# Service difficulty reports: N343NB

A list on [N343NB](https://openairdocs.org/aircraft/N343NB.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 5 · 223 reports

- [SDR DALA2026092705359](https://openairdocs.org/sdr/DALA2026092705359.md): Lanyard · misinstalled · Sep 25, 2026 · N343NB · Airbus A319114 · Emergency Equipment
  > ALL FOUR CABIN DOORS (L1, R1, L2, R2) SURVIVAL KIT ATTACH LANYARDS INSTALLED BACKWARDS. C/A: REINSTALLED ATTACH LANYARD UPRIGHT & "LANYARD" NOW VISIBLE. REF A319 SVC CK. (LP: 8900283, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091005064](https://openairdocs.org/sdr/DALA2026091005064.md): Rudder · no discrepancy · Sep 8, 2026 · N343NB · Airbus A319114 · Rudder Structure
  > WEIGH RUDDER IAW AMDS WORKCARD 5540-01015-02. WEIGHED RUDDER IAW AMDS WORKCARD 5540-01015-02 AND IAW AMDS WORK CARD 2721-4001 FOR REMOVAL AND REINSTALL. NO FINDINGS NOTED. (LP: 1801737, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026083004890](https://openairdocs.org/sdr/DALA2026083004890.md): Wire Harness · faulted · Aug 30, 2026 · N343NB · Airbus A319114 · Landing Gear System Wiring
  > GO-AROUND, AFTER GEAR EXTENSION, LT MAIN INDICATOR LIGHT DISPLAYED UNLK WITH NO GREEN TRIANGLE. WHEEL PAGE ON ECAM DISPLAYED RED TRIANGLE ON THE LEFT SIDE OF LT MAIN GEAR & GREEN TRIANGLE ON THE RT. ON LANDING ROLLOUT GOT L/G SYSTEM DISAGREE ECAM MESSAGE. LT
- [SDR DALA2026083004888](https://openairdocs.org/sdr/DALA2026083004888.md): Gcu · excess play · Aug 27, 2026 · N343NB · Airbus A319114 · Landing Gear Position and Warning
  > GO-AROUND, 2 FLIGHTS IN A ROW L/G SYS DISAGREE ON LANDING ROLLOUT. R & R LGCIU 2 IAW AMM 32-31. TEST OK. DURING INSPECTION OF 29GA PROX SENSOR, FOUND LINKAGE BETWEEN LT MLG DOOR BYPASS VALVE AND UPLOCK W/ EXCESSIVE PLAY W/ GEAR DOOR CLOSED AND MANIPULATING L
- [SDR DALA2026082004760](https://openairdocs.org/sdr/DALA2026082004760.md): Bonding Strap · corroded · Aug 19, 2026 · N343NB · Airbus A319114 · APU Exhaust System
  > LEVEL 2 CORROSION, EMPENNAGE, APU EXHAUST TAIL CONE, FR86 WERE FOUND BONDING ANGLE, FRAME AUXILIARY AND LOWER CHANNEL WITH CORROSION. REPLACED BONDING ANGLE P/N: D9248511520200, FRAME AUXILIARY P/N: D5248538220201 AND CHANNEL IAW SRM 51- 72-11-911-001, REV 15
- [SDR DALA2026081804713](https://openairdocs.org/sdr/DALA2026081804713.md): Keelbeam · cracked · Aug 17, 2026 · N343NB · Airbus A319114 · Fuselage Main, Keel
  > CENTER FUSELAGE LEFT KEEL BEAM BOTTOM PANEL, FR46 STR 37L, H4 AND H6 HOLES WITH CRACK INDICATIONS. REPAIRED IAW ER/A 636109-14AD. (1761870) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026081704695](https://openairdocs.org/sdr/DALA2026081704695.md): Strap · corroded · Aug 14, 2026 · N343NB · Airbus A319114 · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE SECTION BETWEEN RIB 24 AND RIB 26 LOWER SECTION STRAPS WITH CORROSION. REPLACED STRAPS (2EA) AT RH WING TRAILING EDGE SECTION BETWEEN RIB 24 AND RIB 26 IAW SRM TASK 51-72-11-911-001. (1756355) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026071304082](https://openairdocs.org/sdr/DALA2026071304082.md): Unknown · odor · Jul 12, 2026 · N343NB · Airbus A319114 · Air Distribution System
