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 CALA0500005Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT SCREW HOLE ON FORWARD FLANGE AT STA 986.5, RBL 43 TO RBL 44. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW SRM 53-00-51, FIGURE 203.SDR CALA0500004Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT SCREW HOLE ON FORWARD FLANGE AT STA 986.5, RBL 29. THE CORROSION WAS REMOVED AND A STRAP REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 203.SDR CALA0500034Throttle Cable · jammedTHE NR 1 THROTTLE JAMMED AND DID NOT RETARD (STUCK AT 83 PERCENT N1) ON INITIAL LEVEL OFF. THE NR 1 ENGINE WAS SHUTDOWN FOLLOWING QRH. THROTTLES SPLIT. TRIED TURNING OFF AUTOTHROTTLE TO NO AVAIL. THE NR 1 THRUST CONTROL PUSH-PULL CABLE WAS REMOVED AND REPLSDR CALA0500033Throttle Cable · stiffTHE THROTTLES WOULD NOT REDUCE TO CLIMB POWER IN VNAV CAPTAIN SIDE THROTTLES WERE VERY STIFF. TROUBLESHOOTING FOUND BOTH NR 1 & NR 2 ENGINE THRUST CONTROL PUSH-PULL CABLES AT FAULT. THE NR 1 & NR 2 ENGINE THRUST CONTROL PUSH-PULL CABLES WERE REMOVED AND REPLSDR CALA0400685Angle · corrodedINSPECTION FOUND CABIN FLOOR R-2 ENTRYWAY Z-ANGLE CORRODED AT STA 943-993, RBL 50. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0400681Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN PILOT'S FORWARD WINDOW POST SKIN AT NR 1 WINDSHIELD UPPER O/B CORNER, STA 196.5, S6L. THE CRACKED AREA WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-10-01, FIGURE 210.SDR CALA0400661Keelbeam · corrodedRIGHT KEEL BEAM HAS TWO NUT PLATES THAT APPEAR TO HAVE CORROSION UNDER THEM AT STATION 724 AND 721. FABRICATED AND INSTALLED REPAIR PER EC/RA 5311-01204.SDR CALA0400627Relay · burnedON FINAL APPROACH, A/C LOST MULTIPLE ELECTRICAL COMPONENTS INCLUDING NR 1 RADIO, NR 1 & 2 FWD FUEL PUMPS, ANTI-SKID, TR-1 SHOWED ZERO, AUTO BRAKE, YAW DAMPER, NR 1 ELEC HYD, EMERGENCY EXIT LIGHTS, NR 1 N 2, & FUEL FLOW GUAGE. A/C LANDED W/OUT PROBLEM. NR 1 TR SDR CALA0400624Skin · dentedINSPECTION FOUND THE LT WING NR 3 SPOILER DENTED ABOVE THE ACTUATOR. THE SPOILER WAS REPAIRED IAW SRM 57-70-01.SDR CALA0400623Skin · dentedINSPECTION FOUND THE RT WING NR 6 SPOILER DENTED ABOVE ACTUATOR. THE SPOILER WAS REPAIRED IAW SRM 57-70-01.SDR CALA0400622Skin · dentedINSPECTION FOUND THE RT WING NR 7 SPOILER DENTED. THE SPOILER WAS REPAIRED IAW SRM 57-70-01.SDR CALA0400621Angle · crackedINSPECTION FOUND A 4 INCH CRACK IN UPPER ANGLE ON INTERCOSTAL ADJACENT TO CABIN FLOOR A/C DISTRIBUTION BAY AT STA 482B-520 IN FORWARD CARGO BIN. A NEW UPPER ANGLE WAS INSTALLED IAW SRM 51-40-02.SDR CALA0400605Power Supply · inoperativeTHE FIRST CLASS CABIN SEAT EMERGENCY LIGHTS WOULD NOT TEST. THE M1674 POWER SUPPLY WAS REMOVED AND REPLACED IAW MM 33-51-51.SDR CALA0400603Frame · cutINSPECTION FOUND A 3 INCH CUT IN WEB ON FRAME AT STA 219.8, RBL 20. A DOUBLER WAS INSTALLED IAW SRM 51-70-13.SDR CALA0400591Angle · corrodedINSPECTION FOUND L-2 DOOR ZEE ANGLE CORRODED IN SEVERAL AREAS FROM BS 910-1016. THE ZEE ANGLE WAS REPLACED IAW SRM 51-10-2.SDR CALA0400585Skin · dentedINSPECTION FOUND A DENT IN FUSELAGE SKIN AT PRODUCTION LAP JOINT APPROXIMATELY