# Service difficulty reports: N365NB

A list on [N365NB](https://openairdocs.org/aircraft/N365NB.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 · 132 reports

- [SDR DALA2026050102754](https://openairdocs.org/sdr/DALA2026050102754.md): Display · faulted · Apr 28, 2026 · N365NB · Airbus A319114 · Central Display
  > ATO - AT APPROXIMATELY 22 KNOTS DUE TO LOSS OF CAPTAINS PFD. MAINTENANCE IN PROGRESS. (LP: 7794686). AIRCRAFT WAS GROUNDED
- [SDR DALA2026040402153](https://openairdocs.org/sdr/DALA2026040402153.md): Not Reported · not reported · Mar 29, 2026 · N365NB · Airbus A319114 · Standard Practices/Structures
  > PERFORM ER/A 632197-14 FOR GAIN ACCESS TO REPLACEMENT CONTINUITY FITTINGS LT & RT. COMPLIED WITH ER/A 632197-14 REV ORIGINAL MATCHES WITH ALL STEPS OF ER/A 632197-14 PRI REV 0 IT IS BEEN VALIDATED, PERFORMED REPAIR INSTRUCTIONS FOR GAIN ACCESS TO REPLACEMENT
- [SDR DALA2026033002090](https://openairdocs.org/sdr/DALA2026033002090.md): Window Frame · cracked · Mar 29, 2026 · N365NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON WINDOW FRAME NR 2, LOWER NODE ATTACHMENT AREA CONTINUITY FITTING LT SIDE, CRACK LENGTH IS 0.200. CRACK DIRECTION IS VERTICAL. COMPLIED WITH ER/A 632268-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF ER/A 632268-14AD PRI REV 0 AND REV 1, PE
- [SDR DALA2026033002087](https://openairdocs.org/sdr/DALA2026033002087.md): Window Frame · cracked · Mar 29, 2026 · N365NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION ON FRAME 2 OF WINDSHIELD CENTER POST LOWER NODE, ATTACHME NT POCKET LT SIDE, INBD FLANGE, FROM UPPER TENSION BOLT, CRACK LENG TH IS 0.120, CRACK DIRECTION IS 2 OCLOCK. AD 2020-17-03 / WORKC ARD 5311-01226-01. COMPLIED WITH ER/A 632195-14AD,
- [SDR DALA2026033002086](https://openairdocs.org/sdr/DALA2026033002086.md): Floor Support · corroded · Mar 27, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORRODED FLOOR SUPPORT, +Y765, BTW FR 66 & FR 70 IN AFT GALLEY AREA. INSTALLED SPLICES ON FR 66 IAW SRM 51-42-11, AND DWG D53472816, ISSUE A. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-42-11, SRM 51-72-11, & DWG D53472816, ISSUE A. TOOK MEASURE
- [SDR DALA2026033002085](https://openairdocs.org/sdr/DALA2026033002085.md): Floor Support · corroded · Mar 27, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORRODED FLOOR SUPPORT +Y1162.5 LOCATED BTW FR 69 & FR 70 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-42-11, SRM 51-72-11, & DWG D53472780, TOOK MEASUREMENT OF CORROSION: L=1.014 IN, W= 0.840 IN, D= 0.044 IN, (LP: 1515362)
- [SDR DALA2026032602015](https://openairdocs.org/sdr/DALA2026032602015.md): Plate · corroded · Mar 24, 2026 · N365NB · Airbus A319114 · Wing, Plate/Skin
  > CORROSION LOWER SURFACE EXTERNAL SKIN REINFORCING PLATE LOCATED AT LEVEL RIB 8 ON RH WING. C/A: COMPLIED WITH ER/A 632291-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF PRI 632291-14AD REV 0 AND REV 1 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON BOTTOM
- [SDR DALA2026032602008](https://openairdocs.org/sdr/DALA2026032602008.md): Fitting · not reported · Mar 23, 2026 · N365NB · Airbus A319114 · Standard Practices/Structures
  > DTE ERA 632268-14AD REV. ORIGINAL. REPLACEMENT OF CONTINUITY FITTING IS TIME LIMITED, REQUIRING DTE FOLLOW UP PRIOR TO 61,196 TFC. REVISE AND UPDATE ERA 632268-14AD WITH DTE RESULTS PRIOR TO 61,196 TFC. REFERENCE AIRBUS DOSSIER 81739836. ASSOCIATED AA 5311-01
