N365NB

Service difficulty reports · 132

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 = 'N365NB' 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 DALA2020092103147Warning Message · false activationECAM; DOOR LT EMER EXIT ILLUMINATED. ECAM AND QRH COMPLIED WITH. ILLUMINATED AT 8000 MSL DESCENDING, WENT OUT ON IT'S OWN AT 5000 MSL. CORRECTIVE ACTION: INSPECTED DOOR FOR FAIRING TO FUSELAGE AND DOOR LATCHING. DOOR IS LOCKED AND SECURE. CREW REPORTED PESep 20, 2020 · N365NB · Airbus A319114 · Door Warning SystemSDR DALA2020092103141Warning Message · false activationLEFT EMERG EXIT MESSAGE ON DURING DESCENT THROUGH 14000', LIGHT WENT OUT BELOW 7000'. PER QRH, NO V/S CHANGE IN CABIN ALTITUDE. CORRECTIVE ACTION: REMOVED DOOR AND INSPECTED FOR DEFECTS, NONE NOTED. FOUND ACCESS COVER LOOSE AND MISALIGNED AND BELIEVE TO BE Sep 20, 2020 · N365NB · Airbus A319114 · Door Warning SystemSDR DALA2020110603617Bushing · corrodedCORROSION ELEVATOR BUSHING HINGE 1 OUTBOARD SIDE ON RT HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED BUSHING (1 EA) ON OUTBOARD LUG OF HINGE FITTING NR 1 RT ELEVATOR, AS PER PRI ERA 533420-14 REV B PRI REV 0 ERA 533420-14 REV B AND A319 SRM 55-26-41-300Sep 12, 2020 · N365NB · Airbus A319114 · Elevator StructureSDR DALA2020091423064Access Panel · damagedSHIP 3165, ELONGATED HOLE FUEL TANK ACCESS PANEL CUT OUT BETWEEN RIB 14 TO RIB 15 ON RT WING. CORRECTIVE ACTION: DEFERRED; MONITORING.Sep 12, 2020 · N365NB · Airbus A319114 · Wing, Plate/SkinSDR DALA2020091423062Stringer · corrodedSHIP 3165, CORROSION STRINGER 39R BETWEEN FR 61 TO FR 65 AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON STRINGER 39R BETWEEN FR 61 TO FR 65 AFT CARGO COMPARTMENT, AS PER PRI 587599-14 REV O PRI 587599-14 REV 1 AND ERA 587599-14 REV ORIGINAL.Sep 11, 2020 · N365NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2020091103046Bushing · corrodedSHIP 3165, CORROSION ELEVATOR ACTUATOR BUSHING INBOARD ON RT HORIZONTAL STABILIZER. CORRECTIVE ACTION: REMOVED AND REPLACED BUSHINGS (2EA) ON INBOARD ACTUATOR RT HORIZONTAL STABILIZER, AS PER AIRBUS CMM 55-21-15.Sep 9, 2020 · N365NB · Airbus A319114 · Elevator StructureSDR DALA2020091103045Power Supply · inoperativeSHIP 3165, INOP EMERGENCY POWER SUPPLY UNIT 10WL FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED EMERGENCY POWER SUPPLY UNIT 10WL FWD GALLEY AREA.Sep 8, 2020 · N365NB · Airbus A319114 · Emergency LightingSDR DALA2020090903015Skin · corrodedSHIP 3165, CORROSION INTERNAL STRUCTURE INTERNAL SKIN LOCATED BETWEEN FR30 TO FR34 AND BETWEEN STRG 41L TO STRG 41R IN FWD CARGO COMPARTMENT. CORRECTVE ACTION: PERFORMED PERMANENT REPAIR, AS PER ER/A NR 587500-14 REVISION ORIGINAL AND PRI NR 587500-14 REVISIOSep 4, 2020 · N365NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2020090953008Frame · crackedSHIP 3165, CRACK INDICATION ON FRAME 20 RT SIDE ON OPEN FASTENER HOLE 1 INTERCOSTAL FITTING LAYER AT DOOR STOP 7, CRACK DIRECTION IS 4 O`CLOCK. CORRECTIVE ACTION: REPLACED INTERCOSTAL FITTING ON FRAME 20 RT SIDE AT LEVEL OF DOOR STOP NR 7, AS PER ER/A N. 5875Sep 4, 2020 · N365NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2020090933005Frame · crackedSHIP 3165, CRACK INDICATION ON FRAME 16 LT SIDE ON OPEN FASTENER HOLE 3 FRAME AND INTERCOSTAL FITTING LAYERS AT DOOR STOP 7. CRACK DIRECTION IS 1 O`CLOCK. CORRECTIVE ACTION: REPLACED ON FRAME 16 LT SIDE INTERCOSTAL FITTING AT DOOR STOP 7, AS PER PRI 587446-1Sep 2, 2020 · N365NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2020090933004Frame · crackedCRACK INDICATION ON FRAME 16 RT SIDE ON OPEN FASTENER HOLES 1 AND 3 INTERCOSTAL FITTING LAYER AT DOOR STOP 7. CRACK DIRECTIONS ARE FOR HOLE 1:6 AND 8 O`CLOCK, FOR HOLE 3:9 AND 10 O`CLOCK. CORRECTIVE ACTION: REPLACED ON FRAME 16 RT SIDE INTERCOSTAL FITTING ATSep 2, 2020 · N365NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2020090923003Frame · crackedCRACK INDICATION ON FRAME 16 RT SIDE HOLE 6 AT DOUBLE JOGGLE AREA AT LEVEL DOOR STOP 7 ON UPPER FUSELAGE (1EA), CRACK AT 1 O'CLOCK. CORRECTIVE ACTION: REPAIRED FR 16 RT SIDE HOLE 6 AT DOUBLE JOGGLE AREA AT LEVEL DOOR STOP 7 ON UPPER FUSELAGE, AS PER PRI 58740Sep 2, 2020 · N365NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2020090923002Frame · crackedCRACK INDICATION ON FRAME 20 AT FASTENER HOLE 6 AT LEVEL OF DOOR STOP 7 RT SIDE. CRACK DIRECTION 10 O`CLOCK VIEW LOOKING INBOARD AND DEPTH IS 0.071 INCH. CORRECTIVE ACTION: PERFORMED REPAIR ON FRAME 20 RT ON FASTENER HOLE NR 6 AT LEVEL OF DOOR STOP NR 7 DOUBSep 2, 2020 · N365NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2020090302947Floor Support · corrodedCORROSION FLOOR BEAM +Y1292 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM +Y1292 LOC. BTW FRAME 64 TO FRAME 66 AT AFT GALLEY AREA AS PER PRI 587501-14 REV "0" AND ER/A 587501-14 REV.ORIGINALSep 2, 2020 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2020090322946Slide · misinstalledIMPROPERLY PACKED PASSENGER CREW DOOR 832 SLIDE RAFT DUE TO TOUCH FUSELAGE IN PASSENGER CABIN . CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 832 SLIDE RAFT IN PASSENGER CABIN THE INSTALLATION IS TO BE ACCOMPLISHED AS PER AMDS CARD #2561-4001-LA.Sep 1, 2020 · N365NB · Airbus A319114 · Escape SlideSDR DALA2020090282923Floor Support · corrodedCORROSION LEVEL: 2 FOUND CORROSION AT FLOOR BEAM +Y1292 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTIION: REPLACED FLOOR BEAM +Y1292 LOCATED BTW FR66 TO FR68 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND DRAWING D53472780, ISSUE KAug 27, 2020 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2020090262919Floor Support · corrodedCORROSION FLOOR BEAM -Y1292 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1292 LOCATED BTW FR.64 TO FR.66 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND DRAWING #D53472000, ISSUE:AF, RELEASE DATE:06-JAN-03.Aug 25, 2020 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2020090262918Floor Support · corrodedCORROSION FLOOR BEAM -Y1162 LOCATED BTW FR 67 TO FR 69 AT AFT GALLEY AREA . CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1162 LOCATED BTW FR.67 TO FR.69 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND DRAWING # D53472780, ISSUE "J" RELEASE DATE:26-APR-18.Aug 25, 2020 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA202008242846Seat Track · corrodedCORROSION FLOOR STRUCTURE LOCATED AT FR 20 AND -Y765 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE (SEAT TRACK) LOC AT FR 12 TO FR24 -Y765 IN PASSENGER CABIN ASPER A319 SRM 51-72-11, 51-42-11 AND DRAWING #D53112812 RELEASE DATE 08-JUN-97 ISSUAug 20, 2020 · N365NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA202008242845Seat Track · damagedREPLACE SEAT TRACK Y1292 LOC ON FRAME 57 PREVIOUSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2032-DE WAS FOUND OUT LIMITS CORRECTIVE ACTION: REPLACE SEAT TRACK Y1292 AND FASTENER LOC BTW FR 47 TO FR 64 AS PER A319 SRM 51-72-11Aug 20, 2020 · N365NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA202008242844Floor Support · corrodedCORROSION FLOOR STRUCTURE