N345NW

Service difficulty reports · 204

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N345NW' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2020122304203Damper · no testPASSENGER CREW DOOR 841 FWD GALLEY AREA DAMPER FAILED TEST. CORRECTIVE ACTION: REPLACED DAMPER, OK FOR SERVICE.Nov 25, 2020 · N345NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020120403967Damper · no testCREW DOOR DAMPER AT DOOR 831 AT FWD GALLEY AREA FAILED TEST. CORRECTIVE ACTION: REPLACED DOOR DAMPER AT DOOR 831 FWD GALLEY AREA. OK FOR SERVICE.Nov 25, 2020 · N345NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020120103926Damper · no testPASSENGER CREW DOOR DAMPER 841 DOESN'T PASS TEST. CORRECTIVE ACTION: REPLACED DOOR 841 DAMPER. OK FOR SERVICE.Nov 25, 2020 · N345NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020113003902Dampener · no testCREW DOOR 842 DAMPER DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DOOR DAMPER. OK FOR SERVICE.Nov 23, 2020 · N345NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2020111703761Spar · corrodedCORROSION FOUND ON MATING SURFACES OF LT WING REAR SPAR (AFT SURFACE). CORRECTIVE ACTION: COMPLIED WITH ERA 588446-14AD (1656889).Nov 16, 2020 · N345NW · Airbus A320212 · Wing SparSDR DALA2019090905247Apu · leakingAFTER TAKEOFF AND THROUGH 9000FT HEAVY ODOR IN COCKPIT AND FORWARD GALLEY ROTTEN EGG/ BURNED OIL SMELL. APU OIL LEAKAGE, FOUND OIL WETNESS IN DUCTING OF APU COOLING FAN ASSY, REPLACED APU.Aug 30, 2019 · N345NW · Airbus A320212 · APU Core EngineSDR DALA2018112706872Apu · leakingDURING BOARDING MAINTENANCE WAS NOTIFIED OF PASSENGERS COMPLAINTS OF OILY ODOR IN CABIN. FLIGHT CREW SMELLED ODOR ALSO. TURNED PACKS OFF AND ODOR DISSIPATED. NO SMOKE NOTED. COMPLY WITH NO GO ODI PREVENTION PROGRAM. FOUND SOURCE OF SMELL COMING FROM APU. FOUNDNov 24, 2018 · N345NW · Airbus A320212 · Airborne Auxiliary Power Unit (APU) SystemSDR DALA2018111966668Apu · odor(LP# 3837008) DIRTY SOCK SMELL DETECTED AFTER TAKEOFF. DISSIPATED ABOVE 600'. ON DESCENT ODOR RETURNED. DESCENDING THRU FL200. TROUBLESHOT AND DETERMINED APU TO BE SOURCE OF SMELL. APU CHANGED ON LP# 0825252Nov 15, 2018 · N345NW · Airbus A320212 · Airborne Auxiliary Power Unit (APU) SystemSDR DALA2019082805008Pivot · damagedSCHEDULED FOR RESTORATION THRUST REVERSER, LT HALF #1; INSPECTION OF THRUST REVERSER PIVOT FITTING AD SECTION 01 EM 7831-01102, REPLACEMENT OF PIVOT FITTING DONE I.A.W. ER/A 578826-14AD REV O.Oct 9, 2018 · N345NW · Airbus A320212 · Engine Thrust ReverserSDR DALA2018061404013Safety Valve · defectiveALT GEAR - CREW DID A GO-AROUND DUE TO THE FAILURE OF THE LANDING GEAR ON EXTENSION DURING APPROACH INTO TPA WITH ECAM WARNING. L/G GEAR NOT DOWNLOCKED. PERFORMED A MANUAL GEAR EXTENSION AND LANDED UNEVENTFULLY AND WAS TOWED TO THE GATE. REPLACED HYDRAULIC CONJun 13, 2018 · N345NW · Airbus A320212 · Landing Gear Retraction/Extension SystemSDR DALA2018043002915Actuator · leakingSMOKE AND FUMES ON INITIAL CLIMB OUT, DIRTY SOCK ODOR FOR ABOUT 5 MINUTES THEN DISSIPATED. DURING APPROACH, VERY STRONG DIRTY SOCK ODOR DETECTED THROUGHOUT FLIGHT DECK AND CABIN. TROUBLESHOT AND INSPECTED. FOUND RIGHT OUTBOARD COWL