# Service difficulty reports: N341NB

A list on [N341NB](https://openairdocs.org/aircraft/N341NB.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 · 213 reports

- [SDR DALA2026062503771](https://openairdocs.org/sdr/DALA2026062503771.md): Brake Assy · overheated · Jun 20, 2026 · N341NB · Airbus A319114 · Landing Gear Brake System
  > RIGHT SIDE LEFT INBOARD BRAKE TEMP 470 / 295 LEFT SIDE INBD & OTBD BRAKES 290/320. THIS OCCURRED ON LANDING BUT DURING TAKEOFF BRAKES TEMPS SHOW A VAST DIFFERENCE BETWEEN INBOARD AND OUTBOARD. INSP NBR 3 MLG BRAKE FOUND DRAGGING. REPLACED SAME PAR A319 AMM 3
- [SDR DALA2026050602891](https://openairdocs.org/sdr/DALA2026050602891.md): Bottle · low pressure · May 5, 2026 · N341NB · Airbus A319114 · Passenger/Crew Doors
  > DURING SERVICE CHK FOUND THE R2 DOOR ASSIST BOTTLE PRESSURE BELOW LIMITS. SERVICED R2 DOOR ASSIST BOTTLE WITH NOITROGEN IAW AMM 52-10 -00-610-801C1 (ALT PROCEDURE) NO LEAKS NOTED. OK FOR SERVICE. (LP: 8676291). AIRCRAFT WAS GROUNDED
- [SDR DALA2026011700393](https://openairdocs.org/sdr/DALA2026011700393.md): Unknown · fumes · Jan 15, 2026 · N341NB · Airbus A319114 · Air Distribution System
  > F/A REPORTED FUMES EVENT AFTER LANDING IN CABIN, SMELLED ELECTRICAL ODOR AND CABIN WAS HAZY, NO REPORTS IN COCKPIT. PERFORMED NO GO ODI, MSI PREVENTION PROGRAM ATA 21-72 SMOKE/ FUMES AND COMPLETED W/C 0550-2002 STEPS 1-4, INCLUDING TYPE 9 ELEC. SMOKE/ODOR IN
- [SDR DALA2025082106240](https://openairdocs.org/sdr/DALA2025082106240.md): Skin · dented · Aug 20, 2025 · N341NB · Airbus A319114 · Trailing Edge Flaps
  > FOUND DENT ON RT INBD FLAP. ACTION: PER ER/A 628685-14 (7589627)
- [SDR DALA2025081306066](https://openairdocs.org/sdr/DALA2025081306066.md): Unknown · odor · Aug 13, 2025 · N341NB · Airbus A319114 · Air Distribution System
  > CAPT AND F/O ALL OF A SUDDEN BOTH NOTICED A STRONG SULFER/ROTTEN EGG SMELL. INSP APU COMPARTMENT NO DEFECTS NOTED. RAN PACK NO ODOR DETECTED. C/W W/C 0550-2002.
- [SDR DALA2025060304252](https://openairdocs.org/sdr/DALA2025060304252.md): Pin · damaged · Jun 2, 2025 · N341NB · Airbus A319114 · Emergency Equipment
  > SHIP 3141 SLIDE DISARMING PIN ATTACHING LANYARD MISSING OR DAMAGED. CORRECTIVE ACTION: FOUND ALL LANYARD SLIDE DISARMING PINS INTACT NO PROBLEMS NOTED. (1001902).
