Boeing 737-301

Service difficulty reports · 4,797

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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 = '737301'
  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 USAA990722Skin · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT NR 1 ENGINE PYLON SKIN AT ACCESS PANEL NR 5727 CUTOUT LOWER AFT CORNER. INSTALLED DOUBLER PER TR 54-30-07. (M)Jul 29, 1999 · N338US · Boeing 737301 · Nacelle/Pylon, Plate/SkinSDR USAA990721Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STATION 520 STRINGER 7R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990719Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 500C STR 7R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990718Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STA 600 STR 8L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990717Longeron · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH LONGERON CRACK AT FORWARD L/B CORNER STATION 277 STRINGER 14R. FABRICATED NEW LONGERON WEB AND INSTALLED PER SRM 51-30-2. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990716Stringer · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK IN STRINGER AT STA 306 STR 4L. FABRICATED NEW WEB AND INSTALLED PER SRM 53-10-15. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA990715Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK IN FRAME AT STA 727D, RBL 2. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-00-07 AND EA 65131 PAGES 1 AND 2. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, FrameSDR USAA990685Angle · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT BS 480 STRINGER 9L BAG BIN ATTACH ANGLE. FABRICATED NEW REPAIR DOUBLER PER SRM 53-00-07 AND EA 650009. (M)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990684Bulkhead · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK AT STA 178 BULKHEAD LBL 5 W/L 195 SKIN. INSTALLED DOUBLER PER TR 53-10-07. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990683Bulkhead · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND 1 INCH CRACK AT STA 178 BULKHEAD LBL 5 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER TR 53-10-07. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990682Bulkhead · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND .50 INCH CRACK AT STA 178 BULKHEAD RBL1 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-08 FIG 203. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990681Bulkhead · crackedCLT - DURING A Q-3 CHECK VISUAL INSPECTION FOUND .50 INCH CRACK AT STA 178 BULKHEAD LBL1 W/L 188 SKIN. INSTALLED REPAIR DOUBLER PER SRM 53-10-08 FIG 203. (X)Jul 29, 1999 · N338US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990680Angle · corrodedCLT - DURING A Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION AFT RT Z-ANGLE AT AFT SERV DOOR. CORROSION LEVEL 2. REPLACED PER SRM 51-10-02. (M)Jul 29, 1999 · N338US · Boeing 737301 · Service DoorsSDR USAASB99197Battery Pack · dischargedEWR - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHTS INOPERABLE OVER THE COCKPIT AND FORWARD ENTRY DOOR. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)Jul 25, 1999 · N590US · Boeing 737301 · Emergency LightingSDR SWAA991237Battery Charger · inopDURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY DOOR EVACUATION SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED FWD ENTRY DOOR SLIDE EMERGENCY LIGHT BATTERY CHARGER ASSY PER MM.Jul 25, 1999 · N660SW · Boeing 737301 · Emergency LightingSDR USAASB99183Charger · failedBDL - MAINTENANCE FOUND THE AISLE EMERGENCY LIGHTS AT SEAT ROWS 17 THROUGH 20 INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AT STA 962L. OPERATIONAL CHECKED GOOD. (X)Jul 24, 1999 · N592US · Boeing 737301 · Emergency LightingSDR 99ZZZX2826Intercostal · crackedDEN - DURING C-CHECK INSPECTION, REPORTED 1 INCH CRACK IN FLOOR INTERCOSTAL WEB, BS 178, WL 207, RBL 19.0. MAINTENANCE FABRICATED DOUBLER AND REPAIRED PER SRM 51-70-13 AND SRM 53-10-08. (X)Jul 23, 1999 · N578US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB99178Tr Unit · malfunctionedBWI - FLT 0166 - DURING CRUISE, EN ROUTE PHX/PHL, THE WEATHER RADAR BECAME UNRELIABLE. TEST PAGE SHOWED 'R/T FAULT' FOLLOWED BY 'NO WXR'. SYSTEM WORKED FINE INITIALLY. FLIGHT DIVERTED TO BWI AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE OPERATIONALLY CHJul 19, 1999 · N563AU · Boeing 737301 · Weather Radar