# Service difficulty reports: N325NB

A list on [N325NB](https://openairdocs.org/aircraft/N325NB.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 138 reports

- [SDR DALA2026102005759](https://openairdocs.org/sdr/DALA2026102005759.md): Skin · dented · Oct 1, 2026 · N325NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > ER/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) FRO
- [SDR DALA2026092105242](https://openairdocs.org/sdr/DALA2026092105242.md): Skin · cracked · Sep 17, 2026 · N325NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > ER/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 50,800
- [SDR DALA2026090204941](https://openairdocs.org/sdr/DALA2026090204941.md): Cover · broken · Aug 29, 2026 · N325NB · Airbus A319114 · Emergency Lighting
  > LIGHT COVER ABOVE 1L DOOR BROKEN/FELL OFF. SECURED LIGHT COVER ABOVE 1L DOOR. OPS CHKD GOOD. (LP: 9489242, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026081104622](https://openairdocs.org/sdr/DALA2026081104622.md): Light Sys · faulted · Aug 8, 2026 · N325NB · Airbus A319114 · Emergency Lighting
  > AFTER 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 DALA2026080604530](https://openairdocs.org/sdr/DALA2026080604530.md): Seal · faulted · Aug 5, 2026 · N325NB · Airbus A319114 · Flight Compartment Equipment
  > AT 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 POP
- [SDR DALA2026053003281](https://openairdocs.org/sdr/DALA2026053003281.md): Power Supply · faulted · May 27, 2026 · N325NB · Airbus A319114 · Emergency Lighting
  > EMERGENCY 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 PRE
- [SDR DALA2026050602892](https://openairdocs.org/sdr/DALA2026050602892.md): Oxygen Box · open · May 4, 2026 · N325NB · Airbus A319114 · Passenger Oxygen System
  > CREW 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 GROUNDED
- [SDR DALA2026042002463](https://openairdocs.org/sdr/DALA2026042002463.md): Repair · not reported · Apr 18, 2026 · N325NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > REMOVE 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 DALA2026042202554](https://openairdocs.org/sdr/DALA2026042202554.md): Skin · not reported · Apr 17, 2026 · N325NB · Airbus A319114 · Standard Practices/Structures
  > DAMAGE 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 DALA2026042002462](https://openairdocs.org/sdr/DALA2026042002462.md): Skin · dented · Apr 17, 2026 · N325NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > UPPER 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 E
- [SDR DALA2026042002461](https://openairdocs.org/sdr/DALA2026042002461.md): Skin · cracked · Apr 17, 2026 · N325NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > LOWER 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 REPAIR
- [SDR DALA2026041702436](https://openairdocs.org/sdr/DALA2026041702436.md): Door Frame · damaged · Apr 16, 2026 · N325NB · Airbus A319114 · Fuselage Main, Structure
  > FR68 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 EVA
- [SDR DALA2026042202551](https://openairdocs.org/sdr/DALA2026042202551.md): Door Frame · not reported · Apr 15, 2026 · N325NB · Airbus A319114 · Standard Practices/Structures
  > DAMAGE 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 DALA2026042202550](https://openairdocs.org/sdr/DALA2026042202550.md): Door Frame · not reported · Apr 15, 2026 · N325NB · Airbus A319114 · Standard Practices/Structures
  > DAMAGE 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 5311-01
- [SDR DALA2026042202553](https://openairdocs.org/sdr/DALA2026042202553.md): Door Frame · damaged · Apr 15, 2026 · N325NB · Airbus A319114 · Fuselage Main, Structure
  > ER/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 DALA2026042002460](https://openairdocs.org/sdr/DALA2026042002460.md): Skin · not reported · Apr 15, 2026 · N325NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > DAMAGE 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 1
- [SDR DALA2026041502383](https://openairdocs.org/sdr/DALA2026041502383.md): Stringer · corroded · Apr 13, 2026 · N325NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > AFT 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 DALA2026042002464](https://openairdocs.org/sdr/DALA2026042002464.md): Lug · damaged · Apr 10, 2026 · N325NB · Airbus A319114 · Trailing Edge Flaps
  > DAMAGE 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. ASSOCIATED
- [SDR DALA2026041202307](https://openairdocs.org/sdr/DALA2026041202307.md): Window Frame · cracked · Apr 9, 2026 · N325NB · Airbus A319114 · Fuselage Main, Structure
  > REQUESTING 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 DALA2026040902270](https://openairdocs.org/sdr/DALA2026040902270.md): Seat Track · corroded · Apr 8, 2026 · N325NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER 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 SECT
- [SDR DALA2026040902269](https://openairdocs.org/sdr/DALA2026040902269.md): Seat Track · corroded · Apr 8, 2026 · N325NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER 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 I
- [SDR DALA2026040902268](https://openairdocs.org/sdr/DALA2026040902268.md): Seat Track · corroded · Apr 8, 2026 · N325NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER 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 I
- [SDR DALA2026040902267](https://openairdocs.org/sdr/DALA2026040902267.md): Seat Track · corroded · Apr 8, 2026 · N325NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER 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 I
- [SDR DALA2026040802232](https://openairdocs.org/sdr/DALA2026040802232.md): Floor Support · corroded · Apr 6, 2026 · N325NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > PASSENGER 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 P
- [SDR DALA2026040602161](https://openairdocs.org/sdr/DALA2026040602161.md): Support Angle · corroded · Apr 5, 2026 · N325NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LOWER 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 1