- [SDR DALA2025050103353](https://openairdocs.org/sdr/DALA2025050103353.md): Skin · contaminated · Apr 29, 2025 · N341NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3141 DISC: AIRCRAFT EXTERIOR EXPOSED TO FIRE FIGHTING FOAM. C/A: AIRCRAFT EXTERIOR CLEANED IAW PROCESS STANDARD 900-1-2-1 NO 4. (LP: 7081240)
- [SDR DALA2025041702981](https://openairdocs.org/sdr/DALA2025041702981.md): Valve · faulted · Apr 14, 2025 · N341NB · Airbus A319114 · Cabin Temperature Control System
  > SHIP 3141 - ATB - DUE TO CABIN TEMP BEING UNCONTROLLABLE. FWD TRIM AIR SYS WAS ALREADY ON MEL. CORRECTIVE ACTION: REPLACED TRIM AIR PRV, AND TRIM AIR VALVE, PACK 1 REHEATER, CONDENSER, AND TEMP SENSORS DUE TO INDICATION. PACK 1 AND 2 FLOW CONTROL VALVES REPLAC
- [SDR DALA2025040802687](https://openairdocs.org/sdr/DALA2025040802687.md): Oxygen Mask · unwanted deploy · Apr 5, 2025 · N341NB · Airbus A319114 · Passenger Oxygen System
  > SHIP 3141 DISC: OXYGEN PANEL MASK DEPLOYED. C/A: VERIFIED AFT LEFT LAV OXYGEN MASK PNL DEPLOYED. REQUIRES MEL 32- 21-02. ACCOMPLISHED "M" PROCEDURE. RECEIVED MCC DISP APPR. PLACARD INSTALLED. R/R AFT LAV O2 CONTAINER ASSY PER A319 AMM 35-21. OK FOR SVC. MEL &
- [SDR DALA2025040402553](https://openairdocs.org/sdr/DALA2025040402553.md): Elec Connector · corroded · Apr 1, 2025 · N341NB · Airbus A319114 · Flight Control System Wiring
  > SHIP 3141 DISC: CORROSION TRAILING EDGE ELECTRICAL CONNECTOR ON WING TIP BRAKE LOCATED BETWEEN RIB15 TO RIB16 ON RH WING. C/A: REPLACED ELECTRICAL CONNECTOR OF WING TIP BRAKE ON TRAILING EDGE RH WING AS PER A320 FAM AWM 27-51-14, AIRBUS ESPM 20-44-11-0101, PER
- [SDR DALA2025040402551](https://openairdocs.org/sdr/DALA2025040402551.md): Fitting · cracked · Apr 1, 2025 · N341NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3141 DISC: CRACK INDICATION WAS FOUND IN CONTINUITY FITTING RH SIDE LOCATED ON FRAME 2 ON COCKPIT, CRACK LENGHT IS 0.100 INCHES APROX CRACK DIRECTION 6 O CLOCK AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISH
- [SDR DALA2025033002338](https://openairdocs.org/sdr/DALA2025033002338.md): Flap Track · corroded · Mar 28, 2025 · N341NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3141 DISC: *DTE* DURING M2 AND WHILE ACCOMPLISHING JIC 2750-1020-LT CORROSION WAS FOUND IN TRACK #3, RIB #5 INB'D AND OUTB'D FACES OF RIB 5 BORE. DTE REQUIRED PER SECITON DTE OF 624541-14, THE REPAIR OF SECTION I IS LIMITED TO 97,976 FC FROM SECTION I. A
- [SDR DALA2025032802325](https://openairdocs.org/sdr/DALA2025032802325.md): Skin · corroded · Mar 27, 2025 · N341NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3141 CORROSION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 624232-14. (0881688)
- [SDR DALA2025100207189](https://openairdocs.org/sdr/DALA2025100207189.md): Skin · corroded · Mar 26, 2025 · N341NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > CORROSION INTERNAL SKIN LOCATED AT LEVEL FR20 AND BETWEEN STR28L TO STR29L IN LATERAL AVIONIC COMP LH. REPAIRED PER ER/A 624546-14. (0879376)
- [SDR DALA2025100207188](https://openairdocs.org/sdr/DALA2025100207188.md): Skin · corroded · Mar 26, 2025 · N341NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > CORROSION INTERNAL SKIN LOCATED AT LEVEL FR16 AND BETWEEN STR28L TO STR29L IN LATERAL AVIONIC COMP LH. REPAIRED PER ER/A 624546-14. (0879365)
- [SDR DALA2025032702276](https://openairdocs.org/sdr/DALA2025032702276.md): Skin · chafed · Mar 26, 2025 · N341NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3141 CHAFING MARKS ON EXTERNAL FUSELAGE SKIN PANEL AT FR34 BTW STR 43 LH AND 43 RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 624730-14AD. (0879393)
