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 = '5541' 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 = '5541' 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 CALA0600152Rib · crackedINSPECTION FOUND A 1.3 INCH CRACK IN VERTICAL STABILIZER FRAME (VERT STAB T/E HINGE RIB) WHERE RUDDER RIG PIN R-5 GOES THROUGH FEEL AND CENTERING FRAME. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5530-01445, PART 3.SDR CA060510002Rib · crackedAT A 100 HOUR INSPECTION A CRACK WAS FOUND UNDER THE LEFT INBOARD RUDDER BAR BLOCK, AT THE MOST FORWARD BOLT HOLE. RUDDER BLOCK HAD ABNORMAL MOVEMENT. CRACK COULD ONLY BEEN SEEN AFTER BLOCK WAS REMOVED.SDR WRNA20060030Spar · corrodedDURING M72 CHECK, FOUND CORROSION ON RUDDER SPAR BOX ANGLE AT RIBS RR20 AND RR38. REMOVED CORROSION AND INSTALLED DOUBLERS PER EMTEQ REPAIR ORDER 2-41054-801SDR ASAA0640412Frame · leakingFOUND RUDDER T/E HAS LIGHTING STRIKE 10" FROM TOP ON LT SIDE. REMOVED DAMAGED CONDUCTIVE FRAME FABRICATED AND INSTALLED REPLACEMENT CONDUCTIVE FRAME PER SRM.SDR 2006FA0000321Rib · missingRUDDER WAS REMOVED TO REPLACE CRACKED CORRUGATED SKIN BETWEEN LOWER TWO RIBS. ON SKIN REMOVAL, IT WAS DISCOVERED THAT SLANT RIB 0531005-1, (EXTENSION OF REAR SPAR) WAS MISSING. THERE WERE NO HOLES DRILLED IN BOTTOM RIB P/N 0531001-25 OR RIB P/N 0531001-22 TO WSDR 2005FA0001114Spar · brokenTHE UPPER RUDDER SPAR WAS BROKEN 12.5 INCHES ABOVE THE UPPER HINGE. IN ADDITION, THE SPAR CRACKED UNDER THE UPPER HINGE FITTINGS. THIS CAUSED THE RUDDER COUNTER BALANCE TO BE LOOSE RESULTING IN RUDDER FLUTTER. FURTHER FLIGHT COULD HAVE RESULTED IN LOSS OF RSDR 2005UALA00722Rib · lightning strikeELECTRICAL DISCHARGE ON RT OUTBD ANCHOR NUT HOLE ON RIB FITTING ASSY STA 522.702. RUDDER RIB FITTING WAS DAMAGED FROM A LIGHTNING STRIKE AND WAS REPLACED PER BAC DWG 175W5109, SRM 51-40-02.SDR DHL2005802541Web · crackedRUDDER L/E FRONT SPAR FWD NOSE RIB WEB CRACK 1.500 STA ZR 71.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DOUGLAS DWG 5700556, JC EA55100012-001-D. REMOVED DAMAGED RIB IAW SRM 51-1-21 PG. 1. FABRICATED NEW RIB (AL2024"O" 0.063) IAW DWG 5700556, EA SEMAN 2005SDR 2005FA0000801Plate · debondedDURING FLEET-WIDE INSPECTION OF AIRCRAFT, TECH FOUND EXCESSIVE MOVEMENT BETWEEN RUDDER AND RUDDER LEVER ASSY. FURTHER INSPECTION SHOWED DISBONDING BETWEEN THE RUDDER SPAR AND THE RUDDER LEVER ASSY SPACER PLATE. PROBABLE CAUSE APPEARS TO BE EXCESSIVE FLEXING SDR 2005FA0000800Plate · debondedDURING FLEET - WIDE INSPECTION OF AIRCRAFT, TECH FOUND EXCESSIVE MOVEMENT BETWEEN RUDDER AND RUDDER LEVER ASSY. FURTHER INSPECTION SHOWED DISBONDING BETWEEN THE RUDDER SPAR AND THE RUDDER LEVER ASSY SPACER PLATE. PROBABLE CAUSE APPEARS TO BE EXCESSIVE FLEXINSDR 2005FA0000799Plate · debondedDURING ROUTINE INSPECTION OF AIRCRAFT, TECH FOUND EXCESSIVE MOVEMENT BETWEEN RUDDER AND RUDDER LEVER ASSY. FURTHER