N345NB

Service difficulty reports · 174

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 = 'N345NB' 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 DALA2019112326864Damper · failedDONT WORK CORRECTLY DAMPER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. REPLACE DAMPER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA ASPER A320 FAM AMM 52-13-14.Nov 21, 2019 · N345NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2019112006791Skin · corrodedCORROSION LIP SKIN BTW 3 AND 9 O CLOCK ON ENGINE 1. REPLACED THE AIR INTAKE COWL ON ENG #1 ASPER A320 FAM AMM.Nov 19, 2019 · N345NB · Airbus A319114 · Engine Air Intake SystemSDR DALA2019112086790Stringer · corrodedCORROSION STRINGER 42R BTW FR60 TO FR61 IN AFT CARGO COMPARTMENT (0 EA) ( REFERENT TO LOGPAGE 1355938 TO UPDATE DEFERRAL CONDITION ). REPAIRED STRINGER 42R BTW FR60 TO FR61 IN AFT CARGO COMPARTMENT ASPER A319 SRM 53-00-13-300-002 FIG 001 SHEET 04 MEASURE OF CONov 17, 2019 · N345NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2019111306627Stringer · corrodedCORROSION LEVEL: 2. CORROSION STRINGER 32L AT FR 58 IN AFT CARGO COMPARTMENT. REPAIR STRINGER 32L AT FR58 IN AFT CARGO COMPARTMENT AS PER A319 SRM 53-00-13-300-001, FIG 001 SHEET 2. MEASURE OF CORROSION: L= 7.465"; W=0.838", THIS REPAIR MUST BE INSPECTED AT 60Nov 12, 2019 · N345NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2019111206596Stringer · corrodedCORROSION LEVEL: 2. CORROSION STRINGER 42R BTW FR60 TO FR61 IN AFT CARGO COMPARTMENT. REPAIRED STRINGER 42R BTW FR 60 TO FR 61 IN AFT CARGO COMPARTMENT AS PER A319 SRM 53-00-13-300-002 FIG 001 SHEET 04. MEASURE OF CORROSION L=2.763" W=0.949" THIS REPAIR MUST BNov 12, 2019 · N345NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2019111206595Attach Fitting · crackedCRACK INDICATION ON WINDSHIELD SIDE POST UPPER ATTACHMENT FITTING FR4 LH FASTENER HOLE. CRACK DEPTH = 0.085 IN. APPROX. IN COCKPIT ( 1 EA) (REF. WORK CARD 5311-2029). PERFORMED TIME LIMITED REPAIR ON WINDSHIELD SIDE POST UPPER ATTACHMENT FITTING FR 4 L/H FASTENov 12, 2019 · N345NB · Airbus A319114 · Fuselage Main, StructureSDR DALA201911116532Floor Support · corrodedCORROSION LEVEL: 2. CORROSION FLOOR BEAM -Y765 AND FR 68 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR BEAM -Y765 LOC BTW FR66 TO FR70 AT AFT GALLEY AREA AS PER A19 SRM 51-72-11 AND DRAWING #D53472093 ISSUE K, RELEASE DATE:09-JAN-15 MEASURE OF CORROSION ARE Nov 10, 2019 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2019111106534Attach Fitting · crackedFUSELAGE / OPENING FRAMES / NOSE FWD / LH SLIDING WINDOW / UPPER ATTACHMENT / CRACK. ACCOMPLISH ER/A 582578-14 SECTION II REPAIR WITHIN 5000 CYCLES FROM ACCOMPLISHMENT OF THE SECTION I TIME-LIMITED REPAIR. ENTRY OPEN ***** MONITOR/QC *****Nov 8, 2019 · N345NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2019111196527Floor Support · corrodedCORROSION LEVEL: 2. CORROSION FLOOR BEAM -Y1292 BRW FR68 TO FR69 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR BEAM -Y1292 LOCATED BTW FR68 TO FR69 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND DRAWING #53472089 ISSUE:A, RELEASE DATE:02-OCT-13, SRM A319 51Nov 8, 2019 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2019111196526Floor