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 USAA051507Wedge · delaminatedFOUND DELAMINATION INBOARD FOREFLAP TOP SKIN INBOARD END. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 3.5.SDR USAA051489Attach Angle · crackedFOUND S15L INTERCOSTAL WEB FWD ATTACH ANGLE AT I/B END IN RADIUS. REMOVED AND REPLACED ANGLE IAW SRM 51-10-02 AND DWG NR 69-16970, DEFECT SIZE: 1/2" CRACK.SDR USAA051486Intercostal · corrodedFOUND INTERCOSTAL CORRODED BETWEEN STA 967 AND STA 986, LBL 18. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: 1/4 INCH SPOTS OF CORROSION ON TOP AND BOTTOM OF NUTPLATE HOLES ON INTERCOSTAL 18" LEN.SDR USAA051474Attach Angle · crackedFOUND CRACK S15L INTERCOSTAL WEB FWD ATTACH ANGLE AT I/B END IN RADIUS. REMOVED AND REPLACED ANGLE IAW SRM 51-10-02 AND DWG 69-16970, DEFECT SIZE: 1/2" CRACK.SDR USAA051475Splice · crackedFOUND SPLICE CRACKED, BS 908 AT STRINGER 5R. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 50-40-02, DEFECT SIZE: 2" CRACK.SDR USAA051473Floorbeam · corrodedFOUND CORROSION STA 986.5 BELOW TO BL45. REMOVED DAMAGED FABRICATED NEW T CAP AND INSTALLED ON FLOORBEAM IAW 53-10-05, DEFECT SIZE: .5 INCH AREAS OF CORROSION AROUND CLIP NUT HOLES 38 INCHES IN LENGTH.SDR USAA051469Intercostal · crackedS16L INTERCOSTAL WEB STA 300 CRACKED. REPLACED WITH IDENTICAL PART, FABRICATED WEB FROM .040 INCH 7075=T6, INSTALLED PER SRM 53-10-15.SDR USAA051468Intercostal · corrodedBETWEEN STA 967 & STA 986 LBL 18 CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-10-02, DEFECT SIZE: .25 INCH SPOT OF CORROSION ON TOP & BOTTOM OF NUT PLATE HOLES ON INTERCOSTAL.SDR USAA051463Skin · damagedLEFT RUDDER SKIN 4 FEET FROM THE BOTTOM. MAJOR REPAIR, REMOVED DAMAGED, LAYED UP AND CURED REPAIR PLYS IAW SRM 51-70-17, DEFECT SIZE: 2 X 12 INCHES.SDR USAA051452Repair · unknownFOUND COMPOSITE REPAIR LOWER SURFACEOF RT ELEVATOR, 26.5" OTBD OF INBD END 3" FWD OF THE T/E. COMPOSITE REPAIR IAW 55-40-01. DEFECT SIZE: COMPOISTE REPAIR AT LOWER SURFACE OF RT ELEVATOR, 26.5" OTBD OF INBD END 3" FWD.SDR USAA051451Repair · unbondedFOUND RUDDER COMPOSITE REPAIR APROX 7.5" DIA, 24" FWD OF T/E AND 41" UP FROM BOTTOM L/E. COMPOSITE REPAIR IAW SRM 55-40-01, DEFECT SIZE: APPROX 7.5" DIA LOCATED 24" FWD OF T/E AND 41" UP FROM BOTTOM L/E. (RT SIDE)SDR SB05156Actuator · crackedON APPROACH, CREW REPORTED THE LOSS OF SYSTEM A HYDRAULICS SHORTLY AFTER GEAR EXTENSION. CREW REPORTED THE PUMPS WERE OPERATING DRY FOR LESS THAN 2 MINUTES. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE FOUND THE NR 9 SPOILER ASDR SB05154Downlock Sensor · failedCLT - FLT266 ON CLIMB OUT FROM CLT, CREW REPORTED THE NOSE LANDING GEAR RED UNSAFE LIGHT ILLUMINMATED AFTER GEAR RETRACTION. CREW EXTENDED LANDING GEAR NORMALLY AND RETURNED TO FIELD. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. NO EMERGESDR USAA051411Skin · crackedLWR SURFACE AT AFT ROW OF FASTNERS AT ACTUATOR MAJOR REPAIR, INSTALLED DOUBLER IAW SRM 57-43-01 REPAIR 6.SDR USAA051412Skin · crackedLWR SURFACE, AFT ROW OF FASTENERS AT ACTUATOR CRACKED. MAJOR REPAIR, INSTALLED DOUBLER IAW SRM 57-43-01 REPAIR 6.SDR USAA051413Skin · debondedNR 2 SLAT T/E WEDGE SS 246.4 - 241.9 DEBONDED. INSTALLED DOUBLER IAW EA 97124. DEFECT SIZE: 5 INCH X 4 INCH.SDR USAA051410Skin · crackedLWR SURFACE, AFT FASTENER ROW AT OUTBOARD END TO 20.750 INCH INBOARD CRACKED. MAJOR