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 QXEA200600312Structure · wornYYC - C3 RIGHT AILERON LOWER INBOARD LEADING EDGE WORN BY SEAL, 22" IN FROM INBOARD END. REPAIRED IAW CRJ700/900 51-12-00-001-001-A01 AND SRM 51-25-01-001-A01.SDR QXEA200600311Structure · wornYYC - C3 LEFT HAND AILERON TOP INBOARD LEADING EDGE WORN BY SEAL UNDER PANEL 598AT, 598BT. REPAIRED IAW CRJ700/900 SRM 51-12-00-001-001-A01 AND SRM 51-25-01-001-001-A01.SDR IXXA06SMN028SAileron · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING INBOARD AILERON WITH CORROSION AND NON STANDARD REPAIR IN LOWER PLATING AT STA XA 550.00. PERFORMED MAJOR REPAIR. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED EXISTING PANEL PLATING (CORRODED) + REPAIR NON STANDSDR 2006FA0000057Balance Weight · brokenREMOVED EXISTING BALANCE WEIGHT ASSEMBLY, PN 65388-34 ON THE LT AILERON AND REPLACED WITH A SERVICEABLE BALANCE WEIGHT ASSEMBLY OF THE SAME PN AND WEIGHT. AT ANNUAL INSPECTION, THE WEIGHT WAS FOUND BROKEN OFF AT THE ATTACHMENT TUBE. THE EXISTING RIVET PATTERSDR 2006FA0000125Aileron · delaminatedRT AILERON UPPER SKIN FOUND DELAMINATED FROM HONEYCOMB CORE. DELAMINATION COVERS MORE THAN 50 PERCENT OF UPPER SURFACE. AILERON REPLACED WITH SERVICEABLE UNIT. (K)SDR AWXA200600235Channel · corrodedSAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED CORROSION ON THE RT AILERON TRAILING EDGE LOWER SURFACE CHANNEL. NO ALLOWABLE DAMAGE WAS FOUND IN THE AIRBUS SRM. MAINTENANCE REMOVED AND INSTALLED NEW AILERON TRAILING EDGE LOWER SURFACE CHANNEL IAW AIRBUS 320SDR TIM2006F00001Skin · corrodedTHE SKIN ON THE UPPER LEADING EDGE OF THE RT AILERON WAS FOUND TO BE TEARING AFT. INVESTIGATION DETERMINED THAT THERE WAS SIGNIFICANT CORROSION ON THE INSIDE OF THE AILERON. (K)SDR IXXA06SMN019SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, LT OUTBD AIL LWR SKIN CORRODED, STA XA 726.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-8-1 FIG 4. REMOVED CORROSION FROM LT OTBD AIL LWR SKIN, STA 726.000 IAW DC-8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 57SDR 2006FA0000083Skin · corrodedCORROSION BEYOND 10 PERCENT LIMITS IN LEADING EDGE SKIN UNDER BALANCE WEIGHTS. FOUND DURING SB238. (K)SDR IXXA05SMN276SRepair · misinstalledDURING C CHECK, LT INBD AIL LWR SKIN HAS NO STANDARD REPAIR (STA XA 543.000-551.000). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-8-1 FIG 1. REMOVED PANEL PLATING WITH NON STANDARD REPAIR ON IT IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FAB`D NEW PLATING (AL2024T30 0.02SDR IXXA05SMN275SSkin · corrodedDURING C CHECK , LT OUTBD AIL LWR SKIN CORRODED, STA XA 722.000. PERFORMED REPAIR IAW FAA FORM 8110-3 NR 05580 DATE 12-21-05, SEMAN DWG NR ED 4119 DATE 12-20-05 & EO SEMAN NR 20051449 DATE 12-21-05. REMOVED FASTENERS. REMOVED CORROSION. FOUND OUT OF LIMITSSDR IXXA05SMN274SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, DURING ROUTINE C-CHECK INSPECTION, LT IB AIL LWR SKIN CORRODED, STA 593.000. PERFORMED MAJOR REPAIR IAW SRM 52-2-0 FIG. 4 (SHEET 3). REMOVED EXISTING REPAIR IAW SRM 51-1-21. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.050”)SDR AU510001914Bolt · loose(AUS) LT AILERON TAB OB HINGE BRACKET ATTACHMENT BOLTS LOOSE. BOLTS WERE THREADBOUND IN ANCHOR NUTS. INVESTIGATION FOUND INCORRECT BOLTS WERE FITTED BY A PREVIOUS OPERATOR IN THE US. (CASA NR 510001914)SDR AU510001808Skin · crackedLT AILERON PN HC576C0077-000 CRACKED AT THE SECOND OUTBOARD AILERON HINGE FOR THE OUTBOARD TAB. RT AILERON PN HC576C0077-001 ALSO CRACKED AT THE OUTBOARD TAB HINGE.SDR AU510001706Spar · crackedLT AILERON ASSEMBLY SPAR CRACKED IN AREA UNDER THE AILERON PUSH-PULL ROD ATTACHMENT BRACKET. FOUND USING COLOR CONTRAST DYE PENETRANT INSPECTION IAW AD/PA31/118 AMDT1.SDR AU510001705Spar · crackedRT AILERON ASSEMBLY SPAR CRACKED IN AREA UNDER THE AILERON PUSH-PULL ROD ATTACHMENT BRACKET. FOUND USING COLOR CONTRAST DYE PENETRANT INSPECTION IAW AD/PA31/118 AMDT1.SDR AU510001482Spar · cracked(AUS) RT AILERON UPPER DOUBLER AND SPAR CRACKED. CRACK LENGTHS 10MM (0.39IN) IN DOUBLER AND 5MM (0.196IN) IN SPAR. (CASA# 510001482)SDR AU510001469Bracket · cracked(AUS) LH AND RH AILERONS PNO 105-130000-1 (LH) AND PNO 105-130000-2 (RH) SPARS AND DOUBLER BRACKETS CRACKED AT PUSHROD SUPPORT BRACKETS. (CASA# 510001469)SDR AU510001460Spar · cracked(AUS) LT AND RT AILERONS PNO 105-130000-1 (LT) AND PN 105-130000-2 (RT) SPARS AND DOUBLER BRACKETS CRACKED AT PUSHROD SUPPORT BRACKETS. (CASA# 510001460)SDR AU510001458Structure · cracked(AUS) LT AND RT AILERONS PNO 105-130000-1 (LT) AND PN 105-130000-2 (RT) SPARS AND DOUBLER BRACKETS CRACKED AT PUSHROD SUPPORT BRACKETS. FLEET INSPECTION FOUND SIMILAR CRACKING ON FOUR OF SEVEN AIRCRAFT. (CASA# 510001458)SDR AU510001448Spar · cracked(AUS) LT AILERON SPAR AND DOUBLER LOCATED BEHIND THE HINGE ATTACHMENT AND CONTROL INPUT HINGE CRACKED IN TWO PLACES. SPAR HAD BEEN PREVIOUSLY REPAIRED. SUSPECT REPAIR WAS POORLY DESIGNED AND NOT STRONG ENOUGH. AILERON HAD BEEN REMOVED FOR A BEARING REPLACEMENTSDR DHL2005803536Bracket · brokenITEM REF. NR. 033548: LT IB AILERON BRACKET BROKEN (NR 2 HINGE) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PAGE 1. REMOVED DAMAGED BRACKET IAW SRM 51-1-21, SRM 51-3-0, SRM 51-1-20D. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW BRASDR SIMA200533603Fitting · wornTHE LT AILERON OB HINGE POINT BEARING HOLE WAS FOUND TO BE WORN BEYOND MANUAL LIMITS. REMOVED DAMAGED HINGE FITTING. LOCATED AND DRILLED IN NEW FITTING. APPLIED ALODINE AND PRIMER TO ALL BARE SURFACE. REPAIR DONE IAW SRM. (K)SDR 05FDEA03894Repair · properLT WING OUTBOARD AILERON UPPER SURFACE FOUND A REPAIR 5" BY 2.75" ON SKIN AT STA XOA 997. PERFORMED A GVI OF REPAIR IAW SRM 57-00-01 FIG 4 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-2P E3.SDR 05FDEA03887Repair · properRT WING OUTBOARD AILERON FOUND FLUSH DOUBLER REPAIR ON LOWER SKIN FROM STA XOA 