N352NW
Service difficulty reports · 179
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 = 'N352NW' 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.
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 = 'N352NW' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2021021900974Bushing · corrodedSHIP 3252 CORROSION RUDDER HINGE FIXED BUSHING ATTACH FITTING HINGE NR 7 ( RUDDER SIDE) ON VERTICAL STABILIZER (2 EA). CORRECTIVE ACTION: REPLACED BUSHINGS PER AIRBUS SRM 51-72-12. (1733651)SDR DALA2021021900973Bearing · corrodedSHIP 3252 CORROSION BEARING IB FLAP (MAIN ECCENTRIC BEARING) ON RT WING (1 EA). CORRECTIVE ACTION: REPLACED BEARING PER AIRBUS CMM 57-52-21. (1733632)SDR DALA2021021800936Support Bracket · corrodedSHIP 3252 CORROSION AFT ATTACHMENT SUPPORT BRACKET BEARING AT PYLON LT (2EA). CORRECTIVE ACTION: REMOVED AND INSTALLED NEW BEARING PER A320 FAM AMM 54-51-17.SDR DALA2021021700896Profile · crackedSHIP 3252 CRACK ON EMERGENCY EXIT DOOR 844 RH AFT LOAD TRANSMITTING PROFILE FWD. DOOR LOCATED IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FWD LOAD TRANSMITTING PROFILE PER A320 SRM 51-72-11 AND 51-42-11. OK FOR SERVICE. (1732082)SDR DALA2021021700892Floor Support · corrodedSHIP 3252 CORROSION FLOOR BEAM -Y1292 LOCATED FROM FR12 TO FR24 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (1732182)SDR DALA2024032103605Skin · gougedA GOUGE WAS FOUND IN EXTERNAL FUSELAGE SKIN BETWEEN FR50 - FR51 AND STR 40L - STR 42L. C/A: ***DTE REQUIRED*** PER SECTION DET OF 589897-14, THE REPAIR OF SECTION I IS LIMITED TO 63,000 FC / 132,000 FH TOTAL FROM FIRST FLIGHT (WHICHEVER COMES FIRST). ADDITIONASDR DALA2021021600858Control Cable · deterioratedSHIP 3252 DETERIORATED PASSENGER CREW DOOR 832 FLEXIBLE CONTROL CABLE OF EMERGENCY ESCAPE SLIDE MECHANISM. CORRECTIVE ACTION: REPLACED PASSENGER CREW DOOR 832 FLEXIBLE CONTROL CABLE PER DELTA WORK CARD AMDS 5210-7089. OPS CK GOOD. (1730655)SDR DALA2021021600855Strut · corrodedSHIP 3252 CORROSION IB FLAP INTERCONNECTING STRUT ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT PER DELTA WORKCARDS AMDS 2750-6010-LT AND 2750-6020-LT. (1730439)SDR DALA2021021600854Shear Tie · gougedSHIP 3252 GOUGE SHEAR TIE LOCATED AT FR 25 AND BTW STR 36L TO STR 37L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11. (1729201)SDR DALA2021021200820Strut · corrodedSHIP 3252 CORROSION IB FLAP INTERCONNECTING STRUT ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT RH PER DELTA WORKCARD AMDS 2750-6010-RT AND 2750-6020-RT. (1728301)SDR DALA2021020900747Door · out of adjustSHIP 3252 PASSENGER CREW DOOR 841 OUT OF ADJUSTMENT. CORRECTIVE ACTION: PERFORMED ADJUSTMENT ON PASSENGER CREW DOOR PER A320 FAM AMM 52-11-14. OK FOR SERVICE. (1725109)SDR DALA2021020900746Skin · damagedSHIP 