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 C2XA08SH078Attach Bracket · damagedLEFT DAMPER ATTACHMENT BRACKET ON AILERON SPAR O/B HAT BUSHING IS MIGRATED. MX REMOVED AND REPLACED LEFT AILERON DAMPER ATTACH BRACKET IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR USAA920081145Aileron · delaminatedCLT - MAJOR REPAIR - C20 CHECK - RIGHT WING AILERON LEADING EDGE HAS DELAMINATION, WS 417. REPLACED RIGHT WING AILERON IAW US AIRWAYS TASK CARD JCR3M27015.SDR MALA080100Skin · delaminatedRT WING, RIGHT AILERON P/N 7294576-618 S/N 0266 INBOARD LEADING EDGE DELAMINATED. REPAIRED IAW EO NR S51031. COLD BOND (WET LAYUP) REPAIR IN ACCORDANCE WITH SAAB SRM 51-70-50.SDR C2XA08TY050Bracket · damagedTYS - DURING A CURRENT C-CHECK INSPECTION THE LT AILERON I/B PCA ACTUATOR ROD ATTACHMENT FITTING WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE PCA BRACKET IAW EC 5750-01177. A/C WILL BE RELEASED UPON COMPLETION OF THE C-CHECK INSPECTION.SDR SWIA200819592Link · wornFLT 4110 - EXCESSIVE AILERON TRIM REQUIRED IN ORDER TO MAINTAIN COORDINATED FLIGHT. REPLACED RIGHT AILERON LINKS, BOLTS AND BUSHINGS IAW 27-15-01.SDR SWIA200820011Skin · crackedFS 559 UNDER RT SIDE LT AILERON HAS CRACKS IN WEB FOUND AT C-CHECK. REPAIRED PER REO 601R-53-41-260 STEP 13 A-E STEP 14 C,C REV "B".
SDR C2XA08TY048Attach Bracket · wornRIGHT AILERON PCA ATTACH BRACKET WORN. REMOVED AND REPLACED PCA BRACKET IAW EC5750-01177. OPS CHECK GOOD AIRCRAFT STILL IN "C" CHECK.SDR 08FDEA01627Skin · dentedRT WING INBD AILERON HAS NUMEROUS HAIL DENTS ON UPPER SKIN. DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-61-11, MAT ID 2024-T3 PO NR 605306.1 IAW SRM 57-61-11 AND 51-21-00, PAGE 23-24 TABLE 3 SHEET 3, FABBED DOUBLER AND FILLER IAW SRM 57-61-11, FIG 206. ALODINESDR IXXA08SMN166SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD AILERON UPPER SKIN HAS IMPROPER REPAIR AT STATION XA 542.000 - 603.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, BONDED DOUBLER. BONDED PARTS AS NEEDSDR DLM88080609Fairing · damagedLT AILERON TRIM TAB ACTUATOR ROD MISSING A PORTION OF FAIRING. DRILLED AND INSTALLED PANEL O/B OF AILERON TRIM SURFACE NEED PAINTED. REMOVED PNL PAINTED AND REINSTALLED. LEFT ALL CONT TAB AND LEFT AILERON PER JIC OPERATION NR 7037 7038 7039. REQUIRED INSPESDR C2XA08SH068Attach Fitting · wornSHV - DURING C-CHECK THE RIGHT HAND AILERON TO PCA ATTACH FITTING WAS FOUND TO HAVE MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA08SH067Attach Fitting · gougedSHV - DURING C-CHECK THE LEFT HAND OUTBOARD AILERON TO PCA ATTACH FITTING WAS FOUND TO BE GOUGED AND ALSO HAD MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR HALA0800536Skin · damagedLIGHTNING STRIKE DAMAGE, L WING AILERON STATIC WICK AND AILERON BURNED TOP SIDE. REMOVED AND REPLACED LT AILERON AND TAB ASSY PER AMM 27-10-01. FUNCTIONAL CK OK.
