Boeing 737-301
Service difficulty reports · 4,797
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 = '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.
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
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 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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.SDR 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)SDR 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)SDR 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 CHSDR 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)SDR 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)SDR USAASB99169Battery Pack · dischargedIAH - MAINTENANCE FOUND THE RIGHT OVERWING EMERGENCY EXIT LIGHT INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (X)SDR 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 IAHSDR 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 INCIDSDR 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)SDR 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)SDR 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 SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR DL733991393Bearing · failedAILERONS BINDING WITH FLAPS AT 5 DEG DURING CONTROL CHECK. FOUND AILERON CENTERING CAM BEARING FROZEN. REPLACED BEARING AND SYS OPS NORMAL.SDR 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)SDR 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)SDR 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)SDR 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)SDR 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)SDR 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. MASDR 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 ENGINSDR 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)
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