# Service difficulty reports: N359NB

A list on [N359NB](https://openairdocs.org/aircraft/N359NB.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 · 126 reports

- [SDR DALA2026092405333](https://openairdocs.org/sdr/DALA2026092405333.md): Autobrake Sys · faulted · Sep 23, 2026 · N359NB · Airbus A319114 · Landing Gear Brake System
  > AUTOBRAKES DISCONNECTED ABRUPTLY AND HARSHLY AT 60 KNOTS ( AFTER BRAKES WERE ALREADY APPLIED). ON TAXI IN, NOTICED AUTOBRAKES STILL SET TO MEDIUM TURNED OFF AUTOBRAKES MANUALLY WITH PUSH BUTTON. PERFORMED BITE TEST OF THE BSCU IAW AMM 32-46-00, NO FAULTS NOT
- [SDR DALA2026071504147](https://openairdocs.org/sdr/DALA2026071504147.md): Frame · damaged · Jul 10, 2026 · N359NB · Airbus A319114 · Fuselage Main, Frame
  > PERMANENT REPAIR (REPLACEMENT OF FR16 LHS) WAS ACCOMPLISHED AT PREVIOUS M2 CHECK, PER 586145-14 REV D. AT REV E STAGE 2 AND/OR STAGE 3 REPAIR APPROVAL ACHIEVED. NEW REPAIR ICA'S ARE IMPLEMENTED. C/A: PER SECTION VII OF 586145-14 REV E, ACCOMPLISH SECTION VII
- [SDR DALA2026071504146](https://openairdocs.org/sdr/DALA2026071504146.md): Frame · damaged · Jul 10, 2026 · N359NB · Airbus A319114 · Fuselage Main, Frame
  > *DTE*PERMANENT REPAIR (REPLACEMENT OF FR16 LT) ACCOMPLISHED AT PREVIOUS M2 CHECK, PER 586145-14 REV D. AT REV E STAGE 2 AND/OR STAGE 3 REPAIR APPROVAL ACHIEVED. NEW REPAIR ICA'S ARE IMPLEMENTED. *DTE* PER SECTION DTE III OF 586145-14 REV E,FR16 LHS CROSS BEA
- [SDR DALA2026071504145](https://openairdocs.org/sdr/DALA2026071504145.md): Frame · damaged · Jul 10, 2026 · N359NB · Airbus A319114 · Fuselage Main, Frame
  > *DTE* PERMANENT REPAIR (REPLACEMENT OF FR16 LT) ACCOMPLISHED AT PREVIOUS M2 CHECK, IAW 586145-14 REV D. AT REV E, STAGE 2 AND/OR STAGE 3 REPAIR APPROVAL ACHIEVED. NEW REPAIR ICA'S ARE IMPLEMENTED. *DTE* PER SECTION DTE II OF 586145-14 REV E, FR16 LHS DBL JG
- [SDR DALA2026062203691](https://openairdocs.org/sdr/DALA2026062203691.md): Light · unknown · Jun 19, 2026 · N359NB · Airbus A319114 · Emergency Lighting
  > EMERGENCY LIGHTS IN CABIN COME ON WHEN ENG ANTI ICE IS TURNED ON. IT HAPPENED EVERY TIME THE ANTI -ICE SWITCHES WERE CYCLED IN FLIGHT. PERFORMED EMERGENCY LIGHTING TEST IAW TSM 33-52-00-810-881A. TEST PASSED. PERFORMED OPS CHECK OF ENG ICE PROTECTION SYSTEM
- [SDR DALA2026042202552](https://openairdocs.org/sdr/DALA2026042202552.md): Oxygen Mask · faulted · Apr 19, 2026 · N359NB · Airbus A319114 · Crew Oxygen System
  > SHIP 3159 DISC: DURING CAPT OXYGEN MASK TEST THE MASK STARTED FLOWING OXYGEN NON - STOP. THE MASK WAS REMOVED. SPINNING THE EMER DIAL AND FLIPPING THE 100% SWITCH HAD NO EFFECT. AFTER ABOUT 45 SECONDS IT SHUT OFF WITH NO OTHER ACTIONS. C/A: R&R CAPT'S O2 MASK
- [SDR DALA2026031701840](https://openairdocs.org/sdr/DALA2026031701840.md): Unknown · haze · Mar 15, 2026 · N359NB · Airbus A319114 · Air Distribution System
  > FA'S ADVISED SLIGHT HAZE IN CABIN ON TAXI IN. THRUST REVERSERS WERE HELD OUT TO MAX REVERSE UNTIL ROUGHLY 45-50KN DUE TO RUNWAY CONDITIONS. NO ODOR NOTICED BY FA'S. SMOKE & FUMES REPORT COMPLETED. C/A: CONFERRED WITH MCC, DUE TO THIS SPECIFIC EVENT BEING REPOR
