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 jasc_code = '5751' 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 jasc_code = '5751' 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 UPS08153919Aileron · dentedINSPECTION TYPE:1C3C RT WING ALL SPEED AILERON UPPER T/E NUMEROUS DENTS. REPAIRED RT WING ASA UPPER T/E REF EO C-5750-31147-A AND EA 300- 5751-01-A1554.SDR UPS08854248Skin · misrepairedINSPECTION TYPE:SV APPENDIX G SURVEY SEQ 715-W4-01 EXTERNAL DOUBLER DOES NOT MATCH SRM 57-02-01-0 FIG 002Y UPPER SURFACE RW OUTBOARD AILERON. REPLACED DOUBLER IAW SRM 57-02-01 FIG 002Y REV 78.SDR IXXA08SMN201SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD AILERON LOWER HAS IMPROPER REPAIR AT STATION XW 698.000. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PSDR COEA0809917Rib · corrodedFOUND AT COE LEVEL 2 CORROSION. CORROSION ON LT WING AILERON HORN ATTACHMENT RIB.SDR 08FDEA04508Skin · chafedLT WING INBD AILERON INBD LOWER NOSE PANEL IS CHAFED. BLENDED OUT DAMAGE. FOUND OUT OF LIMITS IAW SRM 57-00-01. FABRICATED NEW SKIN PANEL IAW IAW DWG ARC 1316. ALODINED & PRIMED IAW SRM 51-21-01. PAINTED IAW SRM 51-21-01. INSTALLED IAW DWG ARC 1316 & SRSDR 08FDEA04409Brace · crackedLEFT WING INBD AILERON BAY, VERTICAL TEE BRACE LOCATED AT XW 373 AND 22 INCHES AFT OF THE REAR SPAR HAS A CRACK TO THE BOTTOM OF THE TEE ANGLE. REMOVED CRACKED TEE ANGLE IAW SRM 51-33-01. LOCATED & DRILLED HOLES IN NEW ANGLE & INSTALLED IAW DWG ARC 0472 & SSDR ASAA0843592Spar · delaminatedLT WING AILERON FRONT SPAR DELAMINATED I/B CORNER. REMOVED AND REPLACED LT AILERON IAW B737 400 MM 27 11 11.SDR COEA0804917Skin · corrodedMAJOR REPAIR AND LEVEL 2 CORROSION. RT WING AILERON TRAILING EDGE HAS SURFACE CORROSION, JUST OB OF THE TRIM TAB. CORROSION BLEND-OUT WAS BEYOND ACCEPTABLE LIMITS. FOUND AT COE MAJOR REPAIR AND LEVEL 2 CORROSION. RT WING AILERON TRAILING EDGE HAS SURFACE CSDR C2XA08TY122Fitting · wornRT AILERON PCA FITTING OTBD LUG (ON AILERON) MISSING HAT BUSHING. REMOVED AND REPLACED FITTING IAW EC5750-01177, REV B. AIRCRAFT CURRENTLY IN C-CHECK. (K)SDR C2XA08TY121Bushing · wornACFT CURRENTLY IN A C-CHECK STATUS WAS FOUND WITH THE LT AILERON PCA BRACKET WITH MIGRATING BUSHINGS IAW EC5740-01152 AND WILL BE RELEASED AT THE END OF THE CHECK. (K)SDR DHLA2008745503Skin · dentedDENTS ON LT O/B AILERON LOWER SURFACE AT LWBL 578. ACCOMPLISHED FLUSH REPAIR BETWEEN LWBL 576-582 IAW B727 SRM 57-50-1 FIG 1.SDR DHLA2008745506Skin · dentedRIGHT I/B AILERON SKIN DENTED AT RWBL 258 AND 276. ACCOMPLISHED FLUSH REPAIR ON AILERON LOWER SKIN PER B727 SRM 57-50-5 FIG 1. REF N/R 4987-6-21.SDR C2XA08SH125Fitting · damagedSHV - DURING C-CHECK LT AILERON PCA ATTACHMENT HAS MIGRATED BUSHING. MX REMOVED AND REPLACED LT AILERON PCA FITTING IAW EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR DL757081238Spar · crackedDURING SHOP OVERHAUL