Boeing 737-301
Service difficulty reports · 4,797
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 = '737301' 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 = '737301' 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 AWXA200500185Web · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF SHEAR WEB BETWEEN BS 1009 AND BS 1015, LBL 41 AND LBL 45, WL 207.5. MAINTENANCE REMOVED CORRODED SHEAR WEB FROM BS 1009 TO BS 1015, LBL 41 TO LBL 45; FABRICATED A NEW RSDR SB05013Wire · openBWI - MAINTENANCE REPORTED THE EMERGENCY LIGHT AT SEAT 4ABC INOPERATIVE. MAINTENANCE REPAIRED AN OPEN IN WIRING AT SEAT ROW 4ABC. OPERATIONAL CHECK GOOD.SDR AWXA200500335Channel · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN STRINGER SPLICE CHANNEL AT BS 360, STR 14 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE CHANNEL AT BS 360, STR 14 LT; FABRICATED A NEW REPLACEMENT SPLICE CHANNEL; INSTALLED REPAIR PART IAWSDR AWXA200500330Sill · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON R-1 DOOR SILL INNER CHORD BETWEEN BS 291 AND BS 356, RBL 59, WL 208. MAINTENANCE REMOVED CORRODED R-1 DOOR SILL INNER CHORD FROM BS 291 TO BS 356, RBL 59; FABRICATED A NEW REPLACEMENT CHORD PER DWGSDR AWXA200500313Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 344, BETWEEN RBL 12 AND LBL 50. MAINTENANCE REMOVED CORRODED SECTION OF FLOORBEAM UPPER CHORD AT BS 344, FROM RBL 12 TO LBL 50; FABRICATED A NSDR AWXA200500256Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 328, BETWEEN LBL 29 AND RBL 32, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 328, FROM LBL 35 TO RBL 67; FABRICATED A NEWSDR AWXA200500255Sill · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON L-1 DOOR SILL LOWER INNER CHORD AT LBL 58, BETWEEN BS 298 AND BS 343, WL 208. MAINTENANCE REMOVED DAMAGED SECTION OF L-1 DOOR SILL LOWER INNER CHORD AT LBL 58, FROM BS 298 TO BS 343; FABRICATED A NSDR AWXA200500254Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM UPPER CHORD AT BS 312, BETWEEN LBL 9 AND RBL 36, WL 208. MAINTENANCE CUT OUT DAMAGE IN FLOORBEAM UPPER CHORD AT BS 312, FROM LBL 9 TO RBL 36; FABRICATED A NEW RSDR AWXA200500237Stiffener · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK EXFOLIATION CORROSION WAS FOUND ON FLOOR SUPPORT STIFFENER AT RBL 11, BETWEEN BS 315 AND BS 326. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT STIFFENER AT RBL 11, FROM BS 315 TO BS 326; FABRICATED A NEW REPLACEMENT STIFFENSDR AWXA200500236Stiffener · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK GALVANIC CORROSION WAS FOUND ON FLOOR SUPPORT STIFFENER AT LBL 11, BETWEEN BS 331 AND BS 341. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT STIFFENER AT LBL 11, FROM BS 331 TO BS 341; FABRICATED A NEW REPLACEMENT STIFFENER SDR AWXA200500228Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN MAIN CABIN FRAME AT R-1 DOOR BS 294.5, STR 7 RT. MAINTENANCE CUT OUT CRACK IN FRAME AT R-1 DOOR BS 294.5, STR 7 RT; FABRICATED A FILLER AND REPAIR ANGLE; INSTALLED REPAIR PARTS IAW 51-70-11.SDR AWXA200500224Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN R-1 DOOR INNER WEB AT FORWARD END, AFT OF NR 4 DOOR STOP BS 328, RBL 60, WL 240. MAINTENANCE CUT OUT CRACK IN R-1 DOOR INNER WEB; FABRICATED A FILLER AND DOUBLER; INSTALLED REPAIR PARTS IAW SDR SB05010Sensor · faultyCMH - FLT 184 ON APPROACH TO CMH FROM CLT, CREW RECEIVED A NOSE LANDING GEAR RED UNSAFE LIGHT AFTER GEAR EXTENSION. A FLYBY OF THE TOWER CONFIRMED THE GEAR WAS DOWN. CREW CHECKED VIEWPORT AND STRIPES WERE ALIGNED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. ASDR AWXA200500227Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN FUSELAGE SKIN AT BS 874, A .5 INCH ABOVE STR 24 RT RIVET ROW. MAINTENANCE CUT OUT CRACK IN FUSELAGE SKIN AT BS 874, STR 24 RT; FABRICATED A DOUBLER; INSTALLED REPAIR PART IAW 53-00-10 FIG 229.SDR AWXA200500225Skin · delaminatedMCN - MAJOR REPAIR - DURING C-18 CHECK THE LOWER SURFACE SKIN OF THE NR 3 SLAT WAS FOUND DELAMINATED AT SLAT STA 14.5. MAINTENANCE REMOVED PREVIOUS REPAIR AND DAMAGED AREA OF LOWER NR 3 SLAT SKIN; FABRICATED A CORE FILLER AND EXTERNAL DOUBLER; BONDED REPAIR PSDR AWXA200500306Wire · brokenMCN - EEL - DURING C-18 CHECK BROKEN WIRES WERE FOUND AT MAIN CABIN FORWARD FLIGHT ATTENDANT STATION EMERGENCY EXIT LIGHT ASSEMBLY. MAINTENANCE REPLACED CONTACT PIN ON REMOVABLE SPLICE AT MAIN CABIN FORWARD FLIGHT ATTENDANT STATION EMERGENCY EXIT LIGHT, OPERASDR AWXA200500291Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A 1 INCH CRACK WAS FOUND IN FUSELAGE SKIN ON LT AFT SIDE OF WING TO BODY FAIRING BS 727E, STR 24 LT. MAINTENANCE CUT OUT DAMAGE IN FUSELAGE SKIN BS 727E, STR 24 LT; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKSSDR AWXA200500241Frame · crackedDURING C-18 CHECK A .75 INCH CRACK WAS FOUND IN R-1 DOOR AT 3RD STOP PIN BRACKET FROM THE BOTTOM ON AFT SIDE OF DOOR BS 328, STR 14 RT. MAINTENANCE TRIMMED OUT CRACK IN R-1 DOOR AT 3RD STOP PIN BRACKET FROM THE BOTTOM; FABRICATED A REPAIR DOUBLER; INSTALLED RSDR SWAA050096Skin · crackedDURING SCHEDULED C4 CHECK, FOUND 3 EACH FUSELAGE SKIN CRACKS BETWEEN BS 440 AND BS 480, STRINGER 10R. REPAIRED SKIN SECTIONS PER EA.SDR SWAA050095Bearing · wornDURING SCHEDULED C4 CHECK, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR BEARING AND SLEEVE ON LT CLEVIS PER MM.SDR SB05005Wire · faultyPHL - MAINTENANCE REPORTED SEVERAL EMERGENCY EXIT ROW LIGHTS INOPERATIVE. MAINTENANCE REPAIRED WIRING. OPERATIONAL CHECK OF EMERGENCY LIGHTS GOOD.SDR USAA050058Skin · crackedCLT - FOUND SKIN CRACKED 1 INCH, STATION 727D AT STRINGER 23L. INSTALLED DOUBLER IAW SRM 