N321NB

Service difficulty reports · 106

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 = 'N321NB' 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 DALA2021102006481Control Valve · faultySHIP 3121 - AFTER RELEASING PARK BRAKE FOR PUSH BACK, BRAKE PRESSURE STAYED AT 500 PSI BOTH SIDES. BRAKES WOULD NOT RELEASE FULLY IN A TIMELY MANNER, WOULD PARTIALLY RELEASE. CORRECTIVE ACTION: R/R PARKING BRAKE CONTROL VALVE PER A319 AMM 32-45-51 OPS AND LEAKOct 18, 2021 · N321NB · Airbus A319114 · Landing Gear Brake SystemSDR DALA2021102006480Battery · failedSHIP 3121 - EPSU COMM EMER L MESSAGE DURING EPSU SYS TEST. EMER OPS TEST FAIL CORRECTIVE ACTION: R/R EPSU 11WL A SECOND TIME PER A319 AMM 33-51-38. OPS TEST NORMAL, EPSU TEST OK.(7937475)Oct 18, 2021 · N321NB · Airbus A319114 · Emergency LightingSDR DALA2021042902475Strap · missingSHIP 3121 - SEAT ROW 14DEF DITCHING STRAP MISSING. CORRECTIVE ACTION: FOUND DITCHING STRAP WITH OTHER STRAP. RELOCATED TO CORRECT POSITION. (7423617)Apr 27, 2021 · N321NB · Airbus A319114 · Emergency EquipmentSDR DALA2020021801209Life Line · tornTORN ROW NUMBER BIN 14 RH LIFE LINE IN PASSENGER CABIN. REPLACED ROW NUMBER BIN 14 RH LIFE LINE IN PASSENGER CABIN ASPER DWG 25-5428.Feb 17, 2020 · N321NB · Airbus A319114 · Emergency EquipmentSDR DALA2019120907164Unknown · unknownDURING TAXI BRAKE CHECK 5.14.2 TRANSISTOR TO NORMAL / GREEN BRAKE TOOK APROX 6 SECONDS FOR BRAKE GAGE ON PANELNTO DROP TO ZERO. ALL OTHER BEHAVIOR NORMAL. PERFORMED BITE TEST OF BSCU ALL CKD GOOD NO DEFECT NOTED AT THIS TIME SYS OPS AS NORM NO 3 DAY REPETITIVEDec 9, 2019 · N321NB · Airbus A319114 · Landing Gear Brake SystemSDR DALA2018120326996Light · brokenEMERGENCY LIGHT AT 20E CONNECTED TO AISLE SEAT IS BROKEN, RE SECURED LIGHT LENS TO SEATNov 30, 2018 · N321NB · Airbus A319114 · Emergency LightingSDR DALA2018111506636Wire · brokenEMERGENCY LIGHTS TEST FAILED ON CIDS PANEL EPSU EXT LOAD FWD L FAULT DISPLAYED, FOUND WIRES 3351-5108 AND 3351-5109 BROKEN BETWEEN 2819VCA AND 2821VC, REPAIRED DAMAGED AND REPLACED SLIDE AND EPSU 10WLNov 13, 2018 · N321NB · Airbus A319114 · Light System WiringSDR DALA2018040302169Blades · damagedTOOK A BIRD STRIKE AT 500' ON TAKEOFF WHICH TOOK OUT THE #1 ENGINE EXTREME VIBRATION BUT NO FIRE INDICATION BROUGHT THRUST TO IDLE AND SHUTDOWN ENGINE, FOUND DAMAGED BLADES IN ALL SECTIONS OF HPC WITH FEW BLADES IN HPC 4 BEING OUT OF SERVICEABLE LIMITS. REPLACApr 2, 2018 · N321NB · Airbus A319114 · Engine (Turbine/Turboprop)SDR DALA2018022701245Frame · crackedCRACK FOUND ON FRAME 68, STRINGER 8R, PERFORMED A PERMANENT REPAIR IAW PRI 565276-14, REVISIONS 0, 1, 2, 3, 4, 5. 