3252 BROKEN SLAT 2 TRAILING EDGE AND IB SIDE ON LH WING. PERFORMED PERMANENT REPAIR PER A320 SRM 57-43-21. (1725165)SDR DALA2021020400671Seat Track · corrodedSHIP 3252 CORROSION SEAT TRACK +Y765 AND FR20 AT FWD GALLEY AREA. CORRECTIVE ACTION REPLACED SEAT TRACK PER A320 SRM 51-72-11.SDR DALA2021020400669Web · corrodedSHIP 3252 CORROSION WEB LOCATED -Y1732 AND FR20 AT FWD GALLEY AREA. CORRECTIVE ACTION REPLACED WEB PER A320 SRM 51-72-11.SDR DALA2020090983017Gust Lock · inoperativeSHIP 3252, MAIN DOOR GUST LOCK WILL NOT ENGAGE. CORRECTIVE ACTION: CLEANED AND EXERCISED GUST LOCK MECHANISM. OPS CHK GOOD.SDR DALA2020071902603Lamp · inoperativeEXTERIOR LEFT OVERWING EMERGENCY EXIT LIGHTS INOP, REPLACED THE LAMPS FOR THE LEFT OVERWING EXTERIOR EMERGENCY EXIT LIGHTSSDR DALA2019123107667Fitting · damagedL/H INBD FLAP TRUNNION FITTING FOUND DAMAGED BEYOND REPAIR, REPLACED L/H INBD FLAP TRUNNION FITTING PER ERA 584216-14AD REV " O"SDR DALA2019102546147Light · brokenSEAT 12D EMERGENCY LIGHT HOLDER ASSY BROKEN, REPLACED SEAT 12D EMERGENCY PATH LIGHT ASSYSDR DALA2019101415876Plenum · abnormalBURNED OIL TYPE ODOR ON BOARD WITH APU SUPPLY BLEED TO PACKS, FOUND APU COMPARTMENT INTAKE PLENUM CONTAMINATED WITH OIL, DEEP CLEANED APU COMPARTMENT AND REPLACED APUSDR DALA2019100435678Battery Pack · no testEMERGENCY LIGHT TEST FAULT "EPSU BATT EMER R" MSG DISPLAYED, REPLACED BATTERY PACK (12WL)SDR DALA2019040752269Pressure Panel · crackedCRACK INDICATION ON INTERNAL STRUCTURE FITTING HOLE #7 OF THE PRESSURE PANEL LOC. FR 36 AND Y+1295 LEFT SIDE IN FWD CARGO COMPARTMENT .(CRACK INDICATION 6 O"CLOCK), REPLACED FITTING OF THE PRESSURE PANEL LOC. AT FR.36 AND AT LEVEL STR.30 Y+1295 ON INTERNAL STRSDR DALA2019040752271Beam · crackedCRACK INDICATION ON FRAME 35 TO FR 36 LH SIDE LOCATED AT LONGITUDINAL BEAM AT HOLE ''A'' PRESSURE FLOOR PANEL ON LOWER FUSELAGE (1 EA) .(CR ACK POSITION AT 9 O'CLOCK. REPAIR IN ACCORDANCE WITH WORK CARD 5311-01 171-04A PRIOR TO FURTHER FLIGHT,"AA 5311-01171","SDR DALA2019021501068Switch · malfunctionedEMERGENCY CABIN LIGHTS CAME ON AND WENT TO OFF DURING FLIGHT. ON TOUCHDOWN LIGHTS RE-ILLUMINATED. RESET BOTH EMERGENCY LIGHT SWITCHES. OPERATION CHECKS OKAY.SDR DALA2019012700606Unknown · fumesCLIMBING THROUGH 300 AGL COCKPIT BEGAN TO SMELL LIKE WET MOLDY MILDEW SOCK. GOT STRONGER UNTIL 8000FT WHEN SMELL TAPERED OFF. GONE Y 23000FT. MAINTENANCE ISOLATED SOURCE OF FUMES TO ENGINE NR 1. PERFORMED WC 7900-2001. NO DEFINITE FINDINGS. PERFORMED VERIFICATSDR DALA2018091105560Filter · odorOIL SMELL IN COCKPIT CLOSE TO LANDING IN MCO. SMELL CLEARED AFTER LANDING. MAINTENANCE COMPLIED WITH NO GO ODI PREVENTION PROGRAM. BOROSCOPED BOTH ENGINES. REPLACED OZONE AND RECIRC FAN FILTERS. PERFORMED HIGH POWER RUNS. NO