N320NB

Service difficulty reports · 221

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 = 'N320NB' 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 DALA2020092803189Engine · failedATB/DE DECLARED EMERGENCY AND PERFORMED ATB DUE TO NUMBER 1 ENGINE FAILURE. A/C RETURNED WITH OUT FURTHER INCIDENT. MAINTENANCE FOUND DEBRIS IN THE TAILPIPE AND THE ENGINE WILL NOT TURN. CORRECTIVE ACTION: FOUND LEFT ENGINE TURBINE AND TAIL CONE DAMAGE WITSep 25, 2020 · N320NB · Airbus A319114 · Engine (Turbine/Turboprop)SDR DALA2020012200488Window · crackedCRACK FIXED WINDOW LT SIDE IN COCKPIT. REPLACED FIXED WINDOW LT SIDE IN COCKPIT IAW AMM 56-11-12-400-002-A.Jan 20, 2020 · N320NB · Airbus A319114 · Flight Compartment WindowsSDR DALA2020012000387Frame · crackedCRACK INDICATION ON FRAME 36 THAT EXCEEDS THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE PANEL BETWEEN FR35L AND FR36L. ENGINEERING CORRECTIVE ACTION IS REQUIRED PRIOR TO FURTHER FLIGHT. AA 5311-01171. SB A320-53-1263. AD-2018-06-04. IN FWD CARGO CJan 19, 2020 · N320NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2020012000386Frame · crackedCRACK INDICATION ON FRAME 36 LT SIDE IN OPEN O/B HOLE A. REPAIR IN ACCORDANCE WITH WORK CARD 5311-01171-04A PRIOR TO FURTHER FLIGHT, AA 5311-01171, SB A320-53-1264, AD-2018-06-04 IN AIR CONDITIONING BAY (2 EA) D=0.135 INCH. (CRACK DIRECTIONS 6 AND 12 O CLOCK VJan 19, 2020 · N320NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2020010900153Intercostal · crackedCRACK INDICATION ON FRAME 16 RH SIDE AT OPEN FASTENER HOLE LWR IB IN DOOR STOP 7, CRACK INDICATION FOUND IN INTERCOSTAL LAYER ONLY. CRACK DIRECTION ARE 10 AND 11 OCLOCK. AT FWD GALLEY AREA (2 EA). REPLACED INTERCOSTAL AND FASTENERS LOCATED FRAME 16 R/H SIDE ATJan 7, 2020 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2020010900152Intercostal · crackedCRACK INDICATION ON FRAME 16 RH SIDE AT OPEN FASTENER HOLE UP IB IN DOOR STOP 7, CRACK INDICATION FOUND IN INTERCOSTAL LAYER ONLY. CRACK DIRECTION ARE 9, 10 AND 12 OCLOCK. AT FWD GALLEY AREA (1 EA). REPLACED INTERCOSTAL AND FASTENERS LOCATED FRAME 16 R/H SIDE Jan 7, 2020 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2020010900151Intercostal · crackedCRACK INDICATION ON FRAME 16 RH SIDE AT OPEN FASTENER HOLE LWR IB IN DOOR STOP 1, CRACK INDICATION FOUND IN INTERCOSTAL LAYER ONLY. CRACK DIRECTION IS 9 OCLOCK. AT FWD GALLEY AREA (1 EA). REPLACED INTERCOSTAL FITTING ON FRAME 16 RH SIDE AT LEVEL DOOR STOP #1 AJan 7, 2020 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2019122307485Indicator · inoperativeSLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:607 / ACARS TEXT: FRC527102607 2L DOOR SHOWS DISARMEDON ECAM DOOR PAGE. FAREPORTS DOOR IS ARMED. / INTERIOR. CLEANED AND ADJUSTED GIRT BAR AND SENSORS PER A319 AMM 52-71-00. PRESSURIZED A/C PER A219 AMM 05-53. Dec 20, 2019 · N320NB · Airbus A319114 · Emergency EquipmentSDR DALA201812036995Flap · wornDURING FLAP/TRUNNIONS SLIDING PANEL INSPECTION FOUND NEW WEAR IN AD AREA, REPAIR REF ER/A 573428-14ADNov 30, 2018 · N320NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2018012400455Window Frame · crackedCRACK INDICATION ON THE WINDOW FRAME STIFFENER, REPLACED THE WINDOW FRAME IAW PRI 563907-14, REV 0, PRI:563907-14, REV 1, PRI 563907, REV 2, AND