Boeing 737-230
Service difficulty reports · 466
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 = '737230' 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 = '737230' 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 COOSDR010083Rib · crackedRIGHT WING, INBOARD MID FLAP RIB CRACKED AT WBL 86.74.SDR COOSDR010111Skin · debondedFUSELAGE SKIN SECTION FROM BS 330 TO BS 350 BETWEEN STR 21L AND 23L WITH DISBONDING.SDR COOSDR010110Rib · crackedLEFT WING LEADING EDGE RIB CRACKED, LOCATED AT FSS 394, NR2 SLAT OUTBOARD MAIN TRACK SUPPORT.SDR COOSDR010109Rib · crackedLEFT WING LEADING EDGE RIB CRACKED, LOCATED AT FSS 267, NR3 SLAT INBOARD MAIN TRACK SUPPORT.SDR COOSDR010108Skin · delaminatedFUSELAGE SKIN SECTION FROM BS 635 TO BS 663 BETWEEN STR 14R AND 15R WITH DELAMINATION.SDR COOSDR010107Doubler · delaminatedFUSELAGE SKIN DOUBLER FROM BS 639 TO BS 663 BETWEEN STR 9L AND 10L WITH DELAMINATION.SDR COOSDR010106Bulkhead · crackedBULKHEAD WEB SECTION CRACKED, RBL 10, BETWEEN WL 237.25 AND WL 230.5SDR COOSDR010105Bulkhead · crackedBULKHEAD WEB SECTION CRACKED, AT LBL 10, BETWEEN WL 237.25 AND WL 230.5.SDR COOSDR010104Skin · delaminatedFUSELAGE SKIN FROM BS 950 TO BS 955 BETWEEN STR 5R AND STR 6R DELAMINATED.SDR COOSDR010103Skin · corrodedFUSELAGE SKIN AT BS 340 AT STR 24L WITH CORROSION.SDR COOSDR010102Doubler · debondedFUSELAGE SKIN FROM BS 335 TO BS 350 BETWEEN STR 24L AND STR 25L WITH DOUBLER DEBONDED.SDR COOSDR010101Skin · crackedFUSELAGE SKIN FROM BS 500B+6 TO BS 500B+10 AT STR 19R UPPER SKIN WITH CRACK INDICATION.SDR COOSDR010100Skin · delaminatedFUSELAGE SKIN FROM BS 847 TO BS 867 BETWEEN STR 22R AND STR 23R WITH DELAMINATION.SDR P2EA01137Valve · failedFLT 940 - MCI - ON DESCENT TO 12,000 FEET POWER AT IDLE, CABIN NI 700 FEET DESCENT. WHEN ADVANCING POWER AT 12,000 TO 1.3 EPR CABIN SHOWED DESCENT OF 2000 FEET WITH NOTICEABLE PRESSURE CHANGE IN OUR EARS. IN DESCENT TO 12,000 FEET WITH POWER AT IDLE SHOWED 4SDR P2EA01133Warning Light · illuminatedFLT 554 - MCI - AFTER PUSH BACK FROM GATE AND AFTER APPLICATION OF AIRCRAFT POWER, THE AFT SERVICE DOOR UNSAFE LIGHT ILLUMINATED. RETURNED TO THE GATE. INSPECTED THE AIRCRAFT L2 DOOR, OPEN AND CLOSED DOOR NORMALLY. NO DEFECTS FOUND. (M)SDR 2001F00076Indicator · intermittentSAL - FLT 441 - AFTER TAKEOFF, WHEN PILOT SELECTED FLAP TO UP POSITION, IT DID NOT RESPONDED. ALTERNATE FLAP EXTENSION WAS PERFORMED FOR LANDING. THE AIRCRAFT RETURN TO THE EL SALVADOR AIRPORT. AT EL SALVADOR STATION, MAINTENANCE TECHS TESTED THE FLAPS INDISDR 2001F00074Flap · malfunctionedSAL - FLT 441 - AFTER TAKEOFF, WHEN PILOT SELECTED FLAP TO UP POSITION, IT DID NOT