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 2003UALA00681Fitting · crackedLT AILERON PCU FITTING CRACKED IN 3 PLACES AND RT AILERON PCU FITTING CRACKED IN 1 PLACE. REPLACED BOTH AILERONS.SDR CA030714001Counterweight · torn(CAN) PILOT DISCOVERED ON HIS POST FLIGHT WALKAROUND THAT THE LT AILERON COUNTERWIEGHTWAS HANGING DOWN ON THE INBOARD END OF THE AILERON. THE AILERON WAS REMOVED AND THE BALANCE WEIGHT WAS FOUND TO HAVE TORN OUT OF THE INBOARD BOLT HOLE. THE DAMAGED PART OF THSDR 2003FA0000715Hinge · failedDURING 50 HR INSPECTION THE TECH FOUND THE RETAINING CLIP COMING OUT OF BEARING.SDR AUS20030693Rivet · faulty(AUS) AILERON MASS BALANCE WEIGHT ATTACHMENT RIVETS FAULTY. APPROXIMATELY HALF OF THE RIVETS FAILED TESTING AND INSPECTION IAW AD/CESSNA180/28.SDR SWAA031495Frame · crackedAIRCRAFT REQUIRES EXCESSIVE LEFT AILERON TO FLY STRAIGHT. FOUND NR 7 CANOE FAIRING A FRAME CRACKED. REMOVED AND REPLACED A FRAME PER MM.SDR DHL2003873554Skin · dentedRT OTBD. AILERON 0.750 DENTED ON UPPER PLATING AT ZA.651.000. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG 2X PG 30-31. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. TRIMMED OUT DAMAGED AREA IAW SRM 57-2-1 FIG 2X PG 30-31. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-SDR DHL2003604672Skin · damagedLT IB AILERON LWR SURFACE WITH INTERIM REPAIR BETWEEN STA.XA441.000 AND XA.502.000. PERFORMED MAJOR REPAIR IAW EODHL-030569, ED-3399. REMOVED FASTENERS AND DAMAGED SKIN SEGMENT INCLUDING INTERIM REPAIR IAW SRM 51-1-21 PG.1. FABRICATED NEW SKIN SEGMENT (2024-TSDR DHL2003604663Skin · crackedLT WING INBD. AILERON L/E UPPER PLATING HAS THREE CRACKS OF 0.750, 0.500, 0.500 AT STA. XA 487.000 - XA 569.000. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 57-8-1 FIG.1. REMOVED DAMAGED PLATING IAW SRM 51-1-21 PG. 1. CLEANED, TREATED AND PRIMED AREA IAW SDR DHL2003604592Panel · damagedLT WING INBD AILERON UPPER PLATING SHOWS INTERIM REPAIRS BETWEEN STA XA 441.000 - XA 542.000. PERFORMED MAJOR REPAIR IAW EODHL-030570, ED-3398. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED DAMAGED SKIN PANEL IAW EODHL-030570, ED-3398. CLEANED, TREATED ASDR UPS03240920Hinge · crackedINSPECTION TYPE: C, LT O/B AILERON I/B BALANCE BAY FWD PANEL IDLER HINGE CRACKED & BROKEN. REPLACED LT O/B AILERON I/B BALANCE BAY FWD PANEL IDLER HINGE IAW MM 27-10-04 & ON REMOVAL OF HINGE, PIN FOUND TO BE DAMAGED, PIN REPLACED IAW MM 27-10-04.SDR SWAA031290Aileron · delaminatedDURING SCHEDULED PM CHECK, FOUND LT AILERON DELAMINATED AT T/E. REMOVED AND REPLACED LEFT AILERON PER MM.SDR 349811Block · separatedTUNGSTEN BLOCK (BALLAST WEIGHT) AT OUTBOARD END OF LT AILERON FOUND SEPARATED FROM MAIN