# Service difficulty reports: N327NB

A list on [N327NB](https://openairdocs.org/aircraft/N327NB.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 · 124 reports

- [SDR DALA2026092805367](https://openairdocs.org/sdr/DALA2026092805367.md): Oxygen Panel · unsecure · Sep 25, 2026 · N327NB · Airbus A319114 · Passenger Oxygen System
  > SEATS 10E, 10D, & 10F OXYGEN PANEL CAME LOOSE DURING TAKE OFF. SECURED THE PANEL. NOW CHKD GOOD. (LP: 1831789, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026092405335](https://openairdocs.org/sdr/DALA2026092405335.md): Blades · dented · Sep 21, 2026 · N327NB · Airbus A319114 · Turbine Engine Air Inlet Section
  > FOUND TWO BLADES DENTED ON NR 2 ENG. FOUND BLADES 29 AND 30 DENTS TO BE OUT OF LIMITS IAW AMM 72 -21-00-320-001-Q, DAMAGE EXCEEDS A DEPTH OF 1 INCH IN SECTION D INTO SECTION C. REROMVED SPINNER FRONT & REAR CONE IAW AMM 72-21 REMOVED AND REPLACED THE FAN B
- [SDR DALA2026082404780](https://openairdocs.org/sdr/DALA2026082404780.md): Cowling · damaged · Aug 20, 2026 · N327NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > WITH THE PARKING BRAKE SET, THE JETWAY HIT THE AIRCRAFT. PERFORMED INSP IAW AMM 05-51-27-200-001-A FOUND INLET COWL DAMAGED. NO ADDITIONAL DAMAGE NOTED. W.I.P. R & R ENG #1 AIR INTAKE COWL PER AMM 71-11. NO LEAKS. OK FOR SERVICE. (LP: 7916802, AIRCRAFT WAS
- [SDR DALA2026031701839](https://openairdocs.org/sdr/DALA2026031701839.md): Fitting · not reported · Mar 15, 2026 · N327NB · Airbus A319114 · Fuselage Main, Structure
  > PERFORM ER/A 569090-14AD. C/A: COMPLIED WITH ER/A 631878-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON PRI 631878-14AD REV.0 IT HAS BEEN VALIDATED. PERFORMEDREPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITTINGS LH AND RH AS PER ERA 6
- [SDR DALA2026031701838](https://openairdocs.org/sdr/DALA2026031701838.md): Fitting · not reported · Mar 14, 2026 · N327NB · Airbus A319114 · Fuselage Main, Structure
  > PERFORM ER/A 631878-14AD CONTINUITY FITTINGS REPLACEMENT. C/A: COMPLIED WITH ER/A 631878-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON PRI 631878-14AD REV.0 IT HAS BEEN VALIDATED. PERFORMEDREPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY
- [SDR DALA2026031701837](https://openairdocs.org/sdr/DALA2026031701837.md): Fitting · not reported · Mar 14, 2026 · N327NB · Airbus A319114 · Fuselage Main, Structure
  > PERFORM ER/A 631878-14AD CONTINUITY FITTINGS REPLACEMENT. COMPLIED WITH ER/A 631878-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON PRI 631878-14AD REV.0 IT HAS BEEN VALIDATED. PERFORMEDREPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITT
- [SDR DALA2026031301774](https://openairdocs.org/sdr/DALA2026031301774.md): Seat Track · corroded · Mar 12, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON THE SEAT TRACK +Y1292 AT FWD GALLEY AREA (SSI:531189). REPLACED THE SEAT TRACK Y1292 LOC. BTW FR 12 TO FR 24 AT FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11. (LP 1491705)
- [SDR DALA2026031301773](https://openairdocs.org/sdr/DALA2026031301773.md): Floor Support · corroded · Mar 12, 2026 · N327NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT -Y1292.0, BTW FR 66 TO FR 68 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR SUPPORT - Y1292.0, BTW FR 66 TO FR68 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11. (LP 1491698)
