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 C2XA07SH047Shroud · debondedSHV - DURING C-CHECK MAINTENANCE FOUND RIGHT LWR AILERON SHROUD HAS BAD BONDING ON OUTBOARD END. MAINTENANCE REPAIRED RIGHT LWR AILERON SHROUD IAW EC 5750-01315 REV D. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR DHL2007746509Tab · crackedDURING AN "C" CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; LT OUTBD AILERON BALANCE TAB, LEADING EDGE CENTER HAS A CRACK. REF NR 099154, REMOVED DAMAGED SECTION OF LT O/B AILERON BALANCE TAB L/E CENTER IAW B727 SRM 51-30-2. FABRICATED AND INSTALLED NEW SECSDR TAMF20070007SWeb · wornDURING (C) CHECK INSPECTION (TASK CARD 57-592-00) WAS FOUND WORN OUT OF LIMITS ON IB AILERON LT - OB CLOSURE RIB WEB. DAMAGE WAS REPAIRED IAW BOEING SERVICE REQUEST 1-500301558 AND EWO 767-57-024. ALSO, FAIL-SAFE FITTING PN 113T6145-11 WAS FABRICATED AND INSTSDR SWIA200718685Link · corrodedLEFT WING AILERON PCU LINK HAS SURFACE CORROSION, FOUND AT C-CHECK. REMOVED SURFACE CORROSION ON PCU LINK PER SRM 51-21-06-001-001-A01 PART 6.SDR TRBA2007049Indicator · failedFLAP UNLOCK INDICATION ON APPROACH. DECLARED EMERGENCY AND ABORTED APPROACH. LANDED WITH ZERO FLAPS. PERFORMED OP CK OF FLAP VALVE BLOCK IAW JIC NR 27-54-71. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW JIC NR 27-55-81. PERFORMED OP CK OF FLAP SYSTEMSDR SWIA200718498Aileron · wornREPLACE RIGHT AILERON DUE TO EXCESSIVE BACKLASH. REPLACED RIGHT AILERON WITH A SERVICEABLE UNIT IAW 27-15-01. OPS CHECK GOOD.SDR MAC070707Tee Fitting · corrodedDURING INSPECTION, LEVEL 2, CORROSION WAS FOUND ON THE (T-FITTINGS) ATTACHING THE RIBS TO THE SPAR. THE FITTINGS AFFECTED ARE LOCATED AT RT IB, CENTER, AND OB HINGE FITTINGS. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS IN ALUMINUM ALLOYED FITTINGS)SDR MAC070706Fitting · corrodedDURING INSPECTION, LEVEL 2 CORROSION WAS FOUND ON THE (T- FITTINGS) ATTACHING THE RIBS TO THE SPAR. THE FITTINGS AFFECTED ARE LOCATED AT THE IB, CENTER, AND OB HINGE FITTINGS. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS IN ALUMINUM ALLOYED FITTINGSSDR C2XA07TY035Bracket · wornRIGHT AILERON PCA ATTACH FITTING I/B MOST LUG WORN AND HAS CORROSION INSIDE BORE. REMOVED AND REPLACED PCA BRACKET IAW EC 5750-01177. AIRCRAFT IS STILL IN C-CHECK.SDR C2XA07TYBracket · wornRIGHT AILERON PCA ATTACH FITTING I/B MOST LUG WORN AND HAS CORROSION INSIDE BORE. REMOVED AND REPLACED PCA BRACKET IAW EC 5750-01177. AIRCRAFT IS STILL IN C-CHECK.SDR HNAA0700216Rib · crackedRIB CRACKED INSIDE RIGHT AILERON APPROX YW 444. RIGHT AILERON RIB AT STA YW 4444 (APPROX) REPLACED AND INSTALLED WITH BLIND RIVETS AS PER THE SRM 51-40-00. REPAIRED SKIN PER SRM 57-60-21.SDR 2007FA0000594Support Fitting · mismanufacturedAFTER REMOVAL OF AILERON AND SERVICE SUPPORT FITTING AT BL 9R FUSELAGE STATION 199.579. FOUND SEVERAL