N337NB

Service difficulty reports · 236

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 = 'N337NB' 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.

SDR DALA13037673137Floor Panel · corrodedAFT UTILITY FLOOR PANEL 261FF CORRODED. REPLACED AFT UTILITY FLOOR PANEL.Aug 1, 2013 · N337NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13037663137Blanking Plate · corrodedL2 DOOR AFT BLANKING PLATE CORRODED. REPLACED L2 DOOR BLANKING PLATE.Aug 1, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13037653137Sill · corrodedLEFT AFT DOOR SILL INBD SIDE AT FR 68 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14. R & R SILL IAW SRM 51-42-11 & DWG D53480019.Aug 1, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13037643137Floor Support · corrodedFWD UTILITY AREA BETWEEN FR 16 & FR 20 FLOOR SUPPORT Y-254 CORRODED. 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 & TRM 53-21-01.Aug 1, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13037343137Support · corrodedAFT CABIN BETWEEN FR 69 & 70 RT SHEAR PLATE SUPPORT CORRODED. REMOVED CORROSION, NO ESTABLISHED LIMITS IAW SRM 53-41-14. R & R SUPPORT IAW SRM 51-42-11.Aug 1, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13037333137Floor Panel · corrodedFWD UTILITY FLOOR PANEL 221FF CORRODED. REPLACED FLOOR PANE IAW SRM 51-72-11.Jul 31, 2013 · N337NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13037323137Floor Panel · corrodedAFT UTILITY FLOOR PANEL 262FF CORRODED. REPLACED AFT UTILITY FLOOR PANEL IAW SRM 51-72-11.Jul 31, 2013 · N337NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13037313137Floorbeam · corrodedFWD UTILITY AREA FR 20, FLOORBEAM Y-765 CORRODED. R & R FLOORBEAM IAW SRM 51-42-11 AND TRM 53-21-01. FLOORBEAM WAS CORRODED OUT OF LIMITS.Jul 31, 2013 · N337NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA13037283137Sill · corrodedLT AFT DOOR SILL, AFT SHAPE SILL AROUND FASTENER HOLES CORRODED. REMOVED CORROSION IAW SRM 51-74-00 NO ESTABLISHED LIMITS ON SRM. LOCATED AND DRILLED NEW FITTING CORNER IAW SRM 51-44-11. INSTALL NEW FITTING.Jul 30, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13037273137Floor Support · corrodedFWD UTILITY AREA, FR 20 FLOOR SUPPORT AT Y1732, SUPPORT ANGLE CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND 51-44-11.Jul 30, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13037263137Sill · corrodedLEFT AFT DOOR SILL, FWD SHAPE SILL AROUND FASTENER HOLES CORRODED. REMOVED CORROSION IAW SRM 51-74-00. NO ESTABLISHED LIMITS ON SRM. LOCATED AND DRILLED NEW FITTING CORNER IAW SRM 51-44-11. INSTALLED NEW FITTING.Jul 30, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13037253137Blanking Plate · corrodedRI DOOR GIRT BAR FITTING BLANKING PLATE CORRODED AROUND FASTENER HOLES AFT GIRT BAR FITTING. REMOVED DAMAGE IAW SRM 51-74-00. NO ALLOWABLE DAMAGE LIMITS IN SRM 53-02-00. REMOVED & INSTALLED.Jul 30, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13036893137Floor Support · corrodedAFT CABIN FLOOR SUPPORT +Y512 AT FR 66 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-14. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.Jul 29, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13036503137Floor Support · corrodedFWD UTILITY AREA FRAMES 16 & 20 FLOOR SUPPORT Y1292 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMIT IAW SRM 53-11-15. R & R Y1292 FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.Jul 28, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13036493137Floor Support · corrodedAFT CABIN FLOOR SUPPORT -Y765 FRAMES 66 - 68 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. R & R FLOOR SUPPORT IAW TRM 53-21-01.Jul 28, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13036483137Floor Support · corrodedAFT CABIN FLOOR SUPPORT +Y765 FRAMES 66 TO 70 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. REWORKED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15, FIG 1. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Jul 28, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13036473137Floor Support · corrodedAFT FLOOR SUPPORT +Y765 BET FRAMES 64-66 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. REWORKED AREA, FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15, FIG 1. R & R FLOOR SUPPORT IAW SRM 51-42-11 AND TRM 53-21-01.Jul 28, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13036433137Floor Support · corrodedFWD UTILITY AREA FR20 Y-1732 FLOOR SUPPORT WEB CORRODED. REMOVED CORROSION IAW SRM 51-74-00". NO DAMAGE LIMITS FOUND IN SRM 53-11-14. R & R FLOOR SUPPORT WEB IAW SRM 51-42-11 AND DWG D53114332.127821.Jul 26, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13036423137Floor Support · corrodedFWD UTILITY AREA BETWEEN FR 18 & 21 FLOOR SUPPORT CORRODED. 