N977DL, cancelled Sep 6, 2019
Service difficulty reports · 239
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 = 'N977DL' AND deregistration_id = 'N977DL-2019-09-06' 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 = 'N977DL' AND deregistration_id = 'N977DL-2019-09-06' 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 DALA2019032901995Cable · burnedDURING WAKE UP CHECK LIST AMP INDICATION NO SHOW. ELECTRICAL CABLE P44A24 AND C/B WERE FOUND BURNED, CABLE AND C/B B1-171 WERE REPLACED PER MD88 SWPM 20-10-06 AMD AMM 24-00-00. TEST WAS PERFORMED PER AMM 24-30-02 TEST OK. (LP4883756)SDR DALA2019032801990Fastener · looseAWR. IN REFERENCE AMDS 5530-01045-05 STEP 2 LOOSE FASTENERS WAS FOUND ON VERTICAL STABILIZER LEADING EDGE STA ZFS: 52.26. FASTENERS ON VERTICAL STABILIZER LEADING EDGE STA ZFS: 52.26 WERE REPLACED PER ETI-88-19-028 REV.2 AND ERA 576759-14AD REV. ORIGINAL. SECTSDR DALA2019032901993Skin · damagedSTABILIZERS VERTICAL FIXED LE SKIN, ZFS. ELONGATED HOLES. DTA MONITOR INSPECTION LOG REFERENCE ER/A 576759-14AD SECTION II REQUIRES DTA APPROVAL ON OR BEFORE THE NEXT 24 MONTHS. DISCONTINUE REVENUE SERVICE ON OR BEFORE THE NEXT 24 MONTHS PENDING A DAMAGE TOLERSDR DALA2019032601911Doubler · crackedINITIAL INSPECTION: CRACK ON DOUBLER REPAIR OF LEADING EDGE BTW XRS= 190 AND XRS= 210 LT WING. DOUBLER REPAIR OF LEADING EDGE BTW XRS= 190 AND XRS= 210 LT WING WAS REPLACED PER ETI-88-19-026 REV. ORIGINAL AND ER/A 532516-14 REV A SECTION III. (LP1001760)SDR DALA2019032501887Spacer · corrodedINITIAL INSPECTION: CORROSION AT SPACER OF THE CENTER LOWER CARGO DOOR JAMB BEAM. (CORROSION LEVEL 2): SPACER WAS REPLACED PER SRM 53-05 FIG 123A (SHEET1). (LP1000032)SDR DALA2019032301883Doubler · wornINITIAL INSPECTION : WEAR ON REPAIR DOUBLER AT EXT USELAGE SKIN FWD PASSENGER DOOR ( L1 ) PROJECTION LONG 16/ 15L AT FUSELAGE. REPAIR DOUBLER AT EXT FUSELAGE SKIN FWD PASSENGER DOOR, PROJECTION LONG 16/ 15L WAS REPLACED PER SRM 52-05 PAR. 17 FIG. 20A. (LP09970SDR DALA2019032201843Skin · wornWEAR AT UPPER PREVIOUS REPAIR SKIN ON INTERNAL VANE GUIDE AT OUTBOARD FLAP RT WING. INTERNAL VANE GUIDE AT OUTBOARD FLAP RT WING WAS REPAIRED PER SRM 57-03D. (LP0995827)SDR DALA2019031801764Spacer · corrodedINITIAL INSPECTION: CORROSION AT SPACER OF THE AFT LOWER CARGO DOOR JAMB BEAM. (CORROSION LEVEL 2): SPACER OF THE AFT LOWER CARGO DOOR JAMB BEAM WAS REPLACED PER SRM 53-05 FIG. 123. (LP0990137)SDR DALA2019020400703Bulb · inoperative23D SEAT EMERGENCY LIGHT OUT. R/R BULB AT SEAT 23D PER STANDARD PRACTICE. (LP4807909)SDR DALA2019012100375Skin · crackedFOUND CRACK AT STA. 1474 LEFT SIDE FWD OF