N301NB

Service difficulty reports · 169

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 = 'N301NB' 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 DALA2022031001590None · noneCOLDWORK HOLE 8 AND HOLE 9 IN ACCORDANCE WITH WORK CARD 5311- 01171-03A PRIOR TO FURTHER FLIGHT IS REQUIRED. AA 5311-01171, SB A320-53-1264, AD-2018-06-04. PERFORMED COLDWORK HOLE 8 AND HOLE 9 LOC. FR35LH-FR36LH PRESSURE PANEL AND LONGITUDINAL BEAM IN ACCORDANMar 9, 2022 · N301NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2022031101606None · noneSHIP 3101 COMPLY WITH INSPECTION PER ERA 554182-14 REV B (MAJOR REPAIR) CORRECTIVE ACTION: COMPLIED WITH INSPECTION. (1471164)Feb 1, 2020 · N301NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2019091605336Trunnion · wornWHILE WORKING INSP.32 AD FLAP TRUNION DRV/ SLIDE PANEL LT. FOUND DAMAGE OUT SIDE OF INSPECTION AREA. BLENDED OUT DAMAGE IAW CMM 57-52-21 AND SRM 51-73-00-801. REMOVED .120 ", 1" BY 2.5" PER ENGINEERING. HFEC NEEDS ACCOMPLISHED TO VERIFY NO CRACKS. NO FAULTS FOSep 15, 2019 · N301NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2019091505335Trunnion · wornA/C 3101 CLOSED LOG 1271818 FLT/CHK 2170. REF LP 6334545 LT IB FLAP TRUNION WEAR OUT OF LIMITS. REFERENCE LOG 6334545. ERA 581355-14AD, PRI, CARD# 5751-01025-01C, AMDS 2750-1010 LT AND 2750-6010-LT, FOR ALL WORK ACCOMPLISHED. REPLACED THE DRIVE TRUNNION ASSEMBSep 15, 2019 · N301NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2019042202539Cover · missingPDA PART DEPARTED AIRCRAFT. A/C 3101 CLOSED LOG 4002230. FLT/CHK 1496. 1 FLAP TRACK MOVEABLE FAIRING PIVOT COVER MISSING. INSTALLED REPLACEMENT COVER PER A319 AMM 27-50-00.Apr 19, 2019 · N301NB · Airbus A319114 · Trailing Edge FlapsSDR DALA2018010200014Battery Pack · inoperativeDURING EMERGENCY BATTERY PACK CHARGE, FOUND THE LEFT AFT DOOR SLIDE BATTERY PACK BAD. REMOVED AND REPLACED THE SLIDE.Dec 30, 2017 · N301NB · Airbus A319114 · Escape SlideSDR DALA2017121808673Stringer · corrodedAFTER REMOVAL OF OUTFLOW VALVE, FOUND CORROSION ON STRINGER 31R BETWEEN FRAMES 65-66, REPAIRED IAW ER/A 564294-14 REV ORIGINAL, AND PRI 564294-14 REV ORIGINAL.Dec 17, 2017 · N301NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2016110808685Box Beam · crackedLEFT SIDE BOX BEAM UPPER FLANGE TOP HOLE IN PRESSURE PLATE HAS A CRACK, REPLACED IAW AMDS 5310-01450-02.Nov 7, 2016 · N301NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2016110808684Box Beam · crackedLEFT SIDE BOX BEAM UPPER FLANGE TOP HOLE IN FRAME HAS CRACK, . REPAIR IAW AMDS 5310-01450-02.Nov 7, 2016 · N301NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2018110606457Hinge Arm · gougedRH HORIZONTAL STABILIZER / ELEVATOR HINGE ARM 4 GOUGED; PERFORMED PERMANENT REPAIRED #4 HINGE FITTING P/N D55981522003 IAW DELTA ER/A 546039-14, REV ''O'' SECTION 1May 20, 2016 · N301NB · Airbus A319114 · Horizontal Stabilizer StructureSDR DALA2016051704018Skin · dentedLEFT WING, NR 1 L/E SLAT, DENT UPPER NOSE SKIN, JUST INBD OF MID-POINT, REPAIRED IAW SRM 57-40-00, FIG 205.May 16, 2016 · N301NB · Airbus A319114 · Leading Edge DevicesSDR DALA2016050903841Pin · corrodedLEFT MLG PINTLE