N58101
Service difficulty reports · 128
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 = 'N58101' 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 = 'N58101' 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 CALA2009061200306Door Frame · crackedB757-53-3-0357, FWD ACCY ACCESS DOOR FRAME FWD FRAME HAS DAMAGE ON FRAME FROM DOOR PIN APPROX STA 224. CUT OUT DAMAGED AREA AND REPAIRED DOOR FRAME WEB REF ECRA 5313- 01036. ACCOMPLISH A PERMANENT REPAIR WITHIN 12 MONTHS. PLANNING TO CONTACT ENGINEERING AFTSDR CALA2009060400300Skin · corrodedSUPPORT TASK CARD CORROSION ON CENTER TANK BOX UPPER SKIN UNDER MAIN FRAME AT WING SLICE STATION 960 RIGHT. REPAIRED CENTER FUEL TANK UPPER SKIN REF ECRA 5730-02555 REV A.SDR CALA2009060400299Skin · corrodedSUPPORT TASK CARD CORROSION ON CENTER TANK BOX UPPER SKIN UNDER MAIN FRAME AT WING SLICE STATION 960 LEFT. INSTALLED STUB BEAM AT STA 960 LEFT REF ECRA 5730-02555 REV A.SDR CALA2009060400298Skin · corrodedSUPPORT TASK CARD CORROSION ON CENTER TANK BOX UPPER SKIN UNDER MAIN FRAME AT WING SLICE STATION 980 LEFT. INSTALLED STUB BEAM AT STA 980 LEFT REF ECRA 5730-02555 REV A STEP 1 THROUGH 15.SDR CALA2009060300297Skin · corrodedSUPPORT TASK: CORROSION ON CENTER TANK BOX UPPER SKIN UNDER MAIN FRAME AT WING SPLICE STATION 980 RIGHT. REMOVED CORROSION, SHOT PEENED, TREATED AND RESEALED REWORKED AREA PER EC/RA 5730-02555, REV A.SDR CALA2009060200295Floorbeam · corrodedSUPPORT TASK MAIN CABIN FLOORBEAM AT STA 1640 RBL 56 FOUND TO BE OUT OF LIMITS AFTER CORROSION REMOVAL. INSTALLED REPAIR ANGLES, STRAPS AND T-CHORD ON FLOORBEAM STA 1640 RBL 38-66 PER SRM 53-00-01.SDR CALA2009052700282Floorbeam · corrodedSUPPORT TASK: CABIN FLOORBEAM UPPER CORD HAS CORROSION STA 1640 LBL 30 TO RBL 20. REPAIRED FLOORBEAM REF SRM 53-00-51 REPAIR 3.SDR CALA0800794Fuse · blownSEAT PATH LIGHTS OUT FROM SEAT 25 ABC TO LAST SEAT ROW WHEN EMERGENCY LIGHTS TESTED. FOUND BATTERY CHARGER FUSE BLOWN LOCATED AT AFT CABIN CEILING M736. REPLACED FUSE P/N 76005 PER CHAPTER 20 WIRE PRACTICES AND W/D 33-51-22, PG 902 SHT 1. OPERATIONAL CHECKSSDR CALA0700664Shade · burnedTHE FLIGHT CREW INDICATED THEY SAW AND SMELLED SMOKE IN THE CABIN AREA WITH LIGHTS ON DIM WHILE AT CRUISE. LIGHTS WERE TURNED OFF AND THE SMOKE AND ODOR DISSIPATED. THE FLIGHT WAS CONTINUED WITHOUT FURTHER PROBLEM. TROUBLESHOOTING BY MAINTENANCE FOUND THE LTSDR CALA0700008Lever · brokenTHE RIGHT OFF WING ESCAPE SYSTEM DISABLE LEVER AT RIGHT EMERGENCY EXIT HATCHES WOULD NOT MOVE FROM THE DISABLED POSITION TO THE ARMED POSITION. THE DISABLE LEVER ASSEMBLY WAS FOUND BROKEN. A NEW DISABLE LEVER WAS INSTALLED IAW MM 25-60-11. OPERATIONAL CHECKSDR CALA0600539Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER SURFACE CORRODED AT STA 377, LBL 36. THE CORRODED SECTION OF FLOORBEAM WAS CUT OUT AND SUPPORT ANGLES AND STRAPS WERE INSTALLED IAW SRM 53-00-51, REPAIR 1.SDR CALA0400318Slide · out of rigCARRIER DEPLOYMENT WAS INTERMITTENT DURING RIGHT OFF WING SLIDE DEPLOYMENT FUNCTION TEST. THE RIGHT OFF WING SLIDE DOOR WAS RIGGED AND ADJUSTED IAW MM 25-65-09, PARAGRAPH 3D, ITEMS 9-14.SDR CALA0400311Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 378, RBL 10. REPAIRED