SDR SWAA082019Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RIGHT WING AILERON LOWER SURFACE DELAMINATED. REPAIRED AILERON PER SRM.SDR S9BA200800018Channel · corrodedDURING CAMP INSPECTION, FOUND LT AILERON OB WEIGHT BALANCE CHANNEL CORRODED. REMOVED AND REPLACED WEIGHT AND BALANCE CHANNEL, AND STATIC BALANCED AILERON IAW SRM 57-50-21 PAGE 3 AND SRM RD6-57-085.SDR 08FDEA01388Wedge · crackedRIGHT OUTBD AILERON T/E WEDGE IS CRACKED ALONG THE EDGE AT THE INBD END. CUT OUT DAMAGED SECTION OF THE WEDGE IAW SRM 57-20-00; FIG 10; VOL I. FABRICATED A NEW WEDGE SECTION AND ZEE ANGLE IAW SRM 57-20-00; FIG 10; VOL I. ALODINED AND PRIMED IAW SRM 51-2SDR NSVA2008020Aileron · damagedAIRCRAFT WAS STOPPED ON TAXIWAY ANOTHER ACFT TAXIED AROUND OUR ACFT ON THE RIGHT SIDE. LEFT WINGTIP/WINGLET IMBEDDED INTO RT AILERON. AIRCRAFT RETURNED TO GATE FOR MX INSPECTION. REMOVED RT AILERON, INSPECTED RT AILERON AIRFRAME HINGES IAW SAAB SRM 51-10-00SDR C2XA08TY046Bracket · wornRIGHT AILERON PCA BRACKET BORE FOR THE BUSHING WORN. REMOVED AND REPLACED PCA BRACKET IAW EMB EC5750-01177, AIRCRAFT STILL IN C-CHECK.SDR MAC040803Tee Fitting · corrodedDURING INSPECTION LEVEL 2 CORROSION WAS FOUND ON THE AILERON "TEE PICKUPS" (TEE CLIPS) ON THE LEFT AILERON ASSEMBLY. THE EXFOLIATION CORROSION WAS ALONG THE EDGES AND SIDES OF THE FITTINGS. REFERENCE: ATR 42 SRM 57-61-10 P 115/116 FIG 1. REASON FOR INSPECTISDR MAC040802Fitting · corrodedDURING INSPECTION LEVEL 2 EXFOLIATION CORROSION WAS FOUND ALONG EDGE OF BEARING OUTER FITTING I/B ON THE RT AILERON OUTBOARD HINGE/SHACKLE ASSEMBLY. THE BEARING OUTER HINGE WAS REPLACED. INSPECTION REASON: MRB 576108-01
REFERENCE ATR 42 SRM 57-61-10 P115-11SDR 2008FA0000267Rib · bowedREMOVED THE RT AILERON DUE TO REPORTS OF BINDING BETWEEN THE AILERON AND WING DURING AEROBATIC MANEUVERS. ON THE GROUND THE IB AILERON TO AILERON BAY RIB CLEARANCE WAS APPROX .0625 INCH. IAW TECH SUPPORT THE CLEARANCE SHOULD BE .2500 INCH. THE WING IB AILERSDR CPCP20080022Hinge · corroded(4) HINGE FITTINGS OF LT AILERON TRIM TAB ARE CORRODED. LT AILERON TRIM TAB HINGE FITTING REPLACED NR 2 AND 33 IAW SRM 51-25-03.SDR C2XA08SH054Bracket · gougedSHV - DURING C-CHECK THE LEFT HAND DAMPER BRACKET WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW EMB 145XR SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA08TY041Bushing · looseRIGHT AILERON O/B PCA BRACKET FITTING HAS LOOSE BUSHING. REMOVED AND REPLACED AILERON PCA FITTING IAW EC 5750-01177 REV B. AIRCRAFT STILL IN C-CHECK.SDR SWIA200819402Aileron · damagedFLT 3903 - AILERON DAMAGE FOUND ON THE RIGHT SIDE. REPLACED RIGHT AILERON ASSEMBLY IAW CRJ 200 MM 27-15-01, PN: CC670-13000-2, SN OFF: SBRJ364.