RESPOND. ALTERNATE FLAP EXTENSION WAS PERFORMED FOR LANDING. THE AIRCRAFT RETURNED TO THE EL SALVADOR AIRPORT. THE AIRCRAFT REMAINED ON GROUND FOR MAINTENANCE. (M)SDR TSAA0153079Skin · damagedAIRCRAFT SKIN AND FRAME DAMAGED AT BS 847 THROUGH BS 887, STRINGER 25L THROUGH STRINGER 25R. REMOVED DAMAGED AREA ,PERFORMED HFEC INSPECTION AROUND CUT OUT NO DEFECTS NOTED. REPAIRED STRINGER S27L AT BS 847 IAW SRM 53-10-3 FIG INSTALLATION OF REPAIR DOUBLER SDR P2EA01092Tube · damagedMCI - FLT 906 - DURING WALK AROUND, FOUND THAT THE AIRCRAFT REFUELING DOOR HAD BEEN LEFT OPEN ON ITS FLIGHT FROM MSY. DAMAGE WAS CAUSED TO AN ANTI-ICE DUCT, TWO HOLD OPEN RODS AND ATTACH BRACKETS IAW BOEING MM 30-22-0, 57-30-00. (M)SDR P2EA01055Flap · malfunctionedMCI - FLT 356, 354, 2259 - WHILE ON APPROACH INTO MCI FROM BUF, FLAPS WOULD NOT EXTEND BEYOND 25 DEGREES. MAINTENANCE PERFORMED OPERATIONAL CHECK PER BOEING MM 27-51-01. SYSTEM CHECKED NORMAL ON GROUND. SUBSEQUENTLY, ON APPROACH TO MDW FROM MCI, FLAPS WOULD SDR P2EA01050Proximity Switch · out of adjFLT 350 - MCI-MDW EN ROUTE CALL, 'INTRANSIT' LEADING EDGE SLAT. WOULD HAVE TO MAKE FLAPS 15 LANDING AND WOULD BE UNABLE TO LAND IN MDW. DECISION MADE TO RETURN TO MCI. DID NOT DECLARE EMERGENCY IN MCI. OVERNIGHT MAINTENANCE AT MCI ADJUSTED NR 1 SLAT PROXIMSDR P2EA2001V0009Skin · dentedON LEADING EDGE OF AFT CARGO DOOR SKIN APPROXIMATELY 18 INCHES FROM LOWER EDGE WITH BOEING TEMPORARY REPAIR PER VAG-MCI-01-0002H DUE DENT OUT LIMITS. INSTALLED PERMANENT REPAIR PER SRM 52-00-3 FIG 5 AT AFT CARGO DOOR EXTERNAL SKIN FROM BS 796 TO BS 800.5 BETWSDR TSAA0133030Light · inoperativeREPLACED NR 6 FLOOR PROXIMITY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133024Light · inoperativeREPLACED CENTER AISLE EMERGENCY EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0153006Frame · crackedIDENTIFIED CRACK AT FASTENER HOLE CAUSED BY A SHORT EDGE DISTANCE AT BS 1112 FRAME. TRIM OUT THE DAMAGED AREA OF FRAME, FABRICATED AND INSTALLED FILLER OF 056 INCH 7075-T6, FABRICATED AND INSTALLED 063 INCH REPAIR STRAP, CLEANED AND TREATED ALL EXPOSED AREAS SDR P2EA01002Warning System · malfunctionedMCI - FLT 101 - DURING APPROACH WITH LANDING GEAR HANDLE DOWN, GEAR INDICATION OF 3 GREEN, 3 RED LIGHTS ON AND WARNIGN HORN SOUNDING. ABORTED APPROACH AND WENT AROUND, CYCLED GEAR 2ND TIME ALL INDICATIONS NORMAL. TESTED GEAR LIGHTS AND HORN IAW BOEING MM 32-SDR TSAA0155001Spar · crackedIDENTIFIED CRACK AT LEFT HORIZONTAL STABILIZER CENTER SECTION REAR SPAR UPPER CHORD AFT UPPER CLEVIS LUG DURING SCHEDULED INSPECTION PER ECO 1384R6/SB 737-55-1033R1. (M)SDR 20010111CW001Sensor · out of adjDURING CLIMB, IN