MISSED DRILLED/ELONGATED /FILLED FASTENER HOLES IN T CASTING P/N:25W17124, ANGLE P/N:25W171126 AND AILERON AND SERVICES SUPPORT FITTING CASTING P/N:25W353216SDR 2007FA0000593Support Fitting · damagedAFTER REMOVAL OF AILERON AND SERVICE SUPPORT FITTING AT BL 9R FUSELAGE STATION 199.579. FOUND SEVERAL MISSED DRILLED/ELONGATED /FILLED FASTENER HOLES IN T CASTING P/N:25W17124, ANGLE P/N:25W171126 AND AILERON AND SERVICES SUPPORT FITTING CASTING P/N:25W35321SDR 07FDEA02361Skin · damagedRT AILERON IS AT RIB 1 UPPER SKIN TRAILING EDGE DAMAGED REPAIR PERFORMED BY INSTALLING EXTERNAL PATCH IAW SRM 517712 PB.200 PARA 4.SDR IXXA07SMN192SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND DENTS LEFT WING OUTBOARD AILERON LEADING EDGE SKIN BETWEEN STATION 680.000 AND XA 674.000. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TSDR IXXA07SMN171SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LEFT WING INBOARD AILERON LOWER SKIN FROM STATION XA 542.000 TO STATION XA 603.000. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND DOUBLER. BONDED BOTH PARTS AS NEEDED WITH HYSOL. CLEANED, TREATSDR IXXA07SMN170SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR ON LEFT WING OUTBOARD AILERON LOWER SKIN FROM STATION XW 546.000 TO STATION XA 630.000. REMOVED SKIN WITH NON STANDARD REPAIR. FABRICATED NEW SKIN, EXTERNAL DOUBLER, AND INTERNAL DOUBLER. BONDED PARTSSDR AWXA200700847Skin · delaminatedMCN - MAJOR REPAIR - C-12 CHECK - NR 5950929, RIGHT WING AILERON INBOARD LOWER SURFACE IS DELAMINATED, WS 667 - WS 668. REPAIRED RIGHT WING AILERON INBOARD LOWER SURFACE, WS 667 - WS 668 IAW B757-200 SRM 51-70-04.SDR MAC070702Tee Fitting · corrodedDURING INSPECTION, LEVEL 2 CORROSION WAS FOUND ON A T-FITTING IN THE AILERON S/N 1257 P/N S57610250-001, MFG DATE 08/92. THE -T- REPLACED HAD EXFOLIATION CORROSION ALONG THE FITTING EDGES. LOCATED AT THE CENTER OUTBOARD SECTION. REF ATR42 SRM 57-61-10 FIG 1SDR MAC070201Tee Fitting · corrodedDURING INSPECTION, LEVEL 2 CORROSION WAS FOUND ON A T-FITTING IN THE AILERON S/N 1257, P/N S57610250-001, MFG DATE 08/92. THE T-REPLACED HAD EXFOLIATION CORROSION ALONG THE FITTING EDGES. LOCATED AT THE CENTER OUTBOARD SECTION. REF ATR42 SRM 57-61-10 FIG 10SDR ASAA0741820Skin · damagedRT AILERON IS DAMAGED AT FWD SPAR UPPER SKIN. REPAIRED AILERON IAW SRM 51-70-17 REPAIR 7 AND ASA EA 5750 02373.SDR ASAA0741791Skin · delaminatedRIGHT AILERON LOWER SURFACE IS SEPARATING. REPAIRED RIGHT AILERON LOWER SURFACE DAMAGE IAW SRM 51-70-03 REPAIR 6 PG 16.SDR ASAA0741790Skin · delaminatedRIGHT AILERON I/B FWD UPPER SURFACE PANEL IS SEPARATING AT EDGE. REPAIRED RIGHT AILERON UPPER SURFACE DAMAGE IAW SRM 51-70-03 REPAIR 6 PG 16.SDR ASAA0741789Skin · delaminatedRIGHT AILERON FWD SPAR IS SEPARATING AT I/B UNDER LWR SURFACE. REPAIRED RIGHT AILERON I/B LWR SURFACE DAMAGE IAW SRM 51-70-03 REPAIR 6 PG 16 AND EA 5760 01011.SDR 07FDEA02122Skin · corrodedLT O/B AILERON BULGING AT FASTENERS ON SKIN. [07-17-07] REMOVED DAMAGED SKIN AND INSTALLED NEW SKIN IAW SRM 51-35-01 VOL II . MAJOR REPAIR.SDR MAC060702Attach Fitting · corrodedDURING A 2 YEAR INSPECTION, LEVEL 2 CORROSION WAS FOUND ON THE T-FITTINGS ATTACHING THE RIBS TO THE SPAR. THE FITTINGS AFFECTED ARE LOCATED AT THE I/B, O/B HINGE POINTS. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS IN ALUMINUM ALLOYED FITTINGS (20SDR MAC060701Attach Fitting · corrodedDURING A 2 YEAR INSPECTION, LEVEL 2 CORROSION WAS FOUND ON THE T-FITTINGS ATTACHING THE RIBS TO THE SPAR. THE FITTINGS AFFECTED ARE LOCATED AT THE I/B, AND O/B HINGE ATTACH POINTS. THE PROBABLE CAUSE IS DISSIMILAR MATERIALS (STEEL BOLTS IN ALUMINUM ALLOYED FSDR LX5R200700004Balance Weight · detachedUPON PILOT PREFLIGHT, IT WAS DISCOVERED THAT THE RIGHT HAND AILERON HAD SOMETHING LOOSE INSIDE MOVING AROUND. THE AIRCRAFT WAS BROUGHT INTO MAINTENANCE AND THE AILERON WAS REMOVED AND IT WAS DISCOVERED THAT PART OF THE BALANCE WEIGHT HAD COME LOOSE. THE LEADSDR LX5R200700002Balance Weight · detachedUPON PILOT PREFLIGHT, IT WAS DISCOVERED THAT THE RIGHT HAND AILERON HAD SOMETHING LOOSE INSIDE MOVING AROUND. THE AIRCRAFT WAS BROUGHT INTO MAINTENANCE AND THE AILERON WAS REMOVED AND IT WAS DISCOVERED THAT PART OF THE BALANCE WEIGHT HAD COME LOOSE. THE LEADSDR SWIA200718526Bearing · corrodedLEFT AILERON PCU LINK BEARINGS AND AFT ATTACH BOLTS ARE CORRODED, DISCOVERED AT C-CHECK. INSTALLED NEW LEFT AILERON PCU OUTPUT LINKS PER CRJ200 AMM 27-14-015-400-801.SDR UIEA200700219Skin · damagedFOUND ON WALK AROUND RT OUTBD LOCATION LOWER SURFACE HAS TWO LOCATIONS WITH PREVIOUS REPAIRS NOT PAINTED. REPAIRED PER XEO 57-050807-2.SDR K11A2008120372211Skin · damagedDAMAGED SKIN RT OUTBOARD AILERON.SDR DHL2007788516Skin · delaminatedLT OB AILERON TAB HAS AREA OF DELAMINATION AT OB END UPPER SURFACE. CUTOUT DELAMINATED AREA ON LT OB AILERON TAB UPPER OB END APPROX 1" BY 3 1/2". FABRICATED FILLER APPROX 1" BY 3 1/2" AND DOUBLER APPROX 2 1/2" BY 5" FROM 2024T3 PO NR 9003621. CLEANED, PREPSDR UIEA200700210Structure · damagedRIGHT INBOARD AILERON OUTBOARD AFT CORNER DAMAGED TO PREVIOUS REPAIR APPROX 3.0" BY 4.0". REPAIRED IAW XEO- 57-042307-1SDR QXEA200700698Skin · chafedC4 OKC - RIGHT AILERON CHAFED ON TOP LEADING EDGE. REPAIRED IAW SRM 57-61-01, 51-12-00 AND 51-21-11.SDR CA070417002Rib · damaged(CAN) DAMAGE FOUND TO BOTH AILERONS ON THE (2) FIRST CENTER HINGE RIBS ASSEMBLY, ADJACENT TO THE FIXED STOPS. A/C HOURS; 4658.7, CYCLES; 2973 (TC NR 20070417002)SDR S2G2007F00001Hinge Bracket · crackedFOUND SEVERAL CRACKS IN BOTH LT AILERON HINGE BRACKETS IN RADIUS OF THE LOWER EARS. THIS WAS FOUND DURING AN ANNUAL INSPECTION. (K)SDR S2G2007F00000Hinge Bracket · crackedFOUND SEVERAL CRACKS IN BOTH LT AILERON