Support · corrodedCORROSION LEVEL: 2. CORROSION FLOOR BEAM +Y1292 BTW FR66 TO FR68 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR BEAM +Y1292 BTW FR66 TO FR68 AT GALLEY AREA AS PER A319 SRM 51-72-11 AND DRAWING #D53472089 ISSUE L, RELEASE DATE:02-OCT-13, MEASURE OF CORROSION INov 8, 2019 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2019042432598Light · inoperativeSEAT 26D EMERGENCY EXIT PATH LIGHT DAMAGED. R&R LIGHT ASSY.Apr 22, 2019 · N345NB · Airbus A319114 · Emergency LightingSDR DALA2019030101464Wire · brokenEMERGENCY SEAT LIGHTS 19FED & 20FED WILL NOT ILLUMINATE, FOUND BROKEN WIRE AT PLUG 9155VC. REPINNED WIRE AND REPLACED MISSING WIRE LENGTH.Feb 22, 2019 · N345NB · Airbus A319114 · Light System WiringSDR DALA2018080764897Connector · damagedROW 22 AND ROW 23 SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE, FOUND THE CONNECTOR 9157VC CONTACT PIN B PUSHED BACK, RESET THE PINAug 5, 2018 · N345NB · Airbus A319114 · Light System WiringSDR DALA2019082104886Stringer · damagedFWD ATG4 HAS OVERSIZE HOLES IN STR'S, REPAIRED PER SECTION 1 ER/A 557001-14ADMar 27, 2017 · N345NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2017022401525Power Supply · failedEPSU FWD LEFT UNIT FAILED LIGHT ILLUMINATED EMERGENCY LIGHT CHECK, REPLACED EPSU.Feb 23, 2017 · N345NB · Airbus A319114 · Emergency LightingSDR DALA2017011700438Power Supply · faultedFWD EPSU (10WL) FAULTING, R & R EPSU WITH BATTERYJan 16, 2017 · N345NB · Airbus A319114 · Emergency LightingSDR DALA2016092306795Connector · looseROW 22 & 23 EMERGENCY LIGHTS INOPERATIVE, FOUND LOOSE CONNECTOR, RECONNECTEDSep 21, 2016 · N345NB · Airbus A319114 · Light System WiringSDR DALA2016092006762Connector · miswiredCENTER AFT EMERGENCY EXIT LIGHT BURNED OUT, ABOVE SWIVEL JUMP SEAT. FOUND CONNECTOR 9164VCA MISWIRED, CORRECTED WIRING.Sep 17, 2016 · N345NB · Airbus A319114 · Light System WiringSDR DALA2015120907501Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242LF DELAMINATED, FABRICATED NEW ON VTMAE TRAVELER T15/1175459 IAW DWG NW3025-40640.Dec 7, 2015 · N345NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2015120907500Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241MF DELAMINATED, 11" X 2", FABRICATED NEW FLOOR PANEL 241MF ON VTMAE TRAVELER T15/11775454 IAW DWG NW3025-40640.Dec 7, 2015 · N345NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2015120907499Floor Panel · delaminatedAFT CABIN FLOOR PANEL 261EF HAS DELAMINATED, 20" X4", FABRICATED NEW PANEL 261EF ON VTMAE TRAVELLER T15/1175964 IAW DWG NW3025-40640.Dec 7, 2015 · N345NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2015120907498Floor Panel · delaminatedAFT CABIN FLOOR PANEL 2620EF IS DELAMINATED. 4" X 4", FABRICATED NEW PANEL 262EF ON VT TRAVELLER T15/1175963 IAW DWG NW3025-40640.Dec 7, 2015 · N345NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2015120907497Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 242MF DELAMINATED, 7" X 10", FABRICATED NEW FLOOR PANEL ON VTMAE TRAVELER T15/1175493 IAW DWG NW302540640.Dec 7, 2015 · N345NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2015070604189Light · inoperativeEMERGENCY EXIT LIGHT INOPERATIVE SEAT 1B. REPLACED 1B SEAT EMERGENCY LIGHT ASSY.Jul 5, 2015 · N345NB · Airbus A319114 · Emergency LightingSDR DALA2015061203718Light · damagedEMERGENCY SEAT 5C, MOUNTED LIGHTING DAMAGED, REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSY.Jun 11, 2015 · N345NB · Airbus A319114 · Emergency LightingSDR DALA2015050603089Skin · damaged1 LT PAX DOOR SKIN DAMAGE IN LOWER AFT CORNER. 