REPAIR, INSTALLED DOUBLER IAW SRM 57-43-01 REPAIR 6.SDR SB05150Battery Pack · dischargedFLL - MAINTENANCE REPORTED THE AFT EMERGENCY LIGHT BATTERY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY. OPERATIONAL CHECK GOOD.SDR SB05147Fuse · blownMAINTENANCE REPORTED THE AFT LEFT EXTERIOR EMERGENCY LIGHT AND THE SEAT MOUNTED EMERGENCY LIGHTS AT ROWS 22 AND 23 INOPERATIVE. MAINTENANCE RELAMPED THE EXTERIOR EMERGENCY LIGHT AND REPLACED A BLOWN FUSE ON POWER SUPPLY M1197. OPERATIONAL CHECK GOOD.SDR USAA051406Skin · puncturedRIGHT WING LEADING EDGE ABOVE NR 4 LEADING EDGE FLAP, APPROX L/E STA 205 DENTED. REMOVED EXISTING REPAIR, CUT OUT DAMAGE, INSTALLED FILLER & DOUBLER PER EA 96961. DEFECT SIZE: .6"L X .4"W X .080"D, 2.5"L X 1"W X .100"D DENT & PUNCTURE, .75"L X .3"W.SDR USAA051405Skin · crackedFWD SERVICE DOOR BOTTOM HINGE CUTOUT SKIN CRACKED. FABRICATED DOUBLER & FILLER PER SRM 52-00-01, 52-10-01. DEFECT SIZE: .250 INCH.SDR USAA051404Angle · crackedMAIN CABIN FLOOR BELOW FLOOR AT BS 616 LEFT SIDE CRACKED. REMOVED & REPLACED ANGLE, INSTALLED FILLER PER SRM 51-40-02 & TYP REP 53-62-01. DEFECT SIZE: .5 INCH.SDR USAA051403Floorbeam · corrodedMAIN CABIN FLOORBEAM TEE STA 986.5 RBL 20-30 CORRODED. REMOVED & REPLACED TEE PER TYP REP 53-60-01. DEFECT SIZE: 10 INCHES.SDR SWAA053326Light · inoperativeDURING SCHEDULED A1 CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT INOP AFT OF LT WING. RELAMPED LIGHT ASSY PER MM.SDR SWAA053325Skin · crackedDURING SCHEDULED A1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 884, STR 25R. REPAIRED SKIN PER SRM.SDR USAA051221Angle · corrodedSTA 907 TO 1006; NO TASK OF LEVEL, CORROSION. FABRICATED PART PER TR 549929, DWG 6941226, SRM 51-40-02, 53-60-15, DEFECT SIZE: 2L X 0.5W X .049 INCH DEEP.SDR USAA051220Skin · debondedFWD ENTRY DOOR INNER WALL AT LWR SKIN DISBONDED. FABRICATED REPAIR DOUBLER, FILLER PER TR 52-10-16, DEFECT SIZE: 0.250 INCH.SDR USAA051211Skin · crackedBS 727 S19R CRACKED. INSTALLED DOUBLER IAW 53-00-01 FIG 201, DEFECT SIZE: 1.35 INCH.SDR USAA051210Skin · crackedBS 727E -10 S-18R CRACKED. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 201, REPAIR 31 DEFECT SIZE: 3.25 INCH.SDR SB05131Power Supply · inoperativeMAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 12 THROUGH 16 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD.SDR USAA051199Bulkhead · crackedAFT PRESSURE BULKHEAD CRACKED. REPAIRED AS REQUIRED, DOUBLER INSTALLED EA 96994, DEFECT SIZE 1 INCH.SDR SB05126Outflow Valve · faultyCLT - FLT568 - EN ROUTE FROM PIT TO RSW, AT FL310, AIRCRAFT WOULD NOT MAINTAIN CABIN PRESSURIZATION. CREW DESCENDED FLIGHT TO FL260 AND WAS ABLE TO GAIN CONTROL OF CABIN PRESSURE WITH PACKS IN HIGH FLOW MODE ONLY. MAINTENANCE ADVISED CREW TO DIVERT TO CLT WHSDR AWXA200501172Battery · inoperativePHX - EEL - CREW REPORTED "FWD F/A EMERGENCY FLASHLIGHT INOP". MAINTENANCE REMOVED AND REPLACED THE FORWARD F/A EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECKS GOOD.SDR SWAA053008Skin · crackedDURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19L. REPAIRED SKIN PER SWA EA AND SRM.SDR SB05123Battery Pack · dischargedPHL - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT ABOVE THE L2 DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK PER MM 33-51-51. OPERATIONAL CHECK GOOD.SDR AWXA200501105Circuit Breaker · damagedCREW REPORTED "ON CLIMB OUT LEFT GENERATOR CAME OFF LINE FOLLOWED BY RIGHT GENERATOR. AC POWER LOST MOMENTARY. CYCLED BOTH GENERATORS. BOTH CAME BACK ON." CREW ELECTED TO RETURN TO PHX. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE COULD NOT DUPLICATE DISSDR SB05115Indicator · faultyDFW FLT1262 - DURING FINAL APPROACH TO DFW, CREW SELECTED FLAPS FROM 15 TO 25 UNITS AND NOTICED A DEVELOPING SPLIT IN THE LEFT AND RIGHT FLAP POINTERS. AT 25 UNITS, THERE WAS A NOTICEABLE SPLIT BUT NO APPARENT AIRCRAFT ROLL. CREW EXECUTED A GO-AROUND AND LANSDR USAA200509002Skin · cracked2 INCH CRACK EXTENDING FROM UNDER A PREVIOUS REPAIR AT STA 727E - 747 STRINGER 23L. REMOVED REPAIR DOUBLER, FABRICATED NEW DOUBLER AND FILLERS AND INSTALLED REPAIR PER SRM 53-00-01 FIG 201.SDR SB05112Outflow Valve · leakingAIRCRAFT WOULD NOT MAINTAIN CABIN PRESSURIZATION. AT FL030, CABIN ALTITUDE CLIMBED 1,200 FEET PER MINUTE WITH OUTFLOW VALVE FULLY CLOSED. CREW DESCENDED BELOW FL020 BEFORE CABIN ALTITUDE WOULD DESCEND BELOW 8,000 FEET. FLIGHT CONTINUED. MX PRESSURIZED AIRCSDR USAA200509001Skin · cracked1-7/8 INCH CRACK AT BS 727D AND STRINGER 3L. REMOVED DAMAGED SKIN AND REPAIRED PER SRM 53-00-01.SDR SB05109Indicator · faultyORD - FLT551 - ON APPROACH TO ORD, CREW EXTENDED FLAPS FROM 5 TO 10 UNITS AND A SPLIT FLAP INDICATION OF L-5 AND R-10 WAS DISPLAYED. FLAPS LOCKED OUT. CREW ACCOMPLISHED A GO-AROUND AND ON SUBSEQUENT APPROACH, FLAPS OPERATED NORMAL. FLIGHT LANDED WITHOUT FURTSDR SB05108Pump · leakingPHL - FLT803 - ON CLIMB-OUT FROM PHL, CREW REPORTED THE NR 1 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED ON GEAR RETRACTION. SYSTEM "A" HYDRAULIC QUANTITY DROPPED TO LESS THAN ONE-QUARTER. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER ISDR USAA200508005Fitting · chafedFOUND 3/8" BY .045" CIRCULAR WEAR AT OUTBOARD HINGE BRACKET FOR NR 5 SPOILER BOARD, WBL 169.25R. DEFECTIVE PART REPLACED WITH IDENTICAL PART.SDR SB05103Light · inoperativeCLT - MAINTENANCE REPORTED THE CABIN SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 13 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD.SDR SB05102Connector · disconnectedCLT - MAINTENANCE REPORTED THE CABIN MOUNTED EMERGENCY LIGHTS FROM SEAT ROWS 12 THRU 16 WERE INOPERATIVE. MAINTENANCE SECURED A CONNECTOR BENEATH SEAT ROW 12. OPERATIONAL CHECK GOOD.SDR USAA051041Bushing · corrodedVERTICAL FIN AFT JUGS RT BUSINGS AFT FACES CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED BUSHINGS IAW BOEING DWG 69-72039, 65-55274, DEFECT SIZE: 1 X 2 INCH TYPICAL.SDR USAA051046Threshold · crackedAFT CARGO DOOR MOST FWD THRESHOLD HAS CRACK. WELDED CRACK IAW BOEING PROCESS SPEC BAC 5975, DEFECT SIZE: .75 INCH.SDR USAA051045Strip · wornAFT CARGO CAP STRIP BETWEEN SCUFF PLATE AND ACF-3 DAMAGED. REMOVED DAMAGED STRIP, FABRICATED & INSTALLED NEW STRIP IAW BOEING DWG 65-49613 DEFECT SIZE: 3 X 2 INCH WORN AREA.SDR USAA051044Fitting · corrodedO/B ATTACH HOLE IN RT AFT DRAG BRACE ATTACH FITTING OFR VERTICAL FIN CORRODED. REMOVED CORROSION, FABRICATED BUSHING AND INSTALLED IAW EA 96816, DEFECT SIZE: 1 X 2 INCH TYPICAL.SDR USAA051042Bushing · corrodedVERTICAL FIN, AFT MOUNT LUGS LT SIDE BUSHINGS, FWD FACE CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED BUSHINGS IAW BOEING DWGS 69-72039 & 65-52274 DEFECT SIZE: 1 X 2 INCH AREA.
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