N348NB

Service difficulty reports · 197

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 = 'N348NB' 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 DALA2019102196029Repair · unknownERA 568357-14 HAS BEEN ISSUED FOR PUNCTURE AND DENT THAT WAS REP AIRED PER EA 31-203749 REV F. DURING AIRBUS' RDAS REVIEW FOR THE A319 WV INCREASE PROJECT THE APPROVAL REQUIRED REVISION. ERA 568357-14 SECTION IV IMPOSES A LIFE LIMIT ON THE BOTTOM SKIN REPAIR. May 14, 2018 · N348NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2018020800836Frame · corrodedAPU TAILCONE FRAME 86 HAS CORROSION AROUND LOWER GUIDE PIN, REPLACED THE FRAME SECTION IAW DWG D5358541820200, AND SRM 53-51-12-300-001.Feb 7, 2018 · N348NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2016022501470Skin · gougedRT AFT FUSELAGE SKIN APPROXIMATELY 4" FWD OF FRAME 70 BETWEEN STR 14 - 15R, DENT WITH SHARP GOUGE, DOUBLER REPAIR IAW SRM 53-00-11, FIG 229.Feb 20, 2016 · N348NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2016021401154Floor Panel · corrodedAFT CABIN FLOOR PANEL 262FF HAS CORROSION. REPLACED THE FLOOR PANEL IAW SRM 51-72-11.Feb 13, 2016 · N348NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2015022201624Light · inoperativeEMERGENCY LIGHT AT 4C INOPERATIVE, PLUGGED LIGHT IN.Feb 21, 2015 · N348NB · Airbus A319114 · Emergency LightingSDR DALA2014062503775Battery Pack · inoperativeLEFT OVER WING EMERGENCY EXIT LIGHT BATTERY FAULT ILLUMINATED. REPLACED EPSU BATTERY PACK IAW AMM 33-51-38, PG 401.Jun 25, 2014 · N348NB · Airbus A319114 · Emergency LightingSDR DALA14020473148Lens · damagedSEAT 14C EMERGENCY SEAT MOUNTED LIGHT DAMAGED. REPLACED BROKEN LENS 4. OPS CHECKED OK IAW AMM 33-51. OK FOR SERVICE.Apr 3, 2014 · N348NB · Airbus A319114 · Emergency LightingSDR DALA14013153148Skin · dentedDURING M1 CHECK, A DENT WAS FOUND ON SKIN BETWEEN FRAMES 21-23 AND STRINGER 25L. FOUND OUT OF LIMITS IAW SRM 53-11-11 PB 4.C DIAGRAM 10. REPAIRED IAW ERA 521960-14 SECTION I.Feb 13, 2014 · N348NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA14009803148Skin · dentedDURING M1 CHECK, A DENT WAS LOCATED BETWEEN FRAMES 21 - 23 AND S25L. DENT FOUND BEYOND LIMITS IAW SRM 53-11-11, PB 4.C DIAGRAM 10. REPAIRED IAW ERA 521960-14 SECTION I.Feb 12, 2014 · N348NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2016102608025Structure · corrodedCORROSION ON UPPER SURFACE OF CENTER WING BOX LOC AT LEVEL FR 42 AND BTW -Y1732 TO -Y 1292 PAX CABIN MEASURE L=1.500" W=1" D=0.002" APPROX. REPAIR ON UPPER SURFACE OF CENTER WING BOX LOCATED AT LEVEL FR41 TO FR42 BTW Y-1292 TO Y-1732 AND RIB 1 PAX CABIN PER EFeb 11, 2014 · N348NB · Airbus A319114 · Wing, Center BoxSDR DALA14009423148Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANEL 540FB. REPLACED ACCESS PANEL 540FB ON LT WING IAW AMM 57-27-11-400-001-A.Feb 11, 2014 · N348NB · Airbus A319114 · Wing, Plate/SkinSDR DALA14009333148Skin · corrodedCORROSION ON EXTERNAL SKIN LOCATED ON AREA OF DRAIN MAST FRAME 30-34, STR 42L-43L. REWORKED AREA IAW SRM 51-74-00 ON EXTERNAL FUSELAGE SKIN LOCATED FR30, FR34, STR 42L TO 43L LT SIDE EVALUATED AND FOUND WITHIN LIMITS ASPER SRM 53-21-11, PARA 4E FIG 115 AND DIAFeb 9, 2014 · N348NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA14009323148Sill · corrodedCORROSION ON LOWER SILL LOCATED FWD PAX CABIN ENTRY DOOR BETWEEN FR 16 AND FR 20 RT WITH MEASUREMENT L=0.080", W=0.060", D=0.006", APPROX. PERFORMED REPAIR ON LOWER SILL LOCATED FWD PAX CABIN ENTRY DOOR BETWEEN FRAME 16-20 RT SIDE IAW SRM 53-11-14, FIG 108 SHEFeb 9, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14009313148Sill · corrodedCORROSION ON LOWER SILL LOCATED FWD PAX CABIN ENTRY DOOR LT BETWEEN FRAME 16-20 WITH MEASUREMENT L=0.080", W=0.050", D=0.005" APPROXIMATELY, SSI 531189. PERFORMED