ACTUATOR LEAKING. REMOVApr 26, 2018 · N345NW · Airbus A320212 · Engine Thrust ReverserSDR DALA2020083102907Frame · crackedCRACK INDICATION FOUND IN HOLES #5 AND #6 NEAR DOOR STOP #7 ON FR16 RHS, OUTB'D FLANGE. CORRECTIVE ACTION: ER/A 553532-14 REVISED TO LEVEL "B" PERMANENT - CAT A REPAIR INSTALLED AT REV B.Jan 23, 2017 · N345NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2017012000510Angle · corrodedCORROSION ON FRAME 67 REINFORCEMET ANGLE BETWEEN STRINGERS 38R AND 38L, IN THE AFT CARGO BAY. REPLACED THE ANGLE IAW SRM A320 51-42-11 AND DRAWING 53480212.Jan 19, 2017 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2020123004339Rib · damagedRT WING MLG SUPPORT RIB TOOLING DAMAGE (MONITORED). CORRECTIVE ACTION: REPAIRED PER ER/A 587681-14AD REV A. OK FOR SERVICE.Jan 9, 2017 · N345NW · Airbus A320212 · Wing, Landing Gear Attach FittingsSDR DALA2016102607603Box Beam · crackedA ROTOTEST INSPECTION OF THE LEFT SIDE BOX BEAM, FOUND CRACKED. REPAIRED IAW AMDS 5310-01450-02.Oct 25, 2016 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2017011600424Rivet · damagedLIGHTNING STRIKE TO RIVET ON FWD CROWN LOC FR 32 =1 ON THE STR 1R, PERFORMED PERMANENT REPAIR ON EXACTLY LOCATION FR 33 AND STR 1R ASPER SRM 53-21-11 PAR 5 I FIG 202.Mar 28, 2016 · N345NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015040802670Floor Panel · corrodedDURING INSPECTION, FOUND CORROSION ON COVER SHEET IN AFT CARGO COMPARTMENT FROM FRAME 52A TO FRAME 56 BETWEEN STR 39R TO STR 41R. L=1.000"; W=0.500"; D=0.002". MEASURES APPROXIMATELY, SSI 534107. REPLACED COVER SHEET AND FASTENERS IN AFT CARGO COMPARTMENT FRApr 7, 2015 · N345NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2015040202571Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y254 AT FWD GALLEY AREA FROM FRAME 12 TO FRAME 24, L=0.900", W=0.200", D=0.002". REPLACED FLOORBEAM -Y254 AT FWD GALLEY AREA FROM FR 12 TO FR 24 IAW ERA 533434-14 REV ORIGINAL PRI 533434-14, REV O AND SRM 51-7Apr 1, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015040202568Skin · unknownDURING INSPECTION, FOUND CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON EXTERNAL SKIN ON LOWER FUSELAGE ON FRAME 72+11" AND STR 34. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOWER FUSELAGE BETWEEN FRAME 72 TO FRAME 75 AND BETWEEN STR 31R TO STR 32L IN AFTApr 1, 2015 · N345NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015040102533Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STR 43L IN AFT CARGO COMPARTMENT FROM FRAME 56 TO FRAME 58+3", L=0.500", W=0.400", D=0.005". MEASURE APPOXIMATELY SSI534107. REPLACED STRINGER 43L IN AFT CARGO COMPARTMENT FROM FRAME 54 TO FRAME 60 SRM 51-72-11 AND DWG DMar 31, 2015 · N345NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015033002518Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK +Y765 FRAME 36 TO 41 IN PASSENGER CABIN L=4.262", W=0.396", D=0.082". EVALUATED SEAT TRACK AND FOUND OUT LIMITS ON JOB CARD 2500-2031. REPLACED SEAT TRACK +Y765 LOCATED FRAME 36 TO FRAME 41 IN PASSENGER CABINMar 29, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015033002503Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK-Y1292 