N932DL, cancelled Sep 16, 2019
Service difficulty reports · 110
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 = 'N932DL' AND deregistration_id = 'N932DL-2019-09-16' 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 = 'N932DL' AND deregistration_id = 'N932DL-2019-09-16' 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 DALA2018082405240Fastener · missingLMLG INBD DOOR MISSING FASTENERS AND IS CRACKED AT FWD HINGE. REMVD LMLG DOOR REF MD88 AMM 32-12-01. INSTLD LMLG DOOR THROUGH STEP 3D REF MD88 AMM 32-12-01(520426. DOOR INSTALLATION AND RIG CKS COMPLETED IAW MD88 AMM 32-12-01. (LP4591052)SDR DALA2018071004436Light · inoperativeENTRY LIGHT FWD INOP. F/A REPORT ENTRY L1 DOOR LT BULB INOP. RE-LAMPED ENTRY WAY BULB AT L1 DOOR. OPS GOOD OK FOR SVC.SDR DALA2018042002663Lamp · inoperativeTHRESHOLD LIGHT INOPERATIVE. ENTRY LIGHT BLEW WITH SPARKS. REPLACED THE LAMPS. CHECKED OK.SDR DALA2018022701206Panel · corrodedCORROSION ON THE AFT LAVATORY SERVICE PANEL. REPAIRED IAW TOPP 20-50-20, AND PRI 541624-14 REV O -2. ERA 541624-14 REV A STEPS 1-13.SDR DALA2018022601126Spar · crackedRT VERTICAL STAB FRONT SPAR FORWARD FLANGE L/E ATTACH HOLES 3 EACH INDICATE CRACK. HOLES ARE MARKED 4,7, AND 8 BELOW L/E SPLICE PLATE. COMPLIED WITH ERA 556177-14AD REV A AND FOUND TO MATCH PRI 556177-14 REV A REVISION 0.SDR DALA2018013000500Battery Pack · defectiveSEAT MOUNTED EMERGENCY LIGHTS FROM 31 BACK INOP. SUSPECT BATTERY PACK B5-212, STA 1233, RT OVERHEAD BIN. ACCESS PANEL OPENED. T/S PER WDM 33-51-14 SHT2, FOUND FUSE OF B5-212 BLOWN. ISOLATED TAIL CONE HANDLE LT ASSY, LT OPN NML, REMOVED WIRES L982T14 AND L983E1SDR DALA2018012500418Fuse · blownIN SEAT EMERGENCY LIGHTS OUT ROWS 31 AFT. REMOVED BATTERY PACK FOR ASSOCIATED SEATS AND FOUND ONE FUSE BAD ON THE CRADLE. REPLACED FUSE, REINSTALLED BATTERY AND OPS CK GOOD REF AMM 33-53.SDR DALA2018012200327Fuse · failedSEAT EMERGENCY LIGHTS AT ROWS 31-36 FOUND INOPERATIVE. REPLACED THE FUSES FOR THE BATTERY PACK IAW AMM 33-53. CHECKED GOOD.SDR DALA2018012200326Battery Pack · inoperativeEMERGENCY LIGHTS IN THE TAIL SECTION FOUND INOPERATIVE. REPLACED THE BATTERIES, CHECKED GOOD IAW AMM 33-53.SDR DALA2017122008759Smoke Detector · false activationFWD LAVATORY SMOKE DETECTION SYSTEM- SMOKE DETECTOR SOUNDED WITH NO EVIDENCE OF SMOKE OR ODORS. REMOVED AND REPLACED THE FWD LAV TRASH SMOKE DETECTOR.SDR DALA2017091806921Fire Loop · malfunctionedLEFT ENGINE FIRE LIGHT ILLUMINATED WITH AURAL WARNING DURING DESCENT. ACCOMPLISHED QRH PROCEDURE. ENGINE FIRE LIGHT REMAINED ON AFTER BOTH FIRE BOTTLE AGENTS USED. ENGINE SHUTDOWN AT 27,000 FT. ALL ENGINE INDICATIONS NORMAL BEFORE SHUTDOWN. LEFT ENGINE LOOSDR DALA2017071905534Engine · making metalLEFT ENGINE OIL STRAINER