Boeing 737-232
Service difficulty reports · 1,700
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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 = '737232' 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 = '737232' 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 DL73K001784Indicator · malfunctionedNR 2 ENGINE OIL TEMP GAUGE READING ABOVE RED LIMIT ALL OTHER ENGINE INDICATIONS READ NORMAL. A/C DIVERTED TO ATL OFF FLT 2426. FOUND OIL TEMP GAUGE PEGGED HIGH. REPLACED OIL TEMP BULB, CKS GOOD.SDR DL73K001749Frame · crackedTHE FS 947.5 FRAME WAS FOUND CRACKED AT THE CUTOUT FOR S-19R. THE DAMAGE WAS REMOVED WITH A 1.25 X 1.0 INCH CUTOUT IN THE FRAME VERTICAL WEB. THE DAMAGE WAS REPAIRED PER ERA 334913-14 AT HMV.SDR DL73K001755Skin · gougedTHE FUSELAGE SKIN AT THE C1 DOOR CUTOUT FWD EDGE (FS 440) WAS FOUND WITH SEVERAL GOUGES AND SCRATCHES BETWEEN STRINGERS 21R & 25R. THE SKIN WAS CUT OUT TO REMOVE THE DAMAGE. THE CUTOUT WAS REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 3784SDR DL73K001756Skin · gougedTHE FUSELAGE SKIN WAS FOUND WITH A GOUGE AT THE STRINGER 25R SKIN LAP SPLICE AT FS 847. THE GOUGE WAS IN THE UPPER SKIN OF THE LAP ONLY AND WAS REMOVED WITH A CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER, INSTALLED PER ER/A 3SDR DL73K001731Frame · corrodedTHE FS 400 FRAME WAS FOUND CORRODED ABOVE STR 26R, 3.5 INCHES BELOW THE EXISTING FACTORY SPLICE. THE CORROSION WAS FOUND IN THE TOP OF THE INBOARD FLANGE. THE DAMAGE CUTOUT EXTENDED INTO THE VERTICAL WEB OF THE FRAME. THE DAMAGE WAS REPAIRED PER ERA 334912-SDR DL73K001718Strap · corrodedTHE INBOARD STRAP ON THE FORWARD FRAME OF THE C2 DOOR CUTOUT WAS FOUND CORRODED. THE STRAP WAS CUT AT RBL 25 AND A NEW INBOARD END WAS SPLICED IN. THE DAMAGE WAS REPAIRED PER ERA334883-14 AT HMV.SDR DL73K001708Frame · corrodedLEVEL TWO CORROSION FOUND ON FUSELAGE FRAME 787 SKIN ATTACH ANGLE O/B OF STRINGER 27 LEFT. REPAIRED PER MAINTENANCE MANUAL 53-11-0, FIG 801.SDR DL73K001703Floorbeam · crackedTHE UPPER CHORD, WEB AND DOUBLER OF THE RBL 24.8 FLOORBEAM WAS FOUND CRACKED AT FS 675. THE CHORD WAS SPLICED AND THE WEB AND DOUBLER WERE REPAIRED PER ERA 334875-14. THE DAMAGE WAS FOUND DURING INSPECTION AT HMV.SDR DL73K001689Floor Panel · crackedTHE COCKPIT FLOOR WEBS AT WL 207 THAT EXTEND FROM FS 178 TO FS 188 O/B OF LBL AND RBL 24 WERE FOUND CRACKED. THE CRACKS WERE FOUND DURING INSPECTION AND MODIFICATION OF THE FS 178 BULKHEAD WEB PER BAC S/B 737-53A1173, REVISION 3. THIS ER/A INSTRUCTS TO REPLASDR DL73K001687Fitting · corrodedTHE HORIZONTAL STABILIZER ATTACH LUGS WERE FOUND CORRODED. THE DAMAGE WAS REMOVED BY OVERSIZING THE BORES AND BLENDING SOME OF THE FACES. THE DAMAGE WAS REPAIRED AT HMV PER ERA 334874-14.SDR DL73K001686Fitting · corrodedTHE RT AND LT FUSELAGE CLEVIS LUGS THAT ATTACH THE HORIZ STABILIZER WERE FOUND CORRODED. SEVERAL BORES WERE OVERSIZED AND SOME OF THE