AT AFT GALLEY AREA FROM FRAME 47 TO FRAME 64 . L=5", W=0.370", D=0.081, EVALUATE AND FOUND OUT LIMITS ON JOB CARD NR 2500-2032-DE. REPLACED SEAT TRACK -Y1292 AT AFT GALLEY AREA FROM FRAME 47 TO FRAME 64Mar 29, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015033002502Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK +Y1292 AT AFT GALLEY AREA FROM FRAME 47 TO FRAME 64, L=5.0", W=0.370", D=0.070". EVALUATED AND FOUND LIMITS ON JOB CARD NO 25002032. REPLACED SEAT TRACK +Y1292 AT AFT GALLEY AREA FROM FRAME 47 TO FRAME 64 IAWMar 29, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015032902500Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 AT FWD GALLEY AREA BETWEEN FR 12 TO FR 24, L=7", W=0.900", D=0.003". REPLACED FLOORBEAM -Y765 LOCATED AT FWD GALLEY BETWEEN FR 12 TO FR 24 IAW D53112812.Mar 28, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032802495Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK-Y1292, FRAME 35 TO 36 IN PASSENGER CABIN L=4.082", W=0.358", D=0.062". EVALUATED SEAT TRACK AND FOUND OUT LIMITS ON JOB CARD 2500-2031. REPLACED SEAT TRACK-Y1292 LOCATED BETWEEN FR 35 TO FR 36 IN PASSENGER CAMar 27, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015032802491Static Port · damagedDURING INSPECTION, FOUND SCRATCH ON STATIC PORT LOCATED BETWEEN FR 3 TO FR 4 LT SIDE PANEL ON LOWER FUSELAGE. PERFORMED PERMANENT REPAIR PRINCIPLE 1 ON STATIC PORT LOCATED BETWEEN FR 3 TO FR 4 LT SIDE SKIN FUSELAGE IAW SRM 53-11-11, PARA 5A, FIG 203, PAGES 21Mar 27, 2015 · N345NW · Airbus A320212 · Fuselage Structure (General)SDR DALA2015032802490Static Port · damagedDURING INSPECTION, FOUND SCRATCH ON STATIC PORT LOCATION BETWEEN FR 23 TO FR 24 RT SIDE ON LOWER FUSELAGE. PERFORMED PERMANENT REPAIR PRINCIPLE 1 ON STATIC PART LOCATED BETWEEN FR 23 TO FR 24 RT SIDE SKIN FUSELAGE IAW SRM 53-11-11, PARA 5A, FIG 203, PAGES 215Mar 27, 2015 · N345NW · Airbus A320212 · Fuselage Structure (General)SDR DALA2015032802489Skin · damagedDURING INSPECTION, FOUND SCRATCH ON STATIC PORT LOCATED BETWEEN FR 23 TO FR 24 LT SIDE ON LOWER FUSELAGE. PERFORMED PERMANENT REPAIR PRINCIPLE 1 ON STATIC PART LOCATED BETWEEN FR 23 TO FR 24 LT SIDE SKIN FUSELAGE IAW SRM 53-11-11, PARA 5A FIG 203, PAGES 215/2Mar 27, 2015 · N345NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015032802487Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 43R AT LEVEL FR 61 IN AFT CARGO COMPARTMENT, L=0.400", W=0.250", D=0.002". MEASURES APPROXIMATELY SSI534107. REPLACED STRINGER 43R LOCATED BETWEEN FR 60 TO FR 65 AFT CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53Mar 27, 2015 · N345NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015032802486Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 FRAME 35 TO 36 IN PASSENGER CABIN L=3.303", W=0.365", D=0.053. EVALUATED SEAT TRACK AND FOUND OUT LIMITS ON JOB CARD 2500-2031. REPLACED SEAT TRACK -Y765 LOCATED BETWEEN FR 35 TO FR 36 IN PASSENGER CABIMar 27, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015032702433Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR LT LOAD TRANSMITTING PROFILE LOCATED EXIT HATCHES, DOOR 844 IN PASSENGER CABIN. ATTACH THE FORM 