TAILCONE SLIDE HANDLE. REPAIRED PER SRM 53-01 FIG 2 SHEET 3. (LP5088564)SDR DALA2018111506633Bottle · low pressureDURING SVC, FOUND L1 DOOR SLIDE BOTTLE PRESSURE IN RED ''NO GO'' STATUS. R/R L1 DOOR SLIDE PER W/C 2561-4964. ACFT OK FOR SVC. (LP5055352)SDR DALA2018100405889Light · inoperativeFOUND LT OVERWING EXIT UPPER EMERGENCY LIGHT INOP. RELAMPED OVERWING EXIT EMERGENCY LIGHT IAW AMM 33-50. OPS CK NML. (LP3740096)SDR DALA2018080644858Charger · inoperativeAFT CABIN EMERGENCY LIGHT ON THE CEILING FROM ROW 32 AND BACK WERE INOPERATIVE. FOUND THE CHARGER NOT CHARGING THE BATTERY PACK. REPLACED THE CHARGER IAW AMM 33-51. LIGHTS TESTED GOOD.SDR DALA2017122708913Floor Panel · damagedFLT CREW REPORTS SOFT SPOT IN GALLEY FLOOR BETWEEN G1 AND G3. FLOOR PANEL REF IPC 53-21-00-02J AND REPLACED NICKEL MAT. OK FOR SVC.SDR DALA2017060104397Pump · malfunctionedON TAKEOFF ROLL CENTER FUEL PRESS LO LIGHT ILLUMINATED. CB J21 AND J23 WERE FOUND POPPED ON CLIMBOUT. T/S PER MM REF 28-20-07-101 THRU STEP 4 - WIRING CK AT TERMINAL STRIP S3-10 CKS OK. REF WDM 28-21-00 RANG LT AND RT BOOST PUMPS PHASES A B C TO GRD AND PHASESDR DALA2017050103519Wire · arcedON DESCENT INTO ATL TURNED ON W/S ANTI-FOG SWITCH. RECEIVED A QUICK FLASH IN COCKPIT, POPPING SOUND, EFIS FLICKERED MOMENTARILY. HAD ELECTRICAL BURNING SMELL FOR ABOUT 10 SECONDS, NO SMOKE, DISSIPATED QUICKLY. EVERYTHING NORMAL AFTER INCIDENT. PERFORMED 2120-2SDR DALA2017040702855Connector · brokenEMERGENCY LIGHT INOPERATIVE AT SEAT 31 AB. REPLACED A BROKEN CONNECTOR IAW SWPM 20. OPS CHECKED GOOD.SDR DALA2017030901904Light · malfunctionedAFT EMERGENCY LIGHTS ILLUMINATED WITH POWER REMOVED FROM ACFT. PERFORMED EMERGENCY LIGHT CHECK IAW AMM 33-53. RECYCLED ARM SWITCH WITH POWER OFF, OPS CHECKED GOOD.SDR DALA2017020701007Frame · crackedFRAME BS 1451 CRACKED AT LONGERON 1. . REPAIRED IAW ERA 554841-14 REV ORIG.SDR DALA2017020600997Bulkhead · damagedRIGHT AFT PRESSURE BULKHEAD LOWER SHEAR ANGLE DAMAGED. REPAIRED IAW ERA 554877-14 REV ORIG.SDR DALA2017020600996Bulkhead · damagedLEFT AFT PRESSURE BULKHEAD LOWER SHEAR ANGLE DAMAGED. REPAIRED IAW PRI 554877-14 REV 0 AND COMPLIED WITH ERA 554877-14 REV ORIG.SDR DALA2017020500988Frame · crackedFRAME BS 1437 FWD SIDE HAS A 2 INCH LONG CRACK THRU THREE FASTENER HOLES, RBL 7. REPAIRED IAW PRI 554290-14 REVISIONS 1, 2, AND 3 AND COMPLY WITH ERA 554290-14 REVISION ORIGINAL.SDR DALA2017020500987Frame · crackedFRAME BS 1437, FWD SIDE HAS A 2 INCH LONG CRACK, LBL 7. REPAIRED IAW PRI 554290-14, REVISIONS 1, 2, AND 3 AND COMPLIED WITH ERA 554290-14 REVISION ORIGINAL.SDR DALA2017020400950Shear Tie · crackedTAIL