- [SDR DALA2026031001634](https://openairdocs.org/sdr/DALA2026031001634.md): Fitting · damaged · Mar 5, 2026 · N327NB · Airbus A319114 · Fuselage Main, Structure
  > DURING CURRENT M2 FRONT WINDSHIELD FRAMES SCHEDULED TO BE REPLACED PER ER/A 569090-14AD REV A, HOWEVER MIRROR FTG REPAIR WAS FOUND FEASIBLE. MIRROR FTG REPAIR INSTALLED PER THIS ER/A 569090-14AD REV B. PER SECTION IV OF 56909014AD REV B ACCOMPLISH SECTION IV
- [SDR DALA2026031001633](https://openairdocs.org/sdr/DALA2026031001633.md): Window Frame · damaged · Mar 5, 2026 · N327NB · Airbus A319114 · Fuselage Main, Structure
  > DURING CURRENT M2 FRONT WINDSHIELD FRAMES SCHEDULED TO BE REPLACED PER ER/A 569090-14AD REV A, HOWEVER MIRROR FTG REPAIR WAS FOUND FEASIBLE. MIRROR FTG REPAIR INSTALLED PER THIS ER/A 569090-14AD REV B. C/A: *DTE* PER SECTION DTE OF 569090-14AD REV B THE REPAIR
- [SDR DALA2026030801586](https://openairdocs.org/sdr/DALA2026030801586.md): Fitting · damaged · Mar 5, 2026 · N327NB · Airbus A319114 · Fuselage Main, Structure
  > 1 RPTD BY BAMBERG 00197334 SAL 05MAR26 ENTR 00197334 S DURING CURRENT M2 FRONT WINDSHIELD FRAMES WERE SCHEDULED TO BE REPLACED PER ER/A 569090-14AD REV A, HOWEVER MIRROR FTG REPAIR WAS FOUND FEASIBLE. THIS ER/A IS ISSUED TO REPLACE CONTINUITY FTGS IN CONJUNCTI
- [SDR DALA2026030801585](https://openairdocs.org/sdr/DALA2026030801585.md): Floor Support · corroded · Mar 5, 2026 · N327NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLE Y AREA (SSI 534147). REPLACED FLOOR SUPPORT - Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11 AND DWG D53472189, DWG D53472089, DWG D53474250. MEA
- [SDR DALA2026030801584](https://openairdocs.org/sdr/DALA2026030801584.md): Shear Tie · corroded · Mar 5, 2026 · N327NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > CORROSION INTERNAL STRUCTURE SHEAR TIE FR30 STE40R TO STR41R IN FWD CARGO COMPARTMENT. REPLACED SHEAR TIE LOCATED FR30 AND STR40R TO STR41R IN FWD CARGO COMPARTMENT IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53233211 ISSUE: D00 RELEASE DATE: 28-MAY-98 TOOK MEASU
- [SDR DALA2026030301460](https://openairdocs.org/sdr/DALA2026030301460.md): Stringer · corroded · Feb 28, 2026 · N327NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > CORRODED STRINGER 42R BTW FR29 TO FR30 IN FWD CARGO COMPARTMENT. REPLACED DOUBLER STRINGER 42R AND FASTENERS.LOC BTW FR28 TO FR34 IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11, DWG: D53233523, RELEASE DATE:21/OCT/98, ISSUE: D00 AND DWG: D53230319, RELEAS
- [SDR DALA2026030301459](https://openairdocs.org/sdr/DALA2026030301459.md): Shear Tie · corroded · Feb 27, 2026 · N327NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > CORROSION INTERNAL STRUCTURE ON SHEAR TIE FR30 LOC STR41R TO STR42R IN FWD CARGO COMPARTMENT. REPLACED SHEAR TIE AND FASTENERS ON FR30 LOC STR41R TO STR42R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11-801, SRM 51-72-11 AND DWG: D53230337, ISSUE:DO0 RELEA
- [SDR DALA2026030301458](https://openairdocs.org/sdr/DALA2026030301458.md): Shear Tie · corroded · Feb 27, 2026 · N327NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > CORROSION INTERNAL STRUCTURE SHEAR TIE FR28 STR41R TO STR42R IN FWD CARGO COMPARTMENT. FINAL REPAIR RESOLUTION: ADDED INFORMATION REQUIRED.REPLACED SHEAR TIE AND FASTENERS ON FR28 STR41R TO STR42R IN FWD CARGO BAY IAW SRM 51-42-11-801, SRM 51-72-11 AND DWG: D