5100-3201, SSI 522102-01-1. REPLACED EMERGENCY EXIT DOOR LOAD TRANSMITTING PROFILE LEFT, SEGMENT ANGLE, LOCMar 26, 2015 · N345NW · Airbus A320212 · Emergency ExitsSDR DALA2015032702432Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR LOAD TRANSMITTING PROFILE RT LOCATED EXIT HATCHES 834 IN PASSENGER CABIN. ATTACH THE FORM 5100-3201, SSI 522102-01-1. REPLACED EMERGENCY EXIT DOOR LOAD TRANSMITTING PROFILE RT, SEGMENT ANGLE, LOCATED AT EMar 26, 2015 · N345NW · Airbus A320212 · Emergency ExitsSDR DALA2015032602419Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1292, LOCATED BETWEEN FRAME 64 AND FRAME 66+5" AT AFT GALLEY AREA, L=1", W=0.700", D=0.002". SSI 534147. REPLACED FLOORBEAM -Y1292, LOCATED BETWEEN FRAME 64 AND FRAME 66+5" AT AFT GALLEY AREA IAW SRM 51-72-Mar 25, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032602418Support · corrodedDURING INSPECTION, FOUND CORROSION ON EMERGENCY EXIT DOOR SUPPORT TEE LOCATED EXIT HATCHES 833 IN PASSENGER CABIN. REPLACED EMERGENCY EXIT DOOR SUPPORT T LOCATED EXIT HATCHES 833 IAW SRM 51-72-11 AND DWG D52279010.Mar 25, 2015 · N345NW · Airbus A320212 · Emergency ExitsSDR DALA2015032602417Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK +Y765 AT AFT GALLEY AREA FROM FRAME 47 TO FRAME 64, L=3.0", W=0.370", D=0.046". EVALUATED AND FOUND OUT OF LIMITS ON JOB CARD NR 2500-2032-DE. REPLACED SEAT TRACK +Y765 AT AFT GALLEY AREA FROM FRAME 47 TO FRAMar 25, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015032502415Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE LOCATED EXIT HATCHES DOOR 844 IN PASSENGER CABIN. ATTACH THE FORM 5100-3201, SSI 522102-01-1. REPLACED EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE LOCATED EXIT HATCHES DMar 24, 2015 · N345NW · Airbus A320212 · Emergency ExitsSDR DALA2015032502414Support · corrodedDURING INSPECTION, FOUND CORROSION ON EMERGENCY EXIT DOOR SUPPORT LOCATED EXIT HATCHES 834 IN PASSENGER CABIN. REPLACED SUPPORT AND SEGMENT FRAME LOC ON EMERGENCY EXIT DOOR LOCATED EXIT HATCHES 834 IN PASSENGER CABIN IAW SRM 51-72-11 AND DWG D52279040.Mar 24, 2015 · N345NW · Airbus A320212 · Emergency ExitsSDR DALA2015032502413Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STR 23L, L=0.500", W=0.300", D=0.002", SSI 534147. REPLACED LOWER SILL LT LOCATED AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STR 23L IAW SRM 51-72-11 AND Mar 24, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032502412Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292, FRAME 41 TO 47 IN PASSENGER CABIN, L=4.070", W=0.760", D=0.059". EVALUATED SEAT TRACK AND FOUND OUT LIMITS ON JOB CARD 2500-2031. REPLACED SEAT TRACK -Y1292 LOCATED BETWEEN FRAME 41 TO FRAME 47 IN PASSMar 24, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015032502408Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 AT AFT GALLEY AREA FROM FRAME 66+5" TO FRAME 70 L=0.500", W=0.250", D=0.002, SSI 534147. REPLACED FLOORBEAM -Y765 BETWEEN FR 66+5" TO FR 70 IAW SRM 51-72-11 AND DWG D53472000; D5347093.Mar 24, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032502380Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR ON TRANSMITTING PROFILE RT LOCATED 