Boeing 737-3S3
Service difficulty reports · 1,209
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 = '7373S3' 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 = '7373S3' 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 AWXA200400181Tire · fodTIRE DEBRIS & MLG DOOR ON RUNWAY, NO ABNORMAL FLT CHARACT/INDICATIONS. LOWERED MLG & FLEW BY TOWER, EMER LANDING DECLARED. LANDED W/O INCID. MAINT FOUND NR 4 TIRE SHREDDED, RT MLG INNER DOOR MISSING. DAMAGED RT MLG CENTER DOOR, RT INBD T/E FORE FLAP AT MID SPSDR AWXA200400173Wire Harness · brokenPHX - EEL - DURING A-01 CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 1 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 1 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301565Trim Motor · bindingON C/O, CAPTAINS EFIS IND SPEED TRIM WARNING LIGHT. A/C COULD NOT ATTAIN FL 290 IN MODE CONTROL PANEL, A/C DESCENDED & AIRSPEED DECREASED AS STAB OUT OF TRIM LIGHT ILLUM. TURNED OFF AUTOPILOT, STAB WOULD NOT TRIM IN ELECTRIC OR MANUAL MODE. LOWER ALTITUDE & SPSDR AWXA200301525Line · chafedLAS - FUEL LEAK - DURING B-3 CHECK FUEL WAS FOUND DRIPPING FROM RT ENGINE PYLON AFT DRAIN LINE, UPON FURTHER INVESTIGATION A FUEL LEAK WAS FOUND ON RT ENGINE FUEL FEED LINE AT 90 DEGREE ELBOW APPROXIMATELY 2 INCHES FROM ADEL CLAMP UNDER THE HOT AIR BLEED DUCT SDR AWXA200301125Wire · brokenDFW - EEL - DURING INSPECTION DISCOVERED A BAD CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 9 LT. ISSUED MEL 33-19, COND. 1 (FLOOR PROXIMITY LIGHT INOP). WHEN AIRCRAFT RETURNED TO PHX MAINTENANCE RE-TERMINATED CONNECTOR AT SEAT ROW 9 LT, OPERATIONASDR AWXA200301055Control Panel · failedDURING CRUISE EN ROUTE FROM PHX TO MSY AT 33000 FT AUTOPILOT DISCONNECTED DUE TO MODE CONTROL PANEL (MCP) FAILURE, FLIGHT DIRECTORS AND AUTOPILOT INOPERATIVE. ONLY WINDOW WORKING ON MCP WAS THE FIRST OFFICERS COARSE SELECTOR, FLIGHT INSTRUMENTS AND RADIO MAGNESDR AWXA200301003Flashlight · inoperativeFLIGHT CREW REPORTED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300870Duct · leakingAPPROX 3 MIN AFTER DEPARTURE THE RT WING TO BODY OVERHEAT LIGHT ILLUMINATED. FOLLOWED QRH PROCEDURES AND LIGHT EXTINGUISHED APPROX 2 MIN LATER. DURING TAXI & TAKEOFF PACK WAS IN AUTO POSITION, AND AFTER TAKEOFF POSITIONED PACK TO HIGH WITH OVERHEAT CONDITIONSDR AWXA200300815Stringer · crackedPHX - MAJOR REPAIR - DURING INSPECTION A CRACK WAS FOUND ON STRINGER 23 LT AT BS 727E. MAINTENANCE REMOVED EXISTING DOUBLER AND REMOVED DAMAGED SECTION OF STRINGER 23 LT AT BS 727E; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOSDR AWXA2003007AAIndicator · false indicationON DECENT INTO BUR EN ROUTE FROM PHX TRAILING EDGE FLAPS LOCKED OUT BETWEEN 1 AND 2 DEGREES. RUNWAY TO SHORT AT BUR, DIVERTED TO LAX WITH LONGER RUNWAY. MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE FLAP POSITION