VISIT, A CRACK WAS FOUND IN THE SKIN AND SPAR OF THE LT OUTBOARD AILERON. REPAIRED PER 470474-14.SDR ASAA0843621Hinge Fitting · gougedUPON REMOVAL OF LT WING AILERON FOUND NR 1 HINGE LUG ON FITTING GOUGED IN 2 PLACES. REMOVED NR 1 HINGE FITTING DAMAGE FOUND TO BE OUT OF LIMITS. LOCATED, DRILLED AND INSTALLED A REPLACEMENT FITTING IAW B737 400 SRM 51 40 02 AND AAR EA 12969 ASA EA 5750 02509SDR CA081001003Skin · cracked(CAN) AT INSPECTION THE LT AILERON OTBD HINGE ASSY WAS FOUND CRACKED. THE CRACKS WERE LOCATED AT THE BEND RADIUS OF THE LOWER AFT ATTACH ANGLES.SDR C2XA08TY106Bushing · wornACFT CURRENTLY IN C-CHECK STATUS. MAINTENANCE FOUND THE LT AILERON IB PCA HAD BUSHING MIGRATED. MAINT REMOVED AND REPLACED THE HAT BUSIONS IAW EC5740-01152 AND WILL BE RELEASED AT THE END OF THE CHECK. (K)SDR C2X2008F00030Bonding Strap · corrodedAC IS CURRENTLY IN C-CHECK AND THE RT AILERON SHROUD BONDING STRAPS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE BONDING STRAP PLATE IAW EC 575001315. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (K)SDR C2X2008F00029Bonding Strap · corrodedAC IS CURRENTLY IN C-CHECK AND THE LT AILERON SHROUD BONDING STRAPS WERE FOUND CORRODED. MAINT REMOVED AND REPLACED THE BONDING STRAP PLATE IAW EC 5750-01315. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK. (K)SDR C2XA08TY089Bracket · gougedA/C WAS IN A C CHECK STATUS AND THE O/B BUSHION HOLE ON THE PCA BRACKET ATTACH POINT WAS FOUND OVERSIZE ON THE RT AILERON. MX REPLACED THE PCA BRACKET IAW EC 5750-01177. ALL WORK WAS ACCOMPLISHED AND WAS RELEASED BACK TO SERVICE.SDR ASAA0843418Skin · delaminatedLT WING AILERON TRIM TAB HAS DELAM. LT WING AILERON TRIM TAB REPAIRED IAW B737 400 SRM CH 51 70 16.SDR 08FDEA03575Panel · crackedLEFT AILERON BOOSTER PANEL IS CRACKED. REPLACED THE LEFT AILERON BOOSTER PANEL IAW A300-600 AMM 27-11-28-4.SDR C2XA08SH107Bracket · wornSHV - DURING C-CHECK. THE RT AILERON TO PCA ATTACHMENT BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145 SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)SDR C2XA08SH102Bracket · wornSHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA BRACKET HAD A MIGRATED HAT BUSHING. THE HOLE WAS WORN OUT OF LIMITS AND WOULD NOT RETAIN THE BUSHING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145XR SRM 51-40-02. THE ACFT WAS APSDR 08FDEA03258Structure · corrodedLEFT OUTBD AILERON IS BULDGING AROUND THE RIB ATTACH FASTENERS AT XOA 960. LEFT WING OUTBD AILERON WAS REPLACED ON SNRM N00728. CORROSION WAS FOUND TO BE OUT OF LIMITS.SDR 08FDEA03257Skin · corrodedLEFT OUTBD AILERON LOWER SKIN IS CORRODED/BULGED AROUND THE HINGE FITTING. LEFT WING OUTBD AILERON WAS REPLACED ON SNRM N00728. CORROSION WAS FOUND TO BE OUT OF LIMITS.SDR ASAA0843355Hinge Fitting · crackedUPON REMOVAL OF RT AILERON TAB FOUND 2ND FROM O/B HINGE FITTING ON AILERON CRACKED AT FWD UPPER CENTER. AREA