833 IN PASSENGER CABIN. REPLACED TRANSMITTING PROFILE RT LOCATED 833 EMERGENCY EXIT DOOR IAW SRM 51-72-11 AND DWG D52279020.Mar 24, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032502379Frame · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR ON VERTICAL FRAME SEGMENTS LT LOCATED EXIT HATCHES 843 IN PASSENGER CABIN. REPLACED VERTICAL FRAME SEGMENTS LT LOCATED EXIT HATCHES EMERGENCY EXIT DOOR 843 IAW SRM A320 51-72-11 AND DWG D52279010.Mar 24, 2015 · N345NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2015032502378Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR LOAD TRANSMITTING PROFILE LT LOCATED AT EXIT HATCHES 833 IN PASSENGER CABIN. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-72-11 AND DWG D52279010.Mar 24, 2015 · N345NW · Airbus A320212 · Emergency ExitsSDR DALA2015032502377Profile · crackedDURING INSPECTION, FOUND CRACK ON EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE LOCATED EXIT HATCHES 843 IN PASSENGER CABIN. ATTACH THE FORM 5100-3201, SSI 522102-01-1. REPLACED LOAD TRANSMITTING PROFILE LOCATED EXIT HATCHES 843 EMERGENCY EXIT DOOR AS IAW Mar 24, 2015 · N345NW · Airbus A320212 · Emergency ExitsSDR DALA2015032502376Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765, FRAME 41 TO 47 IN PASSENGER CABIN L=3.6 90", W=0.362", D=0.049". EVALUATED SEAT TRACK AND FOUND OUT LIMITS ON JOB CARD 2500-2031. REPLACED SEAT TRACK -Y765 LOCATED BETWEEN FRAME 41 TO FRAME 47 IAW SRM 5Mar 24, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015032502375Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 FRAME 36 TO 41 IN PASSENGER CABIN L=4.012", W=0.367", D=0.063". EVALUATED SEAT TRACK AND FOUND OUT LIMITS ON JOB CARD 2500-2031. REPLACED SEAT TRACK -Y765 LOCATED BETWEEN FR 36 TO FR 41 IAW SRM 51-72-1Mar 24, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015032402374Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STRINGER 23R, L=0.700", W=0.350", D=0.002". REPLACED LOWER SILL AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STRINGER 23R IAW SRM 51-72-11 AND DWG D53480505.Mar 23, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032402373Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y512 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 70, L=0.300", W=0.150", D=0.002". REPLACED FLOORBEAM Y512 AND FASTERNERS LOCATED BETWEEN FRAME 64 TO FRAME 70 IAW SRM 51-72-11 AND DWG D53472000.Mar 23, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015032402372Seat Track · corrodedDURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 AT AFT GALLEY AREA FROM FRAME 47 TO FRAME 64, L=3.0", W=0.370", D=0.063". EVALUATED AND FOUND OUT LIMITS ON JOB CARD, NR 2500-2032-DE. REPLACED SEAT TRACK -Y765 AT AFT GALLEY AREA BETWEEN FRAME 47 TO FRAMar 23, 2015 · N345NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015032402371Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y512 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66. REPLACED THE FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG A534-72230 AND 51-42-11.Mar 23, 2015 · N345NW · Airbus A320212 · Fuselage Miscellaneous Structure
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