INDICATOR, OPERATIONAL CHECK WAS GOOD IAW SDR AWXA200300773Indicator · false indicationON DESCENT INTO BUR EN ROUTE FROM PHX TRAILING EDGE FLAPS LOCKED OUT BETWEEN 1 AND 2 DEGREES. RUNWAY TO SHORT AT BUR, DIVERTED TO LAX WITH LONGER RUNWAY. MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE FLAP POSITION INDICATOR, OPERATIONAL CHECK WAS GOOD ISDR AWXA200300713Battery · dischargedEMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300518Valve · openSTL - DIVERSION - FLT 0126 - EN ROUTE FROM PHX TO MKE, NR 2 ENGINE COWL ANTI-ICE VALVE FAILED TO OPEN, DUE TO ICING CONDITIONS DIVERTED TO STL. MAINTENANCE AT STL COMPLIED WITH MEL PROCEDURE 30-3, COND 4, OPENING OF THE NR 2 ENGINE COWL ANTI-ICE VALVE. WHEN SDR AWXA200300392Line · brokenPHX - ABORTED TAKEOFF - FLT 0126 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR MKE AT 110 KTS THE NR 2 ENGINE LOST POWER, ABORTED TAKEOFF. AFTER TAXIING OFF RUNWAY THE NR 2 ENGINE EGT STAYED AT 750. MOVED NR 2 THROTTLE THROUGH FULL RANGE OF MOTION, HAD NO EFFECT ON SDR AWXA200300359Shutoff Valve · inoperativeMCI - ABORTED TAKEOFF - FLT 702 - PREPARING FOR TAKEOFF AT MCI EN ROUTE FOR PHX LT BLEED PRESSURE INDICATED ZERO, TAXIED OFF RUNWAY AND RETURNED TO GATE. MAINTENANCE ISSUED MEL 36-5, COND 2, NR 1 ENG BLEED AIR SHUTOFF VALVE INOP. WHEN AIRCRAFT RETURNED TO PHSDR AWXA200300352Actuator · wornYVR - FLIGHT CONTROL - DURING C-16 CHECK THE HORIZONTAL STABILIZER MANUAL TRIM WAS FOUND TO HAVE 3/4 TURN SLACK IN EITHER UP OR DOWN DIRECTION. MAINTENANCE FOUND LT AND RT STAB HINGE FITTINGS FRETTING AROUND BEARINGS; REMOVED AND REPLACED LT AND RT HINGE FITTSDR AWXA200300364Channel · crackedLCQ - EES - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND ON CABIN FLOOR SUPPORT CHANNEL AT BS 520, LBL 4. MAINTENANCE REMOVED DAMAGED FLOOR SUPPORT CHANNEL BS 520, LBL 4 - 21; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT CHANNEL; INSTALLED REPAIR PART IAW B737-SDR AWXA200300363Fitting · corrodedLCQ - EES - DURING C-18 CHECK CORROSION WAS FOUND ON THE L-1 DOOR AFT GIRT BAR ATTACH FITTING BS 344. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR AFT GIRT BAR LOCK AND ATTACH FITTINGS. PART NAME; LOCK, MFG; BOEING, P/N; 65-65972-3.SDR AWXA200300332Intercostal · crackedDURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON FORWARD OUTBOARD CORNER OF INTERCOSTAL, JUST FORWARD OF L-1 DOOR AT BS 294 TO BS 303, STR 7 LT. MAINTENANCE REMOVED DAMAGED INTERCOSTAL AT BS 294 TO BS 303, STR 7 L/H; FABRICATED A NEW REPLACEMENT INTERCOSTAL PESDR AWXA200300361Skin · chafedLCQ - MAJOR REPAIR - DURING C-18 CHECK A LEADING EDGE REPAIR AT THE INBOARD END OF THE LT OUTBOARD MID FLAP WAS FOUND CHAFED. MAINTENANCE REMOVED EXISTING REPAIR AT THE INBOARD END OF THE LT OUTBOARD MID FLAP; FABRICATED A DOUBLER AND FILLER; INSTALLED REPAIRSDR AWXA200300321Intercostal · crackedDURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON FORWARD END OF INTERCOSTAL BETWEEN FLOORBEAMS AT BS 328 AND BS 344, LBL 46. MAINTENANCE REMOVED DAMAGED INTERCOSTAL BETWEEN FLOORBEAMS AT BS 328 AND BS 344, LBL 46; FABRICATED A NEW REPLACEMENT INTERCOSTAL; INSTALLSDR AWXA200300320Frame · crackedDURING C-16 CHECK A 1/2 INCH CRACK WAS FOUND ON LT SIDE FRAME OF 178 BULKHEAD, WL 195. MAINTENANCE REMOVED DAMAGED SIDE FRAME, 178 BULKHEAD, WL 195; FABRICATED A NEW REPLACEMENT SIDE FRAME PER DWG 65-16300; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PG.SDR AWXA200300322Angle · corrodedDURING C-16 CHECK CORROSION WAS FOUND ON ANGLE AT FIRST OFFICERS SIDE STATION 219, BELOW THE RT NR 2 SLIDING WINDOW. MAINTENANCE REMOVED CORRODED ANGLE AT FIRST OFFICERS SIDE STATION 219, BELOW THE RT NR 2 SLIDING WINDOW; FABRICATED A NEW REPLACEMENT ANGLE PERSDR AWXA200300345Frame · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A .5000 INCH CRACK WAS FOUND ON LT AND RT SIDE FRAMES, BS 178 BULKHEAD, WL 207. MAINTENANCE CUTOUT DAMAGED SECTION OF RT SIDE FRAMES, BS 178, WL 207; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATSDR AWXA200300350Skin · delaminatedDURING C-16 CHECK THE NR 3 LEADING EDGE SLAT UPPER SURFACE WAS FOUND DELAMINATED AT THE INBOARD CORNER. MAINTENANCE REMOVED THE NR 3 LEADING EDGE SLAT; PERFORMED COMPOSITE REPAIR OF THE INBOARD CORNER PER B737-300 SRM 51-70-10, FIG. 32, REPAIR 23; INSTALLED SDR AWXA200300335Bulkhead · crackedMAJOR REPAIR - DURING C-16 CHECK 5 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT WL 218 LBL 12, WL 212 LBL 5.7, WL 198 LBL 5.0, WL 198 LBL 62, AND WL 201 LBL 6.2. MAINTENANCE PERFORMED NDT INSPECTION ON BS 178 BULKHEAD WEB AT WL 218 LBL 12, WL 212 LBL 5.7, SDR AWXA200300268Battery · dischargedUPON ARRIVAL AT AIRCRAFT THE FLIGHT CREW FOUND THE EMERGENCY LIGHTS ON. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY PACKS, EMERGENCY LIGHT TEST WAS GOOD.SDR AWXA200300351Skin · delaminatedDURING C-16 CHECK SEVERAL AREAS OF THE LT OUTBOARD FOREFLAP UPPER SURFACE WERE FOUND DELAMINATED AT THE INBOARD END. MAINTENANCE REMOVED AND REPLACED THE LT OUTBOARD FOREFLAP IAW BMM 27-51-37, PG. 401-407.SDR AWXA200300349Skin · delaminatedDURING C-16 CHECK THE NR 5 LEADING EDGE SLAT UPPER SURFACE WAS FOUND DELAMINATED AT THE CENTER, INBOARD & OUTBOARD CORNERS. MAINTENANCE REMOVED THE NR 5 LEADING EDGE SLAT; PERFORMED COMPOSITE REPAIR OF THE CENTER, INBOARD & OUTBOARD CORNERS PER B737-300 SRM 51SDR AWXA200300347Structure · delaminatedYVR - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE OUTBOARD TRAILING EDGE OF THE NR 2 SLAT WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED NR 2 SLAT IAW BMM 27-81-21, PG. 401-419.SDR AWXA200300346Structure · delaminatedYVR - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE, INBOARD CORNER OF THE