CLOGGED. EMERGENCY DECLARED. CHIP DETECTOR CLEAN AND FILTER CHECKED GOOD. FOUND METAL IN OIL TANK AND REPLACED ENGINE.SDR DALA2017070505220Cap · displacedON TAXI IN, CABIN BEGAN TO FILL WITH SMOKE. FOUND APU OIL CAP ON CROOKED AND OIL DRIPPING OUT OF APU INLET.SDR DALA2017031101966Spar · crackedVERTICAL STABILIZER SPAR LEADING EDGE CRACKED. COMPLIED WITH ERA 556177-14AD, REV ORIG, AND PRIS 556177-14AD, REV 0-8.SDR DALA2017031101965Spar Cap · crackedRIGHT HORIZONTAL STAB FRONT SPAR CAP HAD CRACK INDICATIONS, REPAIRED IAW ERA 556177-14 AD REV ORIG.SDR DALA2016031401942Charger · failedMAINTENANCE FOUND EMERGENCY LIGHTS INOPERATIVE FROM SEAT ROWS 1 TO 30. THE BATTERY CHARGER AND DIODE WAS REPLACED.SDR DALA2016030301652Battery Pack · inoperativeTHE FLIGHT CREW OF FLIGHT 333, FOUND EMERGENCY EXIT LIGHTS AT LT AND RT FORWARD DOORS, FORWARD GALLEY, AND SEAT ROWS ROWS 1 THROUGH 30 INOPERATIVE. CVG MAINTENANCE REPLACED BATTERY PACK AND CHARGER B5-211 AND THE LIGHTS CHECKED OK.SDR DALA2016012500570Support Bracket · crackedCRACKED UPPER BRACKET SUPPORT AND MISSING SCREW ON LOWER BRACKET SUPPORT OF EST NDAR ELECTRONIC MODULE AT FWD FACE OF FUEL CENTER TANK BRACKET SUPPORT WAS REPLACED IAW DWG 5939757-3, REV K.SDR DALA2016012400551Skin · corrodedCORROSION ON FUSELAGE SKIN AND INNER PRODUCTION DOUBLER AROUND AFT LAV SERVICE PANEL. ALSO CORROSION IS RUNNING UNDER SKIN, PANEL AND DOUBLERS. DUE TO EXCESSIVE CORROSION AREA WAS REPAIRED IAW ERA 541624-14, REV ORIG.SDR DALA2016012200528Door Frame · corrodedCORROSION ON LOWER EDGE AT DOOR JAMB AFT, MID AND FWD CARGO. MID CARGO WAS ATTENDED WITH NRC 20000097097, CARD 156, ZONE 100, AFT CARGO: NEW SPACER WAS INSTALLED IAW ERA 489172-14, REV ORIGINAL SRM 51-10-3, PAR 21, 14, 38 AND 26 FWD CARGO WAS ATTENDED WITH NRSDR DALA2016012300537Skin · corrodedEXFOLIATION CORROSION BS 674 BETWEEN LONGERON 30 RT AND 29 RT AT FUSELAGE SKIN. REPAIR FUSELAGE SKIN AT BS 674 BETWEEN LONGERON 30 RT AND 29 RT WAS ACCOMPLISHED IAW ER/A 541626-14, REV ORIGINAL.SDR DALA2016012100500Access Panel · damagedDAMAGE PAINT ON ACCESS PLATE 6508A, RUDDER. ACCESS PLATE 6508A, RUDDER WAS PAINTED IAW SRM 51-10-3B. PROCESS B & C AND METALIZED WAS REPAIRED IAW SRM 51-70-1A, D PAR 27.SDR DALA2016012000443Access Panel · damagedDAMAGE FLAME SPRAY ON ACCESS PLATE 6504A0. ACCESS PLATE 6504A WAS REPAIRED IAW SRM 51-70-1AD, PAR 23, AND CARD 2000-8149-01, JOB 000-002.SDR DALA2016012300543Bottle · low pressureMAINTENANCE FOUND THE R1 EMERGENCY ESCAPE SLIDE BOTTLE PRESSURE INDICATOR IN THE RED. THE R1 EMERGENCY ESCAPE SLIDE WAS REPLACED.SDR DALA2016011800416Longeron · crackedCRACKED LONGERON 4L AT INTERSECTION WITH FRAME AT BS 200. SECTION OF THE LONGERON WAS REMOVED IAW SRM 53-02, PAR 12, FIG 