# Service difficulty reports: N321NB

A list on [N321NB](https://openairdocs.org/aircraft/N321NB.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 · 106 reports

- [SDR DALA2025122209287](https://openairdocs.org/sdr/DALA2025122209287.md): Cover · out of adjust · Dec 19, 2025 · N321NB · Airbus A319114 · Emergency Exits
  > LEFT WING EMER DOOR KEPT SHOWING OPEN THEN ARMED FA SAYS DOOR SEAL ON TOP IS VISIBLE. FOUND COVER FLAP FOR PROX SWITCH OUT OF PLACE. REMOVED AND RE INSTALLED. COVER FLAP. OPS CK. GOOD. A/C OK FOR SVC. REF. AMM 52-71. (7797136)
- [SDR DALA2025092907080](https://openairdocs.org/sdr/DALA2025092907080.md): Panel · damaged · Sep 27, 2025 · N321NB · Airbus A319114 · Fixed Inner Doors
  > FWD LATCH ON LAV SERVICE PANEL DAMAGED/INOP. REMOVED LAV SVC DOOR IAW A319 AMM 52-42. R/R LATCH ASSY IAW A319 SRM 52-41. INSTALLED LAV SVC DOOR IAW A319 AMM 52-42. (1220476).
- [SDR DALA2025071605349](https://openairdocs.org/sdr/DALA2025071605349.md): Sensor · fod · Jul 15, 2025 · N321NB · Airbus A319114 · Door Warning System
  > SHIP 3121, 1R DOOR WILL NOT INDICATE ARMED. REMOVED DEBRIS. IAW A319 AMM 52-20.
- [SDR DALA2025050103352](https://openairdocs.org/sdr/DALA2025050103352.md): Dampener · no test · Apr 26, 2025 · N321NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3121 DISC: DONT PASS OPERATIONAL TEST EMERGENCY DOOR DAMPER ON PASSENGER CREW DOO R 831 (REFER TO AMDS CARD 5210-7089-LF RII). C/A: REPLACED DOOR DAMPER ON PASSENGER CREW DOOR 831 AS PER A320 FAM AMM 52-11-14-000-001-A AS PER A320 FAM AMM 52-11-14-400-001
- [SDR DALA2025042403196](https://openairdocs.org/sdr/DALA2025042403196.md): Door Frame · cracked · Apr 24, 2025 · N321NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE 2 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.110 INCH APPROX, HOLE DIAMETER IS 0.250 INCH APPROX, AA 5311-01216, AD RELATED, ACTIONS REQUIRED PRIOR TO FURTHER FLIG
- [SDR DALA2025042403195](https://openairdocs.org/sdr/DALA2025042403195.md): Door Frame · cracked · Apr 24, 2025 · N321NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE 4 AT DOOR S TOP FITTING 1 POSITION, CRACK DIRECTION IS 6 AND 12 OCLOCK, CRACK DEPT. PERFORMED REPAIR INSTRUCTIONS ON FRAME 68 RH SIDE IN HOLE 4 AT DOOR STOP FITTING 1 POSITION AS PER A319 SRM SRM 53-4
- [SDR DALA2025042403193](https://openairdocs.org/sdr/DALA2025042403193.md): Frame · cracked · Apr 23, 2025 · N321NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE 4 AT DOOR S TOP FITTING 1 POSITION, CRACK DIRECTION ARE 6 AND 12 OCLOCK, CRACK DEP TH IS 0.120 INCH APPROX, HOLE DIAMETER IS 0.250 INCH APPROX, AA 5311-0 1216, AD RELATED, ACTIONS REQUIRED PRIOR TO FUR
- [SDR DALA2024122311915](https://openairdocs.org/sdr/DALA2024122311915.md): Table · damaged · Dec 21, 2024 · N321NB · Airbus A319114 · Buffet/Galleys
  > SHIP 3121 AFT GALLEY COMPARTMENT 512 WORK TOP LOWER SKIN AREA OF DELAMINATION AT BOTH TROLLEY BLOCK AREAS. CORRECTIVE ACTION: DAMAGE HAS BEEN REPAIRED IAW ER/A 623096-14AD. (0721410)