PIN CORRODED AT ATTACH LUG, REPLACED PINTLE PIN WITH NEW PN 201173600.May 8, 2016 · N301NB · Airbus A319114 · Fuselage, Landing Gear Attach FittingsSDR DALA2016050303653Floor Support · corrodedFWD CABIN FLOOR SUPPORT 1292 BETWEEN FRAME 14 AND 21, TOP SURFACE, HAS 3 AREAS CORRODED, REPLACED FWD CABIN SUPPORT, SEAT TRACK, 1292, BETWEEN FRAME 14 AND FRAME 21 IAW SRM 53-11-15.May 1, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016050303651Floor Support · corrodedFWD CABIN FLOOR SUPPORT AT 81 BETWEEN FRAME 12 AND 16, HAS 3 AREAS OF CORROSION, REMOVED 0.011" MATERIAL, CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.May 1, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016050303650Floor Support · corrodedFWD CABIN FLOOR SUPPORT 254 HAS 5 AREAS CORRODED FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.May 1, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016050303649Floor Support · corrodedFWD CABIN FLOOR SUPPORT ATTACHED ANGLE PROFILER BETWEEN FRAME 12 AND FRAME 13, BETWEEN 1292 AND 1732, LOWER FLANGE TOP SURFACE CORRODED. BLENDED OUT CORROSION IAW SRM 51-73-00, FOUND 100 PERCENT MATERIAL LOSS, OUT OF LIMITS IAW SRM 53-00-14. R & R ATTACHED ANMay 1, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016050303648Floor Support · corrodedL1 PAX DOOR LOWER CUTOUT FLOORBOARD ATTACHMENT FITTING AT FRAME 18 - 20, SEVERAL SPOTS HAVE CORROSION. REPLACED FLOOR SUPPORT IAW SRM 51-44-11.May 1, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016050303656Not Reported · corrodedREMOVED CORROSION IN SEVERAL LOCATIONS IAW SRM 51-10-02. CHECKED LIMITS, LOCATIONS 3 & 6 FOUND TO BE OUT OF LIMITS, D=0.034" REMAINING MATERIAL 0.029", ORIGINAL MATERIAL 0.063". REMAINING MAT. 0.093", ORIGINAL MATERIAL 0.150", IAW SRM 53-41-14, FIG 101, SH.1.Apr 30, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016050303655Floorbeam · corrodedFRAME 68, FLOORBEAM 1292 IS CORRODED. REMOVED AND INSTALLED NEW FLOORBEAM, IAW SRM 51-42-11.Apr 30, 2016 · N301NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2016050303654Floor Support · corrodedBETWEEN FR 67-68, FLOOR SUPPORT 1292 IS CORRODED. REMOVED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11.Apr 30, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016050303652Web · corrodedCABIN FLOOR WEB BETWEEN FRAME 20, FRAME 21, 1732 CORRODED. R & R CABIN FLOOR WEB FRAME 20-33, +Y1732, IAW SRM 51-42-11, 51-44-11, PN D5311278520201.Apr 29, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016043003484Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT 765 BETWEEN FRAME 12 AND 23 TOP SURFACE HAS 4 AREAS CORRODED. REPLACED FLOOR SUPPORT, BEAM, TRACK IAW SRM 51-42-11.Apr 29, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016043003483Floor Support · corrodedFWD CABIN FLOOR SUPPORT 81 BETWEEN FRAME 12 AND 14, ATTACHED ANGLE HAS CORROSION. REPLACED FLOOR SUPPORT ANGLE BETWEEN FRAME 12 AND 14, PN IAW SRM 51-42-11.Apr 29, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016043003482Floor Support · corrodedRIGHT SIDE FLOOR SUPPORT BETWEEN FRAME 66-67, 1292 IS CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.Apr 29, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016043003481Floorbeam · corrodedRT SIDE FRAME 68, -1292 FLOORBEAM IS CORRODED. REPLACED FLOORBEAM IAW 51-42-11.Apr 29, 2016 · N301NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2016043003480Floor Support · corrodedFWD CABIN FLOOR SUPPORT 254 BETWEEN FRAME 18 AND 20 TOP SURFACE HAS 2 AREAS CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS 1" X .5" 100 PERCENT MATERIAL LOSS. REPLACED FLOORBEAM IAW SRM 51-42-11.Apr 29, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016043003479Attach Angle · corrodedFWD CABIN FLOOR SUPPORT WEB Y 1732 BETWEEN FRAME 20 AND 21 ATTACH ANGLE PROFILE CORRODED. REMOVED CORROSION IAW SRM 51-22-11, NO LIMITS FOUND ON THE SRM, R & R FLOOR SUPPORT WEB AND ANGLE IAW SRM 51-42-11.Apr 29, 2016 · N301NB · Airbus A319114 · Fuselage Main, Attach FittingsSDR DALA2016043003485Tray · crackedAFT CABIN TRAY, FRAMES 68-69 IS CRACKED. INSTALLED NEW TRAY IAW SRM 51-42-11.Apr 29, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016042803435Floor Support · corrodedFWD CABIN FLOOR SUPPORT Y+503 BETWEEN FRAMES 12 - 16 SIX AREAS CORRODED. REMOVED FLOOR SUPPORT ASSY DUE OUT OF LIMITS CORROSION IAW SRM 53-11-14 &51-42-11, LOCATED AND DRILLED NEW SUPPORT BEAM IAW SRM 51-44-11. INSTALLED NEW SUPPORT BEAM IAW SRM 51-42-11.Apr 27, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016042803434Floor Support · corrodedFWD CABIN FLOOR SUPPORT FRAMES 20 - 21 TOP SURFACE HAS TWO AREAS CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM A319 51-42-11 AND TRM 53-21-01.Apr 27, 2016 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2016042303174Floor Panel · corrodedAFT CABIN FLOOR PANEL 261FF HAS CORROSION. NEW FLOOR PANEL INSTALLED.Apr 22, 2016 · N301NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2015101306158Battery Pack · failedFORWARD EMERGENCY BATTERY FAILED. REPLACED FWD EMERGENCY BATTERY.Oct 12, 2015 · N301NB · Airbus A319114 · Emergency LightingSDR DALA13020783101Light · inoperativeSEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT ROW 15ABC. R & R ESCAPE LIGHT ASSY. OPS CHECKED GOOD.May 2, 2013 · N301NB · Airbus A319114 · Emergency LightingSDR DALA13040173101Frame · corrodedFRAME 20 CORRODED. OPENSep 7, 2012 · N301NB · Airbus A319114 · Fuselage Main, FrameSDR DALA12001833101Wire Harness · disconnectedEMERGENCY ESCAPE PATH LIGHTING OUT AT SEATS 13A AND 19A. FOUND HARNESS LOOSE AND SEATS 13A AND 19A. CONNECTED WIRE HARNESS AND SECURED. EMERGENCY LIGHTS OPS CHECKED GOOD. OK FOR SERVICE.Jun 19, 2012 · N301NB · Airbus A319114 · Light System WiringSDR DALA12000173101Light · detachedSEAT 1B EMERGENCY MOUNTED LIGHT IS DAMAGED AND INOPERATIVE. ATTACHED LIGHT. OPS CHECKED GOOD. OK FOR SERVICE.May 19, 2012 · N301NB · Airbus A319114 · Emergency LightingSDR DALA1136003101Wire · damagedDURING EMERGENCY LIGHT TEST UPPER RED EXIT LIGHT ROW 9L INOPERATIVE, REPAIRED WIRE AND TESTS OK.May 20, 2011 · N301NB · Airbus A319114 · Light System WiringSDR DALA1114653101Wire · brokenDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 13 ABC INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.Mar 1, 2011 · N301NB · Airbus