COUNTER WEIGHT. BLOCK SLID FORWARD AGAINST WING REAR BEAM AND WAS RESTRICTING AILERON DOWNWARD MOVEMENT. PROBABLE CAUSE: LOOSE AND MISSING HARDWARE. ONE SCREW AND TWO NSDR QXEA200300696Skin · chafedCKB - RIGHT HAND AILERON LEADING EDGE UPPER SURFACE CHAFED. REPAIRED IAW CRJ 700 SRM 51-25-01.SDR DHL2003604700Support Fitting · crackedRT INBD AILERON INBD SUPPORT FITTING ASSY AT STA. XA.448.000 WITH 1.000 CRACK IN IT. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG.1, SRM 51-1-20D PG.9,21. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NSDR AUS20030541Doubler · cracked(AUS) RT AILERON OUTBOARD HINGE DOUBLER CRACKED. FOUND DURING INSPECTION IAW AD/PA28/16A2.SDR 2003FA0000519Structure · debondedTHE AILERON IS AN ALL ALUMINUM BONDED ASSEMBLY. THE AILERON WAS REPAIRED BY REPLACING THE AFT SKIN, USING DER APPROVED DATA AND WAS RETURNED TO SERVICE 11-15-2002. ON 05-08-2003 A BOND LINE SEPARATION WAS DISCOVERED ON A SKIN EDGE. REVIEW OF THE REPAIR PROCSDR AMTA200300745Structure · damagedRT INBOARD AILERON INBOARD SUPPORT FITTING ATTACHMENT HOLE GOUGED. REPAIRED FITTING IAW ER/A L10-57R-5157. (M)SDR DL76S030395Skin · delaminatedDELAMINATED SPOT ON LEFT OUTBOARD AILERON. REPAIRED AILERON.SDR CA030725001Counterweight · loose(CAN) RT AILERON BALANCE WEIGHT ARM RIVETS FOUND LOOSESDR UPS03240545Hinge · corrodedINSPECTION TYPE: C&SI, O/B AILERON, LT WING, O/B TAB HINGE HAS EXCESSIVE CORROSION 2ND I/ B IS CRACKED AND THE OTHER TWO ARE PITTED EXTENSIVELY. TAB HINGES REPLACED IAW SRM 51-30-02 FOR O/B AILERON TAB INSTALLATION REF. NRC 664356SDR DHL2003801036Skin · crackedLT OUTBOARD AILERON NOSE PLATING WITH TWO CRACKS OF 1.000 AND 0.500 INCH BETWEEN STA XA 674.000 AND 752.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-8-1 PG 9 FIG 4. REMOVED DAMAGED NOSE PLATING SKIN IAW SRM 51-1-21 PG 1. FABRICATED NEW SKIN (2024-TSDR DHL2003801041Structure · crackedLT WING- LT AILERON T/E CRACKED 0.500 INCH BETWEEN STA XA 715.000 AND XA 780.000. REMOVED AILERON T/E (CRACKED) IAW SRM 51-1-21A PG 3-4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW T/E (2024-T3 AL0.020) IAW SRM 57-8-1 PG 8. CLEANED, TRSDR DHL2003801075Skin · crackedLT WING LT AILERON T/E CRACKED 0.500 INCH BETWEEN STA XA 622.00 AND STA XA 662.000. REMOVED AILERON T/E (CRACKED) IAW SRM 51-1-21A PG 3-4. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED NEW T/E (2024-T3 AL0.020) IAW SRM 57-8-1 PG 8. CLEANED, SDR CALA0300196Skin · dentedTHE RT AILERON SKIN WAS DENTED IN THREE PLACES BY HAIL. THE DENTS MEASURED 0.023 INCH DEEP X 0.75 INCH DIAMETER, 0.031 INCH DEEP X 0.75 INCH DIAMETER, AND 0.028 INCH DEEP X 1 INCH DIAMETER. THE SKIN WAS REPAIRED IAW ECRA 5760-01008.SDR CALA0300195Skin · dentedTHE LT AILERON UPPER SKIN WAS DENTED BY HAIL. ONE DENT MEASURED 0.027 INCH DEEP AND 1.25 INCH DIAMETER. THE OTHER MEASURED 0.031 INCH DEEP AND 0.75 INCH DIAMETER. THE DAMAGED SKIN WAS REPAIRED IAW ECRA 5760-01007.SDR UPS03M40909Support · corrodedINSPECTION TYPE: RT WING FWD INBOARD AILERON FOUND CORROSION AT PANEL SUPPORT FROM ST A XW=291 TO XW=373 AS MARK. CORROSION ON PANEL SUPPORT RT WING STA XW291 TO XW373 REMOVED AND PROTECTED IAW SRM 51-21-01 VOLIIREV32. FOUND OUT OF LIMIT IAW SRM 57-00-0 1 VOSDR ASAA0310190Fitting · crackedOKC - DURING D-CHECK, FOUND RIGHT AILERON NR 1 HINGE FITTING AT WING STATION 517.757 CRACKED. REMOVED DAMAGE, FORMED, FABRICATED ADN INSTALLED REPAIR ANGLE PER SRM. (M)SDR AUS20030394Doubler · cracked(AUS) AILERON SPAR OUTBOARD HINGE DOUBLER CRACKED. FOUND DURING INSPECTION IAW AD/PA31/118.SDR CA030317007Skin · cracked(CAN) 1/2 INCH CRACK ON TOP SKIN OF LT AILERON FROM TRIM TAB OPENING FAR OUTBOARD CORNER TO FIRST RIVET.SDR CA030312014Skin · cracked(CAN) .5 INCH CRACK FROM TRIM TAB OPENING OUTBOARD CORNER TO FIRST RIVET.SDR CA030726006Rivet · loose(CAN) LOOSE RIVETS ON BOTH WINGS AT AILERON HINGE BRACKET REPLACED.SDR ASAA0380142Panel · crackedOKC - FOUND DURING 30K CHECK, RIGHT AILERON HINGE PANEL NR 3 IS CRACKED AT DRAIN HOLE. STOP DRILLED CRACK AND VERIFIED CONTAINMENT BY EDDY CURRENT INSPECTION PER SRM 51-01. (M)SDR PCAA0303051Aileron · crackedDURING C LEVEL INSPECTION LEFT AILERON SKIN FOUND TO BE CRACKED AT OUTBOARD ATTACH POINT, LOWER SKIN AT CORNER OF ATTACH POINT CUT OUT. CRACK WAS REPAIRED IN ACCORDANCE WITH PIEDMONT ENGINEERING DRAWING EO8-57-03-0248 AND APPROVED THROUGH CALLAHAN REPAIR SERVISDR 2003FA0000226Pushrod · looseAILERON RODEND JAM NUTS FOUND LOOSE. HAVE FOUND SIMULAR CONDITION ON PREVIOUS AIRCRAFT NEW FROM FACTORY.SDR DHL2003804909Skin · crackedLT INBOARD AILERON L/E UPPER SKIN SURFACE WITH 0.500 INCH CRACK AT STA XA.502.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, SRM 57-8-1 PG 2. REMOVED UPPER SKIN ON LT INBOARD AILERON L/E STA XA. 502.000 IAW SRM 51-1-21 PG 1. FABRICATED NEW SDR CA030211001Rib · cracked(CAN) CRACKED RIB FLANGE OUTBOARD MOST RIB WING STATION 376.20.SDR C2XA03TY015Bracket · damagedTYS, During a scheduled inspection both left hand outbd aileron PCA attachmrnt points have migrating bushings. Maintenance removed and replaced the aileron attchment bracket I/A/W-EMB-SRM-51-21-04/05/06 and EC5750-0117. Aircraft will be released to service upoSDR CA030129005Skin · cracked(CAN) A 1.5 CENTIMETER CRACK FOUND RADIATING FROM A RIVET ON SECOND RIB FROM INBOARD EDGE AND LAST RIVET HOLE BEFORE THE TRAILING EDGE. ANOTHER .5 CENTIMETER CRACK IN SKIN FOUND RADIATING