ODOR. MCC NOTIFIED.SDR DALA2021012500466Skin · corrodedTOP SKIN CORROSION REPAIRED, PER ERA 533453-14 SECT I, APPROVED AS PERM, CAT 'B'. NEW RDAS CHANGES REP INSP INTERVAL, A/C TYPE EFFECT. CORRECTIVE ACTION: PERFORMED DVI ON REWORKED AREA LOCATED CENTER WING BOX UPPER SKIN PANEL UPPER SURFACE FR 42 AND Y1292, ASDR DALA2017050103530Engine · leakingCONDITION AIR STINKS, BORESCOPED HPC1 AND 2, DISCOVERED OIL ON ALL BLADES, PRESENCE OF OIL AT BOOSTER OUTLET. REPLACED POWERPLANT AND REPLACED LT AND RT CABIN AIR RECIRCULATION FILERS AND LEFT PACK OZONE FILTER.SDR DALA2016112108991Structure · crackedCORROSION AND CRACK INDICATION AT FWD LT PASSENGER DOOR FASTENER. OVERSIZED REAMED HOLE AND INSTALLED FASTENER.SDR DALA2016112108990Structure · crackedCORROSION AND CRACK INDICATION AT FWD LT PASSENGER DOOR FASTENER. OVERSIZED REAM AND INSTALLED FASTENER.SDR DALA2016112108989Structure · crackedCORROSION AND CRACK INDICATIONS FWD RT PASSENGER DOOR FASTENER FWD 2ND FASTENER DOWN AREA B FR 20. REAM OVERSIZED HOLE, INSTALLED FASTENER.SDR DALA2016112108988Structure · crackedCORROSION AND CRACK INDICATION AT FWD RT PASSENGER DOOR FASTENER. REAM OVERSIZED HOLE, INSTALLED FASTENER.SDR DALA2016112108987Structure · crackedCORROSION AND CRACK INDICATIONS FWD RT PASSENGER DOOR FASTENER. OVERSIZE REAMED HOLE AND INSTALLED FASTENER.SDR DALA2016112108986Structure · crackedCORROSION AND CRACK INDICATION AT FWD RT PASSENGER DOOR FASTENER. OVERSIZE REAMED AND INSTALLED FASTENER.SDR DALA2016112108985Structure · crackedCORROSION AND CRACK INDICATION AT FWD LT PASSENGER DOOR FASTENER. REAM OVERSIZED HOLE AND INSTALLED FASTENER.SDR DALA2016112108984Structure · crackedCORROSION AND CRACK INDICATION AT FWD LT PASSENGER DOOR FASTENER. REAM OVERSIZED HOLE AND INSTALLED FASTENER.SDR DALA2016112108983Structure · crackedCORROSION AND CRACK INDICATION AT FWD RT PASSENGER DOOR FASTENER. REAM OVERSIZED HOLE AND INSTALLED FASTENER.SDR DALA2015112107247Gearbox · leakingPILOT REPORTED VERY STRONG ODOR, CHEMICAL LIKE, PRESENT IN CABIN AND COCKPIT UPON BOARDING AND ALL OF FLIGHT. IRRITATING TO EYES, CAPTAIN, AND VERY BOTHERSOME. APU GENERATOR OIL DRAIN PLUG DRIPPING ON TO PLENUM. REPLACED SEAL WASHER, FOUND OIL LEAKING FROM SDR DALA2016112209108Frame · corrodedOUT OF LIMITS CORROSION SPOTS FOUND ON THE INBD FLANGE OF FRAME 20 RT. REPAIRED IAW ER/A.SDR DALA2016112209107Support · corrodedCORROSION FOUND ON RIB GEAR SUPPORT AT RIB 5 AREA OF LT WING. REPAIRED IAW ER/A.SDR DALA2015040102531Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 43L IN AFT CARGO COMPARTMENT BETWEEN FRAME 56 TO FRAME 58+3", L=7.000", W=1.000", D=0.004", MEASURES APPROXIMATELY SSI 534107, CARD 534107. CARD 5320-5012-DE ATTACH FROM 5100-3201. IF CORROSION IS LEVEL 2 OR GRESDR