INSPECTION SHOWED DISBONDING BETWEEN THE RUDDER SPAR AND THE RUDDER LEVER ASSY SPACER PLATE. PROBABLE CAUSE APPEARS TO BE EXCESSIVE FLEXING OF SDR CA050503001Spar · crackedRUDDER TORQUE TUBE P/N 101-630010-9 LOWER ATTACH BOLTS (3) FOUND LOOSE, HOLES IN TORQUE TUBE ELONGATED. RUDDER CONTROL HORN P/N 101-524059-1 DAMAGED AT CENTER ATTACH HOLE DUE BENT ATTACH BOLT, BEARING P/N MS28913-5C DAMAGED FROM BOLT. ALL ABOVE PARTS REPLACESDR USAA050355Spar · chippedPIT - Q4 - RUDDER L/E SPAR, .2500 INCH X .1250 INCH DEEP CHIP IN EDGE CHIP, LT L/E SPAR TAB. BLEND OUT REPAIR, HFEC INSPECTION AND VISUAL, SEALED IAW EA 79967. (K)SDR USAA041060Frame · separatedPIT - Q5 - CONDUCTIVITY FRAME, 15 INCHES X 12 INCHES, SEPARATION, RUDDER TOP LT SURFACE, UPPER LT CONDUCTIVITY FRAME SEPARATING FROM RUDDER. INSTALLED NEW CONDUCTIVITY FRAME IAW MM AND BAC 5010 AND DWG 65C25841.SDR 2005FA0001126Rib · crackedCRACK WAS FOUND IN THE RIB THAT ATTACHES THE RUDDER COUNTER WEIGHTS. THIS HAS BEEN NOTICED IN THE PAST, THE FIX IS TO REPLACE RIB. PARTS NO LONGER AVAILABLE. NOTICED THIS ON AIRFRAMES WITH MORE THAN 4000 HOURS. (K)SDR 2005FA0000375Spar · crackedDURING SERVICE OF THE AIRCRAFT THE RUDDER WAS REMOVED. NOTHING WAS FOUND ABNORMAL. REMOVAL OF THE UPPER RUDDER HINGE (PN 2018300). CRACKS WERE FOUND AT THE HINGE ATTACH POINT OF THE RUDDER SPAR (2072910). (K)SDR 2005FA0000374Spar · crackedDURING SERVICE OF AIRCRAFT THE RUDDER WAS REMOVED. NOTHING WAS FOUND ABNORMAL. REMOVAL OF THE UPPER RUDDER HINGE (PN 2018300. CRACKS WERE FOUND AT THE HINGE ATTACH POINT OF THE RUDDER SPAR (2072910). (WP07200505589) (K)SDR 2005FA0000373Rib · corrodedDURING AN ANNUAL INSPECTION, MORE THAN NORMAL SURFACE CORROSION WAS FOUND ON THE RUDDER TAIL POST. UPON DISASSEMBLY OF THE RUDDER, DISSIMILAR METAL CORROSION WAS PRESENT WHERE THE STEEL STIFFENER ATTACHES TO THE LOWER RIB (PN 2072904). (WP07200505592) (K)SDR LR7A04111Angle · crackedDURING SCHEDULED C6 INSPECTION IAW JOB CARD HC5511, FOUND RUDDER TRIM ACTUATOR MOUNT ASSY LT AND RT MAIN ATTACH ANGLES CRACKED AND WORN AT FS 1129, VSS 98, LBL 2 AND RBL 2. REPAIRED IAWEA 382-55-04-069. NR 0297.SDR LR7A04102Beam · crackedDURING SCHEDULED C6 INSPECTION PER JOB CARD HC5511 FOUND RUDDER INTERNAL AUX BEAM AND STIFFENERS WITH CRACKS AT FS 1128.5, BL 0, VSS 10. REPAIRED IAW SRM SMP 583 51-140-18. BALANCE CHECK CARRIED OUT IAW SMP 583 51-50, PARA D.SDR MALA040545Frame · chafedDURING C-CHECK INSPECTION, RUDDER HINGE A-FRAME AT RB 10 WAS FOUND WITH THE AFT RUDDER ATTACH BEARING OUT OF THE FRAME. THE A-FRAME WAS CHAFED AS WELL AS CHAFFING DAMAGE TO THE RUDDER. REPAIRS CARRIED OUT ON 409 NR 186829.SDR QXEA200400362Rib · damagedPDX - RIGHT HAND UPPER PORTION OF THE RUDDER HAS A SMALL CREASE BETWEEN RIB. REPAIRED IAW HORIZON AIR EA 6-27-161.SDR 2004FA0000532Spar · crackedLT SKIN CRACKED 6 INCHES AFT OF LOWER RUDDER HINGE POINT. RT SKIN WRINKLED 