INTERIOR, CROWN SHEAR TIE HAS 2 CRACKS, BS 1437, RBL 8. REPAIR PER DWG 9953016.SDR DALA2017020300881Skin · crackedTAIL SKIN HAS A CRACK BETWEEN TWO RIVETS AT BS 1437, LONGERON 4 & 5L. REPAIRED IAW PRI 554872-14 REV 0RIGINAL AND COMPLIED WITH ERA 554872-14 REV ORIGINAL.SDR DALA2016122010001Wire · brokenFOUND EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRES AT SEAT 31ED IAW SWPM. OK FOR SERVICE.SDR DALA2016101207190Vane · damagedHOLE IN INBD FIXED VANE, OTBD SECTION OF RT WING TE FLAP. REMOVED AND REPLACED THE VANE IAW AMM 27-51-03 P 201.SDR DALA2016101107176Tab · damagedRUDDER CONTROL TAB HAS FLAME SPRAY MISSING IN CRITICAL AREAS. REMOVED & REPLACED RUDDER CONTROL TAB IAW WORK CARD 2720-4321. OK FOR SERVICE.SDR DALA2016042003141Wire · brokenMSP MAINTENANCE FOUND THE EMERGENCY LIGHTS INOPERATIVE AT SEAT ROWS 17DE, 22DE, AND 33DE. BROKEN WIRES WERE FOUND AND REPAIRED UNDER 17R, 22E AND 33E. ALL LIGHTS CHECKED OK.SDR DALA2016040802712Tab · damagedLEFT ELEVATOR ANTI-FLOAT TAB HAS LIGHTNING STRIKE. REPLACED TAB IAW AMDS CARD 2730-4382.SDR DALA2015102606485Wire Harness · damagedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT SEAT 12D WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.SDR DALA2015022601663None · noneINADECUATE RIVETS ON STA 435 AND BETWEEN LONGERON 20 TO 24RT. FASTENERS WERE REMOVED. AREA WAS TREATED AND PAINTED AND NEW FASTENERS WERE INSTALLED IAW SRM 51-30-5, 51-10-3, PAR 14 AND 21. REPAIR WAS ACCOMPLISHED IAW ER/A 532510-14, REV ORIGINAL AND ETI-88-SDR DALA2015022601660Doubler · corrodedTHE AFT LAV CUTOUT DOUBLER WAS CORRODED AND REPAIRED, 532435-14.SDR DALA2015022601667Panel · corrodedCORROSION WAS FOUND ON INTERNAL DOUBLER AT FWD LAVATORY SERVICE PANEL BTW STA Y= 282 TO 287 AND LONGS 20LH TO 22LH. REPAIR WAS PERFORMED WITH ER/A 473507-14 REV "A". (LP1836669)SDR DALA2015022301584Door Frame · crackedCONTINUED CRACK ON AFTER TO PREVIOUS REPAIR AT DOOR JAMB AT STA Y=46, X=29 AT NOSE WHEEL WELL STRUCTURE. DOOR JAMB WAS REPAIRED IAW ETI-88-15-033, REV 4 AND ER/A 531399-14, REV ORIGINAL.SDR DALA2015022301583Angle · corrodedCORROSION ON CUSP ANGLE IN STA Y=646, Y=655 AND Y=674 ON X=-60 RT SIDE AT PAX CABIN STRUCTURE. REPAIR WAS PERFORMED WITH ER/A 532529-14, REV ORIG.SDR DALA2015022301582Slat Track · crackedCRACKED LOWER EDGE CUT OUT SLAT TRACK NR 7 LT WING. L/E OUTER WING SKIN WAS REPAIRED IAW ETI-88-15-063, REV 3 AND ER/A 532516-14, REV ORIGINAL.SDR DALA2015022301580Access Panel · crackedCRACKED SETTLEMENT AREA, BOTH SIDES OF ACCESS PANEL 6301B AT DORSAL FIN L/E. DORSAL ANGLES WERE REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, 51-10-3 PARA 14 & 21, AND DWG 5912188 REV BD.SDR DALA2015022201570Door Frame · corrodedCORROSION ON LOWER DOOR JAMB, BETWEEN STA Y=638 TO Y=893 ON LONGERON 28 AT CTR CARGO COMPARTMENT. PREVIOUS REPAIR SPACER WAS REPLACED IAW SRM 53-05, FIG 123A.SDR DALA2015022201565Access Panel · corrodedCORROSION ON COUNTERSINK AT LT MAIN FUEL TANK ACCESS PLATE NR 1311C. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120.SDR DALA2015022201564Access Panel · corrodedCORROSION ON COUNTERSINK AT LT MAIN FUEL TANK ACCESS PLATE NR 1335C. ACCESS PLATE WAS REPLACED AND WILL BE INSTALLED UNDER CARD 2800-0120.SDR DALA2015022201563Track · corrodedSEVERAL CORROSION POINTS ON RT TIE TRACK FROM STA Y=1212 TO 1320 AFT CARGO COMPARTMENT THE TRACK WAS REPLACED IAW 51-30-1 AND DWG 5936660, REV BZ.SDR DALA2015022201562Track · corrodedSEVERAL CORROSION POINTS ON LT TIE TRACK FROM STA Y=1174 TO 1320 AFT CARGO COMPT. TIE TRACK WAS REPLACED IAW SRM 51-30-1 AND DWG 593666, REV BZ.SDR DALA2015022201537Frame · corrodedSEVERAL CORROSION POINTS ON FRAME AT STA Y=1250 BETWEEN LONGS 27L TO 27R AFT CARGO COMPT CORROSION WAS REMOVED; MEASURED AND FOUND OUT OF LIMITS IAW SRM 51-10-3 PAR 26 AND 53-01, FIG 1, BETWEEN L-28 TO L-28R. UT WAS ACCOMPLISHED ORIGINAL THICKNESS IS 0.063" ASDR DALA2015022101530Floor Support · crackedCRACKED FLOOR SUPPORT AT STA Y=1136 BETWEEN LONGERONS 27L TO 26L AFT CARGO COMPT. FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-2 AND ER/A 413029-14MA, REV "D".SDR DALA2015022101529Structure · wornWEAR ON UPPER SURFACE ALSO UPPER/INBD EDGE AT OTBD FLAP/OTBD VANE RT WING. UPPER SURFACE ALSO UPPER/INBD EDGE AT OTBD FLAP/OTBD VANE RT WING WERE REPAIRED IAW ER/A 521199-14MA REV ORIGINAL AND SRM 57-03D.SDR DALA2015022101522Floor Panel · unknownINITIAL REPAIR AS REQUIRED PAX CABIN FLOOR PANELS FROM STA Y=120 TO 1338 BETWEEN X=- 44 TO X= 44. FLOOR PANELS NRS 160A, 160E, 160F, 148A, 148B, 148D, 148C, 200C, 160D, 160B, 200E, 826C, 826F, 927B, 927D, 617E, 389F, 769E, 160C, 200D, 826D, 886C, 120E, 617C, SDR DALA2015022101520Rib · crackedCRACKED RIBS AT VERTICAL STABILIZER L/E STA ZFS 23.500 AND STA ZFS 17.656. CRACKED RIBS WERE REPAIRED IAW SRM 55-02, FIG 27.SDR DALA2015022101518Rib · crackedCRACKED RIBS AT VERTICAL STABILIZER L/E. CRACKED RIBS WERE REPAIRED IAW SRM 55-02, FIG 27.SDR DALA2015022101517Web · crackedCRACKED LOWER DOOR JAMB WEB AT STA Y=1217 APPROXIMATELY BETWEEN PROJECTION LONGERONS 28R AND 27R AFT CARGO COMPT WEB WAS REMOVED. NEW WEB WAS DRILLED, TREAT AND PAINTED AND WAS INSTALLED IAW DWG 5936442, REV "A" SRM 51-10-3, PAR 21 AND 14; 51-10-4, 51-30-1, 5
Back to N977DL, cancelled Sep 6, 2019