# Service difficulty reports: N363NB

A list on [N363NB](https://openairdocs.org/aircraft/N363NB.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 · 129 reports

- [SDR DALA2026032602016](https://openairdocs.org/sdr/DALA2026032602016.md): Apu · odor · Mar 25, 2026 · N363NB · Airbus A319114 · APU Core Engine
  > RAN APU WITHOUT BLEED FOR 8 MINUTES BEFORE TURNING ON BLEED WHEN BLEED TURNED ON DIRTY SOCKS SMELL STARTED, RAN WITH BLEED FOR ABOUT 1 MINUTE AND THE SMELL GOT STRONGER, TURNED BLEED OFF SMELL WENT AWAY. FLIGHT ATTENDANTS DID NOT SMELL IT BUT BOARDING DOOR WAS
- [SDR DALA2025120908968](https://openairdocs.org/sdr/DALA2025120908968.md): Light · detached · Dec 8, 2025 · N363NB · Airbus A319114 · Emergency Lighting
  > SEAT 16D FLOOR LIGHTING DETACHED FROM SEAT. RE-ATTACHED TRIM PER A319 AMM 33-52. A/C OK FOR SVC. (7935918).
- [SDR DALA2025112408541](https://openairdocs.org/sdr/DALA2025112408541.md): Door Frame · cracked · Nov 21, 2025 · N363NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION FOUND AT HOLE 6 LOC. FR 16RH DOUBLE JOGGLE AREA. REPAIRED PER ERA 629916-14AD REV ORIGINAL. (1314847)
- [SDR DALA2025112408537](https://openairdocs.org/sdr/DALA2025112408537.md): Fitting · cracked · Nov 21, 2025 · N363NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON RH CONTINUITY FITTING OF THE WINDSHIELD LOWER ATTACHMENT AREA INTERNAL. REPAIRED PER ERA 629854-14AD REV ORIGINAL. (1315086)
- [SDR DALA2025112108508](https://openairdocs.org/sdr/DALA2025112108508.md): Stringer · corroded · Nov 21, 2025 · N363NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 43L AT LEVEL FR55 IN AFT CARGO COMPARTMENT (SSI 53 4107). CORRECTIVE ACTION: REPAIRED PER ERA 630525-14 REV ORIGINAL. (1314257)
- [SDR DALA2025112108510](https://openairdocs.org/sdr/DALA2025112108510.md): Hinge Fitting · worn · Nov 20, 2025 · N363NB · Airbus A319114 · Fuselage, Door Hinge
  > WEAR ON FWD KEEL BEAM HINGE FITTING RH MLG DOOR. COMPLIED WITH ER/A 630159-14AD REV. ORIGINAL. (1313581)
- [SDR DALA2025112108509](https://openairdocs.org/sdr/DALA2025112108509.md): Hinge Fitting · worn · Nov 20, 2025 · N363NB · Airbus A319114 · Fuselage, Door Hinge
  > WEAR ON FWD KEEL BEAM HINGE FITTING LH MLG DOOR. REPAIRED PER ERA 630160-14AD REV. ORIGINAL. (1313575)
- [SDR DALA2025112108511](https://openairdocs.org/sdr/DALA2025112108511.md): Hinge Fitting · worn · Nov 19, 2025 · N363NB · Airbus A319114 · Fuselage, Door Hinge
  > WEAR WAS FOUND ON THE RH MLG DOOR FWD HINGE FITTING AT THE FWD LUG, FWD FACE AND THE FLANGED BUSHING WAS FOUND DAMAGED. REPAIRED PER ERA 630159-14. (1311751)
- [SDR DALA2025112008485](https://openairdocs.org/sdr/DALA2025112008485.md): Bushing · damaged · Nov 19, 2025 · N363NB · Airbus A319114 · Fuselage, Door Hinge
  > MULTIPLE DAMAGES FOUND ON LT MLG DOOR FWD HINGE FITTING LUG FACE, LUG BOR E AND FLANGED BUSHING. REPAIRED PER ER/A 630160-14. (1311665)
- [SDR DALA2025112008484](https://openairdocs.org/sdr/DALA2025112008484.md): Door Frame · cracked · Nov 19, 2025 · N363NB · Airbus A319114 · Fuselage Main, Frame
  > CRACK INDICATION WAS FOUND IN HOLE NR 6 OF FR16 RT DOUBLE JOGGLE AREA. COMPLIED WITH ER/A 629916-14AD. (1312243).