FACES WERE BLENDED. THE REPAIR WAS ACCOMPLISHED AT HMV PER ERA 334873-14.SDR DL73K001658Circuit Breaker · damagedSVC CK FAILS STEP 13 BATT VOLTAGE CK. REPLACED BATTERY, CHARGER, AND C/B C167 BATTERY TRANSFER CONTROL. REPLACED BATTERY BUS CIRCUIT BREAKER C20. RAN TEST OPS NORMAL.SDR DL73K001631Fastener · wrong partDURING ACCOMPLISHMENT OF THE FUSELAGE FRAME SPLICE AT FS 440 PER S/B 737-53-1125 IT WAS NOTED THAT FIVE FASTENERS WERE INSTALLED AT THE FACTORY WERE .25 INCHES IN DIAMETER. THE S/B CALLS FOR .2187 INCH FASTENERS. ERA 334853-14 ALLOWS FOR THE .25 INCH FASTESDR DL73K001620Light · inoperativeON LAYOVER, EMERGENCY LIGHT INOP AT ROW 10 DEF. REPLACED LIGHT ASSY, CKS GOOD.SDR DL73S001606Transmitter · failedAT TAKEOFF POWER, NR 1 ENGINE OIL PRESSURE INDICATED 33 PSI. RTO AT 70 KNOTS. LIGHT BRAKING TO EXIT RUNWAY. REPLACED OIL PRESSURE TRANSMITTER.SDR DL73K001564Attach Fitting · wornVERTICAL STAB MOVES UP AND DOWN WHEN PUSHING ON UPPER TRAILING EDGE AREA. FOUND ATTACH FITTINGS WORN. REPAIRED SAME.SDR DL73K001580Frame · crackedTHE INBOARD STRAP WAS FOUND CORRODED AND CRACKS WERE FOUND IN THE FORWARD FRAME OF THE C2 DOOR OPENING AT APPROX WL 160. THE STRAP WAS REPLACED AND THE FRAME MODIFIED PER S/B 737-53-1096 WITH SOME DEVIATIONS PER ERA 334753-14 AT HMV.SDR DL73K001579Skin · crackedA CRACK WAS FOUND IN THE FUSELAGE SKIN AT THE AFT GALLEY DOOR UPPER AFT CORNER. THE CRACK WAS ROUTED OUT AND A DOUBLER AND TRIPLER WAS INSTALLED PER ERA 334709-14 AT HMV.SDR DL73K001578Skin · crackedA CRACK WAS FOUND IN THE FUSELAGE SKIN AT THE AFT ENTRY DOOR LOWER HINGE CUTOUT. A REPAIR WAS INSTALLED SIMILIAR TO B737-200 SRM 53-30-3, FIGURE 36 PER ERA 334778-14 AT HMV.SDR DL73K001577Attach Fitting · corrodedTHE RT AND LT ATTACH FITTINGS OF THE HORIZONTAL STABILIZER WERE FOUND CORRODED. THE BORES WERE OVERSIZED AND SOME OF THE FACES WERE BLENDED PER ERA 334715-14 AT HMV.SDR DL73K001576Attach Fitting · corrodedTHE NUMBER 2 LUG ON THE VERTICAL STABILIZER ATTACH FITTING WAS FOUND CORRODED. THE BORE WAS OVERSIZED AND NEW BUSHINGS WERE MANUFACTURED PER ERA 334730-14 AT HMV.SDR DL73K001575Attach Fitting · corrodedTHE HORIZONTAL STABILIZER RT AND LT CLEVIS LUGS WERE FOUND CORRODED. THE LUG DIAMETER WAS ENLARGED AND NEW BUSHINGS WERE INSTALLED PER ERA 334719-14 AT HMV.SDR DL73K001574Floorbeam · crackedA CRACK WAS FOUND IN THE RBL 24 LONGITUDINAL FLOORBEAM AT APPROX FS 656. THE CRACK WAS REMOVED AND A DOUBLER WAS INSTALLED PER ERA 334706-14 AT HMV.SDR DL73K001573Frame · corrodedTHE FS 500 FRAME WAS FOUND CORRODED BETWEEN STR 25R AND STR 26R. THE DAMAGE WAS CUT OUT AND A FORMED SECTION REPAIR INSTALLED PER ERA 334713-14 AT HMV.SDR DL73K001550Intercostal · crackedTHE SIDE CHORD INTERCOSTALS COMMON TO THE FS 178 BULKHEAD AT WL 195 WERE FOUND WITH CRACKING TYPICAL OF BAC S/B 737-53A1173 AND AD 2000-05-29. THE DAMAGED INTERCOSTALS WERE REMOVED AND NEW INTERCOSTALS INSTALLED