SDR USAA920080809Aileron · delaminatedCLT - MAJOR REPAIR - Q6 CHECK - A 1" AREA OF DELAMINATION ON LEFT AILERON AT MIDDLE HINGE AREA. REPLACED AILERON IAW JOB CARD O3L30627001.SDR C2XA08SH051Bracket · wornSHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA BRACKET WAS WORN AND WOULD NOT CONTAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA08SH050Bracket · gougedSHV - DURING C-CHECK IT WAS FOUND THAT THE LT PCA BRACKET ON THE AILERON WAS GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR A6WA200840256Skin · damagedLT AILERON LEADING EDGE UPPER SKIN FOUND ABRADED. LT AILERON LEADING EDGE UPPER SKIN SHROUD REPLACED IAW CRJ 200 SRM 51-42-21. (M)SDR 08FDEA01060Skin · crackedRT OUTBD AILERON LOWER SKIN FWD EDGE IS CRACKED. REMOVED SKIN PANEL IAW SRM 51-31-01; VOL II. FABRICATED IAW SRM 57-00-01 FIG 4 PARA 12 VOL I. HEAT TREAT IAW TPS 1003 REV A. LOCATED & DRILLED HOLES IAW SRM 51-35-01 VOL II. ALODINED & PRIMED IAW SRM 51-21-SDR 08FDEA01045Panel · chafedLT WING INBD AILERON L/E INBD SURFACE CLOSE OUT PANEL HAS CHAFING WEAR. LT WING INBD AILERON L/E INBOARD SURFACE CLOSE OUT PANEL WAS WORN BEYOND ALLOWABLE LIMITS IAW SRM 57-00-01 VOL I. FABRICATED, TREATED & PRIMED IAW THE FOLLOWING SRM`S 57-00-01 VOL I & 51SDR 08FDEA01044Skin · dentedLT WING; FOUND 2 DENTS ON THE INBD AILERON LOWER SURFACE SKIN IN THE FWD OUTBD EDGE AREA. CHECKED DENT, FOUND TO BE OUT OF LIMITS IAW SRM 51-80-01 VOL II AT STA XIA 350. FABRICATED IAW SRM 57-10-00 FIG 85 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 PGS SDR C2XA08SH045Attach Fitting · damagedSHV - DURING C-CHECK RIGHT AILERON TO PCA BRACKET HAS AN ELONGATED BUSHING HOUSING. MX REMOVED AND REPLACED RIGHT AILERON TO PCA FITTING IAW EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR 08FDEA00895Wedge · crackedTHE RT OUTBD AILERON T/E WEDGE IS CRACKED AND THE AFT EDGE IS SEPARATED. CUT OUT DAMAGED SECTION OF THE WEDGE IAW SRM 57-20-00 FIG 10 VOL I. FABRICATED A NEW WEDGE SECTION & ZEE ANGLE IAW SRM 57-20-00 FIG 10 VOL I. ALODINED & PRIMED IAW SRM 51-21-01 VOL SDR 08FDEA00894Skin · departedRT OUTBD AILERON UPPER SKIN HAS NUMEROUS DENTS. MEASURED DEPTH IS .056. FOUND TO BE WITHIN LIMITS IAW SRM 51-80-01; PROCEDURE "F" PG 1 VOL II. MINOR REPAIRSDR 08FDEA00893Wedge · crackedRT OUTBD AILERON T/E WEDGE IS CRACKED AND THE AFT EDGE IS SEPARATED. THIS SDR WAS OPENED FOR AIRCRAFT N425FE INSTEAD OF AIRCRAFT N365FE IN ERROR. SDR 08-0895 HAS BEEN INITIATED TO ADDRESS THE DISCREPANCY DOCUMENTED ON NON-ROUTINE N00026 THAT WAS WRITTEN AGAISDR C2XA08SH041Fitting · wornSHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA ACTUATOR ATTACHMENT FITTING ON THE AILERON SPAR HAD MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC 5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SSDR C2XA08SH040Fitting · wornSHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA ACTUATOR ATTACHMENT FITTING ON THE AILERON SPAR HAD MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SESDR TAMF20080006SWeb · chafedDURING C CHECK INSPECTION, FOUND CLOSURE RIB WEB WITH CHAFING OUT OF LIMITS AT LT WING INBOARD AILERON. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-033 AND BOEING SERVICE REQUEST 1-773827820. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.SDR TAMF20080002SRib · chafedDURING INSPECTION CHECK, FOUND A WEAR OUT OF LIMITS ON INBOARD AILERON RT OUTBOARD CLOSURE RIB WEB. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-034 AND BOEING SERVICE REQUEST 1-773827820. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.SDR F3LA200800071Seal · corrodedDURING C5 C CHECK, MAINTENANCE REPORTED CORROSION FOUND ON RIGHT WING AILERON HINGE SEAL NEAR OUTBOARD HINGE LOCATION. MAINTENANCE REMOVED AND REPLACED AILERON SEAL IN ACCORDANCE WITH REQUIREMENTS OF A319 SRM 51-72-11 AND EA A9-57R-30062. TOUCH PAINTING PERFSDR IXXA08SMN078SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT INBOARD AILERON UPPER SKIN HAS DENT AND NO STANDARD REPAIR AT STATION XA 580.000 TO XA 610.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTSDR MAC020804Tee Fitting · corrodedDURING INSPECTION LEVEL 2 CORROSION WAS FOUND ON A TEE FITTING INSIDE THE RIGHT WING AILERON. THE AILERON WAS REPLACED.SDR C2XA08SH021Bushing · migratedSHV - DURING C-CHECK RT WING AILERON ATTACHMENT BRACKET TO PCA HAS MIGRATING HAT BUSHING. MX REMOVED AND REPLACED RT WING AILERON ATTACHMENT BRACKET IAW EC5750-01177 REV B. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.SDR UPS08M51860Skin · gougedINSPECTION TYPE:3C RT WING IB AILERON UPPER SURFACE AT OB VERY LE HAS 5 INCH LONG DEEP GOUGE RUNNING THRU REPAIR DOUBLER. REMOVED PREVIOUS REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER PER MD-11 SRM 57-00-01 AND 51-SDR IXXA08SMN054SSkin · scratchedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD AILERON LOWER SKIN SCRATCHED BETWEEN STATION XA 737.000 AND XA 763.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH SDR USAA920080419Skin · crackedCLT - MAJOR REPAIR - Q5 CHECK - RIGHT WING AILERON UPPER SKIN CRACKED. REPAIRED RIGHT WING AILERON UPPER SKIN IAW B737 SRM 57-70-17.SDR HNJ2008F00000Spar · crackedLT AILERON SPAR CRACKED AT CENTER AND OB HINGE BRACKET ATTACH POINTS. POSSIBLY DUE TO TWISTING EFFECT OF AILERON ACTUATOR INSTALLED AT EXTREME IB END OF AILERON. (K)SDR C2XA08SH020Housing · damagedSHV - DURING C-CHECK LEFT AILERON O/B MOST FITTING (FOR PCA ATTACHMENT) FLANGER BUSHING HOUSING (ON BRACKET) IS ELONGATED. MX REMOVED AND REPLACED LEFT AILERON O/B MOST FITTING FLANGER BUSHING HOUSING IAW EC5750-01177. THE AIRCRAFT WAS APPROVED TO RETURN FORSDR QXEA200800190Skin · damagedPDX - C5 CHECK - LEFT AILERON OUTBOARD TRAILING EDGE JUST OUTBOARD OF STATIC WICK APPEARS TO BE A LIGHTING EXIT POINT. REMOVED TRAILING EDGE AND INSTALLED NEW TRAILING EDGE IAW DHC8 200 SRM 51-40-00, 51-20-26, 57-60-71 PARA 2B. PERFORMED WICK CHECK IAW DHC8 2
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