- [SDR DALA2025032702275](https://openairdocs.org/sdr/DALA2025032702275.md): Skin · corroded · Mar 25, 2025 · N341NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3141 CORROSION FOUND ON INTERNAL SURFACE OF FUSELAGE SKIN PANEL BETWEEN FR15-FR21 AT LATERAL STR ON THE LHS. CORRECTIVE ACTION: REPAIRED PER ER/A 624546-14. (0876789)
- [SDR DALA2025032702274](https://openairdocs.org/sdr/DALA2025032702274.md): Skin · corroded · Mar 25, 2025 · N341NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3141 DURING M2 AND WHILE INSPECTING PER 5320-3013, CORROSION FOUND ON INTERNAL SURFACE OF FUSELAGE SKIN PANEL BETWEEN FR15-FR21 AT LATERAL STR ON THE LHS. CORRECTIVE ACTION: COMPLIED WITH ER/A 624546-14. (0876782)
- [SDR DALA2025032702272](https://openairdocs.org/sdr/DALA2025032702272.md): Plate · damaged · Mar 25, 2025 · N341NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3141 DURING M2 AND WHILE ACCOMPLISHING JIC 2750-1020-RT CORROSION FOUND IN OB ALUMINUM PLATE (FACE AND BORE) AT TRACK #3 IN OUTER RIB 5 ECCENTRIC BEARING AREA ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 624731-14. (0875905)
- [SDR DALA2025032702273](https://openairdocs.org/sdr/DALA2025032702273.md): Support · corroded · Mar 24, 2025 · N341NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3141 DURING M2 AND WHILE INSPECTING PER JIC 2750-1020-LT CORROSION FOUND IN PENDULUM SUPPORT, INB'D AND OUTB'D LUG BORES OUTER FACE OF OUTB'D LUG AT FLAP TRACK #4 OF OUTB'D FLAP ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 31-624475. (0875434)
- [SDR DALA2025032202147](https://openairdocs.org/sdr/DALA2025032202147.md): Rib · corroded · Mar 20, 2025 · N341NB · Airbus A319114 · Elevator, Spar/Rib
  > SHIP 3141 DISC: CORROSION ELEVATOR O/B RIB ON RH HORIZONTAL STABILIZER. C/A: EPLACED OB RIB 10 ELEVATOR ON RH HORIZONTAL STABILIZER AS PER A319 SRM 55-21-12-300-002 AND A319 SRM 51-42-11 AND A319 SRM 51-72-11. (LP: 0868194)
- [SDR DALA2025032002101](https://openairdocs.org/sdr/DALA2025032002101.md): Seat Track · corroded · Mar 19, 2025 · N341NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3141 DISC: CORROSION SEAT TRACK +Y1292 LOCATED BETWEEN FR64 TO FR66 AT AFT GALLEY AREA (SSI 534147). C/A: REPLACED SEAT TRACK Y1292,LOC BETWEEN FR64 TO FR66 STR23L AFT GALLEY AREA AS PER A319 SRM 51-42-11,A319 SRM 51-72-11 AND NATDWG-10N01048 RELEASE. (LP
- [SDR DALA2025032002100](https://openairdocs.org/sdr/DALA2025032002100.md): Rib · corroded · Mar 19, 2025 · N341NB · Airbus A319114 · Elevator, Spar/Rib
  > SHIP 3141 DISC: CORROSION OB RIB ELEVATOR ON LH HORIZONTAL STABILIZER. C/A: REPLACED OB RIB 10 ELEVATOR ON LH HORIZONTAL STABILIZER AS PER A319 SRM 55-21-12-300-002 AND A319 SRM 51-42-11 AND A319 SRM 51-72-11. (LP: 0866709)
- [SDR DALA2025031501996](https://openairdocs.org/sdr/DALA2025031501996.md): Angle · cracked · Mar 13, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CRACK ON TI-ANGLE LOC FR42 RH SIDE HYDRAULIC COMPARTMENT LOWER FUSELAGE AD 19-08-07 REQUIRED PRIOR TO FURTHER FLIGHT AA CARD 5353-01006-02. C/A: REPLACED OF TI-ANGLE LOC FR42 RH SIDE ON HYDRAULIC COMPARTMENT LOWER FUSELAGE IS PCW ON AA CARD 535
- [SDR DALA2025031602004](https://openairdocs.org/sdr/DALA2025031602004.md): Access Panel · eroded · Mar 11, 2025 · N341NB · Airbus A319114 · Aerodynamic Fairings
