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 AWXA200301523Doubler · crackedDURING C-18 CHECK A .5 INCH CRACK WAS FOUND ON RT WING NR 6 FLAP TRACK FAIRING TRACK GUIDE DOUBLER AT WBL 204.4. MAINTENANCE REMOVED AND REPLACED THE RT WING NR 6 FLAP TRACK FAIRING TRACK GUIDE DOUBLER AT WBL 204.4 IAW B737-300 SRM 51-40-02 PG 1.SDR AWXA200301511Outflow Valve · faultyEN ROUTE, AT CRUISE FL 24000. CABIN ALTITUDE KEPT CLIMBING AT 400 FPM UNTIL IT REACHED 10000 FT. DIVERTED TO LAS, NO MASKS DEPLOYED. MAINTENANCE PERFORMED PRESSURIZATION INTEGRITY CHECK, TEST FAILED. REMOVED AND REPLACED OUTFLOW VALVE IAW T/C R6A21001. ALSSDR SWAA032603Control Panel · faultyDIVERSION, CABIN ALTITUDE WARNING HORN SOUNDED, BOTH A/C PACKS SET IN HIGH AND NO HELP, OUTFLOW VALVE INDICATED FULL CLOSED. REMOVED AND REPLACED CABIN PRESS CONTROL PANEL AND RESEALED L1 DOOR HINGE AREAS PER MM.SDR DL733031048Oven · failedON TAKEOFF, SMOKE FROM FWD GALLEY OVEN. REPLACED SAME.SDR AWXA200301489Light · brokenPHX - EEL - DURING 8-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 18 LT BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT SEAT ROW 18 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301480Module · failedON DESCENT, A-SYSTEM HYDS FAILED, A/C WAS TOWED OFF RUNWAY TO GATE. MX FOUND CHECK VALVE BLOWN OUT OF A-SYSTEM HYD PRESSURE MANIFOLD, R / R A-SYSTEM HYD PRESSURE MODULE ASSY IAW BMM. DUE TO LOSS OF FLUID REPLACED A-SYSTEM HYD EDP IAW T/C R5M29001, A-SYSTEM HSDR AWXA200301478Battery · dischargedPHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD.SDR USAASB03204Circuit Card · failedON FINAL APPROACH, CREW RECEIVED THREE GREEN AND THREE RED GEAR LIGHTS AFTER GEAR WAS SELECTED DOWN. CREW RAISED THE GEAR AD EXECUTED A GO-AROUND. QUICK REFERENCE HANDBOOK PROCEDURES WERE ACCOMPLISHED AND ON THRID GEAR CYCLE, RED UNSAFE LIGHTS REMAINED EXTINSDR AWXA200301350Odor · detectedSLC - DIVERSION - FLT 0587 - EN ROUTE FROM PHX TO GEG FLIGHT ATTENDANTS NOTICED A STRONG SULFUR ODOR IN THE CABIN THAT SEEMED TO COME AND GO, DIVERTED TO SLC. MAINTENANCE RAN AIR CONDITIONING PACKS, PRESSURIZED THE AIRCRAFT AND INSPECTED THE INTERIOR LIGHTINGSDR AWXA200301334Light · brokenPHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 11 LT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 11 LT, OPERATIONAL CHECK WAS GOOD.SDR F3LA200300152Support · crackedDURING C-5 CHECK, INSPECTION REPORTED ATTACH ANGLE CRACKED AT LOWER AFT END OF NR 1 PYLON. REPLACED DAMAGED SUPPORT IAW SRM 51-40-02.SDR F3LA200300151Channel · crackedDURING C-5 CHECK, INSPECTION REPORTED NR 1 ENGINE CHANNEL CRACKED OUTBOARD LOWER AFT END LT PYLON AT STA 320. REPLACED CHANNEL PER SRM 51-40-02.SDR F3LA200300150Frame · crackedDURING C-5 CHECK, INSPECTION REPORTED AFT LOWER END OF NR 1 ENGINE PYLON AT STA. 363 CRACKED. REPLACED NR 1 ENGINE AFT LOWER END "A" FRAME IAW SRM 51-40-02.SDR USAA030214Stiffener · corrodedFOUND RADIAL STIFFENER CORRODED 2 INCH BY 1 INCH AREA, AFT PRESS BULKHEAD STATION 1016 AT BL 0. INSTALLED SPLICE SECTION AND REPAIR DOUBLERS PER EO 5302V112 AND BOEING DWG 65C28106 AND EA 77188. (M)SDR USAASB03182Proximity Sensor · inoperativeON CLIMB-OUT FROM CLT, EN ROUTE TO IAH, CREW RECEIVED A NOSE LANDING GEAR RED UNSAFE LIGHT WHEN GEAR WAS RETRACTED. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND RECYCLED GEAR. RECEIVED THREE GREEN LIGHTS WHEN GEAR WAS DOWN AND WHEN GEAR WAS BROUGHT USDR USAASB03179Control Column · stiffEN ROUTE FROM CLT TO RDU, CREW REPORTED STIFF FLIGHT CONTROLS, ELEVATOR AND AILERONS. FEELS SOMEWHAT LIKE MANUAL REVERSION. DURING FLARE ON FINAL, THE CONTROL COLUMN BOUND FOR A MOMENT AND THEN BROKE FREE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCSDR USASB03177Battery Pack · inoperativeMAINTENANCE REPORTED SEVERAL CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN CEILING ABOVE SEAT ROW 10R. OPERATIONAL CHECK GOOD. (M)SDR USAASB03180Controller · overheatedEN ROUTE FROM CLT TO DFW, CREW REPORTED AN ELECTRICAL BURNING ODOR IN FORWARD GALLEY. OVEN, CONTROLLER AND BACKWALL OF GALLEY WAS HOT. TURNING OFF GALLEY POWER APPEARED TO BE OF SOME HELP. FLIGHT LANDED AT DFW WITHOUT FURTHER INCIDENT. MAINTENANCE IN DFW PUSDR USAASB03176Battery · inoperativeFOUND AFT GALLEY DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)SDR DL733030901Indicator · malfunctionedCAPTS VSI STARTED SPARKING WHEN AT THE GATE IN SLC BRIEF ELECTRICAL FIRE FOLLOWED BY SMOKE IN COCKPIT. C PERFORMED EXTERNAL LEAK CHECK OF AREA ABOVE CAPT'S INSTRMENT CLUSTER NO FLUID LEAKS DETECTED. FOUND AN EMPTY SCREW HOLE IN THE GLARE SHIELD ABOVE THE INSTSDR AWXA200301242Web · crackedMCN - MINOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON RT AFT OUTBOARD SUBFLOOR WEB BS 992, RBL 60, WL 206. MAINTENANCE CUT OUT DAMAGE ON RT AFT OUTBOARD SUBFLOOR WEB BS 992, RBL 60, WL 206; FABRICATED A FILLER AND REPAIR PLATE; INSTALLED REPAIR PSDR AWXA200301199Retainer · missingON ROLL BACK PRIOR TO TAXI RT INBOARD MAIN LANDING GEAR WHEEL ASSEMBLY WAS NOTICED COMING OFF AXLE. UPON FURTHER INVESTIGATION THE NR 3 WHEEL RETAINER RING WAS FOUND MISSING AND THE AXLE NUT WAS BACKED OFF. DAMAGE WAS NOTED TO THE WHEEL AND BRAKE ASSEMBLIES, SDR AWXA200301251Floorbeam · crackedDURING C-17 CHECK A 2.2500 INCH CRACK WAS FOUND ON CABIN FLOORBEAM AT BS 660, BL (0), WL 208. MAINTENANCE PERFORMED A HFEC INSPECTION OF CRACK AND FOUND UPPER CHORD (REINFORCING ANGLE) SEVERED; REMOVED STIFFENERS, ANGLE AND SECTION OF WEB AND DOUBLER; CUTOUT CSDR AWXA200301256Skin · debondedMCN - MINOR REPAIR - DURING C-17 CHECK FOUND TOP CENTER AREA OF TAIL CONE DISBONDED, 18 INCHES-22 INCHES FROM FORWARD EDGE. MAINTENANCE CUTOUT DISBONDED AREA OF TOP CENTER TAIL CONE, 18 INCH-22 INCHES FROM FORWARD EDGE AND PERFORMED A BOND REPAIR IAW B737-300 SDR AWXA200301246Intercostal · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT INTERCOSTAL AT STR 25 RT, BETWEEN BS 747 AND BS 767. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AFT CARGO COMPARTMENT INTERCOSTAL AT STR 25 RT, SDR AWXA200301243Rib · crackedDURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BRACKET BELOW UPPER RUDDER HINGE, AT RDR STA 196. MAINTENANCE REMOVED CRACKED BRACKET BELOW UPPER RUDDER HINGE AT RDR STA 196; FABRICATED A NEW REPLACEMENT BRACKET PER DWG 65C25971; INSTALLED REPAIR PART IAW B737SDR AWXA200301230Bulkhead · crackedDURING C-17 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD VERTICAL WEB AT LIGHTENING HOLE RBL 17, WL 184. MAINTENANCE CUT OUT DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL WEB AT RBL 17, WL 184; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST;SDR AWXA200301257Connector · damagedMCN - EEL - DURING C-17 CHECK SEVERAL EMERGENCY ESCAPE PATH LIGHT HARNESS CONNECTORS WERE FOUND DAMAGED BETWEEN BS 370 TO BS 920 L/H SIDE. MAINTENANCE REMOVED AND REPLACED DAMAGED EMERGENCY ESCAPE PATH LIGHT HARNESS CONNECTORS AND SPLICES BETWEEN BS 370 TO BS SDR AWXA200301234Bulkhead · crackedDURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB ON FORWARD SIDE AT EDGE OF STRAP RUNNING VERTICALLY, RBL 4.75, WL 212. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB ON FORWARD SIDE AT RBL 4.75, WL 212; FABRICATED A REPAIR DOUBLER; INSTALSDR AWXA200301247Support · corrodedDURING C-17 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT SUPPORT ZEE AROUND NUT PLATE HOLES BS 727D-767, RBL 17. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AFT CARGO COMPARTMENT SUPPORT ZEE BS 727D-767, RBL 17; INSDR AWXA200301241Crease Beam · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT CREASE BEAM UPPER SURFACE OF BOTTOM LEG BS 940-993, RBL 52, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED RT AFT CREASE BEAM BS 940-993, RBL 52 TO RBL 54,SDR AWXA200301240Filler · corrodedDURING C-17 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FILLER PLATE BS 951, RBL 49, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FILLER PLATE BS 951, RBL 49, WL 208; FABRICATED A TAPERED FILLER PER DWG 65C10592SDR AWXA200301239Strap · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT SUBFLOOR UPPER STIFFENER AT BS 1019-1023, RBL 27.5, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED RT AFT SUBFLOOR UPPER STIFFENER AT SDR AWXA200301238Shear Tie · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF LT AFT OUTBOARD SHEAR WEB BS 986-1016, LBL 38-46, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED LT AFT OUTBOARD SSDR AWXA200301237Pan · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF RT AFT LAVATORY SUBFLOOR PAN REPAIR DOUBLER BS 1020, RBL 15, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED RT AFT LAVATORY SUBFLOOR PASDR AWXA200301236Floor Support · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT FORWARD LEG BS 992, LBL 28-45, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT BS 992, LBL 28-45, WL 208; FABRICATED SDR AWXA200301235Floor Support · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT INBOARD LEG BS 1006-1016, LBL 37, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT BS 1006-1016, LBL 37, WL 2SDR AWXA200301232Strap · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF AFT CENTER SUBFLOOR PAN UPPER STRAP AT BS 1006-1029, LBL 5 TO RBL 5, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED SUBFLOOR PSDR AWXA200301229Skin · chafedDURING C-17 CHECK THE UPPER SURFACE OF RT OUTBOARD FORE FLAP HAS A CHAFE MARK AT OUTBOARD END OF NR 7 