6, 7, AND ERA 565276-14AD, REV ORIGINAL, SECTION I.Feb 26, 2018 · N321NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2018022601243Frame · crackedCRACK ON FRAME 68, STRINGER 8L, REAR SIDE. PERFORMED A PERMANENT REPAIR IAW PRI 565269-14, REVISIONS 0, 1, 2, 3, 4, 5, 6, AND ER/A 565269-14AD, REV ORIGINAL.Feb 25, 2018 · N321NB · Airbus A319114 · Fuselage Main, FrameSDR DALA2018022601240Cover · dentedDENT ON THE COVER SHEET LOCATED AT FRAME 56+10 INCHES. REPLACED THE COVER SHEET IAW SRM 51-42-11, 51-72-11, 51-72-11, AND DRAWING D53477000.Feb 25, 2018 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018022401238Angle · crackedCRACK EMERGENCY EXIT DOOR 834 FWD SEGMENT IN PASSENGER CABIN, REPLACED SEGMENT ANGLE LOC. ON EMERGENCY EXIT DOOR 834 PASSENGER CABIN IAW SRM 51-72-11 AND DWG #D52279026Feb 24, 2018 · N321NB · Airbus A319114 · Emergency ExitsSDR DALA2018021700993Seat Track · corrodedCORRODED SEAT TRACK, +Y1292, FRAMES 64 TO 66. REPLACED THE SEAT TRACK IAW SRM 51-42-11, AND 51-72-11.Feb 17, 2018 · N321NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018021600991Floor Support · corrodedCORROSION FLOOR SUPPORT, FRAME 67+16, AND + Y1162. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, 51-42-11, AND DRAWING D53472780.Feb 16, 2018 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018021600990Floor Support · corrodedCORRODED FLOOR SUPPORT +Y1162.5, FRAME 67+8.Feb 16, 2018 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018021600989Floor Support · corrodedCORRODED FLOOR SUPPORT, -Y765, FRAME 68, REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 66 - 70 IAW SRM 51-72-11, 51-42-11, AND DRAWING D534720000.Feb 16, 2018 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018021600988Seat Track · corrodedCORRODED SEAT TRACK, -Y765, FRAMES 64 TO 66. REPLACED THE SEAT TRACK IAW SRM 51-72-11, 51-42-11, AND DRAWING D53472000.Feb 15, 2018 · N321NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018021600987Floor Support · corrodedCORRODED FLOOR SUPPORT, +Y254, BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, DRAWING D53112816, AND D53110984.Feb 15, 2018 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018021600986Seat Track · corrodedCORRODED SEAT TRACK, -Y765, FRAME 20. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DRAWING D53112812, AND D53110920Feb 15, 2018 · N321NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018021500916Seat Track · corrodedCORRODED SEAT TRACK, +Y765, FRAMES 64 TO 66. REPLACED THE SEAT TRACK IAW SRM 51-72-11Feb 14, 2018 · N321NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018021300915Floor Support · corrodedCORRODED FLOOR SUPPORT, FRAME 67+16, - Y 1162, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11.Feb 13, 2018 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018021300914Floor Support · corrodedCORRODED FLOOR SUPPORT +Y765, BETWEEN FRAMES 12 TO 24, REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, 51-42-11, AND DRAWING D531128120.Feb 13, 2018 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA2018021300913Seat Track · corrodedCORRODED SEAT TRACK -Y1292, FROM FRAMES 19 TO 20, REPLACED THE SEAT