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 AWXA200300536Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT UNDER FLANGE IN AFT CARGO COMPARTMENT BS 859, RBL 3. MAINTENANCE CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOOR SUPPORT BS 859, RBL 3; FABRICATSDR AWXA200300477Stringer · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND AT END FASTENER OF STRINGER 16 LT, BS 504C. MAINTENANCE REMOVED FASTENER AND CUT OUT DAMAGED SECTION OF STRINGER 16 LT, AT BS 504C; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXISTSDR AWXA200300456Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BEAM BS 1006-1016, LBL 10. MAINTENANCE REMOVED FLOOR SUPPORT BEAM BS 1006-1016, LBL 10 AND UPON FURTHER EVALUATION DISCOVERED FILLER WAS CORRODED BEYOND LIMITS; FABRICATEDSDR AWXA200300454Web · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 3 INCH CRACK WAS FOUND ON CUSP WEB AT BS 1003, LBL 62. MAINTENANCE REMOVED CRACKED CUSP WEB AND ATTACH ANGLE AT BS 1003, LBL 62; FABRICATED A NEW REPLACEMENT WEB; INSTALLED REPAIR WEB AND REMOVED ATTACH ANGLE IAW B737-SDR AWXA200300453Stringer · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK 2 EACH 1 INCH CRACKS WERE FOUND AT END OF STRINGER 16 RT, AT BS 504C. MAINTENANCE CUTOUT CRACKED AREA OF STRINGER 16 RT, AT BS 504C; FABRICATED 2 EACH REPAIR ANGLES, A HAT SECTION, AND CHANNEL; INSTALLED REPAIR PARTS IAWSDR AWXA200300481Sill · corrodedLCQ - MAJOR REPAIR - DURING C-17 CHECK INTERGRANULAR CORROSION WAS FOUND AROUND SCREW HOLES ON FORWARD CARGO DOOR SCUFF PLATE BS 460. MAINTENANCE MECHANICALLY REMOVED CORROSION FROM FORWARD CARGO DOOR SCUFF PLATE (SILL WEB) BS 460, AND FOUND MATERIAL LOSS TO SDR AWXA200300478Shear Tie · corrodedLCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON SHEAR TIE AT BASE OF FRAME BS 927, STR 27 LT TO STR 27 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF SHEAR TIE; FABRICATED A RSDR AWXA200300476Shear Tie · corrodedLCQ - MAJOR REPAIR - DURING C-17 CHECK INTERGRANULAR CORROSION WAS FOUND ON SHEAR TIE AT BS 500B BETWEEN STR 28 LT AND 28 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT CORRODED AREA OF SHEAR TIE AT BS 500B BETWEEN STR 28SDR AWXA200300455Shear Tie · corrodedLCQ - MAJOR REPAIR - DURING C-17 CHECK INTERGRANULAR CORROSION WAS FOUND ON SHEAR TIE AT BS 500B, BETWEEN STR 28 LT AND 28 RT. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF SHEAR TIE AT BS 500B, BETWEEN SSDR AWXA200300485Keelbeam · corrodedLCQ - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON KEEL BEAM LOWER ANGLE IN RT AIR CONDITIONING BAY, BS 540. MAINTENANCE REMOVED 2 EACH ANGLE SUPPORTS FOR ACCESS AND FOUND CORROSION INDICATIONS IN ALL SIX HOLES; REAMED OUT HOLES AND PERSDR AWXA200300461Channel · corrodedDURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT CARGO COMPARTMENT FLOOR PANEL SUPPORT CHANNEL, BS 859, RBL 7. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLOOR PANEL SUPPORT CHANNEL; FABRICATED SDR AWXA200300572Frame · corrodedMCN - MAJOR REPAIR - DURING C-17 CHECK EXFOLIATION CORROSION WAS FOUND ON BS 847 FRAME LOWER STIFFENER STRAP RBL 19-25, WL 160. MAINTENANCE BLENDED OUT CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED -12 INNER FRAME CHORD STRAP; FABRICASDR AWXA200300422Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A .3125 INCH CRACK WAS FOUND ON STRINGER TIE CLIP IN AFT CARGO COMPARTMENT AT THE FORWARD SIDE