- [SDR DALA2025111908458](https://openairdocs.org/sdr/DALA2025111908458.md): Skin · dented · Nov 18, 2025 · N363NB · Airbus A319114 · Wing, Plate/Skin
  > DENT WAS FOUND ON LH WING PANEL 2 UPPER SURFACE AT RIB 22 AND STR 16LH. COMPLIED WITH ER/A 629925-14. (1310683).
- [SDR DALA2025111808408](https://openairdocs.org/sdr/DALA2025111808408.md): Elec Connector · worn · Nov 16, 2025 · N363NB · Airbus A319114 · Flight Control System Wiring
  > WEAR ELECTRICAL CONNECTOR RECEPTACLES (2 EA) (FIN 7543VC AND 7541VC) A ND PROXIMITY SENSOR CONNECTORS (2 EA) (FIN 37CV AND 39CV) ON INTERCONNECTING STRUT I/B FLAP LH WING. CORRECTIVE ACTION: R/R ELECTRICAL CONNECTOR RECEPTACLES (2 EA) (FIN 7543VC AND 7541VC) A
- [SDR DALA2025111908457](https://openairdocs.org/sdr/DALA2025111908457.md): Elec Connector · corroded · Nov 15, 2025 · N363NB · Airbus A319114 · Hydraulic Power System Wiring
  > CORROSION ON ELECTRICAL CONNECTORS UPPER AREA RAT (2EA). R & R ACTUATOR RAT AS PER A320 FAM AMM 29-22-53-000-10-A AND AMM 29-22-53-400-010-A. R/R ELECTRICAL CONNECTORS (1GEC) AND (1GEE) AS PER A320 FAM AWM 29-22-03 AND AS PER AIRBUS ESPM 20-44-11 AND AS PER
- [SDR DALA2025111808407](https://openairdocs.org/sdr/DALA2025111808407.md): Bottle · leaking · Nov 14, 2025 · N363NB · Airbus A319114 · Passenger/Crew Doors
  > LEAK WAS FOUND ON EMERGENCY DOOR DAMPER AT PASSENGER CREW DOOR 832. R & R DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGERCREW DOOR 832 IAW FAM AMM 52-13-14-000-001-B AND IAW FAM AMM 52-13-14-400-001-B. (1304671).
- [SDR DALA2025111308320](https://openairdocs.org/sdr/DALA2025111308320.md): Strap · cracked · Nov 12, 2025 · N363NB · Airbus A319114 · Elevator Structure
  > CRACK STRAP ASSY ELEVATOR HINGE ARM 1 ON LT HORIZONTAL STABILIZER. REPLACED STRAP ASSY ELEVATOR HINGE ARM 1 ON LT HORIZONTAL STABILIZER AND FASTENERS AS PER SRM-51-42-11 AND AS PER SRM-51-72-11. (1301316).
- [SDR DALA2025111308319](https://openairdocs.org/sdr/DALA2025111308319.md): Strap · cracked · Nov 12, 2025 · N363NB · Airbus A319114 · Elevator Structure
  > CRACK STRAP ASSY ELEVATOR HINGE ARM 4 ON RH HORIZONTAL STABILIZER. REPLACED STRAP ASSY AND FASTENERS ELEVATOR HINGE ARM 4 ON RH HORIZONTAL STABILIZER AS PER A319 SRM 51-42-11 AND SRM: 51-72-11. (1301375).
- [SDR DALA2025111308318](https://openairdocs.org/sdr/DALA2025111308318.md): Stringer · corroded · Nov 12, 2025 · N363NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 38R LOCATED BTW FR 59 TO FR 60 IN AFT CARGO COMPARTMENT. REPLACED STRINGER 38R LOCATED BTW FR 59 TO FR 60 IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1301361).