LOCATED BTW FR 18 TO FR 20 AND -Y254 IN PASSENGER CABIN (1EA) .CORRECTIVE ACTION: REPLACED FLOOR BEAM LOCATED BTW FR12 TO FR24 AND -Y254 IN PASSENGER CABIN (1EA) AS PER A319 SRM 51-72-11Aug 19, 2020 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA202008242843Floorbeam · corrodedCORROSION FLOOR STRUCTURE LOCATED AT FR 16 HARD POINT AND Y1292 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM LOCATED AT FR12 TO FR24 AND Y1292 IN PASSENGER CABIN (1EA) AS PER A319 SRM 51-72-11 AND DRAWING #D53112812, ISSUE E.Aug 19, 2020 · N365NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA2020091103048Dampener · malfunctionedSHIP 3165, DONT WORK CORRECTLY PASSENGER CREW DOOR 841 DAMPER. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 841 DAMPER IN PASSENGER CABIN, AS PER A320 FAM AMM 52-11-14-400-001-B.Aug 17, 2020 · N365NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA202007292669Proximity Sensor · out of adjustAIR TURNBACK, DUE TO A AFT CARGO DOOR OPEN INDICATION. OPERATIONAL DECISION BY FLIGHT CREW. NO CONTACT WITH THE MCC WAS MADE. REPLACED THE DOOR FRAME PROXIMITY SENSOR 32WV AND ADJUSTED GAP WITH TARGET TOO LARGE.Jul 19, 2020 · N365NB · Airbus A319114 · Door Warning SystemSDR DALA2020061752471Switch · failedEMERGENCY LIGHTS ON WHEN THE EMERGENCY LIGHT SWITCH ON AND OFF POSITION. FOUND THE EMERGENCY LIGHT SWITCH BAD. R & R IAW AMM 33-51-01, TESTED OK.Jun 13, 2020 · N365NB · Airbus A319114 · Emergency LightingSDR DALA2020042802309Mechanism · defective(AIRCRAFT 3165, L/P 7069612) L2 DOOR GUST LOCK INOP. CORRECTIVE ACTION: REPLACED GUST LOCK CONTROL MECHANISM, CKS GOOD. PER A319 AMM 52-13.Apr 24, 2020 · N365NB · Airbus A319114 · Passenger/Crew DoorsSDR DALA2018111536635Fan · odorSTRONG BURNING ELECTRICAL OR PLASTIC SMELL IN COCKPIT, FOUND AVIONICS EXTRACT FAN OVERHEATING, REPLACED AVIONICS FANNov 13, 2018 · N365NB · Airbus A319114 · Air Distribution FanSDR DALA2022080105249None · noneSHIP 3165 CRACK DAMAGE TO LH ENGINE PYLON FWD FAIRING PANEL 411AL. CORRECTIVE ACTION: COMPLIED WITH ERA 572128-14 SECTION I. (0776862)Oct 9, 2018 · N365NB · Airbus A319114 · Nacelle/Pylon StructureSDR DALA2018052003451Housing · damagedEMERG LIGHT HOUSING AT SEAT 19D DAMAGED, REPLACED EMERGENCY LIGHT HOUSING AT SEAT 19D.May 12, 2018 · N365NB · Airbus A319114 · Emergency LightingSDR DALA2017100907386Fan · failedAIR TURNBACK, DUE TO AN AVIONICS VENT EXTRACT FAULT ECAM WARNING WITH A BURNING ODOR REPORTED BY THE CREW DURING CLIMB OUT. REPLACED THE EXTRACT FAN AND THE VMU.Oct 8, 2017 · N365NB · Airbus A319114 · Air Distribution FanSDR DALA2017092707139Light · inoperativeEMERGENCY LIGHT INOPERATIVE AT ROW 15DEF, REPLACED THE EMERGENCY LIGHT ASSY.Sep 26, 2017 · N365NB · Airbus A319114 · Emergency LightingSDR DALA2017030801895Skin · dentedUPON REMOVAL OF LT FRACTAL DOUBLER, A DENT WAS FOUND. BETWEEN FR 59 AND FR 60 BETWEEN STR. 19L AND 20L. WIDTH 3.2 ( FORE AND AFT) HEIGHT 2 ( UP & DOWN ) APP DEPTH .031 6 EXISTING FAST. HOLES ARE LOCATED INSIDE OF THIS AREA CTR IS 5.0 FROM AFT EDGE OF ORIG. DOUMar 7, 2017 · N365NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2016110908686Box Beam · crackedCRACKED LT AND RT SIDE BOX BEAM AT FRAME 43, REPAIRED IAW AMDS 5310-01450-02.Nov 8, 2016 · N365NB · Airbus A319114 · Fuselage Main, StructureSDR DALA2016071605463Skin · damagedFWD LOWER FUSELAGE SKIN DAMAGED BETWEEN FRAMES 1 AND 2. COMPLIED WITH FINAL ER/A 548858-14.Jul 15, 2016 · N365NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2016071605462Web · deformedWEB AT -Y25 BETWEEN FRAMES 