TRACK IAW SRM 51-42-11, 51-72-11, AND DRAWING 53112814.Feb 13, 2018 · N321NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018021300912Skin · dentedRIGHT WING, NR 2 SLAT LEADING EDGE AREA DENTED. PERFORMED A PERMANENT REPAIR IAW SRM 57-43-21-300-023.Feb 13, 2018 · N321NB · Airbus A319114 · Leading Edge DevicesSDR DALA2017020901112Slide · faultedDURING EMERGENCY LIGHTS CHECK, FOUND "EPSU EXT LOAD AFT L" FAULT. REPLACED AFT LEFT DOOR SLIDE.Feb 7, 2017 · N321NB · Airbus A319114 · Escape SlideSDR DALA2015102006272Wire · damagedROW 9 EMERGENCY LIGHT RED INOPERATIVE, REPAIRED WIRE.Oct 19, 2015 · N321NB · Airbus A319114 · Emergency LightingSDR DALA2015031202105Skin · dentedBIRD STRIKE DAMAGE BELOW F/O SLIDING WINDOW, FOUND DENT APPROXIMATELY 9" X 7" AT STA 539 FWD OF FRAME 9. DENT IS OUT OF LIMITS DUE TO CLOSENESS OF FASTENERS ON FRAME 9. CUT OUT DAMAGE, FAB. DOUBLER AND INSTALLED IAW ER/A 532347-14, REV A, AND SRM 53-00-11.Jan 20, 2015 · N321NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA14001943121Circuit Breaker · failedAFTER STARTING BOTH ENGINES, EMERGENCY EXIT AND ISLE LIGHTS ILLUMINATED. LIGHTS EXTINGUISHED WHEN POWER ADVANCED FOR TAKEOFF. AT GEAR EXTENSION LIGHTS ON AGAIN FOR 10-15 SECONDS. CIDS 2, NO RESPONSE. ATTEMPTED CIRCUIT BREAKER RESET. CIRCUIT BREAKER G2 "DIJan 8, 2014 · N321NB · Airbus A319114 · Emergency LightingSDR DALA1232133121Stringer · corrodedAFT CARGO COMPARTMENT FR 62 STR 41R HAS CORROSION APPROXIMATELY 10 INCHES LONG. CUT DAMAGE OUT OF STRINGER IAW SRM 53-00-13. FABRICATED REPAIR STRINGER IAW SRM 53-00-13. FABRICATED REPAIR COUPLING IAW SRM 53-00-13. FOUND OUT OF LIMITS IAW SRM 53-00-13. May 10, 2012 · N321NB · Airbus A319114 · Fuselage Main, Longeron/StringerSDR DALA1228953121Floor Panel · damagedFORWARD CABIN FLOOR PANEL 231AF HAS 2 DAMAGED LATCHES. REMOVED AND REPLACED FLOOR PANEL PER WORK CARD 5242-01006-01.May 3, 2012 · N321NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1228823121Fitting · corrodedFORWARD RIGHT PASS DOOR SILL AFT GIRT BAR FITTING ALL 4 FASTENER HOLES HAVE CORROSION AROUND THEM. REMOVED AND REPLACED DOOR SILL IAW SRM 51-44-11AND 51-42-11. PAINTED FASTENERS IAW SRM 51-75-12. DAMAGE DIM: L=1.750" W=1.250" D=.052".May 2, 2012 · N321NB · Airbus A319114 · Fuselage Main, Attach FittingsSDR DALA1228813121Panel · delaminatedAFT PIT SLOPE PANEL 152TG DELAMINATED. FABRICATED NEW SLOPE PANEL IAW DWTG 3D25-40532. DAMAGE DIM: 6.0" X 4.0".May 1, 2012 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1228803121Floor Panel · corrodedAFT CABIN FLOOR PANEL 261FF CORRODED. REPLACED WITH NEW FLOOR PANEL & INSTALLED ON WORKCARD 2500-6602. DAMAGE DIM: L=2.5" W=2.0".May 1, 2012 · N321NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1228783121Floor Panel · corrodedAFT CABIN FLOOR PANEL 262FF CORRODED. REPLACED WITH NEW FLOOR PANEL & INSTALLED ON WORKCARD 2500-6602. DAMAGE DIM: L=2.0" W=3.0".May 