N502DA
Service difficulty reports · 76
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 = 'N502DA' 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 = 'N502DA' 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 DL72L954075Battery Pack · dischargedON LAYOVER, FOUND AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK OPERATION NORMAL.SDR DL72L953338Skin · gougedDURING INSPECTION, AN APPROXIMATE 4.25 BY 3.25 CUTOUT WAS MADE IN THE SKIN TO REMOVE DAMAGE FROM GOUGE. MAINTAINING SCHEDULE OF THE A/C, A TIME LIMITED REPAIR WILL BE INSTALLED AND THE PERM REPAIR WILL BE ACCOMPLISHED AT NEXT HMV IN ACCORDANCE WITH B727 SRM 5SDR DL72L952294Rib · crackedUPON INSPECTION, RIB NR 11 FOUND CRACKED IN LWR FWD CORNER. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT.SDR DL72L952293Rib · crackedUPON INSPECTION, A CRACK WAS FOUND IN THE LOWER FWD CORNER OF NR 10 RIB. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT.SDR DL72L952292Heat Shield · crackedUPON INSPECTION, A CRACK WAS FOUND IN HEAT SHIELD BETWEEN RIBS 11 AND 12, AND BETWEEN RIBS 12 AND 13. REPAIRED PER MM 57-54-0, FOR NR 7 L/E SLAT.SDR DL72L952262Rib · crackedUPON INSPECTION BY MAINT. RIB NR 11 IN NR 7 L/E SLAT WAS FOUND CRACKED. REPAIRED PER MM 57-54-0.SDR DL72L952074Rib · cracksFOUND CRACKS ON RIBS NR 13 AND NR 14 DURING SHOP INSPECTION OF NR 7 L/E SLAT. REPAIRED PER SRM 57-54-00.SDR DL72L951768Skin · corrodedFOUND ON CV2 CHECK, CORROSION ON SKIN FOUND UPON REMOVAL OF STR SPLICE ON STA 1010 REF N/R 127. REPAIRED SKIN PER SRM 53-30-3 FIG 3A AND ID PER PS 900-5-1 FIG 4.SDR DL72L951955Gusset · crackedTHE RT TORQUE BOX HORIZONTAL BEAM GUSSET AT FS 1273 WAS FOUND CRACKED. REPAIRS WERE ACCOMPLISHED PER S/B 53-0129.SDR DL72L951767Stringer · corrodedFOUND ON CV2 CHECK, CORROSION ON TOP OF STR 30 BETWEEN STA 1148 AND 1166 BL 0. REPAIRED AS PER SRM 53-10-3 AND ID PER PS 900-5-1 FIG 4.SDR DL72L951729Intercoastal · corrodedFOUND ON CV2 CHECK, CORROSION ON LWR LEG OF INTERCOSTAL AFT OF STA 680 I/B OF STR 26R. REPAIRED PER SRM 51-40-3.SDR DL72L951728Floorbeam · corrodedFOUND ON CV2 CHECK, FLOORBEAM STA 1166 LBL 47 WITH CORROSION DAMAGE. REPAIRED PER SRM 53-10-8.SDR DL72L951665Former · crackedFOUND ON CV2 CHECK, 1 INCH CRACK ON STATION 480 FORMER ABOVE STRINGER 27L. REPAIRED PER SRM 51-40-3.SDR DL72L951664Clip · corrodedFOUND ON CV2 CHECK, CORROSION ON SKIN CLIP AT STA 500 BETWEEN STR 28R AND 27R. REPAIRED PER M/M 53-11-0.SDR DL72L951663Clip · corrodedFOUND ON CV2 CHECK, CORROSION ON AFT SIDE OF FORMER AT STATION 500, JUST INBD OF 27R. REPAIRED AS PER M/M 53-11-0 AND CHECKED LIMIT PER SRM 53-10-1.SDR DL72L951662Clip · corrodedFOUND ON CV2 CHECK, CORROSION AT SKIN CLIP STA 1030 BETWEEN S29R AND 28R. REPAIRED PER M/M 53-11-0 AND IDENT PR 8.7 900-5-1 FIG 4.SDR DL72L951661Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION ON L/T OUTBD SEAT TRACK JUST AFT OF STA 344. REPAIRED PER M/M 53-20-11.SDR DL72L951660Seat Track · corrodedFOUND ON CV2 CHECK, CORROSION ON L/T INBD SEAT TRACK JUST AFT OF STA 344. REPAIRED PER M/M 53-20-11.SDR DL72L951774Bracket · crackedFOUND ON CV2 CK, .5 INCH VISIBLE CRACK ON NR 6 L/E FLAP ACTUATOR O/B ATTACH BRACKET IN LOWER RADIUS. REPAIRED PER M/M 57-20-21 PAR 12.SDR DL72L951736Flange · crackedFOUND ON CV2 CHECK, CRACKED FLANGE STA 1342.4 WHERE LOWER EDGE OF FWD COWLS MATES WITH FUSELAGE AT PREVIOUS REPAIR (6 O'CLOCK POSITION). REPAIRED PER M/M 53-11-0 PG 801 IDENTIFY REPAIR AS PERMANENT REPAIR PER PS 900-5-1 NR 4.SDR DL72L951735Foreflap · crackedFOUND ON CV2 CHECK, 1 INCH CRACK ON NR 3 FOREFLAP ABOVE NR 6 FLAPTRACK CARRIAGE. REPAIRED AS PER SRM 57-50-4.SDR DL72L951734Foreflap · crackedFOUND ON CV2 CHECK, 1 INCH CRACK ON NR 4 FOREFLAP ABOVE NR 7 FLAPTRACK. REPAIRED AS PER SRM 57-50-4.SDR DL72L951730Rib · crackedFOUND ON CV2 CHECK, (1) .25 INCH VISIBLE CRACK ON NR 5 SLAT L/E RIB O/B OF ACTUATOR ROD. (2) 2.0625 INCH CRACKS ON NR 5 SLAT L/E RIB I/B OF ACTUATOR ROD. REPAIRED PER M/M 57-54-0 PAR 3.SDR DL72L951702Stiffener · crackedFOUND ON CV2 CHECK, CRACK IN STIFFENER STA 1400 OVERHEAD OF NR 2 ENGINE COMPARTMENT SECTION. REPAIRED PER SRM 54-10-3 AND IDENTIFIED PER PS 900-5-1 FIG 4.SDR DL72L950625Nose Rib · crackedFOUND DURING C-2 LETTER CHECK, NR 7 SLAT I/B ACTUATOR NOSE RIB CRACKED .1250 INCH. REPAIRED PER B727 MM 57-54-0 PG 803.SDR DL72L950511Skin · punctureDURING SHOP INSPECTION, NR 1 ENGINE NOSE COWL OUTER SKIN WAS FOUND WITH PUNCTURE DAMAGE AT 7 O'CLOCK POSITION. REPAIRED PER SRM 54-30-3.
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