APPROX .200 LENGTH. RECEIVED A REPLACEMENT FITTING, INSTALLED NEW FITTING IAW B737 400 SOPM 20 50 01 PG 2 STEP 3 AND CMM 57 50 25 PG 701 STEP 2E FIG SDR WRLA2008061Wedge · debondedDURING 4C CHECK INSPECTION DISBOND WAS FOUND ON THE LT WING OUTBOARD AILERON BETWEEN T/E CORE AND THE UPPER SKIN ASSEMBLY. BOEING HAS AUTHORIZED A TEMPORARY REPAIR WITH A-CHECK REINSPECTIONS AND C-CHECK PERMANENT REPAIR. (A)SDR C2X2008F00015Bracket · gougedACFT IS CURRENTLY IN A C-CHECK STATUS AND THE LT AILERON TO PCA ATTACHMENT POINT O/B LUG HAT BUSHION WAS FOUND MIGRATED. MAINTENANCE REMOVED AND REPLACED THE BRACKET AND REINSTALLED THE AILERON. OPS CHECKS GOOD IAW EMB 145XR EC 5750-01177. ALL WORK WAS ACCOSDR 08FDEA03039Skin · failedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING AILERON LOWER SKIN BETWEEN RIBS 12 TO 16 MEASURES 18.5 X 11.3 INCHES REPAIR NOT IAW SRM REQUIREMENTS. REMOVED 3 EACH FASTENERS FROM PREVIOUS REPAIR DOULBLER AND INSTALLED 3EACH CORRECT FASTENERS ON LEFSDR 08FDEA02993Skin · damagedFOUND OLD PATCH REPAIR ON LT AILERON LOWER SKIN TRAILING EDGE AREA RIB 13- 17 WITH BAD OLD DOCUMENTATION. THE REPAIR RENEWED IAW RAS/FOK/139/2008 ISS A, APPROVED BY EA 6-5761-120107.SDR 08FDEA02992Skin · damagedFOUND TWO OLD PATCH REPAIRS ON RT AILERON LOWER SKIN TRAILING EDGE AREA RIB 10-12 AND 4-10 WITHOUT OLD DOCUMENTATION. THE TWO REPAIRS RENEWED IAW RAS/FOK/138/2008 ISS A, APPROVED BY EA 6-5761-120106 .SDR F3LA200800487Skin · chafedDURING C-CHECK INSP NOTED THE RT AILERON APPEARS TO BE CHAFING AT IB LOWER EDGE. MAINT CLEANED AREA OF DAMAGE AND REPAIRED IAW SRM 51-75-12. UPON COMPLETION OF THE REPAIR IT WAS INSPECTED AND FOUND ACCEPTABLE. (B)SDR C2XA08SH093Bushing · migratedSHV - DURING C-CHECK RT AILERON OUTBOARD CONTROL ROD ATTACHING BRACKET ON AILERON, HAS MIGRATED HAT BUSHING. MX REMOVED AND REPLACED RT AILERON OUTBOARD CONTROL ROD ATTACHING BRACKET IAW EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)SDR C2XA08SH094Bushing · migratedSHV - DURING C-CHECK BOTH HAT BUSHING ON RT AILERON DAMPER ATTACHMENT FITTING ON AILERON ARE MIGRATED. MX REMOVED AND REPLACED RT AILERON DAMPER ATTACHING FITTING IAW EMB 145-SRM-51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (A)SDR UPS08852897Skin · crackedINSPECTION TYPE-C1, 2 INCH CRACK IN LT AILERON AS MARKED ON LEADING EDGE AT X 499, STOP DRILLED CRACK , FABBED AND INSTALLED REPAIR DOUBLER IAW, SRM, 51- 1-8, 57-2-0 FIG. 2 , 51-3-1.SDR TRAX200800872Structure · corrodedCORROSION FOUND IN LEFT AILERON AROUND THE HINGE INTERNAL AREA. OPEN (B)SDR CA080701003Skin · damaged(CAN) DEPARTING AND DURING CLIMB OUT THE ACFT WAS STRUCK BY LIGHTNING CAUSING DAMAGE TO LT AILERON TIP. DECISION WAS MADE TO RETURN THE ACFT TO AIRPORT FOR INSPECTION. INSPECTION COMPLETED PER AMM 05-50-31 AND DAMAGE WAS FOUND AT THE LT AILERON TIP AND ALL STASDR C2XA08SH085Fitting · wornSHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA FITTING HAD MIGRATED HAT BUSHINGS. THE HOLES WERE FOUND TO BE WORN OUT OF LIMITS AND WOULD NOT RETAIN THE BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED FITTING IAW CONTINENTAL EXPRESS EC5750SDR 08FDEA02289Structure · crackedLEFT WING OUTBD AILERON T/E IS CRACKED AND DETERIORATING. REMOVED T/E SECTION IAW DC/MD-10 SRM 51-35-01; VOL II. MATERIAL ID FOR T/E SECTION IS 3913181-72, PO 621834.1 AND "Z" CHANNELS 2024-T3, 0.032, PO 473755.1. FABRICATED IAW DC/MD-10 SRM 57-20-01; FIG 1SDR IXX2008F00059Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD AILERON UPPER SKIN IMPROPER REPAIRS AT STATION XA 630.000-724.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYSDR IXX2008F00054Skin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD AILERON UPPER SKIN IMPROPER REPAIRS AT STATION XA 630.000-724.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HSDR CA080610003Skin · delaminated(CAN) WHILE ON DECENT THROUGH 32,000 FT ENROUTE A MUFFLED BANG WAS HEARD BY THE CREW OF THE ACFT. AFTER A REVIEW OF THE ACFT INDICATIONS AND HANDLING AND GENERAL CONDITION, IT WAS UNCERTAIN WHERE THE NOISE HAD COME FROM. IT HAD BEEN THOUGHT THAT IT MAY HAVE BESDR SIMA200816401Bolt · damagedWHILE INVESTIGATING SCRATCHES ON THE NUMBER ONE AILERON MAINTENANCE DISCOVERED THAT THE NUMBER ONE AILERON DAMPENER TO AILERON ATTACHMENT FITTING BOLT WAS NOT ATTACHED TO THE AILERON. IT WAS LATER DISCOVERED THAT THE NUMBER ONE AILERON DAMPENER BOLT WAS SHEASDR DLM88080826Skin · crackedDISBOND IN SKIN AND CRACK FOUND IN SPAR ON AILERON DURING SHOP VISIT. REPAIRED PER DELTA ERA 467537-14, REV A.SDR QXEA200800595Skin · chafedRFD-C4 CHECK - RT AILERON CHAFED ON UPPER AND LOWER LEADING EDGE. BLENDED CHAFED AREA IAW CRJ SRM 57-61-01. LEADING EDGE FOUND TO BE OUT OF LIMITS IAW CRJ SRM 57-61-01. REMOVED UPPER LEADING EDGE PANEL IAW CRJ SRM 51-42-21, INSTALLED NEW LEADING EDGE IAW CRSDR COEA0811911Hinge · corrodedFOUND DURING HEAVY CHECK AT COE. FOUND LEVEL 2 CORROSION ON RT AILERON O/B HINGE FITTING ON THE AILERON HAS EXFOLIATING CORROSION. REMOVED AND REPLACED RT AILERON ASSY. (S)SDR COEA0812911Fitting · corrodedFOUND DURING HEAVY CHECK AT COE. RT AILERON CENTER TEE PICKUP FITTING I/B SIDE HAS EXFOLIATING CORROSION. REMOVED AND REPLACED RT AILERON ASSY. (S)SDR C2XA08TY054Bracket · damagedTYS - DURING C-CHECK, THE LEFT AILERON DAMPNER BRACKET WAS FOUND DAMAGED. THE BRACKET WAS REMOVED AND REPLACED IAW EMB 145 SRM 51-40-02. THE A/C IS CURRENTLY STILL IN C-CHECK.SDR HALA0800604Skin · damagedRT UPPER OUTBOARD AILERON UPPER OUTBOARD SKIN HAS A PIECE MISSING FROM THE FORWARD AND OUTBOARD SIDE. THE MIDDLE PIECE OF SKIN IS PEELED BACK. REPAIRED UPPER SURFACE RIGHT AILERON CONDUCTIVE FRAME PER SRM 57-60-02-1A-1, NOTE:O (O FOR SERVICE). AIRCRAFT RELE
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