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 AALA202307057100Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON #3 HINGE PIN AT WS 12870 AND RIB 24. REPLACED HINGE PIN PER AMM 27-14-41.SDR AALA202306260213Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON # 4 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C60027005.SDR AALA202307056272Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON #5 HINGE PIN BETWEEN WS 14057 AND WS 14459 AND BETWEEN RIB 26 AND RIB 27. REPLACED HINGE PIN PER AMM 27-14-41.SDR SWAA2023072560193Counterweight · corrodedCORROSION AILERON BALANCE ADJUSTMENT WEIGHT LOCATED BALANCE BAY #5 UPPER AND LOWER AT LT WING 2023-394673<[01] REPLACED AILERON BALANCE WEIGHT LOC. BALANCE BAY #5 UPPER AND LOWER LT WING IAW B737-700 SRM 51-60-01-0G-0 STEP 5.A.(5)(D);[02] REPLACED AILERON BALASDR SWAA2023072560194Counterweight · corrodedCORROSION AILERON BALANCE ADJUSTMENT WEIGHT LOCATED BALANCE BAY #5 UPPER AND LOWER AT RT WING 2023-394674<[01] REPLACED AILERON BALANCE WEIGHT LOC. BALANCE BAY #5 UPPER AND LOWER RT WING IAW B737-700 SRM 51-60-01-0G-0 STEP 5.A.(5)(D).;[02] REPLACED AILERON BALSDR SWIA202308020609Unknown · gougedRH WING INBD TRAILING EDGE GOUGE ON APRON SKIN WS48.0 (C-CHECK RO 7/30/2023) REPLACED THE 601R-53-41-115 (-2 ONLY) SKIN SECTION REF CRJ200 SRM 51-42-06 AND SRM 51-42-21 AND REO 601R-53-41-115 REV A DATE 2005-07-20.COMPLIED WITH 51-900-1003-SKYSDR IPXA2024020873411Skin · damaged*** SUPPLEMENTAL SDR *** R/H WING OUTBRD AILERON DAMAGE***SM26/LM4***HGR*** REMOVED LOTO OF AILERONS AND REACTIVATED IAW B767 AMM 27-11-00. OPS CHECK GOOD.SDR IPXA2023100273411Unknown · unknownRT WING OUTBRD AILERON DAMAGE. PROVIDED EO-88303-REQ1. THE NEW MOMENT FOR THE AILERON IS -107.635LB-IN. OPENSDR FDEA202305050992Unknown · unknownLH WING FIXED T/E ARROW EXTRUSION GOT CORROSION BETWEEN RIB26 & RIB28 REPLACED THE DAMAGED SECTION WITH NEW PART AND FASTENERS. I.A.W A300-600F SRM 51- 72-10-001, PAGE 2. AND 51-40-21-001, PARA 13, PAGE 149 - 156SDR AALA202305107532Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON #4 HINGE PIN AT WS 14057 AND RIB 26. REPLACED HINGE PIN PER TASK CARD 26C50027005.SDR SWI2023F00090Unknown · gouged*R/H INBD FLAP AFT LUG PLATES FOR INBD HINGE ARM GOUGED (2EA) (MARKED) (C-CHECK RO 6/20/2023) BLENDED OUT 2 EA GOUGES ON R/H INBD FLAP AFT LUG PLATES FOR INBD HINGE ARM. REF: CRJ200 SRM 51-12-00. DAMAGE REPAIRED PER REO 601R-57-52-2487, REV: --, 2023SDR SWI2023F00089Unknown · damaged*R/H INBD FLAP INBD HINGE ARM ASSY. TOP PLATE HAS IMPACT DAMAGE (MARKED) (C-CHECK RO 6/20/2023) DENTS ARE NOT PERMITTED ON HINGE ARM FITTING. FOUND TO BE OUT OF LIMITS REF CRJ200 SRM 57-54-00. REMOVED AND INSTALLED NEW BRACKET REF CRJ200 SRM 51-42-06 ANSDR SWIA20230530326Unknown · chafedR/H I/B FLAP VANE SKIN CHAFFED ON L/E AT 3 LOCATIONS COMMON TO BUMP STOPS (C-CHECK