- [SDR DALA2024122311914](https://openairdocs.org/sdr/DALA2024122311914.md): Table · damaged · Dec 21, 2024 · N321NB · Airbus A319114 · Buffet/Galleys
  > SHIP 3121 AFT GALLEY COMPARTMENT 511 WORKTOP LOWER SKIN BULGED. CORRECTIVE ACTION: DAMAGE HAS BEEN REPAIRED IAW ER/A 623096-14AD. (0721405)
- [SDR DALA2024122311913](https://openairdocs.org/sdr/DALA2024122311913.md): Table · damaged · Dec 21, 2024 · N321NB · Airbus A319114 · Buffet/Galleys
  > SHIP 3121 AFT GALLEY COMPARTMENT 511 WORKTOP LOWER SKIN AREA OF DELAMINTION AT OUTBD TROLLEY BLOCK AREA. CORRECTIVE ACTION: DAMAGE HAS BEEN REPAIRED IAW ER/A 623096-14AD. (0721402)
- [SDR DALA2024122311912](https://openairdocs.org/sdr/DALA2024122311912.md): Table · damaged · Dec 21, 2024 · N321NB · Airbus A319114 · Buffet/Galleys
  > SHIP 3121 AFT GALLEY COMPARTMENT 511 WORKTOP LOWER SKIN AREA OF DELAMINTION AT INBD TROLLEY BLOCK AREA. CORRECTIVE ACTION: DAMAGE HAS BEEN REPAIRED IAW ER/A 623096-14AD. (0721401)
- [SDR DALA2024110210585](https://openairdocs.org/sdr/DALA2024110210585.md): Bleed Air Sys · leaking · Nov 1, 2024 · N321NB · Airbus A319114 · Pneumatic Distribution System
  > SHIP 3121 - ATB - DUE TO AIR ENG 2 BLEED LEAK ECAM MESSAGE. UNABLE TO CONTINUE DUE TO WEATHER IN MSP. CORRECTIVE ACTION: FOUND LEAKS ON TLT, TCT, AND PRV. REPLACED PYLON OVERHEAT SENSING ELEMENT. FAN CONTROL THERMOSTAT, BLEED PRESSURE REGULATOR VALVE CONTROL,
- [SDR DALA2024012901283](https://openairdocs.org/sdr/DALA2024012901283.md): Bolt · loose · Jan 27, 2024 · N321NB · Airbus A319114 · Nose/Tail Landing Gear
  > SHIP 3121 - MISC/DE - DUE TO A L/G SHOCK ABSORBER FAULT AND LOSS OF BOTH AUTO PILOTS. CORRECTIVE ACTION: FOUND NLG AIR/GROUND HOUSING LOWER BOLT LOOSE, TIGHTENED SAME. FOUND SENSOR 24GA INDUCTANCE VALUE OUT OF RANGE, REPLACED SAME. VERIFIED NLG STRUT SERVICED
- [SDR DALA2024010800300](https://openairdocs.org/sdr/DALA2024010800300.md): Not Reported · not reported · Jan 6, 2024 · N321NB · Airbus A319114 · Auto Flight System
  > SHIP 3121 - ATO - AT 60KTS DUE AN ELAC 1 PITCH FAULT ECAM MESSAGE. CORRECTIVE ACTION: R/R ELAC 1. OPS CHECK GOOD. OK FOR SERVICE. (4862934)
- [SDR DALA2023110609112](https://openairdocs.org/sdr/DALA2023110609112.md): Unknown · unknown · Nov 5, 2023 · N321NB · Airbus A319114 · Air Distribution System
  > SHIP 3121 - CREW REPORTED VISIBLE SMOKE AND ODOR IN COCKPIT AFTER TAKEOFF, DONNED 02 MASKS. SMOKE/FUMES DISSIPATED, CONTINUED TO SLC. CORRECTIVE ACTION: FOUND A COPIOUS AMOUNT OF DE-ICE FLUID DRIPPING FROM THE TAIL WITH HEAVY INGESTION INTO THE APU INLET. APU
- [SDR DALA2023101308424](https://openairdocs.org/sdr/DALA2023101308424.md): Unknown · unknown · Oct 12, 2023 · N321NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3121 RH WING INBOARD FLAP RIB 9 ASSY FITTING INNER/OUTER ALUMINIUM BORES AND INBOARD/OUTBOARD LUG FACES CORROSION. CORRECTIVE ACTION: REPAIRED PER ERA 607784-14 (0014274).