REPAIR ON LOWER SILL LOCATED FWD PAX CABIN ENTRY DOOR BETWEEN FRAME 16 LT AND FR 20 LT IAW SRM 5Feb 9, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14008283148Channel · corrodedCORROSION ON RETAINER NUT PLATES AT FRONT AREA OF DOOR BETWEEN RIBS 5 - 6 IN LT WING DRY BAY. REPLACED CHANNEL IAW SRM A319 51-42-11 AND DWG D57252700.Feb 8, 2014 · N348NB · Airbus A319114 · Wing Miscellaneous StructureSDR DALA14008273148Skin · delaminatedDELAMINATION ON LT INBD FLAP UPPER AND LOWER SKIN. REPAIRED IAW SRM 57-52-00, PARA 8.0, ITEMS 2 AND 3 .Feb 7, 2014 · N348NB · Airbus A319114 · Trailing Edge FlapsSDR DALA14007383148Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 - 69 + Y1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.Feb 4, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007393148Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT FRAME 20, Y-254. REPLACED FLOOR SUPPORT.Feb 3, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007373148Fitting · corrodedCORROSION ON AFT CORNER FITTING LOCATED FRAME 66. REPLACED AFT CORNER FITTING IAW SRM 51-72-11 AND DWG D53480009.Feb 3, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007363148Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT FRAME 20, Y-1292. REPLACED FLOOR SUPPORT BETWEEN FRAMES 12 - 24 IAW SRM 51-72-11 AND DWG D53112812.Feb 3, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007353148Sill · corrodedCORROSION ON LOWER SILL LOCATED RT PAX CREW DOOR BETWEEN FRAMES 66 - 68. REPLACED SILL IAW SRM 51-72-11, & DWG D53480009.Feb 3, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007233148Sill · corrodedCORROSION ON LOWER SILL LOCATED LT AFT PAX CREW DOOR BETWEEN FRAMES 66 TO 68. REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG D53480009.Feb 3, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007153148Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 68 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.Feb 2, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007193148Fitting · corrodedCORROSION ON AFT CORNER FITTING LOCATED FR 68 AFT PAX CABIN LT SIDE. REPLACED AFT CORNER FITTING IAW SRM 51-72-11.Feb 1, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007083148Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT -Y1225, FRAMES 66 - 67+15.5. REPLACED FLOOR SUPPORT IAW SRM A319 51-72-11 AND DWG D534 72780.Feb 1, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007053148Support · corrodedAFTER REMOVING SHEAR PLATE, FOUND CORROSION ON SUPPORT BETWEEN FRAMES 69- 70. REPLACED SUPPORT IAW 51-72-11 AND D53470100.Feb 1, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007143148Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 64 - 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 & DWG D53472815.Jan 31, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007133148Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAME 66 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.Jan 31, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007113148Floor Support · corrodedCORROSION ON FLOOR SUPPORT Y1292 BETWEEN FRAMES 64 - 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.Jan 31, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007103148Floor Support · corrodedCORROSION ON FLOOR SUPPORT Y1225 BETWEEN FRAMES 66 - 67+15.5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, & DWG D53472780.Jan 31, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007093148Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1292, BETWEEN FRAMES 64 - 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534-72815.Jan 31, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007043148Fitting · corrodedCORROSION ON CENTER FITTING LOCATED FWD ENTRY PAX CABIN DOOR RT BETWEEN FRAMES 16-20. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D531-12198.Jan 31, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14006963148Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT FRAME 20 LEVEL Y-765. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812 AND D53110984.Jan 31, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14006953148Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y160, BETWEEN FRAMES 66-68. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.Jan 31, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14007123148Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y465, BETWEEN FRAMES 64 - 67+10. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.Jan 30, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14006503148Floor Support · corrodedCORROSION ON FLOOR SUPPORT Y765 FRAMES 66 TO 70. REPLACED FLOOR SUPPORT IAW SRM A319 51-72-11 AND DWG D53472000.Jan 30, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14006493148Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FRAMES 16-20, Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812 AND D53110920.Jan 30, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14006483148Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FRAMES 18 AND 23 Y254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112816, D53110984 AND D55110920.Jan 30, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14006303148Floor Support · corrodedCORROSION ON FLOOR SUPPORT Y765, FRAMES 64 - 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Jan 29, 2014 · N348NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14006283148Dummy Rail · corrodedCORROSION ON DUMMY RAIL BETWEEN FRAMES 14-16. REPLACED DUMMY RAIL IAW SRM A319 51-72-11 AND DWG D53112825.Jan 29, 2014 · N348NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA14004933148Skin · gougedGOUGE ON EXTERNAL FUSELAGE SKIN AT FRAME 28 PLUS 2 INCHES BETWEEN S43-44L LOWER FWD FUSELAGE. FOUND WITHIN LIMITS IAW SRM 53-21-11. HFEC INSPECTION DONE IAW NTM 51-10-08. NO CRACK INDICATIONS FOUND.Jan 22, 2014 · N348NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13045013148Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND EPSU UNIT FAULT ON FWD LT EPSU. REPLACED EPSU UNIT AND BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.Sep 16, 2013 · N348NB · Airbus A319114 · Emergency LightingSDR DALA13036093148Battery · inoperativeESPU BATTERY FWD L MESSAGE FOUND WHILE PERFORMING STEP 7 OF THE SERVICE CHECK. R & R OVERWING EPSU BATTERY. INSTALLED SERVICEABLE BATTERY PACK IAW AMM 33-51-38, P6 401. OP TESTED OK FOR SERVICE.Jul 14, 2013 · N348NB · Airbus A319114 · Emergency LightingSDR DALA14004243148Skin · dentedDAMAGE TO FUSELAGE SKIN JUST AFT OF CARGO DOOR FS 59. FOUND TO BE WITHIN LIMITS IAW SRM 53-41-11. TREATED BUT DID NOT PAINT.Oct 26, 2012 · N348NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA1217433148Trunnion · damagedLEFT INBOARD FLAP TRUNNION DAMAGED. AREA WORN APPROXIMATE .250 DEEP. REMOVED LEFT INBOARD FLAP INBOARD TRUNNION IAW A319/320 CMM 57-52-21 (903393). REPLACED LEFT INBOARD FLAP TRUNNION IAW A319/320 CMM 57-52-21 AND PER PRI501285-14 REV 1. INSTALLED INBOARDMar 19, 2012 · N348NB · Airbus A319114 · Trailing Edge FlapsSDR DALA1123893148Light · inoperativeDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATHLIGHT AT ROW 13 INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT ASSEMBLY AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Apr 3, 2011 · N348NB · Airbus A319114 · Emergency LightingSDR DALA1022953148Skin · dentedDURING LINE CHECK, FOUND DENT IN FUSELAGE UNDER DOOR 1L. TEMPORARY REPAIR ACCOMPLISHED IAW SRM 53-00-11, FIG 219 TIME LIMITED TO 3000 FLIGHT CYCLES.Sep 15, 2010 · N348NB · Airbus A319114 · Fuselage Main, Plate/Skin
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