N341NW
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 = 'N341NW' 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 = 'N341NW' 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 DALA2016092006760Frame · gougedDURING AN L-CHECK, MAINTENANCE FOUND A GOUGE LOCATED AT STR 6L ON THE FLANGE OF FRAME 47. BLEND OUT THE GOUGE IAW ER/A 550853-14, REV 0.SDR DALA2016011800387Wire · brokenEMERGENCY LIGHT IN SEAT 16ABC INOPERATIVE. REPAIR BROKEN WIRE 16ABC.SDR DALA2015070904192Wire · brokenFOUND EMERGENCY LIGHT AT 5 & 6 ABC INOPERATIVE. REPAIRED BROKEN WIRE AT 5 ABC IAW ESPM 20. INSERTED LOOSE PIN IN CONNECTOR AT 6 ABC BOTH AND FUNCTIONAL CHECK WAS NORMAL.SDR DALA2014101705605Power Supply · no testDURING PERFORMANCE OF EMERGENCY LIGHT SYSTEM TEST ON CIDS PANEL. FAULTED EPSU EXT LOAD AFT L. MAINTENANCE REPLACED AFT L EPSU AND FUNCTIONAL CHECK WAS NORMAL AND R2 DOOR EXIT SIGNS ILLUMINATED.SDR DALA2014091705068Profile · crackedDURING INSPECTION, FOUND A CRACK ON RT LOAD TRANSMITTING PROFILE OF THE EMERGENCY EXIT DOOR 843 INTERNAL STRUCTURE. REPLACED TRANSMITTING PROFILE OF THE EMERGENCY EXIT DOOR 843 INTERNAL STRUCTURE IAW SRM 51-72-11 AND DWG D52279021.SDR DALA2014091705067Profile · crackedDURING INSPECTION, FOUND A CRACK ON LT LOAD TRANSMITTING PROFILE OF THE EMERGENCY EXIT DOOR 833 INTERNAL STRUCTURE. REPLACED LT LOAD TRANSMITTING PROFILE OF THE EMERGENCY EXIT DOOR 833 INTERNAL STRUCTURE IAW SRM 51-72-11 AND DWG D52279040.SDR DALA2014091705066Profile · crackedDURING INSPECTION, FOUND A CRACK ON RT LOAD TRANSMITTING PROFILE OF THE EMERGENCY EXIT DOOR 833 INTERNAL STRUCTURE. SSI 522102-01-1. REPLACED RT LOAD TRANSMITTING PROFILE OF THE EMERGENCY EXIT DOOR 833 INTERNAL STRUCTURE IAW SRM 51-72-11 AND DWG D52279040.SDR DALA2014091605053Stringer · corrodedDURING INSPECTION, CORROSION ON STRINGER 42L BETWEEN FRAMES 56 - 57. REPAIRED IAW ER/A 528117-14 AND PRI 528117-14 REVISION 0.SDR DALA2014091605052Stringer · corrodedDURING INSPECTION, FOUND CORROSION ON STRINGER 43L BETWEEN FRAMES 56 - 57. REPLACED THE STRINGER IAW ER/A 528117-14 AND PRI 528117-14.SDR DALA2014091205008Door Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER DOOR SILL STRINGER 23L AND BETWEEN FRAMES 66 - 68. REPLACED LOWER DOOR SILL IAW SRM 51-72-11 AND DWS D53480505 AND D53470150.SDR DALA2014091004965Door Sill · corrodedDURING INSPECTION, FOUND CORROSION ON LOWER SILL IN AFT PAX CABIN LOCATED AT STR 23R AND BETWEEN FR 66 TO FR 68. MEASURES: L=1.750, W=1", D=0.002", APROXIMATELY SSI 534147. REPLACED LOWER SILL IN AFT PAX CABIN LOCATED AT STR 23R AND BETWEEN FRAME 66-FRAME 6SDR DALA2014090904964Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FR16 TO FR20 AT LEVEL OF STRG 23L IN FWD PAX CABIN MEASURE L=0.130", W=0.032", D=0.008" APPROXIMATELY, SSI531180. REPLACED CENTER FITTING LOCATED BETWEEN FRAME 16 TO FRAME 20 AT LEVEL OF STRSDR DALA2014090804934Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1292 BETWEEN FRAMES 64 - 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-75-11 AND DWG D53472831.SDR DALA2014090804933Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1225 BETWEEN FRAMES 66+5 - 67 +15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.SDR DALA2014090804932Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.SDR DALA2014090704931Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CORNER FITTING FRAME 68. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53480505.SDR DALA2014090704930Floorbeam · crackedDURING INSPECTION, FOUND CRACK ON UPPER FLANGE OF FLOORBEAM FRAME 26 Y-254. REPAIRED IAW SRM 53-21-14, PARAGRAPH 5.A, FIG 201, PAG 202-206, 207-208.SDR DALA2014090604929Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y160 BETWEEN FRAMES 68 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72000, D534 74250.SDR DALA2014090504925Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 64 - 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472831.SDR DALA2014090504924Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 20 - 21 Y-189. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.SDR DALA2014090504923Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAME 66 +5 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472815.SDR DALA2014090504922Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y160 BETWEEN FRAMES 68 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472097.SDR DALA2014090504921Fitting · corrodedDURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FRAME 66 TO FRAME 68. REPLACED CENTER FITTING IAW SRM 51-72-11 AND DWG D53480505.SDR DALA2014090504920Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y765 BETWEEN FRAMES 66+5 - 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472816.SDR DALA2014090504919Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWG D53472000, AND D53470150.SDR DALA2014062603784Wire · brokenDURING NON-ROUTINE CHECK, FOUND SEAT 4 ABC EMERGENCY LIGHT OUT. MAINTENANCE REPAIRED BROKEN WIRE AND FUNCTIONAL CHECKED NORMAL.SDR DALA14005743241Decoder · failedF/A REPORTED EMERGENCY EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED DECODER-ENCODER UNIT AND FUNCTIONAL CHECKED NORMAL.SDR DALA12015443241Connector · damagedDURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT ROW 18ABC INOPERATIVE. MX REPAIRED CONNECTION AND FUNCTIONAL CHECK WAS NORMAL.SDR DALA12002923241Wire Harness · damagedDURING NON ROUTINE CHECK, FOUND SEAT ROW 24 ABC EMERGENCY PATH LIGHT INOPERATIVE. MAINTENANCE REPLACED ROW 24 SEAT HARNESS AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR DALA12001583241Lamp · inoperativeEMERGENCY LIGHT BULBS IN THE CABIN EXIT SIGNS INOPERATIVE. MAINTENANCE RELAMPED AND FUNCTIONAL CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR DALA1202053241Light · inoperativeAT LGA, FLIGHT CAPTAIN FOUND DOOR 1R EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE SECURED LIGHT ASSEMBLY IN HOUSING AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED SERVICE.SDR DALA1152263241Skin · puncturedDURING GEAR CHANGE IN MSP, MTC PUNCTURED THE FUSELAGE SKIN WITH THE STABILIZING JACK LOCATED AT FRAME 73 AND STRINGER 33LH. REPAIRED PER ER/A 495955-14.REV ORIGINAL.SDR DALA1151643241Skin · puncturedFUSELAGE SKIN - PUNCTURED ADJACENT TO AFT TAIL JACK PAD LT SIDE. REMOVED DAMAGE WITH 3.125"X4" CUTOUT PER A320 SRM 53-00-11. FABED DOUBLER PER A320 SRM 53-00-11. INST DOUBLER IAW ER/A 495955-14 REV 1 AND AIRBUS A320 SRM 53-00-11 FIG 203.SDR DALA1150923241Wire Harness · damagedDURING EMERGENCY LIGHT TEST FOUND SEAT ROW 9 PATH RED LIGHT INOP. REPAIRED SEAT HARNESS DISC PIN