- [SDR DALA2026040202137](https://openairdocs.org/sdr/DALA2026040202137.md): Skin · damaged · Mar 30, 2026 · N325NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > LOWER 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 53-21-11-3
- [SDR DALA2026033002089](https://openairdocs.org/sdr/DALA2026033002089.md): Seat Track · corroded · Mar 29, 2026 · N325NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER 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 DALA2026033002088](https://openairdocs.org/sdr/DALA2026033002088.md): Seat Track · corroded · Mar 29, 2026 · N325NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER 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 DALA2026032602014](https://openairdocs.org/sdr/DALA2026032602014.md): Power Supply · inoperative · Mar 24, 2026 · N325NB · Airbus A319114 · Emergency Lighting
  > PAX 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 DALA2026032602011](https://openairdocs.org/sdr/DALA2026032602011.md): Support Angle · corroded · Mar 24, 2026 · N325NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > FORWARD 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 C
- [SDR DALA2026012200482](https://openairdocs.org/sdr/DALA2026012200482.md): Slide · low pressure · Jan 17, 2026 · N325NB · Airbus A319114 · Escape Slide
  > RIGHT FWD DERVICE DOOR SLIDE HAS LOW PRESSURE. REMOVED AND REPLACED RIGHT FORWARD DOOR SLIDE IAW AMDS TC 2561-4004-RF. (LP: 9141074)
- [SDR DALA2024021201959](https://openairdocs.org/sdr/DALA2024021201959.md): Skin · dented · Feb 9, 2024 · N325NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3125 THREE DENTS IN FUSELAGE UNDER FWD CARGO DOOR. CORRECTIVE ACTION: REPAIRED PER ER/A 501814-14. (0194327)
- [SDR DALA2024010800299](https://openairdocs.org/sdr/DALA2024010800299.md): Not Reported · not reported · Jan 6, 2024 · N325NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3125 DENT FWD OF L2 DOOR. CORRECTIVE ACTION: REPAIRED PER A319 SRM 53-41-11-283-059. (5381348)
- [SDR DALA2023121210152](https://openairdocs.org/sdr/DALA2023121210152.md): Unknown · unknown · Dec 12, 2023 · N325NB · Airbus A319114 · Emergency Lighting
  > SHIP 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 DALA2023103008915](https://openairdocs.org/sdr/DALA2023103008915.md): Unknown · unknown · Oct 28, 2023 · N325NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 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 DALA2023102008648](https://openairdocs.org/sdr/DALA2023102008648.md): Unknown · unknown · Oct 20, 2023 · N325NB · Airbus A319114 · Fuselage Main, Floor Beam
  > SHIP 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 DALA2023102008647](https://openairdocs.org/sdr/DALA2023102008647.md): Unknown · unknown · Oct 20, 2023 · N325NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 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 DALA2023102008646](https://openairdocs.org/sdr/DALA2023102008646.md): Floorbeam · unknown · Oct 20, 2023 · N325NB · Airbus A319114 · Fuselage Main, Floor Beam
  > SHIP 3125 FLOOR BEAM CORRODED -Y765 FR 68. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 PER A319 SRM 51-42-11. (0026255).
- [SDR DALA2023041503002](https://openairdocs.org/sdr/DALA2023041503002.md): Unknown · unknown · Apr 12, 2023 · N325NB · Airbus A319114 · Airborne Auxiliary Power Unit (APU) System
  > AIRCRAFT 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 LO
- [SDR DALA2023031501884](https://openairdocs.org/sdr/DALA2023031501884.md): Unknown · unknown · Mar 11, 2023 · N325NB · Airbus A319114 · APU Oil System
  > AIRCRAFT 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 DALA2023020700922](https://openairdocs.org/sdr/DALA2023020700922.md): Not Reported · not reported · Feb 1, 2023 · N325NB · Airbus A319114 · Turbine Engine Compressor Section
  > SHIP 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 AM
- [SDR DALA2022110807227](https://openairdocs.org/sdr/DALA2022110807227.md): None · none · Nov 7, 2022 · N325NB · Airbus A319114 · Air Conditioning System
  > SHIP 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 DALA2022060103811](https://openairdocs.org/sdr/DALA2022060103811.md): Mask · deployed · Jun 1, 2022 · N325NB · Airbus A319114 · Passenger Oxygen System
  > SHIP 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 DALA2023062805193](https://openairdocs.org/sdr/DALA2023062805193.md): Unknown · unknown · May 9, 2022 · N325NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 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 DALA2021060703104](https://openairdocs.org/sdr/DALA2021060703104.md): Fan · noisy · Jun 4, 2021 · N325NB · Airbus A319114 · Air Distribution Fan
  > SHIP 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 DALA2021042802451](https://openairdocs.org/sdr/DALA2021042802451.md): Acoustic Liner · corroded · Apr 24, 2021 · N325NB · Airbus A319114 · Engine Air Intake System
  > SHIP 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 DALA2020031201797](https://openairdocs.org/sdr/DALA2020031201797.md): Warning Light · false activation · Mar 11, 2020 · N325NB · Airbus A319114 · Fire Bottle, Fixed
  > SHIP 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 DALA2019102196030](https://openairdocs.org/sdr/DALA2019102196030.md): Panel · torn · Oct 18, 2019 · N325NB · Airbus A319114 · Aerodynamic Fairings
  > ON 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 DALA2019082004860](https://openairdocs.org/sdr/DALA2019082004860.md): Fire Warning · false activation · Aug 19, 2019 · N325NB · Airbus A319114 · Fire Detection
  > IN 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 DALA2019032001835](https://openairdocs.org/sdr/DALA2019032001835.md): Cover · missing · Mar 18, 2019 · N325NB · Airbus A319114 · Main Landing Gear Strut/Axle/Truck
  > PDA 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

Next page: https://openairdocs.org/aircraft/N325NB/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N325NB/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.