N59053
Service difficulty reports · 93
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 = 'N59053' 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 = 'N59053' 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 CALA2017060901770Socket · dirtyEXT EMER SLIDE LIGHT DOOR R3 INOP, RELAMP NO HELP. CLEANED SOCKET AND RELAMPED R3 DOOR SLIDE LIGHT IAW AMM 33-51-06 . OPS CHK GOOD.SDR CALA2017060901769Socket · dirtyEXT EMER SLIDE LIGHT DOOR L3 INOP, RELAMP NO HELP. CLEANED SOCKET AND RELAMPED L3 DOOR SLIDE LIGHT IAW AMM 33-51-06 . OPS CHK GOOD.SDR CALA2017021700380Bulb · inoperativeR3 DOOR SLIDE EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-51-06. OPS CHECHED GOOD.SDR CALA2016122601171Floorbeam · corrodedBS 325, RBL 33 - 55 FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 ALLOWABLE DAMAGE 1, FIG 101. REPAIRED IAW SRM 53-00-51, REPAIR 2, FIG 201.SDR CALA2016122601170Floorbeam · corrodedBS 347 RBL 24-48 FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 ALLOWABLE DAMAGE 1, FIG 101. REPAIRED IAW SRM 53-00-51, REPAIR 2, FIG 201.SDR CALA2016122601169Floorbeam · corrodedBS 325 LBL 22 TO 54 FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.SDR CALA2016122601168Floorbeam · corrodedBS 303, LBL 11 TO 53, FLOORBEAM UPPER TEE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02, AND FOUND OUT OF LIMITS IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.SDR CALA2016090600627Actuator · inoperativeCREW REPORTED APU DOOR STATUS MESSAGE IN FLIGHT WITH NOTICEABLE VIBRATION & BUFFETING. APU WOULD NOT START. REMOVED APU INLET DOOR ACTUATOR IAW AMM 49-15-06. INSTALLED APU INLET DOOR ACTUATOR IAW AMM 49-15-06 UP TO STEP G(1)(J).SDR CALA2015042000295Battery Pack · dischargedFOR SDR REPORTING R4 & L4 EMER LIGHTS IN OPERATION. R & R EMER LIGHT BATTERY PACK AT 4R DOOR FLIGHT ATTENDANT SEAT. OPERATIONS TESTED GOOD IAW AMM 33-51-07. PN INSTALLED AD-D717-01-100, SN 155504, 29-3351-3-001 3.SDR CALA2014121801541Shutoff Valve · failedON TAKEOFF ROLL, LT ENG BLEED OFF, EICAS MSG. AFTER DEPARTURE RAN QRH V LIST, LIGHT REMAINED ILLUMINATED. NOTICED RESIDUAL BLEED AIR OF 15 PSI ON LT SIDE WITH LT ENG BLEED OFF. ALSO LT BLEED HPSOV STATUS MSG. ACCOMPLISHED ASCTU BITE PROCEDURE IAW MM 36-23-SDR CALA2014110501420Unknown · odorON CLIMB OUT HAD LIGHTNING STRIKE ON NOSE WITH STRONG ELEC SMELL. PREFORMED LIGHTNING INSPECTION IAW 05-51-19-212-001.SDR CALA2014052800685Shutoff Valve · failedRIGHT ENG BLEED LIGHT CAME ON DURING TAKEOFF ALONG WITH RT REVERSER ISOLATION VLV. IAW NR 4712443 FOR R & R OF HPSOV, PERFORMED AIR SUPPLY DISTRIBUTION SYS TEST IAW 36-11-00-715-029-0-01, SYS CHECKED NORMAL AT THIS TIME, NO DEFECTS NOTED.SDR CALA2014020700167Battery Pack · dischargedB767-33-3-0006 CABIN FWD ZONE SEAT PROXIMITY EMERGENCY LIGHT FOUND NOT ILLUMINATED. EMERGENCY LIGHT BATTERY REPLACED & OPERATION TESTED NORMAL IAW AMM 33-51-07.SDR CALA2014020700166Light · defectiveIAW B767-33-3-0006 CABIN SEAT 1D FWD POSITION EMERGENCY LIGHT DIM. SEAT 1D FWD POSITION EMERGENCY LIGHT LAMP REPLACED & LAMP TEST NORMAL IAW AMM 33-51-10.SDR CALA2012082400529Charger · inoperativeEMERGENCY LIGHT BATTERY CHARGER M1210, STA 1545 DR, 4R SELF TEST FUNCTION INOPERATIVE. R & R BATTERY CHARGER, OPS CHECKED NORMAL.SDR 2011FA0000569Brake · fracturedAFTER ACFT DEPARTURE, THE AIRPORT AUTHORITY FOUND SEVERAL BRAKE DEBRIS ON THE INNER TAXIWAY NEAR THE POSITION 17. THE DEBRIS HAVE BEEN GIVEN TO OUR LINE MX PERSONNEL, AND HAVE MX STORE. FOLLOWING THIS QUICK INVESTIGATION, IT APPEARS THAT THE BRAKE DISK AND PSDR CALA2011032400179Floorbeam · corrodedCABIN: STA 303 LBL 30 TO 40 FLOORBEAM DOUBLER CORROSION FOUND. CABIN: STA 303 LBL 30 TO LBL 40 FLOORBEAM DOUBLER COR BLEND OUT D 0.020"(ORG 0.063") OUT OF SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101 LIMIT AND FLOORBEAM UPPER CHORD AND DOUBLER REPAIRED AS PER SRSDR CALA2011032400178Floorbeam · corrodedCABIN: STA 325 LBL 48 TO 53 FLOORBEAM CORROSION FOUND. CABIN STA 325 LBL 48 TO 53 FLOORBEAM CORRODED BLEND OUT D0.037" (ORG 0.090") OUT OF SRM 53-00-51 ALLOWABLE DAMAGE, FIG 101 LIMIT AND COR FLOORBEAM REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND FORM 44SDR CALA2011020900076Floorbeam · corrodedCABIN STA 325 LBL 30 TO 51 FLOORBEAM DOUBLER CORROSION FOUND. CABIN STA 325 LBL 30 TO 51 FLOORBEAM DOUBLER CORROSION BLEND OUT D:0.018 (ORG 0.063) OUT OF SRM 53-00-51 ALLOWABLE DMG 1 FIG 101 LIMIT AND DOUBLER REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 WORKSDR CALA2011020900075Floorbeam · corrodedCABIN STA 303 LBL 51 TO 55 FLOORBEAM UPPER CHORD CORROSION FOUND. STA 303 LBL 51 TO 55 FLOORBEAM UPPER CHORD CORROSION BLEND OUT D:0.036 (ORG 0.090") OUT OF SRM 53-00-51 ALLOWABLE DMG FIG 101 LIMIT AND FLOORBEAM UPPER CHORD REPAIRED AS PER SRM 53-00-51 REPAIRSDR CALA2011020900074Splice Plate · corrodedCABIN STA 325 RBL 38 TO 41 FLOORBEAM SPLICE PLATE CORRODED. STA 325 RBL 38 TO 41 FLOORBEAM SPLICE PLATE CORROSION BLEND OUT D:0.019" (ORG.063") OUT OF SRM 53-00-51 ALLOWABLE DMG 1 FIG 101 LIMIT AND SPLICE PLATE REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 WOSDR CALA2011032400182Seat Track · corrodedCABIN STA 1222-1351 RBL 88.5 SEAT TRACK CORROSION FOUND. CABIN STA 1222-1351 RBL 88.5 SEAT TRACK CORROSION BLEND OUT D:0. 038" W:0.8" L:2.5" OUT OF SRM 53-00-52 ALLOWABLE DAMAGE FIG 101 LIMIT AND SEAT TRACK REPAIRED AS PER ECRA 5320-02010 AT STA 1219 TO STA 1SDR CALA2011032400181Floor Support · corrodedCABIN STA 301 TO 304 LBL 84 FLOOR SUPPORT CORROSION FOUND. CABIN FLOOR SUPPORT CORROSION BLEND OUT D:0.047" (ORG.0063") OUT OF SRM 53-00-15 ALLOWABLE DMG FIG 101 LIMIT AND CORRODED FLOOR SUPPORT REPLACED AS PER SRM 51-10-02 AND NEW FLOOR SUPPORT INSTALLED AS SDR CALA2011032400180Seat Track · corrodedCABIN: BS 1480 LBL 55 SEAT TRACK BASE CORRODED. CABIN BS 1480 LBL 55 SEAT TRACK BASE CORROSION BLEND OUT D:0.036" OUT OF SRM 53-00-52 ALLOWABLE DMG 1 FIG 101 LIMIT AND CORRODED SEAT TRACK REPLACED AS PER SRM 51-10-02 AND NEW SEAT TRACK INSTALLED AS PER SRM 5SDR CALA2011031600148Seat Track · corrodedCABIN RBL 88 STA 1386 TO 1390 SEAT TRACK CORROSION FOUND. CABIN RBL 88 STA 1386 TO 1390 SEAT TRACK CORROSION BLEND OUT D :0.035 OUT OF SRM 53-00-52 ALLOWABLE DMG 1 FIG 101 LIMIT AND CORRODED SEAT TRACK REPAIRED AS PER ECRA 5320-02010 AT STA 1219 TO STA 1417 RSDR CALA2010043000182Stiffener · crackedSUPPORT TASK FCD 5420-01488 NR 2 PYLON NAC STA 285 I/B STIFFENER FOUND CRACKED. NR 2 PYLON NAC STA 285 I/B STIFFENER REPLACED AND INSTALLED AS PER FCD5420-01488 STEP 6 AND BOEING DWG 311T2400.SDR