  > SHIP 3141 EROSION ACCESS PANEL 191BB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 542077-14TR. (0851374)
- [SDR DALA2025031001800](https://openairdocs.org/sdr/DALA2025031001800.md): Seat Track · corroded · Mar 9, 2025 · N341NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3141 DISC: CORROSION SEAT TRACK -Y765 LOCATED BETWEEN FR12 TO FR24 FWD GALLEY AREA (SSI 531189). C/A: REPLACED SEAT TRACK -Y765 LOCATED BETWEEN FR12 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG:D53110984, DWG:D53918123, DWG: D5
- [SDR DALA2025031001799](https://openairdocs.org/sdr/DALA2025031001799.md): Floor Support · corroded · Mar 7, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION FLOOR BEAM -Y1292 LOCATED BETWEEN FR12 TO FR24 FWD GALLEY AREA (SSI 531189). C/A: REPLACED FLOR BEAM -Y1292, LOC BTW FR 12 TO FR 24 FWD GALLEY AREA AS PER A319 SRM 51-42-11, AND A319 SRM 51-72-11 DWG: D53112812 AND DWG D53135202. (LP:
- [SDR DALA2025031001797](https://openairdocs.org/sdr/DALA2025031001797.md): Floor Support · corroded · Mar 7, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION FLOOR BEAM -Y254 LOCATED BETWEEN FR12 TO FR24 FWD GALLEY AREA (SSI 531189). C/A: REPLACED FLOOR BEAM -Y254 LOCATED BETWEEN FR12 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-72-11; A319 SRM 51-42-11 AND DWG D53111462 AND D53110984. (LP:
- [SDR DALA2025031001798](https://openairdocs.org/sdr/DALA2025031001798.md): Seat Track · corroded · Mar 6, 2025 · N341NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3141 DISC: CORROSION SEAT TRACK +Y1292 LOCATED FROM FR12 TO FR24 AT FWD GALLEY AREA (SSI: 531189). C/A: REPLACED SEAT TRACK Y1292 LOC FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 DWG 53112812 AND DWG D53110920. (LP: 084457
- [SDR DALA2025030601751](https://openairdocs.org/sdr/DALA2025030601751.md): Seat Track · corroded · Mar 5, 2025 · N341NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3141 DISC: CORROSION SEAT TRACK +Y765 LOCATED FROM FR12 TO FR24 AT FWD GALLEY AREA (SSI: 531189). C/A: REPLACED SEAT TRACK Y765 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11; A319 SRM 51-42-11 AND DWG D53110984, DWG D53112812 AND DWG D5
- [SDR DALA2025030601750](https://openairdocs.org/sdr/DALA2025030601750.md): Floor Support · corroded · Mar 5, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION FLOOR BEAM -Y189 LOCATED BETWEEN FR20 TO FR24 FWD GALLEY AREA (SSI 531189). C/A: REPLACED FLOOR BEAM -Y189 LOCATED BETWEEN FR20 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-42-11, SRM 51-72-11 AND DWG D53111406. (LP: 0842678)
- [SDR DALA2025030601749](https://openairdocs.org/sdr/DALA2025030601749.md): Dummy Rail · corroded · Mar 4, 2025 · N341NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3141 DISC: CORROSION RAIL DUMMY Y503.2 LOCATED FROM FR12 TO FR16 AT FWD GALLEY AREA (SSI: 531189). C/A: REPLACED RAIL DUMMY Y503.2 LOCATED FROM FR12 TO FR16 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11 A319 SRM 51-72-11 AND DWG:D53112639, DWG: D53110984 AN
- [SDR DALA2025030601748](https://openairdocs.org/sdr/DALA2025030601748.md): Seat Track · corroded · Mar 4, 2025 · N341NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3141 DISC: CORROSION SEAT TRACK +Y765 LOCATED BETWEEN FR64 TO FR66 AT AFT GALLEY AREA (SSI 534147). C/A: REPLACED SEAT TRACK Y765 LOC. BTW FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11; A319 SRM 51-72-11 AND NAT DWG 10N01048. (LP: 0841112)