18. A NEW SECTION AND REPAIR SPLICE WERE ADJUSTED IAW SRM 53-02, PAR 12, FIG 18. THE NEW LONGERON AND SPLICE WERE TREATED AND PAINTED IASDR DALA2016011800415Skin · wornWEAR ON BS 1309, LONGERON 19R OUTER FUSELAGE SKIN. REPAIRED IAW SRM 53-04-2, FIGURE 2, SHEET 3.SDR DALA2016011500361Skin · dentedPROTUBERANCE ON, BETWEEN LONGERON 24RT AND 25RT BS 168 AT OUTER FUSELAGE SKIN. THIS DAMAGE WAS FOUND WITH PREVIOUS REPAIR IAW SRM 53-04-2, FIG 2, SHEET 3.SDR DALA2016011400300Skin · crackedCRACK ON FUSELAGE SKIN BS 1480. THE SKIN WAS REPAIR IAW SRM 53-01.SDR DALA2016010600052Fuse · failedFWD CABIN, ROWS 30 AND UP, AISLE EMERGENCY LIGHTS INOPERATIVE, SEAT MOUNTED. REPLACED FUSE IN BATTERY PACK B5-211. OPS CHECK GOOD.SDR DALA2016010300015Wire · damagedMAINTENANCE FOUND ALL AISLE AND L1 AND R1 EMERGENCY EXIT SIGNS INOPERATIVE. A WIRE FOR SEAT ROW 13-23 WAS FOUND DISCONNECTED AT PLUG AND COMING IN CONTACT WITH AIRFRAME. THE WIRE WAS REINSTALLED AND THE LIGHTS CHECKED OK.SDR DALA2015123107770Fuse · failedMAINTENANCE FOUND EMERGENCY LIGHTING INOPERATIVE AFT OF SEAT ROW 35. THE BATTERY PACK FUSE WAS REPLACED AT ROW 35. LIGHTS CHECKED OK.SDR DALA2015071504389Support Angle · crackedDURING JACKSCREW INSPECTION FOUND RT VERTICAL STABILIZER STRUCTURE CRACKED. REMOVED RT VERTICAL STABILIZER SUPPORT ANGLE. THE SUPPORT ANGLE WAS FABRICATED, HEAT TREATED, DRILLED AND INSTALLED IAW DWG 9911808 AND SRM 51-30-04.SDR DALA2015071504388Support · crackedDURING JACKSCREW INSPECTION, FOUND LT VERTICAL SUPPORT STRUCTURE CRACKED. REMOVED LT VERTICAL STABILIZER SUPPORT STRUCTURE, CLIP, REPLACEMENT CLIP WAS FABRICATED. DRILLED, PAINTED AND INSTALLED IAW DWG 9911808 AND SRM 51-30-04 AS A REF.SDR DALA2015052803572Unknown · smokeFLIGHT RETURNED TO DEPARTURE AFTER SMOKE ACCUMULATED IN THE CABIN AND COCKPIT. THE AFT LAVATORY SMOKE DETECTOR ALSO SOUNDED BRIEFLY. MAINTENANCE REPLACED A LEAKING APU AND ACCOMPLISHED THE PNEUMATIC SYS DUCT BURN OUT PROCEDURES.SDR DALA2015051903361Gasket · leakingF/A AND PASSENGERS EXPERIENCED HAZE AND SMOKE IN CABIN AFTER TAKEOFF. THE AFT LAVATORY SMOKE DETECTOR WAS SOUNDING DURING THE CLIMB THROUGH 7000 FT. THE CREW DECLARED AN EMERGENCY AND RETURNED. MAINTENANCE FOUND THE APU INLET CONTAMINATED WITH OIL. A LEAK ATSDR DALA2014072804254Pin · unsecureDURING INSPECTION OF THE L1 DOOR SLIDE, MAINTENANCE FOUND THE SLIDE PIN NOT ENGAGED AND SLIDE PARTIALLY INFLATED. MAINTENANCE R & R THE SLIDE PACK.SDR DALA14015820932Wire · brokenEMERGENCY ESCAPE LIGHT AT ROW 28 INOPERATIVE. FOUND WIRE BROKEN AT CONNECTOR. INSTALLED NEW CONNECTOR IAW CH 20, OPS CHECKED OK.SDR DALA14005160932Bracket · wornMAINTENANCE DISCOVERED THAT THE TAILCONE LT AND RT SPRING BRACKETS ARE WORN BEYOND 50 PERCENT. BRACKETS REPLACED