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 AWXA200400605Stringer · crackedLCQ - MAJOR REPAIR - DURING C-19 CHECK A .6875 INCH CRACK WAS FOUND IN STRINGER AT BS 495C, STR 16 RT, WL 188. MAINTENANCE CUT OUT CRACKED SECTION OF STRINGER AT BS 495C, STR 16 RT, WL 188; FABRICATED A NEW REPLACEMENT SECTION OF STRINGER, HAT SECTION, CHANNESDR AWXA200400602Stringer Clip · crackedDURING C-19 CHECK A .5 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 727B, STR 4 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727B, STR 4 RT FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-35352; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02 PSDR AWXA200400535Light · inoperativeDEN - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY EXIT LIGHT JUST FORWARD OF THE L-2 DOOR IN THE LT AFT GALLEY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT AFT GALLEY EMERGENCY EXIT LIGHT ASSEMBLY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400607Skin · crackedLCQ - MAJOR REPAIR - DURING C-19 CHECK 10 EACH CRACKS WERE FOUND ON UPPER AND LOWER FASTENER ROWS OF FUSELAGE SKIN LAP SEAM BETWEEN BS 950 AND BS 960, STR 20 LT, WL 192. MAINTENANCE REMOVED EXISTING DOUBLER & FILLER AND ENLARGED CUTOUT TO REMOVE CRACKED SECTISDR AWXA200400643Attach Angle · crackedLCQ - MAJOR REPAIR - DURING C-19 CHECK A 2 INCH CRACK WAS FOUND IN RIGHT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE ON AFT OUTBOARD SIDE BS 665, RBL 64. MAINTENANCE REMOVED CRACKED RIGHT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE; FABRICATED A NEW REPSDR AWXA200400642Angle · crackedLCQ - MAJOR REPAIR - DURING C-19 CHECK A 1 INCH CRACK WAS FOUND IN LT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE ON AFT OUTBOARD SIDE BS 665, LBL 64. MAINTENANCE REMOVED CRACKED LT RAM AIR HEAT EXCHANGER DUCT UPPER ATTACH ANGLE; FABRICATED A NEW REPLACEMESDR AWXA200400485Battery · dischargedDURING 8-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHTING AFT OF SEAT ROW 18 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT AFT EMERGENCY POWER SUPPLY BS 947, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400457Battery · dischargedDEN - EMERGENCY EQUIPMENT - DURING A-01 CHECK FOUND THE FORWARD EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR 2004F00182Oven · burnedSMOKE COMING FROM LOWER P6 PANEL, ACCOMPLISHED NNC 8.4-8.5 SMOKE DISSIPATED LANDED IN KMIA WITHOUT INCIDENT. FOUND FORWARD GALLEY OVEN SHORTED OUT. REMOVED OVEN FOR REPAIRS AND A/C RETURNED TO SERVICE WITHOUT INCIDENT. (M)SDR AWXA200400356Light · inoperativeDEN - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 7 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 7 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400353Wire · brokenPHX - EMERGENCY EQUIPMENT - DURING EMERGENCY DESCENT AND MANUAL OXYGEN MASK DEPLOYMENT, MASKS FAILED TO DEPLOY AT SEAT ROW 11 RIGHT. MAINTENANCE RE-TERMINATED BROKEN SPLICE AT PASSENGER OXYGEN LATCH MECHANISM SEAT ROW 11 RIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400352Outflow Valve · failedAT FL 350 LOST CABIN PRESSURE, COULD NOT CONTROL IN ANY MODE. EXECUTED EMERGENCY DESCENT & MANUALLY DEPLOYED MASKS, DECLARED EMERGENCY. MX PERFORMED TEST OF OUTFLOW VALVE & FOUND HEATER GASKET INOP. R / R OUTFLOW VALVE, CABIN PRESS CONTROLLER AND CABIN PRESSDR AWXA200400331Light · inoperativeDEN - EEL - DURING 8-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 22 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400286Wire · brokenPHX - EEL - DURING 4-DAY CHECK THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 