- [SDR DALA2025111308317](https://openairdocs.org/sdr/DALA2025111308317.md): Strap · cracked · Nov 12, 2025 · N363NB · Airbus A319114 · Elevator Structure
  > CRACK STRAP ASSY ELEVATOR HINGE ARM 2 ON LH HORIZONTAL STABILIZER. REPLACED STRAP ASSY ELEVATOR HINGE ARM 2 ON LH HORIZONTAL STABILIZER AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1301350).
- [SDR DALA2025111308316](https://openairdocs.org/sdr/DALA2025111308316.md): Web · cracked · Nov 12, 2025 · N363NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CRACK WEB LOCATED FLOOR STRUCTURE FROM FR68 TO FR69 AND STR23RH AT AF T GALLEY AREA. REPLACED WEB LOCATED FLOOR STRUCTURE FROM FR68 TO FR69 AND STR23RH AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND AS PER A319 SRM 51-72-11. (1301335).
- [SDR DALA2025111308315](https://openairdocs.org/sdr/DALA2025111308315.md): Stringer · corroded · Nov 12, 2025 · N363NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 42R AT LEVEL FR60 IN AFT CARGO COMPARTMENT. REPLACED STRINGER 42R AT LEVEL FR60 IN AFT CARGO COMPARTMENT AS PER SRM 51-42-11. (1301326).
- [SDR DALA2025111108231](https://openairdocs.org/sdr/DALA2025111108231.md): Dampener · no test · Nov 10, 2025 · N363NB · Airbus A319114 · Passenger/Crew Doors
  > DONT PASS OPERATIONAL TEST EMERGENCY DOOR DAMPER ON PASSENGER CREW DOOR 832. REMOVED UNSERVICEABLE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER CREW DOOR 832 AS PER A320 FAM AMM 52-13-14-000-001-B. (1297664).
- [SDR DALA2025111108230](https://openairdocs.org/sdr/DALA2025111108230.md): Bushing · excess play · Nov 10, 2025 · N363NB · Airbus A319114 · Passenger/Crew Doors
  > EXCESSIVE PLAY AT BUSHINGS BTW UPPER LINK, LOWER LINK AND SUPPORT ARM (8EA) PASSENENGER CREW DOOR 832. REPLACED BONDED BUSHES UPPER, LOWER LINK AND SUPPORT ARM (8EA)AT PASSENGER CREW DOOR 832 AS PER A320 FAM AMM 52-13-21-000-001-A, AS PER A320 FAM AMM 52-10-
- [SDR DALA2025111108225](https://openairdocs.org/sdr/DALA2025111108225.md): Shear Tie · mechanic error · Nov 10, 2025 · N363NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > MISDRILLED HOLE INTERNAL STRUCTURE ON SHEAR TIE FR29 AND FR30 STR41 TO STR42 LH SIDE IN FWD CARGO COMPARTMENT. REPLACED SHEAR TIE FR29 AND FR30 STR41 TO STR42 LH SIDE IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1297363).
