N344NB

Service difficulty reports · 212

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 = 'N344NB' 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 DALA2019091805417Skin · corrodedCORROSION LEVEL: 2. CORROSION EXTERNAL SKIN LOC. FR 65+10 STR 31R STR 32R AT LOWER FUSELAGE (1 EA) SSI 534108 AND WORK CARD 5100-3201. PERFORMED PERMANENT REPAIR LOC BTW FR 65 TO FR 66 AND STR 31R TO STR 33R AS PER SRM 53-00-11-300-033, ER/A 581054-14AD REVISISep 18, 2019 · N344NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2019091605334Angle · crackedA/C 3144 CLOSED LOG 1273169 FLT/CHK H2. CRACK OB FIXED LEADING EDGE I/B AND O/B TELESCOPIC ANGLE ON LT WING ( 2 EA). REPLACED TELESCOPIC ANGLE (2E/A) LOC FIXED LEADING EDGE I/B AND O/B ON LT WING AS PER SRM 51-72-11, SRM 51-42-11 DRAWING #D57447202.Sep 16, 2019 · N344NB · Airbus A319114 · Wing Miscellaneous StructureSDR DALA2019091605333Door Frame · crackedCRACK INDICATION ON PASSENGER CREW DOOR FRAME FASTENER HOLE NR 6. LOCATED AT FR16 UPPER DOUBLE JOGGLE AREA, LT SIDE. IN PASSENGER CABIN (1 EA). PERFORMED PERMANENT REPAIR ON PASSENGER CREW DOOR FRAME FASTENER HOLE N.6 LOCATED AT FR 16 UPPER DOUBLE JOGGLE AREA Sep 16, 2019 · N344NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2019091605332Door Frame · crackedCRACK INDICATION ON PASSENGER CREW DOOR FRAME 16 STOP FITTING 7 AT UPPER INBOARD FASTENER HOLE. RT SIDE. IN PASSENGER CABIN (1 EA). PERFORMED PERMANENT REPAIR ON PASSENGER CREW DOOR FRAME 16 STOP FITTING 7 AT UPPER INBOARD FASTENER HOLE AS PER ER/A NR 580938 -Sep 16, 2019 · N344NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2019091605331Door Frame · crackedCRACK INDICATION ON PASSENGER CREW DOOR FRAME 16 STOP FITTING 7 AT LOWER INBOARD FASTENER HOLE. RT SIDE. IN PASSENGER CABIN (1 EA). PERFORMED PERMANENT REPAIR ON PASSENGER CREW DOOR FRAME 16 STOP FITTING 7 AT LOWER INBOARD FASTENER HOLE AS PER ER/A NR 580738-1Sep 16, 2019 · N344NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2019091605330Door Sill · corrodedCORROSION LEVEL: 2. CORROSION LOWER SILL FR66 RT SIDE AT AFT GALLEY AREA (SSI 534147). PERFORMED REPAIR ON LOWER SILL FR 66 RT SIDE AT AFT GALLEY AREA AS PER SRM 53-41-14-300-301 PRINCIPLES 1 MEASURES OF CORROSION ARE: L=0.567" W=0.446" D=0.080".Sep 16, 2019 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2019091605329Door Frame · crackedCRACK INDICATION ON FRAME 16 LH SIDE ON OPEN FASTENER HOLES LOWER IB AND UPPER IB AT DOOR STOP FITTING 7 (CRACK DIRECTIONS ARE: LOWER IB: 1, 3 AND 5 OCLOCK, UPPER IB: 1, 3 AND 5 OCLOCK) AT FWD GALLEY AREA (6 EA). REPLACED AFFECTED INTERCOSTAL FITTING LOC BTW FSep 16, 2019 · N344NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2019091605328Frame · corrodedCORROSION LEVEL: 2. CORROSION WEB FRAME 20 RT SIDE AT FWD GALLEY AREA (SSI 531189). REPLACED WEB FRAME 20 RT SIDE AT FWD GALLEY AREA LOC FR 20 10 FR 23 RT ASPER SRM 51-72-11 AND DWG # D53114392 RELEASE DATE 01- FEB-19 MEASURE OF CORROSION ARE: L=119.09MM W=38.Sep 16, 2019 · N344NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2019091605327Floorbeam · corrodedCORROSION LEVEL: 2. CORROSION FLOORBEAM +Y1292 BTW FR16 TO FR20 FWD GALLEY AREA ( SSI 531 189 ). REPLACED FLOORBEAM +Y1292 BTW FR 12 TO FR 24 FWD GALLEY AREA AS PER SRM 51-72-11 AND DWG D53112812.Sep 16, 2019 · N344NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2019091605326Seat Track · corrodedCORROSION LEVEL: 2. CORROSION SEAT TRACK -Y1292 AT LEVEL OF FR20 FWD GALLEY AREA ( SSI5311 63). REPLACED SEAT TRACK -Y1292 AT LEVEL FR 12 TO FR 24 FWD GALLEY AREA AS PER SRM 51-72-11. MEASURES OF CORRODED AREA IS:D= 0.102".Sep 16, 2019 · N344NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019091605325Support · crackedCRACK STRUCTURE SUPPORT AFT TI-ANGLE LOCATED AT FR 42 RT SIDE IN MAIN WHEEL WELL (1EA) AD 19-08-07, REQUIRED PRIOR TO FURTHER FLIGHT REF AA 5353-01006-02. REPLACED SUPPORT STRUCTURE AFT TI-ANGLE LOCATED AT FR 42 RT SIDE IN MAIN WHEEL WELL AS PER AA 5353-01006-Sep 16, 2019 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2019091505324Door Frame · crackedCRACK INDICATION ON PASSENGER CREW DOOR FRAME FASTENER HOLE NR 6. LOCATED AT FR16 UPPER DOUBLE JOGGLE AREA, RT SIDE. IN PASSENGER CABIN (1 EA). PERFORMED PERMANENT REPAIR ON PASSENGER CREW DOOR FRAME FASTENER HOLE NR 6 LOCATED AT FR 16 UPPER DOUBLE JOGGLE AREASep 14, 2019 · N344NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2019091505323Door Frame · crackedCRACK INDICATION ON PASSENGER CREW DOOR FRAME 20 STOP FITTING 7 AT LOWER INBOARD FASTENER HOLE RT SIDE IN PASSENGER CABIN (1EA). PERFORMED PERMANENT REPAIR ON PASSENGER CREW DOOR FRAME 20 AT LOWER INBOARD FASTENER HOLE AT LEVEL DOOR STOP FITTING 7 RT SIDE AS PSep 13, 2019 · N344NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2019091105262Intercostal · crackedCRACK INDICATION ON FRAME 20 LT SIDE ON LOWER INBOARD OPEN FASTENER HOLE AT DOOR STOP 7 (CRACK DIRECTION IS 9 OCLOCK) AT FWD GALLEY AREA (1EA). REPLACED INTERCOSTAL FITTING LOCATED BTW FR 20 TO FR 21 AT LEVEL ON DOOR STOP FITTING #7 AT FWD GALLEY AREA AS PER SSep 11, 2019 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2019090905208Floorbeam · corrodedCORROSION LEVEL: 2. CORROSION FLOORBEAM +Y1292 FR66 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOORBEAM +Y1292 FR 66 AT AFT GALLEY AREA (SEAT TRACK) P/N:14N00031-101 AS PER SRM 51-72-11, SRM 51-42-11 AND DWG D53472090 ISSUE G RELEASE DATE:19-MAY-16 ISSUE Q.Sep 9, 2019 · N344NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2019090705198Floorbeam · corrodedCORROSION LEVEL: 2. CORROSION FLOORBEAM -Y765 BTW FR67 TO FR68 AT AFT GALLEY AREA ( SSI 534147). REPLACED FLOORBEAM -765 LOC FR 66 TO FR 70 AT AFT GALLEY AREA ASPER SRM 51-72-11 AND DWG #D53472104202 AND ISSUE: A,B,E RELEASE DATE:17-DEC-15, MEASURE OF CORROSIOSep 6, 2019 · N344NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2019090405133Floorbeam · corrodedCORROSION LEVEL: 2. CORROSION FLOORBEAM -Y1292 FR 67 AT AFT GALLEY AREA (SSI 534147 ). REPLACED FLOORBEAM -Y1292 FR67 TO FR68 AT AFT GALLEY AREA ASPER SRM 51-42-11 SRM 51-72-11 AND DWG D53472000 ISSUE S RELEASE DATE 06-JAN-05 MEASUREMENTS OF CORROSION IS L=1.1Sep 4, 2019 · N344NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2019090405132Floorbeam · corrodedCORROSION LEVEL: 2. CORROSION FLOORBEAM -Y1292 AT FR68 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOORBEAM -Y1292 AT FR 68 TO FR 69 AFT GALLEY AREA ASPER SRM 51-42-11 SRM 51-72-11 AND DWG D53472001 ISSUE K RELEASE DATE 25-OCT-17 MEASUREMENTS OF CORROSION IS L=Sep 4, 2019 · N344NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2019090305115Seat Track · corrodedCORROSION LEVEL: 2. CORROSION SEAT TRACK -Y765 AT LEVEL OF FR20 FWD GALLEY AREA ( SSI 531163). REPLACED SEAT TRACK -Y765 BTW FR 12 TO FR 20 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DRAWING #D53112812.Sep 3, 2019 · N344NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019090205112Door Sill · corrodedCORROSION LEVEL: 2. CORROSION LOWER SILL FR68 RT SIDE AT