1, 2012 · N321NB · Airbus A319114 · Fuselage Floor PanelSDR DALA1228123121Support · corrodedAVIONICS DOOR SUPPORT FR 21 HAS CORROSION. REMOVED DAMAGED DOOR SUPPORT AT FR 21 IAW SRM A319 51-42-11. FABRICATED NEW SUPPORT IAW SRM 53-11-14. TREATED AND PRIMED APPLIED PAINT IAW SRM 51-21-11 AND 51-75-12. LOCATED AND DRILLED INSTALLED NEW SUPPORT IAW SApr 30, 2012 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1228113121Support · corrodedAVIONICS DOOR SUPPORT AT FR 23 HAS CORROSION. REMOVED DAMAGED DOOR SUPPORT AT FR 23 IAW SRM A319 51-42-11. FABRICATED NEW SUPPORT IAW SRM A319 53-11-14. TREATED AND PRIMED APPLIED PAINT IAW SRM A319 51-21-11 AND 51-75-12. LOCATED, DRILLED AND INSTALLED NEApr 30, 2012 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1228093121Floor Support · corrodedFLOOR SUPPORT AT FR 20,-Y1732 HAS 1 INCH WIDE AND 2 INCH LONG AREA OF CORROSION. REMOVED AND REPLACED FLOOR SUPPORT AT FR 20 IAW SRM 51-42-11.Apr 27, 2012 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1227083121Shear Plate · corrodedAFT CABIN BETWEEN FR69 - FR70 RT SHEAR PLATE, UPPER AND LOWER SURFACE HAS CORROSION. REMOVED CORROSION FR69 - FR70 RT SHEAR PLATE UPPER AND LOWER SURFACE IAW A319 SRM 51-74-00, NO LIMIT ALLOW IN SRM AND RIGHT SHEAR TIE PLATE IAW A319 SRM 51-42-11. RECEIVApr 25, 2012 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1227053121Floorbeam · corrodedAFT LAV/GALLEY BET FR65 TO FR66, Y-465, FLOORBEAM HAS CORROSION. SSI 534147. REMOVED CORROSION AT FLOOR BEAM Y-465, FR 65-66 IAW A319 SRM 51-74-00 AREA OF REWORK L=1.36", W=.85", D=.043" MAX ALLOWABLE DEPTH=.016" ORIG MAT =.150". FOUND TO BE OUT OF LIMITS IApr 24, 2012 · N321NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA1227033121Floor Support · corrodedFORWARD UTILITY FLOOR SUPPORT +Y254 HAS 2 AREAS OF CORR. NR 1 AT FR 18, NR 2 AT FR 20. SSI 531189. REMOVED CORROSION IAW A319 SRM 51-74-00. ORIG MAT 0.061" DAMAGE DIML=3" W=2" D=0.021" FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 104. REMOVED AND REPLApr 24, 2012 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1227023121Seat Track · corrodedFORWARD UTILITY FLOOR SUPPORT SEAT TRACK CROWN -Y765 HAS 3 AREAS OF PITTING CORROSION BETWEEN FR20 AND FR23 BLENDED AREAS IAW A319 SRM 51-73-00. DIMENSIONS OF REWORKED AREA: L=2" W=.500" D=0.032". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-15. REMOVED DAMApr 24, 2012 · N321NB · Airbus A319114 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1227013121Floor Support · corrodedFORWARD UTILITY FLOOR SUPPORT -Y178 HAS CORROSION FORWARD OF FR 14 AROUND GALLEY MOUNT. SSI 531189. REMOVED COCKPIT DOOR STUD IAW A319 SRM 51-42-11. REMOVED CORROSION IAW A319 SRM 51-74-00. ORIG MAT. 0.061". DAMAGE DIM: L=2" W=2.500" D=0.027". REMOVED FLApr 23, 2012 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1227003121Floorbeam · corrodedAFT LAV/GALLEY BET FR 64 TO FR 