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 AWXA200500959Frame · crackedDURING C18 CHECK DISCOVERED FRAME CRACKED, .17 INCHES IN LENGTH, UNDER DOOR ASSIST HANDLE AT THE R2 DOOR, BS 954, STR14R. MAINTENANCE TRIMMED OUT CRACK AT DOOR ASSIST HANDLE AT THE R2 DOOR, BS 954, STR 14R IAW AMERICA WEST AIRLINES (AWA) ENGINEERING REPAIR (ESDR AWXA200500924Spoiler · debondedDURING C18 CHECK FOUND A DISBOND AREA ON THE UPPER SURFACE OF THE NR 4 SPOILER, 36" FROM INBOARD END FROM WBL 123.75 TO WBL 135.75. MAINTENANCE REMOVED DISBOND AREA FROM THE UPPER SURFACE OF THE NR 4 SPOILER, 36" FROM INBOARD END IAW BOEING 737-300 SRM. FABRSDR AWXA200500918Clip · crackedDURING C18 CHECK FOUND SEVERAL CLIPS CRACKED LOCATED AT BS 380, STRINGER 1 (1.5" LONG), STRINGER 2R (1.5" LONG) AND STRINGER 8L (.26" LONG). MAINTENANCE REMOVED CRACKED CLIPS AT BS 380, STRINGER 1, STRINGER 2R AND STRINGER 8L IAW BOEING 737-300 SRM 51-40-02-0SDR AWXA200500916Clip · crackedDURING C18 CHECK DISCOVERED ATTACH CLIP AT BS 500A, STRINGER 16R CRACKED .275 INCHES IN LENGTH. MAINTENANCE REMOVED CRACKED CLIP AT BS 500A, STRINGER 16R. RECEIVED AND PREPARED NEW STRINGER CLIP FOR INSTALLATION IAW BOEING 737-300 SRM 51-40-05-0 FIG 2 & 3. SDR AWXA200500994Skin · crackedMCN - DURING C18 CHECK DISCOVERED, 4 CRACKS IN THE NR 2 SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK, FROM SS 90 TO SS 164. MAINTENANCE REMOVED DAMAGED AREA OF NR 2 SLAT SKIN BELOW THE INBOARD AUXILIARY TRACK, FROM SS 90 TO SS 164 IAW BOEING 737-300 SRM 57-43SDR AWXA200500993Skin · crackedDURING C18 CHECK DISCOVERED, THE NR 3 SLAT SKIN AT OUTBOARD END, SS 124, CRACKED .375 INCHES IN LENGTH. MAINTENANCE REMOVED DAMAGED AREA OF THE NR 3 SLAT SKIN IAW BOEING 737-300 SRM 57-43-01-2. FABRICATED FILLER AND SPLICE PLATE IAW BOEING 737-300 SRM 52-43-SDR AWXA200500925Tab · delaminatedDURING C18 CHECK DISCOVERED, THE LT HORIZONTAL ELEVATOR TAB DELAMINATED, AT OUTBOARD END, TOP SURFACE FROM ES 127L TO ES 129L. MAINTENANCE CUT OUT DELAMINATED AREA ON THE LT HORIZONTAL ELEVATOR TAB IAW BOEING 737-300 SRM 51-70-17-0 FIG 11. SANDED AND CLEANEDSDR AWXA200500922Frame · crackedDURING C18 CHECK DISCOVERED ANGLE CRACKED, .375 INCHES IN LENGTH, AT FORWARD UPPER CORNER OF THE R1 DOOR, CUTOUT. MAINTENANCE CUT OUT CRACKED AREA OF FRAME ANGLE IAW BOEING 737-300 SRM 51-70-11-0. FABRICATED FILLER AND DOUBLER IAW BOEING 737-300 SRM 51-70-11SDR AWXA200500915Skin · crackedDURING C18 CHECK DISCOVERED FUSELAGE SKIN CRACK, 1.43 INCHES IN LENGTH, AT BS 727E+4 INCHES, STRINGER 24R. MAINTENANCE CUT OUT DAMAGED AREA OF SKIN AT BS 727E+4 INCHES, STRINGER 24R IAW BOEING 737-300 SRM 53-00-01-3 FIG 229. FABRICATED DOUBLER, TRIPLER AND SDR AWXA200500909Clip · crackedDURING C18 CHECK DISCOVERED CLIP CRACKED, .375 INCHES IN LENGTH, AT BS 336 STRINGER 6R. MAINTENANCE REMOVED CRACKED CLIP AT BS 336 STRINGER 6R IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED NEW CLIP IAW BOEING 737-300 DWG 65-45874 AND BOEING 51-30-01-0 SDR AWXA200500907Stringer Clip · crackedDURING C18 CHECK DISCOVERED STINGER CLIP CRACKED, .200 INCHES IN LENGTH, AT BS 277, STRINGER 10R. MAINTENANCE REMOVED STRINGER CLIP AT BS 277, 10RT IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. FABRICATED NEW STRINGER CLIP IAW BOEING DWG 65-45805. MAINTENANCE INSDR AWXA200500930Frame · crackedDURING C18 CHECK DISCOVERED R1 DOOR FORWARD STOP CUTOUT, FOURTH FROM TOP, CRACKED, .60 INCHES IN LENGTH. MAINTENANCE TRIMMED OUT CRACK AREA AT R1 DOOR FORWARD STOP CUTOUT, FOURTH FROM TOP IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5200-5214-SS1. FABRSDR AWXA200500921Strap · crackedDURING C18 CHECK DISCOVERED STABILIZER STRAP CRACKED, .65 INCHES IN LENGTH, ON CABIN FLOOR AT BS 330, BL 15L, WL 204. MX STOP DRILLED CRACK IN STABILIZER STRAP AT BS 330, BL 15L, WL 204 IAW BOEING 737-300 SRM 53-10-51-2. FABRICATED REPAIR PLATE IAW BOEING 7SDR AWXA200500917Wedge · delaminatedDURING C18 CHECK DISCOVERED LT INBOARD FORE FLAP LOWER SURFACE DELAMINATED, AT THE INBOARD TRACK ATTACHMENT. MAINTENANCE REMOVED DAMAGED AREA ON THE LT INBOARD FORE FLAP LOWER SURFACE AND CLEANED AREA IAW BOEING 737-300 SRM 51-70-10. FABRICATED FILLER AND DOSDR AWXA200500914Wedge · delaminatedMCN - DURING C18 CHECK, DISCOVERED THE LT OUTBOARD AFT FLAP DELAMINATED AT THE INBOARD END OF THE UPPER AND LOWER SURFACES AT WBL 23.68 TO WBL 235.68. MAINTENANCE REMOVED DAMAGED AREA ON THE LT OUTBOARD AFT FLAP AND PREPARED FOR REPAIR IAW BOEING 737-300 SRM SDR AWXA200500805Handle · stuckDURING CLIMB OUT OF DFW EN ROUTE TO PHX GEAR HANDLE WOULD NOT GO PAST CENTER POSITION AFTER DEPARTURE, GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO DFW WITHOUT FURTHER INCIDENT. AIRCRAFT WAS FERRIED BACK TO PHX AND IS CURRENTLY BEING TROUBLESHOT. MAINTENANCSDR AWXA200500932Structure · crackedDURING C18 CHECK DISCOVERED SEVERAL SUBSTRUCTURES CRACKED AT THE L1 FWD ENTRY DOOR CUTOUT FROM STR 15L TO STR 16L, BS 348.20. MX REMOVED ALL DAMAGED PARTS, (1) CLIP CRACKED .5", (2) CLIP CRACKED .5", (3) CLIP CRACKED .5", (4) CLIP CRACKED .5" IAW AMERICA WESTSDR AWXA200500770Flashlight · inoperativeDURING GROUND HANDLING FLIGHT ATTENDANT REPORTED AFT OUTBOARD CABIN EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED OUTBOARD AFT FLIGHT ATTENDANT FLASHLIGHT. OPERATIONAL CHECKS GOOD.SDR AWXA200500673Warning System · malfunctionedLAS - ABORTED TAKEOFF - FLT 879 - DURING TAKEOFF, WHEN THROTTLES WERE ADVANCED FOWARDED RECIEVED TAKEOFF WARNING ALERT FOR STABILIZER TRIM OUT OF GREEN BAND. ABORTED TAKEOFF AND PUT STAB TRIM BACK IN GREEN BAND. TOOK OFF FROM LAS WITHOUT FURTHER INCIDENT.SDR AWXA200500644Warning System · malfunctionedAFTER T/O & EN ROUTE, RECEIVED RT MLG RED & GREEN LIGHT INDICATION. ON APPROACH, AFTER LOWERING GEAR ALL THREE LIGHTS INDICATED