  > STRONG ODOR/FUMES OF ALCOHOL BLOWING FROM FO GASPER VENT, AFTER STARTING ENGINES. C/W NO GO ODI, COMPLETED AMDS W.C #0550-2002, NO FUMES OR ALCOHOL SMELL NOTED IN CP, CBN, CREW REPORTED LEVEL A, C/W LEVEL A INSP, NO OIL OR HYD LEAKS NOTED OR FOUND IN APU INTA
- [SDR DALA2026061103521](https://openairdocs.org/sdr/DALA2026061103521.md): Wire Harness · damaged · Jun 10, 2026 · N343NB · Airbus A319114 · Landing Gear System Wiring
  > DECLARED EMERGENCY DUE TO A LANDING GEAR DISAGREE MESSAGE AFTER GEAR EXTENSION FOR APPROACH. GEAR DOORS STAYED OPEN DUE TO A RT DOWN LOCK 14GA PROX SENSOR FAULT. ALL NORMAL AFTER SECOND GEAR EXTENSION. CORRECTIVE ACTION: FOUND SENSOR HARNESS STUCK BETWEEN SENS
- [SDR DALA2026042002475](https://openairdocs.org/sdr/DALA2026042002475.md): Unknown · unknown · Apr 20, 2026 · N343NB · Airbus A319114 · Flight Control System
  > ATB - DUE TO AIRCRAFT PITCHING UP WITH A/P OFF. REPLACED ACCELEROMETER UNIT 12CE4, THS ZERO ADJUSTMENT CHECK, AND ELEVATOR FREE PLAY CHECK. NTF, AND ALL OPS CHECK GOOD. (LP: 7729382). AIRCRAFT WAS GROUNDED.
- [SDR DALA2026020600880](https://openairdocs.org/sdr/DALA2026020600880.md): Unknown · odor · Feb 1, 2026 · N343NB · Airbus A319114 · Air Distribution System
  > AFTER LANDING THERE WAS A HINT OF SMELLY SCENT IN FLIGHT DECK AND CABIN. LASTED FOR ABOUT 1 MINUTE BEFORE DISSIPATING. VERY FAINT SMELL. C/W NO MSI WORK CARD 0550-2002, ENGINES AND APU CLEAN, NO ODORS IN THE CABIN AFTER RUNNING RECIRC FANS FOR 20 MIN. OK FOR
- [SDR DALA2026010600100](https://openairdocs.org/sdr/DALA2026010600100.md): Warning Message · illuminated · Jan 5, 2026 · N343NB · Airbus A319114 · Central Warning
  > ATO - AT THROTTLE UP DUE TO A F/CTL GND SPLR 5 FAULT ECAM WARNING MESSAGE. RESET SYSTEM WITH MCC AND CONTINUED. (LP: 6590614)
- [SDR DALA2025121209083](https://openairdocs.org/sdr/DALA2025121209083.md): Apu · contaminated · Dec 11, 2025 · N343NB · Airbus A319114 · APU Core Engine
  > VERY STRONG DIRTY SOCK/MUSTY ODOR AFTER APU TURNED ON AND PACKS TURNED ON. A/C WAS ON EXT AIR W/ APU OFF WHEN WE ARRIVED. ODOR STARTED AFTER APU TURNED ON. PERFORMED GVI OF APU INLET. FOUND PUDDLE OF DEICE FLUID UNDER BULKHEAD DRAIN AND APU INLET CLEANED. PE
- [SDR DALA2025111808441](https://openairdocs.org/sdr/DALA2025111808441.md): Secu · faulted · Nov 14, 2025 · N343NB · Airbus A319114 · Drag Control System
  > ATO - AT 10KNTS DUE TO A F/CTL GND SPLR 5 FAULT ECAM WARNING MESSAGE. R & R SEC 2 IAW AMM 27-94. OPS NORMAL. EFCS 1 & EFCS 2 TEST NO FAULTS. (LP 7338020)
- [SDR DALA2025090506582](https://openairdocs.org/sdr/DALA2025090506582.md): Floor Panel · damaged · Sep 5, 2025 · N343NB · Airbus A319114 · Fuselage Floor Panel
  > FWD CARGO FLOOR PANEL FOUND DAMAGED. COMPLIED WITH ER/A 587849-14TR. (7781763).
