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 ABXA9900119Fitting · crackedLEFT INBOARD AILERON, INBOARD HINGE FITTING CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21.SDR ABXA9900095Fitting · crackedLEFT INBOARD AILERON INBOARD HINGE FITTING WAS CRACKED. REPLACED FITTING IAW DC8 SRM 51-1-21.SDR 99ZZZX955Rib · crackedDURING 100-HOUR INSPECTION, FOUND CRACK INBOARD AILERON RIB.SDR DHL9971221CPanel · wornAT C-CHECK, GROOVE WORN INTO I/B AILERON LEADING EDGE PANEL 8310. REPLACED ACCESS PANEL PER SRM 57-50-1, 13 X 9.5.SDR DHL9971212CFitting · corrodedAT C-CHECK, RIGHT WING TRAILING EDGE I/B AILERON CENTER HINGE FITTING FASTENER HOLE CORRODED. REPLACED FITTING PER SRM 51-30-2.SDR 99ZZZX610Skin · corrodedDURING A C-CHECK, CORROSION WAS NOTED ON LOWER SKIN RT OUTBOARD AILERON.SDR UPS99828344Skin · crackedINSPECTION TYPE:C RT INBD AILERON UPPER L/E SKIN AT THE MANUAL REVERSION MECH IS CRACKED. CUT OUT DAMAGED SKIN AND SPLICED IN NEW SECTION IAW SRM 57-2-0.SDR CA990310045Skin · delaminated(CAN) FOUND SKIN DELAMINATION APPROXIMATELY 1 SQUARE FOOT OF UPPER SKIN OF AILERON. REPLACED.SDR CALA9802155Skin · debondedINSPECTION FOUND LT O/B AILERON TRAILING EDGE O/B CORNER DEBONDED. THE AILERON WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2, PAGE 18 AND 51-8-4.SDR 99ZZZX205Rib · gougedDURING PERFORMANCE OF C-CHECK INSPECTION TASK ON THE LEFT WING, THE AILERON ATTACH RIB 20 WAS FOUND TO HAVE A GOUGE APPROXIMATELY 1 INCH LONG BY .027 INCH DEEP ON THE OUTBOARD SIDE. THIS WAS APPARENTLY CAUSED BY PREVIOUS REMOVAL OR INSTALLATION OF AILERON. TSDR CA981202001Doubler · cracked(CAN) AILERON DOUBLER FOUND CRACKED AT THE OUTER END ON THE UPPER RADIUS CORNER. THIS DOUBLER SUPPORTS THE MASS BALANCE. A TWISTING OF THE DOUBLER HAPPENS IN ROUGH AIR OR WITH HEAVY FLIGHT LOADS. IN ADDITION, THE SUBMITTER SUGGESTS THAT THE CONTROL LOCK LOCSDR ARWA981125Skin · corrodedC-CHECK, CORROSION FOUND BETWEEN LOWER SKIN AND RIBS ON LT I/B AILERON. REMOVED DAMAGED LOWER SKIN, FABRICATED REPAIR SKIN PER EO DRAWING NR 98-0924-3, ON 8110-3, DATED SEPT 25, 1998 UNDER WORK ORDER NR 1299.SDR EISA98273Skin · delaminatedDURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD FOUND LEFT AILERON DELAMINATED AT OUTBOARD TRAILING EDGE. REPAIRED DELAMINATION PER SRM 51-40-6, 51-40-8 AND 51-40-9. (M)SDR EISA98270Skin · delaminationROUTINE C-CHECK WORK ACCOMPLISHMENT REVEALS RIGHT AILERON, OUTBOARD T/E HAS TWO AREAS OF DELAMINATION. REPAIRED AREAS OF DELAMINATION PER SRM 51-40-5, 51-40-6 AND 51-40-8 AND 51-40-9. (M)SDR MWEA981042Skin · crackedLEFT AILERON LOWER SKIN WAS FOUND CRACKED AROUND A PREVIOUS REPAIR. REMOVED OLD REPAIR AND DAMAGED SKIN FABRICATED FILLERS AND DOUBLERS INSTALLED REPAIR SECTIONS OF SKIN.SDR SWAA982753Angle · crackedDURING SCHEDULED 1/4D CHECK, FOUND AILERON ACCESS PANEL 7104L SUPPORT ANGLE CRACKED IN TWO PLACES. REMOVED AND REPLACED ANGLE PER BOEING SRM.SDR DHL9872027DSkin · wornAT D CHECK, L/W INBD AILERON PANEL 8310 OUTER SKIN SURFACE AHS SOME WORN AREAS. FABRICATED NEW PANEL PER SRM 57-50-2, 12.5 BY 9, .63 N/R 1887.SDR P2EA98304Skin · delaminatedSJO - RIGHT AILERON DELAMINATED, DEFECT SIZE TOTAL 20 SQUARE INCH. REPAIRED RIGHT AILERON PER COOPESA EO COO-3-57-703-98 DATED NOV 27, 1998. (M)SDR AU981435Aileron · damaged(AUS) LEFT AILERON TIP DAMAGED IN A GROUND ACCIDENT. PART TC: 24,413.SDR RRXA99980Hinge · damagedDURING A MAINTENANCE VISIT, FOUND HINGE FITTING, LEFT OUTBD AILERON, 2014-T6 FORG REQUIRED TO BE REPLACED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW FAA APPROVED TIMCO DER ENSDR 99ZZZX1024Bracket · crackedDURING ANNUAL INSPECTION, FOUND BRACKET CRACKED AT AILERON CONTROL ARM ATTACH POINT.SDR CA981028011Spar · cracked(CAN) CRACKS FOUND IN LEFT AILERON INBOARD RIB P/N 17100-13, TO WHICH IS ATTACHEDTHE HINGE LEFT INBOARD P/N 17095-00 THROUGH THE SPAR. CRACKS LOCATED AT BOTTOM HOLE.SDR COMA9860315Skin · damagedLEFT AILERON, LOWER OUTER SKIN IS DAMAGED. REPLACED AILERON.SDR CALA9801972Skin · bentINSPECTION FOUND LT OUTBOARD AILERON INBOARD END UPPER AND LOWER SKIN BENT. THE AILERON WAS REMOVED AND REPLACED IAW MM 27-20-13.SDR AU981346Bracket · misinstalled(AUS) RIGHT AILERON HINGE BRACKET INCORRECTLY RE-FITTED FOLLOWING REPAIR. PART TC: 9,832.SDR AU981345Bracket · misinstalled(AUS) LEFT AILERON HINGE BRACKET INCORRECTLY RE-FITTED FOLLOWING REPAIR. PART TC: 9,382.SDR UPS98828031Skin · crackedINSPECTION TYPE-C, THE RT I/B AILERON UPPER L/E SKIN AT THE ACTUATOR IS CRACKED AT ONE SCREW HOLE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 51-1-21 AND DWG 5705334.SDR P2EA98248Skin · damagedSJO - LEFT AILERON DELAMINATED AND WITH HAIL DAMAGE, DEFECT SIZE VARIOUS. REPAIRED LEFT AILERON PER COOPESA EO COO-3-57-565-98 DATED OCT 15, 1998. (M)SDR CKSA98598Skin · corrodedLT AILERON T/E GROUND STRAP DISBONDED AND CORRODED AT STATIC DISCHARGERS. REPAIRED IAW CKF-EXW-088 SUPP SHEET 2. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBER MO280, CORROSION TASK CARD NUMBER C57-560-01-01.SDR 98ZZZX4063Rivets · corrodedDURING INSPECTION, AILERON BALANCE WEIGHTS WERE OBSERVED TO HAVE SEVERAL RIVET HEADS POPPED. FURTHER RIVETS COULD BE POPPED BY HAND (HEADS POPPING OFF). THE RIVET CORROSION WAS NOT VISIBLE FROM UNDER/AROUND HEADS.SDR CALA9801920Skin · delaminatedINSPECTION FOUND THE LT OUTBOARD AILERON TRAILING EDGE DELAMINATED SIX INCHES FROM OUTBOARD END. THE PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 51-30-2.SDR 98ZZZX3931Hinge · looseRIGHT AND LEFT OUTBOARD AILERON HINGE AS ATTACHED TO SPAR. RIVETS THAT PASS THROUGH HINGE, SPAR, AND LAST RIB HAVE SHEARED LEAVING LAST RIB UNSUPPORTED CRACKING SKIN IN ONE PLACE; AS WELL AS OUTER MOST PART OF REAR SPAR NOT BEING SUPPORTED WHEN AIR LOADS ARE SDR 98ZZZX3930Hinge · looseRIGHT AND LEFT OUTBOARD AILERON HINGE AS ATTACHED TO SPAR. RIVETS THAT PASS THROUGH HINGE, SPAR, AND LAST RIB HAVE SHEARED LEAVING LAST RIB UNSUPPORTED CRACKING SKIN IN ONE PLACE; AS WELL AS OUTER MOST PART OF REAR SPAR NOT BEING SUPPORTED WHEN AIR LOADS ARE SDR WRLA98092Balance Weight · corrodedDURING C-CHECK, RIGHT-HAND, OUTBOARD AILERON WAS IDENTIFIED AS HAVING CORROSION ON BALANCE WEIGHTS. MAINTENANCE PERSONNEL REMOVED CORROSION ON NR 3 AND NR 