Boeing 737-522
Service difficulty reports · 1,682
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 = '737522' 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 = '737522' 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 142Skin · damagedAFT CARGO DOOR REQUIRES RESKIN.SDR DU4R0507141Skin · dentedRIGHT WING INBOARD FORE FLAP LOWER SKIN SURFACE HAS NUMEROUS DENTS.SDR DU4R0507002Skin · chafedLT WING NR 3 SLAT HAS SKIN CHAFED THRU AT T/E LOWER IB SKIN SURFACE. S/O 269008, OPS NR 24936SDR DU4R00507139Skin · gougedRIGHT WING NR 4 SLAT HAS SKIN CHAFED THRU AT T/E LOWER INBOARD SKIN SURFACE.SDR 138Skin · gougedRT WING OB FORE FLAP GOUGED ON OB END. S/O 269008, OPS NR 24931.SDR DU4R0507001Skin · dentedLT WING IB FWD FLAP LWR SIDE HAS 8 DENTS AT STA. WBL 85 TO 95 AT VARIOUS LOCATIONS.SDR DU4R0507126Stringer · crackedCABIN S-15L CRACKED, ALSO END FITTING.SDR CA050629002Pump · failed(CAN) ON APPROACH THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP (EDP) LOW PRESSURE LIGHT ILLUMINATED. THE A-SYSTEM HYDRAULIC QUANTITY WAS ALSO LOW AT 22 PERCENT. THE AIRCRAFT CONTINUED TO THE DESTINATION WITHOUT ANY INCIDENT. MAINTENANCE INSPECTION REVEALED A DAMAGSDR 2005UALA00602Strip · missingAFT GALLEY EMERGENCY EEL STRIP IN FRONT OF CART STOWAGE COMPARTMENT MISSING. SUPPLEMENTAL DATA UPDATE EEL STRIP WAS MISSING AND WAS REPLACED.SDR 2005UALA00588Battery Pack · dischargedEMERGENCY LIGHTS INOP AT DOOR 1L EXTERIOR SLIDE LIGHT, FIRST CLASS EEL LIGHTS, BULLNOSE LIGHT AT SEATS 2B & 6C, EXIT SIGN OVER DOOR 1R & FLIGHT DECK DOOR, AND FLIGHT DECK EMERGENCY DOME LIGHT. BATTERY PACK WAS REPLACED, OK.SDR 2005UALA00561Connector · inoperativeEEL LIGHTS OUT FROM ROW 15 BACK. *S/D* EEL LIGHT CONNECTORS WERE REMOVED, CLEANED AND REINSTALLED.SDR 2005UALA00555Structure · dentedNR 2 ENGINE INLET COWL DENTED AT APPROXIMATELY 4 O`CLOCK. DENT IS OUT OF LIMITS. INSTALLED REPAIR PER SRM 54-10-01 FIG 203 DET II.SDR 2005UALA00530Frame · crackedBODY STATION 663 FRAME IS CRACKED AT STRINGER CUTOUTS 1R, 2R AND 3R. CRACKS ARE ON LT SIDE OF STRINGERS IN RADIUS NEAR FUSELAGE SIDE OF FRAME. INSTALLED DOUBLER REPAIR PER SRM 53-00-07 FIG 209.SDR 2005UALA00508Skin · damagedFUSELAGE SKIN AT AFT CARGO DOOR CUTOUT AFT SIDE HAS HOLE IN FUSELAGE SKIN BUT NOT IN BEAR STRAP, MID WAY UP CUTOUT. DAMAGED REMOVED, INSTALLED DOUBLER AND TRIPLER WITH FILLER PER SRM 53-00-01.SDR 2005UALA00494Crease Beam · corrodedCREASE BEAM AT DOOR 2R HAS CORROSION. REPLACED CREASE BEAM PER SRM 53-60-15 AND BOEING DRAWING 65-45855.SDR 2005UALA00493Skin · dentedSKIN DAMAGE AT FS 482, APPROX 2.5 FT AFT OF FORWARD CARGO DOOR, IN LINE WITH LOWER CUTOUT OF DOOR. UPPER DENT IS A=1.5 IN AND Y=0.093 IN. LOWER DENT IS A=1.0 IN AND Y=0.062 IN. DAMAGE AREAS ARE 2.5 INCHES APART. MAJOR REPAIR ACP'D PER SRM 53-00-01 FIGURE 22SDR 2005UALA00488Skin · crackedCRACKS FOUND AT BS 1006-1016 STR S6L. REPLACED TEMPORARY REPAIR AND INSTALLED PERMANENT DOUBLER REPAIR PER SRM 53-60-01 FIG 205.SDR 99Skin · dentedNUMEROUS DENTS ON AFT CARGO DOOR SKIN AND CREASES ON THE REPAIR DOUBLER. S/O 269010, NR 22292SDR 98Fitting · damagedSTRINGER 13L END FITTING REQUIRES PERMANENT REPAIR.SDR CA050510004Window · cracked(CAN) NR 4 WINDOW CRACKED AT ALTITUDE. WINDOW REPLACED.SDR 2005UALA00429Motor · inoperativeRETURNED TO BLOCKS DUE TO A CAPTAIN'S STICK SHAKER PROBLEM. CAPTAIN'S STICK SHAKER INOPERATIVE WHEN PERFORMING NR 1 STALL WARNING TEST. CLEANED AND INSPECTED PINS TO EIS DISPLAY AND STALL MANAGEMENT COMPUTER. THE EIS PRIMARY DISPLAY WAS REPLACED TO GET STICK SDR 2005UALA00402Wire · damagedD3732 HAS MULTIPLE WIRES DAMAGED FROM ARCING. CONNECTOR IS IN CEILING, INBOARD OF FWD LAV. REPLACED DISCONNECT D3732 AND REPAIRED DAMAGED WIRING. SECURED BUNDLE. AN EG CALLOUT WAS ISSUED TO LOOK AT SIX ADDITIONAL AIRPLANES. CHAFING WAS FOUND ON HARNESS INSULSDR 2005UALA00390Window · leakingFLIGHT RETURNED TO IAH DUE TO A FLIGHT DECK WINDOW AIR LEAK. F/O SLIDING WINDOW LEAKED, AFTER TAKEOFF. F/O SLIDING WINDOW HAD AN AIR LEAK. FOUND CLIP LODGED IN WINDOW FRAME. REMOVED AND INSPECTED AREA AND FOUND NO DAMAGES. SEAL INTACT AND AS PRECAUTIONARYSDR 2005UALA00370Warning Light · illuminatedLANDED UNDER AMBER ALERT IN IAH DUE TO SPLIT FLAPS INDICATION. THE SUBJECT SPLIT FLAP INDICATION AND ASSOCIATED INHIBITED FLAP MOVEMENT WAS DUE TO A FAULTY FLAP POSITION INDICATOR (PN 18-1299-6-2, PCN 421 9632). THE SUBJECT INDICATOR WAS REMOVED AND REPLACEDSDR UALA200504AASkin · dentedFOUND FUSELAGE EXTERNAL SKIN HAS A GROUP OF DENTS FROM BS 380-400 BETWEEN STR. 15L-17L. S/O 269010, N/R 22034SDR 2005UALA00301Battery Pack · inoperativeEEL FLOOR LIGHTS INOP ROWS 3-11 ABC. REPLACED BATTERY PACK M1134 .SDR CA050329002Window · broken(CAN) ON APPROACH, THE PILOTS NR 4 WINDSHIELD (EYEBROW) APPEARED TO SHATTER. THERE WAS NO LOSS OF PRESSURIZATION. THE LANDING WAS CONTINUED WITHOUT PROBLEM. ON INVESTIGATION, THE GLASS LAYER SEEMS TO HAVE FAILED. THE OUTER LAYERS WERE INTACT BUT THE INNER SDR 2005UALA00262Skin · dentedDENT ON FWD SIDE OF FWD CARGO DOOR, MEASURES 1.25 WIDE, .157 DEEP. MAJOR REPAIR ACCOMPLISHED. CAUSED BY CONTACT WITH LOADER. INSTALLED DOUBLER REPAIR.SDR 2005UALA00251Fire Loop · malfunctionedDIVERTED TO LNK DUE TO NR 2 ENGINE OVERHEAT INDICATION. SHUTDOWN NR 2 ENGINE AND BLEW BOTH FIRE BOTTLES. THERE WERE NO EVIDENCE OF FIRE OR OVERHEAT ON POST FLT INSP. REPLACED UPPER FAN OVERHEAT DETECTOR LOOP M1120. ENGINE OVERHEAT DETECTION SYSTEM TESTED NSDR CA050316003Arm · punctured(CAN) DURING GROUND HANDLING, MAINTENANCE DISCOVERED A SIGNIFICANT FUEL LEAK ON THE RT WING. FUEL WAS RUNNING DOWN THE OB FLAP CANOE AND DRIPPING ONTO GROUND. AIRCRAFT WAS REMOVED FROM SERVICE AND PLACED INTO HANGAR FOR FURTHER INSPECTION AND FUEL DRAINING. ASDR 2005UALA00245Overheat Loop · malfunctionedSHUT DOWN NR 2 ENG DUE TO OVERHEAT INDICATION. CREW REPORTED NR 2 ENG OVERHEAT LIGHT CAME ON WITH NO ABNORMAL ENGINE INDICATION. OVERHEAT LIGHT STAYED ON AFTER THE CHECKLIST. CREW SHUT DOWN NR 2 ENGINE. OVERHEAT LIGHT WENT OUT. UPON ARRIVAL AT THE GATE BOTHSDR LCQ75Skin · dentedDENT IN EXTERIOR FUSELAGE SKIN AT FS 412 S-18R. S/O 269004, N/R 24964.SDR LCQ74Skin · gougedGOUGE BETWEEN S-27L - S-28L BS 420. S/O 269004, N/R 24710.SDR LCQ73Tab · brokenCOMPOSITE TAB ON L/E SPAR OF RUDDER BROKEN OFF. S/O 269004, N/R 24993.SDR 2005UALA00172Frame · damaged178 BULKHEAD