N228NW

Service difficulty reports not matched to an aircraft · 26

They name N228NW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N228NW' AND registry_match IS NULL
  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 0102941228Bolt · backed outON WALKAROUND, FOUND LEFT MAIN LANDING GEAR DOOR EXTENDED. SUBSEQUENT INSPECTION FOUND SUPPORT BOLT IN MAIN LANDING GEAR SIDE BRACE ATTACH FITTING BACKING OUT. REMOVED, INSPECTED, AND REINSTALLED SIDE BRACE ATTACH FITTING WITH NEW BOLTS AND BARREL NUTS. OPEAug 18, 2001 · N228NW · Doug DC1030 · Landing Gear DoorsSDR 0100901228Fire Loop · faultyEN ROUTE, ENGINE FIRE LIGHT ON FORWARD PANEL FLASHED INTERMITTENTLY. NR 3 START LEVER, NR 3 ENGINE FIRE HANDLE, AND NR 3 ENGINE LOOP ''A'' ALL CAME ON INTERMITTENTLY AND INCREASED IN FREQUENCY AND INTENSITY. REPLACED A AND B FAN AND CORE LOOP ASSEMBLIESFeb 24, 2001 · N228NW · Doug DC1030 · Fire DetectionSDR 9806331228Compressor · stalledDURING TAKEOFF AT ROTATION, THE NR 3 ENGINE COMPRESSOR STALLED SEVERAL TIMES WITH VISIBLE FIRE REPORTED BY THE TOWER AND FLIGHT ATTENDANT. NOTICEABLE FUEL FLOW DECREASE AND POWER LOSS OCCURRED. BOTH FIRE BOTTLES FOR THE NR 3 ENGINE WERE DISCHARGED AND THE ENApr 6, 1998 · N228NW · Doug DC1030 · Turbine Engine Compressor SectionSDR 9804091228Bleed Duct · leakingDURING CLIMB AND CRUISE, NR 1 NACELLE TEMPERATURE WAS 200C WITH PNEUMATIC TEMPERATURE INDICATOR AT 20C AND PNEUMATIC PRESSURE AT 10 PSI. NACELLE TEMPERATURE WAS REDUCED BY REDUCING N1 TO 80 PERCENT. SHUTTING NR 1 PNEUMATIC SUPPLY OFF HAD NO EFFECT ON NACELLEMar 9, 1998 · N228NW · Doug DC1030 · Pneumatic Distribution SystemSDR 9716471228Skin · crackedDURING L-CHECK, FOUND CRACK IN LEFT WING FIXED LEADING EDGE STA XOS 610. REPAIRED PER EA 12-150746.Aug 26, 1997 · N228NW · Doug DC1030 · Wing, Plate/SkinSDR 9626031228Pneu Ind Syst · malfunctionedDURING CRUISE, THE NR 2 MANIFOLD FAIL LIGHT ILLUMINATED. FLIGHT DIVERTED TO NRT AND DUMPED 30,000 LBS OF FUEL. NR 2 PNEUMATIC INDICATION SYSTEM WAS PLACED ON MEL 36-1D AND 36-10A.Dec 9, 1996 · N228NW · Doug DC1030 · Pneumatic Indicating SystemSDR 96ZZZX4187Rate Gyro · failedDURING CHECK, UPPER YAW DAMPENER FAILED SYSTEM NR 2 TEST ON FLIGHT GUIDANCE MANAGEMENT ASSESSMENT PANEL. TROUBLESHOT FOUND B-CHANNEL YAW RATE GYRO INOP. ALSO, FOUND RESISTANCE OF A AND B ON LVDT IS LOWER THAN NORMAL. REMOVED AND REPLACED RATE GYRO. REMOVEDMay 6, 1996 · N228NW · Doug DC1030 · Autopilot SystemSDR 96037122820Actuator · failedDURING CHECK, UPPER YAW DAMPENER FAILED SYSTEM NR 2 TEST ON FLIGHT GUIDANCE MANAGEMENT ASSESSMENT PANEL. TROUBLESHOT FOUND B-CHANNEL YAW RATE GYRO INOP. ALSO, FOUND RESISTANCE OF A AND B ON LVDT IS LOWER THAN NORMAL. REMOVED AND REPLACED RATE GYRO. REMOVEDMay 6, 1996 · N228NW · Doug DC1030 · Rudder ActuatorSDR 96035122819Valve Assy · leakingDURING CHECK, FOUND NR 1 ENGINE FIRE HANDLE HYDRAULIC SHUT-OFF VALVE LEAKS INTERNALLY. REMOVED, REPLACED, AND RIGGED NR 1 ENGINE FIRE HANDLE HYDRAULIC SHUT-OFF VALVE ASSY IAW MM 29-15-1. MAINTENANCE ACCOMPLISHED BY