FLIGHT, TPU-012, LIM-IQT, AFT SRV ANNUNCIATION LIGHT CAME ON. PERFORMED CK ON DOOR, LISTENED FOR A PRSUR LEAK, AC RETURNED TO APRT. TECH ADJUSTED SRVC DOORPROXIMITY SENSOR, AND PRSUR TEST. AC RETURNTO NORMAL OPERATION.SDR E6RA200124002Regulator · failedON TAKE-OFF, NUMBER 2 GENERATOR FAILED. TAKE-OFF ABORTED AND AIRCRAFT RETURNED TO GATE. SWAPPED NUMBER 2 GENERATOR CONTROL UNIT (GCU) WITH APU GCU AND CONFIRMED FAILURE. INOPERATIVE GCU WAS DEFERRED IN ACCORDANCE WITH MEL. GCU WAS FUNCTIONALLY TESTED IN ACCORSDR TSAA0053256Skin · crackedIDENTIFIED 3 INCH CRACK AT BS 500 STRINGER 15R. TEMPORARY REPAIR INSTALLED BY TRIM OYT OF CRACK, INSPECTED CUTOUT USING HFEC METHOD AND INSTALLED EXTERNAL DOUBLER. RECEIVED 8110-3 APPROVAL. PERMANENT REPAIR REQUIRED WITHIN 1 MONTH OR 500 CYCLES WHICHEVER ISSDR TSAA0033252Battery Pack · inoperativeREPLACED NR 2 AND NR 4 EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR P2EA00465Indicator · malfunctionedUPON LANDING, FLAPS WOULD NOT EXTEND OR RETRACT PER CONVENTIONAL METHODS. ALTERNATE FLAPS USED AND AIRCRAFT LANDED WITHOUT INCIDENT.RESET FLAP INDICATOR. FLAP SYSTEM INSPECTED AND OPERATIONAL CHECK PERFORMED. NO DEFECTS NOTED.SDR P2EA00464Indicator · malfunctionedDURING FLIGHT HYDRAULIC PRESSURE WENT TO ZERO. AIRCRAFT LANDED AND RETURNED TO GATE WITH NO INCIDENT. RESERVOIR CHECKED UPON LANDING, NO DEFECTS NOTED. HYDRAULIC SYSTEM CHECKED FOR LEAKS AND ALL FLIGHT CONTROLS WERE CYCLED TO REMOVE AIR. HYDRAULIC SYSTEM OSDR TSAA0333038Battery Pack · inoperativeREPLACED LT OVERWING EMERGENCY IDENT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0033244Battery Pack · inoperativeREPLACED NR 6 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0033242Battery Pack · dischargedREPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR P2EA00462Indicator · malfunctionedMCI - FLT 625 - IN-FLIGHT AND WITH NR 2 FUEL QUANTITY INDICATOR ON DEFERRAL, THE NR 2 FUEL FLOW INDICATOR READ 1800/HR WHILE NR 1 FUEL FLOW INDICATOR READS 2700/HR. AIRCRAFT RETURNED TO MCI WITH NO INCIDENT. REPLACED FUEL FLOW INDICATOR IAW MM 31, OPERATIONASDR TSAA0055246Spar · corrodedIDENTIFIED CORROSION AT VERTICAL STABILIZER REAR SPAR CHORD AND REPAIR CONSISTED OF BLEND OUT AT 20 TO 1 RATIO. PERFORMED HFEC INSPECTION NO DEFECTS NOTED, CLEANED AND TREATED AFFECTED AREA. IAW ECO 2509 AND RECEIVED 8110-3. AIRCRAFT OK FOR SERVICE. (M)SDR TSAA0055238Spar · corrodedIDENTIFIED LEFT HORIZONTAL STABILIZER REAR SPAR UPPER CHORD CORROSION AT STABILIZER STATION 110. REPAIRED BY BLENDOUT 10 TO 1 RATION SPANWISE COMPLETED 12/13/2000. CLEANED AND TREATED REWORKED SURFACES, RECEIVED 8110-3, IAW ECO 2154R2. (M)SDR