- [SDR DALA2026022701380](https://openairdocs.org/sdr/DALA2026022701380.md): Seat Track · corroded · Feb 26, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK +Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA (SSI 534147). REPLACED SEAT TRACK Y1292 LOCATED AT FR64 TO FR 66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG:10N01048, ISSUE: F. RELEASE DATE: 19-MAY-15, MEASURE OF CORR
- [SDR DALA2026022701378](https://openairdocs.org/sdr/DALA2026022701378.md): Floor Support · corroded · Feb 25, 2026 · N327NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR BEAM LOCATED BTW FR 16 TO FR 18 AND Y254 AT FWD GALLEY AREA (SSI 531189). FINAL REPAIR RESOLUTION: REPLACED FLOOR BEAM Y254 LOCATED BETWEEN FR12 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG.D53110920 ISSUE: E00 RELE
- [SDR DALA2026022401324](https://openairdocs.org/sdr/DALA2026022401324.md): Floorbeam · corroded · Feb 23, 2026 · N327NB · Airbus A319114 · Fuselage Main, Floor Beam
  > CORRODED FLOORBEAM LOCATED BTW FR 18 - FR 20, -Y 254 AT FWD GALLEY AREA. REPLACED FLOORBEAM, FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, & DWG D53111462. (LP 1464261)
- [SDR DALA2026022101252](https://openairdocs.org/sdr/DALA2026022101252.md): Seat Track · corroded · Feb 20, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 3127, CORROSION SEAT TRACK -Y1292 AT FWD GALLEY AREA (SSI:531189). CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1292 AND FASTENERS BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWG D53110920. (LP 1460565)
- [SDR DALA2026021901181](https://openairdocs.org/sdr/DALA2026021901181.md): Floor Support · corroded · Feb 18, 2026 · N327NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT -Y765 LOCATED BTW FR 67 TO FR 68 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT -Y765 AND FASTENERS LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53472816. (LP 1457078)
- [SDR DALA2026021601063](https://openairdocs.org/sdr/DALA2026021601063.md): Seat Track · corroded · Feb 15, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK +Y765 AT FWD GALLEY AREA. REPLACED SEAT TRACK Y765 ON FWD GALLEY AREA IAW SRM 51-42-11-801 AND SRM 51-72-11. (LP 1452655)
- [SDR DALA2026021201024](https://openairdocs.org/sdr/DALA2026021201024.md): Support · corroded · Feb 11, 2026 · N327NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION ON THE LOWER SILL, FR 68 LT SIDE IN THE AFT GALLEY AREA. PERFORMED A PERMANENT REPAIR ON THE LOWER SILL IAW SRM 53-41-14-300-001, STEP 2.A, FIG.001, SHEET 4, PRINCIPLE 7. (LP 1447024)
- [SDR DALA2026021201023](https://openairdocs.org/sdr/DALA2026021201023.md): Seat Track · corroded · Feb 11, 2026 · N327NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK, -Y765 IN THE FWD GALLEY AREA. REPLACED SEAT TRACK -Y765, BTW FR 12 TO FR 24 IAW SRM 51-42-11, & SRM 51-72-11. (LP 1447020)
- [SDR DALA2024031103201](https://openairdocs.org/sdr/DALA2024031103201.md): Skin · damaged · Mar 8, 2024 · N327NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3127 BURNED RIVET ON STR 31 BETWEEN FR 1 AND FR 2. CORRECTIVE ACTION: DRILLED UP HOLE PER A319 SRM 53-11-11. INSTALLED PERMENANT FASTENERPER A319 SRM 53-11-11-300-034. (0235398)