- [SDR DALA2026032602007](https://openairdocs.org/sdr/DALA2026032602007.md): Fitting · not reported · Mar 23, 2026 · N365NB · Airbus A319114 · Standard Practices/Structures
  > TE ERA 632195-14AD REV ORIGINAL. REPAIR AT MIRROR FITTINGS, AREA 3 IS TIME LIMITED, REQUIRING DTE FOLLOW UP PRIOR TO 91,696 TFC. REVISE AND UPDATE ERA 632195-14AD WITH DTE RESULTS, PRIOR TO 91,696 TFC. ASSOCIATED AA 5311-01226 ADDED FOR AC 3165 ASSOCIATED ER/
- [SDR DALA2026032602006](https://openairdocs.org/sdr/DALA2026032602006.md): Not Reported · not reported · Mar 23, 2026 · N365NB · Airbus A319114 · Standard Practices/Structures
  > INSPECTION ERA 632195-14AD REV. ORIGINAL. REPAIR OF WINDSHIELD FRAMING AREA 2 REQUIRES FOLLOW-ON INSPECTIONS PRIOR TO 58,696 TFC AND EVERY 4,700 FC, THEREAFTER. ACCOMPLISH FOLLOW-ON INSPECTIONS PER ERA 632195-14AD SECTION II PRIOR TO 58,696 TFC AND EVERY 4,70
- [SDR DALA2026032201925](https://openairdocs.org/sdr/DALA2026032201925.md): Shear Plate · corroded · Mar 21, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION SHEAR PLATE LOCATED BTW FR 69 TO FR 70 AT LEVEL STR 23L AT AFT GALLEY AREA. C/A: REPLACED SHEAR PLATE, AND FASTENERS LOC BTW FR69TO FR70 STR 23L AFT GALLEY AREA AS PER A319 SRM 51-72-11, SRM 51-42-11 AND DWG: D53474180 ISSUE: AA RELEASE DATE: 09/SEP/
- [SDR DALA2026032201924](https://openairdocs.org/sdr/DALA2026032201924.md): Floor Support · corroded · Mar 21, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE ON FRAME WEB LOC BTW FR69 TO FR70 STR23RH SIDE IN PASSENGER CABIN. C/A: REPLACED FRAME WEB, AND FASTENERS LOC BTW FR69 TO FR70 STR 23 RH SIDE IN PASSENGER CABIN AS PER A319 SRM 51-72-11, SRM 51-42-11 AND DWG: D53474180 ISSUE: AA RELEA
- [SDR DALA2026032201923](https://openairdocs.org/sdr/DALA2026032201923.md): Floor Support · corroded · Mar 21, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR STRUCTURE ON FRAME WEB LOC BTW FR 69 - FR 70, STR 23L SIDE IN PASSENGER CABIN. REPLACED FRAME WEB, AND FASTENERS LOC BTW FR 69 TO FR 70 STR 23L, PASSENGER CABIN IAW SRM 51-72-11, SRM 51-42-11 AND DWG D53474180, ISSUE AA. MEASURES OF CORROSIO
- [SDR DALA2026032201922](https://openairdocs.org/sdr/DALA2026032201922.md): Shear Plate · corroded · Mar 21, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION SHEAR PLATE LOCATED BTW FR 69 TO FR 70 AT STR 23R, AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS LOC BTW FR 69 TO FR 70, STR 23R AFT GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11, AND DWG D53474180, ISSUE AA, MEASURES OF CORROSION ON SHEAR PLA
- [SDR DALA2026031101672](https://openairdocs.org/sdr/DALA2026031101672.md): Skin · misrepaired · Mar 10, 2026 · N365NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > DURING THE INSPECTION OF EXISTING MAJOR REPAIR AT LOWER FUSELAGE FR1 BL0 (INTERNAL SIDE) BETWEEN FR1 AND FR2 / LBL12 TO RBL 12. SEVERAL FASTENERS (3EA) ARE LOCATED IN THE CHEM MILLED RADIUS AREA THAT ARE NOT SPOT FACED. REFERENCE DELTA AIR LINES ER/A 548858-14
