N325NB
Service difficulty reports · 138
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 = 'N325NB' 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.
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 = 'N325NB' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2026102005759Skin · dentedER/A 633023-14 REV A: UPPER REAR FUSELAGE SKIN WITH DENT AT FR55 470MM, STRG 6/7LT. SUBJECT REQUIRES FOLLOW ON ACTIONS. ACCOMPLISH SEC. II WITHIN 33,700 FLIGHT HOURS OR 16,800 FLIGHT CYCLES THRESHOLD (WITHIN AIRCRAFT TOTAL TIME OF 93,219 FH OR 47,634 FC) FROSDR DALA2026092105242Skin · crackedER/A 632717-14 REV A: A319 / 3125 / REAR FUSELAGE SKIN PANEL / BTW FR65-66 & STGR31RH-32RH / CORRODED AND CRACKED. SUBJECT REQUIRES FOLLOW ON ACTIONS. ACCOMPLISH SECTION III EXTERNAL INSPECTIONS AT DOUBLER AT A THRESHOLD OF 99,500 TOTAL FLIGHT HOURS OR 50,800SDR DALA2026090204941Cover · brokenLIGHT COVER ABOVE 1L DOOR BROKEN/FELL OFF. SECURED LIGHT COVER ABOVE 1L DOOR. OPS CHKD GOOD. (LP: 9489242, AIRCRAFT WAS GROUNDED)SDR DALA2026081104622Light Sys · faultedAFTER ROTATING FA REPORTS CABIN EMERGENCY LIGHTS CAME ON MOMENTARY, THEN TURNED OFF. PERFORMED CIDS TEST IAW AMM 23-73. TEST OK. VERIFIED EMERGENCY EXIT LIGHTS OPS NORMAL IAW AMM 33-50. (LP: 9587650, AIRCRAFT WAS GROUNDED)SDR DALA2026080604530Seal · faultedAT CRUISE, ODORS & ELECTRIC ACRID ODORS. TURNED CABIN FANS OFF AS WE HEARD A HIGH WHINE SOUND. LASTED 3-5 MINS THEN DISSIPATED. . DISCOVERED CAPTAINS ELECTRIC MOTOR TO CHAIR WASN'T WORKING. INSPECTED FLT DECK & FWD AVIONICS BAY, FOUND C/B FOR CAPT CHAIR POPSDR DALA2026053003281Power Supply · faultedEMERGENCY EXIT SIGNS INOPERATIVE. THE EXIT SIGNS ABOVE DOORS 2L AND 2R DO NOT ILLUMINATE WHEN THE GEAR IS DOWN, INSTEAD THE SMALL EMERGENCY LIGHTS BETWEEN THE EXIT SIGN AND DOOR COME ON. R & R EPSU AND EPSU POWER SUPPLY REF A319/320 AMM 33-51. FAULT STILL PRESDR DALA2026050602892Oxygen Box · openCREW REPORTS O2 MASK DOOR OPENED ON LANDING SEAT 12DEF. PACKED AND SECURED O2 MASK DOOR AT SEAT 12 DEF IAW AMM 35- 21. (LP: 8885420). AIRCRAFT WAS GROUNDEDSDR DALA2026042002463Repair · not reportedREMOVE EXISTING EXTERNAL REPAIR LOCATED BTWN FR1 AND FR3 STRG 34R AND RT LOWER STRG AND PERFORM VISUAL INSPECTION OF THE UNDERLYING STRUCTURE. REPAIRED R/H NOSE FWD FUSELAGE SKIN BETWEEN FRI-FR3 BETWEEN STRG -34R-36R I/A/W DELTA ER/A 633282-14AD REV: ORIGINAL SDR DALA2026042202554Skin · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR SKIN REPAIR INSTALLED AT FR 65 - 66 S31 - 32R IAW ER/A 632717-14. C/A: SECTION I IS LIMITED TO 6MO ( 182 DAYS ) FROM 15APR26. ER/A TO B E REVISED PRIOR TO THIS LIMIT ELSE REMOVED A/C FROM SERVICE. ASSOCIATED ER/SDR DALA2026042002462Skin · dentedUPPER FUSELAGE FR55+470MM BETWEEN STR 6L-7L SKIN PANEL WITH DENT. REPAIRED UPPER REAR FUSELAGE SKIN PANEL WITH DENT FR55+470MM BETWEEN STRG 6LH - 7LH IAW DELTA ER/A 633023-14 REV ORIGINAL DATED 15/APR/26. NOTE: THIS IS CLASSIFIED AS MAJOR REPAIR. ASSOCIATED ESDR DALA2026042002461Skin · crackedLOWER FUSELAGE AT FR65+220MM BETWEEN STRG 31R-32R SKIN PANEL CORRODED AND CRACKED. REPAIRED UPPER REAR FUSELAGE SKIN PANEL BETWEEN FR65-FR66 AND STRG 31RH-32RH I/A/W DELTA ER/A 632717-14 REV. ORIGINAL DATED 17 -APR-26. NOTE: THIS IS CLASSIFIED AS MAJOR REPAIRSDR DALA2026041702436Door Frame · damagedFR68 DOOR