# Service difficulty reports: N360NB A list on [N360NB](https://openairdocs.org/aircraft/N360NB.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 · 179 reports - [SDR DALA2026092805366](https://openairdocs.org/sdr/DALA2026092805366.md): Strut · corroded · Sep 9, 2026 · N360NB · Airbus A319114 · Wing Main, Frame Structure > CORROSION ON INTERNAL BARREL OF INTERCONNECTING STRUT OF LT WING. REMOVED & REPLACED THE INTERCONNECTING STRUT IAW AMM 27-51-44-000-001- A, STEP 1, THRU 3.D(1), & 4.A. - [SDR DALA2026092805365](https://openairdocs.org/sdr/DALA2026092805365.md): Strut · corroded · Sep 9, 2026 · N360NB · Airbus A319114 · Wing Main, Frame Structure > CORROSION ON INTERNAL BARREL OF INTERCONNECTING STRUT ON RT WING. REMOVED INTERCONNECTING STRUT OF RT WING IAW FAM AMM 27-51-44-000-001-A, STEP 1, THRU 3.D(1) AND 4.A. REPLACED INTERCONNECTING STRUT IAW AMM 27-51 -44-000-001-A, & AMM 27-51-44-400-001-A. (LP - [SDR DALA2026090104920](https://openairdocs.org/sdr/DALA2026090104920.md): Computer · failed · Aug 31, 2026 · N360NB · Airbus A319114 · Pitot/Static Anti-Ice System > DIVERTED TO IAD DUE TO BURNING ELECTRICAL ODOR AFTER TAKEOFF WITH ASSOCIATED NR 2 PROBE HEAT, COMPUTER FAILURE MESSAGES. CONFIRMED PROBE HEAT COMPUTER FRIED. REPLACED COMPUTER AND PERFORMED A LEVEL A DECONTAMINATION OF THE ECS. (LP: 9117321, AIRCRAFT WAS GRO - [SDR DALA2026070103869](https://openairdocs.org/sdr/DALA2026070103869.md): Drain Mast · missing · Jun 25, 2026 · N360NB · Airbus A319114 · Engine (Turbine/Turboprop) > NR 2 ENGINE ARRIVED WITH DRAIN MAST MISSING. INSTALLED NR 2 ENGINE DRAIN MAST IAW AMM 71-71-42. (LP: 8906834, AIRCRAFT WAS GROUNDED) - [SDR DALA2026021901179](https://openairdocs.org/sdr/DALA2026021901179.md): Fan · faulty · Feb 18, 2026 · N360NB · Airbus A319114 · Air Distribution Fan > BAD VIBRATION AND NOISE UNDER FLOOR OF FWD GALLEY AT PUSH TIME. T/S PER AMM 21-26, FOUND BAD EXTRACT AND BLOWER FAN (ONLY ONE FAN TWO FUNCTIONS), R & R SAME IAW AMM 21-26, OPS CHKD GOOD. (LP: 7732812) - [SDR DALA2025102907910](https://openairdocs.org/sdr/DALA2025102907910.md): Structure · damaged · Oct 28, 2025 · N360NB · Airbus A319114 · Buffet/Galleys > FOUND LAMINATE DAMAGED IN AFT GALLEY. REPLACED LAMINATE PER A319 AMM 25-31. (1276137). - [SDR DALA2025072405555](https://openairdocs.org/sdr/DALA2025072405555.md): Oxygen Mask · unwanted deploy · Jul 23, 2025 · N360NB · Airbus A319114 · Passenger Oxygen System > SHIP 3160 ON TAKEOFF OXYGEN MASK AT 3CD FELL OUT. CORRECTIVE ACTION: CLOSED 3CD OXYGEN GEN CONTAINER REF A319 AMM 35-21. (77408748). - [SDR DALA2024112111130](https://openairdocs.org/sdr/DALA2024112111130.md): Limiter · tripped · Nov 21, 2024 · N360NB · Airbus A319114 · Trailing Edge Flap Actuator > SHIP 3160 - FCNT - PERFORMED A GO-AROUND ON FIRST APPROACH DUE TO F/CTL FLAPS FAULT ECAM MESSAGE, CYCLED FLAPS AND WORKED NORMALLY ON SECOND APPROACH. CORRECTIVE ACTION: FOUND LEFT WING ACTUATOR #1 (6205CM) TORQUE LIMITER TRIPPED. REPLACED LEFT WING FLAP TORQU - [SDR DALA2024111510973](https://openairdocs.org/sdr/DALA2024111510973.md): Window Frame · cracked · Nov 14, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 CRACK INDICATIONS WERE FOUND AT LH, RH, FRONT WINDSHIELD FRAMING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620461-14. (0660002) - [SDR DALA2024111510969](https://openairdocs.org/sdr/DALA2024111510969.md): Window Frame · cracked · Nov 14, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA, CONTINUITY FITTING RH