- [SDR DALA2026031101671](https://openairdocs.org/sdr/DALA2026031101671.md): Skin · misrepaired · Mar 10, 2026 · N365NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > DURING THE INSPECTION OF EXISTING MAJOR REPAIR AT LOWER FUSELAGE FR1 BL0 (INTERNAL SIDE). ONE FASTENER LOCATED 11 ROWS OUTBOARD (LEFT) OF THE FILLER CUTOUT AND 3 ROWS AFT OF FORWARD BULKHEAD IS SPOT FACED BUT DOES NOT MEET THE SRM REQUIREMENTS (EDGES ARE NOT B
- [SDR DALA2026030801583](https://openairdocs.org/sdr/DALA2026030801583.md): Floor Support · corroded · Mar 4, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT -Y1292 BTW FR 66 TO FR 68 AT AFT GAL LEY AREA (SSI 534147). C/A: REPLACED FLOOR SUPPORT -Y1292 LOCATED BTW FR66 TO FR68 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 DWG D53472172 RELEASE DATE:24/NOV/22 ISSUE: K, DWG
- [SDR DALA2026030801582](https://openairdocs.org/sdr/DALA2026030801582.md): Floor Support · corroded · Mar 4, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOORBEAM -Y765 LOCATED AT FR 68 AT AFT GALLEY AREA (SSI 5 34147). REPLACED FLOOR BEAM -Y765 AND FASTENERS LOCATED AT FR 67 TO FR 70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72- 11, DWG D53472816, DWG D53478309 AND DWG D53472093. TOO
- [SDR DALA2026030801581](https://openairdocs.org/sdr/DALA2026030801581.md): Seat Track · corroded · Mar 4, 2026 · N365NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3165 DISC: CORROSION SEAT TRACK -Y765 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 5 31189). C/A: REPLACED SEAT TRACK -Y765 LOCATED BTW FR12 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG D53112812, ISSUE: E00, RELEASE DATE: 08/JAN/
- [SDR DALA2026030801580](https://openairdocs.org/sdr/DALA2026030801580.md): Floorbeam · damaged · Mar 3, 2026 · N365NB · Airbus A319114 · Fuselage Main, Floor Beam
  > MISSING MATERIAL FLOOR BEAM LOCATED BTW FR 20 TO FR 21 AND - Y 250 AT FWD GALLEY AREA. REPLACED FLOOR BEAM -Y189 AND FASTENERS LOCATED BTW FR20 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWG D53111406 RELEASE DATE: 20/DEC/96 ISS
- [SDR DALA2026031901901](https://openairdocs.org/sdr/DALA2026031901901.md): Strut · corroded · Mar 2, 2026 · N365NB · Airbus A319114 · Trailing Edge Flaps
  > CORROSION ON INTERCONNECTING STRUTS LH. REMOVED INTERCONNECTING STRUTS L/H P/N:D5757032201100, S/N: 02370 ON UNSERVICEABLE CONDITION AS PER FAM AMM 27-51-44- 000-001-A EXCEPT STEP 3.D.(2). JOB IN PROGRESS. REPLACED INTERCONNECTING STRUT ON LH WING AS PER A320
- [SDR DALA2026031901896](https://openairdocs.org/sdr/DALA2026031901896.md): Strut · corroded · Mar 2, 2026 · N365NB · Airbus A319114 · Wing Main, Frame Structure
  > CORROSION ON INTERCONNECTING STRUTS RT. REMOVED INTERCONNECTING STRUTS IAW AMM 27-51-44- 000-001-A EXCEPT STEP 3.D.(2). REPLACED INTERCONNECTING STRUT IAW AMM 27 -51-44-000-001-A AND AMM 27-51-44-400-001-A,
- [SDR DALA2026030301461](https://openairdocs.org/sdr/DALA2026030301461.md): Seat Track · corroded · Mar 1, 2026 · N365NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK -Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK -Y1292 LOCATED BTW FR12 TO FR24 FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, DWG D53110984, DWG D53110920, DWG D53112812, AND DWG D53918124. TOOK MEASURE
- [SDR DALA2026022701382](https://openairdocs.org/sdr/DALA2026022701382.md): Floor Support · corroded · Feb 26, 2026 · N365NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR SUPPORT -Y1162.5 AND FASTENERS LOC FR68 TO FR 69 AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG: DWG D53472780 RELEASE DATE: 26/APR/