- [SDR DALA2024031103200](https://openairdocs.org/sdr/DALA2024031103200.md): Skin · damaged · Mar 8, 2024 · N327NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3127 BURNED RIVET ON FR3 APPROX 4 INCHES ABOVE STR 31. CORRECTIVE ACTION: DRILLED UP HOLE PER A319 SRM 53-11-11. INSTALLED PERMANENT FASTENER PER A319 SRM 53-11-11-300-034. (0235394)
- [SDR DALA2024031103199](https://openairdocs.org/sdr/DALA2024031103199.md): Skin · damaged · Mar 8, 2024 · N327NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3127 BURNED RIVET ON FR3 APPROX. 2" INCHES ABOVE STR 31. CORRECTIVE ACTION: DRILLED UP HOLE PER A319 SRM 53-11-11. INSTALLED PERMENANT FASTENER PER A319 SRM 53-11-11-300-034. (0235387)
- [SDR DALA2024031103198](https://openairdocs.org/sdr/DALA2024031103198.md): Skin · damaged · Mar 8, 2024 · N327NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3127 BURNED RIVET ON STR 31 BETWEEN FR4 AND FR5. CORRECTIVE ACTION: DRILLED UP HOLE PER A319 SRM 53-11-11. INSTALLED PERMANENT FASTENER PER A319 SRM 53-11-11-300-034. (0235386)
- [SDR DALA2024031103197](https://openairdocs.org/sdr/DALA2024031103197.md): Skin · damaged · Mar 8, 2024 · N327NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3127 FOUND BURN IN SKIN BETWEEN FR2 AND FR3 AND BETWEEN STR 32 AND 31. CORRECTIVE ACTION: DRILLED OUT DAMAGE PER A319 SRM 53-11-11. INSTALLED PERMENANT FASTENER PER A319 SRM 53-11-11-300-034. (0235380)
- [SDR DALA2024031103195](https://openairdocs.org/sdr/DALA2024031103195.md): Tat Probe · damaged · Mar 8, 2024 · N327NB · Airbus A319114 · Outside Air Temperature Indicator/Sensor
  > SHIP 3127 DURING LIGHTING STRIKE INSPECTION FOUND LT TAT PROBE DAMAGED. CORRECTIVE ACTION: R&R LT TAT PROBE PER A319 AMM 34-11-18. OK FOR CONT. SERVICE. (0235608)
- [SDR DALA2024012901309](https://openairdocs.org/sdr/DALA2024012901309.md): Cover · detached · Jan 26, 2024 · N327NB · Airbus A319114 · Emergency Exits
  > SHIP 3127 - ATO - AT 60 KTS DUE TO DOOR L EMER EXIT ECAM MESSAGE. CORRECTIVE ACTION: LEFT OVERWING EMERGENCY EXIT DOOR HANDLE COVER CAME OFF. REMOVED AND INSPECTED COVER AND RESET. NO DEFECTS NOTED. ALL INDICATIONS NORMAL.
- [SDR DALA2023120409921](https://openairdocs.org/sdr/DALA2023120409921.md): Unknown · unknown · Dec 4, 2023 · N327NB · Airbus A319114 · Localizer/VOR System
  > SHIP 3127 -DIV- TO IND DUE TO ILS TUNING ISSUE ON APPROACH TO DTW. FMGC RESET WAS NO HELP. CORRECTIVE ACTION: COULD NOT DUPLICATE. PERFORMED AFS LAND TEST, AIRCRAFT RTS. (5059882)
- [SDR DALA2023112709741](https://openairdocs.org/sdr/DALA2023112709741.md): Unknown · unknown · Nov 25, 2023 · N327NB · Airbus A319114 · Air Distribution System
  > SHIP 3127 DIRTY SOCK SMELL. CORRECTIVE ACTION: REPLACED BOTH RECIRC FILTERS REF A319 AMM 21-21. (0080347)
- [SDR DALA2023100908300](https://openairdocs.org/sdr/DALA2023100908300.md): Unknown · unknown · Oct 7, 2023 · N327NB · Airbus A319114 · Rudder Control System
  > SHIP 3127 BLUE SYS RUDDER SERVO HAS EXCESSIVE PLAY. CORRECTIVE ACTION: REMOVED BLUE SYS RUDDER SERVO PER A319 AMM 27-24-51. (0005175)
- [SDR DALA2023012600649](https://openairdocs.org/sdr/DALA2023012600649.md): Slide · unwanted deploy · Jan 24, 2023 · N327NB · Airbus A319114 · Escape Slide
  > 1L DOOR SLIDE DEPLOYED. SLIDE REPLACED PER AMDS 2561-4003-LF.