OF BS 887, STR 22 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 887, STR 22 RT, FABRICATED A NEW REPLACEMENT STRINGSDR AWXA200300387Battery Pack · dischargedPHX - EEL - EMERGENCY ESCAPE PATH LIGHT SYSTEM WAS FOUND ACTIVATED. MAINTENANCE REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERY PACKS IAW T/C A1C33011, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300538Skin · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A 1.4375 INCH CRACK WAS FOUND AT FASTENER HOLE ON SKIN OF L-1 DOOR CUTOUT, LOWER AFT CORNER BS 334, LBL 63. MAINTENANCE REMOVED CENTER SCUFF PLATE ATTACH ANGLE; HFEC INSPECTION INDICATED CRACKS ON ALL 3 LAYERS. TRIMMED OSDR AWXA200300535Skin · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK HFEC INSPECTION INDICATED A .25 INCH CRACK AT FASTENER HOLE ON FUSELAGE SKIN FORWARD OF L-1 DOOR LOWER HINGE CUTOUT. MAINTENANCE TRIMMED OUT DAMAGE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST. FABRICATED ASDR AWXA200300438Plate · corrodedMCN - EES - DURING C-17 CHECK CORROSION WAS FOUND ON TOP SURFACE OF GIRT FITTING ATTACH BRACKET (PLATE) AT L-2 DOOR FWD FITTING. MAINTENANCE REMOVED AND REPLACED GIRT FITTING ATTACH BRACKET AT L-2 DOOR PER T/C C1D25018.SDR AWXA200300524Floorbeam · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK 5 EACH CRACKS WERE FOUND ON FLOORBEAM SHEAR WEB BS 927 TO BS 947, BL 0. MAINTENANCE REMOVED CRACKED FLOORBEAM SHEAR WEB FROM BS 927 TO BS 947, AND ATTACH ANGLE; FABRICATED AND NEW REPLACEMENT SHEAR WEB PER DWG 69-36656-5SDR AWXA200300432Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A .1875 INCH CRACK WAS FOUND ON THE RT WING INBOARD TRAILING EDGE UPPER FIXED PANEL LOWER SUPPORT ANGLE WBL 72.25. MAINTENANCE REMOVED CRACKED LOWER SUPPORT ANGLE AT WBL 72.25; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLSDR AWXA200300388Flashlight · inoperativeMCN - EMERGENCY EQUIPMENT - DURING C-17 CHECK THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300325Light · brokenFLIGHT CREW REPORTED THE EMERGENCY EXIT LIGHT WAS DAMAGED AT R-2 DOOR. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT AT R-2 DOOR, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300654Skin · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON SKIN AT LOWER ROW OF FASTENER HOLES STR 4 LT BS 387. MAINTENANCE CUTOUT CRACKED SKIN AT STR 4 LT, BS 387; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A DOUBLESDR AWXA200300653Skin · crackedDURING C-17 CHECK 6 EACH .0625 INCH CRACKS WERE FOUND ON SKIN AT LOWER ROW OF FASTENER HOLES STR 4 LT, BS 500D+4, BS 500D+13, BS 522, BS 523, BS 525, AND BS 527. MAINTENANCE CUT OUT CRACKED SKIN AT STR 4 LT BS 500D+4, BS 500D+13, AND FROM BS 518 TO BS 526; PESDR AWXA200300216Indicator · unreliableON CLIMB FROM PHX EN ROUTE TO LAX TRAILING EDGE FLAPS SPLIT AND WERE ASYMMETRIC AT 1 AND 2 DURING FLAP RETRACTION FROM FLAP 5 TAKEOFF. TURNED BACK TO PHX AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE FOUND THE LEFT FLAP POSITION INDICATOR CIRCUIT BREAKER POPPSDR AWXA200300146Seat Track · misalignedLCQ - MAJOR REPAIR - DURING C-18 CHECK THE L/H OUTBOARD SEAT TRACK SPLICE WAS FOUND INTERFERING WITH THE SEAT ATTACH POINT BS 847. MAINTENANCE REMOVED SEAT TRACK FROM BS 807 TO BS 847, LBL 45; FABRICATED A NEW REPLACEMENT SEAT TRACK; INSTALLED REPAIR PART IAW SDR AWXA200300165Fitting · corrodedLCQ - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON R/H FORWARD VERTICAL TO FUSELAGE ATTACH FITTING BS 1088. MAINTENANCE REMOVED CORRODED ATTACH FITTING BS 1088; FABRICATED A NEW REPLACEMENT ATTACH FITTING; INSTALLED REPAIR PART IAW B737-SDR AWXA200300166Frame · crackedLCQ - MAJOR REPAIR - DURING C-18 CHECK A 7/8 INCH CRACK WAS FOUND ON BS 178 RT SIDE FRAME, PASSING THROUGH WL 207 COCKPIT FLOOR AREA.. MAINTENANCE REMOVED DAMAGED RT SIDE FRAME BS 178; FABRICATED A NEW REPLACEMENT FRAME; INSTALLED REPAIR PART IAW B737-300 SRM SDR AWXA200300164Web · crackedLCQ - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT LBL 5, WL 200 TO WL 201.25. MAINTENANCE CUTOUT CRACKS ON BS 178 BULKHEAD WEB AT LBL 5, WL 200 TO WL 201.25; PERFORMED HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXISTSDR AWXA200300162Web · crackedLCQ - MAJOR REPAIR - DURING C-18 CHECK 2 EACH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB, APPROXIMATELY WL 196.75 TO WL 198, AT APRON OF RBL 5. MAINTENANCE CUTOUT CRACKS AT RBL 5, WL 196.75 AND WL 202; PERFORMED HFEC INSPECTION OF CUTOUTS TO VERIFY NO CRACKS EXISDR AWXA200300163Fitting · corrodedLCQ - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON AFT LAVATORY AREA FLOOR BOARD ATTACH HOLE BS 986, RBL 20. MAINTENANCE REMOVED AND REPLACED ATTACH FITTING AT BS 986, RBL 20 IAW B737-300 SRM 51-40-02, PG. 6-9.SDR AWXA200300076Light · inoperativeDURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300118Panel · crackedLCQ - MAJOR REPAIR - DURING C-18 CHECK 2 EACH 1" CRACKS WERE FOUND ON KEEL BEAM PANEL BETWEEN WHEEL WELLS AT FORWARD END BS 685. MAINTENANCE REMOVED EXISTING DOUBLER AT BS 660 TO BS 690; STOP DRILLED CRACKS AND PERFORMED HFEC INSP TO VERIFY CRACKS CONTAINED; FSDR AWXA200300029Skin · crackedPHX - MAJOR REPAIR - DURING INSPECTION A 2 1/2" CRACK WAS FOUND ON SKIN AT BS 767 BELOW EMERGENCY EXIT LIGHT ON R/H SIDE OF AIRCRAFT. MAINTENANCE CUTOUT CRACK; PERFORMED HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER AND FILLER; ANDSDR AWXA200201248Indicator · inoperativeFLT 204 - WHEN PREPARING TO LAND, EN ROUTE, WITH GEAR LOWERED, HAD NO GEAR DOWN INDICATION. FOUND GROUND AIR CIRCUIT BREAKER TRIPPED; RESET CIRCUIT BREAKER AND DECLARED EMERGENCY. FUEL INDICATIONS WERE NORMAL, FLEW BY TOWER TO VERIFY LANDING GEAR WAS DOWN; LANSDR AWXA200201161Proximity Sensor · faultyDURING CLIMBOUT AT 5000 FT FORWARD ENTRY DOOR WARNING LIGHT ILLUMINATED. FORWARD ENTRY DOOR HANDLE WAS SECURE. TURNBACK TO LAS. MX ADJUSTED L-1 DOOR SENSOR. ACFT WAS PRESSURIZED TO 4 PSI, NO FAULTS WERE NOTED. DURING PRESSURIZATION SHOOK HANDLE, LIGHT REMSDR 2002200284Battery Pack · inoperativeFLOOR EMERGENCY LIGHTS IN ZONE 3 LEFT SIDE ( AFT CABIN ) ARE INOPERATIVE. REMOVED AND REINSTALLED EMERGENCY LIGHT BATTERY PACK IAW MM AND POWER SUPPLY IAW MM.SDR AWXA200201119Charger · failedDURING C-19 CHECK THE LT AFT OVERHEAD EMERGENCY BATTERY POWER SUPPLY / CHARGER UNIT FAILED FUNCTION TEST. MAINTENANCE REMOVED AND REPLACED THE L./H AFT OVERHEAD EMERGENCY POWER SUPPLY UNIT IAW BMM 33-51-51, PG. 206-207.SDR AWXA200201082Fan · seizedEN ROUTE FROM DFW TO LAS AT CRUISE THE FLIGHT ATTENDANT REPORTED A BURNING ODOR, TURNED OFF RECIRULATION FAN AND BURNING ODOR DISSIPATED. RECIRCULATION FAN REMAINED OFF FOR REST OF THE FLIGHT WITH NO FURTHER EVENTS REPORTED. MAINTENANCE REMOVED AND REPLACED SDR AWXA200201128Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-19 CHECK A 1/4 CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 947.5, STR 26 L/H. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT BS 947.5, STR 26 L/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 65-465601; AND INSTALLED RESDR AWXA200201130Channel · corrodedYVR - MAJOR REPAIR - DURING C-19 CHECK EXFOLIATION CORROSION WAS FOUND UNDER AFT CARGO FLOOR SUPPORT CHANNEL AT SEVERAL ANCHOR NUTS BETWEEN BS 847 - BS 867; MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; CUTOUT DAMAGED SECTION OF FLSDR AWXA200201135Tie Clip · crackedYVR - MAJOR REPAIR - DURING C-19 CHECK A 1/4 CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 947.5, STR 25 R/H. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT BS 947.5, STR 25 R/H; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 65-465601; AND INSTALLED RESDR AWXA200201132Frame · crackedYVR - MAJOR REPAIR - DURING C-19 CHECK A 1/2" CRACK WAS FOUND ON FUSELAGE FRAME AT BS 947.5, STR 18 L/H. MAINTENANCE CUTOUT CRACK AT BS 947.5, STR 18 L/H AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A SHEAR TIE AND 2 EACH BELT FRAME DOSDR AWXA200201142Angle · corrodedYVR - MAJOR REPAIR - DURING C-19 CHECK INTERGRANULAR CORROSION WAS FOUND AT SCREW HOLES ON THE UNDERSIDE OF INTERCOSTAL BEAMS BS 927 TO BS 1016. MAINTENANCE REMOVED ANGLE UNDER DOOR SILL CHORD AT R/H SIDE BS 967 TO BS 987; BLENDED CORROSION ON INTERCOSTALS BS SDR AWXA200201139Skin · crackedYVR - MAJOR REPAIR - DURING C-19 CHECK LOOSE FASTENERS AND A 1 1/4" CRACK WAS FOUND ON SKIN OF THE L/H HORIZONTAL STABILIZER LOWER SURFACE BETWEEN STAB STATIONS 138.70 AND 147.90. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON THE L/H HORIZONTAL STABILIZER LOWER SDR AWXA200201136Skin · delaminatedDURING C-19 CHECK THE NR 3 LEADING EDGE SLAT AT THE OUTBOARD END OF THE TRAILING EDGE WEDGE WAS FOUND TO BE DELAMINATING. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON THE NR 3 LEADING EDGE SLAT AT THE OUTBOARD END OF THE TRAILING EDGE WEDGE. APPLIED ADHESIVE, RSDR AWXA200201131Web · crackedYVR - MAJOR REPAIR - DURING C-19 CHECK A 1/2" CRACK WAS FOUND ON WEB, 5 1/2" ABOVE WL 207 AT BS 178, LBL 5.7, UPPER L/H RADAR ANTENNA MOUNT BRACKET LOCATION. MAINTENANCE CUTOUT DAMAGE AT WL 207 - 212, BS 178, LBL 5.7; FABRICATED A FILLER AND DOUBLER; AND INSTASDR AWXA200201144Skin · delaminatedYVR - MAJOR REPAIR - DURING C-19 CHECK THE RT OUTBOARD FLAP WAS FOUND DELAMINATED AT THE INBOARD AFT CORNER. MAINTENANCE REMOVED AND REPLACED THE RT OUTBOARD FLAP IAW AWA T/C R8M27002.SDR AWXA200201141Skin · delaminatedDURING C-19 CHECK THE NR 5 LEADING EDGE SLAT AT THE INBOARD AND OUTBOARD ENDS OF WEDGE WAS FOUND TO BE DELAMINATED. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON THE NR 5 LEADING EDGE SLAT AT THE INBOARD AND OUTBOARD END OF WEDGE. APPLIED ADHESIVE, REPLACEMENT SSDR AWXA200201140Wedge · delaminatedMAJOR REPAIR DURING C-19 CHECK, NR 4 LEADING EDGE SLAT INBOARD WEDGE WAS FOUND TO BE DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE NR 4 LEADING EDGE SLAT IAW BMM. OPERATIONAL CHECK ACCOMPLISHED IAW BMM.SDR AWXA200201138Skin · delaminatedDURING C-19 CHECK THE LT OUTBOARD FLAP WAS FOUND DELAMINATED AT THE AFT INBOARD CORNER OF THE TRAILING EDGE WEDGE, LT OUTBOARD FLAP. MAINTENANCE REMOVED DAMAGED AREA OF SKIN AT THE AFT INBOARD CORNER OF THE TRAILING EDGE WEDGE, FABRICATED A REPAIR CORE AND EXT
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