SystemSDR F3LA99106Firewall · crackedDEN - DURING C-CHECK, INSPECTION REPORTED FIREWALL FROM CLAMP 12 O'CLOCK POSITION AT NACELLE STA 204.5 (6 INCHES AFT OF FORWARD ENGINE MOUNT ON NACELLE). MAINTENANCE FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 51-70-13. TC: 27,402. (X)Jul 16, 1999 · N578US · Boeing 737301 · Nacelle/Pylon, Bulkhead/FirewallSDR F3LA99105Skin · crackedDEN - DURING C-CHECK, INSPECTION REPORTED CRACK IN NR 1 LEADING EDGE SLAT LOWER SKIN AT TWO RIVETS, OUTBOARD MAIN RACK. MAINTENANCE FABRICATED, TREATED AND INSTALLED REPAIR PER EA 57-737-027. TC: 27,402. (X)Jul 16, 1999 · N578US · Boeing 737301 · Leading Edge DevicesSDR USAASB99169Battery Pack · dischargedIAH - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)Jul 9, 1999 · N349US · Boeing 737301 · Emergency LightingSDR USAASB99167Connector · failedIAH - FLT 1185 - FLIGHT WAS APPROX 150 MILES FROM IAH WHEN THE A/C LOST THE WEATHER RADAR, CAPTAINS HSI, BOTH AUTOPILOTS AND THE CAPTAINS ATTITUDE INDICATOR. CAPTAIN DECLARED AN EMERGENCY WITH AIR TRAFFIC CONTROL DUE TO THUNDERSTORMS 55 MILES NORTHEAST OF IAHJul 9, 1999 · N574US · Boeing 737301 · Flight Management Computing Hardware SystemSDR USAASB99164Engine · fatiguedBOS - FLT 221 - JUST AFTER TAKEOFF, CREW ENCOUNTERED A WINDSHEAR ON DEPARTURE AND APPLIED FIREWALL POWER FOR A PERIOD APPROXIMATELY 10 SECONDS. CAPTAIN FELT HE OVERBOOSTED THE ENGINES AND ELECTED TO RETURN TO FIELD AT BOS. FLIGHT LANDED WITHOUT FURTHER INCIDJul 6, 1999 · N339US · Boeing 737301 · Engine (Turbine/Turboprop)SDR USAA990484Web · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .300 INCH CRACK AT STATION 727 STRINGER 18A LEFT MAIN WHEEL WELL SHEAR WEB. INSTALLED DEFECTIVE PART WITH IDENTICAL PART PER BOEING 6546877 BLUEPRINT. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990565Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH, 1 INCH AND .75 INCH CRACK AT STATION 178 RIGHT SIDE PLUS 6 INCHES WL 200 AT 4.75 AND 6.75 BULKHEAD. INSTALLED DOUBLER PER SRM 53-10-07. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA990573Skin · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 12 INCH AREA OF FUSELAGE OF CORROSION BETWEEN NR 3 VHF ANTENNA MOUNT STATION 727D PLUS 3 TO 727D PLUS 15 AND INTERIOR SKIN FUSELAGE BL 0. REMOVED EXISTING DOUBLER AND REPLACED WITH LARGER SIZE DOUBLER PER SRM Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990574Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 20 INCH AREA OF CORROSION BS 270, LBL 10 - RBL 10 FLOOR SUPPORT. INSTALLED NEW Z-ANGLE PER TR 53-20-04 AND EA 64680. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990575Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 3 INCH AREA OF CORROSION ON T-CAP AND AROUND NUT PLATE HOLES AT BS 294.5 FROM LBL 12 TO RBL 7. CORROSION TASK NR C53-107-102-02. REMOVED ALL CORROSION ON T-CAP PER SRM 53-10-51. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990576Channel · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH AREA OF CORROSION AT BS 986.5 RBL 24 HOT CHANNEL. CORROSION LEVEL 2. INSTALLED FABRICATED PART PER SRM 51-40-04 AND DWG 65-61381. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990578Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION AT STATION 986.5 LBL 24 FLOORBEAM, CORROSION LEVEL 2. FABRICATED NEW PART PER SRM 51-40-02 AND DWG 6561381. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990579Frame · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 6 INCH AREA OF CORROSION ON INBOARD J CHANNEL BS 993.5 FRAME AT WL 208.1, CORROSION LEVEL 2. INSTALLED DOUBLER PER SRM 51-70-11. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, FrameSDR USAA990580Web · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A 2 INCH AREA OF CORROSION AFT RIGHT LAV FILL CONN ON FLOOR WEB, CORROSION LEVEL 2. NEW WEB INSTALLED PER SRM 51-10-02. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990581Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 60 INCH AREA OF CORROSION AT STATION 986.5 FLOORBEAM. INSTALLED UPPER T-CAP PER SRM 53-00-51. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990582Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, LBL 12 T-CAP. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. FABRICATED T-CAP PER SRM 53-10-51 FIG 205.. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990583Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, LBL1 AND LBL 11 FLOORBEAM. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. FABRICATED T-CAP PER SRM 53-10-51 FIG 205. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990584Floorbeam · corrodedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH AREA OF CORROSION AT BS 312, BL 0 LBL 7 AND RBL 8 FLOORBEAM, CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. FABRICATED T-CAP PER SRM 53-10-51 FIG 205. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA990617Skin · crackedCLT - DURING Q-1 CHECK, FOUND .75 INCH CRACK ON SKIN AT PILOTS NR 1 WINDOW CUTOUT UPPER OUTBOARD CORNER. FABRICATED DOUBLER PER EA 64783A. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990606Skin · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A SMALL SKIN CRACK AT CARGO DOOR HANDLE CUTOUT AFT CARGO DOOR, AFT RADIUS OF HANDLE ACCESS CUTOUT EXTERIOR SKIN. INSTALLED EXTERNAL DOUBLER PER SRM 52-00-01 FIG 202. (M)Jun 21, 1999 · N337US · Boeing 737301 · Cargo/Baggage DoorsSDR USAA990586Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND .5 INCH CRACK AT STATION 727D AT LBL 02 AND RBL 02 FRAME. INSTALLED DOUBLER AND FILLERS PER SRM 53-60-07 AND EA 64800. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, FrameSDR USAA990585Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1.5 INCH CRACK ON FRAME AT STATION 727D AT LBL 2 INCH AT VERTICAL ANGLES FOR ANTENNA MOUNT. CUTOUT CRACK AND INSTALLED FILLER AND DOUBLER PER EA 64800. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, FrameSDR USAA990564Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AT STATION 178 BULKHEAD RBL 314 WL 187. INSTALLED DOUBLER PER SRM 53-10-08 FIG 203. (M)Jun 21, 1999 · N337US · Boeing 737301 · Fuselage Main, BulkheadSDR DL733991393Bearing · failedAILERONS BINDING WITH FLAPS AT 5 DEG DURING CONTROL CHECK. FOUND AILERON CENTERING CAM BEARING FROZEN. REPLACED BEARING AND SYS OPS NORMAL.Jun 18, 1999 · N948WP · Boeing 737301 · Aileron Control SystemSDR USAA990600Skin · crackedTPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK IN SKIN FUSELAGE STATION 380 DIRECTLY AFT OF EQUIP COOLING DUCT CUTOUT. INSTALLED REPAIR DOUBLER PER TR 53-30-07. (M)Jun 17, 1999 · N300AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA990598Skin · crackTPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT FORWARD LOWER RADIUS AND .125 INCH CRACK AT FASTENER ABOVE HINGE CUTOUT FORWARD SERVICE DOOR SKIN. INSTALLED DOUBLER PER EA 64745. (M)Jun 17, 1999 · N300AU · Boeing 737301 · Service DoorsSDR USAA990597Skin · crackTPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .281 INCH CRACK AT FORWARD SERVICE DOOR SKIN UPPER AFT CORNER OF UPPER HINGE CUTOUT ON EXTERIOR DOOR SKIN. INSTALLED REPAIR DOUBLER PER SB 52-1096. (M)Jun 17, 1999 · N300AU · Boeing 737301 · Service DoorsSDR USAA990596Angle · corrodedTPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND AN AREA OF CORROSION AT STATION 360 CENTERLINE OF FUSELAGE ON LOWER FRAME ATTACH ANGLE. FABRICATED AND INSTALLED NEW LOWER FRAME ATTACH ANGLE PER SRM 51-10-02. (M)Jun 17, 1999 · N300AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA990595Angle · corrodedTPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND AN AREA OF CORROSION AT STRINGER TIE ANGLE BETWEEN STRINGERS 28L AND 28R STATION 360. FABRICATED AND INSTALLED NEW STRINGER TIE ANGLE PER SRM 51-10-02. (M)Jun 17, 1999 · N300AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB99143Connector · corrodedJAX - FLT 1469 - DURING CRUISE, AT APPROXIMATELY FL 350, THE NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW ELECTED TO DIVERT TO THE NEAREST STATION AT JAX. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO ENGINE SHUTDOWN OCCURRED NOR WAS AN EMERGENCY DECLARED. MAJun 14, 1999 · N590US · Boeing 737301 · Overheat DetectionSDR AWXA9900221Coffeemaker · malfunctionedON CLIMB 24000 FT, F/A REPORTED BURNING ELECTRICAL SMELL NEAR L1. PRIOR TO AIR TURNBACK, ACFT RETURNED TO GATE BECAUSE OF ELECTRICAL SMELL IN CABIN NEAR DOOR L1. REMOVED AND REPLACED THE NR 1 COFFEEMAKER. PROBLEM WAS AN EXPOSED HEAT ELEMENT. RAN BOTH ENGINJun 13, 1999 · N326AW · Boeing 737301 · Buffet/GalleysSDR USAA990563Floorbeam · crackedCLT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN LONGITUDINAL FLOORBEAM AT BS 708.5 AND BS 709.5. INSTALLED DOUBLER AND FILLER PER SRM 511-70-13. (M)Jun 10, 1999 · N337US · Boeing 737301 · Fuselage Main, Floor Beam
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