DALA2015040102530Web · corrodedDURING INSPECTION, FOUND CORROSION ON WEB LOWER SURFACE AT LEVEL STR 38L IN AFT CARGO COMPARTMENT BETWEEN FRAME 58 TO FRAME 59, L=1.500", W=1.000", D=0.002". MEASURES APPROXIMATELY SSI 534107. REPLACED WEB LOWER SURFACE AT LEVEL STR 38L IN CARGO COMPARTMENT SDR DALA2015033102528Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL LT SIDE AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68, L=2", W=1", D=0.003". REPLACED LOWER SILL LT SIDE AND FASTENERS LOCATED ON AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 IAW SRM 51-72-11 AND DWG NR D53480019.SDR DALA2015033102527Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE BEAM, Y1292 AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66, L=5", W=2", D=0.003". REPLACED FLOORBEAM Y1292 LOCATED AT AFT GALLEY AREA FROM FRAME 64 TO FRAME 66 IAW SRM 51-72-11 AND DWG D53472815.SDR DALA2015033102526Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE BEAM -Y310 AT AFT GALLEY AREA FROM FRAME 65 TO FRAME 67, L=2", W=1", D=0.003". REPLACED FLOORBEAM -Y318 AT AFT GALLEY AREA FROM FRAME 65 TO FRAME 67 IAW SRM 51-72-11, DWG D534 72814.SDR DALA2015033102525Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM -Y1162 AT AFT GALLEY AREA FROM FRAME 68 TO FRAME 69, L=5", W=3", D=0.003". REPLACED FLOORBEAM -Y1162 AT AFT GALLEY AREA FROM FRAME 68 TO FRAME 69 IAW SRM 51-72-11 AND DWG D53472000.SDR DALA2015033102524Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE BEAM -Y1292 AT AFT GALLEY AREA ON FRAME 66, L=1", W=0.50", D=0.002". REPLACED FLOORBEAM -Y1292 AT AFT GALLEY AREA LOCATED BETWEEN FRAME 64 TO FRAME 66 IAW SRM 51-72-11 AND DWG D534 72816.SDR DALA2015033102523Floorbeam · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR STRUCTURE BEAM BETWEEN Y1292 AND Y1162 AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68, L=8", W=3", D=0.004". REPLACED FLOORBEAM BETWEEN Y1292 AND Y1162 AFT GALLEY AREA FROM FRAME FR 68 IAW SRM 51-72-11 AND DWG D534 SDR DALA2015033102522Support · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL AT STR 23R AT AFT GALLEY AREA FROM FRAME 66 TO FRAME 68, L=0.500", W=0.300", D=0.002". REPLACED LOWER SILL AT STR 23R AFT GALLEY AREA FROM FRAME 66 TO FRAME 68 IAW SRM 51-72-11.SDR DALA2015033102521Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 68 LT SIDE AT AFT GALLEY AREA. REPLACED CORNER FITTING LOCATED FRAME 68 LT SIDE AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.SDR DALA2015033002520Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOORBEAM +Y1162 AT AFT GALLEY AREA FROM FRAME 68 TO FRAME 69, L=3", W=2", D=0.003". REPLACED FLOORBEAM +Y1162 AT AFT GALLEY AREA FROM FRAME 68 TO FRAME 69 IAW SRM 51-72-11 AND DWG D53472800.
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