3" VERTICAL X 16.75" HORIZONTAL, DURING MAINTENANCE. INSTALLED REPAIR DOUBLER IAW ERA 535743-14, SECTION 1.May 5, 2015 · N345NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2015030401911Stringer · corrodedAFT STRINGER 42L BETWEEN FRAME 59 AND 60 HAS CORROSION. REMOVED DAMAGE IAW SRM 51-74-00, DAMAGE REMOVAL DID NOT EXCEED 50 PERCENT MATERIAL LOSS IAW SRM 53-00-13, FIG 202. INSTALLED REPAIR DOUBLER IAW SRM 53-00-13, FIG 202, SHEET 4.Mar 3, 2015 · N345NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA14007203145Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL 241JF AT PAX CABIN. REPAIRED FLOOR PANEL IAW ER/A 521959-14.Feb 2, 2014 · N345NB · Airbus A319114 · Fuselage Floor PanelSDR DALA14007183145Bushing · corrodedCORROSION ON INBD AND OTBD FIXED BUSHINGS OF ELEVATOR HINGE FITTINGS NR 6 RT SIDE. REPAIRED INBD AND OTBD LUGS OF ELEVATOR HINGE FITTING NR 6 RT SIDE IAW ERA N. 522606-14, SECTION I.Feb 2, 2014 · N345NB · Airbus A319114 · Elevator StructureSDR DALA14007173145Bushing · corrodedCORROSION ON INBD AND OTBD FIXED BUSHING OF ELEVATOR HINGE FITTINGS NR 2 RT SIDE. REPAIRED INBD AND OTBD LUGS OF ELEVATOR HINGE FITTING NR 2 RT SIDE IAW ERA N 522606-14, SECTION I.Feb 2, 2014 · N345NB · Airbus A319114 · Elevator StructureSDR DALA14007163145Bushing · corrodedCORROSION ON INBD AND OTBD FIXED BUSHINGS OF ELEVATOR HINGE FITTINGS NR 1 RT SIDE. REPAIRED INBD AND OTBD LUGS OF ELEVATOR HINGE FITTING NR 1 RT SIDE IAW ERA N. 522606-14, SECTION I. THIS REPAIR MUST BE INSPECTED EVERY 6 YEARS (2190 DAYS) AFTER 31-JAN-14 IAW Feb 2, 2014 · N345NB · Airbus A319114 · Elevator StructureSDR DALA14007223145Bushing · corrodedCORROSION ON INBD AND OTBD FIXED BUSHINGS OF ELEVATOR HINGE FITTINGS NR 5 RT SIDE. REPAIRED INBD AND OTBD LUGS OF ELEVATOR HINGE FITTING NR 5 RT SIDE IAW ERA N.522606-14, SECTION I.Feb 1, 2014 · N345NB · Airbus A319114 · Elevator StructureSDR DALA14007213145Bushing · corrodedCORROSION ON BUSHING SHOULDERED ON INBD ACTUATOR HINGE FITTING OTBD LUG OF LT ELEVATOR. R & R BUSHING ON OTBD LUG OF INBD ACTUATOR HINGE FITTING LT ELEVATOR SRM 55-26-47, SRM 51-72-12. THE REPAIR MUST BE INSPECTED FOR GVI AT 24,000 FC, AFTER COMPONENT FIRST Feb 1, 2014 · N345NB · Airbus A319114 · Elevator StructureSDR DALA14007063145Skin · dentedDENT ON SKIN AT FRAME 73+7 BETWEEN S26-27L . REPAIRED IAW ERA 521954-14.Feb 1, 2014 · N345NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA14008293145Hinge Fitting · corrodedCORROSION FOUND ON INNER SURFACE OF BOTH INBD AND OTBD LUG BORES AT HINGE FITTINGS 1, 2, 5, 6.Jan 31, 2014 · N345NB · Airbus A319114 · Elevator StructureSDR DALA14006973145Profile · crackedCRACK ON PROFILE IN AFT CARGO BAY BETWEEN FRAMES 56 - 57+18. REPAIRED IAW ER/A NR 521955-14, REV ORIGINAL.Jan 31, 2014 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14006293145Skin · dentedDENT ON EXTERNAL SKIN AT FRAME 