N360NB
Service difficulty reports · 179
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 = 'N360NB' 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 = 'N360NB' 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 DALA13073183160Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 262FF SKIN DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. REPLACED FLOOR PANEL IAW SRM 51-72-11.SDR DALA13073173160Floor Panel · damagedMAIN CABIN FLOOR PANEL 222FF HAS EDGE DAMAGE. REPLACED FLOOR PANEL IAW SRM 51-72-11.SDR DALA13073163160Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT -Y254 BETWEEN FRAMES 16-20 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15, FIG. 107. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.SDR DALA13072123160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT Y1292 BETWEEN FRAMES 64-66 HARD POINT HOLES AND UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.SDR DALA13072113160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT Y1292 BETWEEN FRAMES 68-69 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.SDR DALA14003713160Skin · chafedL2 DOOR, UPPER FWD CORNER OF THE FUSELAGE DOOR FRAME, EXTERNAL SURFACE, CHAFED. BLENDED AREA IAW SRM 51-73-00. FOUND WITHIN LIMIT IAW SRM 53-41-11, FIG 106.SDR DALA13072093160Beam · corrodedLEFT AFT PASSENGER DOOR SILL BEAM UPPER FLANGE AT AFT FRAME 66 INBD GIRT BAR FITTING HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, L=1.5", W=1", D=0.080", FOUND OUTPUT OF LIMIT IAW SRM 53-41-14, FIG 101. R & R DOOR SILL IAW SRM 51-42-11 AND DWG DSDR DALA13071623160Seat Track · corrodedFORWARD CABIN SEAT TRACK -Y765 BETWEEN FRAMES 20-22 CROWN CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 101. R & R SEAT TRACK IAW SRM 51-42-11 & TRM 53-21-01.SDR DALA13071613160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT -Y1292 BETWEEN FRAMES 64- 66 UPPER FLANGE AND HARD POINT HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, PAR 3D. R & R FLOOR SUPPORT IAW TRM 53-21-00 & SRM 51-42-11 AND SRSDR DALA13071603160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT -Y1292 BETWEEN FRAMES 68-69 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15, P3.D. R & R FLOOR SUPPORT IAW TRM 53-21-00 & SRM 51-42-11 AND SRM 51-44-11.SDR DALA13071593160Frame · corrodedUPON REMOVAL OF RT SIDE SHEAR PLATE BETWEEN FRAMES 69-70 FOUND SUPPORT FRAME CORRODED. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE LIMITS ESTABLISH ON SRM. R & R SUPPORT FRAME IAW SRM 51-42-11 AND DWG D53474180.SDR DALA13071583160Shear Plate · corrodedAFT UTILITY AREA RT SIDE BETWEEN FRAMES 69-70, S23R SHEAR PLATE CORRODED. REMOVED CORROSION IAW SRM 51-74-00, CHECK LIMITS DIMENSION L=5.8", W=2.7", D=.039". NO ESTABLISH LIMITS FOUND IN SRM, R & R SHEAR PLATE IAW SRM 51-42-11 AND DWG D53474180.SDR DALA13071573160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT -Y1292 BETWEEN FRAMES 66-68 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 51-41-15 PAR. 3D. R & R FLOOR SUPPORT IAW TRM 53-21-00 & SRM 51-42-11 AND SRM 51-44-11.SDR DALA13071563160Sill · corrodedLEFT AFT PASSENGER/CREW DOOR SILL BEAM AT FWD FR68 CORNER FITTING HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, CHECKED LIMITS DIMENSION L=1", W=.500", D=.039". NO LIMIT ESTABLISHED FOR SRM, LOCATED AND DRILLED NEW CORNERS FITTING IAW SRM 51-44-11. INSSDR DALA13071553160Floor Support · corrodedFWD UTILITY AREA FLOOR SUPPORT -Y1292 BETWEEN FRAME 18 - 20 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-15, FIG 104. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.SDR DALA13071543160Floor Support · corrodedFWD UTILITY AREA FLOOR SUPPORT, Y503.2 BETWEEN FRAMES 12-16 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-11-14, FIG 105. R & R FLOOR SUPPORT IAW TRM 53-21-01.SDR DALA13071533160Floor Support · corrodedAFT UTILITY AREA FLOOR SUPPORT Y765 AT FR 68 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.SDR DALA13071523160Floor Support · corrodedFORWARD UTILITY AREA FLOOR SUPPORT Y254 BETWEEN FRAMES 16-20 UPPER FLANGE HAS SCRIBE LINE AND CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.SDR DALA13070753160Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM, Y1292 AT FRAME 68 UPPER INBD SPLICE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. REMOVED AND INSTALLED SPLICE.SDR DALA13070743160Floorbeam · corrodedAFT UTILITY AREA FLOORBEAM Y1292 AT FRAME 68 UPPER INBD SPLICE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. REMOVED & INSTALLED.SDR DALA13070733160Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT, Y189 BETWEEN FRAMES 20-22, UPPER SURFACE FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-17. REMOVED FLOOR SUPPORT IAW SRM 51-42-11 & INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11 ANDSDR DALA13070723160Lug · gougedRT WING SLAT 4 INBD UPPER LUG HAS GOUGED. REMOVED DAMAGED IAW SRM 51-73-00. CHECKED REMAINING LUG THICKNESS IS 0.510" FOUND TO BE WITHIN LIMITS IAW SRM 57-40-00, FIG. 111. HFEC IAW NTM 51-10-08. NO DEFECTS NOTED. FOLLOW-UP INSPECTION IAW SRI 57-40-00-1-004SDR DALA13072803160Floor Panel · damagedMAIN CABIN FLOOR PANEL 251LGIS DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & DWG 3025-40640.SDR DALA13063453160Wire · brokenEMERGENCY LIGHT AT 19ABC INOPERATIVE. REPAIRED BROKEN WIRE IAW ESPM 20-00. CHECKED OK.SDR DALA1164433160Wire Harness · defectiveSEAT 8C ONE RED EMERGENCY PATH LIGHT INOP. REPLACED LIGHT HARNESS AND TESTS OK.SDR DALA1135043160Light · failedDURING ROUTINE CHECK, FOUND THE RIGHT AFT SLIDE EMERGENCY LIGHT SYSTEM FAILED. MAINTENANCE REPLACED SLIDE RAFT EVAC AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR DALA1135033160Power Supply · no testDURING A NON ROUTINE CHECK, FOUND THE EPSU AT 13 WL AFT FAILED SELF TEST. MAINTENANCE REPLACED EPSU AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR DALA1134003160Power Supply · inoperativeDURING A NON ROUTINE CHECK, EPSU INDICATED FAULT AND SUBSEQUENT FAILURE OF SEVERAL EMERGENCY PATH LIGHT. MAINTENANCE REPLACED THE EPSU AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR NWAA082523160Wire · damagedDURING LINE CHECK DISCOVERED ROW 1, 2, 5, 6 EMERGENCY EGRESS LIGHTS INOP. REPAIRED 2 WIRES BELOW SEAT 1 & 2 REPLACED EPSU (10WL), CHECKS NORMAL. (A)
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