FIVE FEET BELOW R-1 DOOR, STA 294, S24R. THE SKIN WAS REPAIRED IAW SRM 53-00-01, FIGURE 229, SHEET 41.SDR CALA0400590Fitting · crackedINSPECTION FOUND A CRACK IN THE FORWARD ENTRY DOOR UPPER AFT CORNER DOOR STOP. THE DOOR STOP FITTING WAS REMOVED AND REPLACED IAW ECRA 5210-01783.SDR CALA0400581Intercostal · crackedINSPECTION FOUND A 24 INCH CRACK IN INTERCOSTAL AT TOP FASTENER HOLES AT STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.SDR CALA0400576Skin · damagedINSPECTION FOUND A DEEP CREASE IN FUSELAGE SKIN AT STA 986.5, S26L TO S26R. A REPAIR WAS INSTALLED IAW ECRA 5331-01131. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR ON OR BEFORE JULY 14, 2006 OR THE ACCUMULATION OF 14,390 TOTAL FLIGHT CYCLES.SDR CALA0400565Fuse · blownTHE EMERGENCY EXIT LIGHTS ABOVE L-2 DOOR AND FLOOR PATH LIGHTS ON ROWS 18-21 WERE FOUND INOPERATIVE. THE BATTERY PACK FUSE WAS REMOVED AND REPLACED IAW MM 33-51-02-101.SDR CALA0400557Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, LBL 42. THE CORROSION WAS REMOVED AND A STRAP WAS INSTALLED IAW ECRA 5321-01196.SDR CALA0400529Linkage · brokenA LOUD NOISE WAS HEARD AND VIBRATION WAS FELT COMING FROM THE NOSE GEAR WHEEL WELL AREA AFTER GEAR RETRACTION LEAVING JAX. THE NOISE STOPPED WHEN THE GEAR WAS LOWERED FOR A RETURN TO JAX. MAINTENANCE FOUND RT NOSE GEAR DOOR LOWER LINKAGE BROKEN. THE LINKAGESDR CALA0400528Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT UPPER FLANGE FASTENER HOLE IN E&E COMPARTMENT BILGE AREA, STA 300, LBL 4. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND BOEING DRAWING 69-48283.SDR CALA0400523Intercostal · crackedINSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT NUT PLATE HOLES, STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.SDR CALA0400521Skin · dentedINSPECTION FOUND FORWARD BAGGAGE BIN DOOR OUTER SKIN DENTED 15 INCHES FROM TOP AND 18 INCHES FROM AFT. A DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.SDR CALA0400513Pressure Panel · crackedINSPECTION FOUND A 3 INCH CRACK IN PRESSURE WEB AT STA 727, RBL 17, FORWARD SIDE IN WHEEL WELL. THE CRACKED AREA WAS CUT OUT AND A DOUBLER AND FILLERS WERE INSTALLED IAW ECRA 5330-03352.SDR CALA0400498Floorbeam · corrodedINSPECTION FOUND AFT MAIN CABIN FLOORBEAM CORRODED AT FS 986, LBL 46. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-31, FIGURE 203.SDR CALA0400493Shutoff Valve · shortedTHE AUTOTHROTTLE DISCONNECTED AND THE NR 1 ENGINE AUTO SHUTDOWN ON FINAL APPROACH TO IAH. NO RESTART WAS ATTEMPTED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE FOUND CANNON PLUG D05162P SHORTED WHICH CAUSED THE NR 1 ENGINE FUEL S/O VALVE TO POWSDR CALA0400494Skin · puncturedINSPECTION FOUND RIGHT HORIZONTAL STABILIZER UPPER SKIN PUNCTURED AT STAB STA 203. THE PUNCTURED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW 55-10-01.SDR CALA0400492Floorbeam · corrodedINSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 927, BL 0, WL 208. THE FLOORBEAM WAS REPAIRED IAW SRM 53-60-51, FIGURE 203.SDR CALA0400491Intercostal · crackedINSPECTION FOUND A 2 INCH CRACK IN UPPER FLANGE OF INTERCOSTAL AT STA 344-360, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02 