FROM THE SECOND RIVET FROM THE TRAILING EDGE ON THE THIRD RIB. THE CRASDR ASAA0240023Bracket · crackedPAE - DURING C-CHECK, FOUND CRACKED BRACKET RIGHT AILERON INBOARD BALANCE BAY OUTBOARD RIB FITTING AND WEB. REPAIRED IAW SRM. (M)SDR 2003UALA00116Aileron · crackedIN DIRECT FLIGHT CONTROL YAW, AIRCRAFT ROLLED LEFT AND REQUIRED 2 UNITS RH YOKE TO LEVEL WINGS. WITH WINGS LEVEL USING RUDDER, LH OB AILERON TE IS UP. INSPECTION OF THE LEFT AILERON FOUND THE INBOARD ATTACH FITTING AT FRONT SPAR CRACKED ON THE INBOARD AND SDR C2XA03TY004Attach Fitting · damagedDURING A SCHEDULED 3-C INSPECTION THE RT AILERON PCA ATTACH FITTING WAS FOUND DAMAGE AND THE BOLT FROZEN. MAINTENANCE REMOVED AND REPLACED THE RT HAND AILERON PCA ATTACH FITTING, PRIMED AND PAINTED IAW EC 5750-01177. ALL WORK WAS ACCOMPLISHED AND WILL BE RELSDR HALA0300012Skin · corrodedHNL - LEVEL 2 CORROSION ON RIGHT AILERON UNDER THE 9957571-23 RUBSTRIP IS BETWEEN XA 374.00 AND XA 382.125. THE CORROSION AFFECTED THE 995757-34 DOUBLER AND 9957571-36 SKIN. THESE 2 PARTS HAD 100 PERCENT CORROSION PENETRATION. THE AILERON WAS REPLACED PER BSDR SWAA030014Aileron · delaminatedDURING SCHEDULED C2 CHECK, FOUND LT AILERON DELAMINATED ON LOWER SKIN BETWEEN NR 2 AND NR 3 HINGES. REMOVED AND REPLACED LT AILERON PER MM.SDR UPS03840032Aileron · crackedINSPECTION TYPE: C2, LT WING OUTBOARD AILERON L/E UPPER SKIN IS CRACKED AT XA 684. REMOVED, FABRICATED AND REPLACED SKIN SECTION IAW SRM 57-8-0 FIG 4.SDR CA030103011Skin · cracked(CAN) TWO OF THE BALANCE WEIGHT ATTACHMENT SCREW HOLE HAD 1/2 INCH CRACKS STARTING FROM UNDER THE SCREW HEADS.SDR ZLW2003F00001Structure · corrodedON 12-11-2002, A STATIC WICK BASE WAS NOTED TO BE LOOSE ON THE LEFT AILERON. THE STATIC WICH BASE WAS REMOVED AND CORROSION WAS FOUND BENEATH IT. AFTER BLENDING OUT THE CORROSION, IT WAS NOT TO BE OUT OF MFG LIMITS.SDR SWAA022860Aileron · delaminatedDURING WALK AROUND INSPECTION, FOUND LT AILERON DELAMINATED AT OUTER EDGE ON BOTH UPPER AND LOWER SURFACE. REMOVED AND REPLACED LT AILERON PER MM.SDR QXEA0202139Aileron · chafedPDX - RIGHT AILERON TRAILING EDGE CHAFED BY BONDING JUMPER AT TRIM TAB INBOARD HINGE. REPAIRED IAW HORIZON AIR EA 2-57-213.SDR QXEA0202138Aileron · lightning strikePDX - RIGHT AILERON TRAILING EDGE HAS LIGHTNING DISCHARGE DAMAGE 2 INCHES OUTBOARD OF FIXED TAB. REPAIRED IAW DHC-8 200 SRM 51-40-00 AND SRM 57-60-71.SDR DLM11021397Aileron · puncturedWING / LH / INBD AILERON / INBD TRAILING EDGE : GROUND DAMAGE REPAIR THE UPPER SKIN, TRAILING EDGE WEDGE, AND INBD CLOSEOUT RIB OF THE LH WING INBD AILERON WERE DAMAGED WHEN THE AIRCRAFT STRUCK A MTC. WORK S
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