SIDE. CORRECTIVE ACTION: REPAIRED PER ER/A 620410-14AD. (0659943) - [SDR DALA2024111410964](https://openairdocs.org/sdr/DALA2024111410964.md): Access Panel · damaged · Nov 13, 2024 · N360NB · Airbus A319114 · Wing, Plate/Skin > SHIP 3160 ELONGATED HOLES (2 EA) ON ACCESS PANEL FUEL TANK CUT OUT BOTTOM SKIN B TW RIB 16 TO RIB 17 ON LH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON HOLES (2E/A) LOC ON ACCESS PANEL FUEL TANK CUT OUT BOTTOM SKIN BTW RIB 16 TO RIB 17 ON LH WING AS - [SDR DALA2024111310920](https://openairdocs.org/sdr/DALA2024111310920.md): Window Frame · cracked · Nov 13, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 CRACK INDICATIONS WERE FOUND AT LH, RH, FRONT WINDSHIELD FRAMING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620465-14AD. (0657445) - [SDR DALA2024111310922](https://openairdocs.org/sdr/DALA2024111310922.md): Bonding Plate · corroded · Nov 12, 2024 · N360NB · Airbus A319114 · Trailing Edge Flaps > SHIP 3160 CORROSION BONDING PLATE FLAP TRACK FAIRING 3 (532CB) ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620610-14. (0657078) - [SDR DALA2024111310921](https://openairdocs.org/sdr/DALA2024111310921.md): Bonding Plate · corroded · Nov 12, 2024 · N360NB · Airbus A319114 · Trailing Edge Flaps > SHIP 3160 CORROSION FLAP TRACK FAIRING 632CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620610-14. (0657071) - [SDR DALA2024111210874](https://openairdocs.org/sdr/DALA2024111210874.md): Elec Connector · corroded · Nov 12, 2024 · N360NB · Airbus A319114 · Flight Control System Wiring > SHIP 3160 CORROSION ON CONNECTOR 7542VC, 7540VC AND CORROSION ON METALLIC CONDU IT OF CONNECTOR 7540VC AND 7542VC AT RH WING. CORRECTIVE ACTION: REPLACED CONNECTORS 7542VC, 7540VC AND METALLIC CONDUIT OF CONNECTORS 7540VC AND 7542VC AT RH WING AS PER AIRBUS ES - [SDR DALA2024111210873](https://openairdocs.org/sdr/DALA2024111210873.md): Fitting · corroded · Nov 12, 2024 · N360NB · Airbus A319114 · Trailing Edge Flaps > SHIP 3160 CORROSION ON BORE I/B FITTING OF O/B FLAP LH. CORRECTIVE ACTION: COMPLIED WITH ER/A 620919-14. (0655751) - [SDR DALA2024111210878](https://openairdocs.org/sdr/DALA2024111210878.md): Plate · gouged · Nov 11, 2024 · N360NB · Airbus A319114 · Wing Miscellaneous Structure > SHIP 3160 GOUGE PLATE LOCATED INBOARD RIB LOWER AREA OB FLAP ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 621862-14. (0655426) - [SDR DALA2024111210877](https://openairdocs.org/sdr/DALA2024111210877.md): Flap Track · corroded · Nov 11, 2024 · N360NB · Airbus A319114 · Trailing Edge Flaps > SHIP 3160 CORROSION BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620610-14. (0655121) - [SDR DALA2024111210876](https://openairdocs.org/sdr/DALA2024111210876.md): Flap Track · corroded · Nov 11, 2024 · N360NB · Airbus A319114 · Trailing Edge Flaps > SHIP 3160 CORROSION FLAP TRACK FAIRING 631CB BONDING PLATE ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 620610-14. (0655117) - [SDR DALA2024111210875](https://openairdocs.org/sdr/DALA2024111210875.md): Strut · corroded · Nov 11, 2024 · N360NB · Airbus A319114 · Wing Structure > SHIP 3160 CORROSION ON INTERCONNECTING STRUT AT RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT RH AS PER A320 FAM AMM 27-51-44-000-001-A AND FAM AMM 27-51-44-400-001-A. (0655297) - [SDR DALA2024111210869](https://openairdocs.org/sdr/DALA2024111210869.md): Web · corroded · Nov 11, 2024 · N360NB · Airbus A319114 · Fuselage Miscellaneous Structure > SHIP 3160 CORROSION ON WEB