NR 4 SLAT WAS FOUND DELAMINATED. MAINTENANCE REMOVED NR 4 SLAT, REPAIRED DAMAGE IAW SRM 51-70-10, FIG. 32, PG. 88I, RE-INSTALLED SLAT AND RIGGED SYSTEM IAW BMM 27-81-21, PG. 414-41SDR AWXA200300238Cover · brokenDURING CLIMB OUT FROM IND EN ROUTE FOR PHX A LOUD SQUEAL DEVELOPED FROM THE FORWARD SIDE OF THE L-1 DOOR, DIVERTED TO CMH FOR REPAIR. MAINTENANCE FOUND THE L-1 DOOR LOWER HINGE COVER PINCHED AROUND DOOR SEAL. REMOVED HINGE COVER, PLACED ON CDL 52-10-1, COND. SDR AWXA200300232Warning System · false activationDURING CLIMB OUT, APU FIRE LIGHT ILLUMINATED, FOLLOWED QUICK REFERENCE HANDBOOK & DISCHARGED APU FIRE EXTINGUISHER BOTTLE. TURNED BACK & LANDED WITHOUT EVENT. MAINTENANCE INSPECTED APU AREA AND FOUND NO DAMAGE, PLACED APU ON MEL 49-1, COND. 1 "APU INOP". WHEN SDR AWXA200300261Battery · dischargedDURING C-11 CHECK THE FORWARD OUTBOARD EMERGENCY FLASHLIGHT LED INDICATOR DID NOT FLASH. MAINTENANCE REMOVED AND REPLACED THE FORWARD OUTBOARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300207Controller · failedON CLIMB OUT FROM MKE EN ROUTE FOR PHX, STANDBY PRESSURIZATION FAILED AT 35,000 FT, TURNED BACK AND LANDED AT MKE WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER IAW BMM 21-31-21, AND CABIN PRESSURE CONTROL PANEL IAW BMM 2SDR AWXA200300241Keelbeam · corrodedDURING C-11 CHECK CORROSION WAS FOUND ON RT KEELBEAM AT BS 540. MAINTENANCE TRIMMED OUT DAMAGED SECTION OF RT KEELBEAM AT BS 500C+9 TO BS 541; FABRICATED A NEW SEGMENT OF KEELBEAM, 2 EACH ANGLES, AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 03-5330-SDR AWXA200300240Frame · crackedDURING C-11 CHECK A 1 INCH CRACK WAS FOUND IN RADIUS OF RT OUTER CHORD OF 178 BULKHEAD AT WL 207. MAINTENANCE CUTOUT DAMAGED SECTION OF RT OUTER FRAME, BULKHEAD 178, WL 207; FABRICATED A NEW SECTION OF FRAME AND SPLICE ANGLES PER SB 737-53A1173, FIG. 61; INSTASDR AWXA200300211Crease Beam · corrodedDURING C-11 CHECK EXFOLIATION CORROSION WAS FOUND ON CREASE BEAM WEB AT BS 727E+10, STR 17 LT. MAINTENANCE REMOVED CORRODED CREASE BEAM WEB BS 727E+10, STR 17 LT; FABRICATED A NEW REPLACEMENT CREASE BEAM WEB PER DWG 65-46822-5; INSTALLED REPAIR PART IAW B737-3SDR AWXA200300199Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-11 CHECK A 3/8" CRACK WAS FOUND UNDER RIVET HEAD ON STRINGER TIE CLIP BS 727D, STR 6 L/H. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT BS 727D, STR 6 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART ISDR AWXA200300242Tab · wornDURING C-11 CHECK THE LT AILERON BALANCE TAB INBOARD AND OUTBOARD HINGES WERE FOUND TO HAVE EXCESSIVE PLAY. MAINTENANCE REMOVED AND REPLACED THE LT AILERON BALANCE TAB IAW T/C R3M27014, AND REPLACED THE INBOARD AND OUTBOARD L/H AILERON BALANCE TAB HINGES IAW OSDR AWXA200300229Skin · crackedDURING C-11 CHECK A 2 INCH CRACK WAS FOUND ON L/H HORIZONTAL STABILIZER