- [SDR DALA2023050903652](https://openairdocs.org/sdr/DALA2023050903652.md): Unknown · unknown · May 8, 2023 · N321NB · Airbus A319114 · Fuselage Structure (General)
  > AIRCRAFT 3121, FCS REPAIR EXTERNAL SKIN LOCATED R /H LOWER STRINGER AT FR 7 LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 608430-14 REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI 608430-14 REV.0, REV.1, REV.2 AND REV.3 IT HAS BEENVALIDATED. PERFORMED REPA
- [SDR DALA2023050903651](https://openairdocs.org/sdr/DALA2023050903651.md): Unknown · unknown · May 7, 2023 · N321NB · Airbus A319114 · Fuselage Structure (General)
  > AIRCRAFT 3121, REPLACE SEAT TRACK -Y765 FR35 TO FR36 PREVIOUSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS IN PASSENGER CABIN (MEASURES OF REWORKED D=0.068 INCH, W=0.767, L=4.230). CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOC.
- [SDR DALA2023050903650](https://openairdocs.org/sdr/DALA2023050903650.md): Unknown · unknown · May 7, 2023 · N321NB · Airbus A319114 · Fuselage Structure (General)
  > AIRCRAFT 3121, REPLACE SEAT TRACK Y1292 FR41 TO FR47 PREVIOUSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS IN PASSENGER CABIN (MEASURES OF REWORK D=0.028 INCH, W=0.767 INCH, L=2.364 INCH). CORRECTIVE ACTION: REPLACED SEAT TRACK Y1
- [SDR DALA2023050703548](https://openairdocs.org/sdr/DALA2023050703548.md): Unknown · unknown · May 7, 2023 · N321NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > AIRCRAFT 3121, ELONGATED HOLE LEADING EDGE ON OUTER WING FRONT SPAR AND AT LEVEL OF R IB 1 ON INBOARD EGDE OF SLAT 1 ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FIXED LEADING EDGE INBOARD SIDE LH WING AS PER ER/A 607848-14. (LP 2755098)
- [SDR DALA2023050703550](https://openairdocs.org/sdr/DALA2023050703550.md): Unknown · unknown · May 4, 2023 · N321NB · Airbus A319114 · Trailing Edge Flaps
  > AIRCRAFT 3121, CORROSION INTERCONNECTING STRUT IB FLAP ON LH WING (REFER TO AMDS CARD 2751-9202 RII). CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT IB FLAP ON LH WING ON SERVICEABLE CONDITION AS PER A320 FAM AMM 27-51-44-000-001-A AND AMM27-51- 44-400-001-
- [SDR DALA2023042903344](https://openairdocs.org/sdr/DALA2023042903344.md): Unknown · unknown · Apr 26, 2023 · N321NB · Airbus A319114 · Trailing Edge Flaps
  > AIRCRAFT 3121, CORROSION FLAP TRACK 3 AND 4 CARRIAGE BOLT ON LH WING (2 EA). CORRECTIVE ACTION: REPLACED FLAP TRACK 3 AND 4 CARRIAGE BOLT ON L/H WING. (LP 2738838)
- [SDR DALA2023042903343](https://openairdocs.org/sdr/DALA2023042903343.md): Unknown · unknown · Apr 25, 2023 · N321NB · Airbus A319114 · Fuselage Main, Structure
  > AIRCRAFT 3121, DENTS ON INTERNAL STRUCTURE CROSS BEAM AT LEVEL FRAME 25 AND BETWEEN STRINGER 38LH TO STRINGER 41RH IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED CROSS BEAM ON INTERNAL STRUCTURE AT LEVEL FRAME 25 AND BETWEEN STRINGER 38LH TO STRINGER 41
- [SDR DALA2023042903342](https://openairdocs.org/sdr/DALA2023042903342.md): Unknown · unknown · Apr 23, 2023 · N321NB · Airbus A319114 · Trailing Edge Flaps
  > AIRCRAFT 3121, CORROSION FLAP TRACK 2 CARRIAGE BOLT ON RH WING (1 EA). CORRECTIVE ACTION: REPLACED FLAP TRACK 2 CARRIAGE BOLT ON R/H WING AND INSTALLATION. (LP 2733776)
