N336NW

Service difficulty reports · 236

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 = 'N336NW' 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 DALA2014070103843Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 66 +5 - 70. REPLACED FLOOR SUPPORT IAW DWG D53472000 AND SRM 51-72-11.Jun 30, 2014 · N336NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR DALA2014070103842Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 64-66+5. REPLACED FLOOR SUPPOR IAW DWG D53472831 AND SRM 51-72-11.Jun 30, 2014 · N336NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014063003816Web · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN WEB LOCATED AT -Y1732 FRAME 20. REPLACED WEB IAW SRM 51-72-11 AND DWG D53114392.Jun 30, 2014 · N336NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014063003815Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE BETWEEN S40-41R ON FRAME 32 IN FWD CARGO BAY. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231586.Jun 29, 2014 · N336NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2014063003814Cover · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN JOINT COVER -Y81 BETWEEN FRAMES 12- 16. REPLACED JOINT COVER IAW SRM 51-72-11 AND DWG D53112620.Jun 29, 2014 · N336NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014062903813Shear Tie · corrodedDURING INSPECTION, FOUND CORROSION ON SHEAR TIE BETWEEN S41-42R ON FRAME 31 OF FWD CARGO BAY. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231586.Jun 29, 2014 · N336NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2014062903812Web · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN WEB -Y1732 AND FRAME 16. REPLACED WEB IAW SRM 51-72-11 AND DWG D531, 12780.Jun 29, 2014 · N336NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2014062803809Floor Support · corrodedDURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN FLOOR SUPPORT Y254 BETWEEN FRAMES 16-21. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53110984.Jun 27, 2014 · N336NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA14013753236Power Supply · inoperativeDURING NON ROUTINE CHECK, FOUND BATTERY BAD ON EMERGENCY LIGHT RIGHT POWER UNIT. MAINTENANCE REPLACED RT MID EMERGENCY POWER UNIT BATTERY AND FUNCTIONAL CHECK WAS NORMAL.Feb 27, 2014 · N336NW · Airbus A320211 · Emergency LightingSDR DALA13016883236Connector · inoperativeDURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHT AT SEAT 1AB INOPERATIVE. MX FOUND BROKEN WIRE AT SEAT TRACK CONNECTOR. INSTALLED NEW CONNECTOR AND SECURED ALL WIRES HARNESS UNDERNEATH SEAT AND FLOOR. FUNCTIONAL CHECK WAS NORMAL.Apr 12, 2013 · N336NW · Airbus A320212 · Light System WiringSDR DALA1019833236Light · inoperativeDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE LIGHT AT SEAT ROW 10L, 11L AND 12L INOPERATIVE. REPLACED EPSU AND BATTERY PACK. PERFORMED FUNCTIONAL CHECK AND CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.Aug 19, 2010 · N336NW · Airbus A320212 · Emergency LightingSDR DALA1019023236Skin · corrodedDURING L-CHECK, FOUND CORROSION ON FUSELAGE SKIN BETWEEN FR 69 & FR 70 ABOVE STINGER 34R. REPAIRED IAW SRM 53-41-11, SRM 51-44-11, SRM 51-52-11, FIG 205.Aug 11, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA1018983236Skin · gougedDURING "L" CHECK FOUND GOUGE ON FUSELAGE SKIN BETWEEN FR24 & FR25, STRINGER 42L & STRINGER 43L. REPAIRED IAW SRM 53-21-11, SRM 51-42-11.Aug 10, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA12004243236Skin · damagedDURING INSPECTIONS, FOUND LIGHTNING STRIKE AT FR60 BET STR 22L AND 23L BOTH RIVET AND ADJACENT SKIN. REMOVED BLIND FASTENER PER SRM 53-41-11. COMPLIED WITH NDT INSPECTION PER NTM 51-10-01, NO CRACKS FOUND. INSTALLED FASTENER PER SRM 53-41-11.Aug 9, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA12004233236Skin · damagedDURING INSPECTIONS, FOUND LIGHTNING STRIKE AT FR 55 BET STR 22L AND 23L BOTH RIVET AND ADJACENT SKIN. REMOVED BLIND FASTENER PER SRM 53-41-11. COMPLIED WITH NDT INSPECTION PER NTM 51-10-01, NO CRACKS FOUND. INSTALLED FASTENER PER SRM 53-41-11.Aug 8, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA12004223236Skin · damagedDURING INSPECTIONS, FOUND LIGHTNING STRIKE AT FR50 BET STR 20L AND 21L BOTH RIVET AND ADJACENT SKIN. REMOVED BLIND FASTENER PER SRM 53-41-11. PERFORMED INSPECTION NTM 51-10-01, NO CRACKS FOUND. REPLACED FASTENER PER SRM 53-41-11.Aug 8, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA12004213236Skin · damagedDURING INSPECTIONS, FOUND LIGHTNING STRIKE BET FR48 & 49 AT STR 21L BOTH RIVET AND ADJACENT SKIN. REMOVED FASTENER IAW SRM 51-42-11/53-00-11. HFEC IAW NTM 51-10-08, NO DEFECTS. REMOVED PAINT, NO DAMAGE FOUND ON SKIN IAW SRM 51-75-11. TREATED AND PRIMED AREAug 8, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA12004203236Skin · damagedDURING INSPECTIONS, FOUND LIGHTNING STRIKE AT 5TH RIVET FWD OF FR 69, STR 21L BOTH RIVET AND ADJACENT SKIN. REMOVED FASTENER PER SRM 53-41-11. PERFORMED BHEC PER NTM 51-10-11, NO CRACKS FOUND. REPLACED FASTENER PER SRM 53-41-11.Aug 8, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA12004293236Skin · damagedDURING INSPECTION, FOUND LIGHTNING STRIKE BET FR 51 AND 52 AT STR 22L BOTH RIVET AND ADJACENT SKIN. REMOVE BLIND FASTENER PER SRM 53-41-11. COMPLIED WITH NDT INSPECTION PER NTM 51-10-01. NO CRACKS FOUND. INSTALLED FASTENER PER SRM 53-41-11.Aug 8, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA12004283236Skin · damagedDURING INSPECTION, FOUND LIGHTNING STRIKE AT FR 52 BET STR 21L AND 22L BOTH RIVET AND ADJACENT SKIN. REMOVED BLIND FASTENER PER SRM 53-41-11. PERFORMED HOLE INSPECTION, NO CRACKS FOUND PER NTM 51-10-01. INSTALLED FASTENER PER SRM 53-41-11.Aug 8, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA12004273236Skin · damagedDURING INSPECTION, FOUND LIGHTNING STRIKE AT FR53 STR 22L BOTH RIVET AND ADJACENT SKIN. REMOVED BLIND FASTENER PER SRM 53-41-11. C/W NDT INSPECTION PER NTM 51-10-01 NO ITEMS. INSTALLED FASTENER PER SRM 53-41-11.Aug 8, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA12004263236Skin · damagedDURING INSPECTIONS, FOUND LIGHTNING STRIKE BET FR52 AND 53 AT STR 22L BOTH RIVET AND ADJACENT SKIN. REMOVED BLIND FASTENER PER SRM 53-41-11. PERFORMED HOLE INSPECTION, NO CRACKS FOUND PER NTM 51-10-01. REPLACED FASTENER PER SRM 53-41-11.Aug 8, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA12004253236Skin · damagedDURING INSPECTIONS, FOUND LIGHTNING STRIKE AT FR48 BET STR 22L BOTH RIVET AND ADJACENT SKIN. REMOVED BLIND FASTENER PER SRM 53-41-11. PERFORMED HOLE INSPECTION, NO CRACKS FOUND PER NTM 51-10-01. REPLACED FASTENER PER SRM 53-41-11.Aug 8, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA12004303236Skin · damagedDURING INSPECTION, FOUND LIGHTNING STRIKE AT FR 54 BET STR 22L AND 23L BOTH RIVET AND ADJACENT SKIN. REMOVED BLIND FASTENER PER SRM 53-41-11 (ID201079). PERFORMED HOLE INSPECTION, NO CRACKS FOUND PER NTM 51-10-01. INSTALLED FASTENER PER SRM 