- [SDR DALA2025111008190](https://openairdocs.org/sdr/DALA2025111008190.md): Stop Pad · worn · Nov 7, 2025 · N363NB · Airbus A319114 · Passenger/Crew Doors
  > WEAR ON DOOR STOP PAD PASSENGER CREW DOOR IN PASSENGER CABIN 841 FWD POSITION 1-2-3 AND AFT POSITION 2-3-4-5-6. REPLACED DOOR STOP PAD PASSENGER CREW DOOR IN PASSENGER CABIN 841 FWD POSITION 1-2-3 AND AFT POSITION 2-3-4-5-6 AS PER A320 FAM AMM 52-11-31-000-0
- [SDR DALA2025111008189](https://openairdocs.org/sdr/DALA2025111008189.md): Stop Fitting · worn · Nov 7, 2025 · N363NB · Airbus A319114 · Passenger/Crew Doors
  > WEAR ON DOOR STOP PAD OF FWD PASSENGER CREW DOORS 831 FWD POSITION 1-4-5-6 AND AFT POSITION 2-3-6 PASSENGER CABIN. REPLACED DOOR STOP PAD OF FWD PASSENGER CREW DOORS 831 FWD POSITION 1-4-5-6 AND AFT POSITION 2-3-6 PASSENGER CABIN AS PER FAM AMM 52-11-31-000-
- [SDR DALA2025110708127](https://openairdocs.org/sdr/DALA2025110708127.md): Skin · damaged · Nov 6, 2025 · N363NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3163 NICK ON EXTERNAL SKIN LOCATED FR27 PLUS 8.5 INCHES BETWEEN STR41RH AN D STR42RH AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED PER A319 SRM 53-21-11-283-018. (1291822)
- [SDR DALA2025110708124](https://openairdocs.org/sdr/DALA2025110708124.md): Roller · deteriorated · Nov 6, 2025 · N363NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3163 DETERIORATED ROLLERS FWD, AFT, UPPER AND LOWER POSITION (4EA) AT PASSENGER CREW DOOR 832. CORRECTIVE ACTION: REPLACED ROLLER FITTINGS FWD, AFT, UPPER AND LOWER POSITION (4EA). AT PASSENGER CREW DOOR 832. AS PER A320 FAM AMM 52-13-31-000- 002-A AND AM
- [SDR DALA2025110708123](https://openairdocs.org/sdr/DALA2025110708123.md): Roller · deteriorated · Nov 6, 2025 · N363NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3163 DETERIORATED ROLLERS FWD, AFT, UPPER AND LOWER POSITION (4EA) AT PASSENGER CREW DOOR 841. CORRECTIVE ACTION: REPLACED ROLLERS FWD, AFT, UPPER AND LOWER POSITION (4EA) AT PASSENGER CREW DOOR 841 AS PER A320 FAM AMM 52-11-31-000-002-A AND AS PER A320 F
- [SDR DALA2025110708122](https://openairdocs.org/sdr/DALA2025110708122.md): Roller · deteriorated · Nov 6, 2025 · N363NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3163 DETERIORATED ROLLERS FWD, AFT, UPPER AND LOWER POSITION (4EA) AT PASSENGER CREW DOOR 831. CORRECTIVE ACTION: REPLACED ROLLERS FWD, AFT, UPPER AND LOWER POSITION (4EA) AT PASSENGER CREW DOOR 831 AS PER A320 FAM AMM 52-11-31-000-002-A AND AS PER A320 F
- [SDR DALA2025110708119](https://openairdocs.org/sdr/DALA2025110708119.md): Skin · dented · Nov 6, 2025 · N363NB · Airbus A319114 · Leading Edge Devices
  > SHIP 3163 DENTS ON SLAT 1 EXTERNAL SKIN ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS LOC ON SLAT 1 NOSE PART OF TOP SKIN, TRACK RIB6 PLUS 2.895 INCH RH WING AS PER A319 SRM 57-40- 00-300-10. (1291855).
- [SDR DALA2025110708118](https://openairdocs.org/sdr/DALA2025110708118.md): Clamp · worn · Nov 6, 2025 · N363NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3163 WEAR ON CLAMP TRUNNION IB FLAP ON LH WING. CORRECTIVE ACTION: R/R CLAMP TRUNNION IB FLAP ON LH WING AS PER AIRBUS CMM 57- 52-21 SUBTASK 57-52-21-350-008-A01. (1291884).
- [SDR DALA2025110708117](https://openairdocs.org/sdr/DALA2025110708117.md): Seat Track · corroded · Nov 6, 2025 · N363NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3163 CORROSION FLOOR STRUCTURE SEAT TRACK LOCATED AT FR 66 -Y 765 AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE SEAT TRACK LOCATED AT FR 66 -Y 765 AFT GALLEY AREA AS PER A319 SRM 51-42-11 A319 AND SRM 51-72-11. (1291865).