CALA2010043000181Stiffener · crackedSUPPORT TASK FCD 5420-01488 NR 2 PYLON NAC STA 285 O/B STIFFENER FOUND CRACKED. NR 2 PYLON NAC STA 285 O/B STIFFENER REPLACED AS PER FCD5420- 01488 STEP 6 AND BOEING DWG 311T2400, AND INSTALLED AS PER FCD 5420-01488 STEP 6 AND BOEING DWG 311T2400.SDR CALA2010043000180Stiffener · crackedSUPPORT TASK FCD5420-01487 NR 1 PYLON NAC STA 285 O/B STIFFENER FOUND CRACKED NR 1 PYLON NAC STA 285 O/B STIFFENER. REPLACED AND INSTALLED AS PER FCD5420-01487 STEP 6 AND BOEING DWG 311T2400.SDR CALA2009030400123Contact · corrodedR-3 DOOR EXTERIOR EMERGENCY LIGHTS NOT WORKING. FOUND CORROSION ON R-3 DOOR EXT EMERGENCY LIGHT CONTACTS. CLEANED LIGHT ASSY CONTACTS PER 33-51-06.SDR CALA2009030400122Contact · corrodedR-4 DOOR EXTERIOR EMERGENCY LIGHTS NOT WORKING. FOUND CORROSION ON R-4 DOOR EMERGENCY LIGHT CONTACTS. CLEANED CONTACTS PER 33-51-06.SDR CALA2009030400121Contact · corrodedL-4 DOOR EXTERIOR EMERGENCY LIGHTS NOT WORKING. FOUND CORROSION ON EMERGENCY LIGHT CONTACTS AT L-4 DOOR. CLEANED CONTACTS PER PER 33-51-06.SDR CALA2009030400120Contact · corrodedL-3 DOOR EXTERIOR EMERGENCY LIGHTS ARE NOT WORKING. L-3 DOOR EMERGENCY LIGHT ASSY FOUND WITH CORROSION ON LIGHT CONTACTS. CLEANED CONTACTS PER 33-51-06.SDR CALA0800209Stiffener · crackedFX FLOORBEAM STIFFENER FOUND CRACKED AT BS 246 LBL 40 FWD SIDE. FX FLOORBEAM BS 246 LBL 40 FWD SIDE STIFFENER REPAIRED AS PER ECRA5310-04723 AND HFEC , NO CRACK FOUND.SDR CALA0800192Floorbeam · corrodedSTA 325 LBL 22 TO 50 FLOOR SUPPORT FOUND CORROSION. REPAIRED PER SRM 53-00-51.SDR CALA0800189Floor Support · corrodedCABIN STA 303 LBL 20 TO 40 FLOOR SUPPORT FOUND CORROSION. REPAIR PER SRM 53-00-51.SDR CALA0700602Charger · inoperativeTHE EMERGENCY PATH LIGHT AT SEATS 5, 6 AND 7 WOULD NOT ILLUMINATE. THE EMERGENCY POWER SUPPLY D21296 WAS REMOVED AND REPLACED IAW AMM 33-51-07.SDR CALA0700360Battery · inoperativeTHE R-4 DOOR FWD EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. THE FLASHLIGHT BATTERY WAS REPLACED.SDR CALA0500383Rib · crackedINSPECTION FOUND A 0.025 INCH CRACK IN RT WING IB AILERON IB HINGE RIB SUPPORT AT AFT HI-LOK AREA, WS 467.8. THE CRACKED AREA WAS TRIMMED OUT AND A REPAIR WAS INSTALLED IAW ECRA 5740-02094.SDR CALA0500381Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 325, LBL 48 - RBL 45. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201.SDR CALA0500380Floor Support · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 303-325, LBL 22-34. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.SDR CALA0300705Actuator · brokenTHE LANDING GEAR DISAGREE AND GEAR DOOR DISAGREE EICAS MESSAGES CAME ON AFTER TAKEOFF FROM GRU. THE GEAR WAS CYCLED TWICE WITH NO CORRECTION. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO GRU WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING PER MM 32-32SDR CALA2000278Computer · malfunctionedAT 90 KNOTS LOST ALL OIL PRESSURE ON LEFT ENGINE. REJECTED TAKEOFF. REPLACED RT DATA CONCENTRATOR UNIT PER MM 31-63-06, PG 401. LOADED SOFTWARE IAW MM 31-63-06, PG 201.SDR CALA0100427Gcu · failedRIGHT GENERATOR CONTROL OFF LIGHT CAME ON IN FLIGHT. STARTED APU BUT APU GENERATOR OFF LIGHT CAME ON. REPLACED RIGHT GENERATOR CONTROL UNIT.
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