- [SDR DALA2026012600551](https://openairdocs.org/sdr/DALA2026012600551.md): Fitting · damaged · Jan 25, 2026 · N359NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > PERFORM ER/A 630835-14 AD FOR REPLACEMENT OF CONTINUITY FITTINGS. C/A: COMPLIED WITH ER/A 630835-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF ERA 630835-14AD PRI REV 0 TO REV 2 IT IS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON CONTINUITY FITTINGS LH AND R
- [SDR DALA2026012600550](https://openairdocs.org/sdr/DALA2026012600550.md): Not Reported · not reported · Jan 25, 2026 · N359NB · Airbus A319114 · Fuselage Structure (General)
  > PERFORM ER/A 586145-14AD REV D FOR REPLACEMENT OF FR16 LT IN PASSENGER CABIN. ER/A 586145-14AD REV D, APPROVED DATE: 23/JAN/26 WAS VERIFIED AGAINST ER/A 586145-14AD REV D PRI REV 0 AND WERE FOUND INCOMPLIANCE WITH THE SCOPE OF THE WORK ACCOMPLISHED, STEP RELA
- [SDR DALA2026012600549](https://openairdocs.org/sdr/DALA2026012600549.md): Window Frame · cracked · Jan 25, 2026 · N359NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON RH WINDSHIELD CENTER POST, LOWER ATTACHMENT ARIA, LOWER CORNER RADIUS, CRACK IS HORIZONTAL DIRECTION, CRACK LENGTH IS 0.190 INCH. AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR
- [SDR DALA2026012900702](https://openairdocs.org/sdr/DALA2026012900702.md): Receptacle · corroded · Jan 24, 2026 · N359NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > CORROSION BORE SPIGOT FITTING RECEPTACLE ON RT PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RT PYLON IAW SRM 54-51-12-300-001, & SRM 54-51-12-283-001. FOUND BEYOND LIMITS, MEASUREMENT OF CORRODED AREA: D: 0.0042 INCH & OF DIAMETER IS 4.348 INCH. (LP: 141796
- [SDR DALA2026012600548](https://openairdocs.org/sdr/DALA2026012600548.md): Floor Panel · corroded · Jan 23, 2026 · N359NB · Airbus A319114 · Fuselage Floor Panel
  > CORROSION INSERT FLOOR PANEL 221PF IN PASSENGER CABIN. C/A: COMPLIED WITH ER/A 631181-14 REV ORIGINAL APPROVED DATE: 06/JAN/ 26. MATCHES WITH ALL STEPS ON ER/A 631181-14 PRI REV.0 IT HAS BEEN VALIDATED. REPLACE FLOOR PANEL 221PF IN PASSENGER CABIN AS PER ER/A
- [SDR DALA2026012600547](https://openairdocs.org/sdr/DALA2026012600547.md): Post · corroded · Jan 23, 2026 · N359NB · Airbus A319114 · Fuselage Main, Structure
  > CORROSION ON AFT LATERAL POST LAVATORY A AT FWD GALLEY AREA. COMPLIED WITH ER/A 631052-14 REV. A. APPROVED DATE: 16-JAN-26 MATCHES WITH ALL STEPS OF ER/A 631052-14 PRI REV. 0 AND REV 1 IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON AFT LATERAL POST L
- [SDR DALA2026012600545](https://openairdocs.org/sdr/DALA2026012600545.md): Frame · damaged · Jan 23, 2026 · N359NB · Airbus A319114 · Fuselage Main, Frame
  > DURING M2 PERMANENT REPAIR (REPLACEMENT OF FR16 LHS) IS DUE AS REQUIRED PER EXISTING LOG 0917237 OF ER/A 586145-14AD, REV C. C/A: *DTE* PER SECTION DTE-1 OF 586145-14AD, REV D, THE REPAIR OF SECTION IV IS LIMITED TO 6 MONTHS (180 DAYS) SERVICE FROM SECTION IV.
