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 AWXA200300121Tie Clip · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 1/4" CRACK WAS FOUND ON STRINGER TIE CLIP AT STR 2 R/H, BS 639. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT STR 2 R/H, BS 639; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM SDR AWXA200300120Tie Clip · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 5/16" CRACK WAS FOUND ON STRINGER TIE CLIP AT STR 2 L/H, BS 639. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT STR 2 L/H, BS 639; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRMSDR AWXA200300119Tie Clip · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 1/4" CRACK WAS FOUND ON STRINGER TIE CLIP AT STR 4 L/H, BS 639. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT STR 4 L/H, BS 639; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP; INSTALLED REPAIR PART IAW B737-300 SRM SDR AWXA200300124Web · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK , A BULKHEAD WEB WAS FOUND CRACKED AT B.S. 178. CRACK WAS CONFIRMED WITH HFEC. MAINTENANCE REMOVED DAMAGED AREA OF BULKHEAD WEB BS 178; FABRICATED A REPAIR DOUBLER, FILLER, AND 3 EACH SHIMS; AND INSTALLED REPAIR PARTS IAWSDR AWXA200300200Skin · crackedMCN - MAJOR REPAIR - DURING C-16 CHECK A 3/16" CRACK WAS FOUND ON THE UPPER EDGE OF EXTERNAL SKIN AT UPPER HINGE CUTOUT OF L-1 DOOR, BS 318, STR 10 L/H; CONFIRMED BY HFEC INSPECTION. MAINTENANCE CUTOUT CRACK ON UPPER EDGE OF EXTERNAL SKIN AT UPPER HINGE CUTOUTSDR AWXA200300052Module · arcedLAS - DIV - FLT771 FROM PHX TO SMF A BLUE ARCING EMMENATED BRIEFLY FROM BEHIND THE OVERHEAD PANEL WITH AN AUDIBLE POP AND BRIEF FLICKER OF THE FORWARD PANEL BACKGROUND LIGHTING, ADDITIONALLY A BRIEF ODOR OF OZONE WAS NOTED. MAINTENANCE REMOVED AND REPLACEDSDR AWXA200300005Floorbeam · crackedDURING C-16 CHECK, A .5000 INCH CRACK WAS FOUND ON LOWER FLOORBEAM TIE STRAP AT BS 340, STR 45 LT, JUST ABOVE AIR STAIR RAIL OUTBOARD END. MAINTENANCE STOP DRILLED END CRACK ON LOWER FLOORBEAM TIE STRAP AT BS 340; FABRICATED A REPAIR PLATE; REMOVED VERTICAL STSDR AWXA200300004Floorbeam · crackedDURING C-16 CHECK, A .5000 INCH CRACK WAS FOUND ON LOWER FLOORBEAM TIE STRAP AT BS 340 JUST ABOVE AIR STAIR RAIL RBL 24.75. MAINTENANCE STOP DRILLED HOLE ON LOWER FLOORBEAM TIE STRAP AT BS 340; FABRICATED A REPAIR PLATE; AND INSTALLED REPAIR PART IAW SRM.SDR AWXA200201245Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 R/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 663, STR 10 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPASDR AWXA200201244Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 2 R/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 616, STR 2 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIRSDR AWXA200201243Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 1. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 616, STR 1; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIR PART IASDR AWXA200201242Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 1" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 616, STR 2 L/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 616, STR 2 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED REPAIRSDR AWXA200201241Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 3/8" CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 663, STR 10 L/H. MAINTENANCE REMOVED THE DAMAGED STRINGER TIE CLIP AT BS 663, STR 10 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-41437; AND INSTALLED RESDR AWXA200300002Skin · crackedDURING C-16 CHECK, CORROSION AND 3 EACH .2500 INCH CRACKS WERE FOUND ON LOWER EXTERIOR FUSELAGE SKIN (LT AND RT KEELBEAM) AT BS 727+5 - BS 727+10, STR 27 LT - STR 27 RT. MAINTENANCE CUT SKIN FOR ACCESS TO KEEL BEAM; TRIMMED OUT DAMAGED AREAS OF OUTBOARD LOWERSDR AWXA200201257Skin · crackedYVR - MAJOR REPAIR - DURING C-16 CHECK A 1/2" CRACK WAS FOUND ON FUSELAGE SKIN AT THE UPPER HINGE CUTOUT OF THE L-2 DOOR, BS 951, STR 10 L/H. MAINTENANCE CUTOUT CRACKED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIRSDR AWXA200201249Slat · delaminatedYVR - MAJOR REPAIR - DURING C-16 CHECK THE #5 SLAT WAS FOUND DELAMINATED AT THE OUTBOARD UPPER TRAILING EDGE SURFACE. MAINTENANCE REMOVED THE #5 SLAT AND REPAIRED DAMAGE IAW B737-300 SRM 51-70-10 REPAIR 22 & 23. REINSTALLED #5 SLAT IAW BMM 27-81-21, PG. 401-41SDR AWXA200201258Control Cable · brokenDURING C-16 CHECK, FLAP FOLLOW UP CABLES WFFA, WFFB WERE FOUND TO HAVE LOW TENSION IAW TABLE 4, W/C 12B27001. WHILE APPLYING TENSION TO CABLES, CABLE WFFA BROKE .1250 INCH INSIDE THE TERMINAL DUE TO NUMEROUS BROKEN WIRE STRANDS. MAINTENANCE REMOVED AND REPLACSDR AWXA200201250Slat · delaminatedYVR - MAJOR REPAIR - DURING C-16 CHECK THE #4 SLAT WAS FOUND DELAMINATED AT THE INBOARD UPPER TRAILING EDGE SURFACE. MAINTENANCE REMOVED THE #4 SLAT AND REPAIRED DAMAGE IAW B737-300 SRM 51-70-10 REPAIR 22 & 23. REINSTALLED #4 SLAT IAW BMM 27-81-21, PG. 401-419SDR AWXA200200997Fan · burned outFLT 0625 - ON TAXI OUT AT PHX THE COCKPIT FILLED WITH A STRONG ELECTRICAL BURNING ODOR, TURNED OFF AIR CONDITIONING PACKS, RECIRCULATION FAN, ENGINE GENERATORS, AND BURNING ODOR DISSIPATED. AIRCRAFT RETURNED TO GATE. MAINTENANCE DISCOVERED THE RECIRCULATION FASDR AWXA200200972Gcu · failedFLT 0769 - ON FINAL APPROACH AT PHX EN ROUTE FROM PVR THE NR 1 GENERATOR TRIPPED OFF AND THE FLIGHT CREW NOTICED AN ELECTRICAL BURNING SMELL. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE NR 1 GENREATOR CONTROL UNIT (GCU) INOPERATISDR AWXA200200911Battery · dischargedPHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THAT A EMERGENCY FLASHLIGHT WAS INOPERATIVE IN THE CABIN. MAINTENANCE REPLACED THE BATTERY IN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200794Structure · brokenUNCOMMANDED FLT INPUT - ON APPROACH AFTER FLAPS SELECTED TO 30 DEG ACFT ROLLED HARD LT, REQUIRED ALMOST FULL RT AILERON TO KEEP STRAIGHT & LEVEL. SELECTED FLAPS TO 40 DEG & PROBLEM REMAINED, LANDED UNEVENTFULLY. MX PERFORMED VISUAL INSPECTION OF WINGS AND FSDR AWXA200200759Light · inoperativePHX - EEL - FLIGHT ATTENDANT REPORTED THAT EMERGENCY EXIT LIGHT IN FIRST CLASS WAS INOPERATIVE. REPLACED BULLNOSE LIGHT ASSEMBLY PER BMM 33-51-21-201, OPERATIONAL CHECK GOOD.SDR AWXA200200523Pump · leakingPHX - AIR TURN BACK - FLT 0320 - ON DEPARTURE FROM PHX EN ROUTE FOR ACA THE HYDRAULIC PUMP B-ENGINE NR 2 LIGHT ILLUMINATED. B-SYSTEM HYDRAULIC QUANTITY