A319114 · Emergency LightingSDR DALA1022693101Skin · damagedDURING M-CHECK FOUND R2 DOOR LOWER CUT OUT EXTERNAL SKIN HAD 8 EA ELONGATED HOLES. REPAIRED IAW SRM 51-90-00, SRM 51-10-01, SRM 51-10-08 & ERA 484908-14.Sep 14, 2010 · N301NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA1022093101Door Frame · corrodedDURING M-CHECK FOUND CORROSION ON DOOR R1 DOOR FRAME 20 AT CABIN FLOOR LINE. REPAIRED IAW NTM 51-10-08, NTM 51-10-02. INDENTIFIED REPAIR AS ENGINEERING APPROVED TIME LIMITED REPAIR IAW ERA 484247-14, SECTION I. INSP TO BE ACCOMPLISHED EVERY 500 FLIGHT CYCLESSep 10, 2010 · N301NB · Airbus A319114 · Fuselage Main, StructureSDR DALA1021993101Mount · gougedDURING M-CHECK FOUND GOUGE IN AFT MOUNT FITTING OF AFT RT ENGINE PYLON MOUNT ADJACENT TO SAFETY WIRE HOLE FOR INBD ATTACH BOLT. REPAIRED IAW ERA 484250-14 SECTION I, SECTION II REQUIRES MFG APPROVAL OF REPAIR WITHIN 6 MONTHS.Sep 9, 2010 · N301NB · Airbus A319114 · Nacelle/Pylon, Attach FittingsSDR DALA1021973101Mount · gougedDURING M-CHECK FOUND GOUGES IN NR 1 PYLON ENGINE MOUNT OTBD SIDE ADJACENT TO SAFETY WIRE HOLE FOR AFT MOUNT BOLT. REPAIRED IAW ERA 484227-14 SECTION I, SECTION II REQUIRES APPROVAL OF REPAIR WITHIN 6 MONTHS.Sep 9, 2010 · N301NB · Airbus A319114 · Engine Mount SectionSDR DALA1021963101Mount · gougedDURING M-CHECK FOUND GOUGE IN NR 1 PYLON AFT ENGINE MOUNT INBD SIDE ADJACENT TO SAFETY WIRE HOLE FOR AFT MOUNT BOLT. REPAIRED IAW ERA 484227-14 SECTION I, SECTION II REQUIRES APPROVAL OF REPAIR WITHIN 6 MONTHS.Sep 9, 2010 · N301NB · Airbus A319114 · Engine Mount SectionSDR DALA1021723101Sill · corrodedDURING M-CHECK FOUND CORROSION ON AFT RT AFT DOOR SILL. REPAIRED IAW SRM 51-44-11, SRM 51-42-11.Sep 8, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021753101Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT AT Y1292 BETWEEN FR 66- FR 68. REPAIRED IAW SRM 51-44-11, SRM 51-42-11 & TRM 53-21-01.Sep 8, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021743101Floor Support · corrodedDURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT -Y1292 BETWEEN FR 67 & FR 68. REPAIRED IAW SRM 51-44-11, SRM 51-42-11 & TRM 53-21-01.Sep 8, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021173101Support · corrodedDURING M-CHECK FOUND CORROSION ON RT SHEAR PLATE SUPPORT AT FR69-FR70. REPAIRED IAW SRM 51-42-11, SRM 51-44-11.Sep 5, 2010 · N301NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1021163101Floor Panel · dentedDURING M-CHECK, FOUND DENTS ON FLOOR PANEL 151ZG. REPLACED FLOOR PANEL IAW DWG 3D25-40532.Sep 4, 2010 · N301NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1021133101Floor Panel · dentedAFT CARGO COMPARTMENT FLOOR PANEL NR 161PF HAS SEVERAL DENTS. FABRICATED NEW PANEL ON STAM TRAVELER NR T10/848931 IAW DWG 3D25-40532.Sep 2, 2010 · N301NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1021123101Floorboard · debondedAFT CARGO COMPARTMENT FLOORBOARD NR151PE HAS DEBONDED DAMAGE ALONG AFT EDGE. FABRICATED NEW PANEL ON STAM TRAVELER NR T10/848917 IAW DWG 3D25-40532.Sep 2, 2010 · N301NB · Airbus A319114 · Fuselage Floor Panel
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