UPPER FRAME ANGLE LT SIDE AT SPLICE HAS 2 EACH HOLES WITH NO EDGE DISTANCE. TRIMMED THE DISCREPANT FRAME, FABRICATED AND INSTALLED REPAIR FRAME SPLICE ANGLE.SDR 2005UALA00105Overheat Loop · damagedDIVERTED TO SFO DUE TO WING BODY OVERHEAT INDICATION. CREW REPORTED RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM AND CONFIRMED A SHORT WITH RIGHT WING LEADING EDGE OVERHEAT DETECTOR LOOP MSDR 2005UALA00098Skin · dentedLT HORIZ STAB LEADING EDGE IS DENTED APROX 4' FROM FUSE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED DENT DAMAGE AND INSTALLED DOUBLER REPAIR.SDR 2005UALA00097Skin · dentedLEFT HORIZONTAL STABILIZER HAS A DENT IN THE LEADING EDGE, FOUND DENT APPROX 4 FT OUTBD ON L/E HORZ STAB. DIMENSIONS ARE 3 INCH BY 2 INCH BY .25 INCH DEEP WITHIN 1 INCH OF FASTENERS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INTERIM DOUBLER REPAIRSDR 2006UALA00101Frame · crackedCABIN FS 616 BELOW STR 17R FRAME CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED ANGLE AND FILLER REPAIR REF MM 53-11-89.SDR 2005UALA00083Frame · damagedBS 178 BULKHEAD ON THE UPPER LT CHORD WAS FOUND TO HAVE INSUFFECENT EDGE DISTANCE AT WL 230 FOR REQUIRED OVERSIZING OF FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED SPLICE REPAIR.SDR 2005UALA00075Floorbeam · corrodedSTA 294 FLOORBEAM UPPER CAP HAS MATERIAL LOSS FROM CORROSION REMOVAL AT RBL 39 TO RBL 52. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. CUTOUT DAMAGED SECTION AND INSTALLED DOUBLE FLANGE REPAIR.SDR 2005UALA00069Stringer · crackedSTR 16 RT HAS A CRACK AT STA 498B JUST AFT OF LIGHT ASSY. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION FROM STRINGER AND INSTALLED SPLICE REPAIR.SDR 2005UALA00073Floorbeam · corrodedSTA 986 FLOORBEAM FWD FLANGE HAS CORROSION FROM RBL 16 TO RBL 41. DATA MAJOR CUT-OUT DAMAGE AND INSTALLED REPAIR ANGLE AND FILLER.SDR 2005UALA00074Skin · dentedDENT FOUND AT LT SIDE OF FUSELAGE 3 FT AFT OF DOOR 1L SILL. CUT-OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR.SDR 2005UALA00072Floorbeam · corrodedFLOORBEAM AT STATION 947 HAS CORROSION FROM LBL 14 TO RBL 53. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTION OF FLOOR BEAM.SDR 2005UALA00063Floorbeam · corrodedFLOORBEAM CORRODED ON AFT FLANGE STA 986 FROM RBL 10 TO LBL 6. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. CUT-OUT DAMAGE AND INSTALLED REPAIR ANGLE AND FILLER.SDR 2005UALA00062Drain Valve · not closedAT FL250 UNABLE TO HOLD CABIN ALTITUDE. CABIN CLIMBING AT 1000 FPM. DRAIN VALVE IN BOTH THE AFT CARGO PIT AND E/E DOOR NOT CLOSING. LUBED FWD ONE AND CLEANED DEBRIS FROM AFT PIT DOOR VALVE.SDR 2005UALA00049Csd · overservicedDIVERTED TO SLC DUE TO ELECTRICAL PROBLEMS. FOUND CSD OVERSERVICED WITH OIL. CHECKED CSD CHIP DETECTOR, ALL DIFF. PRESSURE INDICATORS, ALL OK. SERVICED OIL TO PROPER LEVEL. RAN ENGINE AT IDLE. RESIDUAL VOLTS=19, FREQS 400, 119 VOLTS ALL NORMAL. GENERATOR OPS.SDR 2005UALA00047Stringer · crackedSTATION 482 STRINGER 16R IS CRACKED. INSTALLED SPLICED REPAIR.SDR 2005UALA00048Shear Web · crackedLEFT SHEAR WEB AT STA 194 IS CRACKED AT WL 207. REPLACED SHEAR WEB.
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