- [SDR DALA2022121308045](https://openairdocs.org/sdr/DALA2022121308045.md): Oxygen Mask · dislodged · Dec 12, 2022 · N327NB · Airbus A319114 · Passenger Oxygen System
  > O2 MASK SEATS 23AB AND C FELL FROM OVERHEAD. RESEATED PAX O2 MASKS INTO STORAGE BOX IAW MM 35-21.
- [SDR DALA2022110107065](https://openairdocs.org/sdr/DALA2022110107065.md): A/C Pack · odor · Oct 31, 2022 · N327NB · Airbus A319114 · Air Conditioning System
  > SHIP 3127 - SOCK ODOR VERY STRONG AFTER APU START AND APU BLEED AIR/PACKS ON IN COCKPIT. CORRECTIVE ACTION: PERFORMED PACK BURNOUT AND REPLACED CABIN FILTERS. 9387296)
- [SDR DALA2022092306257](https://openairdocs.org/sdr/DALA2022092306257.md): None · none · Sep 23, 2022 · N327NB · Airbus A319114 · Landing Gear Brake System
  > SHIP 3127 - MISC/DE - DUE TO RT ALTERNATE BRAKE PRESSURE ON TRIPLE INDICATOR STUCK AT 2000PSI ENTIRE FLIGHT. LEFT WAS AT 0. CORRECTIVE ACTION: REPLACED RT ALTERNATE BRAKE PRESSURE TRANSDUCER 62GG. (8653352)
- [SDR DALA2022081905625](https://openairdocs.org/sdr/DALA2022081905625.md): None · none · Aug 19, 2022 · N327NB · Airbus A319114 · Passenger Oxygen System
  > SHIP 3127 - PAX O2 MASKS ROW 28-DEF FELL DOWN. CORRECTIVE ACTION: RESECURE DOOR, MASK AND GENERATOR STILL GOOD. PER A319 AMM 25-26. (9207528)
- [SDR DALA2022081605566](https://openairdocs.org/sdr/DALA2022081605566.md): Door · jammed · Aug 13, 2022 · N327NB · Airbus A319114 · Passenger Oxygen System
  > SHIP 3127 - DURING PSU OXYGEN PNL ACTUATION CHECK FOUND 2L F/A SEAT PSU O2 CONTAINER DOOR FAILED TO OPEN. CORRECTIVE ACTION: R/R FLIGHT ATT. O2 MODULE AT DOOR 2L PER A320 AMM 35-21. (9207503)
- [SDR DALA2022083005815](https://openairdocs.org/sdr/DALA2022083005815.md): None · none · Aug 3, 2022 · N327NB · Airbus A319114 · Landing Gear Actuator
  > SHIP 3127 - RIGHT MLG RETRACT ACTUATOR ANCHORAGE FITTING HAS CORROSION IN THE BORE AND ON THE UPPER AND LOWER BEARING FACES. CORRECTIVE ACTION: REPAI RED LUG REF. PRI 601200-14 REV. 0 AND ERA 601200-14 REV. ORIGINAL, AND A319 SRM 57-26-13. (2348976)
- [SDR DALA2022083005814](https://openairdocs.org/sdr/DALA2022083005814.md): None · none · Aug 3, 2022 · N327NB · Airbus A319114 · Wing, Attach Fittings
  > SHIP 3127 - CORROSION FINDING TO RH WING MLG ANCHORAGE FITTING. CORRECTIVE ACTION: REPAIR IS LIMITED TO THE LESSER OF 80300 TOTAL FLIGHT CYCLES OR 160600 TOTAL FLIGHT HOURS. (2348198)
- [SDR DALA2022042502906](https://openairdocs.org/sdr/DALA2022042502906.md): Mask · activated · Apr 21, 2022 · N327NB · Airbus A319114 · Passenger Oxygen System
  > SHIP 3127 - ROW 25 DEF OXYGEN MAKS DROPPED IN FLIGHT. CORRECTIVE ACTION: REPACKED MASKS AT 25DEF A319 AMM 35-21.(8736792)
