Boeing 737-524
Service difficulty reports · 1,586
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 = '737524' 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 = '737524' 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 CALA0300524Fuse · blownINSPECTION FOUND EMERGENCY LIGHTING ON FIRST CLASS SEATS INOPERATIVE. REPLACED PICOFUSES IN POWER SUPPLY FOR LIGHT.SDR CALA0300523Fuse · blownINSPECTION FOUND THE OVERHEAD EMERGENCY LIGHT ABOVE FIRST/COACH DIVIDER INOPERATIVE. REPLACED PICO FUSES IN POWER SUPPLY FOR LIGHT.SDR CALA0300521Bulkhead · canningINSPECTION FOUND SKIN WEB OIL CANNED AT AFT PRESSURE BULKHEAD FORWARD SIDE RT LOWER SECTION BETWEEN S23R AND Z-CHANNEL. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-80-08, FIGURE 201.SDR CALA0300515Skin · dentedINSPECTION FOUND THE C-2 DOOR SKIN DENTED ABOVE AND AFT OF DOOR HANDLE. THE SKIN WAS REPAIRED IAW SRM 52-00-01, FIGURE 203.SDR CALA0300512Wire Harness · brokenINSPECTION FOUND EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AT ROW 12ABC DUE TO A BROKEN WIRE. THE EMERGENCY ESCAPE PATH LIGHTING WIRE HARNESS WAS REPLACED. OPERATION OF THE EMERGENCY ESCAPE PATH LIGHTING WAS RESTORED AND OPERATIONAL CHECKS WERE GOOD IAW MM 33-SDR CALA0300511Skin · gougedINSPECTION FOUND FUSELAGE SKIN REPAIR PLATE GOUGED AT STA 980 UNDER L-2 DOOR. THE REPAIR PLATE WAS REMOVED AND A NEW REPAIR PLATE WAS INSTALLED IAW SRM 53-00-01, PAGE 204-206.SDR CALA0300481Bushing · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR LOWER FORWARD LUG PITTED AT BUSHING. THE BUSHING WAS REMOVED AND REPLACED IAW CMM 55-10-06.SDR CALA0300480Bushing · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER CENTER FORWARD SPAR LOWER AFT LUG PITTED AT BUSHING. A NEW BUSHING WAS INSTALLED IAW CMM 55-10-06.SDR CALA0300476Angle · gougedINSPECTION FOUND LT VERTICAL STABILIZER PANEL ATTACH ANGLE GOUGED AT STA 1065-1085 JUST BELOW VERTICAL STAB ON LT SIDE JUST FORWARD OF RUDDER. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW ECRA 55380-01013.SDR CALA0300469Skin · gougedINSPECTION FOUND SKIN UPPER SURFACE OF LT ELEVATOR GOUGED. THE SKIN WAS REPAIRED IAW ECRA 5520-01335.SDR 2003F00574Impeller · brokenBROKEN BLADE FROM SECOND STAGE IMPELLER THAT POSSIBLY EXITED TURBINE PLENUM.SDR CALA0300451Angle · corrodedINSPECTION FOUND RT CABIN FLOOR Z-ANGLE CORRODED AT STA 947.5-1006. THE Z-ANGLE WAS REPLACED IAW SRM 51-00-02.SDR CALA0300450Angle · corrodedINSPECTION FOUND LT CABIN FLOOR Z-ANGLE CORRODED AT STA 947.5 TO 1006. THE Z-ANGLE WAS REMOVED AND A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-10-02.SDR CALA0300447Sensor · out of adjustTHE CREW WAS UNABLE TO RAISE THE GEAR AFTER TAKEOFF. THE GEAR HANDLE WAS IN THE OFF POSITION WITH THREE GREEN AND THREE RED INDICATION LIGHTS. THE AIRCRAFT WAS RETURNED TO EWR. TROUBLESHOOTING FOUND THE RIGHT MAIN GEAR SAFETY SENSOR OUT OF ADJUSTMENT. THE SDR CALA0300445Beltframe · crackedINSPECTION FOUND A 2 INCH CRACK IN BELTFRAME AT STA 807 BETWEEN S27L AND S27R. A REPAIR ANGLE WAS INSTALLED IAW SRM 53-00-07.SDR CALA0300446Cooling Fan · failedAN OBJECTIONABLE ODOR WAS DETECTED BY FLIGHT ATTENDANT AND PASSENGERS JUST PRIOR TO DESCENT INTO COS. NO SIGN OF SMOKE WAS DETECTED IN CABIN OR COCKPIT. ALL ELECTRICAL SYSTEMS AND FLUID LEVELS CHECKED NORMAL. THE AIRCRAFT LANDED AT COS WITHOUT INCIDENT. MASDR CALA0300444Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN AFT CARGO COMPARTMENT FORWARD BULKHEAD PANEL SUPPORT LOWER SECTION ANGLE APPROXIMATELY 8 INCHES ABOVE CARGO FLOOR SURFACE. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-70-11.SDR CALA0300443Floor Support · crackedINSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 334, LBL 45. THE FLOOR SUPPORT WAS REPAIRED IAW SRM 51-10-2.SDR CALA0300442Floor Support · crackedINSPECTION FOUND A .5 INCH CRACK IN FLOOR SUPPORT AT STA 316-322, LBL 45. AN INTERCOSTAL WAS INSTALLED IAW SRM 51-10-2.SDR CALA0300440Bushing · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER UPPER FORWARD LUG CORRODED AROUND BUSHING. THE BUSHING WAS REMOVED AND REPLACED IAW SRM 55-10-10.SDR CALA0300438Bushing · corrodedINSPECTION FOUND RT HORIZONTAL STABILIZER UPPER FORWARD LUG CORRODED AROUND BUSHING. THE BUSHING WAS REMOVED AND REPLACED IAW SRM 55-10-10.SDR CALA0300437Mount · corrodedINSPECTION FOUND RT AFT LAV AFT WALL MOUNT PADS CORRODED AT STA 947.5. THE MOUNT PADS WERE REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0300435Bracket · crackedINSPECTION FOUND A 6 INCH CRACK IN RT WING BRACKET UNDER PANEL 5849, WBL 198.6. THE BRACKET WAS REPLACED IAW SRM 51-40-02.SDR CALA0300430Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING NR 8 FLAP TRACK FORWARD FAIRING ATTACH BRACKET. REPAIRED IAW ECRA 5740-02040.SDR CALA0300428Skin · gougedINSPECTION FOUND A GOUGE IN LT WING FIXED L/E UPPER SKIN PANEL AT O/B END OF NR 2 SLAT. THE SKIN WAS REPAIRED IAW SRM 51-70-16 AND ECRA 5721-01048.SDR CALA0300425Skin · dentedINSPECTION FOUND IN AFT CARGO DOOR SKIN APPROXIMATELY 23 INCHES FROM FORWARD EDGE AND 23 INCHES FROM TOP EDGE.SDR CALA0300423Skin · crackedINSPECTION FOUND AFT CARGO DOOR OUTER SKIN DENTED APPROXIMATELY 37 INCHES FROM FORWARD EDGE AND 31 INCHES FROM TOP EDGE. A REPAIR WAS INSTALLED IAW SRM 52-00-01.SDR CALA0300417Skin · gougedINSPECTION FOUND FUSELAGE SKIN GOUGED JUST LEFT OF RUDDER SEAL AT STA 1116. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-80-01.SDR CALA0300416Bushing · corrodedINSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHING CORRODED AT LT O/B AFT LOCATION. THE BUSHING WAS REMOVED AND REPLACED IAW BOEING DRAWING 65-52274.SDR CALA0300415Bushing · corrodedINSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT RT I/B FORWARD AND AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED IAW SOPM 20-50-03.SDR CALA0300413Angle · corrodedINSPECTION FOUND L-ANGLE CORRODED AT STA 951-995, RBL 55. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0300410Bushing · corrodedINSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT LT I/B FORWARD AND AFT AND RT I/B AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED AND HONED TO SIZE IAW DRAWING NR 65-46872.SDR CALA0300409Bushing · corrodedINSPECTION FOUND THE VERTICAL STABILIZER ATTACH FITTING BUSHINGS CORRODED AT LT O/B FORWARD AND AFT AND RT O/B FORWARD AND AFT LOCATIONS. THE BUSHINGS WERE REMOVED AND REPLACED AND HONED TO SIZE PER DRAWING 65-46872.SDR CALA0300407Floor Support · crackedINSPECTION FOUND A 5 INCH CRACK IN FLOOR SUPPORT AT STA 328-344, LBL 45. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING 65C33973.SDR CALA0300406Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 312-328, LBL 45. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0300405Bracket · corrodedINSPECTION FOUND L-1 DOOR GIRT BAR AFT LATCH ATTACH BRACKET CORRODED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02.SDR CALA0300404Floor Support · crackedINSPECTION FOUND FLOOR SUPPORTS AT STA 344-360 BL 0 AND LBL 10 CRACKED. THE CRACKS WERE .5 INCH AND 4 INCH. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02, 51-40-02, AND DRAWING 65C33970-53.SDR CALA0300388Gate · corrodedINSPECTION FOUND CORROSION AND GOUGES ON EXTERIOR OF L-1 DOOR LOWER GATE. THE LOWER GATE WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0300381Beam · crackedINSPECTION FOUND A 1 INCH CRACK IN C-1 DOOR T-BEAM. A REPAIR WAS INSTALLED IAW SRM 51-70-12.SDR CALA0300380Skin · dentedINSPECTION FOUND AFT CARGO DOOR SKIN DENTED 39 INCHES FROM FORWARD EDGE AND 19 INCHES FROM TOP. REPAIRED IAW SRM 52-00-01.SDR CALA0300384Skin · dentedINSPECTION FOUND THE AFT CARGO DOOR EXTERNAL SKIN DENTED 21 INCHES FROM FORWARD DOOR EDGE AND 40 INCHES FROM TOP EDGE. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.SDR CALA0300379Solenoid · inoperativeTHE LANDING GEAR HANDLE WOULD NOT RAISE PAST THE OFF POSITION AFTER TAKEOFF FROM EWR. QRH PROCEDURES WERE FOLLOWED AND THE AIRCRAFT WAS RETURNED TO EWR. MAINTENANCE FOUND THE LANDING GEAR LEVER LOCK CIRCUIT BREAKER POPPED. THE CIRCUIT BREAKER WAS RESET. THSDR CALA0300374Angle · corrodedINSPECTION FOUND R-2 DOOR THRESHOLD Z-ANGLE CORRODED AT AFT AREA OF DOOR CUTOUT. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0300372Intercostal · crackedINSPECTION FOUND A .25 INCH CRACK IN INTERCOSTAL AT STA 344-360, RBL 3. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0300369Intercostal · crackedINSPECTION FOUND FORWARD ENTRY AREA INTERCOSTAL CRACKED AT STA 344-360, BL 0. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-40-00.SDR CALA0300365Hinge Pin · corrodedINSPECTION FOUND EXTERIOR OF INNER PIN AND BORE OF OUTER HINGE PIN FOR HORIZONTAL STABILIZER CORRODED. THE INNER PIN AND OUTER HINGE PIN ASSEMBLY WERE REMOVED AND REPLACED IAW EA 5550-01315 AND MM 27-41-31.SDR CALA0300377Skin · damagedTHE FUSELAGE SKIN WAS FOUND DAMAGED AFT OF BS 1088 BETWEEN STRINGER 18L AND 20L. THE TRIM OUT TO REMOVE DAMAGE MEASURED 1.3 X 1.15 INCH. THE AREA WAS REPAIRED IAW ECRA 5330-03264.SDR CALA0300356Sensor · out of adjustTHE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM HOU. THE AIRCRAFT WAS RETURNED TO HOU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED AND TESTED THE MLG SAFETY SENSORS IAW MM 32-09-01. AN OPERATIONAL CHECK OF THE GEAR WAS PERFORMED IAW MM 32-32SDR CALA0300355Floor Support · crackedINSPECTION FOUND A 2 INCH CRACK IN CENTER FLOOR SUPPORT AT STA 540 LEFT OF CENTER. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0300353Intercostal · crackedINSPECTION FOUND A .5 INCH CRACK IN INTERCOSTAL AT NUT PLATE HOLES BETWEEN STA 344 AND 360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-40.
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