- [SDR DALA2025082006235](https://openairdocs.org/sdr/DALA2025082006235.md): O-Ring · leaking · Aug 19, 2025 · N343NB · Airbus A319114 · Hydraulic System, Main
  > DURING CRUISE, GOT ECAM HYD B RSVR LOW LEVEL. HYD SYS PAGE SHOWS FLUID LEVEL BELOW THE LOW LEVEL LIMIT. R&R O-RING PER A319 AMM 29-12-42. OP-CHECK LEAK CHECK NORMAL. OK FOR SVC. (7781718)
- [SDR DALA2025080105787](https://openairdocs.org/sdr/DALA2025080105787.md): Retainer · cracked · Jul 31, 2025 · N343NB · Airbus A319114 · Buffet/Galleys
  > CRACK ON BOTH GALLEY RETAINING BLOCKS ON COMPARTMENT OF 510M ON UPPER BLOCKS. REMOVED AND REPLACED RETAINING BLOCKS REF CMM PMC 68353751021-4050G-00001-01.
- [SDR DALA2025080105788](https://openairdocs.org/sdr/DALA2025080105788.md): Retainer · cracked · Jul 30, 2025 · N343NB · Airbus A319114 · Buffet/Galleys
  > CRACK ON BOTH GALLEY RETAINING BLOCKS ON COMPARTMENT OF 511M ON UPPER BLOCKS BOTH MEASURING OVER 4 IN ALONG WITH BLOCK PANEL DELAMINATING. REMOVED AND REPLACED RETAINING BLOCKS REF CMM PMC 68353751021-4050G-00001-01. REPAIRED DELAMINATION REF A319 SRM 51-77-1
- [SDR DALA2025060904396](https://openairdocs.org/sdr/DALA2025060904396.md): Fairing · delaminated · Jun 8, 2025 · N343NB · Airbus A319114 · Aerodynamic Fairings
  > SHIP 3143 FOUND WING TO BODY PANEL 192AB DELAMINATION ON WALKAROUND. CORRECTIVE ACTION: REMOVED AND REPLACED PANEL 192AB IAW A319 AMM 53-25-11. (7558541).
- [SDR DALA2025041102798](https://openairdocs.org/sdr/DALA2025041102798.md): None · none · Apr 7, 2025 · N343NB · Airbus A319114 · Standard Practices/Structures
  > SHIP 3143 DISC: THE LOG PAGE INCORPORATES STAGE 2 DTE THRESHOLD FOR ER/A 557100- 14, REV. E. C/A: COMPLY WITH ER/A 557100-14, REV. E THAT REQUIRES ADDITIONAL ENGINEERING APPROVAL TO OPERATE AIRCRAFT BEYOND 65,470 FLIGHT CYCLES OR 129,193 FLIGHT HOURS. ASSOCIAT
- [SDR DALA2025010700138](https://openairdocs.org/sdr/DALA2025010700138.md): Anti-Ice Valve · failed · Jan 6, 2025 · N343NB · Airbus A319114 · Airfoil Anti/De-ice System
  > SHIP 3143 - DIV - TO JFK DUE THE LT WING ANTI-ICE VALVE FAILURE. CORRECTIVE ACTION: REPLACED LEAKING LT ENGINE BLEED OVERPRESSURE VALVE. (LP 6957080, 0746898)
- [SDR DALA2024121211666](https://openairdocs.org/sdr/DALA2024121211666.md): Seat Track · corroded · Dec 11, 2024 · N343NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3143 CORROSION SEAT TRACK +Y1292 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y1292 AND FASTENERS LOC BTW FR64 TO FR66 AS PER A319 SRM 51-42-11 AND SRM 51-72-11.
