N139DL, cancelled May 10, 2017
Service difficulty reports · 87
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 = 'N139DL' AND deregistration_id = 'N139DL-2017-05-10' 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 = 'N139DL' AND deregistration_id = 'N139DL-2017-05-10' 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 DALA2016110108194Lens · damagedR1 EXTERIOR EMERGENCY LIGHT LENS DAMAGED. REPLACED LENS. SYSTEM OPERATION IS NORMAL.SDR DALA2016103107974Housing · looseL1 DOOR SLIDE HOUSING FOUND LOOSE AND REINSTALLED. SYSTEM OPS NORMAL.SDR DALA2016102807829Plate · damagedSLIDE INDICATION LIGHT INOPERATIVE. REPLACED BASE PLATE. SYSTEM OPERATION IS NORMAL.SDR DALA2016012800675Wire · cutLAVATORY DOOR L4 RED MOUNTED EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND WIRE CUT AT CARPET AND KICK PANEL IS LOOSE, FED TEMP WIRE THROUGH HOLE AND REPLACED LIGHT ASSEMBLY.SDR DALA2015100806009Support · damagedRIGHT WING OTBD T/E FLAP, THREE HOLES ON NR 7 SUPPORT 1-2-3 BEAM FASTNER HOLES HAS TOOLING DAMAGE. REPAIRED IAW ERA 539808-14.SDR DALA2015100105910Angle · crackedAT C-CHECK, BS 1809, RT OF HORIZONTAL ANGLE WL 257, BL 28, CRACKED AT FASTENER HOLE. ANGLE REPAIRED IAW SRM 53-80-08, REPAIR 10.SDR DALA2015082705238Lamp · inoperativeEMERGENCY SEAT MOUNTED LIGHT DAMAGED AT SEAT 12B. REPLACED BUMPER, SHROUD AND REPLACED THE LAMP. SYSTEM OPS NORMAL.SDR DALA2015060903950Filter · not reportedTHE CREW SHUTDOWN RT ENGINE IAW QRH DUE TO LOSS OF FUEL FROM RT TANK. CREW ALSO REPORTED A RT HYDRAULIC EICAS MESSAGE. REPLACED RT ENGINE FUEL FILTER. SYSTEM OPERATION IS NORMAL.SDR DALA2014081904603Skin · dentedDURING WALK AROUND, FOUND A DENT IN NR 4 SLAT ON LT WING. REPLACED THE SLAT.SDR DALA13018610139Connector · damagedSEAT EMERGENCY PATH LIGHTS FROM ROW 34-46AB ARE INOPERATIVE. MX RESET PIN 9 ON CONNECTOR D9048. SYS OPS IS NORMAL.SDR DALA13018620139Power Supply · inoperativeIN SEAT EMERGENCY PATH LIGHTING ROW 34AB-46 ARE INOPERATIVE. MX REPLACED THE POWER SUPPLY. SYS OPS IS NORMAL.SDR DALA1309870139Wire · looseDURING SERVICE CHECK, FOUND EMERGENCY LIGHTS INOPERATIVE FROM ROW 34AB. MX FOUND LOOSE CONNECTOR AT SEAT 33AB. SECURED WIRE AND CONNECTOR, SYS OPS IS NORMAL.SDR DALA1233060139Light · damagedEMERGENCY MOUNTED LIGHTING AT SEAT 37B DAMAGED AND INOPERATIVE. MAINTENANCE SECURED LIGHT MOUNTED. SYSTEM OPERATION IS NORMAL.SDR DALA1220810139Battery Pack · inoperativeDURING INSPECTION, EMERGENCY LIGHTING WAS FOUND INOPERATIVE FROM ROW 34 TO 45 ON THE RIGHT SIDE SEATS. MAINTENANCE REPLACED THE BATTERY PACK AT ROW 45. SYSTEM OPERATION IS NORMAL.SDR DALA1207770139Fairing · delaminatedRT WING I/B MAIN FLAP O/B FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 FIG 5 .SDR DALA1207760139Skin · dentedRT WING O/B FLAP T/E LOWER SURFACE IS DENTED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-06 