WITH OVERSIZE FASTENERS AS REQUIRED. TSDR DL73K001536Transmitter · inaccurateRTO AT EWR DUE TO RIGHT ENGINE DID NOT REACH T/O EPR SETTING. REPLACED RIGHT ENGINE EPR TRANSMITTER. OPERATED RIGHT ENGINE AT T/O POWER PER PFHB AND ALL ENGINE PARAMETERS NORMAL.SDR DL73K001551Web · crackedDURING INSPECTION OF THE FS 178 BULKHEAD AND SURROUNDING STRUCTURE PER BAC S/B 737-53A1173, THE ADJACENT COCKPIT FLOOR WEBS COMMON TO THE FS 178 BULKHEAD AT WL 207 AND LBL & RBL 24 WERE FOUND CRACKED. THE DAMAGED WEB SECTIONS WERE REMOVED AND NEW SECTIONS INSSDR DL73K001522Light · failedEEPLS SYSTEM HAS LIGHTS OUT AT E-1 DOOR LOWER EXIT SIGN AND AT SEAT 3DEF. RELAMPED.SDR DL73K001524Bulkhead · crackedTHE FS 178 BULKHEAD WAS FOUND WITH 2 SMALL CRACKS AT WL 235 AND LBL 7. THE CRACKS ARE TYPICAL OF BAC S/B 737-53A1173. THE CRACKS WERE ROUTED OUT OF THE WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER B737 SRM 53-10-11, FIG 1 AND DOCUMENTED PER ER/A 378138-14ADSDR DL73K001489Light · damagedSEAT 01D EMERGENCY LIGHT RIPPED OFF. REPLACED SAME, OPS NORMAL.SDR DL73K001486Generator · inoperativeLT ENGINE GENERATOR FAILED DURING TAKEOFF ROLL AT APPROX 80 KTS. CHECKED NR 1 CSD OIL LEVEL AND FILTER BYPASS, CKS GOOD. REPLACED GCU, RAN ENG FOUND GEN FOLLOWING THROTTLE. REPLACED GENERATOR AND CSD.SDR DL73K001485Power Supply · failedEMERGENCY POWER SUPPLY WOULD NOT TEST AT ROWS 14, 15 DEF. REPLACED POWER SUPPLY.SDR DL73K001445Wire · chafedNR 1 ENG OIL FILTER BYPASS LIGHT ILLUM PASSING THROUGH FL22. REDUCED ENG TO 60 PERCENT AND LIGHT WENT OUT. INSP OIL FILTER FOR CONTAMINATION-NTF. FOUND WIRE CHAFED AT FIREWALL DISCONNECT (W184-021-20). REPAIRED SAME.SDR DL73K001455Skin · crackedTHE FUSELAGE SKIN WAS FOUND CRACKED AT FS 765 JUST ABOVE S-19R. THE CRACK WAS APPROX 1 INCH IN LENGTH AND RAN ALONG THE EDGE OF THE BONDED DOUBLER. THE CRACK IS TYPICAL OF THAT DESCRIBED IN BACO S/B 737-53-1065 EVEN THOUGH THIS S/B IS NOT EFFECTIVE FOR THIS SDR DL73K001454Rib · damagedCRACKS DISCOVERED IN THE UPPER CHORD OF THE WING CENTER SECTION LBL 24 FLOORBEAM IMMEDIATELY FWD STA 680. INSTALLED REPAIR IN ACCORDANCE WITH ER/A 334695-14.SDR DL73K001380Valve · leakingAIRCRAFT TAKEOFF ABORTED AT 120 KIAS. NR 1 ENGINE EGT GOING THROUGH 625 CELSIUS. PEAK TEMP OBSERVED 628 - 629 CELSIUS. PACKS OFF T/O. FOUND NR 1 ENG NOSE COWL ANTI-ICE VLV BYPASSING BLEED AIR. REMOVED AND REPLACED NOSE COWL ANTI-ICE VLV PER MM. PERFORMEDSDR DL73K001336Frame · crackedONE CRACK WAS FOUND IN EACH OF THE LEFT AND RIGHT FS 616 IN THE LOWER FASTENER OF THE INNER CHORD AT FRAME TO STUB BEAM JOINT. THE CRACKS WERE 1.25 INCH IN LENGTH AND WERE TYPICAL TO THOSE SHOWN IN S/B 737-53-1182. ERA 334694-14 AUTHORIZES A REPAIR SIMILIAR SDR DL73K001337Skin · crackedTHE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR SURROUND SKIN WAS FOUND WITH A TYPICAL CRACK. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER. THE REPAIR WAS ACCOMPLISHED PER B727 SRM 53-30-3, FIG 21 AND ER/A 377870-14, REVSDR DL73K001323Frame · mismanufacturedWHILE ACCOMPLISHING THE MODIFICATION TO THE RS FS 440 FRAME PER S/B 737-53-1125 IT WAS NOTED THAT THE INITIAL FASTENERS AT THE SUBJECT LOCATIONS (5) WERE MS20470D8 RIVETS. THE S/B CALLS FOR THESE LOCATIONS TO BE OVERSIZED TO .2187 INCH RIVETS. ERA 334686-14 SDR DL73K001288Skin · crackedTHE FUSELAGE SKIN WAS FOUND CRACKED JUST ABOVE STR 19R AT FS 767. THE 2.5 INCH CRACK WAS CUTOUT AND A REPAIR WAS INSTALLED PER B737-200 SRM 53-30-3, FIGURE 6. THE DAMAGE WAS FOUND AT HMV.SDR DL73K001287Frame · damagedTHE LOWER STUB FRAME FOR THE FORWARD SIDE OF THE AFT GALLEY DOOR CUTOUT WAS FOUND DAMAGE AND REPLACED ON ERA 334610-14 AT HMV.SDR DL73K001286Skin · crackedTHE FUSELAGE SKIN WAS FOUND CRACKED JUST BELOW STR 18L AT FS 727B. THE 3 INCH CRACK WAS CUTOUT AND AN EXTERNAL REPAIR WAS ACCOMPLISHED PER B737-200 SRM 53-30-3, FIGURE 6. THE DAMAGE WAS FOUND AT HMV.SDR DL73K001285Stringer · corrodedTHE LT AFT KEEL CHORD (STR 27L) WAS FOUND CORRODED BETWEEN FS 907 AND FS 927. AS A RESULT STRINGER 27L WAS REMOVED FROM FS 907 TO FS 1016 AND A NEW SECTION SPLICED IN PER ERA 334591-14 AT HMV.SDR DL73K001284Frame · misdrilledA DOUBLE DRILLED HOLE WAS FOUND ON THE ORIGINAL INSTALLATION OF THE FS 663 FRAME BETWEEN STRINGERS 9L AND 10L. THE HOLE WAS CLEANED UP AND REPAIRED PER ERA 334565-14 AT HMV.SDR DL73K001282Floorbeam · crackedTHE BL .07 FLOORBEAM WAS FOUND CRACKED IN THE WEB BETWEEN FS 700 AND FS 717. ERA 334520-14 REPAIRED THE DAMAGE SIMILIARLY TO S/B 737-57-1210 AT HMV.SDR DL73K001281Floorbeam · crackedTHE UPPER CAP AND WEB OF THE LBL 24 FLOOR BEAM WAS FOUND CRACKED BETWEEN STATIONS 670 AND 678. THE UPPER CAP WAS SPLICED AND THE WEB WAS REPAIRED PER ERA 334555-14 AT HMV.SDR DL73K001280Floorbeam · crackedTHE FUSELAGE WING CENTER SECTION FLOOR BEAM AT RBL 12 WAS CRACKED IN THE WEB AND UPPER CAP. THE UPPER CAP WAS CUT AND SPLICED TO REMOVE THE DAMAGE AND THE WEB WAS REPAIRED PER ERA 334535-14. THE DAMAGE WAS FOUND AT HMV.SDR DL73K001279Attach Fitting · corrodedCORROSION WAS FOUND ON THE FUSELAGE SIDE OF THE VERTICAL FIN ATTACH LUGS. LUG BORES WERE OVERSIZED THE THE LUG FACES WERE SPOTFACED TO REMOVE THE CORROSION. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 334526-14.SDR DL73K001278Attach Fitting · corrodedCORROSION WAS FOUND ON THE LEFT AND RIGHT FORWARD AND AFT CLEVIS LUGS. THE DAMAGE WAS REMOVED BY INCREASING THE DIA OF THE BORES AND SPOTFACING SOME OF THE FACE OF THE NR 3 LUG. THE DAMAGE WAS FOUND AT HMV AND REPAIRED BY ERA 334525-14.SDR DL73K001277Attach Fitting · corrodedCORROSION WAS FOUND ON THE RHS AFT SPAR LUGS OF THE HORIZ STABILIZER. CORROSION WAS REMOVED BY OVERSIZING THE BORES AND SPOTFACING THE FORWARD AND AFT FACES OF THE LUG. THE DAMAGE WAS FOUND AT HMV AND REPAIRED PER ERA 334542-14.
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