Boeing 737-219

Service difficulty reports · 72

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '737219'
  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 CALA9701050Chord · corrodedINSPECTION FOUND T-CHORD CORRODED AT STA 351, RBL 16. THE CHORD WAS REPAIRED IAW SRM 51-10-6 AND 53-10-1.Jun 16, 1997 · N10248 · Boeing 737219 · Fuselage Miscellaneous StructureSDR CALA9701005Chord · corrodedINSPECTION FOUND T-CHORD CORRODED AT STA 340, STRINGER 23R. THE CHORD WAS REPLACED IAW SRM 51-30-2 AND 53-10-2.Jun 16, 1997 · N10248 · Boeing 737219 · Fuselage Miscellaneous StructureSDR CALA9701004Skin · dentedINSPECTION FOUND FORWARD FUSELAGE SKIN DENTED FIVE INCHES BELOW S17L AT STA 380 TO 400. THE DENTED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 51-10-2 AND 53-30-3.Jun 13, 1997 · N10248 · Boeing 737219 · Fuselage Main, Plate/SkinSDR CALA9701149Seat Track · gougedNUMBER 4 SEAT TRACK GOUGED AT FS 727. REMOVED DAMAGED SEAT TRACK. FABRICATED AND INSTALLED SEAT TRACK IN ACCORDANCE WITH SRM 53-10-5 AND BAC 1520-1342.Jun 11, 1997 · N10248 · Boeing 737219 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9701152Seat Track · gougedSEAT TRACK GOUGED AT FS 727 TO 731A AT LBL24. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IN ACCORDANCE WITH SRM 53-10-5.Jun 10, 1997 · N10248 · Boeing 737219 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9700234Power Contl Unit · inoperativeTHE AIRCRAFT HAD A BRIEF HISTORY OF STIFF AILERONS. MAINTENANCE FOUND THE B-SYSTEM AILERON POWER CONTROL UNIT AT FAULT. THE AILERON PCU WAS REMOVED AND REPLACED IAW MM 27-11-71, PAGE 401. AN ADJUSTMENT/TEST WAS PERFORMED ON THE AILERON PCU IAW MM 27-11-71, Feb 21, 1997 · N10248 · Boeing 737219 · Aileron Control SystemSDR CALA9700131Circuit Breaker · trippedTHE LANDING GEAR COULD NOT BE RETRACTED AFTER TAKEOFF. THE GEAR HANDLE WOULD NOT GO PAST THE OFF POSITION. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS RETURNED WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEVER LATCH AND PRESS WARNING Feb 3, 1997 · N10248 · Boeing 737219 · Landing Gear Retraction/Extension SystemSDR CALA9601316Wheel Half · detachedWHILE REPLACING THE NR 4 MLG TIRE/WHEEL ASSEMBLY DUE TO TIRE WEAR, THE INNER WHEEL ASSEMBLY HUB WAS FOUND DETACHED FROM WHEEL HALF. THE NR 4 TIRE/WHEEL ASSEMBLY WAS REMOVED AND REPLACED. IN ADDITION, THE NR 3 MLG TIRE/WHEEL ASSEMBLY WAS REMOVED AND REPLACED Sep 15, 1996 · N10248 · Boeing 737219 · Wheel/Ski/FloatSDR CALA9601306Fuel Pump · failedTHE NR 1 ENGINE SURGED AND ROLLED BACK TO APPROXIMATELY 1.6 EPR AND 85 PERCENT ON TAKEOFF AT ROTATION. THE ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENTS. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THSep 12, 1996 · N10248 · Boeing 737219 · Engine Fuel PumpSDR CALA9601167T1 Blade · fracturedTHE NR 1 ENGINE ROLLED BACK TO 1.4 EPR AND AIRCRAFT VIBRATION WAS FELT AFTER GEAR RETRACTION. THE NR 1 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS RETURNED TO CAE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 1 ENGINE DAMAGED. THE NR 1 ENGINE WASAug 13, 1996 · N10248 · Boeing 737219 · Turbine SectionSDR CALA9601111Skin · crackedINSPECTION FOUND A .4375 INCH CRACK IN FUSELAGE SKIN BELOW FIRST OFFICER'S EYEBROW WINDOW. THE SKIN WAS REPAIRED IAW SRM 53-30-3, PAGES 26 TO 28E, REPAIR NR 7.Jul 30, 1996 · N10248 · Boeing 737219 · Fuselage Main, Plate/SkinSDR CAL960441Control Cable · brokenEWR - FLT 1160 - THE AIRCRAFT ROLLED LEFT ON FLAP EXTENSION FOR