4 WEIGHTS PER SRM 51-82-00. NR 2 WEIGHT BEYOND SRM LIMITS. REPLACED WEIGHT WITH NEW PART. (X)SDR CA981007005Balance Arm · cracked(CAN) THE RUDDER AILERON INTERCONNECT TAB MASS BALANCE ARM WAS FOUND CRACKED CLOSE TO THE MOUNTING BASE. THIS IS THE THIRD TIME THIS OPERATOR HAS FOUND THESE ARMS CRACKED ON OTHER AIRCRAFT. THESE CRACKS WERE FOUND DURING ROUTINE WINTER INSPECTIONS. (CANADAIRSDR AU981169Spar · cracked(AUS) LEFT AILERON SPAR CRACKED BENEATH THE INBOARD ATTACHMENT BRACKET.SDR AU981168Spar · cracked(AUS) RIGHT AILERON SPAR CRACKED BENEATH THE INBOARD ATTACHMENT BRACKET.SDR COMA9860282Hinge · wornRIGHT AILERON HAS EXCESSIVE PLAY AT THE HINGE. REPLACED AILERON.SDR CA980916050Skin · cracked(CAN) TRAILING EDGE OF RIGHT HAND AILERON FOUND CRACKED IN 4 DIFFERENT LOCATIONS ON SAME SKIN.SDR UPS98227723Web · crackedINSPECTION TYPE:D LT OUTBD AILERON FIXED WEIGHT BAY, INBOARD WEB IS CRACKED. REPAIRED IAW SRM 51-30-02.SDR UPS98827687Weight · corrodedINSPECTION TYPE-C, LEFT I/B AILERON I/B BALANCE WEIGHT HAS MODERATE CORROSION. REMOVED AND REPLACED THE I/B AILERON IAW MM 27-11-01.SDR UPS98827689Weight · corrodedINSPECTION TYPE-C, RT WING I/B AILERON BALANCE WEIGHT IS CORRODED. REMOVED AND REPLACED I/B AILERON IAW MM 27-11-01.SDR CALA9801555Rib · crackedINSPECTION FOUND A .5 INCH CRACK IN RT OUTBOARD AILERON LEADING EDGE RIB JUST OUTBOARD OF NR 3 HINGE. THE RIB WAS REMOVED AND REPLACED IAW SRM 51-10-1, PAGE 4.SDR CALA9801541Skin · delaminatedINSPECTION FOUND AREAS OF DELAMINATED SKIN ON TOP AND BOTTOM OF LT WING OUTBOARD AILERON OUTBOARD TRAILING EDGE WEDGE PANEL. THE WEDGE PANEL WAS REMOVED AND REPAIRED IAW SRM 57-50-5. THE PANEL WAS REINSTALLED IAW SRM 51-10-1.SDR 98ZZZX3574Aileron · corrodedWATER INGRESS FOUND IN THE LT AILERON DURING A 48 MONTH X-RAY INSPECTION. UPON REPAIR PER RAYTHEON R.I.L. DRAWING, WATER WAS NOT FOUND AS INDICATED BY THE X-RAY. CORROSION WAS FOUND IN THE HONEYCOMB AND ON THE LOWER SKIN OF THE AILERON. PITTING IN ONE AREA HSDR 98ZZZX3573Aileron · corrodedWATER INGRESS FOUND IN THE LT AILERON DURING A 48 MONTH X-RAY INSPECTION. UPON REPAIRING AILERON PER RAYTHEON R.I.L. DRAWING, WATER WAS NOT FOUND, HOWEVER, CORROSION IN THE HONEYCOMB AND PITTING ON THE LOWER AILERON SKIN WAS FOUND. X-RAYS TAKEN PER THE NDT ISDR TSAA9833464Aileron · crushedLEFT AILERON BOTTOM SIDE HAS DENT AND A LARGE SMASH NOTED. REPLACED LT AILERON IAW MM CHAPTER 27-11-0. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. TAT: 33,673.9 HOURS. TAC: 63,646. (X)SDR RRXA98341Skin · crackedDURING A MAINTENANCE VISIT, FOUND RIGHT WING, INBOARD AILERON UPPER O/B SKIN, CRACKED. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO-05281.SDR 99ZZZM481Bearing · wornRIGHT AILERON OUTBOARD HINGE 'A' FRAME BEARINGS WORN. REMOVED AND REPLACED RIGHT AILERON OUTBOARD 'A' FRAME. W/C GEN FOR FUNCTIONAL CHECK. (M)SDR DHL9880302CSkin · crackedAT C CHECK, PANEL ON LT FAIRING 564B UPPER AILERON SURFACE OUTER SKIN FWD EDGE CRACKED. STOP DRILLED CRACK, FABRICATED EXTERNAL DOUBLER 1.0 BY 3.5 PER SRM 55-2-0. N/R 1013.
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