1 AND 2 DEFORMED. REMOVED AND REPLACED THE WEB AND RETAINED GUSSET AND DUCT SUPPORT BRACKET IAW SRM 51-42-11, AND SRM 51-44-11.Jul 14, 2016 · N365NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2016071605461Web · deformedWEB AT Y25 BETWEEN FRAMES 1 AND 2 DEFORMED. REMOVED AND REPLACED THE WEB IAW SRM 51-42-11, AND SRM 51-44-11.Jul 14, 2016 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2014122506910Light · damagedEMERGENCY LIGHT DAMAGED, REPLACED SEAT MOUNTED EMERGENCY LIGHT ASSY.Dec 17, 2014 · N365NB · Airbus A319114 · Emergency LightingSDR DALA2016112309188Channel · corrodedCORROSION ON DRY BAY LOWER GANG CHANNEL ON RT WING FROM RIB 6 TO RIB 6B. REPAIRED IAW ERA.Oct 28, 2014 · N365NB · Airbus A319114 · Wing Miscellaneous StructureSDR DALA2014102705761Stringer · corrodedCORROSION ON STRINGER 33R IN AFT CARGO BAY FRAME 59+14. REPAIR THE STRINGER IAW PRI 529841-14, REV 0 AND ERA 529841-14, REV ORIGINAL.Oct 23, 2014 · N365NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA2014102305760Skin · corrodedCORROSION ON SKIN IN FWD CARGO BAY ON FRAME 30+12 BETWEEN STRINGERS 41-42R. FOUND WITHIN LIMITS IAW SRM 53-21-11, TABLE 101, PARA 4E DIAGRAM 105.Oct 22, 2014 · N365NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2014102205701Floor Panel · corrodedCORROSION ON FLOOR PANEL INTERNAL SKIN FRAME 30+18 BETWEEN STRINGERS 43-44L, FOUND WITHIN LIMITS IAW SRM 53-21-11, TABLE 101, PARA 4E DIAGRAM 105.Oct 21, 2014 · N365NB · Airbus A319114 · Fuselage Floor PanelSDR DALA2014102205700Splice · corrodedCORROSION ON SPLICE LOCATED -Y1162 FRAME 67+15". REPLACED THE SPLICE IAW SRM 51-72-11 AND DWG D53472000.Oct 21, 2014 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2014102205699Shear Tie · corrodedCORROSION ON SHEAR TIE ON FRAME 30 BETWEEN STRINGERS 41-42R. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG D53231582.Oct 21, 2014 · N365NB · Airbus A319114 · Fuselage Internal Mounting StructureSDR DALA2014102205698Skin · damagedLIGHTNING STRIKE ON TAIL FROM FRAME 72 - 73 BETWEEN STRINGERS 10 - 11L. REPAIRED THE SKIN IAW SRM A319 53-51-11.Oct 21, 2014 · N365NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2014102005657Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.Oct 19, 2014 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2014102005656Floor Support · corrodedCORROSION ON FLOOR SUPPORT -765, UPPER FLANGE AT FWD GALLEY AREA ON FRAME 21+9. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWGS D53110920 AND D53112816.Oct 19, 2014 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2014102005655Seat Track · corrodedCORROSION ON SEAT TRACK + Y 1292 BETWEEN FRAMES 36 - 41. FOUND OUT OF LIMITS AND REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DWG D53372500.Oct 19, 2014 · N365NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014102005654Seat Track · corrodedCORROSION ON SEAT TRACK + Y 1292 BETWEEN FRAMES 41 - 47, FOUND OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DWG D53372500.Oct 19, 2014 · N365NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2014101905653Floor Support · corrodedCORROSION ON FLOOR SUPPORT +Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.Oct 18, 2014 · N365NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2014101905652Floor Support · corrodedCORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 66+5 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472780.Oct 18, 2014 · N365NB · Airbus A319114 · Fuselage Miscellaneous Structure
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