53-41-11.Aug 8, 2010 · N336NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA100333236Wire · disconnectedDURING A NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 15C INOPERATIVE. MX RECONNECTED A WIRE AND OPS CHECK WAS GOOD.Jan 12, 2010 · N336NW · Airbus A320212 · Light System WiringSDR NWAA084683236Attach Angle · corrodedDURING H CHECK FOUND CORROSION ON ATTACH FLANGE OF RT AFT PAX DOOR SILL PLATE. REPAIRED PER EA 32-214374.Sep 29, 2008 · N336NW · Airbus A320212 · Fuselage Main, Attach FittingsSDR NWAA071953236Power Supply · no testLEFT FORWARD EMERGENCY LIGHT POWER SUPPLY INTERNAL TEST FAILS (LIGHT HANGS UP). REPLACED LEFT FORWARD EMERGENCY LIGHT POWER SUPPLY CHARGER UNIT, TESTS OK.May 24, 2007 · N336NW · Airbus A320212 · Emergency LightingSDR 9904073236Cable · brokenUPON ARRIVAL AT THE GATE, THE LEFT REAR CABIN DOOR WAS OPENED WITH THE SLIDE ARMED BUT SLIDE DID NOT DEPLOY. MAINTENANCE REPLACED THE SLIDE PACK ASSEMBLY DUE TO A BROKEN SLIDE PACK RELEASE CABLE.Sep 14, 1999 · N336NW · Airbus A320212 · Escape SlideSDR 9718023236Battery · dischargedDURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILS COM LEFT, INT LOADS, ATT. REPLACED EPSU, OPERATIONAL CHECK OK.Sep 24, 1997 · N336NW · Airbus A320212 · Emergency LightingSDR 9715823236Oty Indicator · failedDURING CRUISE, THE GREEN HYDRAULIC SYSTEM QUANTITY AND PRESSURE INDICATED LOW. SHUT DOWN THE GREEN HYDRAULIC SYSTEM AND AIRCRAFT DIVERTED TO DTW. MANUALLY EXTENDED THE LANDING GEAR AND THE AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO THE GATE. RAug 19, 1997 · N336NW · Airbus A320212 · Hydraulic Quantity IndicatorSDR 9707083236Actuator · lockedDURING APPROACH, THE LEADING EDGE SLATS REMAINED IN THE RETRACTED POSITION AFTER SELECTING FLAPS POSITON ONE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND SELECTED FLAPS POSITION THREE. TRAILING EDGE FLAPS EXTENDED NORMALLY. DECLARED AN EMERGENCY AND LANApr 4, 1997 · N336NW · Airbus A320212 · Leading Edge Slat ActuatorSDR 9623933246Power Supply · malfunctionedDURING LINE MAINTENANCE, TEST OF THE EMERGENCY LIGHTS FAULTED INT LOADS FWD-L AND COMM FWD-L. REPLACED EPSU, OPERATIONAL CHECK OK.Nov 9, 1996 · N336NW · Airbus A320211 · Emergency LightingSDR 9623213236Battery · dischargedDURING THE LINE MAINTENANCE EMERGENCY LIGHTS TEST, THE FOLLOWING MESSAGES DISPLAYED: INT LOADS AFT L, COMM FWD L, BATTERY AFT L, EMER L, COMM AFT L. REPLACED AFT LEFT BATTERY PACK, OPERATIONAL CHECK OK.Oct 31, 1996 · N336NW · Airbus A320212 · Emergency LightingSDR 9605033236Prox Sensor · malfunctionedDURING APPROACH, RECEIVED L/G DOORS NOT CLOSED MESSAGE AFTER LOWERING THE LANDING GEAR. ALSO, THE WHEEL PAGE ON ECAM DISPLAYED ONE RED GEAR TRIANGLE. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE Mar 2, 1996 · N336NW · Airbus A320211 · Landing Gear Position and WarningSDR 9605003236Interface Units · malfunctionedON THE WHEEL PAGE OF THE ECAM, THE NOSE LANDING GEAR TRIANGLE INDICATED RED WITH THE GEAR DOWN. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 AND NR 2 LANDING GEAR CONTROL INTMar 1, 1996 · N336NW · Airbus A320211 · Landing Gear Position and WarningSDR 9602903236Idg · malfunctionedDURING CLIMBOUT, THE NR 2 ENGINE INTEGRATED DRIVE GENERATOR LOW OIL PRESSURE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE INTEGRATED DRIVE GENERATOR, LEAK AND OPERATIONAL CHECK OK.Feb 4, 1996 · N336NW · Airbus A320211 · AC Generator-Alternator
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