LOWER SKIN AT FORWARD OF INBOARD BALANCE PANEL, APPROXIMATELY 1 1/2 INCHES FORWARD OF REAR SPAR. MAINTENANCE STOP DRILLED CRACK ON LT HORIZONTAL STABILIZER LOWER SKIN AT FORWARD OF INBOARDSDR AWXA200300221Slat · crackedYVR - MAJOR REPAIR - DURING C-11 CHECK 3 EACH 1" CRACKS WERE FOUND ALONG RIVETS ON LOWER EDGE OF THE NO. 6 LEADING EDGE SLAT AT THE INBOARD AUXILIARY TRACK. MAINTENANCE REMOVED EXISTING EXTERNAL DOUBLER; CUTOUT FOUR DAMAGED FASTENER HOLES; FABRICATED A FILLER SDR AWXA200300203Stiffener · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STIFFENER AT R/H AIR CONDITIONING BAY AFT BULKHEAD JUST ABOVE THE TURBO FAN EXHAUST DUCT. MAINTENANCE REMOVED CRACKED STIFFENER AT R/H AIR CONDITIONING BAY AFT BULKHEAD JUST ABOVE THE TURBO FAN EXHSDR AWXA200300212Intercostal · crackedYVR - MAJOR REPAIR - DURING C-11 CHECK A 1/2" CRACK WAS FOUND ON LOWER WEB FLANGE (INTERCOSTAL) AT BS 360, BL 0. MAINTENANCE CUTOUT CRACKED AREA OF INTERCOSTAL AT BS 360, BL 0; FABRICATED A TAPERED SHIM AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW B737-300 SRMSDR AWXA200300222Beam · crackedDURING C-11 CHECK A 1 INCH CRACK WAS FOUND AT RT STRINGER 18A SHEAR BEAM WEB BS 727 ATTACHMENT. MAINTENANCE REMOVED DAMAGED SHEAR BEAM WEB AT BS 727 ATTACHMENT; FABRICATED A NEW REPLACEMENT SHEAR BEAM WEB PER DWG 65-46877; INSTALLED REPAIR PART IAW B737-300 SRSDR AWXA200300202Frame · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 1/4" CRACK WAS FOUND ON AFT SIDE OF THE AFT CABIN FRAME BS 907, BETWEEN STR 1 & 2 R/H. MAINTENANCE CUTOUT CRACKED AREA OF AFT CABIN FRAME BS 907; FABRICATED A REPAIR CHANNEL AND FILLER; INSTALLED REPAIR PARTS IAW B737-3SDR AWXA200300144Angle · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 1 INCH CRACK WAS FOUND ON THE LT FORWARD, OUTBOARD, WHEEL WELL CUTOUT MOUNTING ANGLE AT THE OUTBOARD END BS 663.75. MAINTENANCE REMOVED THE CRACKED LT FORWARD, OUTBOARD, WHEEL WELL CUTOUT MOUNTING ANGLE BS 663.75; FABRISDR AWXA200300201Tie Clip · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 3/8" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 639, STR 1 L/H. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 639, STR 1 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM SDR AWXA200300145Channel · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK EXFOLIATION CORROSION WAS FOUND ON OUTBOARD EDGE OF STRINGER 28 R/H AT BS 364, BELOW FLOW CONTROL VALVE. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS ON STRINGER END CLIP, STR 28 R/H, BS 364; REMOVESDR AWXA200300122Tie Clip · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 3/8" CRACK WAS FOUND ON STRINGER TIE CLIP AT STR 3 R/H, BS 639. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT STR 3 R/H, BS 639; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM
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