DROPPED TO APPROXIMATELY 3/8 FULL, PRESSURE WAS GOOD. MAINTENANCE FOUND NR 2 ENGINE DRIVEN HYDRAULIC PUMP SDR AWXA200200522Fitting · stuckPHX- AIR TURNBACK- FLT 0663- ON DEPARTURE OUT OF PHOENIX EN ROUTE TO SNA, THE REPORT BY THE PILOT STATED THAT A LOSS OF -B- SYSTEM HYDRAULICS HAD OCCURRED AND THAT THE AIRCRAFT WAS RETURNING TO PHOENIX. MAINTENANCE INSPECTED THE HYDRAULIC SYSTEM AND FOUND THESDR AWXA200200430Ballast · inoperativePHX - EEL - FLIGHT CREW REPORTED STANDBY POWER EMERGENCY INSTRUMENT PANEL FLOOD LIGHTS ARE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE M1181 BALLAST, OPERATIONAL CHECK WAS GOOD.SDR AWXA200200239Keelbeam · corrodedMCN - MAJOR REPAIR - C - DURING C-17 CHECK CORROSION WAS FOUND ON LOWER CHORD FROM BS 520 TO BS 525.5, WL 148.4, LBL 6.5.SDR AWXA200200237Keelbeam · corrodedMCN - MAJOR REPAIR -C- DURING C-17 CHECK CORROSION WAS FOUND ON KEEL BEAM CHORD AT BS 500 TO BS 520, LBL 6.5, WL 148.4.SDR AWXA200200211Connector · incorrectYVR - EEL - "C" - DURING C-15 CHECK SEAT ROW 14 L/H WAS FOUND TO HAVE THE WRONG MATING CONNECTORS AT THE EMERGENCY LIGHTING HARNESS JUNCTIONS. MAINTENANCE REMOVED AND REPLACED MATING CONNECTORS FOR EMERGENCY LIGHTING HARNESS AT SEAT ROW 14 L/H. FUNCTIONAL CHECSDR AWXA200200230Door Frame · crackedMCN - MAJOR REPAIR - C - DURING C-17 CHECK A .125 INCH CRACK WAS FOUND ON THE VERTICAL LEG OF THE FORWARD CARGO DOOR LOWER TEE CHORD IN THE THIRD FASTENER HOLE FROM AFT END OF BEAM BS 487.SDR AWXA200200227Frame · crackedMCN - MAJOR REPAIR - C - DURING C-17 CHECK A 1.2 INCH CRACK WAS FOUND IN FRAME BS 616 LT WL 200 AT THE FIRST FASTENER ABOVE CENTER WING.SDR AWXA200200226Panel · buckledMCN - MAJOR REPAIR - "C" - DURING C-17 CHECK CENTER KEEL PANEL RIVETS WORKING ALONG ALL 4 SIDES, AND CENTER OF PANEL APPEARS TO BE WAVY. MAINTENANCE REMOVED CENTER KEEL PANEL, LEVELED AIRCRAFT, FABRICATED NEW CENTER KEEL PANEL, AND INSTALLED REPAIR IAW AWA ER SDR AWXA200200205Intercostal · crackedYVR - MAJOR REPAIR - C - DURING C-15 CHECK A CRACK WAS FOUND ON THE FWD CARGO DOOR LOWER AREA MID INTERCOSTAL AT BEND RADIUS.SDR AWXA200200177Wire · chafedYVR - EEL - "C" - DURING C-15 CHECK EMERGENCY ESCAPE PATH LIGHTING MAIN WIRE HARNESS WAS FOUND DAMAGED AT SEVERAL PLACES. MAINTENANCE REPAIRED DAMAGED WIRING WITH ENVIRONMENTAL SPLICES IAW SWPM 20-30-12, PG 12, ITEM 6,B. FUNCTIONAL TEST OF ESCAPE PATH LIGHT TOSDR AWXA200200204Beam · gougedYVR - MAJOR REPAIR - C - DURING C-15 CHECK THE RT MAIN LANDING GEAR ACTUATOR WALKING BEAM ATTACH BOLT WAS FOUND INSTALLED BACKWARDS AND GOUGING INTO MAIN LANDING GEAR SUPPORT BEAM.SDR AWXA200200203Crease Beam · crackedYVR - MAJOR REPAIR - C - DURING C-15 CHECK A CRACK WAS FOUND ON CREASE BEAM ASSEMBLY INNER CHORD FRAME ATTACHMENT AT BS 616.SDR AWXA200200202Floorbeam · damagedYVR - MAJOR REPAIR - C - DURING C-15 CHECK DAMAGE WAS FOUND TO CLIP NUTS AT FLOORBEAM SCREW HOLES BS 540 TO BS 727, RLB 24, LBL 24. MAINTENANCE FOUND 5 HOLES BEYOND SERVICEABLE LIMITS.SDR AWXA200200201Frame · crackedYVR - MAJOR REPAIR - C - DURING C-15 CHECK A CRACK WAS FOUND ON RT FUSELAGE FRAME INNER CHORD AT BS 616, STR 17 RT.SDR AWXA200200200Frame · crackedYVR - MAJOR REPAIR - C - DURING C-15 CHECK THE LT FUSELAGE FRAME INNER