AFT GALLEY AREA (SSI 534147). PERFORMED REPAIR ON LOWER SILL FR 68 RT SIDE AT AFT GALLEY AREA AS PER SRM 53-41-14-500-001 PRINCIPIE 7 MEASURES OF CORROSION ARE: L=4.9" W=0.637" D=0.060".Sep 1, 2019 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018020100610Lens · brokenCLEAR EMERGENCY LIGHT LENS BROKEN, REPLACED THE LENS.Jan 31, 2018 · N344NB · Airbus A319114 · Emergency LightingSDR DALA2017101107586Trunnion · wornWEAR ON THE INBD FLAP TRUNNION, LT WING. REPLACED THE LT WING FLAP TRUNNION IAW ERA 561836-14 AD.Oct 10, 2017 · N344NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2017100807384Web · corrodedCORROSION AFT MOVABLE FAIRING HORIZONTAL WEB ON THE LT PYLON, REPLACED THE WEB IAW A319 SRM 51-72-11 AND DRAWING #54510000Oct 7, 2017 · N344NB · Airbus A319114 · Nacelle/Pylon, Main FrameSDR DALA2016112609245Epsu · failedEPSU FAILS STEP 1M AT C1, C2 AND AFT POSITION 13WL, REPLACED AFT POSITION 13WL ESPUNov 25, 2016 · N344NB · Airbus A319114 · Emergency LightingSDR DALA2016111508903Box Beam · not reportedRT SIDE BOX UPPER BEAM FLANGE AT FRAME 43 AFT HOLE REPAIRED PER AMDS 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1Nov 14, 2016 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016111508902Box Beam · not reportedLT SIDE BOX UPPER BEAM FLANGE AT FRAME 43 AFT HOLE. REPAIRED PER 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.Nov 14, 2016 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016050603842Wire · damagedEMERGENCY LIGHT ON SEAT 3B INOPERATIVE, REPAIRED WIRING.May 5, 2016 · N344NB · Airbus A319114 · Light System WiringSDR DALA2015101506157Attach Bracket · crackedRIGHT WING AILERON INBD ACTUATOR ATTACH BRACKET OTBD LUG IS CRACKED, MEASURED AT .610". REPLACED RT WING INBD AILERON ACTUATOR ATTACH BRACKET IAW SRM 51-42-11.Oct 14, 2015 · N344NB · Airbus A319114 · Wing, Control Surface Attach FittingsSDR DALA2015101506156Panel · damagedAFT CARGO SLOPING PANEL 162BF, DAMAGED. FABRICATED A NEW PANEL IAW DWG NW3D25-40532. INSTALLED IAW AMM 53-42-17.Oct 14, 2015 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2015101506155Floor Panel · damagedAFT CARGO FLOOR PANEL 161CF, DAMAGED. FABRICATED A NEW FLOOR PANEL IAW DWG NW3D25-40532. INSTALLED IAW AMM 53-42-17.Oct 14, 2015 · N344NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2015101406154Floor Panel · delaminatedFORWARD CARGO FLOOR PANEL 131EG DELAMINATED & DAMAGED FASTENER HOLES. FABRICATED NEW FLOOR PANEL IAW DWG NW3D25-40532.Oct 13, 2015 · N344NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2015030101756Wire · brokenEMERGENCY LIGHT BROKEN AT SEAT 14 ABC, REPAIRED WIRE AT SEAT 14ABC.Mar 1, 2015 · N344NB · Airbus A319114 · Light System WiringSDR DALA2014092405206Connector · damagedEMERGENCY LIGHT AT ROW 10 INOPERATIVE. FOUND PIN PUSHED OUT AT CONNECTOR. RESEATED PIN, OPS CHECKED NORMAL.Sep 23, 2014 · N344NB · Airbus A319114 · Light System WiringSDR DALA14033073144Sign · inoperativeR1 DOOR LOWER EMERGENCY EXIT SIGN INOPERATIVE. REPLACED EXIT SIGN ASSY IAW AMM 33-51, OPS CHECKED GOOD.Jun 1, 2014 · N344NB · Airbus A319114 · Emergency LightingSDR DALA13066613144Sill · corrodedCORROSION ON LOWER SILL OF L2 DOOR BETWEEN FRAMES 65+23 TO 68+6. REPLACED SILL IAW SRM 51-72-11 AND DWG D53480505.Dec 5, 2013 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13066603144Shear Plate · corrodedCORROSION ON SHEAR PLATE BETWEEN FRAME 69 TO 70 STRINGER 23R AFT PAX CABIN . REPLACED SHEAR PLATE IAW SRM 51-72-11 AND DWG D53474180.Dec 4, 2013 