FRAME R/H, DOOR STOP FITTINGS 1,2,3,4,5,6 AND 7 LOCATIONS WERE FOUND THE HOLES (4 HOLES IN EACH FITTING) COMMON TO THE FRAME WEB GREATER THAN THE MAXIMUM STARTING HOLE DIAMETER (6.38MM/0.251") "ACTION REQUIRED PRIOR TO FURTHER FLIGHT, ENGINEERING EVASDR DALA2026042202551Door Frame · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLED AT FR68RH DOOR STOP AREA OF FRAME WEB PER ER/A 633159-14AD. C/A: SECTION I IS LIMITED TO 60000FC FROM 08APR26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED AA SDR DALA2026042202550Door Frame · not reportedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D ON FRAME WEB FR68RH AT DOOR STOPS PER ER/A 633159-14AD. SECTION I IS LIMITED TO 37900FC FROM 08APR26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED AA 5311-01SDR DALA2026042202553Door Frame · damagedER/A 633159-14AD ISSUED FOR REPAIR TO FR68 RT FRAME WEB AT DOOR STOPS. FOLLOW ON ACTION REQUIRED. PERFORM SECTION II EVERY 19700FC AFTER SECTION I. ASSOCIATED AA 5311-01216 ADDED FOR AC 3125 ASSOCIATED ER/A 14-633159 ADDED FOR AC 3125. (LP: 1545988). AIRCRAFT SDR DALA2026042002460Skin · not reportedDAMAGE TOLERANCE EVALUATION (DTE) REQUIRED FOR FUSELAGE SKIN R EPAIR INSSTALLED AT FR56 AND S-6/7LH PER ER/A 633023-14. SECTION I IS LIMITED TO 6MO (182) DAYS FROM 10APR26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 1SDR DALA2026041502383Stringer · corrodedAFT CARGO BAY, BETWEEN FR 59 & FR 60, STR 43L, STRINGER EXISTING COUPLING REPAIR CORRODED. REPAIRED FUSELAGE S43L BTWN FR 58 - 61. IAW ER/A 633052-14, REV. ORIGINAL. MAJOR REPAIR.SDR DALA2026042002464Lug · damagedDAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR OF LUG B ORE AT RH WING OUTBOARD FLAP PER ER/A 633290-14. SECTION I LIMITED TO 6 MONTHS FROM 09APR26 ON FTN 1X6843. ER/A T O BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE COMPONENT FROM SERV ICE. ASSOCIATEDSDR DALA2026041202307Window Frame · crackedREQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT . FLIGHT DECK, WINDSHIELD FRAMING, LH/RH CONTINUITY FITTING CRACKED. CONTACT LIAISON ENGINEERING FOR FURTHER DISPOSITION. REPLACED CONTINUITY FITTINGS (LH P/N D5311107720200) (SDR DALA2026040902270Seat Track · corrodedPASSENGER CABIN AFT SECTION AT FR65, Y=1292 SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK P/N 14N00031-101 AT FR 64 TO FR 66 Y=1292 WET AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11-911- 001 REV, 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTSDR DALA2026040902269Seat Track · corrodedPASSENGER AFT CABIN AT FR 65, -Y=1292 SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK P/N 14N00031-101 AT FR 64 TO FR 66 -Y=1292 WET AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11-911- 001 REV, 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTION ISDR DALA2026040902268Seat Track · corrodedPASSENGER AFT CABIN AT FR66, Y=765 SEAT TRACK WITH CORROSION. C/A: REPLACED SEAT TRACK P/N 14N00031-103 AT FR 64 TO FR 66 Y=765 WET AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11- 911- 001 REV: 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTION ISDR DALA2026040902267Seat Track · corrodedPASSENGER AFT CABIN AT FR 65, -Y=765 SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK P/N 14N00031-103 AT FR 64 TO FR 66 -Y=765 WET -AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11- 