RO 5/23/2023) REMOVED AND REPLACED RH IB FLAP VANE, MID FLAP VANE CAP REF. CRJ-200 SRM, 51-42-13 AND DWG 601R14303 REV J. RH IB FLAP, OB AND IB FLAP VANE CAPS FOUND TO BESDR AALA202303215458Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON #2 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C50027005.SDR AALA202304184409Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON #5 HINGE PIN BETWEEN WS 14057 AND WS 14459, BETWEEN RIBS 26 AND 27. REPLACED HINGE PIN PER TASK CARD 26C50027005.SDR EE4Y2023031017384Rib · corrodedDURING THE INSPECTION ACCOMPLISMENT PER ALLIGIANT WOR CARD NO ZL-575-01-1-001 LEFT WING TRAILING EDGE CAVITY RIBS (2EA) WITH CORROSION BETWEEN RIB 21 AND 22. DUE TO THIS FACT THE RIBLES P/N: D5754171120000 WERE REPLACED IAW A320 SRM 51-72-11-911-001 AND WAS DSDR DALA2023022201314None · noneSHIP 1812 -ATB- DUE TO OUTBOARD TRAILING EDGE WING AND AILERON DAMAGE OBSERVED IN FLIGHT. NO DEGRADATION TO FLIGHT HANDLING CHARACTERISTICS. CORRECTIVE ACTION: FLIGHT LANDED WITHOUT INCIDENT. REPAIRED AILERON PER ERA 605753-14 REV ORIG. (4146802)SDR SWIA20230200016None · chafedRH INBOARD FLAP VANE OUTBOARD LEADING EDGE CHAFTED(MARKED). (C-CHECK RO 3/7/2023) REMOVED DAMAGE FROM RH INBOARD FLAP VANE OUTBOARD LEADING EDGE REF CRJ200 SRM 51-12-00. FOUND AREA TO BE OUT OF LIMIT. REPLACED FLAP VANE CAP AT RH INBOARD FLAP VANE OUTSDR GTIA2023020136949Spar · corrodedCORROSION FOUND ON SPAR LH WING SHROUD BOX FWD FACE BETWEEN RIBS WX866-WX1069. RAF-01 3102833-01 GENERATED.-PERFROMED PERMANENT REPAIR ON SHROUD BOX FWD FACE BETWEEN RIB 2 TO RIB 3 ON LH WING IAW EA # 57-0593-22 AND EC NO. EO 5751-2236.SDR DALA2023020700916Not Reported · not reportedSHIP 1821 LHW I/B AILERON LOWER SURFACE PUNCTURED AT CENTER AREA. CORRECTIVE ACTION: LHW I/B AILERON LOWER SURFACE REPAIRED AT CENTER AREA AS PER B767-400 SRM 57-60 (2613631)SDR UIEA2023013150082Skin · delaminatedRH I/B AILERON AFT EDGE O/B CORNER FOUND DELAMINATED. PERFORMED COMPOSITE LAYUP REPAIR AS PER SRM 51-70-17 PAR.5G.SDR 2023FA0000048Seal · departedSINCE PURCHASING THE AIRCRAFT AILERON GAP SEALS HAVE DEPARTED IN FLIGHT SEVERAL TIMES. 6 INSTANCES REQUIRED SPECIAL FLIGHT PERMITS TO RELOCATE THE AIRCRAFT TO ENVIRONMENTALLY CONTROLLED HANGARS. THERE WERE AT LEAST 2 OTHER OCCURRENCES THAT DID NOT REQUIRE SPSDR UIEA2023011800055Skin · failed inspDEVIATIONS WERE FOUND DURING THE ACCOMPLISHMENT OF SB767-57-010 PART 8 AT LH WING LOWER SKIN REPAIR AT STGR 9.5 AND WSTA 990.2(THE REPAIR WAS ACCOMPLISHED PER BOEING SR# 3-5538397542)SDR DALA2023012400558Cover · missingDURING INSPECTION FOUND RIGHT AILERON COVER MISSING. REPLACED FAIRING MPN 113A7180-4 REF B737 IPC 27-11-11-02 ITEM 240J ON RT WING AILERON NO DAMAGE FOUND IN AREA.SDR DALA2023012400544Bushing · corrodedCORROSION AILERON FIXED BUSHING ON HINGE FITTING 3 ON RH WING. REPLACED FIXED BUSHINGS (2EA) HINGE #3 RH AILERON AS PER AIRBUS CMM 57-61-21.SDR DALA2023012400542Bushing · corrodedCORROSION AILERON FIXED BUSHING I/B SIDE ON ACTUATOR FITTING 1 ON LH W. REPLACED FIXED BUSHINGS (1E/A) AILERON FIXED I/B SIDE ON ACTUATOR FITTING 1 ON LH WING AS PER , A319 AIRBUS CMM57-61-21.SDR DALA2023012400541Bushing · corrodedCORROSION HINGE 4 AILERON FIXED BUSHING ON LH WING. REPLACED FIXED BUSHINGS (2E/A) HINGE #4 LH AILERON AS PER A319 AIRBUS CMM 57-61-21.SDR DALA2023012400540Bushing · corrodedCORROSION HINGE 2 AILERON FIXED BUSHING ON LH WING. REPLACED FIXED BUSHINGS (2E/A) HINGE #2 LH AILERON AS PER A319 AIRBUS CMM 57-61-21.SDR DALA2023012400539Bushing · corrodedCORROSION AILERON FIXED BUSHING I/B SIDE ON HINGE FITTING 4 ON RH WING. REPLACED FIXED BUSHINGS (1EA) IB SIDE HINGE #4 RH AILERON AS PER AIRBUS CMM 57-61-21.SDR DALA2023012400538Bushing · corrodedCORROSION AILERON FIXED BUSHING I/B SIDE ON ACTUATOR FITTING 2 ON RH WING. REPLACED FIXED BUSHINGS (1EA) AILERON FIXED IB SIDE ON ACTUATOR FITTING 2 ON RH WING AS PER AIRBUS CMM 57-61-21.SDR DALA2023012400537Bushing · corrodedCORROSION AILERON FIXED BUSHING I/B SIDE ON ACTUATOR FITTING 1 ON RH WING. REPLACED FIXED BUSHINGS (1EA) AILERON FIXED IB SIDE ON ACTUATOR FITTING 1 ON RH WING AS PER AIRBUS CMM 57-61-21.SDR DALA2023012400536Bushing · corrodedCORROSION AILERON FIXED BUSHING I/B SIDE ON HINGE FITTING 1 ON RH WING. REPLACED FIXED BUSHINGS (1EA) IB SIDE HINGE 1 RH AILERON AS PER AIRBUS CMM 57-61-21.SDR DALA2023012400535Bushing · corrodedCORROSION AILERON FIXED BUSHING ON HINGE FITTING 3 ON RH WING. FIXED BUSHING ON HINGE FITTING 3 ON RH WING ( 2 EA) REFER TO AMDS CARD: 5760-10105-RH.SDR IXXA20230123444Indicator · unknownFLAP INDICATOR INDICATING SPLIT ON TAKEOFF AND LANDING. LEFT INDICATOR IS JUMPING. AIR TURN BACK TO DEPARTURE STATION WITH AN EMERGENCY DECLARATION. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL AIRCRAFT GROUNDED FOR UNSCHEDULED SDR AALA202301173635Skin · crackedAIRCRAFT IN BASE MAINTENANCE: LEFT WING AILERON UPPER SUFACE PLATE CRACKED. MAINTENANCE REPLACED AILERON PER AMM 27-14-41.SDR COEA2023011017807Channel · corrodedWO 239777 NR 600026 HEAVY CHECK COE/MAJOR REPAIR: R/H AILERON TRIM TAB CLOSE OUT CHANNEL UPPER SURFACE HAS MULTIPLE AREAS OF LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00205880_01...19969 ISSUE A, DATED 1/2/2023.SDR SWIA2023010567079Flap Track · wornL/H I/B FLAP TRACK 1A HAS THICKNESS REDUCTION OF .030". LENGTH OF DAMAGE IS .6". REMOVED AND REPLACED LH I/B FLAP TRACK 1A REF EMB 175 AMM 57-54-25.SDR SWIA20221207None · chafedINSTALL LH INBD FLAP TO FACILITATE OTHER MAINTENANCE PER AMM TO FOM. (C-CHECK RO 2/14/2023) INSTALLED LH I/B FLAP REF. CRJ 200 AMM 27-54-01-400-801SDR DXTA2022120275290Aileron · vibrationSIGNIFICANT AIRFRAME VIBRATION IN LEVEL FLIGHT AND ACCELERATING AT 12000'. VIBRATION CAME ON AT