SPOILER. MAINTENANCE REMOVED DAMAGE RT OUTBOARD FORE FLAP AT OUTBOARD END OF NR 7 SPOILER; CLEANED AND PREPARED SURFACE; FABRICATED REPAIR DOUBLERS; INSTALLESDR AWXA200301228Filler · corrodedDURING C-17 CHECK CORROSION WAS FOUND ON UPPER SURFACE OF FILLER PLATE AT BS 951, RBL 44, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FILLER PLATE AND FILLER AT BS 951, RBL 44, WL 208; FABRICATED A NEW REPLACEMENSDR AWXA200301227Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FLOOR SUPPORT UPPER AFT LEG BS 963, RBL 40, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT BS 963, RBL 40, WL SDR AWXA200301226Angle · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT LAVATORY AFT MOUNT SUPPORT ANGLE BS 1028, RBL 18, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED AFT LAV MOUNT SUPPORT ANGLE BS 1028, RBL 18, WL 208; FABRISDR AWXA200301225Floor Support · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT AT BS 993, RBL 44, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOOR SUPPORT AT BS 993, RBL 24 TO RBL 44, WL 208; FABRSDR AWXA200301223Angle · crackedDURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON ANGLE, TOP OF NR 6 FLAP FAIRING, FORWARD OF CLOSEOUT DOOR WBL 191. MAINTENANCE REMOVED CRACKED ANGLE AT WBL 191; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 65C26309; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-0SDR AWXA200301249Stringer Clip · crackedDURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 360, STR 4 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 360, STR 4 LT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-46831; INSTALLED REPAIR PART IAW B737-300 SRM 51-70-11 PSDR AWXA200301248Rib · crackedDURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON THE 8TH RIB FROM OUTBOARD END ON RT HORIZONTAL STABILIZER LEADING EDGE. MAINTENANCE CUT OUT CRACK ON RIB RT HORIZONTAL STABILIZER LEADING EDGE; FABRICATED A REPAIR ANGLE PER DWG 65-47993; INSTALLED REPAIR PART IAWSDR AWXA200301244Channel · crackedDURING C-17 CHECK A .75 INCH CRACK WAS FOUND ON FLOOR ATTACH CHANNEL BS 787, ABOVE STRINGER 26 RT. MAINTENANCE REMOVED CRACKED FLOOR ATTACH CHANNEL BS 787, STR 26 RT; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PG 1.SDR AWXA200301220Stringer Clip · crackedDURING C-17 CHECK A .375 INCH CRACK WAS FOUND ON STRINGER TIE CLIP BS 380, STR 7 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP BS 380, STR 7 LT; INSTALLED NEW REPLACEMENT TIE CLIP IAW B737-300 SRM 51-40-02, PG 1, FIG 8.SDR AWXA200301233Frame · crackedDURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD LT SIDE CHORD AT WL 207. MAINTENANCE REMOVED CRACKED BS 178 BULKHEAD LT SIDE CHORD AT WL 207; FABRICATED A NEW REPLACEMENT SIDE CHORD; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG 3-4, & 38,SDR AWXA200301231Frame · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1.5 PERCENT CRACK WAS FOUND ON INBOARD RADIUS OF BS 178 BULKHEAD VERTICAL WEB AT LBL 5.7, WL 186. MAINTENANCE CUT OUT DAMAGED SECTION OF BS 178 BULKHEAD VERTICAL WEB AT LBL 5.7, WL 186; PERFORMED HFEC INSPECTION OF CUT
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