911- 001 REV: 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTION ISDR DALA2026040802232Floor Support · corrodedPASSENGER CABIN FLOOR SUPPORT AT Y-1720MM BETWEEN FR 20 & FR 21, WEB AND SUPPORT ANGLES (2EA) WITH CORROSION. REPLACED WEB P/N 5311278520300 AND SUPPORT ANGLE P/N D5311278620101 IAW A319 SRM 53-11-14-07B FIG 007 ITEMS 186A AND 190 AND A319 SRM 51-72-911-001 PSDR DALA2026040602161Support Angle · corrodedLOWER FUSELAGE LT AVIONICS BAY, FR 13 BTWN STRINGERS 31L & 34L, VENTILATION DUCTS SUPPORT STRUCTURE INNER ANGLE WITH CORROSION. REPLACED ANGLE AT L/H AVIONICS COMPARTMENT FR 13 BETWEEN STGR 31L AND STGR 34L I.A.W A319 SRM 51-72-11-911- 001 REV. 155.00 DATED 1SDR DALA2026040202137Skin · damagedLOWER EXTERNAL FUSELAGE AT FR 25+160MM, STGR 40L SKIN WITH TOOL MARKS. FOUND DURING PROCESS WITH ORNRC 100-269. REPAIRED LOWER FUSELAGE SKIN PANEL FROM FR25 +66.5MM TO FR25 + 296.6MM BETWEEN STRG 39LH-41LH DUE TO TOOL MARK OUT LIMITS I/A/W A319 SRM 53-21-11-3SDR DALA2026033002089Seat Track · corrodedPASSENGER CABIN AT Y-765, BETWEEN FR20 AND FR21, SEAT TRACK CORRODED. REPLACED THE SEAT TRACK Y -765, BTW FR 12 TO FR 24 IAW SRM 51-72-11-911-001, PARAG 2.B, REV 155.00, DWGS D53112812, D53112813, D53112639, & D53110920. (LP: 1518556)SDR DALA2026033002088Seat Track · corrodedPASSENGER CABIN AT Y-1292, BETWEEN FR20 AND FR21 , SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK AT Y -1292, BTW FR 12 TO FR 24 IAW SRM 51-72-11-911-001, PARAG 2.B, REV 155.00, DWG D53112812, D53112813, D53110920, & D53112639. (LP: 1518547)SDR DALA2026032602014Power Supply · inoperativePAX CABIN EMERGENCY POWER SUPPLY UNIT INOP. REPLACED EMERGENCY POWER SUPPLY UNIT IAW A319 AMM TASK 33-51-38- 000-001-A AND AMM TASK 33-51-38-400-001-A. (LP: 1510385)SDR DALA2026032602011Support Angle · corrodedFORWARD PASSENGER DOOR (LT) CUTOUT SILL AREA BETWEEN FR16 AND FR20, SCUFF PLATE SUPPORT ANGLE WITH CORROSION. REPLACED SUPPORT ANGLE (FITTING) P/N: D5311219820006 IAW A319 SRM TASK 51-72-11-911-001 REV 155.00 DATED 17/NOV/25 AND DRAWING REF D531 12109 ISSUE CSDR DALA2026012200482Slide · low pressureRIGHT FWD DERVICE DOOR SLIDE HAS LOW PRESSURE. REMOVED AND REPLACED RIGHT FORWARD DOOR SLIDE IAW AMDS TC 2561-4004-RF. (LP: 9141074)SDR DALA2024021201959Skin · dentedSHIP 3125 THREE DENTS IN FUSELAGE UNDER FWD CARGO DOOR. CORRECTIVE ACTION: REPAIRED PER ER/A 501814-14. (0194327)SDR DALA2024010800299Not Reported · not reportedSHIP 3125 DENT FWD OF L2 DOOR. CORRECTIVE ACTION: REPAIRED PER A319 SRM 53-41-11-283-059. (5381348)SDR DALA2023121210152Unknown · unknownSHIP 3125 EXIT LIGHT BURNED OUT AT POSITION 2L. CORRECTIVE ACTION: EXAMINED WIRING PER A319 ASM 33-51-02, FOUND 33WL 1 AND 3 ON 45WL 1 AND 3. PLACED WIRES ON PROPER SIGNS AND ALL LIGHTS OPS CHECK OK. REF A319 TSM 33-51-00-810- 807-A. (9938556)SDR DALA2023103008915Unknown · unknownSHIP 3125 INTERCOSTAL WEB AND SUPPORT CORRODED 4" FWD OF FR70 STR 23R. CORRECTIVE ACTION: REPLACED INTERCOSTAL WEB AND SUPPORT PER A319 SRM 51-42-11. (0038519)SDR DALA2023102008648Unknown · unknownSHIP 3125 FLOOR BEAM CORRODED 10" I/B OF R2 AFT GIRT BAR FITTING. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A319 SRM 51-42-11. (0026267)SDR DALA2023102008647Unknown · unknownSHIP 3125 SUPPORT STRAP AT FR 70 STR 24R CORRODED. CORRECTIVE ACTION: REPLACED STRAP AT FR 70 STR 24R PER A319 SRM 51-42-11. (0026259)SDR DALA2023102008646Floorbeam · unknownSHIP 3125 FLOOR BEAM CORRODED -Y765 FR 68. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 PER A319 SRM 51-42-11. (0026255).SDR DALA2023041503002Unknown · unknownAIRCRAFT 3125, THE AIR QUALITY OFF THE PACKS WAS SUBSTANDARD, MUSTY SMELL. IN ADDITION, THE FLIGHT ATTENDANTS REPORTED THAT THE CABIN WAS HOT ALTHOUGH INDICATED TEMP WAS 68F. QRH 2.47 DIRECTED HOT AIR SWITCH OFF. THIS HELPED CABIN TEMP AND ALSO, WE COULD NO LOSDR DALA2023031501884Unknown · unknownAIRCRAFT 3125, SMOKE FUMES IN CABIN OF A/C WITH ONLY APU RUNNING. CORRECTIVE ACTION: PERFORMED DECONTAMINATE THE ECS WHEN THE APU IS INOP REVERSE FLOW. (LP 9895734)SDR DALA2023020700922Not Reported · not reportedSHIP 3125 -ATB- RETURNED TO TPA DUE TO #1 ENGINE STALL AND EGT RISE. THROTTLE PULLED BACK AND ATTEMPTED TO PUSH THROTTLE UP, EGT FOLLOWS. REPORTS OF AN AUDIBLE BANG. FOUND EXTENSIVE DAMAGE TO 4TH STAGE LPT BLADES. CORRECTIVE ACTION: C/W #1 ENGINE CHANGE REF AMSDR DALA2022110807227None · noneSHIP 3125 - UPON INTITAL DESCENT INTO LGA CAPT + FO NOTICED THE "DIRTY SOCK" SMELL/ODOR. CORRECTIVE ACTION: C/W NO-GO-ODI PREVENTION 21-72. REPLACED BOTH REC AIR CABIN FILTERS PER A319 AMM 21 -21. (8943336)SDR DALA2022060103811Mask · deployedSHIP 3125 - OXYGEN MASKS DROPPED DURING FLIGHT SEATS 16 DEF. CORRECTIVE ACTION: REPACKED OXYGEN MASKS AT SEAT ROW 16DEF. VERIFIED OXYGEN GENERATOR DID NOT ACTIVATE. REF A320 FAM AMM 35-21-43.(8931018)SDR DALA2023062805193Unknown · unknownSHIP 3125 DISCREPANCIES FOUND IN DIAMETER AT HOLES #3,#4,#5 IN FR16 RHS DOORSTOP #7 DBL JOGGLE LEVEL. CORRECTIVE ACTION: INSPECTED HOLES PER STEP 6 SECTION 4 OF ER/A 569171-14AD REV C. (2229119)SDR DALA2021060703104Fan · noisySHIP 3125 - DIV - TO JAX DUE TO A METALLIC SMELL OF UNKNOWN SOURCE THROUGHOUT THE CABIN. CREW DONNED OXYGEN MASKS AND DECLARED AN EMERGENCY INTO JAX. AIRCRAFT WAS OPERATING ON A SINGLE PACK MEL. CORRECTIVE ACTION: COMPLIED WITH NO GO ODI. REMOVED AND REPLACED SDR DALA2021042802451Acoustic Liner · corrodedSHIP 3125 - CORROSION ON ACOUSTIC INNER BARREL AIR INTAKE COWL LOWER AREA ENGINE 2. CORRECTIVE ACTION: REMOVED AIR INTAKE COWL. INSTALLED AIR INTAKE COWL AS PER A320 FAM, AMM 71-11. (1790418)SDR DALA2020031201797Warning Light · false activationSHIP 3125 - DIV - TO PIT DUE TO APU FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED IN CRUISE. CORRECTIVE ACTION - FLIGHT CREW APPLIED MEL PLACARD AND FLIGHT CONTINUED.SDR DALA2019102196030Panel · tornON WALK AROUND TORN ON BODY PANEL 148DB. PER A319 SRM 53-35-11-300-09 DEFERRED SEAL TO MOM WITH DAILY INSPECTION OF SPEED TAPE REQUIRED WITH REPAIRS IN 600 HOURS. LOG PAGE STILL OPEN....SDR DALA2019082004860Fire Warning · false activationIN FLIGHT FL370 APU DISCH FIRE LIGHT CAME ON. WENT OUT AT 8800 MSL CABIN ALT 1100. INSPECTED BLOW OUT DISC ON FUSELAGE - NOT BLOWN. PERFORMED TSM TASK 26-22-00-810-806-A APU EXT LOOP OPERATES NORMALLY.SDR DALA2019032001835Cover · missingPDA PART DEPARTING AIRCRAFT. LOG PAGE 5290092 CLOSED. A/C 3125 FLT/CHK 0842 PILOT REPORT SDR: N POSITION: LT TASK HRS: 000009.2 TASK ELAPSE TIME HRS: 000009.2 01 18MAR19 W LEFT LANDING GEAR STRUT DUST COVER MISSING LOG-PAGE UPDATED @ 18MAR19 1846 UTC 02 18MAR1
Back to N325NB