- [SDR DALA2025110708116](https://openairdocs.org/sdr/DALA2025110708116.md): Seat Track · corroded · Nov 6, 2025 · N363NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3163 CORROSION FLOOR STRUCTURE SEAT TRACK LOCATED AT FR 66 -Y 1292 AFT GALLEY AREA. CORRECTIVE ACTION: R/R FLOOR STRUCTURE SEAT TRACK -Y 1262 LOCATED AT FR 64 TO FR 66 AFT GALLEY AREA AS PER A319 SRM 51-42-11 A319 SRM 51-72-11. (1291858).
- [SDR DALA2025110708115](https://openairdocs.org/sdr/DALA2025110708115.md): Seat Track · corroded · Nov 6, 2025 · N363NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3163 CORROSION FLOOR BEAM +Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM Y1162.5 AND FASTENERS LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND SRM-51-46-11- 801. (1291712).
- [SDR DALA2025110708114](https://openairdocs.org/sdr/DALA2025110708114.md): Seat Track · corroded · Nov 6, 2025 · N363NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3163 CORROSION FLOOR STRUCTURE BEAM LOCATED AT FR 20 AND -Y1292 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM (SEAT TRACK) -Y1292, AND FASTENERS LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (12916
- [SDR DALA2025110708113](https://openairdocs.org/sdr/DALA2025110708113.md): Floorbeam · corroded · Nov 6, 2025 · N363NB · Airbus A319114 · Fuselage Main, Floor Beam
  > SHIP 3163 CORROSION FLOOR STRUCTURE BEAM LOCATED AT FR 16 HARD POINT Y 1292 FWD GALLEY AREA. CORRECTIVE ACTION: R/R FLOOR BEAM (SEAT TRACK) LOCATED AT FR 16 HARD POINT Y 1292 FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1291488).
- [SDR DALA2025110708112](https://openairdocs.org/sdr/DALA2025110708112.md): Web · corroded · Nov 6, 2025 · N363NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3163 CORROSION WEB LOCATED FLOOR STRUCTURE FR20 AND STR23RH AT FWD GALLEY AREA. CORRECTIVE ACTION: R/R WEB LOC BTW FR 20 TO FR 24 AND STR 23R AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1291461).
- [SDR DALA2025111008203](https://openairdocs.org/sdr/DALA2025111008203.md): Receptacle · corroded · Nov 5, 2025 · N363NB · Airbus A319114 · Light System Wiring
  > SHIP 3163 CORROSION ON ELECTRICAL RECEPTACLE POWER SUPPLY UNIT (18LV) IN THS COM PARTMENT. REPLACED POWER SUPPLY UNIT (18LV) AS PER AIRBUS ESPM 20-52-11. (1288749).
- [SDR DALA2025110408042](https://openairdocs.org/sdr/DALA2025110408042.md): Indicator · corroded · Nov 3, 2025 · N363NB · Airbus A319114 · Indicating/Recording System
  > CORROSION BASE RESERVOIR INDICATOR LOCATED BTW FR47/51 TO FR52 LH SID E AT LOWER FUSELAGE. REMOVED THE QUANTITY INDICATOR AS PER A320 FAM AMM 29-31-21-000-001-A. (1286334).
- [SDR DALA2025110408040](https://openairdocs.org/sdr/DALA2025110408040.md): Dummy Rail · corroded · Nov 3, 2025 · N363NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FLOOR STRUCTURE RAIL DUMMY LOCATED BTW FR 12 TO FR 16 AND Y 503.2 FWD GALLEY AREA. REPLACED FLOOR STRUCTURE RAIL DUMMY LOCATED BTW FR 12 TO FR 16 AND Y 503.2 FWD GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM51 -72-11. (1286505).
- [SDR DALA2025110308007](https://openairdocs.org/sdr/DALA2025110308007.md): Door Frame · cracked · Nov 2, 2025 · N363NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION FOUND IN HOLE 1 OF THE DOOR STOP FITTING 7 AT FRAME 1 6 RH SIDE. REPLACED INTERCOSTAL AND FASTENERS LOCATED AT LEVEL DOOR STOP FITTING 7 AT FR 15 TO FR16 RH SIDE AND FASTENERS AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1283977).