- [SDR DALA2023042403187](https://openairdocs.org/sdr/DALA2023042403187.md): Unknown · unknown · Apr 23, 2023 · N321NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 3121, CORROSION SEAT TRACK -Y1292 BTW FR 20 TO FR 21 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1292 BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11 DWG 53110920. (LP 2733811)
- [SDR DALA2023042403186](https://openairdocs.org/sdr/DALA2023042403186.md): Unknown · unknown · Apr 23, 2023 · N321NB · Airbus A319114 · Fuselage Structure (General)
  > AIRCRAFT 3121, CORROSION SEAT TRACK -Y765 LOCATED AT LEVEL FR20 FWD GALLEY AREA AREA (SSI: 531 189). CORRECTIVE ACTION: REPLACED SEAT TRACK AND FASTENERS LOC BTW FR12 TO FR24 -Y765 IN FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND DRAWING D53110920RELEASE DATE 2
- [SDR DALA2023042403185](https://openairdocs.org/sdr/DALA2023042403185.md): Unknown · unknown · Apr 23, 2023 · N321NB · Airbus A319114 · Fuselage Structure (General)
  > AIRCRAFT 3121, CRACK SEAT TRACK -Y254 LOC. FR 24 TO FR 25 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y254 LOC. FR 24 TO FR 35 IN PASSENGER CABIN AS PER A319 SRM 51-42-11, DWG D53110920. (LP 2733780)
- [SDR DALA2023050703549](https://openairdocs.org/sdr/DALA2023050703549.md): Unknown · unknown · Apr 18, 2023 · N321NB · Airbus A319114 · Trailing Edge Flaps
  > AIRCRAFT 3121, CORROSION INTERCONNECTING STRUT IB FLAP ON RH WING (REFER TO AMDS CARD 2751-9202 RII). CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT IB FLAP ON RH WING ON SERVICEABLE CONDITION AS PER A320 FAM AMM 27-51-44-000-001-A AND27-51-44- 400-001-A. (
- [SDR DALA2023040602699](https://openairdocs.org/sdr/DALA2023040602699.md): Unknown · unknown · Apr 4, 2023 · N321NB · Airbus A319114 · Trailing Edge Flaps
  > AIRCRAFT 3121, CORROSION SUPPORT BRACKET ON INTERNAL AREA AT RIB6 OUTBOARD FLAP ON LH WING. CORRECTIVE ACTION: REPLACED LEFT OUTBOARD FLAP. (LP 2703895)
- [SDR DALA2023040202512](https://openairdocs.org/sdr/DALA2023040202512.md): Unknown · unknown · Mar 29, 2023 · N321NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 3121, CORROSION SEAT TRACK +Y765 LOCATED FROM FR65 TO FR66 AT AFT GALLEY AREA (SSI: 534147). CORRECTIVE ACTION: REPLACED SEAT TRACK Y765 LOCATED FROM FR65 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND AS PER A319 51-72-11. (LP 2693938)
- [SDR DALA2023040202511](https://openairdocs.org/sdr/DALA2023040202511.md): Unknown · unknown · Mar 29, 2023 · N321NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 3121, CORROSION SEAT TRACK -Y1292 LOCATED FROM FR65 TO FR66 AT AFT GALLEY AREA (SSI:534147). CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1292 LOCATED FROM FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM 51-72-11 AND DWGD53472832 ISSUE: Y
- [SDR DALA2023032702351](https://openairdocs.org/sdr/DALA2023032702351.md): Unknown · unknown · Mar 25, 2023 · N321NB · Airbus A319114 · Fuselage Floor Panel
  > AIRCRAFT 3121, CORROSION RAIL DUMMY Y503.2 FR 16 AT FWD GALLEY AREA (SSI 531189). CORRECTIVE ACTION: REPLACED RAIL DUMMY AND FASTENERS LOC BTW FR12 TO FR16 IN FWD GALLEY AS PER A319 SRM 51-72-11 AND DWG D53110984, RELEASE DATE:25-JUN-05, ISSUE C00. (LP 2688011
- [SDR DALA2023032602311](https://openairdocs.org/sdr/DALA2023032602311.md): Unknown · unknown · Mar 24, 2023 · N321NB · Airbus A319114 · Fuselage Floor Panel
  > AIRCRAFT 3121, ELONGATED HOLE FLOOR STRUCTURE SPLICE FRAME 24 Y1292 IN PASSENGER CABIN (2 EA). CORRECTIVE ACTION: REPLACED SPLICE (2EA) AND FASTENERS LOC FR24 Y1292 IN FWD GALLEY AS PER A319 SRM 51-72-11 AND DWG D 53111225 RELEASE DATE05-JUN-12 ISSUE A. (LP 26