65, Y-765, FLOORBEAM BESIDE SEAT TRACK HAS CORROSION. SSI 534147. REMOVED CORROSION IAW A319 SRM 51-74-00. ORIG MAT 100 DAMAGE DIM: L=2.3" W=.34" D=.035" OUT OF LIMITS IAW A319 SRM 53-41-15 FIG 102. REMOVED AND REPLACED FLOOApr 23, 2012 · N321NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA1226913121Floorbeam · corrodedAFT LAV/GALLEY BET FR68 TO FR69, Y-1292, FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. CHECKED LIMITS ORIG MAT THICKNESS=.150" L=1.5"W=.75" D=.030" OUT OF LIMITS IAW A319 SRM 53-00-14 PARA 4.B FIG 2. RECEIVED NEW FLOORBEAM. REMOVED FLOApr 22, 2012 · N321NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA1226903121Floorbeam · corrodedAFT LAV/GALLEY BET FR66 TO FR68, Y-1292 FLOOR BEAM HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. CHECKED LIMITS ORIG MAT THICKNESS=.100" L=2.0"W=1.0" D=.025" OUT OF LIMITS IAW A319 SRM 53-00-14 PARA 4.B FIG 102. RECEIVED NEW FLOORBEAM. REMOVED FApr 22, 2012 · N321NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA1226733121Floorbeam · corrodedAFT LAV/GALLEY BET FR68 TO FR69, Y+1292. FLOORBEAM HAS CORROSION. RETAIN FOR RECORDS. REMOVED CORROSION IAW A319 SRM 51-74-00 CHECKED LIMIT L=2" W=1.5" D=.053" ORIG MAT=.153" OUT OF LIMIT IAW A319 SRM 53-00-14 FIG 102. REMOVED DAMAGED FLOOR SUPPORT IAW A31Apr 22, 2012 · N321NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA1226723121Floorbeam · corrodedAFT LAV/GALLEY BET FR65 TO FR66, Y765 FLOORBEAM HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00, DIMENSIONS OF REWORKED AREA ARE: L=1.03" W=.79" D=0.049" FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-00-14 FIG 102. REMOVED DAMAGED FLOORBEAM IAW A319 SRM 51-4Apr 22, 2012 · N321NB · Airbus A319114 · Fuselage Main, Floor BeamSDR DALA1226083121Floor Support · corrodedFORWARD CABIN FLOOR SUPPORT -Y189 HAS SMALL AREA OF CORROSION AT FR 23. REMOVED CORROSION IAW A319 SRM 51-74-00 DIMENSION OF REWORK AREA L=0.7"W=0.4" D=.035". FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-11-74 FIG 105. REMOVED AND REPLACED FLOOR SUPPORT IAW SRApr 20, 2012 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1226073121Floor Support · corrodedFORWARD UTILITY FLOOR SUPPORT AT FR 20 -Y1292 HAS 1 IN WIDE X 1.5 LONG AREA OF EXFOLIATION. RETAIN FOR RECORDS. BLENDED AREA IAW A319 SRM 51-74-00 AREA DIMENSIONS AFTER REWORK L=1.5"W=1.4"D=.048" ORIG MAT THICKNESS .079 FOUND TO BE OUT OF LIMITS IAW A319 SRMApr 20, 2012 · N321NB · Airbus A319114 · Fuselage Miscellaneous StructureSDR DALA1226063121Floor Support · corrodedFORWARD UTILITY FLOOR SUPPORT +Y1292 HAS CORROSION AT FR 20. BLENDED AREA IAW A319 SRM 51-74-00. CHECKED LIMITS L=1.5"W=1.5"D=.019" FOUND TO BE OUTOF LIMITS IAW A319 SRM 53-00-15. REMOVED AND REPLACED FLOOR SUPPORT IAW A319 SRM 51-42-11.Apr 20, 2012 · N321NB · Airbus A319114 · Fuselage Miscellaneous Structure
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