ER/A 563907-14AD.Jan 23, 2018 · N320NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2018011400265Door Frame · crackedCRACKED EMERGENCY EXIT DOOR FRAME. , REPLACED THE DOOR FRAME IAW SRM 51-72-11, AND DRAWING D52279010.Jan 13, 2018 · N320NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2018011400264Door Frame · crackedCRACKED EMERGENCY EXIT DOOR FRAME, REPLACED THE DOOR FRAME IAW SRM 51-72-11, AND DRAWING D52279010.Jan 13, 2018 · N320NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2018011300263Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT +Y765, FRAMES 20 TO 21, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53112813.Jan 12, 2018 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018010900162Floor Support · corrodedCORRODED FLOOR SUPPORT Y503.2, FRAME 16. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING D53112825Jan 8, 2018 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018010900161Floor Support · corrodedCORRODED FLOOR SUPPORT, -Y765, FRAMES 20 TO 21, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53112812Jan 8, 2018 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018010900160Floor Support · corrodedCORRODED FLOOR SUPPORT -Y1292, FRAMES 20 TO 21, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DRAWING D53112812Jan 8, 2018 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018010700115Floor Support · corrodedCORROSION FLOOR SUPPORT AT THE FWD GALLEY, -Y189, FRAME 21. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 20 TO 24 IAW SRM 51-72-11, AND DWG D53111406.Jan 6, 2018 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018010600114Web · corrodedCORROSION ON THE WEB, FRAMES 69 TO 70, IN THE AFT GALLEY AREA, REPLACED WEB IAW SRM 51-72-11, AND DWG D53474180.Jan 5, 2018 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018010400065Floor Support · corrodedFLOOR SUPPORT CORRODED, -Y1292, FRAME 68, REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 67+15 TO 69 IAW SRM 51-72-11, AND DWG D53472089.Jan 4, 2018 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018010400064Floor Support · corrodedFLOOR SUPPORT CORRODED, -Y1292, FR 67+15. REPLACED THE FLOORBEAM BETWEEN FRAMES 66 TO 68-3 IAW SRM 51-72-11 AND DWG D5347816.Jan 3, 2018 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018010700116Web · corrodedCORROSION ON THE FLOOR WEB BETWEEN FRAMES 69 TO 70 IN THE AFT GALLEY AREA, REPLACED THE WEB IAW SRM 51-72-11, AND DWG D53474180.Jan 2, 2018 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2017080106129Unknown · odorSTRONG ODOR FILLED COCKPIT AND CABIN WHEN LEFT PACK TURN ON, SUSPECT OZONE FILTER, R/R OZONE FILTER.Jul 31, 2017 · N320NB · Airbus A319114 · Air Distribution SystemSDR DALA2017071805525Apu · malfunctionedDIRTY SOCK SMELL IN CABIN, FOUND OIL IN AIR PLENUM DUCT AND AIR INLET. REPLACED APU.Jul 14, 2017 · N320NB · Airbus A319114 · APU Core EngineSDR DALA2017041703157Box Beam · crackedLEFT BOX BEAM FLANGE AT FRAME 43 HAD A CRACK INDICATION. REPAIRED IAW 5310-01450-02.Apr 16, 2017 · N320NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2017041703156Box Beam · crackedRT BOX BEAM FLANGE AT FRAME 43 HAD A CRACK INDICATION. REPAIRED IAW 5310-01450-02.Apr 16, 2017 · N320NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2015022701755Power