GREEN. AFTER LANDING MX PINNED GEAR FOR TAXI TO GATE. MX CYCLED GEAR 5 TIMES COULD NOT DUPLICATE PROBLEM. AS A PRECAUTION REPLACSDR AWXA200500641Warning Light · false activationFLT 440 - ON TAKEOFF ROLL AT LAS EN ROUTE TO IAH, A LOW SPEED ABORTED TAKEOFF OCCURRED DUE TO A REPORT OF A TAKEOFF CONFIGURATION WARNING HORN SOUNDED AT THROTTLE ADVANCEMENT. MAINTENANCE PERFORMED A TAKEOFF SYSTEM WARNING TEST IAW AWA TASKCARD NR A1B31009. SDR AWXA200500586Heating Element · shortedLAS - AIR TURN BACK - FLT 797 - ON CLIMB-OUT FROM LAS EN ROUTE TO PDX FLIGHT ATTENDANT REPORTED SMOKE AND A LOUD POP FROM THE FWD COFFEEMAKER. MAINTENANCE DISCOVERED THE WATER HEATER ELEMENT SHORTED. MAINTENANCE REMOVED COFFEEMAKER AND COLLARED CIRCUIT BREAKSDR AWXA200500580Odor · detectedBUR - BURNING SMELL - IMMEDIATELY AFTER TAKEOFF PILOTS REPORTED NOTICEABLE SMELL OR ODOR OF SMOKE. SMELL APPEARED TO DISSIPATE RAPIDLY THEREAFTER. NOTHING REPORTED EN ROUTE. MAINTENANCE REMOVED AND REPLACED THE RECIRCULATION FILTER IAW AWA TASKCARD S2B21003. SDR AWXA200500499Indicator · malfunctionedPHX - ABORTED TAKEOFF - FLT 0583 - ON TAKEOFF ROLL AT PHX EN ROUTE FOR GEG CAPTAINS AIRSPEED INDICATOR AT 200 KTS AND CLIMBING RAPIDLY WITH OFF FLAG, FIRST OFFICERS AIRSPEED INDICATOR AT 80 KTS, REJECTED TAKEOFF AT 90 KTS AND RETURNED TO GATE. MAINTENANCE REMSDR AWXA200500433Wire · backed outPHX - EEL - DURING 4-DAY CHECK FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 2 LT INOPERATIVE. MAINTENANCE FOUND WIRE PULLED OUT OF RECEPTACLE WITH EVIDENCE OF ARCHING. REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 2 LT, OPERATIONAL WAS GSDR AWXA200500366Screw · faultyABQ - EMERGENCY EQUIPMENT FAILURE - FLT 0757 - DURING DESCENT INTO ABQ FOR CAPTAINS WINDSHIELD FAILURE WITH CREW OXYGEN MASKS DONNED, THE CAPTAINS MASK BECAME FOGGED UP. WHEN EMERGENCY POSITION WAS SELECTED ON THE MASK AIRFLOW AND ABILITY TO SPEAK WERE INHIBISDR AWXA200500338Battery · dischargedSNA - EMERGENCY EQUIPMENT - DURING A-01 CHECK FOUND THE AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200500022Packing · tornLAS - DIVERSION - FLT 0765 - APPROXIMATELY 20 MINUTES OUT OF PHX EN ROUTE TO SMF NOTICED HYDRAULIC FLUID LEAKING FROM THE TOP OF LEFT WING, ALSO OBSERVED B-SYSTEM HYDRAULIC QUANTITY DECREASING, FLUID LEVEL STABILIZED AT 1/2 QUANTITY ON INDICATOR, DIVERTED INTOSDR AWXA200500001Wire · brokenPHX - EEL - DURING INSPECTION FOUND BROKEN WIRES AT EMERGENCY ESCAPE PATH LIGHT SEAT ROW 12 LT. MAINTENANCE REPLACED EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200401383Battery · dischargedPHX - EMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE FORWARD BULKHEAD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FORWARD BULKHEAD EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400992Skin · crackedDURING 4-DAY CHECK A 3 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 