14 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED EMERGENCY ESCAPE PATH LIGHT WIRING AT FLOOR CONNECTOR SEAT ROW 14 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400285Skin · crackedPHX - MAJOR REPAIR - DURING 8-DAY CHECK A 1.5 INCH CRACK WAS FOUND IN FUSELAGE SKIN 3 INCHES ABOVE LAP SEAM RT SIDE AT BS 767. MAINTENANCE CUT OUT DAMAGED SKIN 3 INCHES ABOVE LAP SEAM RT SIDE AT BS 767; FABRICATED 2 REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAWSDR AWXA200400260Wire · brokenPHX - EEL - DURING 4-DAY CHECK FOUND EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT INOPERATIVE. MAINTENANCE REPAIRED A BROKEN SPLICE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 15 LT; OPERATIONAL CHECK WAS GOOD.SDR AWXA200400279Angle · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK .625 INCH CRACK WAS FOUND ON RT WING OUTBOARD EXHAUST GATE ANGLE WBL 205. MAINTENANCE REMOVED CRACKED RT WING OUTBOARD EXHAUST GATE ANGLE AT WBL 205; FABRICATED A NEW REPLACEMENT ANGLE; INSTALLED REPAIR PART IAW AWA ER 0SDR AWXA200400270Frame · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK A .5 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT FRAME SHEAR TIE AT BS 807, RBL 4. MAINTENANCE REMOVED DAMAGED SECTION OF AFT CARGO COMPARTMENT FRAME SHEAR TIE AT BS 807, RBL 4; FABRICATED A NEW REPLACEMENT SECTION OF SDR AWXA200400263Channel · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK A 2 INCH CRACK WAS FOUND ON AFT CARGO DOOR HOLD OPEN FITTING SUPPORT (CHANNEL) BETWEEN FLOORBEAM BS 787 AND BS 807, RBL 20. MAINTENANCE REMOVED DAMAGED AFT CARGO DOOR HOLD OPEN FITTING CHANNEL FROM BS 787 TO BS 807, RBL SDR AWXA200400265Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK A .3125 INCH CRACK WAS FOUND ON STRINGER TIE CLIP AT BS 277, STR 10 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 277, STR 10 RT; FABRICATED A NEW REPLACEMENT TIE CLIP PER DWG 69-36600; INSTALLED REPAIR PART IASDR AWXA200400269Strap · corrodedMCN - MAJOR REPAIR - DURING C-20 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT LAVATORY FLOOR STRAP BETWEEN BS 1028, RBL 17, WL 208. MAINTENANCE REMOVED CORRODED RT AFT LAVATORY FLOOR STRAP FROM BS 1028, RBL 17, WL 208; FABRICATED A NEW REPLACEMENT STRAP PESDR AWXA200400268Strap · corrodedMCN - MAJOR REPAIR - DURING C-20 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT LAVATORY FLOOR STRAP BETWEEN BS 1020 AND BS 1025, RBL 27, WL 208. MAINTENANCE REMOVED CORRODED RT AFT LAVATORY FLOOR STRAP FROM BS 1020 TO BS 1025, RBL 27, WL 208; FABRICATED A NSDR AWXA200400258Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-20 CHECK INTERGRANULAR CORROSION WAS FOUND ON UPPER SURFACE OF FLOORBEAM AT BS 1016, RBL 33, WL 208. MAINTENANCE BLENDED OUT CORROSION ON UPPER SURFACE OF FLOORBEAM AT BS 1016, RBL 33, WL 208; FABRICATED A REPAIR STRAP; INSTALLEDSDR AWXA200400293Angle · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK FOUND A .625 INCH CRACK IN ANGLE BS 616, LBL 55, WL 208. MAINTENANCE CUT OUT DAMAGE IN ANGLE BS 616, LBL 55, WL 208; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW AWA ER 03-5311-01143-DD1.SDR AWXA200400290Stringer · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER 16 LT AT BS 500C+4, FORWARD OF LEADING EDGE LIGHT. MAINTENANCE CUT OUT DAMAGE ON STRINGER 16 LT AND REMOVED STRINGER TIE CLIP AT BS 500C+4; FABRICATED A REPAIR CHANNEL, FILLER, ANDSDR AWXA200400281Panel · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK A .75 INCH CRACK WAS FOUND ON LT PYLON PANEL 5727L ACCESS OPENING LANDING NAC STA 211. MAINTENANCE