Boeing 737-33A
Service difficulty reports · 1,809
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 = '73733A' 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 = '73733A' 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 AWXA200401163Angle · corrodedDURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON HORIZONTAL WEB ATTACH ANGLE AT BS 294, RBL 55, WL 208. MAINTENANCE REMOVED CORRODED HORIZONTAL WEB ATTACH ANGLE AT BS 294, RBL 55; FABRICATED A NEW REPLACEMENT ANGLE IAW DWG 69-37402; INSTALLED REPAIR PARTSDR AWXA200401162Floor Support · corrodedDURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER CHORD OF FLOOR SUPPORT AT BS 298, RBL 31, WL 208. MAINTENANCE REMOVED FLOOR SUPPORT UPPER CHORD FROM BS 294 TO BS 312 AT RBL 31; FABRICATED A NEW REPLACEMENT SECTION OF CHORD IAW DWG 65-62175; INSTASDR AWXA200401155Floorbeam · corrodedDURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON BEAM AT BS 328, BETWEEN RBL 11 AND RBL 21, WL 208. MAINTENANCE CUTOUT DAMAGED SECTION OF TEE CAP BEAM AT BS 328, FROM RBL 11 TO RBL 21; FABRICATED 2 EACH REPAIR ANGLES AND A NEW REPLACEMENT SECTION OF CHSDR AWXA200401122Channel · crackedDURING C-18 CHECK A 1.0625 INCH CRACK WAS FOUND IN CHANNEL AT BS 540, BETWEEN BL (0) AND RBL 24. MAINTENANCE REMOVED CRACKED CHANNEL AT BS 540, FROM BL (0) TO RBL 24; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 65-52894; INSTALLED REPAIR PARTS IAW SRM 51-40-SDR AWXA200401121Channel · crackedDURING C-18 CHECK A .9375 INCH CRACK WAS FOUND IN CHANNEL AT BS 540, BETWEEN BL (0) AND LBL 24. MAINTENANCE REMOVED CRACKED CHANNEL AT BS 540, FROM BL (0) TO LBL 24; FABRICATED A NEW REPLACEMENT CHANNEL IAW DWG 65-52894; INSTALLED REPAIR PARTS IAW SRM 51-40-SDR AWXA200401113Stiffener · crackedDURING C-18 CHECK A 5/8 INCH CRACK WAS FOUND IN STIFFENER ON FORWARD SIDE OF BEAM AT BS 328, LBL 28, WL 207. MAINTENANCE REMOVED CRACKED STIFFENER AT BS 328, LBL 28, WL 207; FABRICATED A NEW REPLACEMENT STIFFENER PER DWG 65-45812; INSTALLED REPAIR PART IAW B7SDR AWXA200401112Galley Track · corrodedDURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON AFT END OF FORWARD GALLEY LOWER OUTBOARD TRACK AT BS 294, RBL 42, WL 208. MAINTENANCE REMOVED CORRODED SECTION OF FORWARD GALLEY LOWER OUTBOARD TRACK FROM BS 277 TO BS 294, RBL 42; FABRICATED A NEW REPLASDR AWXA200401109Skin · delaminatedDURING C-18 CHECK, FOUND THE RT OUTBOARD FLAP DELAMINATED ON THE LOWER INBOARD END BETWEEN WBL 230.68 AND WBL 234.68. MAINTENANCE REMOVED DELAMINATION ON RT OUTBOARD FLAP LOWER INBOARD END; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO FLAP IAW B737SDR AWXA200401167Angle · crackedDURING C-18 CHECK A .0625 INCH CRACK WAS FOUND IN FORWARD SCUFF PLATE ATTACH ANGLE AT L-1 DOOR ENTRYWAY BS 298, STR 17 LT. MAINTENANCE REMOVED CRACK IN FORWARD SCUFF PLATE ATTACH ANGLE AT L-1 DOOR ENTRYWAY BS 298, STR 17 LT. PERFORMED HFEC INSPECTION OF CUTOUSDR AWXA200401148Shear Tie · corrodedDURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AT BS 947, BETWEEN STR 26 AND 27 LT. MAINTENANCE REMOVED CORRODED SHEAR TIE AT BS 947, STR 26 AND 27; FABRICATED A NEW REPLACEMENT SHEAR TIE IAW DWG 65-46560; INSTALLED REPAIR PART IAW SRM 51-40-0SDR AWXA200401145Skin · debondedDURING C-18 CHECK, A DISBOND AREA WAS FOUND ON UPPER SURFACE OF NR 6 LEADING EDGE SLAT AT THE INBOARD END WBL 254.40 - 257.90 RT. MAINTENANCE CUTOUT DAMAGED SECTION ON NR 6 LEADING EDGE SLAT; FABRICATED A FILLER AND DOUBLERS; BONDED REPAIR PARTS TO