1003 TO STA 1041 DIMENSION 38" BY 26". PERFORMED A GVI OF REPAIR IAW SRM 57-10-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001-P2 E3.SDR 05FDEA03876Repair · properRIGHT WING OUTBOARD FLAP FOUND DOUBLER REPAIR ON LOWER SKIN AT STA XOF 456 DIMENSION 4.25 X 35 INCHES. PERFORMED AN INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001-P2 E3.SDR 05FDEA03875Repair · properLEFT WING OUTBOARD AILERON LOWER SURFACE FOUND A FLUSH DOUBLER 27 X 16.5 INCHES ON SKIN AT STA XOA 997. PERFORMED INSPECTION ON REPAIR IAW SRM 57-10-00 FIG 2 VOL 1, FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2 E3.SDR 05FDEA03671Doubler · unknownRIGHT WING LOWER SURFACE INBOARD AILERON FOUND AN EXTERNAL DOUBLER REPAIR BETWEEN WING STATIONS XIA316 TO XIA321. PERFORMED A GVI OF EXISTING DOUBLER IAW EO8-5100-7-5001 CRITERIA REQUEST AND FOUND IN COMPLIANCE WITH SRM 57-00-01 FIG 4.SDR 05FDEA03519Skin · crackedFOUND LT WING OUTBD AILERON WITH ONE CRACK 2" LONG WITH A STOP HOLE ON SKIN LOWER SURFACE AT STA XOA 824. TRIMMED BLEND OUT DAMAGE SKIN INSTALLED DOUBLER IAW SRM 57-10-00 FIG 85 AND SRM 51-71-00 PAR 16C VOL 2 AND SRM 51-35-02 PAGE 3-9. FABRICATED PART IAW DESDR AWXA200501439Skin · damagedMCN - DURING C13 CHECK DISCOVERED PLIES SEPARATED ON LOWER SURFACE OF THE RT AILERON AT HINGE ACCESS PANEL. UNABLE TO REPAIR AILERON DUE TO NON-DESTRUCTIVE INSPECTION REQUIREMENTS NOT AVAILABLE AT MCN STATION. MAINTENANCE REMOVED AND REPLACED THE RT AILERON SDR VNAA0510021Skin · undamagedDURING AN FAA RAMP CHECK, THE INSPECTOR DISCOVERED EVIDENCE OF LIGHTNING STRIKE DAMAGE ON TOP OF THE LT AILERON. THE AIRCRAFT WAS FERRIED TO CAK. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION AND FOUND NO LIGHTNING DAMAGE TO THE AIRCRAFT. SDR VNAA0510020Skin · lightning strikeDURING AN FAA RAMP CHECK, THE INSPECTOR DISCOVERED EVIDENCE OF LIGHTNING STRIKE DAMAGE ON THE TRAILING EDGE OF THE RT AILERON AND RT OUTBOARD FLAP. MAINTENANCE COMPLIED WITH AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND EVIDENCE OF LIGHTNING DAMAGE ON THSDR 2005FA0001522Hinge Bracket · corrodedDURING RECENT INSPECTION CORRODED HARDWARE WAS FOUND ON AILERON. AFTER AILERON WAS REMOVED HEAVY GALLING WAS FOUND ON OUTBOARD HINGE SUPPORT AND AILERON FITTING. SEVERAL OTHER AIRCRAFT WERE INSPECTED AND 3 OTHERS AND IDENTICAL GALLING. MFG WAS NOTIFIED AND SDR ASAA0540562Skin · gougedOKC - RIGHT AILERON TRAILING EDGE LOWER SURFACE GOUGED EDGE ADJACENT TO THE THIRD TAB HINGE FROM THE INBOARD EDGE. REMOVED DAMGAED AREA OF PLIES, PREPARED AND APPLIED REPAIR PLIES IAW B737-400 SRM 57-60-01 FIGURE 201 AND 51-70-05 PARAGRAPH 3. WEIGHT AND BALASDR C2XA05SH119Skin · delaminatedSHV - DURING C-CHECK THE LT AILERON HAS TWO AREAS OF DELAMINATION AND CRACKS ON LOWER INNER SKIN AT HINGE POINT. MAINTENANCE REPAIRED THE TWO AREAS OF DELAMINATION AND CRACK ON LOWER INNER SKIN AT HINGE POINT IN THE LT AILERON IAW EC5750-01260. THE AIRCRAFT SDR QXEA200501352Shroud · dentedPDX - DENT IN LOWER AILERON SHROUD, RIGHT HAND WING. REPAIRED IAW HORIZON AIR EA 2-57-322A.SDR USAA051208Skin · erodedRIGHT AILERON UPPER SURFACE I/B EDGE ERRODED. REPAIRED AILERON (COMPOSITE) TIME LIMITED REPAIR PER EA 96922, SRM 51-60-01, 51-70-03. DEFECT SIZE NOT DOCUMENTED.SDR 2005FA0001571Rib · crackedLT ELEVATOR WAS FOUND CRACKED BEHIND ELEVATOR BALANCE WEIGHT AT THE OB END OF THE ELEVATOR. UPON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE BALANCE WEIGHT WAS MODIFIED TO INCREASE THE WEIGHT. THE ADDED WEIGHT WAS DETERMINED TO BE INSTALLED BECAUSE THE SDR ASAA0540524Skin · delaminatedOKC - FOUND RIGHT AILERON LOWER SKIN DELAMINATED ON FORWARD INBOARD CORNER. PREPPED AREA, APPLIED BONDED GRAPHITE LAYUP IAW B737-400 SRM 51-70-17. (M)SDR MWEA050111Rub Strip · crackedLEFT AILERON INBOARD HINGE RUBSTRIP IS CRACKED. FABRICATED AND INSTALLED FILLER.SDR 05FDEA03234Skin · dentedLEFT WING LWR SURFACE INBOARD AILERON FOUND QTY 1 DENT AT STA XW 373. INSTALLED EXT DOUBLER IAW SRM 57-00-01 FIG 4 SHEET 2.SDR IXXA05SMN214SSkin · crackedDURING ROUTINE C CHECK INSPECTION, RT IB AIL L/E UPPER PLATING CRACK .2500 AT STA XA 470.000. PERFORMED MAJOR REPAIR IAW SRM 57-8-1 FIG 1, EO SEMAN NR 20051280 DATED 09-26-05. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL2024T3 0.040) SDR DHL2005742528Hinge · nickedRT AILERON O/B HINGE FITTING O/B SIDE (ON WING) FITTING NICKED AND GOUGED AROUND BUSHING. BLENDED GOUGE FOUND OUT OF LIMITS IAW BOEING DRAWING 65-19259-8. DRILLED, DEBURRED AND INSTALLED NEW FITTING, P/N 65-19259-6 IAW B727 SRM 51-30-2.SDR IXXA05SMN195SSkin · crackedDURING ROUTINE C CHECK INSPECTION, LT WING IB AILERON UPPER PLATING CRACKED 1, XA 502.000 PERFORMED MAJOR REPAIR IAW SRM 57-7-0 FIG 1, SRM 57-8-1 FIG 1, EO SEMAN NR 20051336. REMOVED DAMAGED PLATING IAW SRM 51-1-21. FABRICATED NEW PLATING (AL7075T6 0.040) SDR QXEA200501307Skin · chafedYYC - RIGHT AILERON UPPER NAD LOWER LEADING EDGE SKIN HAS CHAFED MARKS. REMOVED CHAFFING IAW CRJ-700 SRM 51-12-00-001-001-A01. FINISH RESTORED.SDR QXEA200501300Skin · chafedYYC - LEFT AILERON UPPER LEADING EDGE SKIN HAS CHAFED MARKS. REMOVED CHAFFED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01.SDR ASAA0540466Flange · delaminatedOKC - FOUND LEFT AILERON L/E FLANGE DELAMINATED AT WS 607. PREPPED DAMAGED AREA, ACCOMPLISHED HOT BOND REPAIR AT WS 607 IAW B737-400 SRM 51-70-05. (M)SDR ASAA0540465Flange · delaminatedOKC - FOUND LEFT AILERON L/E FLANGE DELAMINATED AT WS 613. PREPPED DAMAGED AREA, ACCOMPLISHED HOT BOND REPAIR AT WS 613 IAW B737-400 SRM 51-70-05. (M)SDR ASAA0540464Skin · delaminatedOKC - FOUND LEFT AILERON NOSE SKIN DAMAGED AT WS 574. PREPPED DAMAGED AREA, ACCOMPLISHED HOT BOND REPAIR IAW B737-400 SRM 51-70-05. (M)SDR ASAA0540463Skin · gougedOKC - FOUND LEFT AILERON OUTBOARD ATTACH AREA IS GOUGED. PREPPED GOUGED AREA, ACCOMPLISHED HOT BOND REPAIR IAW B737-400 SRM 51-70-05. (M)
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