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 P5CA9700242Aileron · damagedR/W O/B AILERON BAD REPAIR ON O/B ENG. REPAIRED PER BOEING SRM 51-40-09.SDR P5CA9700234Skin · delaminatedR/W I/B AILERON LOWER AFT SURFACE DELAMINATED. REPAIRED PER BOEING SRM 51-40-09.SDR IXXA9700043Aileron · corrodedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT OUTBOARD AILERON LOWER EXTERNAL PLATING WAS FOUND TO HAVE SURFACE CORROSION AND BULGING AT STATION XA615 TO XA642. REPAIR WAS ACCOMPLISHED BY REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF NEW SECTIOSDR IXXA9700038Aileron · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT INBOARD AILERON UPPER LEADING EDGE PLATING WAS FOUND TO BE CRACKED AT STATION XA490. REPAIR WAS ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF NEW PLATING SECTION IN ACCORDANCE WITH FAA DSDR UPS97221903Hinge Assy · corrodedINSPECTION TYPE: SI. CORROSION ON LT O/B AILERON CENTER I/B HINGE FITTING (WING SIDE). REMOVED AND REPLACED LT O/B AILERON HINGE FITTING (CENTER I/B) IAW SRM 51-30-2, 51-30-5.SDR RRXA97040Skin · crackedDURING A MAINTENANCE VISIT, FOUND RIGHT SIDE AILERON EXTERIOR SKIN WITH CRACKS IN 2 PLACES, AT XW=698. FABRICATED DOUBLER, FILLER AND INSTALLED IAW FAA DER APPROVED ENGINEERING SKETCH B90-R04 AND DC-8 SRM 51-1-21.SDR ABXA9700599Aileron · corrodedDURING C-INSPECTION, FOUND THE RIGHT AILERON LOWER SURFACE HAS CORROSION BULGES AT AILERON DAMPNERS. REPLACED RIGHT AILERON IAW DC-9 MAINTENANCE MANUAL CHAPTER 27-10-1 AND 27-10-2.SDR CA970204001Skin · delaminated(CAN) UPPER AILERON SKIN DELAMINATED FROM INBOARD END APPROXIMATELY SIX FEET OUTBOARD AND FROM FRONT SPAR TO REAR SPAR. REPLACED.SDR EISA97010Skin · delaminationRIGHT WING OUTBOARD AILERON TAB SKIN HAS AREA OF DELAMINATION. REPAIRED TAB PER SRM 57-50-5. (M)SDR UPS97222139Fitting · corrodedINSPECTION TYPE-SI, CORROSION ON LT I/B AILERON QUADRANT SUPPORT FITTING PITTED AROUND LOWER BOLT. REMOVED AND REPLACED LT I/B AILERON QUADRANT PER SRM 51-10-02, 51-30-5.SDR UPS97821843Hinge · crackedINSPECTION TYPE-C/CK, LOWER REAR SPAR O/B AILERON O/B HINGE CRACKED. REMOVED LT O/B AILERON, REMOVED AND REPLACED SUPPORT ASSY IAW DC8 SRM 51-3-1 AND REINSTALLED LT O/B AILERON IAW DC8 MM 27-11-02.SDR UPS97821832Doubler · crackedINSPECTION TYPE-C, LT O/B AILERON AT CENTER HINGE CUTOUT, SKIN DOUBLER IS CRACKED 2 PLACES. REMOVED DAMAGED DOUBLER, FABRICATED AND INSTALLED DOUBLER PER SRM 57-8-01 FIG 4 AND 51-1-20.SDR MZZA96223Skin · tornTNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, RT WING OUTBOARD AILERON T/E HONEYCOMB LOWER SKIN WAS FOUND TO BE TORN AT AFT EDGE. THE DAMAGED SKIN .375 INCH BY 1 INCH IN SIZE WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-6. REF, HANGAR NON ROUTISDR CKSA96355Skin · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: RIGHT INBOARD AILERON TRAILING EDGE DENTED AND CRACKED. REPAIRED AILERON TRAILING EDGE IAW DC-8 SRM 57-2-0, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81824.SDR CKSA96329Skin · crackedDURING SEVERE TURBULENCE INSPECTION FOUND: LEFT INBOARD AILERON LOWER SURFACE CRACKED APPROXIMATELY .5 INCH LONG. REPAIRED PER DC-8 SRM 57-2-0 AND 57-2-1. TREATED AND PRIMED PER 51-1-8, DC-8 MIP-1 SECTION 15, NON-ROUTINE TASK CARD NR 81816.SDR 96ZZZX6145Spar · crackedDURING C/W AD 96-21-03, A CRACK WAS DETECTED IN THE AILERON