CHORD WAS FOUND CRACKED AT BS 616 JUST BELOW STR 17 LT.SDR AWXA200200199Floorbeam · crackedYVR - MAJOR REPAIR - C - DURING C-15 CHECK OVERWING FLOORBEAM WAS FOUND CRACKED IN TWO PLACES AT BS 663.SDR AWXA200200176Frame · crackedMCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A CRACK WAS FOUND ON FWD UPPER CORNER OF AFT CARGO DOOR UNDER PULLY BRACKET AT BS 795.5. MAINTENANCE REMOVED & REPLACED FWD UPPER CORNER FRAME OF AFT CARGO DOOR IAW 737-300 SRM 51-40-02, PG. 38, 51-40-5, PG. 1-2, 51SDR AWXA200200154Frame · crackedMCN - MAJOR REPAIR - C - DURING C-10 CHECK A 1.375 INCH CRACK WAS FOUND ON FRAME SUPPORT AT BS 616, WL 202, RBL 65. MAINTENANCE CUTOUT DAMAGED AREA OF CHORD AT BS 616, FABRICATED A STIFFENING ANGLE AND REPAIR FILLER, AND INSTALLED REPAIR PARTS IAW AWA ER 03-5SDR AWXA200200175Skin · gougedMCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A GOUGE WAS FOUND ON THE LOWER LEADING EDGE OF THE L/H ELEVATOR JUST INBOARD OF THE #6 HINGE. MAINTENANCE REMOVED DAMAGE AREA AND APPLIED HONEYCOMB REPAIR PLY AT ELEVATOR STA 210.5 IAW B737-300 SRM 51-70-17, AND AWASDR AWXA200200113Hydraulic Line · leakingLAS - DIVERSION - FLT 0221 - C - EN ROUTE FROM SMF TO PHX DURING CLIMB THE A-SYSTEM HYDRAULIC PRESSURE CYCLED AND WENT TO ZERO ACCOMPANIED BY A FLIGHT CONTROL AND A-SYSTEM PRESSURE LIGHT. AIRCRAFT DIVERTED TO LAS WITHOUT FURTHER INCIDENT. IN LAS MAINTENANCE SDR AWXA200200174Frame · crackedMCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A CRACK WAS FOUND ON FWD LOWER CORNER OF AFT CARGO DOOR BS 795.5. MAINTENANCE REMOVED & REPLACED FWD LOWER CORNER FRAME OF AFT CARGO DOOR IAW 737-300 SRM 51-40-02, PG. 38, 51-10-02, PG. 15-16, 51-40-02, PG. 3, AND BSDR AWXA200200112Engine · malfunctionedONT - DIVERSION - FLT 809 - EN ROUTE FROM PHX TO SFO AND AT CRUISING ALTITUDE A NR 2 ENGINE ROLLBACK OCCURRED. THE FLIGHT CREW DECLARED AN EMERGENCY AND THE AIRCRAFT DIVERTED TO ONT. AT FL 200 THE NR 2 ENGINE WAS RESTARTED AND OPERATED NORMALLY FROM THIS TIMSDR AWXA200200159Skin · crackedMCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A 1/4 CRACK WAS FOUND ON EXTERNAL SKIN OF R1 DOOR AT THE UPPER CORNER OF THE LOWER HINGE CUTOUT 307.25. MAINTENANCE CUTOUT THE DAMAGED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED. SDR AWXA200200155Skin · crackedMCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A 1/8" CRACK WAS FOUND AT THE R1 DOOR EXTERNAL SKIN UPPER HINGE CUTOUT LOWER CORNER BS 307.25. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN, FABRICATED A REPAIR DOUBLER AND HINGE COVER, AND INSTALLED REPAIR PARTS IAW AWASDR AWXA200200148Skin · dentedMCN - MAJOR REPAIR - "C" - DURING C-10 CHECK THE L1 DOOR FORWARD LOWER CORNER SKIN WAS FOUND DENTED BS 312, HFEC VERFIED NO CRACKS. MAINTENANCE CUTOUT DAMAGED AREA OF SKIN, FARICATED A REPAIR DOUBLER AND FILLER, AND INSTALLED REPAIRS IAW B737-300 SRM 52-00-01,SDR AWXA200200147Skin · crackedMCN - MAJOR REPAIR - "C" - DURING C-10 CHECK A 5/16" CRACK WAS FOUND ON FUSELAGE SKIN AT UPPER R2 DOOR HINGE CUTOUT BS 952, HFEC INSPECTION AND 10X VISUAL CONFIRMED THE CRACK. MAINTENANCE CUTOUT DAMAGED AREA AND PERFORM HFEC INSPECTION TO VERIFY CRACK WAS CONT
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