# Service difficulty reports: N349NB

A list on [N349NB](https://openairdocs.org/aircraft/N349NB.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 4 · 167 reports

- [SDR DALA2026041202308](https://openairdocs.org/sdr/DALA2026041202308.md): Tire · failed · Apr 8, 2026 · N349NB · Airbus A319114 · Tire
  > BLOWN TIRE ON MAIN LANDING GEAR #4 WITH VISIBLE FLUID ON MAIN GEAR ASSEMBLY 7 WHEEL WELL. R&R #4 MLG WHEEL ASSY PER A320/319 AMM 32-41-11. #4 MLG WHEELASSY OK FOR CONT. SERVICE. (LP: 8676597) AIRCRAFT WAS GROUNDED
- [SDR DALA2026040802237](https://openairdocs.org/sdr/DALA2026040802237.md): Brake Sys · faulted · Apr 8, 2026 · N349NB · Airbus A319114 · Landing Gear Brake System
  > DECLARED EMERGENCY INTO DTW DUE TO A BRAKES SYSTEM 1 FAULT ALONG WITH AN AUTO BRAKE FAULT AND A NORMAL BRAKES SERVO VALVE (18GG) FAULT. MLG #4 WHEEL FLAT SPOTTED AND FAILED DURING THE ROLL OUT. HYDRAULIC LEAK ABOVE THE MAIN LANDING GEAR WAS ALSO DISCOVERED.
- [SDR DALA2026040602163](https://openairdocs.org/sdr/DALA2026040602163.md): Engine · faulted · Apr 4, 2026 · N349NB · Airbus A319114 · Engine (Turbine/Turboprop)
  > REJECT TAKEOFF DUE TO ASYMMETRICAL POWER AND GATE RETURN FOR SIGNIFICANT LAG BETWEEN ENG & 2 ENG 1 LAGS 4 SEC TO ENG 2. INSPECTED PS3 LINE IAW AMM 72-00. PERFORMED ACCEL CHKD IAW AMM 71-00710-010-A ACCEL TIME OF 6.0 SECOND WITH IN LIMIT OF 7.5 AMM LIMIT. RUN
- [SDR DALA2026040302146](https://openairdocs.org/sdr/DALA2026040302146.md): Circuit Breaker · failed · Apr 1, 2026 · N349NB · Airbus A319114 · Ice/Rain Protection System Wiring
  > DIV - TO RDU DUE TO CAPTAIN'S PITOT HEAT INOP (ANTI ICE CAPT PITOT ECAM WARNING) AND FLYING INTO ICING CONDITIONS. REPLACED C/BS 3DA1 AND 2DA1. FOUND 3DA1 LOCK NUT LOOSE, AND WIRE STRAIN FROM BACK SHELL ON PITOT PROBE CONNECTOR (9DA1-A). LGCIU-1 REPLACED AS
- [SDR DALA2026031001636](https://openairdocs.org/sdr/DALA2026031001636.md): Control Box · faulty · Mar 10, 2026 · N349NB · Airbus A319114 · Rudder Control System
  > SHIP 3149 DSC: AFTER T/O AUTO FLT RUD TRV LIM SYS ECAM MESSAGE. FOLLOWED THE ECAM RESET PROCEDURE BUT THAT WAS NOT SUCCESSFUL. T/S PER A319 TSM 22-61-00-810-803-A. FOUND FAULT FAC 1/RTL ACTR 4CC. UNABLE TO RESET/HARD FAULT. NEXT STEP IS TO R/R ELECTRONIC MODU
- [SDR DALA2026022601353](https://openairdocs.org/sdr/DALA2026022601353.md): Plate · missing · Feb 14, 2026 · N349NB · Airbus A319114 · Leading Edge Devices
  > DURING WALK AROUND, FOUND LT SLAT 2 INBD SLAT TRACK CLOSING PLATE MISSING. FWD TO CDL 27-00-03. DISP APPROVED. NO "M" PROC. CDL AND PLACARD INSTALLED. (LP: 8558938)
- [SDR DALA2026012900699](https://openairdocs.org/sdr/DALA2026012900699.md): Window Frame · damaged · Jan 26, 2026 · N349NB · Airbus A319114 · Fuselage Main, Structure
  > AD 2020-17-03 / A.A. WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. FLIGHT DECK, RT WINDSHIELD FRAMING LOWER CENTER POST, & RT CONTINUITY FITTING CRACKED. PERFORMED WING FRAMING MIRROR REPAIR & CONT