53-00-01. (M)SDR USAA050006Skin · crackedCLT - FOUND SLAT SKIN CRACKED 1 INCH, LOWER TRAILING EDGE OF SKIN, 6 INCHES OUTBOARD OF ACTUATOR ON THE NR 4 LE SLAT. INSTALLED DOUBLER. (M)SDR AWXA200500017Outflow Valve · malfunctionedEN ROUTE EXPERIENCED CABIN PRESSURE LOSS, DONNED O2 MASKS & EXECUTED EMERGENCY DESCENT. MANUALLY DEPLOYED CABIN O2 MASKS (MASKS WERE NOT USED), STANDBY & MANUAL DID NOT WORK, TRIED AGAIN LATER AND STANDBY DID WORK. LANDED AT PHX WITHOUT FURTHER INCIDENT, EMESDR SB05002Actuator · failedON CLIMB-OUT FROM CLT, ENROUTE TO DCA, CREW RECEIVED A RT MLG RED LIGHT AFTER GEAR RETRACTION. ALL OTHER GEAR LIGHTS WERE EXTINGUISHED. A SHORT TIME LATER, THE RT MLG GREEN LIGHT ILLUMINATED ALONG WITH THE RED LIGHT. CREW ACCOMP QUICK REF HANDBOOK PROCEDURES SDR SWAA050044Sensor · faultyLT MLG UNSAFE LIGHT ILLUMINATED IN FLIGHT. CYCLED GEAR HANDLE, NO HELP. REMOVED AND REPLACED LT MLG UPLOCK SENSOR PER MM.SDR SB05001Battery Pack · dischargedPVD - MAINTENANCE REPORTED THE AFT CABIN SEAT MOUNTED EMERGENCY LIGHTS DIM. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY PACK. OPERATIONAL CHECK GOOD.SDR USAA050043Reveal · crackedPIT - FOUND REVEAL CRACKED 2 INCHES, UPPER FORWARD CORNER FORWARD SERVICE DOOR REVEAL. REPLACED REVEAL PER EA 79744. (M)SDR SB04172Light · inoperativeCLT - PILOT REPORTED THE EMERGENCY EXIT LIGHT ON SEAT 10C WAS INOPERATIVE. MAINTENANCE INSTALLED A NEW LIGHT ASSEMBLY. OPERATIONAL CHECK NORMAL.SDR USAA041111Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, S-23R AT STATION 727D. INSTALLED DOUBLER IAW SRM 53-00-01. (M)SDR USAA041110Skin · crackedCLT - FOUND SKIN CRACKED 3 INCHES, S-19R AT STATION 767. INSTALLED DOUBLER IAW SRM 53-00-01. (M)SDR SB04168Windshield · arcedPHL - FLT1027 - ON CLIMB-OUT FROM PHL, AT 3,000 FEET, THE CAPTAIN'S L1 WINDSHIELD BEGAN TO ARC. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S L1 WINDSHIELD PER SDR AWXA200401418Keelbeam · crackedMCN - MAJOR REPAIR - DURING INSPECTION PHX MAINTENANCE FOUND A 3 INCH CRACK IN LT PACK BAY FORWARD END KEEL BEAM AT BS 540, CRACK RUNS HORIZONTALLY THROUGH MACHINED STEP. AIRCRAFT WAS MAINTENANCE FERRIED TO MCN FOR REPAIR. CUTOUT DAMAGED SECTION OF KEEL BEAMSDR AWXA200401396Light · shortedPHX - EEL - DURING INSPECTION FOUND THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 4 LT HAD SHORTED OUT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY ESCAPE PATH LIGHT ASSEMBLY AT SEAT ROW 4 L/H, OPERATIONAL CHECK WAS GOOD.SDR SB04167Control Unit · unreliablePIT FLT414 FLIGHT DEPARTED ORD, EN ROUTE TO PHL, WITH THE NR 2 GENERATOR ON MEL 24-1. DURING CRUISE, THE APU GENERATOR DROPPED OFF LINE, LEAVING ONLY THE NR 1 GENERATOR. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLAREDSDR SWAA043561Light · looseEEPLS STRIP FROM ROW 6 ABC TO ROW 8 ABC, LOOSE. SECURED EEPLS STRIP PER MM.SDR AWXA200401361Battery · dischargedLAS - EMERGENCY EQUIPMENT - DURING 8-DAY CHECK, THE AFT EMERGENCY FLASHLIGHT BATTERY WAS FOUND DEAD. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.SDR USAA041076Skin · crackedPIT - B-CHECK - SKIN, 3 INCH CRACK, STA 740, STR 18R. INSTALLED DOUBLER IAW SRM. (K)SDR USAA041030Skin · crackedPIT - B CK - SKIN, 3 INCH CRACK, SKIN AT STA 740, STR 18R. INSTALLED DOUBLER IAW SRM.SDR SWAA043545Skin · delaminatedDURING SCHEDULED SERVICE CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED RT OUTBOARD T/E AFT FLAP PER MM.SDR USAA041029Skin · chafedPIT - RON - L/E SKIN, .5 INCH X 4 INCH CHAFE MARK, LT OB MID FLAP L/E APPROX WBL 204 LT. INSTALLED REPAIR DOUBLER IAW SRM.SDR SB04161Duct · disconnectedMCO FLT1222 EN ROUTE FROM PBI TO DCA, AT FL370, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW COULD NOT CONTROL CABIN ALTITUDE AND BOTH PACKS WERE ACTING ABNORMAL. THEY ALSO RECEIVED A DUCT OVERHEAT. CREW ACCOMPLISHED AN EMERGENCY DESCENT TO REGAIN CONTROL OSDR USAA040987Skin · crackedCLT - RON - SKIN, 1 INCH CRACK. STA 927 TO 947.5, STRINGER 24L. INSTALLED DOUBLER IAW 53-00-01.SDR SB04160Coalescer Bag · contaminatedDFW - FLT 1227 - EN ROUTE, THE CABIN CREW NOTED A STRONG ODOR/FUMES WHICH RESULTED IN PASSENGER COMPALINTS OF BURNING EYES AND HEADACHES. MAINTENANCE FOUND THE WATER SEPARATOR BAGS CONTAMINATED AND REPLACED THEM.SDR SB04158Indicator · faultyDURING APPROACH TO PHL FROM ORD, CREW EXPERIENCED A FLAP DISAGREEMENT WHEN FLAP HANDLE WAS PLACED BEYOND 15 UNITS. A FLAP SPLIT WAS CLEARLY INDICATED. NO ROLL FORCES WERE FELT. AN EMERGENCY WAS DECLARED AND EQUIPMENT WAS CALLED OUT. FLIGHT LANDED WITHOUT ISDR SB04157Light · inoperativePHL - PILOT REPORTED THE SEAT LEVEL EMERGENCY LIGHT AT SEAT ROW 7 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT ROW 7. OPERATIONAL CHECK GOOD.SDR SB04156Charger · failedMAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 2 THRU 4, INCLUDING THE EMERGENCY EXIT SIGN, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND THE BATTERY PACK. OPERATIONAL CHECK GOOD.SDR AWXA200401307Slide · leakingDURING INSPECTION FOUND R-2 DOOR SLIDE PRESSURE LOW. MX R/R R-2 DOOR SLIDE IAW T/C R1C25001. CONFIRMED REASON FOR REMOVAL FINDING RESERVOIR ASSEMBLY LEAKING AT THE RUPTURE DISC. REPLACED RUPTURE DISC AND RE-SERVICED RESERVOIR, LEAK CHECK GOOD PER CMM.SDR USAA040844Skin · crackedFWD SERVICE DOOR SKIN, .1875 INCH CRACK, UPPER HINGE CUTOUT, LWR RADIUS TO DRAIN HOLE. INSTALLED DOUBLER IAW TYP REP 52-10-13.SDR USAA041040Skin · gougedPIT - Q4 - LOWER SKIN SURFACE, SINGLE LAYER COMPOSITE DAMAGE .75 INCH GOUGE, RT ELEVATOR AT 84.5 AND 4 - 5 INCH IN FROM FWD SPAR. PREPARED DAMAGED AREA, APPLIED WET LAY UP REPAIR IAW SRM AND EA.
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