- [SDR DALA2026022701379](https://openairdocs.org/sdr/DALA2026022701379.md): Fitting · corroded · Feb 25, 2026 · N365NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001 AND AS PER A319 SRM 54-51-12-283-001 PARAGRAPH 2. FIGURE 001 SHEET 1 AND 2. FOUND BEYOND OUT MEASURED OF LIMITS TOOL USED CALIPER
- [SDR DALA2026022701377](https://openairdocs.org/sdr/DALA2026022701377.md): Dampener · no test · Feb 23, 2026 · N365NB · Airbus A319114 · Passenger/Crew Doors
  > AIRCRAFT 3165, DONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 841 DOOR DAMPER (REFER TO AMDS CARD 5210-7089-RF (RII)) AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 841 EMERGENCY DAMPER PN: FE240-004, SN: 3977 AS PER A320 FAM AMM 52-11-14-
- [SDR DALA2026010400046](https://openairdocs.org/sdr/DALA2026010400046.md): Apu Bay · contaminated · Jan 3, 2026 · N365NB · Airbus A319114 · APU Cowling/Containment
  > AFTER PARKING AT GATE 11 IN BDL FA REPORTS HAZY. SMOKE VISIBLE IN REAR OF CABIN. SMELL WAS REPORTED AS PLASTICY & CHEMICALLY. THIS OCCURED AFTER PARKING AT GATE 11. APU WAS STARTED MORE THAN 5 MINS BEFORE APU BLEED WAS USED. 5 MINUTES LATER NO INDICATIONS NOTE
- [SDR DALA2025111808410](https://openairdocs.org/sdr/DALA2025111808410.md): Ecs · contaminated · Nov 15, 2025 · N365NB · Airbus A319114 · Air Distribution System
  > FA'S REPORTED A "CHEMICAL SMELL" DURING DECENT. DECENT OCCURRED IN CLOUDS WITH MODERATE MOISTURE AND ENGINE ANTI-ICE ON. T/S IAW TSM 05-50 TASK 831. PERFORMED LEVEL A DECONTAMINATION IAW A320 AMM 21-00. NO DEFECTS NOTED. (7948340).
- [SDR DALA2025100107144](https://openairdocs.org/sdr/DALA2025100107144.md): Duct · contaminated · Sep 30, 2025 · N365NB · Airbus A319114 · Air Distribution System
  > WET DOG ODOR/FUMES NOTICED BY FLIGHT CREW FOLLOWING ENGINE SERVICING AND RUN UP. ACCOMPLISHED WORKCARD 2100- 2005 ECS DECONTAMINATION REVERSE DUCT BURN PROCEDURE. ALSO ACCOMPLISHED A319 AMM 21-00-00-615-803-A DECONTAMINATION OF THE ECS. (7597324).
- [SDR DALA2025051903844](https://openairdocs.org/sdr/DALA2025051903844.md): Hinge Fitting · cracked · May 19, 2025 · N365NB · Airbus A319114 · Fuselage, Door Hinge
  > SHIP 3165 CRACK INDICATION ON DOOR MLG KEEL BEAM HINGE FITTING LH SIDE IN AFT LUG WEB LOWER CORNER RADIUS CRACK LENGTH 0.182 INCH AD RELATED AT MAIN WHEEL WELL. CORRECTIVE ACTION: COMPLIED WITH ER/A 626383-14AD. (0973764)
- [SDR DALA2025051903843](https://openairdocs.org/sdr/DALA2025051903843.md): Hinge Fitting · cracked · May 19, 2025 · N365NB · Airbus A319114 · Fuselage, Door Hinge
  > SHIP 3165 CRACK INDICATION ON DOOR MLG KEEL BEAM HINGE FITTING RH SIDE IN FWD LUG WEB LOWER CORNER RADIUS. CORRECTIVE ACTION: COMPLY WITH ER/A 626382-14AD. (0973969)
- [SDR DALA2025050703517](https://openairdocs.org/sdr/DALA2025050703517.md): Cooling Fan · leaking · May 6, 2025 · N365NB · Airbus A319114 · APU Oil System
  > SHIP 3165 OILY/DIRTY SOCK SMELL WITH PACKS RUNNING APU AND ENGINES. RAN APU. CONFIRMED SMELL W/APU OP. FOUND EVIDENCE OF OIL AROUND APU COOLING FAN. DVI WITH BLACK LIGHT OF APU. REMOVED AND REPLACED APU COOLING FAN PER A319 AMM 49-52. PERFORMED LEVEL B REMOV