HINGE BRACKETS IN RADIUS OF THE LOWER EARS. THIS WAS FOUND DURING AN ANNUAL INSPECTION. (K)SDR 07FDEA01242Skin · delaminatedLT WING OTBD AILERON IS DELAMINATED AT THE OTBD T/E. LT OB AILERON WAS REPAIRED ON SHOP WO NR 11841-5000-0003 REFERENCE SRM 51-40-20. LT OB AILERON IS INSTALLED AND RIGGED ON SNRM NR N00554.SDR 07FDEA01208Skin · delaminatedRT OTBD AILERON OTBD T/E UPPER AND LOWER SURFACE IS DELAMINATED FROM CORE. REMOVED AND REPLACED RT OTBD AILERON REF MM 27-10-031-2.SDR 07FDEA01145Skin · delaminatedLT WING O/B AILERON LOWER T/E SKIN IS DELAMINATED JUST O/B OF TAB. REMOVED, REPAIRED AND REINSTALLED LT O/B AILERON REF MM 27-10-031-2. REPAIR ACCOMPLISHED ON WO NR 11841-5000-0002. REMOVED TAB, REPAIRED DELAMINATED SKIN ON AILERON TE AND REINSTALLED TAB SDR USAA070228Skin · puncturedRIGHT AILERON, UPPER SURFACE, 10.5 INCHES INBOARD OF OUTBOARD EDGE PUNCTURED. REMOVED DAMAGE, LAYED UP PLIES PER EA 98560, DEFECT SIZE: .5 INCH.SDR DHL2007786526Skin · delaminatedLEFT INBD AILERON OUTBD END LOWER SURFACE IS DELAMINATED, LT STAB STA 60.21. CUTOUT DELAMINATED AREA ON LT IB AILERON TAB LOWER SURFACE 4" BY 6". FABRICATED FILLER 4" BY 6" AND DOUBLER 5 1/2" BY 7" FROM .010" 2024T3 PO NR 9003621 IAW B727 SRM 57-50-2. BONDESDR DHL2007786527Skin · delaminatedLEFT OUTBD AILERON TAB WBL 535 AND 567, T/E IS DEBONDED TWO PLACES. REMOVED LEFT OUTBD AILERON TAB IAW B727 M/M 27-10-41 AND WEIGH BEFORE REPAIR IS 3.9 LBS IAW B727 SRM 51-80-06, FIG 2. REMOVED DELAMINATION AREA 38.5" BY 5", CLEANED AND PREPPED REPAIR AREA ISDR 07FDEA00862Skin · crackedCRACKS AT 2 FASTENER HOLES AT AILERON HINGE RIB BOTTOM SKIN, LT WING. REPAIR WAS PERFORMED IAW EA 6-5720-103409 AND RAS/BAE/1003670/2006 ISSUE "A".SDR C2XA07TY012Attach Bracket · wornRIGHT AILERON ATTACH BRACKET WORN AT THE HOLES FOR THE HAT BUSHINGS. REMOVED AND REPLACED AILERON PCA BRACKET IAW EC5750-01177. AIRCRAFT IS STILL IN C-CHECK.SDR 2007UALA00792Wedge · delaminatedHAIL DAMAGE TO T/E WEDGE UPPER SKIN OF T/E DAMAGED. T/E REPAIRED. T/E WEDGE REMOVED FOR REPAIR AND REINSTALLED. UPPER SKIN FWD OF T/E SEAM DAMAGED. SEAM DAMAGE REPAIRED. AIRCRAFT READY FOR SERVICE.SDR C2XA07TY011Attach Bracket · damagedLEFT AILERON PCA ATTACH BRACKET HAS DAMAGED HAT BUSHING HOLES. REMOVED AND REPLACED BRACKET IAW EC5750-01177. AIRCRAFT IS STILL IN C-CHECK.SDR SWIA200718071Bearing · corrodedLEFT AILERON QUADRANT BEARINGS ARE CORRODED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED BEARINGS ON LEFT AILERON QUADRANT ASSEMBLY.SDR 2007FA0000206Aileron · misrepairedDURING POWER OFF (CLEAN CONFIGURATION) STALLS, THE AC WOULD SUDDENLY BREAK LEFT AND IF NOT IMMEDIATELY STOPPED COULD LEAD TO A SPIN. AFTER RERIGGING ALL FLIGHT CONTROLS, CHECKING THE AIRCRAFT ALIGNMENT WITH A LASER AND SEVERAL TEST FLIGHTS BOTH BY COMPANY PIL
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