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 DALA13004413214Bolt · scoredDURING INSPECTION, FOUND RT AILERON, HINGE BOLT NR 4, SCORED. SCORED IS BEYOND LIMITS IAW AMM 27-14-41, PB 601. RECEIVED NEW BOLT TO BE INSTALLED ON JIC 5760-1010S-RT. DIMENSIONS L=.8750" X W=.7500".SDR COEA2013031201913Tee Fitting · corrodedHEAVY CHECK COE/MINOR REPAIR. LEVEL 2 CORROSION LEFT AILERON INTERNAL INBOARD TEE BACK-UP FITTING FOR INBOARD HINGE FITTING ON AFT SIDE OF FWD SPAR IS CORRODED. REPLACED AILERON PER ATR 42 AMM.SDR USAA2013021300020Hinge Pin · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT AILERON NR 4 HINGE PIN BETWEEN WS 1346 TO WS 1406 & BETWEEN WING RIB 26 TO RIB 25. REPLACED LEFT AILERON NR 4 HINGE PIN IAW A321 AMM 27-14-41.SDR ASOA20130115232Attach Bracket · wornLEFT AILERON PCA ATTACH BRACKET HAS A MIGRATED BUSHING. R & R PCA ATTACH BRACKET.SDR IPXA13B77015Skin · dentedRT OTBD AILERON DENT 77" FROM INBD 28.5 FROM T/E. REPAIRED IAW EO B747-5750-49752-A.SDR ASOA20130106006Attach Fitting · gougedDURING C-CHECK, LT AILERON INBD PCA ATTACHMENT FITTING GOUGED. MX R & R LT AILERON INBD PCA ATTACHMENT FITTING IAW EC5750-01177. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR AALA20130112007Aileron · damagedRIGHT AILERON DAMAGED APPROXIMATELY 31 INCHES INBOARD OF NUMBER THREE WEIGHT TOWER. APPLIED PERMANENT WET LAYUP REPAIR TO DAMAGED AREA PER SRM 51-70-17 AND EA COMP-57-027784.SDR IPXA12B76575Skin · wornLT OTBD AILERON UPPER SKIN AT INBD END NEAR T/E WEDGE. REPAIRED IAW EO B747-5750-49455-A.SDR CA121219005Skin · cracked(CAN) TWO CRACKS WERE OBSERVED NEAR THE T/E OF THE INBD UPPER SURFACE OF THE LT AILERON DURING SCHEDULED MAINTENANCE.SDR SWIA201232469Skin · chafedLEFT WING UPPER AILERON LEADING EDGE HAS CHAFING ALONG LEADING UPPER EDGE. (C-CHECK) INSTALLED NEW LEFT LEADING EDGE UPPER AILERON LEADING EDGE IAW SRM.SDR REXA2012121101735Link · chafedRIGHT AILERON OUTBOARD PCU LINK AND AILERON LUG ARE CHAFED ON LOWER SIDE. REPAIRED IAW BOMBARDIER REO 601R-57-61-324.SDR FDEA201212064253Skin · delaminatedRT WING, OTBD AILERON, INBD T/E SURFACE FOUND DELAMINATED. REPAIRED IAW SRM 57-60-80, REPAIR 1, REVISION 51 AND COMPLIED WITH EA 1-5750-165176. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 115.SDR FDEA201211304223Skin · dentedRIGHT WING AILERON LOWER AFT SURFACE HAS 6 DENTS FROM .5 TO 2 SQUARE INCHES AND FROM .009 TO .015 INCHES APPROX DEEP. REPAIRED 6 EA DENTS AT RT AILERON LWR AFT T/E SECTION IAW SRM 51-77-12, PARA 4C, PG 3-6 AND 51-77-12 4C PG 288-289. NDT SHOWS NO DELAMINATIOSDR SIMA20121129002Fitting · damagedDURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON DAMPER FITTING OUTBOARD LUG SCORN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DAMPER FITTING IAW EO EM-27MR-112. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SWAA2012120310098Bolt · corrodedRUST ON BOLTS LOCATED ON BALANCE PANEL AREA OF THE LT AILERON. REPLACED BOLTS LOCATED ON BALANCE PANEL AREA OF THE LT AILERON IAW CMM 57-50-21.SDR CA121212003Bushing · worn(CAN) UPON INSPECTION CONTROL TEE LOWER PIVOT POINT RETAINING BUSHING FOR PIVOT BEARING FOUND TO HAVE COME LOOSE IN ITS CRIMP WITH BLACK FRETTING PRESENT AROUND THE BUSHING. WITH SLIGHT FOR AND AFT MOTION OF THE CONTROL YOKE WITH ONE HAND WILL CAUSE ONE TO SESDR CA121114001Hinge Bracket · corroded(CAN) DURING THE REMOVAL OF THE RT SIDE AILERON FOR PAINTING, THE AME DISCOVERED SEVERE CORROSION ON THE INSIDE HINGE. THE CORROSION REDUCES THE HINGE BRACKET THICKNESS TO ABOUT 60 PERCENT -70 PERCENT OF IT`S ORIGINAL SIZE. CORROSION WAS ALSO FOUND ON THE LTSDR SWAA2012111509477Seal · crackedLEFT WING FIXED T/E PANELS I/B OF AILERON T/E SEAL HAS PIECES MISSING AND CRACKED. REMOVED AND REPLACED T/E PANEL T/E SEAL P/N 14D0014 PO 79019347 IAW B717 SRM 51-41-02.SDR UALA2012110706418Bearing · wornCREW REPORT EXCESSIVE VIBRATION WITH FLAPS DOWN. TEST HOP NO GOOD. FLAP VIBRATION 3-4 POSITION. BECAUSE OF REPEAT DISCREPANCIES FOR AIRFRAME VIBRATION WHEN FLAP ARE LOWERED FROM 3 TO FULL DOWN ACCOMPLISH. FLAPS HYDRAULIC ACTUATION AND POWER TRANSMISSION INSDR SWAA2012110509105Aileron · delaminatedRIGHT WING OUTBOARD PORTION OF AILERON T/E DELAMINATED. REPAIRED AILERON PER MM.SDR CA121105023Skin · cracked(CAN) DURING A REGULAR PHASE INSPECTION, MAINTENANCE NOTICED THE RT AILERON TOP SKIN HAD A 6" CRACK AFT OF THE AILERON SPAR, INBD OF THE MIDDLE HINGE.SDR SIMA20121029003Fitting · damagedDURING MAINTENANCE INSPECTION FOUND THE RIGHT AILERON DAMPNER ATTACHMENT FITTING HAS SEVERAL NICKS AND GOUGES. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE DAMPNER FITTING ON RIGHT AILERON IAW EO EM-27MR-112. THE AIRCRAFT WAS RETUNRED TO SDR USAA2012102900004Skin · delaminatedRON VISIT - DELAMINATION ON RIGHT AILERON UPPER SURFACE AT TRAILING EDGE WEDGE OUTBOARD CORNER. REPLACED RIGHT AILERON IAW JOB CARD.SDR FDEA201210263756Wedge · dentedRT WING LWR EXTERNAL SKIN OF ALL SPEED AILERON HAS 9 EA DENTS ON T/E WEDGE. REPAIRED 9 EA DENTS ON LWR T/E WEDGE OF RT ALL SPEED AILERON IAW FSRM 57-61-11 PB 201, PARA 4E WITHOUT DEVIATION. COMPLIED WITH EA 6-5750-T030028 PT 1 FOR RSC TRACKING. NO FOLLOW USDR UALA2012101805972Aileron · damagedHEAVY LIGHTNING DAMAGE TO LEFT WING OUTBOARD AILERON. REMOVED LEFT WING OUTBOARD AILERON. INSTALLED LEFT AILERON TO STEP 3G10 OF MM 27-11-21 PAGE 406.SDR CA121212005Bushing · loose(CAN) UPON INSPECTION OF CONTROL TEE LOWER PIVOT POINT RETAINING BUSHING FOR PIVOT BEARING FOUND TO HAVE COME LOOSE IN ITS CRIMP WITH BLACK FRETTING PRESENT AROUND THE BUSHING. WITH SLIGHT FOR AND AFT MOTION OF THE CONTROL YOKE WITH 1 HAND WILL CAUSE ONE TO SDR UALA2012101105792Aileron · damagedHEAVY LIGHTNING DAMAGE TO LEFT WING OUTBOARD AILERON. REMOVED AILERON AND SENT TO SHOP. INSTALLED LEFT AILERON TO STEP 3G10 OF MM 27-11-21 PAGE 406. COMPLETED INSTALLATION OF LEFT O/B AILERON.SDR EE4Y2012101100295Attach Fitting · wornDURING STRUCTURE INSPECTION, FOUND THE LT WING AILERON INBD SERVO CONTROL ATTACH FITTING WORN.SDR AALA20121006002Aileron · damagedDAMAGE TO TRAILING EDGE OF LEFT INBOARD AILERON. ACCOMPLISHED HOT BOND REPAIR PER SRM 51-70-17.SDR A6WA20121008547Skin · damagedREF ROUTINE DMI 53252-5000-0051 TEMPORARY REPAIR TO THE LEFT AILERON L/E PERFORM PERMANENT REPAIR AS REQUIRED. REMOVED DAMAGED SKIN AND INSTALLED NEW SERVICEABLE L/E SKIN IAW CRJ 200 SRM 51-42-21, 51-42-06.SDR FDEA201209273482Skin · dentedRT AILERON LOWER SURFACE T/E SKIN HAS A 18.0" X 0.500" X 0.130" DEEP DENT. DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-61-11, PB 201, PARA E. REPAIRED DENT IAW SRM 51-77-12, PARA 4 D. AND 4 A. (5). RESTORED PROTECTIVE COATING IAW SRM 51-75-10 PARA 3 A.SDR FDEA201209273481Skin · dentedRT WING AILERON HAS TWO DENTS ON LOWER SURFACE. DENTS MEASURED 0.500 X 0.500 X 0.023 DEEP AND 1.00 X 1.00 X 0.019 DEEP. ONE DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-61-11 PB 201, PARA E. REPAIRED BOTH DENTS IAW SRM 51-77-12 PAR 4.D. AND 4.A.(5) PAGES 292 ANSDR USAA2012092000012Support · excess play2S CHECK - EXCESSIVE PLAY AT LEFT WING AILERON NR 3 HINGE SUPPORT FRAME ASSEMBLY BETWEEN WS 1287 TO WS 1346 & BETWEEN RIB 24 TO RIB 25 WING AILERON NR 3 HINGE SUPPORT FRAME ASSEMBLY IAW A319 AMM 57-51-31 & SRM 51-72-11.SDR USAA2012092000010Support · excess play2S CHECK - EXCESSIVE PLAY AT LEFT WING AILERON NR 1 HINGE SUPPORT FRAME ASSEMBLY BETWEEN WS 1228 TO WS 1287 & BETWEEN RIB 23 TO RIB 24. REPLACED LEFT WING AILERON NR 1 HINGE SUPPORT FRAME ASSEMBLY IAW A319 AMM 57-51-31 & SRM 51-72-11.SDR N6WA2012091301Bolt · corrodedLT AILERON HINGE MOUNT BOLT CORRODED. UPON INSPECTION, FOUND BONDING JUMPER MOUNTING HARDWARE AT HINGES 1 & 2 TO BE CORRODED. REPLACED MOUNTING HARDWARE IAW AMM 20-21-00. FOUND NO MORE CORROSION ON HINGES.SDR FDEA201209113279Skin · wornLEFT WING INBD AILERON ASSY LOWER FORWARD RUB STRIP WORN. SKIN FABRICATED AS PER DRAWING ARC1250 REVISION D. RUBSTRIP (SKIN) REMOVED AND REPLACED AS PER E.A. 1-5750-162367. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115.SDR AALA20120908003Skin Panel · damagedHAIL DAMAGE TO UPPER SKIN PANEL OF RIGHT OUTBOARD AILERON. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-05.SDR AALA20120906003Skin · damagedHAIL DAMAGE ON TOP SURFACE OF LEFT WING OUTBOARD AILERON AT TWO LOCATIONS. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-05.SDR UALA2012090605022Paint · peelingAT DEPARTURE TIME, RAMP REPORTED PEELING ON TOP OF RIGHT AILERON. REPAIRED AND APPLIED PRIMER, STILL NEEDS TOP COAT PAINT.SDR ASOA20120904092VHinge Fitting · wornDURING C-CHECK THE LT AILERON INBD HINGE FITTING WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MX R & R THE HINGE FITTING IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR IPXA2575274Counterweight · corrodedINSPECTION TYPE: C, RT AILERON INBD SET OF COUNTER BALANCE WEIGHTS CTR OTBD WEIGHT HAS SURFACE CORROSION. COUNTER BALANCE WEIGHTS OUT OF LIMITS, R & R BALANCE WEIGHTS IAW SRM 57-60-02-1A-1 & 51-40-02-0G.SDR CA120918015Balance Weight · corroded(CAN) AILERON L/E BALANCE WEIGHTS FOUND CORRODED. BALANCE WEIGHT, PN 557-60-12-339. REPLACED ON BOTH LT AND RT AILERONS.SDR DALA1247310199Skin · damagedRT INBD AILERON LOWER SURFACE FOUND DAMAGED. COMPOSITE WET LAY UP REPAIR CARRIED OUT PER SRM 57-60-01 REPAIR 1 AND SRM 51-70-17 FIG 10.SDR USAA2012082200007Repair · damagedMECHANICS REPORT - RIGHT OUTBOARD AILERON, 12 INCHES FROM WING TIP ON TOP SKIN SURFACE, PREVIOUS REPAIR TO COMPOSITE HAS WORN OFF & IS MISSING. REPLACED RIGHT OUTBOARD AILERON IAW JOB CARD 12L56027004.SDR FDEA201208203082Skin · misrepairedRT WING INBD AILERON UPPER SKIN MISREPAIRED. REPAIRED AS PER SRM 57-10-00 FIG.85 VOL.I REV.99 SHEET 2. REPAIR CLASSIFED MAJOR AS PER GMM 6-2-100 REV. 115.SDR SPUY20120820025Skin · nickedDURING ROUTINE C CHECK INSPECTION, RIGHT WING OUTBOARD AILERON UPPER SURFACE SHOWS NICKS BETWEEN STA WBL 492.5 AND 602.5 REF NR 0127.SDR SWIA201231686Skin Panel · chafedRIGHT AILERON UPPER LEADING EDGE SKIN CHAFED. (C-CHECK) REPLACED RIGHT AILERON LEADING EDGE SKIN PANEL, PART # CC670-13052-4 IN REFERENCE TO CRJ 700 SRM.SDR A6WA201240801Skin · chafedLT AILERON UPPER L/E CHAFED. BLENDED CHAFED AREAS IAW SRM 51-12-00. MEASURED, FOUND TO BE WITHIN LIMITS IAW REO 601R-57-61-437.SDR SWIA201231687Skin · chafedLEFT AILERON UPPER LEADING EDGE SKIN CHAFED AT INBOARD AND OUTBOARD SIDES OF INBOARD HINGE. (C-CHECK) REPLACED LEFT AILERON UPPER LEADING EDGE SKIN IN REFERENCE TO CRJ700 SRM.SDR UIEA2012081300359Structure · delaminatedRT TRAILING OTBD AILERON EDGE DELAMINATED. REF E/O 6757A039, RT WING OTBD AILERON DELAMINATION: PART I, TIME LIMITED REPAIR ACCOMPLISHED. PART II, DVI EVERY FLT CYCLE. PART III, PERMANENT REPAIR PRIOR TO 750 FLT CYCLES.
Back to JASC 5751