- [SDR DALA2026012200489](https://openairdocs.org/sdr/DALA2026012200489.md): Web · damaged · Jan 21, 2026 · N359NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE WEB FR 56 TO FR 57 AND STR 38L IN AFT CARGO BAY. REPLACED WEB AND FASTENERS LOC FR 56 TO FR 57 AND STR 38L IN AFT CARGO BAY IAW SRM 51-42- 11, SRM 51-72-11, AND DWG D53476318, ISSUE: N. (LP: 1413058)
- [SDR DALA2026012200481](https://openairdocs.org/sdr/DALA2026012200481.md): Window Frame · cracked · Jan 16, 2026 · N359NB · Airbus A319114 · Fuselage Main, Structure
  > DURING M2 & WHILE ACCOMPLISHING EM 5311-01226-01, CRACKS WERE FOUND IN LT & RT FRONT WINDSHIELD FRAMES, LWR CTR NODE AREA. PER SECTION DTE OF 630808-14 THE REPAIR OF SECTION I IS LIMITED TO 30,600 FC FROM SECTION I.
- [SDR DALA2026011700390](https://openairdocs.org/sdr/DALA2026011700390.md): Window Frame · cracked · Jan 14, 2026 · N359NB · Airbus A319114 · Fuselage Main, Structure
  > DURING M2 AND WHILE ACCOMPLISHING EM 5311-01226-01 CRACKS FOUND IN LT & RT FRONT WINDSHIELD FRAMES LWR CTR NODE AREA. *DTE* PER SECTION DTE OF 630808-14 THE REPAIR OF SECTION I IS LIMITED TO 30,600 FC FROM SECTION I (6JAN26). ADDITIONAL ENG'G AUTHORIZATION RE
- [SDR DALA2026011500358](https://openairdocs.org/sdr/DALA2026011500358.md): Seat Track · corroded · Jan 12, 2026 · N359NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK +Y1292, FR 16 LT SIDE FWD GALLEY AREA. REPLACED SEAT TRACK Y1292 FR 12 TO FR 24 IAW SRM 51-42-11 AND SRM 51-72-11, AND DWG D53110920, ISSUE E00, DWG D53110984 ISSUE C00 TOOK MEASURES OF CORROSION ARE: L= 0.916 INCHW= 0.390 INCH D= 0.039
- [SDR DALA2026011500357](https://openairdocs.org/sdr/DALA2026011500357.md): Floor Support · corroded · Jan 12, 2026 · N359NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORRODED FLOOR SUPPORT +Y1292, FR 66 LT SIDE AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT Y1292, AND FASTENERS FR 64 TO FR 66 IAW SRM 51-42-11, SRM 51-72- 11,AND DWG 10N01048, REV A, APPROVED DATE 21/AUG/14 TOOK MEASURE OF CORROSION ARE: L: 2.589 INCHES W:0
- [SDR DALA2026011200256](https://openairdocs.org/sdr/DALA2026011200256.md): Strut · corroded · Jan 10, 2026 · N359NB · Airbus A319114 · Wing Main, Frame Structure
  > CORROSION ON INTERCONNECTING STRUT ON RT WING (REFERS TO AMDS CARD 275 1-9202 FOR RII). REMOVED INTERCONNECTING STRUT OF RH WING ON UNSERVICEABLE CONDITION P/N D5757032201100, S/N 985, IAW AMM 27- 51-44-000-001-A, STEP 1 THRU 3.C AND 4.A. REPLACED INTERCONNEC
- [SDR DALA2026010900207](https://openairdocs.org/sdr/DALA2026010900207.md): Seat Track · corroded · Jan 8, 2026 · N359NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK +Y1225, FR 66 TO 68 LT SIDE AT AFT GALLEY AREA. REPLACED THE SEAT TRACK Y1225 & FASTENERS IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53472780, ISSUE K, DWG D53474250 ISSUE V. MEASUREMENT OF CORROSION ARE L:0.508 INCHES W:0.249 INCHES D:0.