- [SDR DALA2025110308006](https://openairdocs.org/sdr/DALA2025110308006.md): Stop Fitting · cracked · Nov 2, 2025 · N363NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION FOUND IN HOLE 1 OF THE DOOR STOP FITTING 7 AT FRAME 1 6 LH SIDE. REPLACED INTERCOSTAL AND FASTENERS FASTENERS AS PER A319 SRM 51- 42-11 AND A319 SRM 51-72-11. (1283974).
- [SDR DALA2025110308008](https://openairdocs.org/sdr/DALA2025110308008.md): Stop Pad · worn · Oct 31, 2025 · N363NB · Airbus A319114 · Passenger/Crew Doors
  > WEAR ON PASSENGER CREW DOOR 842 STOP PAD FWD POSITION 2 - 4 AND A FT POSITION 1 - 2 - 4 IN PASSENGER CABIN. REPLACED PASSENGER CREW DOOR 842 STOP PAD FWD POSITION 2-4 AND AFT POSITION 1-2-4 IN PASSENGER CABIN (5 EA) AS PER A320 FAM AMM 52-13-31-000-002-A AND
- [SDR DALA2025110308003](https://openairdocs.org/sdr/DALA2025110308003.md): Plate · cracked · Oct 31, 2025 · N363NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CRACK INTERNAL STRUCTURE PLATE LOCATED BTW FR 68 TO FR 69 AND LEVEL S TR 23L AT AFT GALLEY AREA. REPLACED PLATE AND FASTENERS LOCATED BTW FR 68 TO FR 69 AND LEVEL STR 23L AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1282414).
- [SDR DALA2025110308001](https://openairdocs.org/sdr/DALA2025110308001.md): Floorbeam · corroded · Oct 31, 2025 · N363NB · Airbus A319114 · Fuselage Main, Floor Beam
  > CORROSION FLOOR STRUCTURE BEAM LOCATED AT FR 20 AND -Y 765 FWD GALLE Y AREA. REPLACED FLOOR BEAM -Y 765 AND FASTENERS AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1281862).
- [SDR DALA2025103107989](https://openairdocs.org/sdr/DALA2025103107989.md): Bushing · worn · Oct 30, 2025 · N363NB · Airbus A319114 · Elevator Structure
  > WEAR FIXED BUSHING ON HINGE FITTING 1 ON LH ELEVATOR (2 EA). CORRECTIVE ACTION: REPAIRED O/B LUG AND REPLACED BUSHING ON I/B LUG ON HINGE FITTING #1 AT LH ELEVATOR AS PER AIRBUS CMM 55-21-15 AND A319 SRM 55-26-41-300-004. (1280842)
- [SDR DALA2025103107988](https://openairdocs.org/sdr/DALA2025103107988.md): Floor Support · corroded · Oct 30, 2025 · N363NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR BEAM -Y765 LOCATED AT FR 68 AT AFT GALLEY AREA. REPLACED FLOOR BEAM -Y765 AND FASTENERS LOCATED AT FR 66 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1280818)
- [SDR DALA2025103107987](https://openairdocs.org/sdr/DALA2025103107987.md): Floor Support · corroded · Oct 30, 2025 · N363NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR BEAM -Y1292 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA. REPLACED FLOOR BEAM -Y1292 AND FASTENERS LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11. (1280804)
- [SDR DALA2025103107986](https://openairdocs.org/sdr/DALA2025103107986.md): Floor Support · corroded · Oct 30, 2025 · N363NB · Airbus A319114 · Fuselage Floor Panel
  > CORROSION FLOOR BEAM -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLE Y AREA. REPLACED FLOOR BEAM -Y1162.5 AND FASTENERS LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11. (1280788)
- [SDR DALA2025103107985](https://openairdocs.org/sdr/DALA2025103107985.md): Shear Plate · corroded · Oct 30, 2025 · N363NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION SHEAR PLATE STR 23 R FROM FR69 TO FR70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE LOC STR 23 R FROM FR69 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (1280779)

Next page: https://openairdocs.org/aircraft/N363NB/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 = 'N363NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N363NB/reports

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