FIG 9.SDR DALA1207750139Skin · delaminatedLT WING O/B FLAP UPPER SURFACE IS DELAMINATED JUST O/B OF THE NR 1 FLAP TRACK FAIRING AREA AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.SDR DALA1207740139Skin · delaminatedLT WING O/B FLAP T/E UPPER SURFACE IS DELAMINATED JUST I/B OF NR 2 FLAP TRACK FAIRING AREA AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.SDR DALA1207730139Skin · delaminatedRT WING O/B FLAP UPPER SURFACE IS DELAMINATED O/B OF THE NR 7 FLAP TRACK AREA AND REPAIRED PER THE B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.SDR DALA1207720139Skin · delaminatedRT WING O/B FLAP UPPER SURFACE IS DELAMINATED AT THE NR 7 FLAP TRACK AREA AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.SDR DALA1207710139Skin · delaminatedLT WING O/B FLAP UPPER SURFACE IS DELAMINATED APPROX 50" FROM I/B END AND REPAIRED PER B767-300 SRM 57-53-01. REPAIR 1 AND SRM 51-70-06 FIG 9.SDR DALA1207700139Skin · delaminatedRT WING O/B FLAP UPPER SURFACE IS DELAMINATED I/B OF THE NR 7 FLAP TRACK AREA AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-06 FIG 9 (NRC 50813).SDR DALA1207020139Fitting · defectiveNR 2 PYLON UPPER LINK PITCH LOAD FITTING T-CLIPS 112T7010-14 O/B AND 112T7010-16 I/B HAVE SHORT EDGE MARGIN AT FASTENER HOLES (NRC 52406).SDR DALA1207010139Fitting · defectiveNR 1 PYLON UPPER LINK PITCH LOAD FITTING T-CLIPS 112T7010-13 O/B AND 112T7010-15 I/B HAVE SHORT EDGE MARGIN (NRC 52405).SDR DALA1206980139Floorbeam · corrodedFS 1197 + 132 LBL 22 FLOORBEAM UPPER CHORD IS CORRODED AND REPLACED PER B767-300 SRM 51-10-02 PG 2 PARA 9 AND DWG 146T1229 SH 1.SDR DALA1206850139Sealant · crackedNR 1 PYLON UPPER SPAR FITTING AFT BUSHING SEALANT IS CRACKED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 2 FIG 201.SDR DALA1206830139Bushing · migratedNR 1 PYLON LWR AFT FITTING BUSHING MIGRATED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 4 FIG 201.SDR DALA1206820139Sealant · activatedNR 2 PYLON LWR SPAR FITTING AFT BUSHING SEALANT CRACKED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 4 FIG 201.SDR DALA1206800139Sealant · crackedNR 2 PYLON UPPER SPAR FITTING AFT BUSHING SEALANT IS CRACKED AND REPAIRED PER B767-300 SRM 54-51-90 REPAIR 2 FIG 201.SDR DALA1206050139Fairing · crackedRUDDER L/E FAIRING 324KL FOUND CRACKED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT CRACKED AREA AS PER B767-300 SRM 55-40-01 REPAIR 1 AND B767-300 SRM 51-70-06 FIGURE 9.SDR DALA1206040139Panel · damagedRT HORIZONTIAL STAB L/E PANEL 342DR INNER SURFACE DETACHED. METAL HOT BOND REPAIR PERFORMED ON DETACHED AREA AS PER B767-300 SRM 55-10-01 REPAIR 1 FIGURE 201 AND B767-300 SRM 51-70-10 REPAIR 4 FIGURE 202.SDR DALA1206030139Fairing · crackedRUDDER L/E FAIRING 324ML FOUND CRACKED. COMPOSITE PREPREG REPAIR CARRIED OUT AT CRACKED AREA AS PER B767-300 SRM 55-40-01 REPAIR 