AND SYSTEM RIGGED TO SPECIFICATIONS. FUNCTIONAL CHECK COMPLETED SATISFACTORILY.SDR DALA14005150932Conduit · out of positionMAINTENANCE DISCOVERED THAT THE TAILCONE LOCKING CABLE CLAMP DOES NOT CLEAR THE CONDUIT .5. CLAMPS REPLACED AND CONDUIT ADJUSTED IAW THE MM.SDR DALA14005140932Skin · crackedCRACK INDICATION ON SKIN ABOVE PYLON BS 1380, LONGERON 13L, ACCOMPLISHED HFEC OF AREA IAW NDT SPM 06-10-01, CRACK INDICATION VERIFIED. REMOVED CRACK COMPLETED, DAMAGE CONTAINED USING HFEC NDT 06-10-01-001.SDR DALA13037540932Turnbuckle · brokenDURING INSPECTION, MX FOUND THAT THE TAILCONE CATWALK COUNTER BALANCE CABLE WAS BROKEN ON THE RT SIDE. THIS IS CONSIDERED A DEFECT IN THE EMERGENCY ESCAPE SYS AND COULD HAVE AN ADVERSE AFFECT ON THE EVACUATION ROUTE. THE MOVEABLE CATWALK COUNTER BALANCE CABLESDR DALA13013840932Connector · inoperativeDURING SERVICE CHECK, THE SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHTS WERE INOPERATIVE AT ROW 35D. REPLACED SEAT 35D EMERGENCY LIGHT HARNESS CONNECTOR AND OPERATION CHECKED NORMALLY.SDR DALA12016490932Battery · inoperativeDURING LINE CHECK, MX FOUND THAT THE EMERGENCY EXIT SIGN ABOVE ROW 23 WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.SDR DALA1250260932Connector · looseDURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING BETWEEN SEAT ROWS 16 TO 30 WERE INOPERATIVE. MX FOUND A LOOSE CONNECTION AT THE BATTERY PACK AND SECURED. THE FUNCTIONAL CHECK OF THE SYSTEM WAS SATISFACTORY.SDR DALA1248580932Longeron · crackedDURING HMV, A CRACK WAS FOUND ON LT LONGERON 16 BS Y=1437. REPLACED LONGERON SECTION AND SPLICE IAW SRM 51-30-2 51-30-5 53-14-4 AND DWG 5910228, REV KH.SDR DALA1248570932Longeron Splice · damagedDURING HMV, ELONGATED HOLES WERE FOUND ON SPLICE AND LONGERON 2L STA Y=227 AT FUSELAGE INNER STRUCTURE. REPAIRED LONGERON AND SPLICE IAW SRM 53-02, FIG 18.SDR DALA1248550932Skin · corrodedDURING HMV, CORROSION WAS FOUND ON LT WING LOWER SKIN AT STATION XRS=118 LENGTH 3.218" WIDE 0.531" AND DEPTH 0.054". AREA WAS BLENDED OUT AND LEAVE AS IS CONDITION IAW ER/A 506622-14 REV, ORIG.SDR DALA1248450932Skin · crackedDURING HMV, CRACKS WERE FOUND ON FUSELAGE SKIN PRODUCTION. DOUBLER BS 1429 BTW LONGERON 2-3R AND BTW LONGERON 2-3L. REPLACED FUSELAGE SKIN PRODUCTION DOUBLER IAW DWG 5910011, REV CJ.SDR DALA1248440932Skin · crackedDURING HMV, A CRACK WAS FOUND ON FUSELAGE SKIN FWD SERVICE DOOR FRAME AREA AFT LOWER SECTION STA Y=195. CUT OUT DAMAGE SKIN AND INSTALL DOUBLER TRIPLER FILLED IAW ER/A 504401-14AD.SDR DALA1248430932Door Frame · wornDURING HMV, WEAR WAS FOUND ON FWD SERVICE DOOR FRAME FWD LOWER SECTION BS 172. REPLACED LOWER SERVICE DOOR FRAME IAW ER/A 506610-14 REV ORIG AND SRM 53-05 FIG 55.
Back to N932DL, cancelled Sep 16, 2019