- [SDR DALA2026020100733](https://openairdocs.org/sdr/DALA2026020100733.md): Window Frame · damaged · Jan 25, 2026 · N349NB · Airbus A319114 · Fuselage Main, Structure
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR FR 4 WINDOW FRAME. REPAIR PERFORMED PER ER/A 631144-14AD. SECTION I IS LIMITED TO 60000FC FROM EMBODIMENT. ER/A TO BE REVI SED PRIOR TO THIS LIMIT ELSE REMOVE ACFT FROM SERVICE. ASSOCIATED ER/A 14-631144 ADDED
- [SDR DALA2026012900708](https://openairdocs.org/sdr/DALA2026012900708.md): Anchor Fitting · corroded · Jan 25, 2026 · N349NB · Airbus A319114 · Wing, Landing Gear Attach Fittings
  > RIGHT WING REAR SPAR MAIN LANDING GEAR ACTUATOR ANCHORAGE FITTING WITH CORROSION. REPLACED ANCHORAGE FITTING AT RT WING REAR SPAR IAW REPAIR AUTHORIZATION 631319-14AD, REV. ORIGINAL, APPROVED AND DOCUMENTED ON AIRBUS RDAF REF AND ISSUE: 81710803/003/2025 A. C
- [SDR DALA2026012900707](https://openairdocs.org/sdr/DALA2026012900707.md): Window Frame · damaged · Jan 25, 2026 · N349NB · Airbus A319114 · Fuselage Main, Structure
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR LH & RH CONTINU ITY FITTING REPLACEMENT PERFORMED PER ER/A 631144-14AD. SECTION I LIMITED TO 29500FC FROM SECTION I. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 14-63114
- [SDR DALA2026012900706](https://openairdocs.org/sdr/DALA2026012900706.md): Window Frame · damaged · Jan 25, 2026 · N349NB · Airbus A319114 · Fuselage Main, Structure
  > ER/A 631144-14AD ISSUED FOR LT & RT MIRROR FITTING REPAIR. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 27000FC FROM SECTION I AND EVERY 4700F C THEREAFTER. ASSOCIATED ER/A 14-631144 ADDED. (LP: 1419073)
- [SDR DALA2026012600552](https://openairdocs.org/sdr/DALA2026012600552.md): Frame · cracked · Jan 25, 2026 · N349NB · Airbus A319114 · Fuselage Main, Frame
  > FWD FUSELAGE CROSSBEAM SPLICING FR16 L/H, HOLES "H2" AND "H3" WITH CRACK INDICATION AT FRAME LAYER. CONTACT LIAISON ENGINNERING FOR REPAIR DISPOSITION. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. REFER TO EM 5311-01221,
- [SDR DALA2026012900700](https://openairdocs.org/sdr/DALA2026012900700.md): Anchor Fitting · corroded · Jan 24, 2026 · N349NB · Airbus A319114 · Wing, Landing Gear Attach Fittings
  > LEFT WING, REAR SPAR, MAIN LANDING GEAR ACTUATOR, ANCHOR FITTING CORRODED. REPLACED THE ANCHOR FITTING AT LT WING REAR SPAR IAW EO 631312-14, REV 00. AND RA 631312-14AD, REV ORIGINAL APPROVED AND DOCUMENTED ON AIRBUS FORM RDAF REF AND ISSUE 81713336/03/2025
- [SDR DALA2026012600542](https://openairdocs.org/sdr/DALA2026012600542.md): Seat Track · damaged · Jan 24, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER CABIN SEAT TRACK AND SPLICES WITH ELONGATED HOLES AT FR64, +Y=1292. PERFORMED PERMANENT REPAIR ON UPPER FUSELAGE PASSENGER CABIN SEAT TRACK SECTION AND SPLICES BETWEEN 160MM AFT FR62 AND FR64, AT Y=1292 IAW ER/A #631509-14 REV: ORIGINAL THIS IS A MA