- [SDR DALA2024110410605](https://openairdocs.org/sdr/DALA2024110410605.md): Pin · obstructed · Oct 30, 2024 · N343NB · Airbus A319114 · Doors
  > SHIP 3143 FA REPORTED DOOR PIN AT DOOR 2L DOES NOT STAY IN PLACE. CORRECTIVE ACTION: REMOVED DEBRIS AS REQUIRED PER AMM 29-63. (0636971)
- [SDR DALA2024102110249](https://openairdocs.org/sdr/DALA2024102110249.md): Access Door · cracked · Oct 20, 2024 · N343NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3143 CRACK ACCESS DOOR 172AR AROUND AFT HINGE AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 615217-14. (0619050)
- [SDR DALA2024102110248](https://openairdocs.org/sdr/DALA2024102110248.md): Hinge Fitting · cracked · Oct 20, 2024 · N343NB · Airbus A319114 · Fuselage, Door Hinge
  > SHIP 3143 CRACK INDICATION FOUND ON MLG AFT FACE AFT LUG FWD HINGE FITTING LH S IDE. CRACK LENGTH:0.250 INCH APPROX. CORRECTIVE ACTION: COMPLIED WITH ER/A 619993-14AD. (0619061)
- [SDR DALA2024102110246](https://openairdocs.org/sdr/DALA2024102110246.md): Window Post · cracked · Oct 20, 2024 · N343NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3143 CRACK INDICATION FOUND ON WINDSHIELD CENTER POST. CRACK DIRECTION 1 OC LOCK AND 5 OCLOCK. CORRECTIVE ACTION: COMPLIED WITH ER/A 619897-14AD. (0619008)
- [SDR DALA2024102110253](https://openairdocs.org/sdr/DALA2024102110253.md): Skin · corroded · Oct 19, 2024 · N343NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3143 CORROSION WAS FOUND ON THE LOWER SURFACE OF TOP SKIN PANEL 2, BETWEEN WX3494,5 - WX4010,2 AT THE TRAILING EDGE OVERHANG OF THE LEFT-HAND WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 619900-14. (0617492)
- [SDR DALA2024102110252](https://openairdocs.org/sdr/DALA2024102110252.md): Bracket · cracked · Oct 19, 2024 · N343NB · Airbus A319114 · Wing, Attach Fittings
  > SHIP 3143 CRACK OB FIXED LEADING EDGE BRACKET TELESCOPIC DUCT IB SIDE ON RH WIN G. CORRECTIVE ACTION: COMPLIED WITH ER/A 530598-14MA. (0617204)
- [SDR DALA2024102110242](https://openairdocs.org/sdr/DALA2024102110242.md): Skin · corroded · Oct 19, 2024 · N343NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3143 CORROSION INTERNAL SKIN MACHINED AREA AT LEVEL STR 42L AND BTW FR60 TO FR61 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ER/A 557100-14AD. (0617562)
- [SDR DALA2024102110243](https://openairdocs.org/sdr/DALA2024102110243.md): Skin · corroded · Oct 18, 2024 · N343NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3143 CORROSION DAMAGE WAS FOUND ON FUSELAGE SKIN PANEL BETWEEN FR58-61 AND STGR42-43LH. CORRECTIVE ACTION: REPAIR PER ERA 557100-14AD. (0615883)
- [SDR DALA2024101810193](https://openairdocs.org/sdr/DALA2024101810193.md): Deflector · cracked · Oct 18, 2024 · N343NB · Airbus A319114 · Cargo/Baggage Doors
  > SHIP 3143 THE DEFLECTOR OF THE DOOR 831 HAS BEEN FOUND AFFECTED WITH CRAK. CORRECTIVE ACTION: COMPLIED WITH ER/A 621462-14. (0614864)
- [SDR DALA2024101810197](https://openairdocs.org/sdr/DALA2024101810197.md): Access Panel · damaged · Oct 17, 2024 · N343NB · Airbus A319114 · Aerodynamic Fairings
  > SHIP 3142 HOLE ACCESS PANEL 192KB BELLY FAIRING ON EXISTING REPEIR LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 192KB BELLY FAIRING AT LOWER FUSELAGE AS PER ER/A 529512-14MA. (0614169)