SPAR AND REINFORCEM ENT DOUBLER IN BOTTOM BRACKET ATTACH HOLE.SDR ABXA9700550Aileron · brokenDURING LEVEL FLIGHT, BALL CENTERED, BOTH CONTROL WHEELS WERE COCKED APPPROXIMATELY 30 DEGREES TO THE RIGHT AND THERE WAS 30 DEGREES OF AILERON TRIM NEEDED. AS AIRCRAFT WAS SLOWED DOWN MORE AILERON TRIM WAS NEEDED TO KEEP AIRCRAFT LEVEL. REPLACED LEFT INBOARDSDR 9627671220Skin · damagedDURING LINE CHECK, DAMAGE WAS FOUND ON THE UPPER SKIN OF THE RIGHT INBOARD AILERON AT STA XIA=300. REMOVED DAMAGE AND INSTALLED DOUBLER PER EA 12-120115, (P/N NRC6043-502).SDR CA961205018Bearings · worn(CAN) WHILE WORKING ON THE AILERON SYSTEM WEAR WAS NOTED IN THE LEFT AILERON OUTBOARD BEARING. SIMILAR PLAY WAS NOTED ON THE RIGHT SIDE. COMPONENTS REPLACED.SDR CA961205017Spar · cracked(CAN) WHILE CARRYING OUT AD 96-21-03 A CRACK WAS FOUND UNDER THE HINGE. SUBMITTER INSTALLED A NEW AILERON SPAR.SDR 96ZZZX6015Bracket · crackedDURING ANNUAL INSPECTION, FOUND LEFT OUTER AILERON HINGE 'SPAR SIDE' BRACKET COMPLETELY CRACKED IN RADIUS AREA WHERE ATTACHMENTS SCREWS ARE LOCATED.SDR CKSA96198Doubler · dentedDURING C-4 CHECK INSPECTION, FOUND RIGHT WING AILERON HAS DENT ON UPPER LEADING EDGE. REPAIRED RIGHT HAND OUTBOARD AILERON BY INSTALLING DOUBLER IAW EA 96-326 EER D8-05081 AND AIA 8110-3. CORROSION CARD NR 111R-0551, NON-ROUTINE TASK CARD NR 87357.SDR ABXA9700506Skin · crackedLEADING EDGE NEEDS TO BE WELDED. WELDED LEADING EDGE PER ABX REA D957-18214.SDR CA961203007Skin · cracked(CAN) LEFT AILERON UPPER AND LOWER SKINS CRACKED ALONG SPAR AT TRAILING EDGE OF LEADING EDGE SKIN. RIGHT AILERON LOWER SKIN CRACKED SAME PLACE. ALSO, P/N 99-13000-197 AND -199.SDR HAL960103Casting · crackedDURING C-CHECK, FOUND LEFT INBOARD AILERON ACTUATOR CASTING CRACKED AT THE LOWER AFT INBOARD END. REPAIRED PER ESO 7349 DATED 11-1-96. (M)SDR ZIAA961101Skin · corrodedMCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED RT OTBD AILERON LOWER SURFACE CORROSION. REPAIRED IAW DWG A74-R05. (X)SDR CALA9601694Skin · delaminatedINSPECTION FOUND OUTBOARD TRAILING EDGE CORNER OF LEFT OUTBOARD AILERON DELAMINATED. THE DELAMINATED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS INSTALLED IAW SRM 51-40-6.SDR UPS96521481Skin · delaminatedRT AILERON DELAMINATED ON OUTBOARD END TOP OF AILERON. REPAIRED RT AILERON OUTBOARD EDGE IAW EO B757-5760-8740.SDR 96FDEA01670Casting · corrosionLT AILERON NR 3 HINGE CASTING HAS CORROSION AT HINGE PIN AREA. REMOVED AND REPLACED CASTING PER 51-10-1 SRM.SDR 96FDEA01668Casting · corrosionNR 0932, LT OUTBOARD AILERON NR 2 HINGE CASTING HAS CORROSION AT LOWER HINGE HOLES. REMOVED AND REPLACED CASTING PER SRM 51-10-01, (P/N 5700200) HINGE ASSY.SDR DL72S962380Aileron · gougedSPAR GOUGED AT I/B SIDE OF T/E WEDGE. SPLICED IN SPAR SECTION PER SRM 51-40-3.SDR ZIAA96045Skin · corrosionDURING ACCOMPLISHMENT OF AD 92-22-07 (DC-8 CORROSION PROGRAM) THE FOLLOWING INITIAL INSPECTIONS REVEALED LEVEL 2 CORROSION. RT AIL INT XA 474-535. XA 646-678. REPAIRED IAW APPLICABLE SRM'S, DWG., ETC. (X)SDR 9622322706Bushing · wornDURING CLIMBOUT WHILE ACCELERATING TO 300 KTS IN CLEAN CONFIGURATION, THE AIRCRAFT BEGAN A MEDIUM FREQUENCY VIBRATION. VISUAL CHECK OF WINGS SHOWED LEFT INBOARD AILERON VIBRATING UP AND DOWN PLUS OR MINUS 2 INCHES AT THE TRAILING EDGE, RIGHT AILERON PLUS OR MISDR AALA961527Frame · damagedAFW - LEFT AILERON LOWER CONDUCTIVE FRAME HAS SMALL BURN HOLE FROM STATIC DISCHARGE. REPAIRED PER MRB 757-984. (M)SDR CALA9601539Skin · delaminatedINSPECTION FOUND RT WING OUTBOARD AILERON LOWER SURFACE OUTBOARD TIP DELAMINATED. THE DELAMINATED AREA WAS CUT OUT AND A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM'S 51-40-6 AND 51-80-4.SDR 96ZZZX5719Skin · crackedDURING 100-HOUR INSPECTION, FOUND .25 INCH CRACK IN OUTBOARD UPPER TRAILING EDGE OF SKIN OF THE LT AILERON. SUSPECT CAUSE DUE TO VIBRATION. SUBMITTER RECOMMENDATION IS CLOSE INSPECTION OF THE AILERONS.SDR 96FDEA01584Skin · crackedNR 0580 AND 020, CRACK IN L/W O/B AILERON I/B AFT TRAILING EDGE CHORD. *S/D* STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER PER FEDEX SRM 51-40-3.SDR CALA9601461Web · crackedLEFT HAND OUTBOARD AILERON NR 3 AILERON HINGE FITTING AT WING TRAILING EDGE HAS OUTBOARD WEB CRACKED. FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-2.SDR CALA9601460Web · gougedLEFT HAND OUTBOARD AILERON INBOARD HINGE AT WING TRAILING EDGE HAS WEB BADLY GOUGED AT OUTBOARD SIDE OF HINGE FITTING. GOUGE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 57-10-4.SDR CA961003010Balance Weight · cracked(CAN) LEFT AILERON OUTBOARD BALANCE WEIGHT FOUND CRACKED AT CENTRE HOLE. 6 OF 12 OTHER AIRCRAFT FOUND WITH SIMILAR PROBLEM.SDR CA961003009Balance Weight · cracked(CAN) RIGHT AILERON INBOARD BALANCE WEIGHT FOUND CRACKED AT ATTACH HOLE. 6 OF 12 OTHER AIRCRAFT FOUND WITH SAME PROBLEM.SDR CA961003008Balance Weight · cracked(CAN) RIGHT AILERON INBOARD BALANCE WEIGHT FOUND CRACKED AT CENTRE AND OUTBOARD ATTACH HOLES. 6 OF 12 OTHER AIRCRAFT FOUND WITH SAME PROBLEM.SDR CA961003007Balance Weight · cracked(CAN) LEFT AILERON ALL 3 BALANCE WEIGHTS FOUND CRACKED AT CENTRE HOLE. 6 OTHERS OF 12 AIRCRAFT FOUND WITH SAME PROBLEM.SDR CA961003006Balance Weight · broken(CAN) RIGHT AILERON BALANCE WEIGHT FOUND BROKEN AT CENTRE ATTACH HOLE. 6 OTHERS OF 12 AIRCRAFT FOUND WITH SAME PROBLEM.SDR CA961003005Balance Weight · cracked(CAN) LEFT AILERON 2ND FROM INBOARD BALANCE WEIGHT FOUND BROKEN AT 2 ATTACH HOLES. 6 OTHER AIRCRAFT SIMILAR IN FLEET OF 12.SDR CA961003004Balance Weight · broken(CAN) LEFT AILERON INBOARD BALANCE WEIGHT FOUND BROKEN AT CENTRE ATTACH BOLT. WEIGHT HAD BEEN CRACKED FOR SOME TIME. REST OF FLEET OF 12 AIRCRAFT CHECKED AND 6 OTHERS FOUND WITH BROKEN BALANCE WEIGHTS AT SAME PLACE. ALL CRACKED BALANCE WEIGHTS FOLLOWED A SIMILSDR EISA96224Fitting · crackedFOUND 1 INCH CRACK, OUTBOARD AILERON, 2ND FROM OUTBOARD ATTACHED FITTING. REPLACE FITTING WITH NEW PART PER SRM 51-40-01. (M)SDR UPS96221086Fitting · corrodedINSPECTION TYPE: C. L/W I/B AILERON TAB HINGE FITTINGS ARE CORRODED AILERON SIDE. REMOVED AND REPLACED L/W I/B AILERON TAB HINGE FITTINGS PER SRM 51-30-2.SDR 96ZZZX5123Fitting · looseDURING A 100-HOUR INSPECTION, NOTICED THE LEFT AILERON WOULD STILL MOVE AFTER STOPS WERE CONTACTED. THE OUTBOARD ATTACH FITTING WAS FOUND LOOSE AND WORKING. BOTH BOLTS THAT ATTACH THE FITTING TO THE AILERON WERE FOUND LOOSE. NO TORQUE SEAL FOUND ON ANY OF TSDR UPS96221154Spar Chord · crackedINSPECTION TYPE-C, RT O/B AILERON UPPER SPAR CHORD IS CRACKED, JUST O/B OF THE CENTER I/B HINGE. FABBED AND INSTALLED REPLACEMENT PART IAW SRM 57-30-02 AND 51-30-2.
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