- [SDR DALA2024121111622](https://openairdocs.org/sdr/DALA2024121111622.md): Fitting · damaged · Dec 10, 2024 · N365NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > SHIP 3165 DAMAGE WAS FOUND ON THE NO.1 PYLON FORWARD SPIGOT FITTING. CORRECTIVE ACTION: COMPLIED WITH ER/A 31-622911. (0704015)
- [SDR DALA2024113011287](https://openairdocs.org/sdr/DALA2024113011287.md): Sensor · inoperative · Nov 28, 2024 · N365NB · Airbus A319114 · Door Warning System
  > SHIP 3165 FWD CARGO DOOR IND INOP. CORRECTIVE ACTION: R/R PROX SENSOR PER A319 AMM 52-31 OPS CHECKS GOOD. (6560942)
- [SDR DALA2024113011286](https://openairdocs.org/sdr/DALA2024113011286.md): Switch · loose · Nov 28, 2024 · N365NB · Airbus A319114 · Door Warning System
  > SHIP 3165 RECEIVED FWD CARGO DOOR UNLOCK ON ECAM TWO TIMES. CORRECTIVE ACTION: CLEANED AND SECURED PROX SW 30WV AND 28WV HARNESS PROPERLY PER A319 ESPM 20-55-00. OPS CHECK GOOD. (6560938)
- [SDR DALA2024062006267](https://openairdocs.org/sdr/DALA2024062006267.md): Warning Message · false activation · Jun 19, 2024 · N365NB · Airbus A319114 · Landing Gear Brake System
  > SHIP 3165 BRAKES SYSTEM 1 FAULT. COMPUTER RESET UNSECCESSFUL. CORRECTIVE ACTION: PERFORMED MCDU BITE TEST OF BSCU 1 IAW A319 AMM 32-46. NO FAULTS NOTED ON PREVIOUS LEG, TEST PASSED, (6021078)
- [SDR DALA2023110709156](https://openairdocs.org/sdr/DALA2023110709156.md): Unknown · unknown · Nov 7, 2023 · N365NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > SHIP 3165 PYLON PANEL ABOVE 483AR CRACKED AT LOWER T/E. CORRECTIVE ACTION: REPAIRED PER ERA 613522-14. (0053006)
- [SDR DALA2023081606684](https://openairdocs.org/sdr/DALA2023081606684.md): Unknown · unknown · Aug 15, 2023 · N365NB · Airbus A319114 · Nose/Tail Landing Gear
  > SHIP 3165 ON DEPARTURE AT 1000 BOTH F/D FAIL AUTO THRUST FAIL LG SHOCK ABSORBER FAIL. CORRECTIVE ACTION: ADJUSTMENT CHCK ON CENTARING TORQUE LINK PIN ON NLG, FOUND WITHIN CLEARENCE 0-00. CHCK FOR FREE MOVEMENT, FOUND STUCK OUT NOT FREEMOVEMENT IAW AMM A320 32-
- [SDR DALA2023081406597](https://openairdocs.org/sdr/DALA2023081406597.md): Unknown · unknown · Aug 13, 2023 · N365NB · Airbus A319114 · Vertical Stabilizer, Plate/Skin
  > SHIP 3165 CRACK ACCESS PANEL 322BL LH AND RH SIDE VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 610805-14. (2916475)
- [SDR DALA2023081106572](https://openairdocs.org/sdr/DALA2023081106572.md): Unknown · unknown · Aug 11, 2023 · N365NB · Airbus A319114 · Vertical Stabilizer, Plate/Skin
  > SHIP 3165 CRACK EXTERNAL SKIN LH ACCESS PANEL 322AL LEADING EDGE AND RH SIDE VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 610826-14. (2912204)
- [SDR DALA2023081106573](https://openairdocs.org/sdr/DALA2023081106573.md): Unknown · unknown · Aug 10, 2023 · N365NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3165 FUSELAGE / FRAME/FORMERS / FR16RH AT DOOR STOP NO 7 LEVEL DOUBLE JOGGLE / HOLE 6 / CRACKS. CORRECTIVE ACTION: REPAIRED PER ER/A 587403-14. (2911802)
- [SDR DALA2023081006501](https://openairdocs.org/sdr/DALA2023081006501.md): Unknown · unknown · Aug 9, 2023 · N365NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3165 FUSELAGE / FRAME / FR20RH AT DOOR STOP NO 7 LEVEL, DOUBLE JOGGLE AREA / FASTENER HOLE 6 / CRACK. CORRECTIVE ACTION: REPAIRED PER ER/A 587346-14. (2909355)