- [SDR DALA2026012600541](https://openairdocs.org/sdr/DALA2026012600541.md): Fitting · damaged · Jan 24, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AVIONICS RACK 80VU L/H LOWER LATERAL FITTING WITH MATERIAL BURRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. C/A: PERFORMED MAJOR REPAIR ON FWD FUSELAGE EQUIPMENT / RACK 80VU LH LOWER LATERAL SUPPORT DUE TO MATERIAL BURRED (OVAL
- [SDR DALA2026012600540](https://openairdocs.org/sdr/DALA2026012600540.md): Fitting · damaged · Jan 24, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AVIONICS RACK 80VU RT LOWER LATERAL FITTING WITH MATERIAL BURRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT. PERFORMED MAJOR REPAIR ON FWD FUSELAGE EQUIPMENT 1 RACK 80VU RT LOWER LATERAL SUPPORT DUE TO MATERIAL BURRED (OVALIATIO
- [SDR DALA2026012600544](https://openairdocs.org/sdr/DALA2026012600544.md): Frame · damaged · Jan 23, 2026 · N349NB · Airbus A319114 · Fuselage Main, Frame
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR REPAIRED & REPLACED FR16LH PER ER/A 631351-14AD. FOLLOW ON ACTION IS REQUIRED. SECTION I IS LIMITED TO 33500FC AFTER SECTION I. ER/A TO BE REVI SED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED E
- [SDR DALA2026012600543](https://openairdocs.org/sdr/DALA2026012600543.md): Frame · damaged · Jan 23, 2026 · N349NB · Airbus A319114 · Fuselage Main, Frame
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR REPAIR AND FRAME REPLACEMENT OF FR16LH PER ER/A 631351-14AD. FOLLOW ON ACTION R EQUIRED. SECTION I IS LIMITED TO 69600FC AFTER SECTION I. ER/A TO BE REVI SED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASS
- [SDR DALA2026012600539](https://openairdocs.org/sdr/DALA2026012600539.md): Seat Track · corroded · Jan 23, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE PAX CABIN, AFT ENTRY AREA FR 66 +Y1292 LT SEAT TRACK CORRODED. REPLACED THE SEAT TRACK IAW SRM SUPP 53-41-15, REV A. DRAWING # 14N000331, ER/A #631239-14 REV ORIGINAL AND AIPC 53-41-04-20E SHEET 1. REV 133.02.
- [SDR DALA2026012300519](https://openairdocs.org/sdr/DALA2026012300519.md): Seat Track · corroded · Jan 22, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > AFT FUSELAGE FLOOR STRUCTURE AT FR66+90 MM Y-1292 MM LONGITUDINAL BEAM WITH CORROSION. REPLACED SEAT TRACK P/N: 14N00031-101 AT UPPER FUSELAGE PAX CABIN, AFT ENTRY AREA FR66+90MM, Y-1292MM RH SIDE IAW NAT STRUCTURAL REPAIR MANUAL SUPPLEMENT 53-41-15 REV A DAT
- [SDR DALA2026012300518](https://openairdocs.org/sdr/DALA2026012300518.md): Support Arm · corroded · Jan 22, 2026 · N349NB · Airbus A319114 · Fuselage Main, Structure
  > AFT FUSELAGE FLOOR STRUCTURE AT FR 68 Y1260 MM, SILL BEAM WITH CORROSION. PERFORMED REPAIR AT AFT FUSELAGE FLOOR STRUCTURE, FR68 Y12060MM, SILL BEAM IAW ER/A 631462-14 REV ORIGINAL DATED 16/JAN/26. THIS IS A MAJOR REPAIR CATEGORY A WITH NO ADDITIONAL REQUIREM
- [SDR DALA2026012200488](https://openairdocs.org/sdr/DALA2026012200488.md): Web · corroded · Jan 21, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE INTERNAL FLOOR STRUCTURE BTWN FR 69 & FR 70, S23L, WEB WITH CORRDED. REPLACED SHEAR PLATE IAW SRM 53-41-17-01A, FIGURE 001, ITEM 310A AND INSTALLED IAW DWG D534 74180, ISSUE U, SHEET 6.