SLAT IAW BSDR AWXA200401141Crease Beam · corrodedDURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON R-1 DOOR OUTER CHORD (CREASE BEAM ANGLE) BETWEEN BS 299 AND BS 324, RBL 62, WL 209. MAINTENANCE REMOVED DAMAGED R-1 DOOR OUTER CHORD FROM BS 299 TO BS 324, RBL 62; FABRICATED A NEW REPLACEMENT CHORD; INSTASDR AWXA200401140Beam · crackedDURING C-18 CHECK, A 1 1/8 INCH CRACK WAS FOUND IN L-1 DOOR BEAM AT LOWER FORWARD CORNER AT BS 313, STR 16 LT. MAINTENANCE CUTOUT DAMAGE IN L-1 DOOR BEAM AT LOWER FORWARD CORNER BS 313, STR 16 LT; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B7SDR AWXA200401125Stringer Clip · corrodedDURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON STRINGER CLIP FORWARD OF BS 967, STR 25 RT. MAINTENANCE REMOVED DAMAGED STRINGER CLIP AT BS 967, STR 25 RT; FABRICATED A NEW REPLACEMENT STRINGER CLIP; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, FIG SDR AWXA200401124Frame · corrodedDURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON FRAME AT BS 967, INBOARD SIDE OF STR 27 RT. MAINTENANCE CUTOUT DAMAGE ON FRAME AT BS 967, STR 27 RT; FABRICATED A FILLER REPAIR; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FIG 203.SDR AWXA200401123Frame · corrodedDURING C-18 CHECK, EXFOLIATION CORROSION WAS FOUND ON FRAME AT BS 947, INBOARD SIDE OF STR 27 RT. MAINTENANCE CUTOUT DAMAGE ON FRAME AT BS 947, STR 27 RT; FABRICATED A FILLER REPAIR; AND INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-07, FIG 204.SDR AWXA200401157Skin · crackedDURING C-18 CHECK, A 1 3/16 INCH, CRACK WAS FOUND IN FUSELAGE SKIN AT LOWER FORWARD CORNER OF L-2 DOOR BS 963, STR 17 LT. MAINTENANCE STOP DRILLED CRACK AT LOWER FORWARD CORNER OF L-2 DOOR BS 963, STR 17 LT. FABRICATED AN INNER, MIDDLE, AND OUTER PATCH, AND SDR AWXA200401149Skin · crackedDURING C18 CHECK, A 3/4 INCH CRACK WAS FOUND IN CAPTAINS WINDSHIELD OUTBOARD POST AT UPPER CORNER BS 217, WL 259.5. MAINTENANCE CUTOUT DAMAGED SKIN AT UPPER OUTBOARD CORNER OF CAPTAINS WINDSHIELD; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY THAT NO CRACKSSDR AWXA200401139Skin · crackedDURING C-18 CHECK, A 1/2 INCH CRACK WAS FOUND IN LOWER FORWARD RADIUS OF R-2 DOOR LOWER HINGE CUTOUT AT BS 951, ST 16 RT. MAINTENANCE CUTOUT DAMAGE IN R-2 DOOR LOWER HINGE CUTOUT AT BS 951, ST 16 RT; FABRICATED A FILLER, DOUBLER, AND TRIPLER; INSTALLED REPAIRSDR AWXA200401184Skin · crackedDURING C-18 CHECK, 18 CRACKS WERE FOUND AT FASTENER HOLES IN LOWER SURFACE SKIN OF NR 5 SLAT BETWEEN SLAT STA 150 AND SLAT STA 235. MAINTENANCE CUTOUT DAMAGE ON LOWER SURFACE SKIN OF NR 5 SLAT; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; SDR AWXA200401036Pump · intermittentEN ROUTE WITH LT CENTER FUEL TANK PUMP OFF AND RT CENTER FUEL TANK PUMP ON, CROSS FEED VALVE CLOSED, NR 2 ENGINE WAS DRAWING FUEL SLOWLY FROM RT CENTER TANK AND ALSO RT MAIN TANK, DIVERTED, DUE TO WEATHER. MAINTENANCE TROUBLESHOT FUEL SYSTEM; NO DEFECTS FOUNDSDR AWXA200401037Battery · dischargedDURING 4-DAY CHECK, THE AFT GALLEY EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401158Skin · crackedDURING C-18 CHECK, 4 EACH 3/8 INCH CRACKS WERE FOUND IN NR 4 SLAT LOWER SKIN BETWEEN SLAT STA 42 - 78. MAINTENANCE CUTOUT DAMAGE IN NR 4 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01, FIG 206.SDR AWXA200401026Skin · crackedDURING 8-DAY CHECK, A 3 3/16 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT RT TAIL AREA FORWARD OF OUTFLOW VALVE BS 927, STR 23 RT. MAINTENANCE REMOVED DAMAGED AREA OF SKIN AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED A REPAIR DOUBLER AND SDR AWXA200401060Floor Support · corrodedDURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOOR SUPPORT UPPER "T" CAP BETWEEN BS 986.5 AND BS 1016, LBL 6 TO LBL 18. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 986.5 TO BS 1016, LBL 6 TO LBL 18; FABRICATED AND SDR AWXA200401059Skin · damagedDURING C-18 CHECK RIVETS WERE FOUND PULLING THROUGH KEEL BEAM SKIN BETWEEN BS 663 AND BS 727. MAINTENANCE REMOVED DAMAGED KEEL BEAM SKIN FROM BS 663 TO BS 727, LBL 6.3 TO RBL 6.3; FABRICATED A NEW REPLACEMENT KEEL BEAM SKIN PANEL; INSTALLED REPAIR PARTS IAW AWSDR AWXA200400988Drip Tray · corrodedDURING C-18 CHECK, INTERGRANULAR CORROSION WAS FOUND ON BULKHEAD FLOOR WEB AT BS 1035, RBL 5, AFT OF RT AFT LAVATORY. MAINTENANCE REMOVED CORRODED BULKHEAD FLOOR WEB AT BS 1035, RBL 5; FABRICATED A NEW REPLACEMENT FLOOR WEB AND REINFORCEMENT STRAP; INSTALLED SDR AWXA200401061Crease Beam · corrodedDURING C-18 CHECK INTERGRANULAR CORROSION WAS FOUND ON L-1 DOOR CREASE BEAM AT FASTENER HOLES BETWEEN BS 318 AND BS 335. MAINTENANCE REMOVED CORRODED U-CHANNEL AT L-1 DOOR FROM BS 318 TO BS 335; FABRICATED A NEW REPLACEMENT U-CHANNEL; INSTALLED REPAIR PART IASDR AWXA200400909Wire · brokenDURING 4-DAY CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT INOPERATIVE. REPAIRED BROKEN EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400882Light · inoperativeLAX - EEL - DURING 8-DAY CHECK MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT INOPERATIVE. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 4 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400968Stringer · crackedDURING C-18 CHECK, A 5/8 INCH CRACK WAS FOUND IN FORWARD CABIN STRINGER 14 LT AT BS 354. MAINTENANCE REMOVED CRACKED SECTION OF STRINGER 14 LT AT BS 354; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02.SDR AWXA200400850Wire · looseDURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 23 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A LOOSE WIRE AT SPLICE SEAT ROW 23 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400838Connector · damagedABORTED TAKEOFF, ON TAKEOFF ROLL, ENROUTE, HAD NR 2 ENGINE EGT INDICATION OF 1250 DEGREE (C), REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE REPLACED NR 2 ENGINE EGT CONNECTOR (D3304) AT ENGINE FIRE WALL. PERFORMED HIGH POWER ENGINE RUN, OPERATIONAL CHECK SDR AWXA200400845Door Frame · crackedMAJOR REPAIR, DURING 4-DAY CHECK A 4 INCH CRACK WAS FOUND IN FORWARD CARGO DOOR LOWER FRAME AT UP LATCH BRACKET, BS 440. MAINTENANCE REMOVED CRACKED SECTION OF FORWARD CARGO DOOR LOWER FRAME; FABRICATED A NEW REPLACEMENT SECTION OF FRAME; INSTALLED REPAIR PARTSDR AWXA200400812Wire · brokenPHX - EEL - DURING 4-DAY CHECK EMERGENCY ESCAPE PATH LIGHT WAS FOUND INOPERATIVE AT SEAT ROW 16 LT. MAINTENANCE REPAIRED A BROKEN WIRE FOR EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400814Mount · failedON CLIMBOUT OF PHX EN ROUTE TO MCI RECEIVED WEATHER RADAR FAIL ANTENNA MESSAGE, DUE TO WEATHER EN ROUTE TURNED BACK TO PHX FOR REPAIR. MAINTENANCE REMOVED AND REPLACED WEATHER RADAR ANTENNA MOUNT PEDESTAL IAW BMM 34-41-11-4, OPERATIONAL CHECK WAS GOOD. VENDORSDR AWXA200400776Wire Harness · brokenPHX - EEL - DURING 4-DAY CHECK FOUND A EMERGENCY ESCAPE PATH LIGHT WIRE PULLED OUT OF CONNECTOR AT SEAT ROW 19 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT HARNESS AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400772Skin · crackedDURING 4-DAY CHECK A 3.5 INCH CRACK WAS FOUND IN LT FUSELAGE SKIN 4 INCHES ABOVE WING ROOT BETWEEN WINDOWS 11 AND 12, BETWEEN BS 500D+10 AND BS 520, STR 12 LT. MAINTENANCE CUTOUT DAMAGE IN LT FUSELAGE SKIN BETWEEN BS 500D+10 AND BS 520, STR 12 LT. PERFORMED ASDR AWXA200400737Syncronizer · faultyFLIGHT CONTROL, ON APPROACH, ENROUTE FLAPS FAILED TO EXTEND BEYOND FLAPS 5, USED ALTERNATE FLAP PROCEDURES TO EXTEND FLAPS TO 15. MAINTENANCE REMOVED AND REPLACED FLAP POSITION INDICATOR IAW T/C 1B27001, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF FLAP POSSDR AWXA200400664Circuit Breaker · brokenLAX - ABORTED TAKEOFF - FLT 0112 - ON TAKEOFF ROLL AT LAX EN ROUTE FOR LAS THE TAKEOFF WARNING CONFIGURATION HORN SOUNDED, REJECTED TAKEOFF AND FOUND THAT FLAP INDICATOR CIRCUIT BREAKER POPPED AND HAD BROKEN INTO PIECES. MAINTENANCE REMOVED AND REPLACED FLAP SDR AWXA200400635Battery · dischargedPHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400632Wire · brokenDEN - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT CONNECTOR FOR LIGHT ASSEMBLY. REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 21 LT, OPERATIONAL CHECK WAS GOOSDR AWXA200400650Web · crackedLCQ - MAJOR REPAIR - DURING C-19 CHECK A .75 INCH CRACK AND CORROSION WERE FOUND ON AFT CABIN FLOOR WEB WHERE FLANGE ATTACHED TO SEAL AND RETAINER AT BS 1006, RBL 38. MAINTENANCE CUT OUT DAMAGED SECTION OF FLOOR WEB AT BS 1006, RBL 38; FABRICATED A REPAIR DOUSDR AWXA200400648Shear Web · crackedLCQ - MAJOR REPAIR - DURING C-19 CHECK A .875 INCH CRACK WAS FOUND IN AFT CABIN SHEAR WEB, JUST BELOW FLOOR LEVEL AT BS 967, LBL 36. MAINTENANCE REMOVED DAMAGED AFT CABIN SHEAR WEB AT BS 967, LBL 36; FABRICATED A NEW REPLACEMENT SHEAR WEB; INSTALLED REPAIR PASDR AWXA200400649Stringer · corrodedLCQ - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON STRINGER 15 LT AT BS 1006. MAINTENANCE CUT OUT DAMAGE IN STRINGER 15 LT AT BS 1006; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, FILLER AND DOUBLER; INSTALLED SPLICE REPAIR IAW B737-300 SRM 53SDR AWXA200400562Battery · dischargedLCQ - EMERGENCY EQUIPMENT - DURING C-19 CHECK FOUND THE AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400647Shear Tie · crackedLCQ - MAJOR REPAIR - DURING C-19 CHECK A .875 INCH CRACK WAS FOUND IN STRINGER SHEAR TIE BS 500A, STR 16 RT. MAINTENANCE REMOVED DAMAGED STRINGER SHEAR TIE CLIP AT BS 500A, STR 16 RT; FABRICATED A NEW REPLACEMENT SHEAR TIE PER DWG 69-35350; INSTALLED REPAIR PSDR AWXA200400646Crease Beam · corrodedLCQ - MAJOR REPAIR - DURING C-19 CHECK INTERGRANULAR CORROSION WAS FOUND ON L-1 DOOR CREASE BEAM AT TOP OF FLOOR STRUCTURE AROUND FASTENER HOLES FROM BS 300 TO BS 344. MAINTENANCE REMOVED CORRODED CREASE BEAM FROM BS 300 TO BS 344; FABRICATED A NEW REPLACEMENSDR AWXA200400606Splice · crackedLCQ - MAJOR REPAIR - DURING C-19 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER SPLICE AT BS 907, STR 3 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE AT BS 907, STR 3 LT, WL 302; FABRICATED A NEW REPLACEMENT STRINGER SPLICE; INSTALLED REPAIR PART IAW B737-300 SDR AWXA200400645Stringer · crackedLCQ - MAJOR REPAIR - DURING C-19 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER 16 LT AT BS 495D, AFT OF LT WING INSPECTION LIGHT ASSEMBLY. MAINTENANCE CUT OUT DAMAGE IN STRINGER 16 LT AT BS 495D; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, A FILLER AND DO
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