. NO SMOKE OR HAZE WAS VISIBLE AND EVEN WITH THE GALLEY POWER ISOLATED, THE ODOR WAS STILL PRESENT. THE CREW DID DECLARE AN EMERGENCY FOR THE DIVERSION. CORRECTIVE ACTION: SDR DALA201805173101Lens · looseEMERGENCY EXIT SIGN LENS LOOSE. REINSTALLED THE LENS. AIRCRAFT IS OK FOR SERVICE.SDR DALA2018042402773Battery Pack · inoperativeDURING A SERVICE CHECK, PERFORMED AN EMERGENCY LIGHTS TEST, FOUND SEVERAL EXIT LIGHTS THAT WOULD NOT STAY ILLLUMINATED. REPLACED THE BATTERY AND POWER SUPPLY IAW AMM 33-51. OPS TESTED GOOD IAW AMM 33-51.SDR SWAA201710201Channel · crackedDURING AN UNSHEDULED NON ROUTINE CHECK, FOUND INBOARD SPOILER INNER CHANNEL CRACKED.SDR DALA2017090506615Power Supply · defectiveTHE AFT CABIN EMERGENCY EXIT SIGN REMAINED ON WITH THE EMERGENCY SWITCH OFF. MAINTENANCE REPLACED B5-260 EMERGENCY POWER SUPPLY PER AMM 33-51-03 AND THE SYSTEM CHECKS OK.SDR DALA2017090106513Battery Pack · inoperativeDURING A SERVICE CHECK, FOUND EMERGENCY LIGHTS IN AFT EQUIP BAY WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY B5-260 IAW AMM 33-51, OPERATIONAL CHECKED GOOD. AIRCRAFT IS OK FOR SERVICE.SDR DALA2017082206342Access Door · corrodedCORROSION WAS FOUND ON FWD STAIRWAY ACCESS DOOR. DAMAGED AREA WAS REPAIRED IAW ETI-17-17-136, REV 2, AND ER/A 560864-14, REV ORIG.SDR DALA2017082006316Skin · crackedTHREE CRACK INDICATIONS WERE CONFIRMED AT ZFS 49.267, 48.267, AND 44.267. REPAIRED IAW ER/A 560869-14AD, REV ORIGINAL, AND ETI 17-17-128, REV 3.SDR DALA2017082006315Support Fitting · crackedSUPPORT FITTING ON CENTER FUEL TANK FWD FACE WAS FOUND CRACKED ON BS 645, RBL 22, AND Z-9 IN THE FWD CARGO BAY. REMOVED, DRILLED, TREATED, PAINTED, AND INSTALLED IAW SRM 51-41-05.SDR DALA2017082006314Fitting · crackedCRACK ON ANGLE OF WING TO BODY FITTING, LONGERON 22L, BS 661. THE ANGLE WAS REMOVED, FABRICATED, TREATED, PAINTED, AND INSTALLED IAW ER/A 560866-14, AND ETI-17-17-134, REV 3.SDR DALA2017081906313Stiffener · crackedSUPPORT FITTING ON CENTER FUEL TANK FWD FACE WAS FOUND CRACKED ON BS 645, LBL 22, AND Z-9 AT FWD CARGO BAY. THE STIFFENER WAS REMOVED, FABRICATED, DRILLED, AND INSTALLED IAW SRM 51-41-05. NO FOUND LEAKS WERE FOUND.SDR DALA2017081606252Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN BS 1022 AND LONGERON 14L. REPAIRED IAW ETI-17-17-118, REV 2, AND ER/A 559574-14, REV ORIGINAL, ER/A 559574-14, REV ORIGINAL.SDR DALA2017081506244Doubler · damagedDISTRESS LT HOLES (7 EA) ON REPAIR DOUBLER LE STA ZFS=52.267 VERTICAL STABILIZER. REPAIR DOUBLER ON LE STA ZFS=52.267 VERTICAL STABILIZER WAS REPLACED PER SRM 55-30-01 2R REP 7 AND SERVICE GENERAL REPAIR DRAWING SG95550001 REV B.SDR DALA2017081306167Skin · crackedCRACKED FUSELAGE SKIN BS 1076, LONGERON 14R. THE SKIN WAS REPAIRED IAW ETI-17-17-113 REV 1, AND ER/A 559566-14 REV ORIGINAL.SDR DALA2017081006105Rib · crackedDURING SLAT DOOR MECHANISM REMOVAL PER CARD 00229 CRACKED RIB WAS FOUND. RIB WAS REPLACED PER SRM 51-40-05, 51-41-02, 51-41-05, SOPM 20-10-7, AND IPC 57-41-57-01 FIG 101.SDR DALA2017081006104Skin · crackedCRACK ON LWR SKIN FROM STA XRS=170 TO XRS=137 AT TRAILING EGDE RT WING (AD). CRACK ON LWR SKIN FROM STA XRS=170 TO XRS=137 AT TRAILING EGDE RT WING WAS REPLACED PER SRM 51-41-01, 51-41-02, 51-41-05, AND DWG 5912144 REV AN.SDR DALA2017080706014Floor Panel · brokenBROKEN FLOOR PANEL 223KF. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50-2R, REP 3.SDR DALA2017080706013Intercostal · crackedCRACKED INTERCOSTAL BS 427 BTW BEAM 1 AND 2 IN THE FWD CARGO DOOR. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02, AND DWG 9957664, REV N.SDR DALA2017080706012Frame · crackedCRACKED REPAIR DOUBLER ON FRAME FORMER STA 675 BTW AND LONGERON 26R AT CENTER FUSELAGE AREA.REPAIRED IAW SRM 51-70-11-2R.SDR DALA2017080606011Frame · crackedCRACKED FRAME BS 1037 BETWEEN LONGERONS 16R TO 18R. A REPAIR WAS ACCOMPLISHED IAW SRM 53-20-07-2R-4.SDR DALA2017080506008Ferrule · damagedDELAMINATION ON FLOOR PANEL IN THE CABIN. FERRULE REPLACED IAW SRM 53-20-50-2R, REP 3.SDR DALA2017080506006Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL ACCESS PANEL : BUSHINGS FABRICATED IAW SRM 57-10-01-2R-2, CONDITION II AND INSTALLED IAW SRM 57-10-01-2R PROCEDURE 2 STEP 5 (B) 3.SDR DALA2017080406004Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL 211ALF AT COCKPIT. THE FLOOR PANEL WAS REPLACED IAW SRM 53-20-50-2R, REP 3.SDR DALA2017080406003Door Frame · crackedCRACKED DOOR FRAME ON FWD SECTION RT & LT SIDES FRAME 47 AT THE NLG WHEEL WELL AREA. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14, FIG 201-R2. HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-06-10-01. NO CRACKS WERE FOUND AROUND CUT OUT.SDR DALA2017080406002Longeron · crackedCRACKED LONGERON 17L, BS 1022. A NEW LONGERON, AND REPAIR SPLICE WERE INSTALLED IAW SRM 53-00-05-2R-2, AND 51-41-05.SDR DALA2017080305932Cusp Web · damagedELONGATED LIGHTENING HOLES ON THE CUSP WEB BS 617 - 636 AND BS 636 - 655. THE CUSP WEB WAS REPAIRED.SDR DALA2017080205930Cusp Web · corrodedCORROSION ON THE CUSP WEB BS 470 BETWEEN RBL 56 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM.SDR DALA2017080105927Beam · crackedCRACK ON BEAM NR 7, AFT EDGE AT THE L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R-13, FIG 201, SHEET 3.SDR DALA2017073105917Pan · crackedCRACKED OUTER PAN (FWD EDGE) BS 370 BETWEENS BEAM 1 AND 2 AT FWD CARGO COMPARTMENT DOOR. THE PAN WAS REPAIRED IAW SRM. 52-30-02-2R PROCEDURE 3.SDR DALA2017073005913Beam · crackedCRACK ON BEAM NR 1 , AFT EDGE AT PASSENGER ENTRANCE. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, REPAIR 7, FIG 201.SDR DALA2017073005911Floor Support · crackedCRACK ON HAT CHANNEL OF FLOOR PANEL 222 ALF. REPAIRED IAW SRM 53-20-50-2R, REPAIR 5.SDR DALA2015071304341Battery Pack · inoperativeEMERGENCY LIGHTS AT BS 870 - 889 ARE INOPERATIVE. REPLACED THE BATTERY PACK B5-231.SDR DALA2014101405541Battery Pack · inoperativeLT & RT FWD OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY IN POWER SUPPLY IAW AMM 33-51. CHECKS NORMALLY.SDR DALA2014063003810Power Supply · inoperativeDURING LINE CHECK, NOTED THE FORWARD CABIN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY IAW AMM 33-51 AND OPS CHECKED NORMAL.SDR SWAA2013102921674Light · brokenR2 DOOR EMERGENCY EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.SDR SWAA2013102821454Angle · crackedLOWER FUSELAGE EXTERIOR CANTED KEEL LT SIDE FS 660 INTERNAL CRACKED UPPER ANGLE. REPAIRED ANGLE IAW SRM.SDR SWAA2013102221397Angle · crackedLOWER FS EXTERIOR CANTED KEEL LT SIDE AT FS 695 CRACKED UPPER ANGLE. REPAIRED ANGLE IAW SRM.SDR SWAA2013102221396Cusp Web · crackedCUSP WEB CRACKED AT STATION 218, RBL 44. REPAIRED WEB IAW SRM.
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