IAW ECRA 5320-01747.SDR CALA0400310Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER SURFACE CORRODED AT BS 700, LBL 58.2. REPAIRED IAW ECRA 5320-01746.SDR CALA0400309Floorbeam · corrodedINSPECTION FOUND TOP SURFACE OF FLOORBEAM CORRODED AROUND FASTENER HOLES AT BS 1640, BL 0 TO LBL 24.5. REPAIRED IAW ECRA 5320-01749.SDR CALA0400308Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AT BS 680, RBL 16 TO LBL 16. REPAIRED FLOORBEAM IAW SRM 53-00-51, FIGURE 203.SDR CALA0400307Intercostal · corrodedINSPECTION FOUND FLOORBEAM INTERCOSTAL CORRODED AT BS 684, RBL 15. THE INTERCOSTAL WAS REPLACED IAW SRM 51-40-02, FIGURE 12.SDR CALA0400292Wire · chafedMAINTENANCE NOTICED SMOKE WHEN POWERING UP THE AIRCRAFT TO ACCOMPLISH A GEAR SWING WHILE THE AIRCRAFT WAS IN HEAVY CHECK AT YXX. WHEN MAINTENANCE FOUND THE SOURCE OF THE SMOKE THE FIRE HAD SELF EXTINGUISHED. EVIDENCE OF FIRE EXISTED FROM THE HEAT DAMAGE AND SDR CALA0400288Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT FASTENER HOLE, BS 377.7, LBL 58, WBL 208.10. REPAIRED IAW SRM 53-00-51.SDR CALA0400287Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 365, RBL 18. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203.SDR CALA0400276Actuator · inoperativeTHE RIGHT OFF WING ESCAPE SLIDE CARRIER DID NOT DEPLOY WHEN 1500 PSI NITROGEN WAS APPLIED DURING TESTING. MAINTENANCE FOUND THE RIGHT WING ESCAPE SLIDE ACTUATOR AT FAULT. THE ACTUATOR WAS REMOVED AND REPLACED AND A FUNCTIONAL CHECK WAS PERFORMED IAW MM 25-65SDR CALA0300386Engine · shutdownTHE NR 2 ENGINE AUTO SHUTDOWN WITH OIL LOSS AND OIL PRESSURE DROP WHILE EN ROUTE FROM LIM TO EWR. THE AIRCRAFT DIVERTED TO MBJ WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WILL BE REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDSDR CALA0300228Smoke · detectedENROUTE FROM EWR TO LIM THE AIRCRAFT DIVERTED TO GCM FOR SMOKE IN THE CABIN. NO EICAS MESSAGES DISPLAYED. PERFORMED FIM FOR OVERBOARD EXHAUST VALVE AND COOLING TEST. NO PROBLEMS NOTED. INSPECTED RECIRC FANS (LEFT AND RIGHT), INSPECTED AND CLEANED ALL SMOKE DETSDR CALA0100362Spar · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LT HORIZONTAL STABILIZER LEADING EDGE LOWER CHORD/AUX SPAR AT FSS 155.849. THE AREA WAS REPAIRED IAW ECRA 5512-01003.SDR CALA0100317Actuator · wornINSPECTION FOUND HORIZONTAL STABILIZER ACTUATOR GIMBAL WORN BEYOND LIMITS. THE ACTUATOR WAS REMOVED AND REPLACED IAW MM 27-41-10.SDR CALA9801924Skin · dentedINSPECTION FOUND A DENT IN AFT CARGO DOOR EXTERNAL SKIN AT LOWER FORWARD CORNER. THE SKIN WAS REPAIRED IAW SRM 52-30-01, PAGE 209.SDR CALA9701384Bleed Controler · inoperativeTHE NR 2 ENGINE FLAMED OUT WHILE ON FINAL APPROACH. ALL APPROPRIATE CHECKLISTS WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT BLEED VALVE CONTROLLER TO BE AT FAULT. THE CONTROLLER WAS REMOVED AND REPLACED IAW MM 75-32-SDR CAL960061Oil Pump · inoperativeIAH - FLT 0602 - WHILE OPERATING THE APU WITH THE NR 2 GENERATOR PLACARDED INOPERATIVE, THE APU OIL QUANTITY STATUS ADD MESSAGE CAME ON EN ROUTE TO IAH. THE APU SHUT DOWN AUTOMATICALLY SHORTLY BEFORE LANDING. MAINTENANCE FOUND THE APU OIL PUMP AT FAULT. THE
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