- [SDR DALA2024101810196](https://openairdocs.org/sdr/DALA2024101810196.md): Support Angle · cracked · Oct 17, 2024 · N343NB · Airbus A319114 · Horizontal Stabilizer Miscellaneous Structure
  > SHIP 3143 CRACK SUPPORT ANGLE ELEVATOR HINGE ARM 5 ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE (1EA) ON ELEVATOR HINGE ARM 5 HORIZONTAL STABILIZER AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0613962)
- [SDR DALA2024101810194](https://openairdocs.org/sdr/DALA2024101810194.md): Spherical Bearin · corroded · Oct 17, 2024 · N343NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3143 CORROSION ON HOUSING SPHERICAL BEARING TRACK 3 O/B FLAP LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620734-14. (0614370)
- [SDR DALA2024101610128](https://openairdocs.org/sdr/DALA2024101610128.md): Stringer · corroded · Oct 15, 2024 · N343NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > SHIP 3143 CORROSION STRINGER 39L LOCATED BETWEEN FR30 TO FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIR ON STRG 39L LOC BTW FR30 TO FR35 IN FWD CARGO COMPARTMENT AS PER A319 SRM 53-21-13-300-018 AND PERFORMED BLEND OUT ON AFFECTED AREA AS PER A319 SR
- [SDR DALA2024101610127](https://openairdocs.org/sdr/DALA2024101610127.md): Support Fitting · excess play · Oct 15, 2024 · N343NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3143 EXCESSIVE PLAY FITTING SUPPORT LOC FR20 LH SIDE IN AFT AVIONIC COMPARTMENT. CORRECTIVE ACTION: REPLACED FITTING ASSY LOC. ON FR20 LH SIDE ON AFT AVIONIC COMPARTMENT AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0610886)
- [SDR DALA2024101410085](https://openairdocs.org/sdr/DALA2024101410085.md): Access Panel · cracked · Oct 13, 2024 · N343NB · Airbus A319114 · Nacelle/Pylon, Plate/Skin
  > SHIP 3143 CRACK ACCESS PANEL 423DL ON RH PYLON. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 423DL RH PYLON AS PER ER/A # 540187-14MA. (0607492)
- [SDR DALA2024101410083](https://openairdocs.org/sdr/DALA2024101410083.md): Fitting · corroded · Oct 13, 2024 · N343NB · Airbus A319114 · Wing Main, Frame Structure
  > SHIP 3143 CORROSION TRAILING EDGE FITTING LOCATED BTW RIB 7 TO RIB 8 ON LH WING. CORRECTIVE ACTION: REPLACED FITTING ON TRAILING EDGE LOCATED BTW RIB 7 TO RIB 8 ON LH WING AND FASTENERS AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0607442)
- [SDR DALA2024101009958](https://openairdocs.org/sdr/DALA2024101009958.md): Plate · corroded · Oct 9, 2024 · N343NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3143 CORROSION FOUND AT INB & OUTB PLATES TRACK #2, BEARING AT RIB 9 LEVEL. CORRECTIVE ACTION: REPAIR PER ERA 621041-14. (0600186)
- [SDR DALA2024101009957](https://openairdocs.org/sdr/DALA2024101009957.md): Bonding Strap · corroded · Oct 9, 2024 · N343NB · Airbus A319114 · Wing Main, Frame Structure
  > SHIP 3143 CORROSION ACCESS PANEL 531CB BONDING STRAP ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 531CB AS PER ER/A 620280-14. (0601050)
- [SDR DALA2024101009956](https://openairdocs.org/sdr/DALA2024101009956.md): Bonding Plate · corroded · Oct 9, 2024 · N343NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3143 CORROSION STATIC DISCHARGER PLATE-BONDING FLAP TRACK FAIRING 533CB ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 533CB AS PER ER/A 620280-14. (0601042)