- [SDR DALA2026012200487](https://openairdocs.org/sdr/DALA2026012200487.md): Structure · corroded · Jan 20, 2026 · N349NB · Airbus A319114 · Fuselage Main, Structure
  > AFT FUSELAGE FLOOR STRUCTURE, BETWEEN FR67+300 MM & FR 67+ 480 MM, Y1160 MM LONGITUDINAL BEAMS CORRODED. REPLACED LONGITUDINAL BEAMS IAW SRM 51-41-03A, FIG 303, ITEMS 195A AND 190A INSTALLED IAW DWG D534 72780, ISSUE D, ITEMS 42, & 44. DWG D53472088, ISSUE F
- [SDR DALA2026012200480](https://openairdocs.org/sdr/DALA2026012200480.md): Beam · corroded · Jan 19, 2026 · N349NB · Airbus A319114 · Fuselage Main, Structure
  > AFT FUSELAGE FLOOR STRUCTURE AT FR 66+160 MM AT Y765 MM, LONGITUDINAL BEAM CORRODED. REPLACED LONGITUDINAL BEAM IAW SRM 51-72-11-911-001, REV 155, DWG D53472780, ISSUE H, & DWG D53472815, ISSUE E. (LP: 1409456)
- [SDR DALA2026011700389](https://openairdocs.org/sdr/DALA2026011700389.md): Not Reported · not reported · Jan 15, 2026 · N349NB · Airbus A319114 · Standard Practices/Structures
  > ER/A 631013-14AD ISSUED FOR REPAIR 80VU RACK LOWER LATERAL FITTI NGS. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 19500 FROM SECTION I AND EVERY 1000FC THEREAFTER. ASSOCIATED AA 2515-01014 ADDED FOR AC 3149. (LP: 1403132)
- [SDR DALA2026011500364](https://openairdocs.org/sdr/DALA2026011500364.md): Seat Track · corroded · Jan 14, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE PAX CABIN FLOOR STRUCTURE SEAT TRACK LOCATED AT FR 20 -Y1292 WITH CORROSION. REPLACED SEAT TRACK AT UPPER FUSELAGE FR20 - Y1292 IAW SRM 51-72-11-911-001 REV 155, & DRAWING D53112812 ISSUE E, D53110920 ISSUE E00, D53110984 ISSUE B AND D53918122
- [SDR DALA2026011500363](https://openairdocs.org/sdr/DALA2026011500363.md): Seat Track · corroded · Jan 14, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE, PAX CABIN FWD ENTRY AREA, SEAT TRACK +Y765 LOCATED AT FRAME 20 WITH CORROSION. REPLACED SEAT TRACK AT FR20 +Y765 IAW A319 SRM 51-72-11-911-001 REV 155, AND DRAWING D53112812 ISSUE E, D53110920 ISSUE E00 AND ISSUE D AND D53110984 ISSUE B. (LP:
- [SDR DALA2026011500362](https://openairdocs.org/sdr/DALA2026011500362.md): Seat Track · corroded · Jan 14, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE, PAX CABIN FWD ENTRY AREA, SEAT TRACK -Y765 LOCATED AT FRAME 20 WITH CORROSION. REPLACED SEAT TRACK AT FR20 -Y765 IAW SRM 51-72-11-911-001, REV: 155. AND AIRBUS DRAWING D531 12812 ISSUE E, D531 10984 ISSUE B, D5311 10920 ISSUE E00 AND D539 18
- [SDR DALA2026011500361](https://openairdocs.org/sdr/DALA2026011500361.md): Access Panel · corroded · Jan 14, 2026 · N349NB · Airbus A319114 · Aerodynamic Fairings
  > TAIL CONE ACCESS PANEL NUMBER 317AL INTERNAL ANGLES WITH CORROSION. REPLACED TAIL CONE ACCESS PANEL 317AL INTERNAL ANGLES (2EA) IAW SRM 51-72-11-911-001 PARAG 2C REV 155, AND AIPC 53-58-04-05B SHEET 1 & 2 DETAIL H & J, REV 133.01, AND AIRBUS REFERENCE DWG D92
- [SDR DALA2026011500356](https://openairdocs.org/sdr/DALA2026011500356.md): Receptacle · corroded · Jan 12, 2026 · N349NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > ENGINE NR 1 PYLON SPIGOT RECPTACLE AND SPIGOT BALL JOINT WITH CORROSION. REPLACED LOWER SPIGOT FITTING OF PYLON NR 1 IAW SRM TASK 54- 51-12-300-001, REV 155, AND REPLACED PYLON SPIGOT BALL JOINT IAW AMM TASK 54-51-41-000-001-A, PARAG 4C, AND TASK 54-51-41-400