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13065843144Skin · dentedDURING THE CURRENT M-CHECK ON THE SUBJECT ACFT, A DENT WAS FOUND ON THE EXTERNAL SKIN BETWEEN FRAMES 8-9 AND STRG 30L AND 31L. DAMAGED AREA TRIMMED OUT AND REPAIR ACCOMPLISHED IAW ERA 520658 -14, SECTION I. ERA 520658-14, SECTION I ACCOMPLISHED DURING MAINTEDec 2, 2013 · N344NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13065833144Skin · dentedDENT ON EXTERNAL REAR FUSELAGE SKIN AT FRAME 68+14" BETWEEN STR 16R AND STR 17R. REMOVED PAINT BY CHEMICAL METHOD IAW SRM 51-75-11. AFTER REMOVED PAINT, PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND DENT ONLY EXISTING REWORK. EDDY CURRENT INSPECTION DONDec 1, 2013 · N344NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13065283144Sill · corrodedCORROSION ON LOWER R2 DOOR SILL BETWEEN FRAMES 65+23" TO 68+6". REPLACED LOWER SILL IAW SRM 51-72-11 AND DWG D53480505.Nov 30, 2013 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13064113144Shear Plate · corrodedCORROSION ON SHEAR PLATE IN FWD CARGO BAY FRAME 28 S41-42R. REPLACED SHEAR PLATE IAW SRM 51-72-11 AND DWG D53231582.Nov 25, 2013 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13063993144Seat Track · corrodedCORROSION ON SEAT TRACK -Y765, FRAME 59+19. UPPER FLANGE AND BOTTOM SURFACE. REPAIRED SEAT TRACK IAW SRM 53-41-15, PARA 5B, FIG 202.Nov 22, 2013 · N344NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA13063953144Floor Panel · perforatedPERFORATION ON FLOOR PANEL 151PE IN AFT CARGO BAY. REPAIRED FLOOR PANEL IAW SRM 53-02-00, PAR. 8C.Nov 21, 2013 · N344NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13063943144Floor Panel · perforatedPERFORATION ON FLOOR PANEL 162CF IN AFT CARGO BAY. REPAIRED FLOOR PANEL IAW SRM 53-02-00, PAR. 8C .Nov 21, 2013 · N344NB · Airbus A319114 · Fuselage Floor PanelSDR DALA13063933144Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1162 FRAMES 67+17" - 69+4" REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.Nov 21, 2013 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13063923144Floor Support · corrodedCORROSION ON FLOOR SUPPORT FRAMES 66+5" - 67+17" -Y1292 REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.Nov 21, 2013 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13063443144Floor Support · corrodedCORROSION FOUND ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 66+5", -Y765. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472229.Nov 21, 2013 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13064123144Skin · dentedDENT ON EXTERNAL SKIN AT LEVEL FRAME 13 AND BETWEEN S23-24L. FOUND WITHIN LIMITS IAW SRM 53-11-11, PAR 4.B, FIG.104, DIAGRAM 102. PERFORMED DRESS-OUT IAW 51-73-00, PAR.7A AND 53-11-11 4F.Nov 20, 2013 · N344NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA13063893144Floor Support · corrodedCORROSION ON FLOOR SUPPORT FRAMES 64 - 66+5" -Y1292. REPLACED FLOOR SUPORT IAW, SRM 51-72-11, DWG D53472832. AND DWG D53472816.Nov 20, 2013 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13063273144Floor Support · corrodedCORROSION ON FLOOR SUPPORT BETWEEN FRAMES 64 TO 66+5", Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.Nov 20, 2013 · N344NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA13063263144Floor Support · corrodedCORROSION ON FLOOR SUPPORT Y1292 BETWEEN FRAMES 66+5" AND 67+17 ". REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG NR D53472845.Nov 20, 2013 · N344NB · Airbus A319114 · Fuselage Miscellaneous Structure
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