LANDING ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT INBOARD TRAILING EDGE FLAP JAMMED DUE TO A BROKEN FOLLOW-UP CABLE ON INBOARD JACKSCREW. CABLES BC-3 ANApr 5, 1996 · N10248 · Boeing 737219 · Trailing Edge Flap Control SystemSDR CAL950589Rib · corrodedGSO - INSPECTION FOUND THE OUTBOARD RIB/WEB AND BOLT HOLE BUSHINGS CORRODED AT THE NR 3 LEADING EDGE SLAT OUTBOARD TRACK TO SLAT ATTACH POINT. THE CORROSION WAS CLEANED UP AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-50-3 AND SRM 51-30-2. (X)Jul 1, 1995 · N10248 · Boeing 737219 · Leading Edge DevicesSDR CAL950588Intercostal · crackedGSO - THE NR 6 SLAT INTERIOR HAD TWO EACH INTERCOSTALS CRACKED AT INBOARD SLAT TRACK ATTACH FITTING. EACH CRACK WAS APPROXIMATELY .50 INCH LONG. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 57-50-3. (X)Jul 1, 1995 · N10248 · Boeing 737219 · Leading Edge DevicesSDR CAL950587Skin · crackedGSO - A .50 INCH CRACK WAS FOUND IN LT WING FIXED LEADING EDGE SKIN AT TOP OF CENTER OF CUT-OUT FOR OUTBOARD TRACK ON NR 3 SLAT. THE CRACK WAS STOP-DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5762-01020. (X)Jul 1, 1995 · N10248 · Boeing 737219 · Wing, Plate/SkinSDR CAL950586Intercostal · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN INTERCOSTAL OF NR 2 SLAT INBOARD SLAT TRACK, AT SLAT TRACK ATTACH FITTING AREA. THE CRACK WAS STOP-DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-3 AND SRM 51-30-2. (X)Jul 1, 1995 · N10248 · Boeing 737219 · Leading Edge DevicesSDR CAL950585Rib · crackedGSO - INSPECTION FOUND A .25 INCH CRACK IN RADIUS OF RT RIB AT LOWER FORWARD ATTACH HOLE, STA 738. THE CRACK WAS STOP-DRILLED. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 57-10-5. (X)Jul 1, 1995 · N10248 · Boeing 737219 · Wing, Rib/BulkheadSDR CAL950584Webbing · crackedGSO - THE RIGHT WING CENTER INBOARD OF STA 139 HAD WEBBING WITH CRACKS AROUND FASTENER HOLES. THE CRACKS WERE .25 INCH LONG. THE CRACKED AREAS WERE REMOVED. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-40-6. (X)Jul 1, 1995 · N10248 · Boeing 737219 · Wing Miscellaneous StructureSDR CAL950354Eel Power Supply · inoperativeGSO - THE RT EXTERIOR OVERWING EMERGENCY LIGHTING WAS FOUND INOPERATIVE DURING SERVICE CHECK. THE POWER SUPPLY AND BATTERY PACK WAS REPLACED AND OPERATION OF THE EXTERIOR OVERWING EMERGENCY LIGHTING WAS RESTORED. REFERENCE 95ZZZW711.May 1, 1995 · N10248 · Boeing 737219 · Emergency LightingSDR 95ZZZW711Eel Batt · dischargedGSO - THE RT EXTERIOR OVERWING EMERGENCY LIGHTING WAS FOUND INOPERATIVE DURING SERVICE CHECK. THE POWER SUPPLY AND BATTERY PACK WAS REPLACED AND OPERATION OF THE EXTERIOR OVERWING EMERGENCY LIGHTING WAS RESTORED. REFERENCE CAL950354 .May 1, 1995 · N10248 · Boeing 737219 · Emergency LightingSDR CAL950341Eel Wiring · brokenFLT NR 1275 - GSO - AIRCRAFT ARRIVED WITH EMERGENCY PATH LIGHTS ON, LIGHTS WOULD NOT GO OUT REPLACED BATTERY PACK OPS CHECK GOOD. THE BATTERY PACK WAS NOT AT FAULT. MAINTENANCE FOUND WIRING BROKEN AT BOTH THE AFT BULLNOSE LIGHT ASSEMBLY AND AT THE EMERGENCY Apr 30, 1995 · N10248 · Boeing 737219 · Emergency LightingSDR CAL950010Engine · malfunctionedFLT NR 1629 - ATL - THE NR 2 ENGINE OIL TEMPERATURE REACHED RED LINE WHILE EN ROUTE TO MSY. THE NR 2 ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. THE NR 2 ENGINE WAS REMOVED AND REPLACED. LEAK AND OPERATIONAL CJan 3, 1995 · N10248 · Boeing 737219 · Engine (Turbine/Turboprop)
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