LOCKHEED AEROMOD CENTER. (X)Apr 24, 1996 · N228NW · Doug DC1030 · Engine Emergency Shutdown SystemSDR 96034122818Tip · lightning strikeDURING CHECK, FOUND LIGHTNING STRIKE DAMAGE 1 INCH BY .25 INCH AT UPPER TIP OF UPPER AFT RUDDER. REMOVED DAMAGE IAW SRM 55-41-01, VOLUME III, SRM'S 51-35-01, 51-35-02, 54-41-01. MAINTENANCE ACCOMPLISHED BY LOCKHEED AEROMOD CENTER. (X)Apr 24, 1996 · N228NW · Doug DC1030 · Rudder StructureSDR 96032122816Cover · corrosionDURING CHECK, CORROSION WAS FOUND ON 5 FUEL TANK PROBE COVER PLATES ON THE MATING SURFACE. THE PART NUMBERS ARE: 003-001-001, 003-001-002, 003-001-006. CORROSION WAS REMOVED TO A MINIMUM THICKNESS OF 0.160 INCH TRANSITION RADIUS BETWEEN HORIZONTAL AND VERTIApr 24, 1996 · N228NW · Doug DC1030 · Wing, Plate/SkinSDR 96ZZZM1541Longeron · corrodedFOUND SEVERE EXFOLIATION ON LONGERON STRAP 36RT NEAR FS 1801 CENTER CARGO COMPARTMENT. REMOVED AND REPLACED 2 ANGLES AND 1 STRAP ON LONGERON 36RT SPLICE AT FS 1801 CENTER CARGO COMPARTMENT IAW SRM 53-00-01 AND 51-33-01. (M)Mar 11, 1996 · N228NW · Doug DC1030 · Fuselage Main, Longeron/StringerSDR 96019122814Jamb · corrosionCORROSION WAS FOUND ON THE R-2 DOOR JAMB UPPER FLANGE, INBOARD SURFACE. CORROSION REMOVAL WAS BEYOND LIMITS BETWEEN STA 791 AND STA 860. FABRICATED 2 EACH FILLERS AND ANGLES AND INSTALLED IAW LACI ENGINEERING ORDER NR 3617, REV. D (REFERENCE DAC MESSAGES MISMar 5, 1996 · N228NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 96018122813Actuator Ftg · corrosionDURING ACCOMPLISHMENT OF CORROSION REWORK OF THE LEFT MLG TRUNNION FITTING (NWA STOCK NR 12-5743-9-0001) PER SA5743-01026-5, CORROSION ON THE LOWER AFT MLG ACTUATOR FITTING LUG EXCEEDED THE LIMITS OF SA5743-01026-5. THE REMAINING ATTACH AREAS WERE BLENDED WITMar 5, 1996 · N228NW · Doug DC1030 · Landing Gear ActuatorSDR 96017122812Actuator Mount · corrosionFOUND LIGHT PITTING CORROSION ON THE RIGHT MLG RETRACT CYLINDER MOUNTING SURFACE ON TRUNNION WITH LIGHT GALVANIC CORROSION IN THE BORES. MECHANICALLY REMOVED CORROSION ON MLG RETRACT CYLINDER MOUNTING SURACE AND ON BORES. FABRICATED AND INSTALLED FILLER. REMar 5, 1996 · N228NW · Doug DC1030 · Landing Gear ActuatorSDR 96016122811Trunnion Ftg · wornLEFT MLG TRUNNION FITTING ATTACHING BORES (AFT TOP AND BOTTOM) (RETRACT ACTUATOR A-FRAME) ARE RE-WORKED BEYOND MAXIMUM LIMITS PER NWA SA5743-01026-5, NOTE 2. OVERSIZED BORES TO 1.0075 INCHES PER STEP 1 NWA SA5743-01026-5. FABRICATED AND INSTALLED BUSHINGS. Mar 5, 1996 · N228NW · Doug DC1030 · Fuselage Main, Attach FittingsSDR 96014122810Door Farme · blend outFOUND DEEP BLEND-OUT AND NON-SRM REPAIR (KNIFE EDGE BLEND-OUT) ON AFT LOWER CORNER OF FORWARD CARGO DOOR FRAME. FABRICATED AND INSTALLED DOUBLER AND FILLER REPAIR PER SRM 53-50-00, FIGURE 9, SHEET 1 EXCEPT EXTENDED EXTERNAL DOUBLER AFT TO PICK UP 2 ROWS BEYONFeb 27, 1996 · N228NW · Doug DC1030 · Cargo/Baggage DoorsSDR 96013122809Longeron · corrodedLONGERON 15R BETWEEN FS 1953 AND FS 1975 HAS 2 AREAS OF INTERGRANULAR CORROSION. CUT FRAMES AT FS 1953, FS 1964, AND