- [SDR DALA2025030601747](https://openairdocs.org/sdr/DALA2025030601747.md): Web · corroded · Mar 4, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION WEB LOCATED BETWEEN FR20 AND STR23R FWD GALLEY AREA. C/A: REPLACED WEB LOCATED BETWEEN FR20 TO FR24 AND STR23R FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DRAWING-D53114332. (LP: 0841105)
- [SDR DALA2025030601746](https://openairdocs.org/sdr/DALA2025030601746.md): Web · corroded · Mar 4, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION WEB LOCATED BETWEEN FR16 AND STR23L FWD GALLEY AREA. C/A: REPLACED WEB LOCATED BETWEEN FR12 AND FR 16 AND STR23L FWD GALLEY AREA AS PER A319 SRM 51-42-11,A319 SRM 51-72-11 AND DRAWING-D53114392. (LP: 0841099)
- [SDR DALA2025030401659](https://openairdocs.org/sdr/DALA2025030401659.md): Web · corroded · Mar 3, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION WEB LOCATED BETWEEN FR20 AND STR23L FWD GALLEY AREA. C/A: REPLACED WED LOCATED BETWEEN FR20 TO FR24 STR23L AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWG-D53110920. (LP: 0839332)
- [SDR DALA2025030401658](https://openairdocs.org/sdr/DALA2025030401658.md): Stringer · corroded · Mar 3, 2025 · N341NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > SHIP 3141 DISC: CORROSION STRINGER 41R BTW FR 61 TO FR 63 AFT CARGO COMPARTMENT (SSI 534107). C/A: REPLACED STRINGER 41R BTW FR 61 TO FR 63 AFT CARGO COMPARTMENT AS PER A319 SRM 51-72-11 A319 SRM 51-42-11 AND DWG D53476324. (LP: 839325)
- [SDR DALA2025030401657](https://openairdocs.org/sdr/DALA2025030401657.md): Dummy Rail · corroded · Mar 3, 2025 · N341NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3141 DISC: CORROSION RAIL DUMMY -Y81 AND FR16 FWD GALLEY AREA (SSI: 531189). C/A: REPLACED RAIL DUMMY -Y81 AND FR12 TO FR16 FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG D53112829. (LP: 0839322)
- [SDR DALA2025030401656](https://openairdocs.org/sdr/DALA2025030401656.md): Floor Support · corroded · Mar 2, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION FLOOR BEAM Y1292-1162 LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA (SSI 534147). C/A: REPLACED FLOOR BEAM Y1292-1162 LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11,A319 SRM 51-72-11 AND DWG-D53472172. (LP:
- [SDR DALA2025030401655](https://openairdocs.org/sdr/DALA2025030401655.md): Floor Support · corroded · Mar 2, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION FLOOR BEAM +Y1162.5 LOCATED FROM FR68 TO FR69 AT AFT GALLE. C/A: REPLACED FLOOR BEAM Y1162.5 LOC. FROM FR68 TO FR69 AT AFT GALLEY AREA AND SPLICE (1E/A)LOC. FR68 AS PER A319 SRM 51-42-11; A319 SRM 51-72- 11 AND DWG D53472780. (LP: 083
- [SDR DALA2025030401654](https://openairdocs.org/sdr/DALA2025030401654.md): Floor Support · corroded · Mar 2, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION FLOOR BEAM -Y765 LOCATED BETWEEN FR66 TO FR70 AFT GALLEY AREA (SSI 534147). C/A: REPLACED FLOOR BEAM -Y765 LOCATED BETWEEN FR66 TO FR70 AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG D92495100. (LP: 0837298)
- [SDR DALA2025022801553](https://openairdocs.org/sdr/DALA2025022801553.md): Floor Support · corroded · Feb 26, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION FLOOR BEAM +Y765 LOCATED BETWEEN FR66 TO FR70 AT AFT GALLEY AREA (SSI 534147). C/A: REPLACED FLOOR BEAM Y765 LOCATED BETWEEN FR66 TO FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 DWG D53472815. (LP: 0830633)
- [SDR DALA2025022801552](https://openairdocs.org/sdr/DALA2025022801552.md): Bushing · out of limits · Feb 25, 2025 · N341NB · Airbus A319114 · Elevator Structure