- [SDR DALA2026010900206](https://openairdocs.org/sdr/DALA2026010900206.md): Seat Track · corroded · Jan 8, 2026 · N359NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK -Y1292, FR 65 TO FR 66 RT SIDE AFT GALLEY AREA, REPLACED THE SEAT TRACK IAW SRM 51-42-11, SRM 51-72-11, DWG 10N01048, REV A, DWG 14N00031, REV E, MEASUREMENT OF CORROSION WAS: L= 2.577 INCHES W= 0.728 INCHES D= 0032 INCH. (LP: 1392219)
- [SDR DALA2026010900204](https://openairdocs.org/sdr/DALA2026010900204.md): Seat Track · corroded · Jan 7, 2026 · N359NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK -Y765 AT AFT GALLEY AREA. REPLACED SEAT TRACK -Y765 AND FASTENERS LOCATED BETWEEN FR64 TO FR66 RH SIDE AT AFT GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, AND DWG 10N01048, REV A, (LP: 1390695)
- [SDR DALA2026010900203](https://openairdocs.org/sdr/DALA2026010900203.md): Floorbeam · corroded · Jan 7, 2026 · N359NB · Airbus A319114 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM -Y1162.5 LOC. FR 68 RH SIDE AT AFT GALLEY AREA. REPLACED FLOOR BEAM -Y1162.5, SPLICES 2 E/A AND FASTENERS LOC FR 68 TO FR 69 RH SIDE AT AFT GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, DWG D53472089, ISSUE M, DWG D53474250, ISSUE V, DWG D
- [SDR DALA2026010900205](https://openairdocs.org/sdr/DALA2026010900205.md): Support Angle · cracked · Jan 6, 2026 · N359NB · Airbus A319114 · Horizontal Stabilizer Structure
  > CRACK SUPPORT ANGLE, HINGE ARM 1 ELEVATOR ON LT HORIZONTAL STAB. REPLACED SUPPORT ANGLE ON HINGE ARM 1 ELEVATOR IAW SRM 51-42-11, SRM 51-72- 11, DWG D55182701, ISSUE W, AMM 55-16-42-000-001-A, AND AMM 55-16-42-400-001-A, MEASUREMENT OF CRACK WAS 0.408IN.