AND DRAWING 65C33970.SDR CALA0400488Sleeve · crackedINSPECTION FOUND A 1.6" CRACK IN I/B THRUST REVERSER SLEEVE. THE SLEEVE WAS REPAIRED IAW SRM 51-70-17.SDR CALA0400481Skin · corrodedINSPECTION FOUND FUSELAGE SKIN CORRODED AFT OF FORWARD BAG BIN DOOR CUTOUT AT STA 452, S22R. A REPAIR WAS INSTALLED IAW ECRA 5330-03351.SDR CALA0400479Skin · dentedINSPECTION FOUND RT HORIZONTAL STABILIZER LEADING EDGE SKIN DENTED AT STA 105.26. THE DENTED AREA WAS CUT OUT AND A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5510-01741.SDR CALA0400438Angle · corrodedR2 DOOR CUTOUT THRESHOLD Z-ANGLE CORRODED. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02.SDR CALA0400437Angle · wornLEFT WING TRAILING EDGE PANEL WORN JUST INBOARD OF NUMBER 3 FLAP TRACK FAIRING. REMOVED AND REPLACED ANGLE PER SRM 51-10-02.SDR CALA0400406Tab · delaminatedLEFT ELEVATOR TAB DELAMINATED OUTBOARD END AT TRAILING EDGE WEDGE (1 INCH). REPAIRED LEFT ELEVATOR TAB PER SRM 51-70-04.SDR CALA0400392Tab · delaminatedLEFT ELEVATOR TAB DELAMINATED (1 INCH SQ) AT OUTBOARD END OF TRAILING EDGE. REPAIRED LEFT ELEVATOR TAB PER SRM 51-70-04.SDR CALA0400391Stop Fitting · crackedR2 DOOR STOP FITTING CRACKED (1 INCH) FORWARD UPPER FITTING SECOND FROM TOP. REMOVED AND REPLACED FITTING PER SRM 51-40-02.SDR CALA0400360Intercostal · crackedINSPECTION FOUND A 3 INCH CRACK IN CABIN FLOOR INTERCOSTAL BETWEEN FS 344-360, BL 0. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 53-10-51.SDR CALA0400358Intercostal · crackedINSPECTION FOUND A 1.5 INCH CRACK IN CABIN FLOOR INTERCOSTAL BETWEEN FS 344-360, LBL 12. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02.SDR CALA0400278Sill · corrodedINSPECTION FOUND AFT BAGGAGE BIN LOWER SILL CORRODED AT STA 794.3-847, S24R-25R. THE LOWER SILL WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0400272Angle · crackedINSPECTION FOUND A 1.5 INCH CRACK IN ANGLE AT FORWARD BULKHEAD STA 727, RBL 3. A DOUBLER WAS INSTALLED ON THE ANGLE IAW SRM 51-70-11.SDR CALA0400270Floor Support · crackedINSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT BETWEEN STA 312-328, LBL 46. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0400261Panel · brokenINSPECTION FOUND LEFT AILERON PANEL 8106L BROKEN AT CENTER OF PANEL. REPAIRED IAW SRM 51-70-05.SDR CALA0400266Skin Panel · dentedINSPECTION FOUND FUSELAGE SKIN PANEL DENTED BELOW THE FORWARD CARGO DOOR CUTOUT BETWEEN STA 420 AND 440, S27L S26R. REPAIRED IAW ECRA 5311-01190.SDR CALA0400250Bottle · dischargedINSPECTION FOUND R-2 DOOR SLIDE BOTTLE PRESSURE LOW. THE R-2 DOOR SLIDE WAS REMOVED AND REPLACED IAW MM 25-60.SDR CALA0400249Skin · dentedINSPECTION FOUND LEADING EDGE SKIN UNDER NR 6 SLAT DENTED. A HOT BOND REPAIR WAS PERFORMED IAW SRM 51-70-04.SDR CALA0400242Beltframe · bentINSPECTION FOUND BELTFRAME IN FORWARD BAG BIN BENT AT STA 440 BETWEEN S28R AND 27R. REPAIRED BELTFRAME IAW SRM 53-00-07 FIGURE 205.SDR CALA0400219Bracket · crackedINSPECTION FOUND A .75 INCH CRACK IN BRACKET AT BULKHEAD STA 727, RBL 3. A TYPICAL FORM SECTION REPAIR WAS INSTALLED IAW SRM 51-70-11.
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