AND TESTS OK.SDR DALA1149583241Slat · dentedON WALK AROUND, FOUND BIRD STRIKE ON L/E OF RT WING NR 2 SLAT, INBD END, DENT MEASURES APPROX 147MM X 100MM X 6MM DEPTH. OUT OF LIMITS PER SRM 57-40-00 FIG 101 & 102. DENT, WITHIN TEMP REPAIR LIMITS PER SRM 57-40-00. REWORKED DENT PER SRM 51-73-00. REWORKSDR DALA1142673241Connector · not seatedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT 1L FAILED TEST OF EPSU INTERNAL LOAD. MAINTENANCE RESEATED ELECTRICAL CONNECTOR AT EMERGENCY POWER SUPPLY UNIT AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.SDR DALA1034623241Floorboard · damagedDURING LINE CHECK FOUND AFT CARGO FLOORBOARD 151GF DAMAGED. R & R AFT CARGO FLOORBOARD 151GF IAW MM. OK FOR SERVICE.SDR DALA1029073241Seat Track · corrodedDURING L-CHECK FOUND CORROSION ON SEAT TRACK AT BS Y254 BETWEEN FR 18 - FR 20. REPAIRED PER SRM 51-42-11, SRM 51-74-00 & 53-11-15.SDR DALA1029063241Floorbeam · crackedFWD CABIN FLOORBEAM +Y254 BET FR 24 AND FR 25 CRACKED. TRIMMED OUT CRACKED AREA DIM: W=1" X L=3.470" IAW SRM 53-00-14 FIG 204. FABRICATED DOUBLER FROM 7075T6.063 BATCH 1502238. FABRICATED FILLER REPAIR FROM 7075T6.063 BATCH 1766127 IAW SRM 53-00-14 FIG 204.SDR DALA1028603241Panel · damagedDURING L-CHECK FOUND DAMAGE TO CARGO PANEL 131AF. REPLACED PER SRM 53-02-00 FIGURE 205.SDR DALA1028593241Floor Support · corrodedDURING L-CHECK FOUND CORROSION ON FLOOR SUPPORT AT Y765 FR 18- FR 21. REPAIRED PER SRM 51-42-11 & SRM 51-44-11.SDR DALA1027963241Strap · corrodedDURING L CHECK FOUND CORROSION ON FLOORBOARD STRAP AT BETWEEN Y254 & Y254 FR 20. REPAIRED PER SRM 51-42-11, SRM 53-11-27 FIGURE 16, SRM 51-21-10 & SRM 51-75-12.SDR DALA1010383241Wire · brokenDURING A NON ROUTINE CHECK, FOUND SEAT 6C ABC EMERGENCY LIGHT INOPERATIVE. MX REPAIRED BROKEN WIRE AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.SDR DALA108963241Wire · damagedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 16C INOPERATIVE. MX REPAIRED WIRE AT CONNECTOR AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.SDR NWAA085333241Lamp · inoperativeEMERGENCY EGRESS LIGHTING INOP ON ROWS 15, 16, 17, 21, 22, 23. RELAMPED AND REPLACED EPSU 11WL. CHECKS OK.SDR 0203883241Transmitter · malfunctionedFLIGHT CREW ABORTED TAKE-OFF AT 110 KNOTS DUE TO ENGINE NR 1 OIL QUANTITY INDICATION RAPID DECREASE. AIRCRAFT RETURNED TO GATE. MAINTENANCE FOUND ENGINE NR 1 TANK FULL AND NO ENGINE OIL LEAKS. REPLACED OIL QUANTITY TRANSMITTER.SDR 9802903241Engine · failedDURING CRUISE FLIGHT, NR 1 ENGINE FUEL FILTER CLOG ECAM ANNUNCIATED. FLIGHT CREW DIVERTED AIRCRAFT TO MEM. NR 1 ENGINE SHUT DOWN 20 MILES FROM MEM. AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE FOUND THE FUEL FILTER CONTAMINATED WITH BRONZE PARTICLES ANSDR 9802983241Sill · corrodedDURING PERIODIC CHECK, FOUND CORROSION AT THE LEFT AFT PASSENGER DOOR SILL PLATE. REPAIRED PER EA 32-154912.SDR 9707713241Engine · tailpipe fireAFTER PUSHBACK, GROUND PERSONNEL REPORTED FLAMES OUT OF NR 1 ENGINE TAIL PIPE. THE NR 1 ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE BOROSCOPE INSPECTED AND GROUND RUN ENGINE. NO DISCREPANCIES REPORTED.SDR 9625253241Battery · dischargedDURING LINE MAINTENANCE CHECK, THE EMERGENCY LIGHTS TEST FAULTED AFT LEFT UNIT. REPLACED BATTERY PACK, OPS CHECK OK.
Back to N341NW