- [SDR DALA2023032602310](https://openairdocs.org/sdr/DALA2023032602310.md): Unknown · unknown · Mar 24, 2023 · N321NB · Airbus A319114 · Fuselage Floor Panel
  > AIRCRAFT 3121, CORROSION FLOOR BEAM +Y1292 ON FR 16 AT FWD GALLEY AREA (SSI 531189). CORRECTIVE ACTION: REPLACED FLOOR BEAM AND FASTENERS LOC BTW FR12 TO FR24 Y1292 IN FWD GALLEY AS PER A319 SRM 51-72-11 AND DWG D53110920 RELEASEDATE 28-APR-21 ISSUE E00 RII. (
- [SDR DALA2023032302266](https://openairdocs.org/sdr/DALA2023032302266.md): Unknown · unknown · Mar 22, 2023 · N321NB · Airbus A319114 · Fuselage Floor Panel
  > AIRCRAFT 3121, CORROSION FLOOR BEAM -Y765 LOCATED AT LEVEL FR 68 AT AFT GALLEY AREA (SSI 534147). CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOCATED BTW FR66 TO FR 70 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND DWG #D53472000 RELEASES DATE06/JAN/03 ISSUE
- [SDR DALA2023012600648](https://openairdocs.org/sdr/DALA2023012600648.md): Motor · odor · Jan 25, 2023 · N321NB · Airbus A319114 · Windshield/Door Rain/Ice Removal
  > SHIP 3121 - UPON ARRIVAL AT GATE (AUS), COCKPIT SMELLED LIKE AN ELEC BURNING SMELL. CORRECTIVE ACTION: R/R RECIRC CARTRIDGES. R L/H WIPER MOTOR CONVERTER (6DB1) PER A319 AMM 30-45. (9842384)
- [SDR DALA2022121208001](https://openairdocs.org/sdr/DALA2022121208001.md): Computer · failed · Dec 7, 2022 · N321NB · Airbus A319114 · Flight Control System
  > SHIP 3121 - ATO - AT 65 KTS DUE TO A ELAC 1 PITCH FAULT. CORRECTIVE ACTION: REPLACED ELAC 1. (9715176)
- [SDR DALA2022072105043](https://openairdocs.org/sdr/DALA2022072105043.md): None · none · Jul 21, 2022 · N321NB · Airbus A319114 · Flight Control System
  > SHIP 3121 - MISC/DE - DUE TO MULTIPLE MOMENTARY FAILURES AND F/CNTL ALTN LAW DISPLAYED WHEN CONFIGURING FOR FINAL APPROACH. CORRECTIVE ACTION: REPLACED FLIGHT CONTROL ACCELEROMETER 12CE1 DUE TO MULTIPLE CLASS 2 FAILURE MESSAGES. (8971178)
- [SDR DALA2022070504638](https://openairdocs.org/sdr/DALA2022070504638.md): None · none · Jul 2, 2022 · N321NB · Airbus A319114 · Air Conditioning System
  > SHIP 3121 - ATB - DUE TO AN ELECTRICAL BURNING ODOR IN THE FLIGHT DECK. CORRECTIVE ACTION: FOUND #1 ENGINE ANTI-ICE SWITCH (2DN1) WITH STRONG BURNT SMELL. R/R BOTH ENGINE ANTI-ICE SWITCHES (2DN1 AND 2DN2). OPS CHECK NORMAL AND VERIFICATION FLIGHT OK WITH NO IS
- [SDR DALA2022063004554](https://openairdocs.org/sdr/DALA2022063004554.md): None · none · Jun 30, 2022 · N321NB · Airbus A319114 · Exterior Lighting
  > SHIP 3121 - ACRID ELECTRICAL BURNING SMELL IN COCKPIT DURING INITIAL CLIMBOUT AT 10,000FT. CORRECTIVE ACTION: R/R LEFT AND RIGHT LANDING LIGHT CONTROL SWITCHES 5LB AND 6LB PER A319 AWM 33-42-01. R/R NOSE LANDING GEAR TAKEOFF LIGHT SWITCH 4LR PER A319 AWM 33-46
- [SDR DALA2022062904529](https://openairdocs.org/sdr/DALA2022062904529.md): None · none · Jun 29, 2022 · N321NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3121 - CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER LOWER POST. CORRECTIVE ACTION: COMPLIED WITH ER/A 599794-14AD REV ORIGINAL.(2298338)
- [SDR DALA2022062904528](https://openairdocs.org/sdr/DALA2022062904528.md): None · none · Jun 29, 2022 · N321NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3121 - CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER LOWER POST. CORRECTIVE ACTION: COMPLIED WITH PRI 599792-14REV 0 AND REV I.VALIDATED ER/A 599792-14 REV ORIGINAL.(2298335)