- [SDR DALA2026010900202](https://openairdocs.org/sdr/DALA2026010900202.md): Dummy Rail · corroded · Jan 6, 2026 · N359NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION RAIL DUMMY Y503.2 AT FWD GALLEY AREA. REPLACED RAIL DUMMY Y503.2 FR12 TO FR16 LH AND FASTENERS AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND DWG D53112825 AND DWG D53110984. TOOK MEASURES OF CORROSION ARE L:1.562 IN W:1.375 IN D:0.060 IN. (LP: 1
- [SDR DALA2026010900201](https://openairdocs.org/sdr/DALA2026010900201.md): Seat Track · corroded · Jan 6, 2026 · N359NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK -Y765 LOC. FR 20. REPLACED THE SEAT TRACK IAW SRM 51-42-11, SRM 51-72-11, DWG D53110984, ISSUE: C00, DWG D53110920, ISSUE: E00, AND DWG D53112812, ISSUE: E00, MEASUREMENT OF CORROSION: L= 2.790 IN W=1.198 IN D=0.061 IN. (LP: 1389294)
- [SDR DALA2026010900200](https://openairdocs.org/sdr/DALA2026010900200.md): Floor Support · corroded · Jan 6, 2026 · N359NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT -Y1292, FR 18 - 20. REPLACED THE FLOOR SUPPORT AND FASTENERS IAW SRM 51-42-11, SRM 51-72-11, DWG D53110984, DWG D53110920, DWG D53112812. AND IAW ESPM 20-33-41. MEASUREMENT OF CORROSION: P.1 L= 1.184 IN W= 0.787 IN D= 0.026 IN P.2 L
- [SDR DALA2026010900199](https://openairdocs.org/sdr/DALA2026010900199.md): Seat Track · corroded · Jan 6, 2026 · N359NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK +Y765 AT FR66. REPLACED THE SEAT TRACK AND FASTENERS IAW SRM 51-42-11, SRM 51-72 -11, AND DWG 10N01048, ISSUE: F. MEASUREMENT OF CORROSION: L= 2.187 INCHES, W= 0.504 INCHES, D= 0.032 INCHES. (LP: 1389196)
- [SDR DALA2026010900198](https://openairdocs.org/sdr/DALA2026010900198.md): Seat Track · corroded · Jan 6, 2026 · N359NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK +Y1162.5 LOC. FR 68 TO FR 69 LH SIDE AT AFT GAL LEY AREA. REPLACED SEAT TRACK IAW SRM 51-42-11, SRM 51-72 11, AND DWG: D53474180, ISSUE AA, DWG: D53472780, ISSUE K, DWG: D53474250, ISSUE V, DWG: D53472088, ISSUE H, AND DWG D53478309, ISS
- [SDR DALA2026010500048](https://openairdocs.org/sdr/DALA2026010500048.md): Shear Plate · cracked · Dec 31, 2025 · N359NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CRACK SHEAR PLATE STR 23R BTW FR69 AND FR70 AT AFT GALLEY AREA. C/A: REPLACED SHEAR PLATE AND FASTENERS LOC ON STR 23R BTW FR69 AND FR70 AT AFT GALLEY AREA IAW SRM 51-42-11, SRM 51-72- 11 AND DWG D53474180, ISSUE: AA, MEASUREMENT OF CRACK: 0.589 INCH, (LP: 13
- [SDR DALA2025122409393](https://openairdocs.org/sdr/DALA2025122409393.md): Shear Plate · cracked · Dec 23, 2025 · N359NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CRACKED SHEAR PLATE, STR 23L BTW FR 69 AND FR 70 AT AFT GALLEY AREA. REPLACED THE SHEAR PLATE AND FASTENERS IAW SRM 51-42-11, AND SRM 51-72 -11. (1365972).
- [SDR DALA2025122209285](https://openairdocs.org/sdr/DALA2025122209285.md): Roller · worn · Dec 20, 2025 · N359NB · Airbus A319114 · Trailing Edge Flaps
  > WEAR ON CRUISE ROLLER IB FLAP ON RH WING. REPLACED CRUISE ROLLER IB FLAP ON RH WING AS PER AIRBUS CMM 57-52-21, TASK 57-52-21-000-805-A01 AND TASK 57-52-21-400-803-A01. (1360923)
- [SDR DALA2025122209281](https://openairdocs.org/sdr/DALA2025122209281.md): Access Panel · cracked · Dec 19, 2025 · N359NB · Airbus A319114 · Nacelle/Pylon, Plate/Skin
  > CRACK ON ACCESS PANEL 413DL LT PYLON. WITH ER/A 540187-14MA. (1360059).