6 INCHES AFT OF LOWER HINGE POINT. LOWER RIB CRACKED 5 INCHES AFT OF SECURING POINT TO FORWARD RUDDER SPAR, CRACKED ON LT SIDE. PROBABLE CAUSE UNNECESSARY ROUGHNESS. (WP25200404045)SDR 2004FA0000531Spar · crackedLT SKIN CRACKED 6 INCHES AFT OF LOWER RUDDER HINGE POINT. RT SKIN WRINKLED 6 INCHES AFT OF LOWER HINGE POINT. LOWER RIB CRACKED 5 INCHES AFT OF SECURING POINT TO FORWARD RUDDER SPAR, CRACKED ON LT SIDE. PROBABLE CAUSE UNNECESSARY ROUGHNESS. (WP25200406045)SDR 2004FA0000530Spar · crackedLT SKIN CRACKED 6 INCHES AFT OF LOWER RUDDER HINGE POINT. RT SKIN WRINKLED 6 INCHES AFT OF LOWER HINGE POINT. LOWER RIB CRACKED 5 INCHES AFT OF SECURING POINT TO FORWARD RUDDER SPAR, CRACKED ON LT SIDE. PROBABLE CAUSE UNNECESSARY ROUGHNESS. (WP25200406045)SDR OG52004F00000Spar · crackedUPPER SPAR CRACKED ON BOTH SIDES FROM THE TOP TO THE BOTTOM ABOUT AN INCH IN LENGTH. THE CRACK IS ALL THE WAY THROUGH THE SPAR AND ALSO THE DOUBLER.SDR 2004FA0000344Spar · crackedFOUND RUDDER SPAR CRACKED AT LIGHTENING HOLE JUST UNDER TOP RUDDER MOUNTING HINGE. 4 CRACKS WERE PRESENT, THE LONGEST WAS .5 INCH. RECOMMEND INSPECTION EVERY 100 HOURS, REPLACE WITH NEW SPAR MISSING LIGHTENING HOLE IF DEFECTIVE.SDR DHL2004806573Rib · crackedRUDDER STRUCTURAL RIB CRACKED 2.000 AT STA ZR 101.000 (REF CTR DAMPER). REMOVED CRACKED RIB IAW SRM 51-1-21 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW RIB IAW SRM 51-1-21 PG 1.SDR 2004FA0000130Spar · crackedCRACKS FOUND ADJACENT TO UPPER HINGE BRACKET ATTACH HOLES ON RUDDER SPAR. FOUR CRACKS FOUND, EACH BETWEEN .7500 INCH AND 1 INCH LONG. ONE WAS VISIBLE, OTHERS FOUND USING DYE PENTRANT. CRACKS CANNOT BE SEEN WITHOUT REMOVAL OF THE HINGE BRACKET.SDR 2004FA0000129Spar · crackedCRACKS FOUND ADJACENT TO UPPER HINGE BRACKET ATTACH HOLES ON RUDDER SPAR. FOUR CRACKS FOUND, EACH BETWEEN .7500 INCH AND 1 INCH LONG. ONE WAS VISIBLE, OTHERS FOUND USING DYE PENTRANT. CRACKS CANNOT BE SEEN WITHOUT REMOVAL OF THE HINGE BRACKET.SDR QXEA200301562Rib · crackedPDX - FORE RUDDER LOWER CLOSING RIB IS CRACKED. REPLACED IAW DHC-8-200 SRM 51-40-11.SDR C2XA03TY206Spar · crackedDURING A SCHEDULED INSPECTION DAMAGE WAS FOUND ON THE RUDDER 1 AFT SPAR. MAINTENANCE ACCOMPLISHED A SPLICE REPAIR IAW EC 5540-01022 AND EMB CPM 51-21-04/05, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF INSPECTION.SDR AWXA200301243Rib · crackedDURING C-17 CHECK A .5 INCH CRACK WAS FOUND ON BRACKET BELOW UPPER RUDDER HINGE, AT RDR STA 196. MAINTENANCE REMOVED CRACKED BRACKET BELOW UPPER RUDDER HINGE AT RDR STA 196; FABRICATED A NEW REPLACEMENT BRACKET PER DWG 65C25971; INSTALLED REPAIR PART IAW B737SDR QXEA200301167Skin · dentedFORE RUDDER HAS A DENT 4 INCHES FROM LOWER CENTER HINGE. REPAIRED IAW Q400 SRM 51-25-05-370-801, RD 8/4-55-126 AND HORIZON AIR EA 6-55-54.SDR QXEA200300816Rib · damagedPDX - TRAILING RUDDER HAS DAMAGE NINE RIBS DOWN FROM TOP