- [SDR DALA2022040402271](https://openairdocs.org/sdr/DALA2022040402271.md): None · none · Apr 1, 2022 · N327NB · Airbus A319114 · Door Warning System
  > SHIP 3127 - SLIDE DOOR INDICATION 2R DOES NOT SHOW ARMED AT CRUISE. HANDLE WILL NOT STAY FLUSH. CORRECTIVE ACTION: REMOVED & REINSTALLED SAME SLIDE PER AMDS WORK CARD 2561.(8592386)
- [SDR DALA2022032301884](https://openairdocs.org/sdr/DALA2022032301884.md): None · none · Mar 22, 2022 · N327NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3127 - DOOR 2R KEEPS DISARMING DURING FLIGHT. HAD REARM TWICE DURING CRUISE. CORRECTIVE ACTION: REPLACE PROX SWITCH 17WV2. (8592346)
- [SDR DALA2022032201870](https://openairdocs.org/sdr/DALA2022032201870.md): Not Reported · not reported · Mar 21, 2022 · N327NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3127 - DOOR 2R SLIDE WILL NOT STAY ARMED IN FLIGHT. CORRECTIVE ACTION: CLEANED GIRT BAR AND GIRT BAR LOCKING SYSTEM. DOOR ARMING SYSTEM AT2R OPERATES NORMAL. (8592344)
- [SDR DALA2022020900859](https://openairdocs.org/sdr/DALA2022020900859.md): None · none · Feb 9, 2022 · N327NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3127 - CABIN DOOR 2R ARMS NORMALLY ON THE GROUND BUT BECOMES DISARMED WHEN AIRBORNE. CORRECTIVE ACTION: OPENED & CLOSED 2R DOOR OPERATES NORMALLY ARMED & DISARMED NUMEROUS TIMES NO FAULTS, NO HISTORY,GIRT BAR AREA CLEAN. OK FOR SERVICE. (7747594)
- [SDR DALA2022012600530](https://openairdocs.org/sdr/DALA2022012600530.md): None · none · Jan 25, 2022 · N327NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3127 - CRACK INDICATION FOUND IN OPEN HOLE 1, ON FRAME 20 LH AND DOOR STOP FITTING 7 AREA. CORRECTIVE ACTION: COMPLIED WITH PRI 596570-14AD REV 0 AND REV 1. VALIDATED ER/A 596570-14AD REV. ORIGINAL (2098008)
- [SDR DALA2022012600529](https://openairdocs.org/sdr/DALA2022012600529.md): None · none · Jan 24, 2022 · N327NB · Airbus A319114 · Fuselage, Door Hinge
  > SHIP 3127 - CRACK INDICATION ON MLG DOOR KEEL BEAM HINGE FITTING. CORRECTIVE ACTION: COMPLIED WITH PRI #551093-14AD REV.0 AND REV.1, VALIDATED ER/A #551093-14AD REV.C (2097575)
- [SDR DALA2022012400494](https://openairdocs.org/sdr/DALA2022012400494.md): None · none · Jan 23, 2022 · N327NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3127 - CRACK INDICATION FOUND IN OPEN HOLE 3, ON FRAME 16 RH, AND DOOR STOP FITTING 7 AREA. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON FRAME 16 RH, AND DOOR STOP FITTING 7 AREA AS PER ER/A 596568. (2096393)

Next page: https://openairdocs.org/aircraft/N327NB/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 = 'N327NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N327NB/reports

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