FS 1975 PER SRM 53-30-00, FIGURE 5. REPLACED LONGERON 15R IAW MFG DWG AGA3018-2. FABRICATED SPLICES AND REINSTALLED FRAMES IAW SRM 53-30-00,Feb 20, 1996 · N228NW · Doug DC1030 · Fuselage Main, Longeron/StringerSDR 96012122808Floor Beam · corrodedRIGHT MAIN FLOOR SUPPORT BEAM AT FS 1880 RT, RBL 36 IS CORRODED BEYOND SRM LIMITS. REMOVED AND REPLACED FLOOR SUPPORT BEAM IAW SRM 51-30-00. (X)Feb 20, 1996 · N228NW · Doug DC1030 · Fuselage Main, Floor BeamSDR 96011122807Clip · corrodedON NOSE WHEELWELL FORWARD OF PANEL 115AZ BETWEEN LONGERON 51R AND LONGERON 51L IN AVIONICS COMPARTMENT, FOUND 14 EACH CORRODED HILOC FASTENERS AND 2 EACH CORRODED T-CLIPS. REMOVED AND REPLACED 14 EACH HILOCS. FABRICATED AND INSTALLED 2 EACH T-CLIPS IAW SRM 5Feb 20, 1996 · N228NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 96008122806Door Frame · crackedL-3 DOOR FRAME, FS 1254, STR 27, CLOSE OUT PANEL HAS 2 EACH ONE INCH LONG CRACKS INSIDE LOWER INSPECTION HOLE. REMOVED EXISITNG DOUBLER, TRIMMED OUT CRACKS, AND VERIFIED BY NDT CRACKS WERE TRIMMED OUT. FABRICATED DOUBLER AND INSTALLED IAW SRM 53-50-00, FIGURFeb 15, 1996 · N228NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 96007122805Door Frame · crackedL-3 DOOR FRAME, FS 1305, STR 26, CLOSE OUT PANEL HAS 2 EACH ONE INCH LONG CRACKS INSIDE LOWER INSPECTION HOLE. REMOVED EXISITNG DOUBLER, STOP DRILLED CRACKS, AND VERIFIED BY NDT CRACKS DO NOT GO PAST STOP DRILL. FABRICATED DOUBLER AND INSTALLED IAW SRM 53-50Feb 15, 1996 · N228NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 96006122804Door Frame · crackedR-3 DOOR LOWER AFT FRAME AT FS 1305, STR 27 FOUND CRACKED INSIDE LIGHTING HOLE. REMOVED EXISTING DOUBLER. STOP DRILLED CRACK AND VERIFIED BY NDT CRACK DOES NOT GO PAST STOP DRILL. FABRICATED AND ISNTALLED DOUBLER IAW SRM 53-50-00, FIGURE 19. (X)Feb 15, 1996 · N228NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 96005122803Strap · required reworkWING STRINGER 41, STRAP PN SR 10570022-7, REQUIRES REWORK PER NWA ENGINEERING SKETCH SA 5711-01032-7, MACHINED ANGLE. RE-MACHINED ANGLE ON DOUBLER, PN SR 105700227, PER NWA SKETCH SA 5711-01032-7. WORK ACCOMPLISHED IN C/W SB 57-114 AND AD 94-12-05. MAINTENAFeb 6, 1996 · N228NW · Doug DC1030 · Fuselage Miscellaneous StructureSDR 96004122802Skin · crackedCRACK 0.9 INCHES LONG AND .812 INCHES DEEP IN RIGHT FORWARD CENTER SECTION OF HORIZONTAL STABILIZER PANEL AT LOWER HOLE NR 6 AND NR 7. CRACK IS WITHIN FLYABLE LIMITS IAW SA 42248-3. TREATED HOLE AND SURROUNDING AREAS WITH LPS 3 AND NOTIFIED NWA ENGINEERING OFeb 6, 1996 · N228NW · Doug DC1030 · Horizontal Stabilizer, Plate/SkinSDR 96003122801Skin · crackedCRACK 0.9 INCHES LONG AND .650 INCHES DEEP IN LEFT AFT UPPER CENTER SECTION OF HORIZONTAL STABILIZER PANEL AT HOLE NR 5 AND HOLE NR 6. CRACK IS WITHIN FLYABLE LIMITS IAW SA 42248-3. TREATED HOLE AND SURROUNDING AREAS WITH LPS 3 AND NOTIFIED NWA ENGINEERING OFeb 6, 1996 · N228NW · Doug DC1030 · Horizontal Stabilizer, Plate/Skin
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