- [SDR DALA2024101009955](https://openairdocs.org/sdr/DALA2024101009955.md): Bonding Strap · corroded · Oct 9, 2024 · N343NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3143 CORROSION FLAP TRACK FAIRING 633CB BONDING STRAP ON RH WING CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 633CB AS PER ER/A 620280-14 REV. (0601045)
- [SDR DALA2024101009954](https://openairdocs.org/sdr/DALA2024101009954.md): Bonding Plate · corroded · Oct 9, 2024 · N343NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3143 CORROSION STATIC DISCHARGER PLATE-BONDING FLAP TRACK FAIRING 532CB ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 532CB AS PER ER/A 620280-14. (0601037)
- [SDR DALA2024101009953](https://openairdocs.org/sdr/DALA2024101009953.md): Crossbeam · bent · Oct 9, 2024 · N343NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3143 BENT CROSS BEAM INTERNAL STRUCTURE LOCATED FR30 AND STR38L TO STR38R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED CROSSBEAM AND FASTENERS LOCATED FR30 AND STR38L TO STR38R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (
- [SDR DALA2024101009952](https://openairdocs.org/sdr/DALA2024101009952.md): Shear Tie · corroded · Oct 9, 2024 · N343NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > SHIP 3143 CORROSION SHEAR TIE LOCATED FR28 AND BETWEEN STR38L TO STR39L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE LOCATED FR28 AND BETWEEN STR38L TO STR39L IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0600953)
- [SDR DALA2024101009964](https://openairdocs.org/sdr/DALA2024101009964.md): Access Panel · damaged · Oct 9, 2024 · N343NB · Airbus A319114 · Horizontal Stabilizer, Plate/Skin
  > SHIP 3143 ELONGATED HOLE ACCESS PANEL 335AB ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON ACCESS PANEL 335AB AT LH HORIZONTAL STABILIZER AS PER ER/A 620628-14. (0601055)
- [SDR DALA2024101009963](https://openairdocs.org/sdr/DALA2024101009963.md): Access Panel · corroded · Oct 9, 2024 · N343NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3143 CORROSION ACCESS PANEL 631CB BONDING STRAP ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON FLAP TRACK FAIRING 631CB AS PER ER/A 620280-14. (0601048)
- [SDR DALA2024101009946](https://openairdocs.org/sdr/DALA2024101009946.md): Skin · corroded · Oct 8, 2024 · N343NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3143 CORROSION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LH WING. CORRECTIVE ACTION: REPAIR PER ERA 619900-14. (0598728)
- [SDR DALA2024101009945](https://openairdocs.org/sdr/DALA2024101009945.md): Rib · corroded · Oct 8, 2024 · N343NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3143 CORROSION FOUND AT OUTBD FLAP TRACK #3 INNER & OUTER RIB 5 AT ECCENTRIC BEARING. CORRECTIVE ACTION: REPAIR PER ERA 620734-14. (0598319)
- [SDR DALA2024100709766](https://openairdocs.org/sdr/DALA2024100709766.md): Bearing · excess play · Oct 6, 2024 · N343NB · Airbus A319114 · Ailerons
  > SHIP 3143 EXCESSIVE PLAY ON BEARING AILERON HINGE ARM 4 LH WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING (1 E/A) AND SLEEVE (1 E/A) ON HINGE ARM #4 AILERON ON LH WING, AS PER CMM 57-51-54. (0595636)

Next page: https://openairdocs.org/aircraft/N343NB/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 = 'N343NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N343NB/reports

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