- [SDR DALA2026011500355](https://openairdocs.org/sdr/DALA2026011500355.md): Floor Support · corroded · Jan 12, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > UPPER FUSELAGE PAX CABIN, AFT ENTRY AREA FR68 -Y1200 FLOOR SUPPORT ANGLE WITH CORROSION. REPLACED FLOOR SUPPORT ANGLE (BEAM - LONGITUDINAL) AND COUPLING (SECTION - CONNECTING) AT FR68 -Y1200 IAW SRM 51-72-11-911-001 REV: 155, AND DRAWINGS D534 72780 ISSUE D A
- [SDR DALA2026011500354](https://openairdocs.org/sdr/DALA2026011500354.md): Web · corroded · Jan 12, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE INTERNAL FLOOR STRUCTURE BETWEEN FR 68 AND FR 69 AT STGR 23R, WEB WITH CORROSION. REPLACED WEB (SHEET SHEAR) LOCATED BETWEEN FR68 AND FR69 STGR 23 IAW SRM 51-72-11-911-001 REV 155, AND DRAWINGS D53474250, ISSUE L, AND D53480505 ISSUE EU. (LP: 13
- [SDR DALA2026011500353](https://openairdocs.org/sdr/DALA2026011500353.md): Seat Track · corroded · Jan 12, 2026 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE, PAX CABIN, LT SIDE FR16 Y1292 SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK UPPER FUSELAGE LT FR 16 Y1292 IAW SRM 51-72-11-911-001 REV 155, AND DRAWING D53112812 ISSUE E, D53918122, ISSUE A, D53110920 ISSUE E00 AND D531 10984 ISSUE B. (LP: 1
- [SDR DALA2026011200258](https://openairdocs.org/sdr/DALA2026011200258.md): Receptacle · corroded · Jan 11, 2026 · N349NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE PYLON SPIGOT RECPTACLE AND SPIGOT BALL JOINT CORRODED. REPLACED BALL AND RECEPTACLE IAW SRM 54-51-12-300-001 AND AMM 54 -51-41/400. (LP: 1397020)
- [SDR DALA2026011200257](https://openairdocs.org/sdr/DALA2026011200257.md): Receptacle · corroded · Jan 11, 2026 · N349NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > NR 2 ENGINE, PYLON SPIGOT RECEPTACLE AND SPIGOT BALL JOINT CORRODED. REPLACED BALL AND RECEPTACLE IAW SRM 54-51-12-300-001 AND AMM 54 -51-41/400. (LP: 1397017)
- [SDR DALA2026011100248](https://openairdocs.org/sdr/DALA2026011100248.md): Floor Support · corroded · Jan 10, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LOWER FUSELAGE FWD CARGO COMPT, BETWEEN FR 30-34, CENTER FLOOR PROFILE WITH CORROSION, LOOSE RIVETS AND ANCHORNUTS DAMAGE, LH SIDE. REPLACED PROFILES IAW A319 SRM TASK 51-72-11-911-001 PARAG 2 REV 155.00 DATED 17/NOV/25 AND AIRBUS DWG D539-20040 ISUUE A. (LP:
- [SDR DALA2026010900197](https://openairdocs.org/sdr/DALA2026010900197.md): Shear Web · corroded · Jan 6, 2026 · N349NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE INTERNAL FLOOR STRUCTURE BETWEEN FR 69 AND FR 70 AT STGR 23R, WEB WITH CORROSION. REPLACED SHEAR PLATE IAW SRM 53-41 -17-01A, FIGURE 001, ITEM 310-A REV 155 AND INSTALLED IAW DWG D534 74180, ISSUE U, SHEET 6. (LP: 1388591)
- [SDR DALA2025123009489](https://openairdocs.org/sdr/DALA2025123009489.md): Actuator · excess play · Dec 29, 2025 · N349NB · Airbus A319114 · Trailing Edge Flap Actuator
  > LEFT WING, INBD FLAP TRACK NR 1 POSITION, ACTUATOR LEVER WITH EXCESIVE PLAY. REPLACED THE LT FLAP TRACK NR 1 ACTUATOR IAW AMM 27-54-49-000 -001-A AND AMM TASK 27-54-49-400-001-A. (1375546)
- [SDR DALA2025122309347](https://openairdocs.org/sdr/DALA2025122309347.md): Web · corroded · Dec 22, 2025 · N349NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > UPPER FUSELAGE, PAX CABIN, RT FR 20 WEB CHANNEL CORRODED. R & R WEB IAW SRM 51-72-11-911-001. (1364464).
- [SDR DALA2025122309346](https://openairdocs.org/sdr/DALA2025122309346.md): Dummy Rail · corroded · Dec 22, 2025 · N349NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER FUSELAGE, PAX CABIN, RH SIDE FR 16 Y-81 DUMMY RAIL CORRODED. R & R THE DUMMY RAIL IAW SRM 51- 72-11-911-001. (1363951).