14 +3 S32R. REPAIRED IAW ER/A 521951-14. REV ORIGINAL.Jan 29, 2014 · N345NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA14006213145Floor Support · corrodedCORROSION ON PAX CABIN FLOOR SUPPORT -Y254 FRAME 20. REPLACED FLOOR SUPPORT BETWEEN FRAMES 12-24 IAW SRM 51-72-1 AND DWG D53111462.Jan 29, 2014 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14006013145Stringer · corrodedCARGO BAY, CORROSION FOUND ON STRINGER 43L BETWEEN FRAMES 64-65. PERFORMED PERMANENT REPAIR IAW SRM A319 53-00-13.Jan 28, 2014 · N345NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA14006003145Stringer · corrodedCORROSION FOUND ON STRINGER 44 BULK CARGO BAY AREA BETWEEN FRAMES 64-65. PERFORMED PERMANENT REPAIR IAW SRM 53-00-13.Jan 28, 2014 · N345NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA14005953145Web · corrodedTHRESHOLD SHEET AFT CARGO BAY LOCATED BETWEEN FRAME 55A-59 AND S38-39R CORRODED. REWORKED AREA MECHANICALLY IAW SRM 51-74-00. FOUND WITHIN LIMITS IAW DWG D53477153 AND ABS5044A025. HFEC INSPECTION DONE ON REWORKED AREAS IAW NTM 51-10-02-PB6, NO CORROSION INJan 26, 2014 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14005943145Web · corrodedCORROSION ON COVER SHEET AFT CARGO BAY BETWEEN FRAMES 55A-59 AND S39-41R. REWORKED AREA MECHANICALLY IAW SRM 51-74-00. FOUND WITHIN LIMITS IAW DWG D53477154. HFEC INSPECTED IAW NTM 51-10-02-PB6, NO CORROSION INDICATION FOUND.Jan 26, 2014 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14005883145Seat Track · corrodedCORROSION ON SEAT TRACK Y765 FRAME 42+18, FOUND OUT LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53370382.Jan 25, 2014 · N345NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA14005873145Sill · corrodedCORROSION ON LOWER SILL AT AFT PAX DOOR, FRAME 66. REPLACED SILL IAW SRM 51-72-11 AND DWG D53480505.Jan 25, 2014 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14005843145Structure · crackedCRACK ON SECTION CONNECTING FRAME 68 STRINGER 23L. REPLACED IAW SRM 51-72-11 AND DWG D53474250, JOB COMPLETE.Jan 24, 2014 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14005833145Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 AND 66 Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Jan 24, 2014 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14005823145Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 AND 69 Y1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Jan 24, 2014 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14005813145Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 AND 66 Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Jan 24, 2014 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14005073145Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT FRAME 66 Y512. REPLACED FLOOR SUPPORT BETWEEN FRAMES 64 - 67+10" IAW SRM 51-72-11, PAGE 1-2 AND DWG D534 72000.Jan 23, 2014 · N345NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA14005063145Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FRAMES 68 - 69 Y-1162. REPLACED FLOOR BETWEEN FRAMES 67+16 - 69 IAW SRM 51-72-11 AND DWG D53472000 AND D53470150.Jan 23, 2014 · N345NB · Airbus A319114 · Fuselage Miscellaneous Structure
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