STOP DRILLED CRACK ON LT PYLON PANEL 5727L ACCESS OPENING LANDING AT NAC STA 21; PERFORMED A HFEC INSPECTION TO VERIFY CRSDR AWXA200400264Skin · debondedMCN - MAJOR REPAIR - DURING C-20 CHECK FOUND DISBOND AREA ON UPPER SURFACE OF LT OUTBOARD FORE FLAP, 104 INCHES FROM OUTBOARD END. MAINTENANCE CUT OUT DISBOND AREA ON UPPER SURFACE OF LT OUTBOARD FORE FLAP; FABRICATED A REPAIR CORE AND DOUBLER; INSTALLED REPASDR AWXA200400262Frame · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK 2 CRACKS WERE FOUND ON LOWER INBOARD RADIUS OF R-1 DOOR ENTRY WAY FORWARD STUB FRAME AT CREASE BEAM ATTACH POINT BS 294, RBL 59, WL 209. MAINTENANCE CUT OUT DAMAGE ON R-1 DOOR ENTRY WAY FORWARD STUB FRAME BS 294, RBL 59,SDR AWXA200400259Crease Beam · corrodedMCN - MAJOR REPAIR - DURING C-20 CHECK CORROSION WAS FOUND ON L-2 DOOR ENTRY WAY CREASE BEAM UPPER OUTER CHORD BETWEEN BS 960 AND BS 983, LBL 55, WL 209. MAINTENANCE REMOVED CORRODED CREASE BEAM UPPER OUTER CHORD FROM BS 960 TO BS 983, LBL 55, WL 209; FABRICASDR AWXA200400254Stringer · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER 16 RT AT BS 500C, AFT OF LEADING EDGE LIGHT ASSEMBLY. MAINTENANCE CUT OUT DAMAGED END OF STRINGER 16 RT AT BS 500C; FABRICATED FILLER AND REPAIR CHANNEL; INSTALLED REPAIR PARTS IAW SDR AWXA200400252Stringer · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK A .25 INCH CRACK WAS FOUND ON STRINGER 16 LT AT BS 500C, AFT OF LEADING EDGE LIGHT ASSEMBLY. MAINTENANCE CUT OUT DAMAGED END OF STRINGER AT BS 500C; FABRICATED FILLER AND REPAIR CHANNEL; INSTALLED REPAIR PARTS IAW AWA ERSDR AWXA200400251Skin · debondedMCN - MAJOR REPAIR - DURING C-20 CHECK THE UPPER SURFACE OF LT WING INBOARD FORE FLAP WAS FOUND DISBONDED 34.75 INCHES FROM OUTBOARD END. MAINTENANCE CUT OUT DISBOND AREA OF LT WING INBOARD FORE FLAP; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS IAW 51-SDR AWXA200400249Gate · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK A .375 INCH CRACK WAS FOUND AT FASTENER HOLE ON L-2 DOOR LOWER GATE. MAINTENANCE REMOVED L-2 DOOR LOWER GATE ASSEMBLY FROM BS 960 TO BS 986.5, STR 16-17 LT; FABRICATED A NEW REPLACEMENT GATE ASSEMBLY; INSTALLED REPAIR PASDR AWXA200400236Bracket · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK FOUND 2 CRACKS IN L-1 DOOR SILL ATTACH ANGLE BRACKET AT BS 302, LBL 66, WL 207.5. MAINTENANCE REMOVED CRACKED L-1 DOOR SILL BRACKET AT BS 302, LBL 66, WL 207.5; FABRICATED A NEW REPLACEMENT BRACKET; INSTALLED REPAIR PARTSDR AWXA200400245Crease Beam · corrodedMCN - MAJOR REPAIR - DURING C-20 CHECK GALVANIC CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF R-1 DOOR ENTRY WAY CREASE BEAM UPPER CHORD, UPPER LEG, FROM BS 305 TO BS 320, RBL 47, WL 209. MAINTENANCE REMOVED CORRODED UPPER ANGLE OF CREASE BEAM FROM BS 305SDR AWXA200400235Skin · delaminatedMCN - MAJOR REPAIR - DURING C-20 CHECK FOUND THE RT AILERON LEADING EDGE ACCESS PANEL LOWER LAND DELAMINATED 33.5 INCHES FROM THE INBOARD END. MAINTENANCE PERFORMED BOND REPAIR IAW B737-300 SRM 51-70-17, REPAIR 6, FIG 2, 6, 8 & 20.SDR AWXA200400205Battery · dischargedPHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANTS EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400204Fan Blade · damagedAUS - ENGINE FOD - DURING RON INSPECTION MAINTENANCE FOUND 33 FAN BLADES DAMAGED ON THE NR 2 ENGINE. SUSPECT DAMAGE WAS CAUSED BY MISSING ACOUSTIC LINER SCREWS. MAINTENANCE PERFORMED FOD INSPECTION IAW T/C I8M05030, BORESCOPED ENGINE IAW T/C I5M72025, REMOVESDR AWXA200400280Skin · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK 4 CRACKS WERE FOUND ON NR 2 SLAT LOWER SKIN BELOW INBOARD AUXILIARY TRACK WBL 294.40. MAINTENANCE CUT OUT DAMAGE ON NR 2 SLAT LOWER SKIN WBL 294.40; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-3SDR AWXA200400267Skin · delaminatedMCN - MAJOR REPAIR - DURING C-20 CHECK THE NR 1 SLAT WEDGE LOWER SURFACE WAS FOUND DELAMINATED OUTBOARD OF THE INBOARD AUXILIARY TRACK. MAINTENANCE CUT OUT DELAMINATED AREA ON NR 1 SLAT WEDGE LOWER SURFACE; FABRICATED REPAIR DOUBLERS; INSTALLED REPAIR PARTS ISDR AWXA200400266Skin · delaminatedMCN - MAJOR REPAIR - DURING C-20 CHECK FOUND THE LT WING TRAILING EDGE FORE FLAP DELAMINATED ON THE OUTBOARD LOWER SURFACE, APPROXIMATELY 2 INCHES FROM END. MAINTENANCE CUT OUT DELAMINATION ON LT WING TRAILING EDGE FORE FLAP; FABRICATED A REPAIR CORE AND DOUBSDR AWXA200400253Skin · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK 6 CRACKS WERE FOUND ON NR 1 SLAT LOWER SKIN BELOW ACTUATOR AT WBL 445. MAINTENANCE CUT OUT DAMAGED SKIN ON NR 1 SLAT LOWER SKIN WBL 445; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW 57-43-01 FIG 206 PSDR AWXA200400250Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-20 CHECK THE RT WING INBOARD MID FLAP TRAILING EDGE WEDGE WAS FOUND DELAMINATED ON LOWER SURFACE APPROXIMATELY 36 INCHES FROM INBOARD END. MAINTENANCE CUT OUT DELAMINATED AREA OF MID FLAP TRAILING EDGE WEDGE AND FOUND NO CORE DAMSDR AWXA200400248Skin · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK 3 CRACKS WERE FOUND ON NR 3 SLAT LOWER SKIN BELOW ACTUATOR AT WBL 232.40. MAINTENANCE CUT OUT DAMAGE ON NR 3 SLAT LOWER SKIN WBL 232.40; FABRICATED A FILLER AND SPLICE PLATE PER DWG 65C26603; INSTALLED REPAIR PARTS IAW 5SDR AWXA200400246Shear Tie · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK A .5 INCH CRACK WAS FOUND ON SHEAR TIE IN AFT CARGO COMPARTMENT BS 807, BL -0-. MAINTENANCE REMOVED DAMAGED SHEAR TIE IN AFT CARGO COMPARTMENT BS 807, BL -0-; FABRICATED A NEW REPLACEMENT SHEAR TIE; INSTALLED REPAIR PARTSDR AWXA200400240Floorbeam · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK .3125 INCH CRACK WAS FOUND IN LT CENTER CABIN FLOOR PANEL SUPPORT CHANNEL AT BS 540, BL -0-, WL 208. MAINTENANCE REMOVED CRACKED FLOOR CHANNEL AT BS 540, FROM BL -0- TO LBL 25, WL 208; FABRICATED A NEW REPLACEMENT CHANNESDR AWXA200400239Floorbeam · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK .25 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL SUPPORT CHANNEL AT BS 540, RBL 45, WL 208. MAINTENANCE REMOVED CRACKED FLOOR CHANNEL AT BS 540, FROM RBL 25 TO RBL 45, WL 208; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLEDSDR AWXA200400237Floorbeam · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK .25 INCH CRACK WAS FOUND IN CABIN FLOOR PANEL SUPPORT CHANNEL AT BS 540, LBL 45, WL 208. MAINTENANCE REMOVED CRACKED FLOOR CHANNEL AT BS 540, FROM LBL 25 TO LBL 45, WL 208; FABRICATED A NEW REPLACEMENT CHANNEL; INSTALLEDSDR AWXA200400198Connector · loosePHX - EMERGENCY LANDING - FLT 0769 - ON APPROACH INTO PHX EN ROUTE FROM MZT TRAILING EDGE FLAPS WENT ASYMMETRIC BETWEEN FLAP POSITION 1 & 2. ABORTED APPROACH AND RECYCLED FLAPS WITH SAME RESULTS, ACCOMPLISHED TRAILING EDGE FLAP ASYMMETRICAL CHECKLIST AND AS ASDR AWXA200400171Shaft · shearedDURING FULL THRUST TAKEOFF OAT AT 13 DEG, NR 2 ENG EXCEEDED MAX EGT LIMIT, RED EGT WARNING LIGHT ILLUMINATED & EGT 947 DEG FOR 5 SECONDS. ON CLIMB NR 2 ENG RAN 105 DEG HOTTER THAN NR 1 AT 877 DEG. AT CRUISE NR 2 ENG 100 DEG HOTTER THAN NR 1 AT 716 DEG. MX R
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