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 AWXA200301303Indicator · inaccuratePHX - - FLT 0769 - ON TAKEOFF ROLL OUT OF PHX EN ROUTE FOR SMF NR 1 ENGINE OIL PRESSURE WAS LOW, REJECTED TAKEOFF, ON TAXI BACK TO GATE OIL PRESSURE RETURNED TO NORMAL. MAINTENANCE INSPECTED THE NR 1 ENGINE OIL PRESSURE WIRING, NO DISCREPANCIES WERE NOTED, RESDR AWXA200301126Charger · inoperativeLAX - EEL - DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE AT SEAT ROWS 1 - 5 LT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY CHARGER, OPERATIONAL CHECK WAS GOOD.SDR AUS20030972Drain Valve · leaking(AUS) FORWARD TOILET DRAIN VALVE LEAKING. FOUND DURING INSPECTION IAW AD/737/25.SDR AWXA200300999Charger · faultyON CLIMB OUT OF PHX EN ROUTE FOR SFO FLIGHT ATTENDANTS DETECTED AN ODOR IN CABIN LIKE BURNING HAIR, TURNED BACK TO PHX. MAINTENANCE T/S AND FOUND D2936 BATTERY PROTECTION CIRCUIT OPEN, REPAIRED CONNECTION AND REMOVED AND REPLACED MAIN BATTERY AND BATTERY CHARGSDR AWXA200300940Flashlight · inoperativeEMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300929Receptacle · corrodedDOOR EXTERIOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED LENS COVER AND FOUND RECEPTACLE HALF FULL WITH WATER, PLACED ON MEL 33-14, COND. 1, (EXTERIOR EMERGENCY LIGHT INOP). IN PHX ON 07/17/2003, MAINTENANCE REMOVED AND REPLACED THE R-1 DOSDR AWXA200300868Blade · damagedFORIEGN OBJECT DAMAGE WAS FOUND ON THE NR 2 ENGINE FAN BLADES. MAINTENANCE PERFORMED A FOD INSPECTION OF THE NO. 2 ENGINE IAW T/C I8M05030, AND BORESCOPED THE HIGH PRESSURE TURBINE (HTP) IAW T/C I5M72017, NO DAMAGE WAS NOTED TO HPT. REMOVED AND REPLACED ALL FSDR AWXA200300816Skin · crackedPHX - MAJOR REPAIR - DURING INSPECTION A CRACK WAS FOUND ON FUSELAGE SKIN AT BS 520, BETWEEN STRINGER 12-13 LT. MAINTENANCE CUT OUT DAMAGE AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER; INSTALLED REPAIR PART IAW B737-3SDR AWXA200300808Indicator · malfunctionedON APPROACH WHEN FLAP EXTENDED TO 5 DEG, FLAP INDICATOR SPLIT AT 2 DEG, FORWARD AND OVERHEAD PANELS WERE GREEN, RETURNED FLAPS TO 1 DEG AND NEEDLES REMAINED SPLIT FOR APPROX 10 MIN THEN REALIGNED AT 1 DEG. SELECTED FLAPS TO 5 DEG AND SYSTEM OPERATED NORMALLY.SDR AUS20030663Spar · corroded(AUS) RT WING AFT SPAR LOWER SECTION CONTAINED LEVEL 2 CORROSION IN AREAOF RH WING VENT TANK LOCATED BETWEEN WS557 AND WS583. FOUND DURING INSPECTION IAW A-B73-5791-51.SDR AUS20030661Skin · corroded(AUS) RT WING UPPER SKIN LOWER SURFACE AND STIFFENERS CONTAINED LEVEL 2 CORROSION IN THE AREA OF THE RT WING VENT TANK BETWEEN WS557 AND WS583. FOUND DURING INSPECTION IAW A-B73-5791-51.SDR AUS20030687Blade · fod(AUS) NR 1 ENGINE SEVENTH STAGE COMPRESSOR BLADES DAMAGED BY FOD.SDR AUS20030686Compressor · fod(AUS) NR 2 ENGINE COMPRESSOR SIXTH, SEVENTH AND EIGHTH STAGES CONTAINED SUBSTANTIAL FOD DAMAGE.SDR AWXA200300707Actuator · erraticON DEPARTURE, FUEL CROSSFEED VALVE BECAME UN CONTROLLABLE CYCLING TO OPEN AND CLOSED POSITION ON ITS OWN. DISAGREEMENT LIGHT ILLUMINATED IN BOTH SWITCH POSITIONS, TURNED BACK AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE REMOVED AND REPLACED THE FUEL CROSSFEESDR AWXA200300690Wire · brokenPHX - EEL - DURING INSPECTION THE EMERGENCY PATH LIGHTING DID NOT ILLUMINATE AT L1 & R1 DOORS, AND SEAT ROWS 1-4. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY EXIT LIGHTING POWER SUPPLY AND REPAIRED A BROKEN WIRE AT POWER SUPPLY CONNECTOR. OPERATIOSDR AWXA200300688Battery · dischargedDURING INSPECTION THE EMERGENCY EXIT LIGHTS IN AFT CABIN WERE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY EXIT LIGHT POWER SUPPLY IN AFT CABIN, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300677Skin · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK 7 EACH .25 INCH CRACKS WERE FOUND ON FUSELAGE INTERIOR SKIN AT FASTENER HOLES ON LOWER ROW LAP SEAM STR 4 LT, BETWEEN BS 500B+9 AND BS 500B+19. UPON BOEING REQUEST TO EXTEND THE INSPECTION 1 EACH ADDITIONAL CRACK INDICATSDR AWXA200300657Skin · crackedDURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON SKIN AT LOWER ROW OF FASTENER HOLES STR 4 LT, BS 373. MAINTENANCE CUT OUT CRACKED SKIN AT STR 4 LT, BETWEEN BS 373 AND BS 377; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED 2 EACH DSDR AWXA200300655Skin · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK 3 EACH .25 INCH CRACKS WERE FOUND ON SKIN AT LOWER ROW OF FASTENER HOLES STR 4 RT, BS 500B+1, BS 500B+2, AND BS 500B+15. MAINTENANCE CUTOUT AND REMOVED CRACKED SKIN AT STR 4 RT, BETWEEN BS 500A+18 & BS 500B+4, AND BS 500SDR AWXA200300656Skin · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON SKIN AT LOWER ROW OF FASTENER HOLES STR 4 RT, BS 431. MAINTENANCE CUTOUT CRACKED SKIN AT STR 4 RT, BETWEEN BS 428 AND BS 432; PERFORMED A HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST;SDR AWXA200300672Rib · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON LT WING AFT RIB, WBL 135.5. MAINTENANCE CUT OUT CRACKED LT WING AFT RIB AT WBL 135.5; PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A NEW SECTION OF RIB AND 2 EACH REPAIR ASDR AWXA200300668Rib · crackedDURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON LT WING RIB AT WBL 135.5. MAINTENANCE CUT OUT DAMAGED AREA OF LT WING RIB AT WBL 135.5; FABRICATED A NEW SECTION OF AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW ER 03-5723-03149-TB1.SDR AWXA200300666Stringer · crackedDURING C-17 CHECK 2 EACH 1 INCH CRACKS WERE FOUND AT BOTH SIDES OF LIGHT HOUSING ON STRINGER 16 LT, BS 500C&D. MAINTENANCE CUTOUT DAMAGE AT BOTH SIDES OF LIGHT HOUSING ON STRINGER 16 LT, BS 500C&D; FABRICATED A REPAIR CHANNEL, 2 EACH SPLICE ANGLES, AND 4 EACHSDR AWXA200300665Stringer · crackedDURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON FORWARD SIDE OF STRINGER END AT BS 500C, STR 16 RT. MAINTENANCE CUT OUT DAMAGED SECTION OF STRINGER AT BS 500C, STR 16 RT; FABRICATED A REPAIR CHANNEL AND 2 EACH SPLICE ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SDR AWXA200300664Floorbeam · corrodedLCQ - MAJOR REPAIR - DURING C-17 CHECK CORROSION WAS FOUND AT FASTENERS ON FLOORBEAM AT BS 986.5, LBL 25. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED DAMAGED SECTION OF UPPER TEE AT BS 986.5, LBL 25; FABRICATED A NEW REPSDR AWXA200300667Skin · crackedDURING C-17 CHECK 2 EACH 1 INCH CRACKS WERE FOUND AT FASTENER HOLES ON NR 2 SLAT LOWER LEADING EDGE. MAINTENANCE CUTOUT DAMAGED AREA NR 2 SLAT LOWER LEADING EDGE; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 PG 216-219 FIGSDR AWXA200300663Frame · crackedDURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON OUTBOARD FLANGE OF FRAME AT BS 400, STR 14 RT. MAINTENANCE CUTOUT CRACK ON OUTBOARD FLANGE OF FRAME AT BS 400, STR 14 RT, AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A SHEAR TIE AND DOUBSDR AWXA200300691Failsafe · crackedLCQ - FLIGHT CONTROL - DURING C-17 CHECK A 2 INCH CRACK WAS FOUND ON RT WING OUTBOARD FLAP, INBOARD FLAP TRACK, AT WBL 254. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FILLER WELDED STOP DRILL HOLE; GRINDED WESDR AWXA200300660Bulkhead · crackedDURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 1.0, WL 192. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT RBL 1.0, WL 192 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER; INSTASDR AWXA200300651Bulkhead · crackedDURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 7, WL 198.5-199.5. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW SRM 53SDR AWXA200300661Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 6.5, WL 222-233.5. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT RBL 6.5, WL 222-233.5 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED SDR AWXA200300659Bulkhead · crackedDURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 1.0, WL 192. MAINTENANCE CUT OUT CRACK ON BS 178 BULKHEAD WEB AT LBL 1.0, WL 192 AND PERFORMED A HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR DOUBLER AND FILLER; INSTASDR AWXA200300658Bulkhead · crackedDURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT RBL 5.7, WL 212.5-213.5. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK IS CONTAINED; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PART IAW B737-3SDR AWXA200300650Bulkhead · crackedDURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT LBL 4.7, WL 201-202. MAINTENANCE STOP DRILLED CRACK AND PERFORMED A HFEC INSPECTION TO VERIFY CRACK WAS CONTAINED; FABRICATED A DOUBLER AND 2 EACH FILLERS; INSTALLED REPAIR PARTS IAW SRM 5SDR AWXA200300596Skin · crackedDURING C-17 CHECK 9 EACH CRACKS WERE FOUND ON LOWER ROW OF FASTENERS OF LAP SEAM AT BS 492 - BS 502, STR 4 RT. MAINTENANCE REMOVED FASTENERS AT STR 4 RT BETWEEN BS 485 AND BS 508; CUTOUT DAMAGED AREA OF FUSELAGE SKIN FROM BS 487.5 TO BS 506.5; FABRICATED 3 EACSDR AWXA200300552Oxygen Mask · misinstalledMCN - EMERGENCY EQUIPMENT - DURING C-17 CHECK OF EMERGENCY OXYGEN SYSTEM THE PASSENGER SERVICE UNIT OXYGEN MASK AT SEAT ROW 19 LT FAILED DROP CHECK. MAINTENANCE FOUND OXYGEN MASK LANYARD AT SEAT ROW 19 LT MISROUTED, CORRECTLY ROUTED LANYARD, DROP TEST WAS GOOSDR AWXA200300676Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK .1875 INCH CRACK WAS FOUND ON SIDE ANGLE AT L-1 DOOR CUTOUT, BS 344, STR 16 LT. MAINTENANCE REMOVED CRACKED SIDE ANGLE AT L-1 DOOR CUTOUT, BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-16970; INSTALLEDSDR AWXA200300674Strap · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK .1875 INCH CRACK WAS FOUND ON STRAP AT L-1 DOOR CUTOUT, BS 344, STR 16 LT. MAINTENANCE REMOVED CRACKED STRAP AT L-1 DOOR CUTOUT, BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT STRAP PER DWG 65-17685; INSTALLED REPAIR PASDR AWXA200300673Angle · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK .1875 INCH CRACK WAS FOUND ON ANGLE AT L-1 DOOR CUTOUT, BS 344, STR 16 LT. MAINTENANCE REMOVED CRACKED ANGLE AT L-1 DOOR CUTOUT, BS 344, STR 16 LT; FABRICATED A NEW REPLACEMENT ANGLE PER DWG 69-26555; INSTALLED REPAIR PASDR AWXA200300525Clip · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A .25 INCH CRACK WAS FOUND ON AFT LOWER WEB CLIP AT L-1 DOOR CUTOUT BS 344, STR 16 LT. MAINTENANCE REMOVED CRACKED AFT LOWER WEB CLIP AT L-1 DOOR CUTOUT BS 344, STR 16; FABRICATED AND NEW REPLACEMENT WEB CLIP; INSTALLED SDR AWXA200300470Light · missingSJC - EEL - FLIGHT CREW REPORTED THE R-2 DOOR EMERGENCY EXIT LIGHT WAS MISSING. MAINTENANCE REPLACED THE R-2 DOOR EMERGENCY EXIT LIGHT ASSEMBLE, OPERATIONAL CHECK WAS GOOD.SDR AWXA200300487Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-17 CHECK A .75 INCH CRACK WAS FOUND ON STRINGER TIE CLIP IN AFT CARGO COMPARTMENT AT BS 727D, STR 23 LT. MAINTENANCE REMOVED DAMAGED STRINGER TIE CLIP AT BS 727D, STR 23 LT; FABRICATED A NEW REPLACEMENT TIE CLIP; INSTALLED REPAIRSDR AWXA200300486Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD FLOOR WEB AT WL 207, LBL 24. MAINTENANCE REMOVED CRACKED FLOOR WEB BS 178 BULKHEAD, WL 207, LBL 24, AND DISCOVERED A CRACKED ATTACH ANGLE. REMOVED CRACKED ATTACH ANGLE; FABRICSDR AWXA200300484Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT WL 213, LBL 11. MAINTENANCE STOP DRILLED CRACK AND CUT OUT CRACKED AREA OF BS 178 BULKHEAD WEB AT WL 213, LBL 11; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FASDR AWXA200300483Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT WL 210, RBL 6. MAINTENANCE STOP DRILLED CRACK AND CUT OUT CRACKED AREA OF BS 178 BULKHEAD WEB AT WL 210, RBL 6; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRSDR AWXA200300482Bulkhead · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A CRACK WAS FOUND ON BS 178 BULKHEAD WEB AT WL 207, LBL 11. MAINTENANCE STOP DRILLED CRACK AND CUT OUT CRACKED AREA OF BS 178 BULKHEAD WEB AT WL 207, LBL 11; PERFORMED HFEC INSPECTION TO VERIFY NO CRACKS EXIST; FABRICATESDR AWXA200300462Skin · crackedDURING C-17 CHECK 3 EACH 2 INCH CRACKS WERE FOUND ON NR 3 SLAT SKIN AT FASTENER HOLES ABOVE OUTBOARD AUXILIARY TRACK (HFEC VERIFIED). MAINTENANCE CUTOUT CRACKED SECTION OF NO. 3 SLAT SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-3SDR AWXA200300537Skin · crackedDURING C-17 CHECK A .1875 INCH CRACK WAS FOUND AT FASTENER HOLE ON L-1 DOOR UPPER INNER SKIN BS 339, STR 9 LT. MAINTENANCE CUTOUT DAMAGE ON L-1 DOOR UPPER INNER SKIN BS 339, STR 9 LT; FABRICATED A REPAIR DOUBLER AND FILLER; INSTALLED REPAIR PARTS IAW B737-300SDR AWXA200300480Stringer · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND AT RIVET HOLES ON STRINGER 4 RT BS 908-909. MAINTENANCE REMOVED CRACKED STRINGER SPLICE ON STRINGER 4 RT BS 908-909; FABRICATED A NEW REPLACEMENT STRINGER SPLICE; INSTALLED REPAIR PART IAW B737-3SDR AWXA200300479Stringer · crackedLCQ - MAJOR REPAIR - DURING C-17 CHECK A 1 INCH CRACK WAS FOUND AT RIVET HOLES ON STRINGER 4 LT, BS 908-909. MAINTENANCE REMOVED 12 INCH SECTION OF STRINGER SPLICE ON STRINGER 4 LT, BS 908-909; FABRICATED A REPAIR CHANNEL PER DWG 65-51698-2; INSTALLED REPAIR
Back to Boeing 737-33A