- [SDR DALA2022062904527](https://openairdocs.org/sdr/DALA2022062904527.md): None · none · Jun 29, 2022 · N321NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3121 - CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER LOWER POST CONTINUITTY F ITTING LH SIDE. CORRECTIVE ACTION: COMPLIED SECTION I REPAIR INSTRUCTIONS AS PER ER/A599793-14AD REV. ORIGINAL(2298302)
- [SDR DALA2022062904526](https://openairdocs.org/sdr/DALA2022062904526.md): None · none · Jun 29, 2022 · N321NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3121 - REPLACE CONTINUITY FITTINGS RH AND LH. (2 E/A) LOC. BTW FR 1 AND FR 3 AT UPPER FUSELAGE. CORRECTIVE ACTION: ACCOMPLISHED SECTION I REPAIR INSTRUCTIONS ON WINDSHIELD PER ER/A 599794-14ADPRI REV-ORIGINAL.(2298292)
- [SDR DALA2022062204357](https://openairdocs.org/sdr/DALA2022062204357.md): Frame · cracked · Jun 21, 2022 · N321NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3121 - CRACK INDICATION ON FRAME FR16 LH, DOOR STOP 7, HOLE 3 (LOWER INB) ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR LOC FRAME 16 LH, DOOR STOP 7, HOLE 3 AS PER ER/ A 599711-14AD REV. ORIGINAL(2287502)
- [SDR DALA2022062204356](https://openairdocs.org/sdr/DALA2022062204356.md): Frame · cracked · Jun 21, 2022 · N321NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3121 - CRACK INDICATION ON FRAME FR 16 LH, DOOR STOP 7, HOLE 1 (UPPER INB) ON UPPER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR LOC FRAME 16 LH, DOOR STOP 7, HOLE 1 AS PER ER/ A 599711-14AD REV. ORIGINAL(2287509)
- [SDR DALA2022052003459](https://openairdocs.org/sdr/DALA2022052003459.md): None · none · May 17, 2022 · N321NB · Airbus A319114 · Flight Control System
  > SHIP 3121 - ABORT T/O DUE TO F/CTL ELAC 1 PITCH FAULT. CORRECTIVE ACTION: REMOVED LOB ELEVATOR HYD ACTUATOR. INSTALLED L OB ELV HYD SERVO CONTROL REF A319 AMM 27-34. R/R ELAC #1 COMPUTER. OPS CHECK GOOD REF A319 AMM 27-93.(2239143)
- [SDR DALA2022051703415](https://openairdocs.org/sdr/DALA2022051703415.md): None · none · May 12, 2022 · N321NB · Airbus A319114 · Flight Control System
  > SHIP 3121 - ATO - DUE TO ELAC 1 PITCH FAULT AT THROTTLE UP FOR TAKE-OFF. CORRECTIVE ACTION: REMOVED AND REPLACED SERVOVALVE OF ELEVATOR SERVOVONTROL ACTUATOR 34CE3 IAW A319 AMM 27-34-51.(8667912)
- [SDR DALA2022042102790](https://openairdocs.org/sdr/DALA2022042102790.md): None · none · Apr 20, 2022 · N321NB · Airbus A319114 · Passenger Oxygen System
  > SHIP 3121 - OXYGEN PANEL AROUND ROW 16 LEFT OPENED ON LANDING. CORRECTIVE ACTION: REINSTALLED O2 PANEL ASSY @16 ABC PER A319 AMM 35-21. (6183714)
- [SDR DALA2022020700757](https://openairdocs.org/sdr/DALA2022020700757.md): None · none · Feb 6, 2022 · N321NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3121 - L1 DOOR MAY NEED ADJUSTMENT. HANDLE HAS TO BE HELD DOWN TO ARM. CORRECTIVE ACTION: CLEANED AND REMOVED DEBRIS FROM L1 DOOR LWR LATCHES. DOOR HANDLE AND SLIDE ARMING LEVER OPS GOOD. IAW A319 AMM 52-73-00. (8870981)

Next page: https://openairdocs.org/aircraft/N321NB/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 = 'N321NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N321NB/reports

---
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.