- [SDR DALA2025122209288](https://openairdocs.org/sdr/DALA2025122209288.md): Bearing · excess play · Dec 19, 2025 · N359NB · Airbus A319114 · Elevator Structure
  > SHIP 3159 AXIAL PLAY ON BEARING OF ELEVATOR HINGE ARM (HINGE #4 #5 AND #6) RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED BEARING OF ELEVATOR HINGE ARM (HINGE #4 #5 AND #6) RH HORIZONTAL STABILIZER AS PER A320 FAM AMM 55-16-42-000-001-A AND AMM 55-16-42
- [SDR DALA2025121909256](https://openairdocs.org/sdr/DALA2025121909256.md): Roller · deteriorated · Dec 18, 2025 · N359NB · Airbus A319114 · Passenger/Crew Doors
  > DETERIORATED ROLLER FROM UPPER AND LOWER POSITION AND FWD AND AFT SIDE OF PASSENGER CREW DOOR 831. REPLACED ROLLER FROM UPPER AND LOWER POSITION AND FWD AND AFT SIDE OF PASSENGER CREW DOOR 831 (4E/A) AS PER FAM AMM52-11-31-000-002-A AND IAW FAM AMM 52-11-31-4
- [SDR DALA2025121909255](https://openairdocs.org/sdr/DALA2025121909255.md): Roller · worn · Dec 18, 2025 · N359NB · Airbus A319114 · Trailing Edge Flaps
  > WORN CRUISE ROLLER INBD FLAP ON RT WING. REPLACED THE CRUISE ROLLER OF INBD FLAP ON RT WING IAW CMM 57- 52-21, TASK 57-52-21-000-805-A01, & TASK 57-52-21-400-803-A01. (1357915).
- [SDR DALA2025121609157](https://openairdocs.org/sdr/DALA2025121609157.md): Bearing · excess play · Dec 15, 2025 · N359NB · Airbus A319114 · Elevator Structure
  > AXIAL PLAY ON BEARING OF ELEVATOR HINGE ARM (HINGE 6) LT HORIZONTAL STABILIZER. REPLACED HINGE ARM OF ELEVATOR LH HORIZONTAL STABILIZER AS PER A320 FAM AMM 55-16-42-000-001-A AND AS PER A320 FAM AMM 55-16-42-400-001-A. (1353321).
- [SDR DALA2025121109045](https://openairdocs.org/sdr/DALA2025121109045.md): Receptacle · corroded · Dec 10, 2025 · N359NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > CORRODED SPIGOT FITTING RECEPTACLE ON LT PYLON. REPLACED THE SPIGOT FITTING RECEPTACLE IAW SRM 54-51-12-300-001, AND SRM 54-51-12-283-001. (1345070).
- [SDR DALA2025092206924](https://openairdocs.org/sdr/DALA2025092206924.md): Floor Panel · damaged · Sep 17, 2025 · N359NB · Airbus A319114 · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL DAMAGED. R & R FWD CARGO FLOOR PANEL IAW A319 AMM 53-25. (1204238).
- [SDR DALA2025091806851](https://openairdocs.org/sdr/DALA2025091806851.md): Floor Panel · damaged · Sep 17, 2025 · N359NB · Airbus A319114 · Fuselage Floor Panel
  > FOUND FWD CARGO FLOOR PANEL DAMAGED. CORRECTIVE ACTION: COMPLIED WITH ER/A 587849-14TR. (7770058).
- [SDR DALA2025081306063](https://openairdocs.org/sdr/DALA2025081306063.md): Panel · delaminated · Aug 13, 2025 · N359NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > FOUND REPLACEMENT PANEL 192FB TO BE DAMAGED/DELAMINATING, FWD INBD CORNER. COMPLIED WITH ER/A 628505-14.