  > OUT OF LIMIT INNER DIAMETER DIMENSION ON FIXED BUSHING OUTBOARD LUG HINGE N5 AT RH ELEVATOR. REPAIRED BORE AND REPLACED BUSHING (1 EA) ON HINGE FITTING #5 O/ B LUG AT RH ELEVATOR AS PER A319 SRM 55-26-41-300-004. (LP: 0828552)
- [SDR DALA2025022601482](https://openairdocs.org/sdr/DALA2025022601482.md): Dummy Rail · corroded · Feb 25, 2025 · N341NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3141 DISC: CORROSION RAIL DUMMY Y940 FROM FR14 TO FR16 AT FWD GALLEY AREA ( SSI: 531189). C/A: REPLACED RAIL DUMMY Y940 AND FASTENERS BETWEEN FR14 TO FR16 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11,SRM:51-72-11, DWG:D53112823 RELEASE DATE:14-MAR-03 ISSUE
- [SDR DALA2025022301381](https://openairdocs.org/sdr/DALA2025022301381.md): Floor Support · corroded · Feb 22, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION FLOOR BEAM -Y1162.5 FROM FR68 TO FR69 AT AFT GALLEY AREA (SSI: 534147). C/A: REPLACED FLOOR BEAM -Y1162.5 FROM FR68 TO FR69 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11,AS PER A319 SRM 51-72-11, AND DWG D53472089 RELEASE DATE: 12-DEC-
- [SDR DALA2025022301380](https://openairdocs.org/sdr/DALA2025022301380.md): Fitting · corroded · Feb 22, 2025 · N341NB · Airbus A319114 · Nacelle/Pylon, Attach Fittings
  > SHIP 3141 DISC: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. C/A: FINAL REPAIR RESOLUTION: CORRECTED FILL UP ADDITIONAL INFORMATION. REPLACED SPIGOT RECEPTACLE FITTING AND BALL JOINT-SPIGOT ON LH PYLON AS PER A319 SRM 54-51-12-300-001 CONFIG-1 (CFM56) AND
- [SDR DALA2025022301379](https://openairdocs.org/sdr/DALA2025022301379.md): Floor Support · corroded · Feb 22, 2025 · N341NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3141 DISC: CORROSION FLOOR BEAM - Y1292-1162 FROM FR66 TO FR68 AT AFT GALLEY AREA (SSI: 534147). C/A: REPLACED FLOOR BEAM - Y1292-1162 FROM FR66 TO FR68 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWG D53472780 RELEASE DATE 26-APR-1
- [SDR DALA2025022101353](https://openairdocs.org/sdr/DALA2025022101353.md): Receptacle · corroded · Feb 19, 2025 · N341NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > SHIP 3141 DISC: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. C/A: FINAL REPAIR RESOLUTION: CORRECTED FILL UP ADDITIONAL INFORMATION. REPLACED SPIGOT RECEPTACLE FITTING AND BALL JOINT-SPIGOT ON RH PYLON AS PER A319 SRM 54-51-12-300-001 CONFIG-1 (CFM56) AND
- [SDR DALA2025021801184](https://openairdocs.org/sdr/DALA2025021801184.md): Support Angle · cracked · Feb 17, 2025 · N341NB · Airbus A319114 · Horizontal Stabilizer Structure
  > SHIP 3141 CRACK SUPPORT ANGLE ELEVATOR HINGE ARM 5 ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED BONDING PLATE (SUPPORT ANGLE) LOC. ON ELEVATOR HINGE ARM 5 ON LH HORIZONTAL STABILIZER AS PER A319 SRM 51-72-11. (0815699)
- [SDR DALA2025021701177](https://openairdocs.org/sdr/DALA2025021701177.md): Bushing · excess play · Feb 16, 2025 · N341NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3141 EXCESSIVE PLAY PASSENGER CREW DOOR 831 UPPER AND LOWER BUSHING BETWEEN DOOR AND SUPPORT ARM AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED BUSHES FROM UPPER AND LOWER LINK BTW SUPPORT ARM AND DOOR 831 (8 E/A) AS PER A320 FAM AMM 52-11-21-000-001-A.

Next page: https://openairdocs.org/aircraft/N341NB/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 = 'N341NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N341NB/reports

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