FR 16 RH SIDE FWD GALLEY. CORRECTIVE ACTION: REPLACED WEB FR 16 RH SIDE FWD GALLEY AS PER A319 SRM 51-72-11 AND SRM 51-42-11. (0654915) - [SDR DALA2024111110815](https://openairdocs.org/sdr/DALA2024111110815.md): Plate · gouged · Nov 11, 2024 · N360NB · Airbus A319114 · Wing Main, Frame Structure > SHIP 3160 GOUGE PLATE LOCATED AT INBOARD RIB LOWER AREA OB FLAP ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION ON PLATE LOCATED AT INBOARD RIB LOWER AREA OB FLAP ON RH WING AS PER ER/A 621969-14. (0654538) - [SDR DALA2024111110816](https://openairdocs.org/sdr/DALA2024111110816.md): Door Frame · unknown · Nov 10, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 FUSELAGE FRAM E 16 RH DOOR STOP FITTING 1. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION ON DOOR STOP FITTING 1 LOC FRAME 16 RH AS PER ER/A 581772-14AD. (0653436) - [SDR DALA2024111110814](https://openairdocs.org/sdr/DALA2024111110814.md): Skin · gouged · Nov 10, 2024 · N360NB · Airbus A319114 · Wing, Plate/Skin > SHIP 3160 GOUGE UPPER SKIN IB FIXED LEADING EDGE LOCATED BETWEEN RIB2 TO RIB3 ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION ON UPPER SKIN IB FIXED LEADING EDGE LOCATED BETWEEN RIB2 TO RIB3 ON RH WING AS PER ER/A 621939-14. (0652774) - [SDR DALA2024111110808](https://openairdocs.org/sdr/DALA2024111110808.md): Skin · damaged · Nov 9, 2024 · N360NB · Airbus A319114 · Leading Edge Devices > SHIP 3160 BIRD STRIKE LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION ON SLAT 2 BTW CLOSING RIB INB AND END RIB INB ON LH WING AS PER ER/A 621394-14. (0651250) - [SDR DALA2024111110812](https://openairdocs.org/sdr/DALA2024111110812.md): Door Frame · cracked · Nov 8, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 DURING M2 AND WHILE INSPECTING PER SECTION II OF 581772-14, A CRACK WAS FOUND ON PREVIOUSLY REPAIRED HOLE #3 AT DOOR STOP FITTING #1, IN THE FRAME LAYER AT FR16 RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 581772-14. (0650974) - [SDR DALA2024111110811](https://openairdocs.org/sdr/DALA2024111110811.md): Flap Track · corroded · Nov 8, 2024 · N360NB · Airbus A319114 · Trailing Edge Flaps > SHIP 3160 CORROSION WAS FOUND AFFECTING THE INB'D AND OUTB'D AL PLATES AT TRACK #3. CORRECTIVE ACTION: COMPLIED WITH ER/A 31-620919. (0650452) - [SDR DALA2024111110810](https://openairdocs.org/sdr/DALA2024111110810.md): Spar · gouged · Nov 8, 2024 · N360NB · Airbus A319114 · Nacelle/Pylon, Frame/Spar/Rib > SHIP 3160 GOUGE UPPER SPAR CANTILEVER OUTBOARD SIDE BTW RIB8 AND RIB9 ON RH PYLON. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION ON UPPER SPAR CANTILEVER OUTBOARD SIDE BTW RIB8 AND RIB9 ON RH PYLON ASPER ER/A 621023-14 REV ORIGINAL SECTION I HAS BEEN COMPLIE - [SDR DALA2024110810763](https://openairdocs.org/sdr/DALA2024110810763.md): Window Frame · cracked · Nov 7, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 CRACKS FOUND IN LH AND RH FRONT WINDSHIELD FRAMES LWR CENTER NODE AND CONTINUITY FITTINGS. CORRECTIVE ACTION: REPAIRED PER ER/A 620410-14. (0648874) - [SDR DALA2024110810762](https://openairdocs.org/sdr/DALA2024110810762.md): Window Frame · cracked · Nov 7, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 RACKS FOUND IN LH AND RH FRONT WINDSHIELD FRAMES LWR CENTER NODE AND CONTINUITY FITTINGS. CORRECTIVE ACTION: COMPLIED WITH ER/A 31-620465. (0649586) - [SDR DALA2024110810761](https://openairdocs.org/sdr/DALA2024110810761.md): Skin · dented · Nov 7, 2024 · N360NB · Airbus A319114 · Fuselage