- [SDR DALA2023080706421](https://openairdocs.org/sdr/DALA2023080706421.md): Unknown · unknown · Aug 5, 2023 · N365NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3165 CRACK INDICATION ON FRAME 68 LH SIDE DOOR STOP FITTING 4 LOWER INBOARD HOLE (4) CRACK DIRECTION 6 O CLOCK AT AFT GALLEY AREA. CORRECTIVE ACTION: REPAIRED PER A319 SRM53-41-12-300-010. (2902305)
- [SDR DALA2023080406343](https://openairdocs.org/sdr/DALA2023080406343.md): Unknown · unknown · Aug 3, 2023 · N365NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3165 CRACK INDICATION ON FRAME 68 LH SIDE DOOR STOP FITTING 5 LOWER INBOARD HOLE (4) CRAC DIRECTION 5 O CLOCK AT AFT GALLEY AREA. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC ON FRAME 68 LH SIDE DOOR STOP FITTING 5 LOWER INBOARD HOLE (4) AT AFT GALLE
- [SDR DALA2023020600913](https://openairdocs.org/sdr/DALA2023020600913.md): Not Reported · not reported · Feb 3, 2023 · N365NB · Airbus A319114 · Engine Oil System (Airframe Furnished)
  > AIRCRAFT 3165, PASSING 5000' IN CLIMB FLT CREW NOTICED A CHEMICAL ODOR. SMELL QUICKLY DISSIPATED. FLT CREW, FLT ATTENDANTS & PAX NOTICED CHEMICAL ODOR ON APPROACH TO LANDING. AND TAXI. CORRECTIVE ACTION: FOUND OIL WETTING ON HPC STAGES 1,2,3 BLADES. ENGINE REP
- [SDR DALA2023011800374](https://openairdocs.org/sdr/DALA2023011800374.md): Filter · odor · Jan 17, 2023 · N365NB · Airbus A319114 · Air Distribution System
  > INBOUND CREW REPORTED DIRTY SOCK SMELL DURING TAXI IN. REPLACE BOTH RECIRCULATIONS FILTER PER A321 AMM 21-21. C/W AMDS CARD 0550-2001.
- [SDR DALA2021121007612](https://openairdocs.org/sdr/DALA2021121007612.md): Valve · shorted · Dec 9, 2021 · N365NB · Airbus A319114 · Pneumatic Distribution System
  > SHIP 3165 - DIV - TO BIL DUE TO DUE C/B FOR CROSS BLEED VALVE POPPED IN FLIGHT. COULD NOT CONTINUE DUE TO ICING CONDITIONS. REPORTED THAT VALVE FUNCTIONS IN MANUAL MODE BUT C/B POPS WHEN LEFT IN AUTO MODE. CORRECTIVE ACTION: REPLACED CROSS BLEED VALVE PER A319
- [SDR DALA2021112307205](https://openairdocs.org/sdr/DALA2021112307205.md): None · none · Nov 19, 2021 · N365NB · Airbus A319114 · Landing Gear Actuator
  > SHIP 3165 - GEAR - FLT CREW HEARD A LOUD "POP" AND RECEIVED L/G GEAR NOT DOWNLOCKED ECAM MESSAGE DURING GEAR EXTENSION FOR LANDING. GRAVITY GEAR EXTENSION PERFORMED BUT GEAR SYSTEM PAGE INDICATED ONLY MLG WAS DOWN. MAINTENANCE FOUND NLG RETRACT ACTUATOR ROD EN
- [SDR DALA2021111507032](https://openairdocs.org/sdr/DALA2021111507032.md): Light · odor · Nov 14, 2021 · N365NB · Airbus A319114 · Passenger Compartment Lighting
  > A/C 3165 - F/A REPORTED SMELL OF FUMES NO SMOKE. GALLEY LIGHT TURNED OFF, SMELL DISSAPATED. PERFORMED NOGO ODI WORKCARD AMDS 0550-2002 TYPE 9. DEACTIVATED FWD GALLEY WORKLIGHT PER ER/A 600000-14TR REV ORIG. C/W PERM REPAIR PER MSF.
- [SDR DALA2020092503188](https://openairdocs.org/sdr/DALA2020092503188.md): Target · out of adjust · Sep 23, 2020 · N365NB · Airbus A319114 · Door Warning System
  > DOOR L EMER EXIT ECAM MESSAGE IN FLIGHT ECAM DOOR PAGE INDICATIONS, OVERWING EMERGENCY EXITS, OPEN INDICATION. CORRECTIVE ACTION: T/S, PER TSM 52-21-00-810-806-A. ADJUSTED TARGET ON FLAP, OPERATIONS NORMAL.

Next page: https://openairdocs.org/aircraft/N365NB/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 = 'N365NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N365NB/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.