N354NW

Service difficulty reports · 128

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 = 'N354NW' 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 DALA2021033001887Plate · corrodedSHIP 3254 CORROSION SPIGOT BALL JOINT RETAINING PLATE ON LH PYLON. CORRECTIVE ACTION: REPLACED PER A320 SRM 54-51-12. (1767762)Mar 29, 2021 · N354NW · Airbus A320212 · Nacelle/Pylon Miscellaneous StructureSDR DALA2021033001886Dummy Rail · corrodedSHIP 3254 CORROSION RAIL DUMMY Y503.2 BTW FLOORBEAM FR 12/16 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED RAIL DUMMY PER SRM A320 51-72-11. (1767776)Mar 29, 2021 · N354NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2021033001885Fitting · corrodedSHIP 3254 CORROSION CENTER FITTING AT LEVEL OF STR 23 RH BTW FR 16/20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED CENTER FITTING PER A320 SRM 51-72-11. (1767773)Mar 29, 2021 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021033001884Attach Fitting · not reportedSHIP 3254 REMOVE AND RE-INSTALL AFT ATTACH FITTING SLEEVE AND BOLT UPPER POSITION ON LH PYLON. CORRECTION ACTION:RE-INSTALLED PYLON TO WING AFT ATTACH-FITTING BOLT AND SLEEVE AS PER A320 FAM AMM 54-51-17. (1767755)Mar 29, 2021 · N354NW · Airbus A320212 · Nacelle/Pylon, Attach FittingsSDR DALA2021033001883Profile · crackedSHIP 3254 CRACK EMERGENCY EXIT DOOR 834 LOAD TRASMITTING PROFILE LH IN PASSENGER CABIN. CORRECTIVE ACTION: REPAIRED PER A320 SRM 51-42-11. (1767750)Mar 29, 2021 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021032901819Shear Plate · corrodedSHIP 3254 CORROSION SHEAR PLATE STR 23 L BTW FR 69/70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE PER A320 SRM 51-72-11. (1766232)Mar 27, 2021 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021032901818Web · corrodedSHIP 3254 CORROSION WEB FRAME 20 -Y1590 APPROX FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB PER A320 SRM 51-42-11, AND 51-72-11. (1766227)Mar 27, 2021 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2021040702045Slide · deformedSHIP 3254 DEFORMATION OF SLIDE RAFT PASSENGER CREW DOOR 831 AT FWD GALLEY AREA. CORRECTIVE ACTION: R/R SLIDE PER DELTA WORKCARD AMDS CARD 2561-4001-LF. OK FOR SERVICE. (1764675)Mar 25, 2021 · N354NW · Airbus A320212 · Escape SlideSDR DALA2021032301710Floorbeam · corrodedSHIP 3254 CORROSION FLOOR BEAM -Y1292 AT LEVEL OF FR20 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER SRM A320 51-72-11. (1761690)Mar 22, 2021 · N354NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2020071902602Wire · damagedWHITE EMERGENCY LIGHT INOPERATIVE. ON ROW 3 CD SEAT (FWD LIGHT), REPAIRED A WIRE IAW AWM 33-51-06Jul 16, 2020 · N354NW · Airbus A320212 · Light System WiringSDR DALA2020020310860Light · damagedEMERGENCY SEAT MOUNTED LIGHTING DAMAGED LOCATIONS:30D, REPLACED EMERGENCY LIGHT HOUSING ASSYJan 30, 2020 · N354NW · Airbus A320212 · Emergency LightingSDR DALA2019092405511Power Supply · inoperativeEMERGENCY LIGHTS ON SEATS 32D AND 33D INOP, REPLACED AFT EMERGENCY POWER SUPPLY UNIT.Sep 23, 2019 · N354NW · Airbus A320212 · Emergency LightingSDR DALA2019081504802Power Supply · inoperativeEMERGENCY LIGHTS THAT OPERATE ON EPSU 13WL INOP. REMOVED AND REPLACED THE EPSU (13WL) AND BATTERY PACK. REF A320 AMM 33-51.Aug 14, 2019 · N354NW · Airbus A320212 · Emergency LightingSDR DALA2019060423397Power Supply · inoperativeEMERGENCY LIGHTS INOP, REPLACED EPSU AT 13WLJun 2, 2019 · N354NW · Airbus A320212 · Emergency LightingSDR DALA2019052703185Wire · crossedEMERY EXIT LIGHT INOP SEAT 32-33 AND EXIT LIGHT L AND R, FOUND WIRES 8017 AND 8018 AT T/B'S 7222VT CROSSED, REINSTALLED WIRE.May 26, 2019 · N354NW · Airbus A320212 · Light System WiringSDR DALA2019041002448Frame · crackedCRACK INDICATION FOUND ON HOLE 6 FRAME 36 LH MODIFY IN ACCORDANCE WITH WORK CARD 5311-01171-04A PRIOR TO FURTHER FLIGHT . -M-*AA5311-01171*SBA320-53-1263*AD-2018-06-04, SEE NR FOR ADDITIONAL INFORMATION 174-0001:5311-01171-04A/001 00170 REPAIRED PER AMDS 5311-Apr 9, 2019 · N354NW · Airbus A320212 · Fuselage Main, FrameSDR DALA201904152449Skin · crackedLEFT SIDE OF AIRCRAFT, HOLE A (INBOARD SIDE) HAS A CRACK INDICATION IN ALUMINUM, REPAIRED PER AMDS 5311-01171-04AApr 9, 2019 · N354NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2018082205223Unknown · odorCREW AND PASSENGERS COMPLAINED OF TURPENTINE ODOR IN AFT ROWS OF CABIN. REMOVED GROUND SUPPLIED AIR, TURNED ON PACK AND NO ODOR NOTED.Aug 21, 2018 · N354NW · Airbus A320212 · Air Distribution SystemSDR DALA2020120804002Skin · damagedEVIDENCE OF REWORK EXTERNAL SKIN LOCATED AT FR 24A+5" LEVEL OF STGR 41L ON LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED AT FR 24A+5" AT LEVEL OF STR 41L ON LOWER FUSELAGE, AS PER A320 FAM SRM 53-00-11-300-042.May 9, 2017 · N354NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2017050703699Skin · dentedDENT EXTERNAL SKIN DOOR 831 LOC BTW XP 606.3 TO XP 453.3 LOWER EDGE AT FWD GALLEY AREA. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN DOOR 831 BOC BTW XP606-3 TO XP 453.3 LOWER EDGE AT FWD GALLEY AREA AS PER SRM 52-10-00-300-005.May 6, 2017 · N354NW · Airbus A320212 · Passenger/Crew DoorsSDR DALA2016101607388Box Beam · crackedSIDE BOX BEAM UPPER FLANGE LEFT SIDE MIDDLE FASTENER HOLE HAS CRACK INDICATION. REPAIRED IAW AMDS 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1Oct 15, 2016 · N354NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2016101607387Box Beam · crackedSIDE BOX BEAM UPPER FLANGE RIGHT SIDE MIDDLE FASTENER HOLE HAS CRACK INDICATION. REPAIRED IAW AMDS 5310-01450-02.Oct 15, 2016 · N354NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2015051803381Skin · dentedDURING INSPECTION, DENT FOUND FRAME 21.+2 BETWEEN STRINGERS 23-24R.May 17, 2015 · N354NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2015051603302Seat Track · corrodedSEAT TRACK -Y1292, FRAMES 24 TO 35 CORRODED AND FOUND OUT LIMITS; REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53231740.May 15, 2015 · N354NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015051603301Stringer · corrodedCORROSION ON STRINGER 42L IN AFT CARGO BAY BETWEEN FRAMES 53 - 60. REPAIRED THE STRINGER IAW SRM 51-72-11 AND 53-00-13 FIG 201.May 15, 2015 · N354NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2015051403259Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE COUPLING IN FWD CARGO COMPARTMENT FROM FRAME 30 TO FRAME 31 AND STR 41R.May 13, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015051403257Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 24A BETWEEN STR 42R TO STR 43R, L=0.245", W=0.135", D=0.002". SSI532180. REPLACED CLEAT IN FWD CARGO COMPARTMENT ON FRAME 24A BETWEEN STRINGER 42R TO STR 43R IAW SRM 51-72-11 ANDMay 13, 2015 · N354NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015051303217Skin · crackedDURING INSPECTION, FOUND CRACK ON OTBD FIXED L/E SKIN LOWER EDGE AT RIB 15 ON RT WING. PERFORMED PERMANENT REPAIR LOCATED ON OTBD FIXED L/E SKIN LOWER EDGE AT RIB 15 ON RT WING IAW SRM 57-41-11 PARA 5F, ITEM 3, STEP M, THRU STEP P, FIG 206.May 12, 2015 · N354NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2015051303215Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT AT AFT GALLEY AREA FROM FRAMES 65 - 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53474250.May 12, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015051303214Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON CLEAT IN FWD CARGO COMPARTMENT ON FRAME 24A AND STR 44. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53232949.May 12, 2015 · N354NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2015051203204Structure · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STR 23 RT, L=6", W=3", D=0.010". SSI 534147. REPLACED LOWER SILL AND FASTENERS AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 AND STR 23 RT IAW SRM A320 51-72-11 May 11, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015051003168Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT AT AFT GALLEY AREA FROM FRAMES 65 TO 66. INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 74250.May 10, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903167Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 68. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480505.May 9, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903166Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT +Y1225 AT AFT GALLEY AREA FROM FRAMES 66 TO 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72815.May 9, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903165Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1292 AT AFT GALLEY AREA FROM FRAMES 64 TO 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.May 9, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903164Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT +Y1162 AT AFT GALLEY AREA FROM FRAMES 68 TO 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472800.May 9, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903163Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162 AT AFT GALLEY AREA FROM FRAMES 68 TO 69. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472800.May 9, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903162Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1225 AT AFT GALLEY AREA FROM FRAMES 66 TO 68. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72800.May 9, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903161Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1292 AT AFT GALLEY AREA FROM FRAMES 64 TO 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.May 9, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903160Plate · crackedDURING INSPECTION, FOUND CRACK ON PLATE AT AFT GALLEY AREA FROM FRAMES 68 TO 69 AND STR 23 LT. REPLACED THE PLATE IAW SRM 51-72-11 AND DWG D534 80505.May 9, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903159Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y254 LOCATED FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53110984.May 8, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903158Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT +Y765 AT AFT GALLEY AREA FROM FRAMES 64 TO 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472090 AND D53472815.May 8, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903157Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 68 AT STR 23L. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D53480505.May 8, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903156Door Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER DOOR SILL FROM FRAME 66 - 68 STR 23L. REPLACED THE DOOR SILL IAW SRM 51-72-11 AND DWG D53480505.May 8, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050903155Seat Track · damagedDURING INSPECTION, FOUND SEAT TRACK, -Y1292, FRAMES 41 - 47 OUT LIMITS. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG NR D53370500.May 8, 2015 · N354NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2015050803134Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1292 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA L=1", W=0.500", D=0.003". REPLACED FLOORBEAM +Y1292 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWGS D53112812, D5May 7, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050803133Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y765 LOCATION BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA, L=0.800", W=0.400", D=0.004". REPLACED FLOORBEAM +Y765 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA IAW SRM 51-72-11 AND WINGS D53112812May 7, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050803132Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y254 LOCATED BETWEEN. FRAME 12 TO FRAME 24 AT FWD GALLEY AREA L=2", W=1, D=0.005. REPLACED FLOORBEAM +Y254 LOCATION BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA IAW SRM A320 51-72-11 AND DWG D53112816 AND DMay 7, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050803131Floor Support · crackedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1292 LOC. BETWEEN FR 12 TO FR.24 AT FWD GALLEY AREA L=1" W=0.800" D=0.003. REPLACED FLOORBEAM -Y1292 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53110984.May 7, 2015 · N354NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2015050803130Floor Support · crackedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y765 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA L=2", W=1", D=0.003". SSI 531189. REPLACED FLOORBEAM -Y765 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53110May 7, 2015 · N354NW · Airbus A320211 · Fuselage Miscellaneous Structure
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