OF TRAILING RUDDER. REPAIRED IAW HORIZON AIR EA 6-55-46.SDR CA030410005Rib · cracked(CAN) REPOSITIONED RUBBER AND REPLACED CRACKED RIB.SDR DXJ2003F00000Rib · crackedRUDDER OF A/C WAS REMOVED FOR REPAIRS DUE TO CRACKS FOUND BY X-RAY INSP IAW INSTRUCTIONS IN SB. X-RAY INSP REVEALED APPROX 30 CRACKS OF INTERNAL RIB RIVET HOLE DIMPLES AT VARIOUS RIB LOCATIONS THROUGHOUT RUDDER ASSY. UPON DISASSEMBLY OF RUDDER, A VISUAL INSPSDR C2XA02SH152Rib · crackedSHV- DURING C-CHECK RIB FOUND CRACKED ON RUDDER NUMBER 1 AT LOWER CENTER HINGE BRACKET. MAINTENANCE REMOVED AND REPLACED AFFECTED RIB IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.SDR QXEA0202212Rib · crackedPDX- CRACK BEYOND SERVICEABLE LIMITS ON FORE RUDDER LOWER CLOSING RIB. REPAIRED IAW DHC-8 SRM 51-40-11 AND HORIZON AIR TASK 27-20-11-030-802.SDR CA021211001Spar · cracked(CAN) THE RUDDER WAS REMOVED DUE TO A DAMAGED SKIN. WHEN THE SKIN WAS REMOVED THE UPPER SPAR WAS FOUND CRACKED AT THE HOLE FOR A NUT PLATE TO ATTACH TO. THIS NUT PLATE IS USED TO HOLD THE UPPER HINGE TO THE RUDDER. SPAR WAS REPLACEDSDR QXEA0201933Rib · crackedPDX-RIB NR 30 ON TRAILING RUDDER HAS A 3.5 INCH CRACK ON UPPER LEFT HAND SIDE. REPAIRED IAW HORIZON AIR EA. 6-55-19.SDR USAA020374Frame · corrodedPIT - FOUND FRAME CORRODED, BALANCE ASSEMBLY END FRAME ON RUDDER. CORRODED LEVEL 2. REPLACED DEFECTIVE PART WITH IDENTICAL PART PER OM-26 AND JPC J3-65-27500-005. (M)SDR SWIA200211226Rib · damagedRIB IN RUDDER 1 DAMAGED JUST BELOW GREEN RUDDER ACTUATOR ATTACH POINT. DISCOVERED DURING C-CHECK. REPLACED DAMAGED RIB IAW 120 SRM 51-10-02.SDR QXEA0201194Rib · dentedPDX-FORE RUDDER, LOWER RIB IS DENTED. REPAIRED IAW DHC8 SRM 51-40-11 AND SRM 51-20-51.SDR UPS02839036Rib · crackedINSPECTION TYPE:C2 RUDDER RIB CRACKED STA ZR 135. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5656223 AND SRM 51-1-21.SDR UPS02839035Rib · crackedINSPECTION TYPE:C2 RUDDER RIB CRACKED AT STA ZR 140. REMOVED, FABRICATED, AND REPLACED RIB IAW DWG 5656223 AND SRM 51-1-21.SDR QXEA0201138Rib · corrodedPDX- FORE RUDDER CLOSING RIB OUTSIDE SURFACE HAS FRETTING CORROSION AROUND RIVET HOLES. REPAIRED IAW DHC-8 MM TASK 27-20-11-030-802, DHC-8 SRM 51-40-06, 51-40-11 AND 27-20-11.SDR CA020719006Spar · cracked(CAN) DURING A PHASE 2 INSPECTION IT WAS NOTED THAT THE RUDDER SPAR WAS CRACKED APPROXIMATELY 1.3 INCH, WHERE THE CENTRE HINGE BRACKET ATTACHES. THE CRACK WAS RUNNING VERTICALLY ALONG THE LT NUT PLATE FOR ATTACHING THE HINGE BRACKET. UPON REMOVAL OF THE SPAR ISDR USAA020184Rib · corrodedPIT - FOUND RUDDER CORRODED 3 INCHES BY 12 INCH AREA, COVER FACE OF RIB BEHIND BALANCE WEIGHTS ON BEAM. REPLACED RIB PER SRM 51-10-02, 51-20-01, 51-20-00 AND 51-40-02. (M)SDR QXEA0101951Stringer · brokenPDX - RUDDER, RT STRINGER BROKEN AT RIB 6, BEHIND PANEL 57Y. REPAIRED IAW FOKKER SRM 51-31-01.
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