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 AND TRM 53-21-01.Jul 26, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13036393137Floorbeam · corrodedFWD UTILITY AREA FR16 FLOORBEAM Y503 HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-11-11. REMOVED FLOORBEAM IAW SRM 51-42-11. LOCATED & DRILLED IAW SRM 51-44-11. TREATED & PRIMED HOLES IAW SRM 51-21-11. TRANSFERRED EDGEJul 25, 2013 · N337NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA13036403137Sill · corrodedLEFT AFT DOOR SILL CORRODED. REMOVED CORROSION IAW SRM 51-74-00. LOCATED AND DRILLED NEW SILL IAW SRM 51-44-1. INSTALLED.Jul 25, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13035903137Floor Support · corrodedFWD UTILITY AREA BETWEEN FR 20 & 21, FLOOR SUPPORT CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. R & R FLOOR SUPPORT IAW TRM 53-21-01 AND DWG D53111406.Jul 21, 2013 · N337NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13013333137Wire Harness · looseSEAT 22A HAS WIRE BUNDLE HANGING DOWN UNDER SEAT. RESECURED EMER LIGHT WIRES AT SEAT 22A. OK FOR SVC 868084 MEM.Mar 25, 2013 · N337NB · Airbus A319114 · Light System WiringSDR DALA13011883137Floor Panel · delaminatedDURING SERVICE CHECK FOUND AFT CARGO FLOOR PANEL 1512G DELAMINATED ON THREE QUARTERS OF PANEL SURFACE. REMOVED FLOOR PANEL INSTALLED REPAIRED FLOOR PANEL IAW AMM 53-42-14 AND SEALED OK FOR SERVICE.Mar 10, 2013 · N337NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12016853137Connector · dirtyEMERGENCY ESCAPE PATH LIGHT AT ROW 12 ABC INOPERATIVE. CLEANED CONNECTION AT LIGHT BULB AS REQUIRED. OPS CHECKED GOOD. OK FOR SERVICE.Dec 19, 2012 · N337NB · Airbus A319114 · Light System WiringSDR DALA12010363137Floor Panel · delaminatedAFT CARGO FLOOR PANEL 151ZG DELAMINATED AND PUNCTURED. REPAIRED FLOOR PANEL IAW SRM 53-02-00.Oct 15, 2012 · N337NB · Airbus A319114 · Fuselage Floor PanelSDR DALA12002043137Power Supply · inoperativeESCAPE PATH LIGHTS OUT ON ROWS 12, 13, 14, 17, 18, AND 25, 26. REMOVED AND REPLACED EPSU 13WL IAW AMM 33-51-38. OPS CHECKED EPSU.Jun 23, 2012 · N337NB · Airbus A319114 · Emergency LightingSDR DALA1166613137Wire Harness · damagedMAINTENANCE FOUND SEAT 16C EMERGENCY ESCAPE PATH LIGHT INOPERATIVE. FOUND WIRE HARNESS DAMAGED AND PULLED FROM PIN. FEMALE END OF HARNESS NEEDED. SECURED WIRE PER MEL 33-50-03A. PLACARD INSTALLED AND ENTERED IN LIDS (2011-00742). REPAIRED WIRE/CONNECTOR PNov 29, 2011 · N337NB · Airbus A319114 · Light System WiringSDR DALA1141403137Wire · brokenDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 19ABC INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Jun 26, 2011 · N337NB · Airbus A319114 · Light System WiringSDR DALA1105223137Wire · brokenDURING NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT ROW 5, 7 AND 14 INOPERATIVE. MX REPAIRED BROKEN WIRE AND PERFORMED SUCCESSFUL TEST. ACFT RETURNED TO SERVICE.Jan 21, 2011 · N337NB · Airbus A319114 · Light System WiringSDR DALA104343137Wire · damagedDURING NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 11 INOPERATIVE. MX REPAIRED WIRING AT LIGHT PIGTAIL. OPS CHECK WAS NORMAL.Feb 24, 2010 · N337NB · Airbus A319114 · Light System WiringSDR NWAA 091263137Unknown · odorSHORTLY AFTER TAKEOFF, AFT FLIGHT ATTENDANTS REPORTED ACRID ODOR THAT ALSO PRODUCED A SLIGHT BURNING SENSATION IN THEIR EYES. SLIGHT ACRID ODOR NOTED ON FLIGHT DECK, BUT NOT BY 1ST CLASS FLIGHT ATTENDANT STATION. FUMES DISSIPATED WITHIN 3 MINUTES. CONTINUEDApr 17, 2009 · N337NB · Airbus A319114 · Air Distribution SystemSDR NWAA082563137Power Supply · inoperativeSEAT ROWS 11, 15, 16, AISLE EMERGENCY EGRESS LIGHTS INOPERATIVE. REPLACED 3RD LT EMERGENCY POWER SUPPLY UNIT. OPS CHECK GOOD. (A)Jun 7, 2008 · N337NB · Airbus A319114 · Emergency LightingSDR NWAA071763137Epsu · malfunctionedPERFORMED EMERGENCY ESCAPE LIGHT POWER SUPPLY TEST ON FWD L UNIT, FAULT ILLUMINATED. REPLACED FWD L EPSU, CHECKS OK.May 8, 2007 · N337NB · Airbus A319114 · Emergency LightingSDR 0401583137Centering Cam · out of positionAFTER TAKEOFF, UNABLE TO RAISE LANDING GEAR HANDLE AND RETRACT LANDING GEAR. RETURNED TO DTW AND LANDED UNEVENTFULLY. FOUND NOSE GEAR STRUT CENTERING CAM 90 DEGREES OUT OF POSITION. REALIGNED CENTERING CAM AND REASSEMBLED NOSE GEAR STRUT. SERVICED NOSE GEASep 20, 2004 · N337NB · Airbus A319114 · Landing Gear Steering SystemSDR 0201413137Pin · missingPILOT REPORTED LOSS OF HYDRAULIC FLUID IN THE GREEN HYDRAULIC SYSTEM DURING CLIMBOUT. SWITCHED POWER TRANSFER UNIT TO OFF AND GREEN SYSTEM ENGINE 1 PUMP TO OFF. COMPLETED GRAVITY GEAR EXTENSION AND LANDED IN MSP UNEVENTFULLY. FOUND OUTBOARD SWIVEL GLAND IN May 4, 2002 · N337NB · Airbus A319114 · Drag Control Actuator
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