1 AND B767-300 SRM 51-70-04 FIGURE 9.SDR DALA1209440139Fastener · missingNR 1 PYLON HAS FASTENER MISSING. FASTENER INSTALLED ACCOMPLISHED AS PER VA81913AD REV A.SDR DALA1205960139Fastener · activatedNR 1 PYLON MOD ERA 38671-14AD DWG 624T0016 SHEET 1. PRODUCTION FASTENER MISSING; PRI ISSUED NO FINAL REPAIR DATA AT THIS TIME.SDR DALA1205950139Fastener · missingNR 2 PYLON MOD ERA 389672-14AD DWG 624T0016 SHEET 1. PRODUCTION FASTENER MISSING; PRI ISSUED FOR WORK TO CONTINUE NO FURTHER REPAIR DATA AT THIS TIME.SDR DALA1205940139Spar · misrepairedNR 1 PYLON FWD UPPER SPAR WEB; EXISTING REPAIR FASTENER PATTERN NOT SAME AS INDICATED IN SB767-54-008 REV 2 FIGURE 10. PRI REQUESTED FOR REPAIR. NO REPAIR DATA AT THIS TIME.SDR DALA1209480139Spar · misrepairedNR 1 PYLON FWD UPPER SPAR WEB MISREPAIRED. REPAIRED PER ERA 499056-14.SDR DALA1205540139Fairing · delaminatedRIGHT WING I/B MAIN FLAP LEADING EDGE O/B FAIRING FOUND DELAMINATED.SDR DALA1209980139Bulkhead · damagedNR 2 PYLON MIDSPAR AFT BULKHEAD AREA FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 INDICATED. REPAIRED PER ERA 499052-14AD REV ORIG.SDR DALA1209960139Bulkhead · damagedNR 1 PYLON MIDSPAR AFT BULKHD AREA FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 INDICATES. REPAIRED PER ERA 499052-14AD REV ORIG.SDR DALA1209470139Bulkhead Web · crackedNR 1 PYLON AFT BULKHEAD LEFT MID SPAR FITTING AFT BULKHEAD WEB CRACKED APPROX 1/16". CRACK REPAIRED PER ERA 499059-14AD REV ORIG.SDR DALA1205390139Bulkhead · crackedNR 1 PYLON AFT BULKHEAD LT MID SPAR FTG AFT BLKHD WEB NR 2 FASTENER HOLE CRACK APPROX 1/16 INCH.SDR DALA1204900139Bulkhead · damagedNR 2 PYLON MID SPAR AFT BULKHEAD AREA EXISTING FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 ST 1 INDICATES.SDR DALA1204890139Bulkhead · damagedNUMBER 1 PYLON MID SPAR AFT BULKHEAD AREA EXISTING FASTENER HOLES LARGER THAN SB 767-54-0081 REV 1 DWG 624T0016 ST 1.SDR DALA1204910139Skin · bulgedRT WING 11 L/E SLAT WEDGE SKIN FOUND BULGED. HOT METAL BOND REPAIR PERFORMED ON AREA AS PER SRM 57-43-02 REPAIR 1 FIGURE 201 AND SRM 51-70-10 REPAIR 4 FIG 202.SDR DALA1204860139Skin · corrodedCORROSION FOUND AFT CARGO INTERIOR FUSELAGE SKIN AT FS 1077 STRINGER 39L.SDR DALA1204850139Skin · corrodedCORROSION FOUND AFT CARGO INTERIOR SKIN AREA FS STA 1077 FROM STRINGER 39L TO 39R. CP53-151-02I/CP53-152-02I (NRC 51757)SDR DALA1204840139Fairing · crackedDURING HMV 3 VISIT FOUND RT WING INBOARD MAIN FLAP OUTBOARD LEADING EGDE FAIRING CRACKED. COMPOSITE REPAIR CARRIED OUT AS PER B767-300 SRM 57-53-01 REPAIR 1 AND SRM 51-70-05 PAR 5.A(1).SDR DALA1209970139Frame · crackedMAIN DECK BS 903 RBL 89 FRAME CRACKED. REPAIRED PER ERA 499047-14AD REV ORIG SECT 1.SDR DALA1209840139Frame · crackedMAIN DECK BS 903 LBL 89 FRAME CRACKED. REPAIRED PER ERA 499046-14AD REV ORIG.
Back to N139DL, cancelled May 10, 2017