- [SDR DALA2025081206033](https://openairdocs.org/sdr/DALA2025081206033.md): Skin · delaminated · Aug 12, 2025 · N359NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > PANEL UNDER AIRCRAFT BY RIGHT PACK INTAKE DELAMINATING. COMPLIED WITH ER/A 628505-14.
- [SDR DALA2025080505867](https://openairdocs.org/sdr/DALA2025080505867.md): Door · out of adjust · Aug 5, 2025 · N359NB · Airbus A319114 · Passenger/Crew Doors
  > MAIN CABIN L1 DOOR DIFFICULT TO OPEN FROM OUTSIDE. ADJUSTED Z AXIS REF AMM 52-11. CKS GOOD.
- [SDR DALA2025072105474](https://openairdocs.org/sdr/DALA2025072105474.md): Warning Light · false activation · Jul 19, 2025 · N359NB · Airbus A319114 · Door Warning System
  > SHIP 3159 DOOR L FWD CABIN ON ECAM AND DOOR 1L WAS SHOWING OPEN ON DOOR PAGE. COULD NOT DUPLICATE ON THE GROUND 1L DOOR INDICATES NORMALLY OPEN/ CLOSED ON EICAS.
- [SDR DALA2025071405299](https://openairdocs.org/sdr/DALA2025071405299.md): Bolt · missing · Jul 13, 2025 · N359NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3159 L1 WILL NOT SHUT PROPERLY AND WILL NOT ARM. INSTALLED MISSING HARDWARE AND PERFORMED OPS CHECK OF 1L DOOR AND LOCKING SYSTEM PER A319 AMM 52-11-31.
- [SDR DALA2025070104934](https://openairdocs.org/sdr/DALA2025070104934.md): Skin · damaged · Jul 1, 2025 · N359NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3159 DURING DOOR CLOSURE OF 1L, GATE AGENT & LEAD FA NOTICED TOP LEFT OF EXTERIOR DOOR WAS DAMAGED. CORRECTIVE ACTION: REMOVED & REPLACED L1 PAX DOOR PER A319 AMM 52-11. (7012590).
- [SDR DALA2025040702620](https://openairdocs.org/sdr/DALA2025040702620.md): Bleed Valve · overheated · Apr 5, 2025 · N359NB · Airbus A319114 · Compressor Bleed Valve
  > SHIP 3159 - DIV - TO DEN DUE TO DUAL BLEED FAULT (AIR ENG 1 BLEED FAULT AND AIR ENG 2 BLEED FAULT). WAS ABLE TO RECOVER #1 ENGINE BLEED, PRESSURIZATION AND PACKS WORKING AS SHOULD. UNABLE TO CONTINUE DUE TO ENROUTE WEATHER. CORRECTIVE ACTION: REPLACED FAN AIR
- [SDR DALA2024122411972](https://openairdocs.org/sdr/DALA2024122411972.md): Frame · cracked · Dec 23, 2024 · N359NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3159 CRACK INDICATION WAS FOUND ON FR16LH, FASTENER HOLES #11 AND #12. CORRECTIVE ACTION: REPAIRED PER ER/A 586145-14AD. (0725030)
- [SDR DALA2026012900701](https://openairdocs.org/sdr/DALA2026012900701.md): Stop Fitting · temp repair · Dec 22, 2024 · N359NB · Airbus A319114 · Fuselage Main, Structure
  > THE REPAIR INSTALLED ON FR 16L AT DOOR STOP NR 1 & 7 HAS HAD A DTE ACCOMPLISHED AND IS NOW CLASSIFIED AS A TEMPORARY REPAIR REQUIRING A 1900 FLIGHT CYCLE LIMIT. COMPLY WITH TIME LIMITATIONS LISTED IN REV. C OF ER/A 586145-14. ASSOCIATED ER/A 00-586145 ADDED.

Next page: https://openairdocs.org/aircraft/N359NB/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 = 'N359NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N359NB/reports

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