Supply · no testEMERGENCY LIGHT TEST FAIL, REPLACED EPSU AFT LT.Feb 27, 2015 · N320NB · Airbus A319114 · Emergency LightingSDR DALA2015022201625Power Supply · inoperativeAFT EPSU INTERNAL FAILURE, REPLACED 13WL EPSU.Feb 19, 2015 · N320NB · Airbus A319114 · Emergency LightingSDR DALA2014102805782Light · inoperativeEMERGENCY SEAT MOUNTED LIGHT INOPERATIVE, REPLACED THE LIGHT.Oct 27, 2014 · N320NB · Airbus A319114 · Emergency LightingSDR DALA2016112309190Skin · corrodedFOUND CORROSION IN THE AREA OF THE AFT WIFI ANTENNA, BETWEEN FRAMES 59 & 60, STR 43L. REMOVED CORROSION, FABRICATED REPAIR PARTS, TREATED AND PRIMED, INSTALLED REPAIR PARTS. LP#1626149Sep 17, 2014 · N320NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA14010953120Skin · scratchedTHREE SCRATCHES ON EXTERNAL SKIN BETWEEN FRAMES 61 - 62 S23 - 24L AFT FUSELAGE. PERFORMED REPAIR IAW SRM 53-00-11.Feb 19, 2014 · N320NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA14003323120Wire · brokenEMERGENCY PATH LIGHTING INOPERATIVE AT SEATS 5A AND 8A. REPAIRED BROKEN WIRE IAW ESPM 20-10. OPS GOOD.Jan 11, 2014 · N320NB · Airbus A319114 · Light System WiringSDR DALA13060903120Connector · unsecureFOUND EMERGENCY LIGHT AT ROW 10 INOPERATIVE. FOUND CONNECTOR NOT FULLY SEATED. SECURED CONNECTOR. LIGHT OPS NORMAL. OK FOR SERVICE.Nov 12, 2013 · N320NB · Airbus A319114 · Emergency LightingSDR DALA13009793120Wire · brokenFLOOR PROXIMITY EMERGENCY EXIT PATH LIGHT WIRE BROKEN. REPLACED WIRE HARNESS AT SEAT 4ABC. LIGHTS OPS CK GOOD. OK FOR SERVICE.Mar 1, 2013 · N320NB · Airbus A319114 · Light System WiringSDR DALA1224493120Connector · damagedAIRCRAFT 3120. SEATS 7C AND 8C EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE. FOUND PINS PUSHED BACK IN RECEPTACLE BROKEN. REPLACED RECEPTACLE CONNECTOR PER ESPMAND AMM. SECURED 6A LOWER SIDEWALL PANEL. OK FOR SERVICE.Apr 17, 2012 · N320NB · Airbus A319114 · Light System WiringSDR DALA1219223120Floor Support · corrodedAFT CABIN FLOOR SUPPORT -Y465 BETWEEN FR 65 TO FR 66 CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00. L=1.2" W=3.0" D=0.050" ORIGINAL MATERIAL 0.165". OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102 PAGE 106. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW A319 SMar 25, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1219343120Floor Support · corrodedFORWARD MAIN CABIN FLOOR SUPPORT BEAM AT FR 20 -Y765 HAS CORROSION. REMOVED OLD FLOOR SUPPORT IAW A319 SRM 51-42-11. RECEIVED NEW FLOORBEAM. LOCATED AND DRILLED NEW FLOOR SUPPORT IAW A319 SRM 51-44-11. TRANSFERRED BRACKETS IAW A319 SRM 51-42-11. INSTALLEMar 24, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1219333120Floor Support · corrodedAFT CABIN FLOOR SUPPORT -Y1292 BETWEEN FR 66 TO FR 68 CORRODED. SSI 534147. BLENDED AREA IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 53-00-14 FIG 102. REMOVED FLOOR SUPP IAW A319 SRM 51-42-11. INSTALLED FLOOR NEW SUPP IAW A319 SRM 51-42-11. Mar 24, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1219313120Floor Support · corrodedAFT CABIN FLOOR SUPPORT -Y1292 AT FR 66 CORRODED. SSI 534147. BLENDED AREA IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED FLOOR SUPPORT BEAM IAW A319 SRM 51-42-11. INSTALLED COUPLINGS AND HARD POINTS IAW A319 SRM 51Mar 24, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1219293120Floor Support · corrodedAFT CABIN FLOOR SUPPORT -Y1292 BETWEEN FR 68 TO FR 69 CORRODED. SSI 534147. BLENDED AREA IAW A319 SRM 51-74-00 CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED FLOOR SUPPORT AND INSTALLED FLOOR SUPPORT IAW A319 SRM 51-42-11.Mar 24, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1219183120Floor Support · corrodedFORWARD MAIN CABIN FLOOR SUPPORT BEAM AT FR20 -Y1292 HAS CORROSION. SSI 531189. BLENDED AREA IAW A319 SRM 51-74-00. MEASUREMENTS AS FOLLOWS L=3",W=2",W=.073" ORIG MAT.075". MAX DEPTH ALLOWED IS .031". FOUND TO BE OUT LIMITS IAW A319 SRM 53-11-15 FIG 104.Mar 23, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1219163120Floor Support · corrodedAFT CABIN FLOOR SUPPORT +Y1292 BETWEEN FR 66 TO FR 68 CORRODED. SSI 534147. BLENDED AREA IAW A319 SRM 51-73-00 L=.087"W=1.2"D=.027"ORG MAT .087" FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED FLOOR SUPPORT BEAM IAW A319 51-42-11. LOCATED Mar 23, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1219013120Floor Support · corrodedAFT CABIN FLOOR SUPPORT +Y1292 AT FR 66 CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00 L=2.0" W=1.5"D=.062" FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED FLOOR SUPPORT IAW A319 SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT IAW A319 SRM 51-Mar 23, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1219003120Floor Support · corrodedAFT CABIN FLOOR SUPPORT +Y1292 AT FR 68 CORRODED. BLENDED AREA IAW A319 SRM 51-73-00 L=1.5"W=1.0"D=.082" ORIG MAT 0.157" FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED OLD FLOOR SUPPORT IAW A319 SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT IAMar 23, 2012 · N320NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1218993120Floor Panel · delaminatedFLOOR PANEL 261PF IS DELAMINATED. N/R 250/18. FABRICATED FLOOR PANEL 261PF PER DWG 3D25-40640. DAMAGE DIM L=6" W=1".Mar 22, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1218983120Floor Panel · delaminatedFLOOR PANEL 261HG IS DELAMINATED. N/R 250/12. FABRICATED FLOOR PANEL 261HG PER DWG 3D25-40640. DAMAGE DIM:L=2.0" W=1.5".Mar 22, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1218973120Floor Panel · delaminatedFLOOR PANEL 262HG IS DELAMINATED. N/R 250/18. FABRICATED FLOOR PANEL 262HG PER DWG 3D25-40640.Mar 22, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1218963120Floor Panel · delaminatedFLOOR PANEL 232FF IS DELAMINATED N/R 230/41. FABRICATED FLOOR PANEL 232FF PER DWG 3D25-40640. DAMAGE DIM: L=3.0" W=1.0".Mar 22, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1218953120Floor Panel · delaminatedFLOOR PANEL 262EF IS DELAMINATED LOWER SURF. N/R 250/16. FABRICATED FLOOR PANEL 262EF PER DWG 3D25-40640. DAMAGE DIM: L=2.0" W=3.0".Mar 22, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1218943120Floor Panel · delaminatedFLOOR PANEL 261EF IS DELAMINATED N/R 250/14. FABRICATED FLOOR PANEL 261EF PER DWG 3D25-40640. DAMAGE DIM: L=4.0" W=5.0".Mar 22, 2012 · N320NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1218933120Floor Panel · damagedCENTER CABIN FLOOR PANEL 241MF HAS EDGE DAMAGE. FABRICATED FLOOR PANEL 241MF PER DWG 3D25-40640. DAMAGE DIM:L=3" W=2".Mar 22, 2012 · N320NB · Airbus A319114 · Fuselage Floor Panel
Back to N320NB