- [SDR DALA2025050903588](https://openairdocs.org/sdr/DALA2025050903588.md): Skin · dented · May 6, 2025 · N349NB · Airbus A319114 · Leading Edge Devices
  > SHIP 3149 DISC: BIRD STRIKE RIGHT WING #4 SLAT LEADING EDGE. C/A: FOUND #4 SLAT LEADING EDGE DENTED. DEPTH MEASURES 0.277 PER A319 SRM 57-41-11-283-005, OUT OF LIMITS & REQUIRES AIRBUS SUPPORT. STARTED REMOVAL OF #4 SLAT PER A319 AMM 27-84 STEP 3(D)2 (B). REMO
- [SDR DALA2025022301382](https://openairdocs.org/sdr/DALA2025022301382.md): Cover · unsecure · Feb 22, 2025 · N349NB · Airbus A319114 · Emergency Lighting
  > SHIP 3149 DISC: SERVICE CHECK NOTED EMERGENCY ESCAPE PATH LIGHTING AT SEAT ROW 12 AND13 INOP. C/A: PLASTIC COVER AROUND LAMP AT ROW 12 KNOCKED LOOSE ALONG WITH BROKEN WIRE AT CONNECTOR - RESECURED LAMP HOUSING AND REPAIRED WIRE REF. ESPM 20-48, RELAMPED AT ROW
- [SDR DALA2024091609071](https://openairdocs.org/sdr/DALA2024091609071.md): Door · cracked · Sep 12, 2024 · N349NB · Airbus A319114 · Fluid Service Doors
  > SHIP 3149 REFUEL PNL DOOR BELLY FAIRING MOUNTED CRACKED. CORRECTIVE ACTION: REPLACED THE BELLY MOUNTED REFUEL PANEL MPN D5331034701200 IAW A319 AMM 52-42. (5538565)
- [SDR DALA2024083008589](https://openairdocs.org/sdr/DALA2024083008589.md): Battery · inoperative · Aug 29, 2024 · N349NB · Airbus A319114 · Emergency Lighting
  > SHIP 3149 L-2 DOOR EXIT LIGHT INOP. CORRECTIVE ACTION: REPLACED EPSU W-13 AND BATTERY PACK REF A/B 319 AMM 33-51 ALL TESTS GOOD. (5538520)
- [SDR DALA2024081308081](https://openairdocs.org/sdr/DALA2024081308081.md): Skin · gouged · Aug 12, 2024 · N349NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3149 GOUGE LEADING EDGE EXTERNAL SKIN LOCATED AT LEVEL RIB 12 ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 619738-14. (0498177)
- [SDR DALA2024081308080](https://openairdocs.org/sdr/DALA2024081308080.md): Retainer · corroded · Aug 12, 2024 · N349NB · Airbus A319114 · Buffet/Galleys
  > SHIP 3149 GALLEY G1 WORKDECK LOWER SKIN TROLLEY RETAINER AREA CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A # 619696-14. (0497584)
- [SDR DALA2024081308079](https://openairdocs.org/sdr/DALA2024081308079.md): Plate · cracked · Aug 12, 2024 · N349NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3149 DOORS FWD PAX/CREW DOOR 841 UPPER PLATE CRACK. CORRECTIVE ACTION: REPAIRED PER ER/A # 620014-14. (0497506)
- [SDR DALA2024081308077](https://openairdocs.org/sdr/DALA2024081308077.md): Frame · cracked · Aug 12, 2024 · N349NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3149 CRACK INDICATION FOUND IN OPEN FASTENER HOLE 7 LOCATED ON FRAME 16L JO GGLE AREA. CORRECTIVE ACTION: CRACK INDICATIONS WERE FOUND AFFECTING FR16LH DOUBLE JOGGLE HOLES #7, #A & #19. (0497473)
- [SDR DALA2024081308076](https://openairdocs.org/sdr/DALA2024081308076.md): Roller · excess play · Aug 11, 2024 · N349NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3149 EXCESSIVE PLAY ON CRUISE ROLLER ON O/B FLAP, RH AND LH WING 2. CORRECTIVE ACTION: REMOVED AND REPLACED CRUISE ROLLER ON O/B FLAP, RH AND LH WING 2 (E/A) AS PER AIRBUS CMM 57-53-21. (0495627)
- [SDR DALA2024081208002](https://openairdocs.org/sdr/DALA2024081208002.md): Frame · cracked · Aug 10, 2024 · N349NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3149 FUSELAGE FRAME/FORMERS FR16RH AT DOOR STOP #1 & #7 LEVEL DOUBLE JOGGLE CRACK INDICATIONS WERE FOUND AFFECTING HOLE #5. CORRECTIVE ACTION: REPAIRED PER ERA 619634-14AD. (0494945)

Next page: https://openairdocs.org/aircraft/N349NB/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 = 'N349NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N349NB/reports

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