727E, STR 23 LT, APPROXIMATELY 18 INCH AFT OF EXTERIOR EMERGENCY EXIT LIGHT. MAINTENANCE CUTOUT CRACKED AREA OF SKIN AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACK EXISTS. REMOVED SDR AWXA200400913Panel · crackedDURING C-19 CHECK 6 EACH CRACKS WERE FOUND IN NR 6 SPOILER LOWER SKIN, WS 294 TO WS 306. MAINTENANCE CUT OUT DAMAGE IN NR 6 SPOILER LOWER SKIN, WS 294 TO WS 306; FABRICATED A FILLER AND DOUBLER; BONDED REPAIR PARTS TO SPOILER IAW B737-300 SRM 51-70-10 FIG 30.SDR AWXA200400891Intercostal · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A 2 INCH CRACK WAS FOUND IN INTERCOSTAL AT RBL 50, BETWEEN BS 344 AND BS 360. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT RBL 50, FROM BS 344 TO BS 360; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45834; INSTALLEDSDR AWXA200400877Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON LOWER SURFACE UPPER AFT LEG OF FLOORBEAM UPPER CHORD AT BS 294, RBL 13, WL 208. MAINTENANCE CUT OUT DAMAGE ON FLOORBEAM UPPER CHORD AT BS 294, FROM LBL 22 TO RBL 23; FABRICATED A NEW REPLACEMENT SESDR AWXA200400868Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON FLOORBEAM UPPER CHORD AT BS 328 BETWEEN RBL 12 AND RBL 52, WL 208. MAINTENANCE REMOVED CORRODED FLOORBEAM UPPER CHORD AT BS 328 FROM RBL 12 TO RBL 52, WL 208; FABRICATED A NEW REPLACEMENT FLOORBEAMSDR AWXA200400863Skin · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK A PREVIOUS REPAIR ON LOWER SURFACE OF RT AILERON WAS FOUND DELAMINATED AT WBL 480.5. MAINTENANCE REMOVED EXISTING REPAIR ON LOWER SURFACE OF RT AILERON AT WBL 480.5; CLEANED AND PREPARED AREA; FABRICATED NEW REPAIR PLIESSDR AWXA200400862Strap · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A 2 INCH CRACK WAS FOUND IN STRAP ON BOTTOM OF BEAM AT BS 312, RBL 33, WL 200. CRACK IS ENTIRE WIDTH OF STRAP; STOP DRILL IS NOT REQUIRED. FABRICATED A REPAIR PLATE AND INSTALLED REPAIR PART IAW B737-300 SRM 53-10-51 FISDR AWXA200400844Stringer Clip · crackedMAJOR REPAIR, DURING C-19 CHECK A 1 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 500A, STR 16 RT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 500A, STR 16 RT; FABRICATED A NEW REPLACEMENT TIE CLIP IAW DWG 69-35350; INSTALLED REPAIR PART IAW B737-30SDR AWXA200400878Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-19 CHECK CORROSION WAS FOUND ON FLOORBEAM AT BS 986, BETWEEN LBL 25 AND LBL 31, WL 208. MAINTENANCE REMOVED UPPER CHORD OF FLOORBEAM AT BS 294, FROM LBL 51 TO RBL 10; FABRICATED A NEW REPLACEMENT SECTION OF UPPER CHORD; INSTALLEDSDR AWXA200400866Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-19 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT BETWEEN BS 950 AND BS 966, LBL 18, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 950 TO BS 966, LBL 18, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSDR AWXA200400865Floor Support · corrodedMCN - MAJOR REPAIR - DURING C-19 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT BETWEEN BS 954 AND BS 966, RBL 18, WL 208. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT FROM BS 945 TO BS 966, RBL 18, WL 208; FABRICATED A NEW REPLACEMENT FLOOR SUPPORT; INSTASDR AWXA200400888Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK A .75 INCH CRACK WAS FOUND IN STRINGER TIE CLIP AT BS 294.5, STR 11 LT. MAINTENANCE REMOVED AND REPLACED STRINGER TIE CLIP AT BS 294.5, STR 11 LT IAW B737-300 SRM 51-40-02 FIG 8 & 12.SDR AWXA200400880Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 2 EACH CRACKS WERE FOUND IN NR 3 SLAT LOWER SKIN BELOW AUXILIARY TRACK. MAINTENANCE CUT OUT DAMAGED AREA OF NR 3 SLAT LOWER SKIN; FABRICATED A FILLER AND SPLICE PLATE; INSTALLED REPAIR PARTS IAW B737-300 SRM 57-43-01 FIGSDR AWXA200400859Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK THE LT OUTBOARD FLAP WAS FOUND SEPARATED AT THE AFT INBOARD CORNER, WATER WAS FOUND LEAKING FROM INSIDE FLAP AT SEPARATED SKIN, WBL 230.68 TO WBL 231.68. MAINTENANCE CUT OUT DAMAGED AREA OF LT OUTBOARD FLAP SKIN AT AFT ISDR AWXA200400894Connector · damagedMCN - EEL - DURING C-19 CHECK MAINTENANCE DISCOVERED NUMEROUS DAMAGED CONNECTORS AND SPLICES ON EMERGENCY ESCAPE PATH LIGHT HARNESS LT SIDE OF CABIN. REMOVED AND REPLACED DAMAGED CONNECTORS AND SPLICES LT SIDE OF CABIN, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400864Wedge · delaminatedMCN - MAJOR REPAIR - DURING C-19 CHECK A DISBOND AREA WAS FOUND ON UPPER SURFACE OF LT OUTBOARD FORE FLAP 106.5 INCHES FROM OUTBOARD END. MAINTENANCE REMOVED DAMAGED ON UPPER SURFACE OF LT OUTBOARD FORE FLAP FROM WBL 307.11 LT TO 413.61 LT; CLEANED AND PREPARSDR AWXA200400803Wire Harness · brokenDURING 8-DAY CHECK, FOUND WIRES PULLED OUT FROM EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 19 LT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 19 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200400892Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 4 EACH .5 INCH CRACKS WERE FOUND AT RIVET HOLES IN NR 4 SLAT BETWEEN SLAT STA 64.25 AND 78.25. MAINTENANCE CUT OUT CRACKS IN NR 4 SLAT 45.5 TO 61.5 INCHES FROM INBOARD END; FABRICATED A FILLER AND SPLICE PLATE; INSTALLEDSDR AWXA200400889Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 2 EACH .5 INCH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN NR 6 SLAT INBOARD AUXILIARY GUIDE ATTACH AREA 42 INCHES AND 45 INCHES FROM INBOARD END. MAINTENANCE CUT OUT CRACKED NR 6 SLAT SKIN 42 INCHES TO 57 INCHES FROSDR AWXA200400881Skin · crackedMCN - MAJOR REPAIR - DURING C-19 CHECK 5 EACH CRACKS WERE FOUND EMANATING FROM RIVET HOLES IN SKIN AT NR 5 SLAT ACTUATOR ATTACHMENT AREA. MAINTENANCE CUT OUT DAMAGED AREA OF NR 5 SLAT SKIN 42 INCHES TO 51 INCHES FROM INBOARD SIDE; FABRICATED A FILLER AND SPLI
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