Main, Plate/Skin > SHIP 3160 DENT EXTERNAL SKIN LOC. BTW FR82 TO FR83 AT LEVEL STGR 3 LH ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 621495-14. (0648987) - [SDR DALA2024110810759](https://openairdocs.org/sdr/DALA2024110810759.md): Roller · excess play · Nov 7, 2024 · N360NB · Airbus A319114 · Trailing Edge Flaps > SHIP 3160 EXCESSIVE PLAY CRUISE ROLLER OB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER AS PER AIRBUS CMM 57- 53-21 TASK 57-53-21-000-810-B01 AND CMM 57-53-21 TASK 57-53-21-400-810-B01. (0648983) - [SDR DALA2024110710710](https://openairdocs.org/sdr/DALA2024110710710.md): Shear Tie · corroded · Nov 7, 2024 · N360NB · Airbus A319114 · Fuselage Internal Mounting Structure > SHIP 3160 CORROSION SHEAR TIE LOCATED BETWEEN FR62 AND STR41R TO STR42R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS LOCATED BETWEEN FR 62 AND STR 41R TO 42R IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-72-11 AND SRM 51-42-11. ( - [SDR DALA2024110710709](https://openairdocs.org/sdr/DALA2024110710709.md): Shear Tie · corroded · Nov 7, 2024 · N360NB · Airbus A319114 · Fuselage Internal Mounting Structure > SHIP 3160 CORROSION FRAME 58 SHEAR TIE BTW STR40L TO STR 41L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS LOCATED BETWEEN FRAME 58 SHEAR TIE BTW STR40L TO STR 41L IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-72-11 AND SRM 51-42- - [SDR DALA2024110710716](https://openairdocs.org/sdr/DALA2024110710716.md): Window Frame · cracked · Nov 6, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA, FROM UPPER TENSION BOLT IN INNER VERTICAL FLANGE LH SIDE. CORRECTIVE ACTION: REPLACEMENT OF FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA PER A319 AMM 53-11. ( - [SDR DALA2024110710715](https://openairdocs.org/sdr/DALA2024110710715.md): Window Frame · cracked · Nov 6, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHM ENT AREA, FROM UPPER TENSION BOLT IN INNER VERTICAL FLANGE RH SIDE. CORRECTIVE ACTION: REPLACEMENT OF FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT AREA PER A319 AMM 53-11. - [SDR DALA2024110710714](https://openairdocs.org/sdr/DALA2024110710714.md): Window Frame · cracked · Nov 6, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHM ENT INTERNAL AREA, LOWER INBOARD RADIUS RH SIDE. CORRECTIVE ACTION: REPLACEMENT OF FRAME 2 WINDSHIELD CENTER POST LOWER NODE ATTACHMENT INTERNAL AREA PER A319 AMM 53-11. (0647760) - [SDR DALA2024110710713](https://openairdocs.org/sdr/DALA2024110710713.md): Access Panel · punctured · Nov 6, 2024 · N360NB · Airbus A319114 · Aerodynamic Fairings > SHIP 3160 PUNCTURE ON ACCESS PANEL 148FB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 621434-14. (0647783) - [SDR DALA2024110710712](https://openairdocs.org/sdr/DALA2024110710712.md): Access Panel · cracked · Nov 6, 2024 · N360NB · Airbus A319114 · Horizontal Stabilizer, Plate/Skin > SHIP 3160 CRACK ACCESS PANEL 342AB ON RH HORIZONTAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A # 621426-14. (0647633) - [SDR DALA2024110710711](https://openairdocs.org/sdr/DALA2024110710711.md): Access Panel · cracked · Nov 6, 2024 · N360NB · Airbus A319114 · Vertical Stabilizer, Plate/Skin > SHIP 3160 CRACK ACCESS PANEL 322BL LEADING EDGE VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 620762-14. (0647626) - [SDR DALA2024110710708](https://openairdocs.org/sdr/DALA2024110710708.md): Profile · cracked · Nov 6, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 CRACK RH LOAD TRANSMITTING PROFILE ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED PROFILE LOC. AT RH LOAD TRANSMITTING PROFILE ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (06478 - [SDR DALA2024110710707](https://openairdocs.org/sdr/DALA2024110710707.md): Profile · cracked · Nov 6, 2024 · N360NB · Airbus A319114 · Fuselage Main, Structure > SHIP 3160 CRACK LH LOAD TRANSMITTING PROFILE ON EMERGENCY EXIT DOOR 834 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED PROFILE LOC. AT LH LOAD TRANSMITTING PROFILE ON EMERGENCY EXIT DOOR 834 IN PASSENGER CABIN AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (06476 - [SDR DALA2024110710706](https://openairdocs.org/sdr/DALA2024110710706.md): Web · damaged · Nov 6, 2024 · N360NB · Airbus A319114 · Fuselage Miscellaneous Structure > SHIP 3160 ELONGATED HOLE WEB INTERNAL STRUCTURE LOC. FR 25 TO FR 26 AT LEVEL STR 38 LH IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED WEB INTERNAL STRUCTURE LOC. FR 25 TO FR 26 AT LEVEL STR 38 LH IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11-801 AND - [SDR DALA2024110610683](https://openairdocs.org/sdr/DALA2024110610683.md): Skin · corroded · Nov 6, 2024 · N360NB · Airbus A319114 · Fuselage Main, Plate/Skin > SHIP 3160 CORROSION SKIN LOWER EXTERNAL AREA AFT WALL LAVATORY A. CORRECTIVE ACTION: REPLACED PER ER/A 621147-14. (0646441) - [SDR DALA2024110610682](https://openairdocs.org/sdr/DALA2024110610682.md): Access Panel · gouged · Nov 6, 2024 · N360NB · Airbus A319114 · Aerodynamic Fairings > SHIP 3160 GOUGE ACCESS PANEL 148FB BELLY FAIRING AT LOWER FUSELAGE. CORRECTIVE ACTION: REPAIRED AS PER ER/A 621434 -14 REV. (0646437) - [SDR DALA2024110510648](https://openairdocs.org/sdr/DALA2024110510648.md): Frame · cracked · Nov 4, 2024 · N360NB · Airbus A319114 · Fuselage Main, Frame > SHIP 3160 CRACK FOUND IN HOLE #6. CORRECTIVE ACTION: REPAIRED PER ER/A 581727-14. (0644434) - [SDR DALA2024110410603](https://openairdocs.org/sdr/DALA2024110410603.md): Skin · scratched · Nov 2, 2024 · N360NB · Airbus A319114 · Fuselage Main, Plate/Skin > SHIP 3160 SCRATCH ON EXTERNAL SKIN LOCATED AT FR 20 BTW STR 26L TO STR 27L LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 621130-14. (0641576) - [SDR DALA2024110410602](https://openairdocs.org/sdr/DALA2024110410602.md): Skin · dented · Nov 2, 2024 · N360NB · Airbus A319114 · Fuselage Main, Plate/Skin > SHIP 3160 DENTS ON EXTERNAL SKIN LOCATED BTW FR 69 TO FR 70 TW STR 22 R TO STR 23R LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 620969-14. (0641571) - [SDR DALA2024110410598](https://openairdocs.org/sdr/DALA2024110410598.md): Megaphone · expired · Nov 2, 2024 · N360NB · Airbus A319114 · Emergency Equipment > SHIP 3160 EXPIRED DUE DATE MEGAPHONE ON AFT PARTITION RH AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED MEGAPHONE ON AFT PARTITION RH AFT GALLEY AREA AS PER A319 AMM 25-65. (0641439) - [SDR DALA2024110410597](https://openairdocs.org/sdr/DALA2024110410597.md): Plate · cracked · Nov 2, 2024 · N360NB · Airbus A319114 · Fuselage Miscellaneous Structure > SHIP 3160 CRACK ON PLATE LOCATED BTW FR 68 TO FR 69 LEVEL STR 23R AFT GALLEY. CORRECTIVE ACTION: REPLACED PLATE LOCATED BTW FR 68 TO FR 69 LEVEL STR 23R AFT GALLEY AS PER A319 SRM 51-42-11 AND SRM 51-72-11. (0641423) Next page: https://openairdocs.org/aircraft/N360NB/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 = 'N360NB' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N360NB/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.