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 CALA0400193Skin · puncturedINSPECTION FOUND A PUNCTURE IN THE RT ELEVATOR UPPER SKIN AT ELEVATOR STA 137.59. THE ELEVATOR SKIN WAS REPAIRED IAW ECRA 5520-01339.SDR CALA0400179Skin · crackedINSPECTION FOUND A 2.125 INCH CRACK IN RIGHT WING L/E SKIN AT NR 3 KRUEGER FLAP. THE AREA WAS REPAIRED IAW SRM 57-41-01, FIGURE 203.SDR CALA0400156Attach Fitting · gougedINSPECTION FOUND HORIZONTAL STABILIZER FORWARD RIGHT LOWER ATTACH LUG GOUGED BY CLEVIS PIN FROM LOWER RIGHT SLIDER. THE GOUGE WAS BLENDED, FLAP PEENED, TREATED AND PRIMED IAW SRM 55-10-10 AND 51-20-06.SDR CALA0400151Skin · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN RT LOWER HORIZONTAL STABILIZER SKIN AT REAR SPAR STA 100 AND 129. A REPAIR WAS INSTALLED IAW ECRA 5510-01724.SDR CALA0400139Floor Support · crackedINSPECTION FOUND FLOOR SUPPORTS CRACKED AT FASTENER HOLES AT STA 540, RBL 2 AND LBL 2. THERE WAS ONE CRACK IN EACH SUPPORT AND BOTH WERE TWO INCHES LONG. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-40-2.SDR CALA0400137Web · corrodedINSPECTION FOUND THE C-2 DOOR THRESHOLD WEB CORRODED. THE THRESHOLD WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0400136Skin · crackedINSPECTION FOUND A .25 INCH CRACK IN LT WING UPPER L/E SKIN AT NR 3 SLAT ACTUATOR. THE CRACKED AREA OF SKIN WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 57-41-01.SDR CALA0400134Intercostal · damagedINSPECTION FOUND A HOLE IN CABIN FLOOR INTERCOSTAL JUST FORWARD OF STA 360, BL 0. A REPAIR WAS INSTALLED IAW SRM 51-10-02.SDR CALA0400128Channel · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOORBOARD CHANNEL AT STA 537.45, BL 0 TO RBL 14. THE FLOORBOARD CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0400119Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 344-360, LBL 14. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0400118Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1064, S16L. A DOUBLER WAS INSTALLED IAW SRM 53-80-01.SDR CALA0400113Stiffener · crackedINSPECTION FOUND A 1 INCH CRACK IN TEE STIFFENER AT C-2 DOOR AFT LOWER CORNER. THE TEE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0400103Panel · crackedINSPECTION FOUND TWO 1.5 INCH CRACKS IN RT WING FIXED UPPER LEADING EDGE PANEL AT NR 4 SLAT ACTUATOR, SLAT STA 65.92. THE LEADING EDGE PANEL WAS REPAIRED IAW ECRA 5721-01116.SDR CALA0400078Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 887-907, S26R. THE SKIN WAS REPAIRED IAW SRM 53-00-01.SDR CALA0400070Skin · delaminatedINSPECTION FOUND O/B CORNER OF NR 2 SLAT SKIN DELAMINATED. REPAIRED IAW SRM 51-70-10.SDR CALA0400067Skin · damagedINSPECTION FOUND FUSELAGE SKIN DAMAGED ON FORWARD CURVED SIDE AT RIGHT AFT HORIZONTAL STABILIZER ATTACH POINT. THE SKIN WAS REPLACED IAW SRM 51-40-2.SDR CALA0400065Pump · leakingTHE A-HYDRAULIC SYSTEM QUANTITY AND PRESSURE BEGAN TO DROP WHILE CLIMBING THROUGH 24,000 FEET EN ROUTE FROM MDW TO EWR. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF THE A-HYDRAULIC SYSTEM WARNING LIGHT. A MANUAL GEAR EXTENSION WAS REQUIRED. THE AIRCRAFT WAS SDR CALA0400052Angle · corrodedINSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED FROM STA 270-360. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0400051Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT WEB BETWEEN STA 348 AND 360, BL 0. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02.SDR CALA0400030Battery · inoperativeTHE EMERGENCY AISLE PATH LIGHTING IN FIRST CLASS CABIN FAILED AFTER 30 SECONDS OF TESTING. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51 AND OPERATION OF THE EMERGENCY LIGHTS CHECKED GOOD.SDR CALA0400028Spar · gougedINSPECTION FOUND A GOUGE IN RT HORIZONTAL STABILIZER L/E SPAR CAP BETWEEN STA 239.9 AND 249.1 AT I/B SIDE. REPAIRED IAW ECRA 5510-01704.SDR CALA0400026Skin · dentedTHE RT HORIZONTAL STABILIZER LOWER SKIN SURFACE WAS FOUND DENTED APPROXIMATELY 1 INCH FROM FORWARD LOWER SPAR AND APPROXIMATELY 5 FT I/B OF TIP. REPAIRED IAW ECRA 5510-01704.SDR CALA0400072Skin · dentedINSPECTION FOUND A DENT IN FUSELAGE SKIN AT BS 420 BELOW S17L. THE SKIN WAS REPAIRED IAW ECRA 5331-01133.SDR CALA0300714Beltframe · puncturedINSPECTION FOUND LT BELT FRAME PUNCTURED IN TWO PLACES AT STA 847. THE DAMAGE WAS ROUTED OUT AND A BELT FRAME REPAIR WAS INSTALLED IAW SRM 51-70-11.SDR CALA0300711Angle · corrodedINSPECTION FOUND L-2 DOORWAY Z-ANGLE CORRODED AT STA 967. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0300694Skin · gougedAPU ACCESS DOOR INNER SKIN GOUGED LT SIDE FORWARD OF AFT LATCH. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED DOUBLER PER SRM 5200-01.SDR CALA0300687Angle · crackedRT WING 90 DEGREE GREEN ANGLE CRACKED AT FORWARD SIDE OF RT MLG INBOARD DOOR OPENING WBL 71 UNDER STRUT DOOR. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-02.SDR CALA0300685Bushing · corrodedCORROSION ON FORWARD LOWER HORIZONTAL STAB CENTER SECTION LUG ON AFT CLEVIS ON AFT FACE AT BUSHING. REMOVED AND REPLACED BUSHING PER SOPM 20-50-03.SDR CALA0300684Bushing · corrodedFORWARD LEFT LOWER HORIZONTAL STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT BUSHING ON FORWARD FACE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.SDR CALA0300683Bushing · corrodedFORWARD LEFT UPPER STAB CENTER SECTION FORWARD CLEVIS HAS PITTING CORROSION AT THE BUSHING ON FORWARD EDGE. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.SDR CALA0300682Bushing · corrodedCORROSION ON FORWARD UPPER HORIZONTAL STAB CENTER SECTION LUG AFT CLEVIS ON AFT FACE AT BUSHING. REPAIRED AND REPLACED OVERSIZE BUSHING PER SRM 55-10-10.SDR CALA0300680Angle · corrodedINSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 967-990. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0300679Angle · corrodedINSPECTION FOUND LT Z-ANGLE CORRODED AT L-2 DOOR SILL, STA 977. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0300678Fitting · corrodedINSPECTION FOUND VERTICAL STABILIZER RT REAR SPAR FORWARD DRAG ANGLE FITTING CORRODED AT OB MOUNTING BOLT AREA. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0300676Fairing · damagedTHE RT RED GEAR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF. THE GEAR WAS CYCLED, BUT THE LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO DEN WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT I/B FLAP FAIRING HANGING BY FORWARSDR CALA0300658Beltframe · corrodedINSPECTION FOUND BELTFRAME CORRODED AT STA 992, S17-18R. THE CORRODED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-70-11.SDR CALA0300652Attach Angle · gougedINSPECTION FOUND A GOUGE ON VERTICAL ATTACH ANGLE ON RT SIDE OF VERTICAL STRAP AT STA 1121. A NEW ANGLE WAS INSTALLED IAW ECRA 5380-01013.SDR CALA0300651Attach Angle · gougedINSPECTION FOUND ATTACH ANGLE ON LT SIDE OF VERTICAL STABILIZER ON FUSELAGE EXTERIOR AT STA 1121 GOUGED. A NEW ANGLE WAS INSTALLED IAW ECRA 5380-01013.SDR CALA0300649Bushing · corrodedINSPECTION FOUND LT HORIZONTAL STABILIZER FORWARD LUG HAD CORROSION AFT BUSHING. REMOVED AND REPLACED BUSHINGS ON LT HORIZONTAL STABILIZER FWD UPPER IAW SRM 55-10-10.SDR CALA0300618Skin · gougedINSPECTION FOUND RT HORIZONTAL STABILIZER LOWER SKIN GOUGED AT STAB STA 111. THE GOUGED AREA OF SKIN WAS REMOVED AND A DOUBLER AND FILLER WERE INSTALLED IAW SRM 55-10-01, FIGURE 207.SDR CALA0300613Skin · chafedUPPER FUSELAGE SKIN WORN AT STA 867 RBL 5 AND LBL 5 UNDER DORSAL FIN, APPROX 3 X 10 INCH. CUT OUT DAMAGE AND REPAIRED PER SRM 53-00-01 FIG 202.SDR CALA0300612Channel · corrodedR2 DOOR JAMB Z-CHANNEL CORRODED AT STA 992.8. REMOVED AND REPLACED CORRODED Z-ANGLE AT R2 DOOR PER SRM 51-40-02.SDR CALA0300593Channel · crackedINSPECTION FOUND A 1INCH CRACK IN LT PYLON RT SIDE VERTICAL CHANNEL THAT FORWARD END PANEL NR 5843R AND AFT END OF PANEL NR 5842R ATTACHES TO. A NEW SPLICE PLATE WAS INSTALLED IAW SRM 51-40-02.SDR CALA0300596Doubler · crackedINSPECTION FOUND THE EXTERNAL POWER DOOR CUTOUT SKIN DOUBLER CRACKED AT THE FORWARD LOWER CORNER. THE SKIN DOUBLER WAS REPAIRED IAW ECRA 5330-03290. IN ORDER TO VERIFY CRACK REMOVAL IN THE DOUBLER, THE II-SECTION(EXTRUSION) REQUIRED REMOVAL. THE II-SECTION ANDSDR CALA0300569Angle · corrodedINSPECTION FOUND UPPER SURFACE OF R-2 DOOR Z-ANGLE CORRODED. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0300565Skin · dentedINSPECTION FOUND LOWER SURFACE OF LT HORIZONTAL STABILIZER SKIN DENTED APPROXIMATELY 8 INCHES FORWARD OF AFT SPAR AND 102 INCHES O/B OF FUSELAGE. A REPAIR WAS INSTALLED IAW SRM 55-10-01.SDR CALA0300561Panel · crackedINSPECTION FOUND CRACKS ON THE LOWER SIDE OF THE LT HORIZONTAL STABILIZER LEADING EDGE PANEL. THE CRACKS WERE CONFINED TO THE BONDED INTERNAL DOUBLER AT ONE FASTENER HOLE, 5.2 INCHES OB OF THE STA 188 RIB. THE AREA WAS REPAIRED IAW ECRA 5510-01695.SDR CALA0300528Fire Detector · inoperativeTHE APU FIRE DETECTION LIGHT ILLUMINATED WHILE ENROUTE FROM PHL TO IAH. THE APU FIRE BOTTLE WAS DISCHARGED, BUT THE WARNING LIGHT REMAINED ILLUMINATED. THE AIRCRAFT WAS DIVERTED TO ATL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. THSDR CALA0300527Connector · looseINSPECTION FOUND EMERGENCY LIGHT ABOVE LT OVERWING EXIT INOPERATIVE. MAINTENANCE FOUND DISCONNECT ON LT OVERWING EXIT LIGHT ASSEMBLY L-7 AND L-751 WITH LOOSE CONNECTOR D2976 AND LOOSE GROUND GD 1912-DC. RECONNECTED AND OPERATION CHECKED GOOD.SDR CALA0300526Skin · dentedINSPECTION FOUND C-2 DOOR OUTER SKIN DENTED ABOVE HANDLE. THE DOOR SKIN WAS REPAIRED IAW SRM 52-00-01.
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