P2EA00398Warning System · malfunctionedDEN - FLT 206 - ON TAKEOFF ROLL, AS RT ENGINE EPR INCREASED PAST 1.30 RECEIVED TAKEOFF CONFIGURATION WARNING HORN. RECYCLED FLAPS UP, HORN STILL PRESENT. AIRCRAFT RETURNED TO GATE WITH NO INCIDENT. PERFORMED TAKEOFF SYSTEM CHECK IAW JOB CARD J2-A2. COULD NSDR TSAA0033234Battery Pack · dischargedREPLACED NR 6 FLOOR EMERGENCY LIGHT BATTERY PACK DUR TO INOP. OPS CK OK.A/C RETURNED TO SERVICE.SDR P2EA00325Control Handle · faultyMCI - FLT 101 - ON ENGINE SHUT DOWN, ALL THREE RED LANDING GEAR LIGHTS ILLUMINATED. REPLACED LANDING GEAR CONTROL LEVER ASSY PER MM 32-31-11. REPLACED R273 RELAY PER MM 32-61-61. CLEANED ADDITIONAL PLUGS. D5082 AND D2618. SYSTEM OPERATED NORMAL PER MM 32SDR P2EA00323Handle · lack of lubeMCI - FLT 230 - ON APPROACH WHEN LANDING GEAR WAS EXTENDED, THREE GREEN LIGHTS APPEARED INITIALLY. ON 2-MILE FINAL, THREE RED LIGHTS ILLUMINATED. LANDING GEAR WAS EXTENDED BY EMERGENCY PROCEDURES AND MCI - FLT 230 - AN EMERGENCY WAS DECLARED. AIRCRAFT LANDESDR TSAA0033226Battery Pack · dischargedREPLACED CENTER EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR P2EA00301Circuit Board · failedAFTER TAKE OFF AND DURING GEAR RETRACTION EXPERIENCED AN INTERMITTENT LANDING GEAR WARNING HORN ALONG WITH AN OVERHEAD MASTER CAUTION ANNUNICATOR LIGHT. ELECTRICAL ODOR EVIDENT ON SHUTDOWN AT GATE. A/C RETURNED TO GATE WITH NO INCIDENT. ADJUSTED GAP ON PROXISDR CA001103007Antenna · failed(CAN) DURING TEST FLIGHT, THE NR 1 HF ANTENNA SEPARATED AT THE CABLE TENSIONER AFTER TENSIONER FAILURE. THE FREED CABLE WHIPPED AGAINST THE FUSELAGE, DAMAGING 4 CABIN WINDOWS AND DENTING THE FUSELAGE AT 2 PLACES (STA 685 AND 688). THE TURN BARREN SECTION OF THSDR TSAA0033221Battery Pack · dischargedREPLACED NR 3 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR 20010212SG015Filter · faultyYAW DAMPER COUPLER DISENGAGED DURING CLIMB-OUT. WOULD NOT RE-ENGAGE. ITEM WAS DEFERRED IAW MEL. OPEN DEFERRAL WAS CLEARED BY REPLACING THE YAW DAMPER COUPLER. THE FAILURE WAS CONFIRMED BY REPAIR STATION. FAULTY COMPONENT WAS IDENTIFIED AS CHASIS FILTER. SDR E6RA200022001Filter · shortedYAW DAMPER COUPLER DISENGAGED DURING CLIMB OUT. WOULD NOT RE-ENGAGE. ITEM WAS DEFERRED IN ACCORDANCE WITH MEL. OPEN DEFERRAL WAS CLEARED BY REPLACING THE YAW DAMPER COUPLER.THE FAILURE WAS CONFIRMED BY THE REPAIR STATION. FAULTY COMPONENT WAS IDENTIFIED AS THESDR P2EA00251Fitting · crackedSJO - DURING C-CHECK, LEFT WING INBOARD FLAP BOOM FORWARD ATTACH FITTING CRACKED. REPAIRED BY MODIFICATION IAW SB 737-27-1110 SECTION III FIGURES 2, 3 AND 4. (M)
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