BETWEEN 270-290 KNOTS. FELT A LIGHT RUMBLE IN THE YOLK AT 210 KNOTS. REMOVED RT AILERON PANEL. INSTALLED A SERVICEABLE RT AILERON PANEL ASSEMBLY. WORK PERFORMED SDR WX0A1900010031697Skin · corrodedNRC 5000-0013: 1711-57 ON L/H WING, CORROSION SUSPECTED UNDER TRAILING EDGE SEAL PLATE AT INBORD HINGE SPOILER #2. / L/H WING, TRAILING EDGE OVERHANG SKIN PANEL #2 AT INBD HINGE OF SPOILER #2 (BTW RIBS 9-11) UPPER AND LOWER SURFACE PERMANENTLY REPAIRED PER AIRSDR WX0A1900010031696Skin · corrodedNRC 5000-0012: 1711-51 ON L/H WING, CORROSION SUSPECTED UNDER TRAIING EDGE SEAL PLATE OUTBORD MAIN HINGE SPOILER #1. / L/H WING TRAILING EDGE OVERHANG EXTENDING FWD OF THE REAR FALSE SPAR, UPPER SKIN PANEL #2 LOWER SURFACE OUTBD OF OUTBD MAIN HINGE SPOILER #1SDR REXA2022120102653Skin · chafedL/H WING/AILERON PANEL 599AB IS CHAFED. REMOVED CHAFE DAMAGE IAW CRJ-900 SRM 51-12-00-001-001-A01. UPON FURTHER INVESTIGATION, DAMAGE MEASUREMENTS ARE OUT OF LIMITS IAW CRJ-900 SRM 57-61-01-101-001-A01. ORIGINAL THICKNESS: 0.100" MAX MATERIAL REMOVED: 0.075" MSDR FDEA202211232994Balance Weight · corrodedLEFT HAND OB AILERON WEIGHTS HAVE AREAS OF PAINT FLAKE AND CORROSION. REPLACED L/H WING O/B AILERON WEIGHTS IAW CMM 57-51-03 AND EA 1-5750-T0358085 P3.SDR FDEA202211182957Balance Weight · corrodedRH WING O/B AILERON COUNTERBALANCE WEIGHT, 4TH FROM O/B END, HAS LONG AREA OF PEELED TOPCOAT, PITTING WHERE MKD. DBJ-200. REMOVED AND REPLACED R/H WING O/B AILERON THE 4TH FROM O/B END IAW CMM 57-51-03 R P607SDR FDEA202211182956Balance Weight · corrodedRH WING O/B AILERON COUNTERBALANCE WEIGHT , 3RD FROM O/B END, HAS LONG AREA OF PEELED TOPCOAT, PITTING WHERE MKD. DBJ-100. REMOVED AND REPLACED R/H O/B WING O/B AILERON COUNTERBALANCE WEIGHT 3RD FROM O/B END IAW 57-51-03 R P607SDR SWAA2022113069897Balance Weight · corrodedCORROSION ON BALANCE WEIGHTS POSITION NR 3, UPPER AND LOWER AILERON, BALANCE BAY NR 5, LT WING. REPLACED THE AILERON BALANCE WEIGHTS IAW SRM 51-60-01-0G-0 STEP 5, A, 5, D.SDR SWAA2022113069896Balance Weight · corrodedCORROSION ON BALANCE WEIGHTS POSITION NR 3, UPPER AILERON, IN THE BALANCE BAY NR 5, RT WING. REPLACED THE AILERON BALANCE WEIGHT IAW SRM 51-60-01-0G-0, STEP 5.A. 5 . D.SDR AALA202211151302Blucket · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON #1 HINGE BOLT. MAINTENANCE REPLACED HINGE BOLT PER AMM 27-14-41.SDR AALA202211169137Hinge Pin · corrodedAIRCRAFT IN BASE MAINTENANCE CORROSION ON LEFT WING AILERON #1 HINGE PIN AT WS 12277 AND RIB 23 ON THE REAR SPAR AREA. MAINTENANCE REPLACED HINGE PIN PER AMM 27-14-41.SDR LR7A2022110703236Web · crackedDURING SCHEDULED C-14 CHECK UNDER JOB CARD HC5711, FOUND LH AILERON ASSY WEIGHT SUPPORT ASSY WEB CRACKED AT AS29.17L. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 0730. / PSE# 57-50-21, AD 2012-06-09
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