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 = '5755' 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 = '5755' 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 AWXA200600289Bolt · corrodedMCN - LEVEL 2 CORROSION WAS FOUND ON THE RT WING, SPOILERS 1 THROUGH 5, INNER HINGE PIN BOLTS AT THE THREAD AND HEAD RADIUS. NO CORROSION LIMITS WERE AVAILABLE. ALL SPOILER, INNER HINGE, PIN BOLTS WERE REMOVED AND REPLACED ON SPOILERS 1 THROUGH 5 IAW AIRBUS SDR HNAA0600004Bracket · looseNR 1 SPOILER PUSH OFF LIGHT ILLUMINATED INTERMITTENTLY IN FLIGHT FOLLOWED BY UNCOMMANDED ROLL TO LEFT AND STEADY ILLUMINATION OF PUSH OFF LIGHT. CREW DISCONNECTED AUTOPILOT AND SELECTED PUSH OFF SWITCH. TIGHTENED RIGHT HAND SPOILER QUADRANT WHICH WAS LOOSE OSDR AWXA200600290Bolt · corrodedMCN - LEVEL 2 CORROSION WAS FOUND ON THE LT WING, SPOILERS 3 THROUGH 5, INNER HINGE PIN BOLTS AT THE THREAD AND HEAD RADIUS. NO CORROSION LIMITS WERE AVAILABLE. ALL SPOILER, INNER HINGE, PIN BOLTS WERE REMOVED AND REPLACED ON THE LT WING, SPOILERS 3 THROUGH SDR ASAA0640057Skin · puncturedOKC - FOUND NR 5 SPOILER PUNCTURED ON LOWER SURFACE 4 INCHES FROM T/E 33 INCHES FROM INBOARD END. REPAIRED DAMAGED AREA IAW ASA EA 5770-01067SDR AWXA200600401Skin · debondedMCN - DURING C19 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE NR 3 SPOILER, AFT OF SEAL AND INBOARD OF ACTUATOR AT WBL 225L. DISBOND AREA WAS REMOVED AND THE NR 3 SPOILER WAS PREPPED FOR REPAIR IAW BOEING 737-300 SRM 51-70-10-2R4. THE DISBONDED SDR DHL2006804502Skin · delaminatedLT WING NR 2 SPOILER UPPER SKIN DELAMINATED. REMOVED AND REPLACED NR 2 LT SPOILER PANEL IAW MM 27-61-1 PG 201-207. REFER TO NR 044174 FOR OPS CHECK.SDR 0601051Spoiler · delaminatedREPAIRED LEFT WING SPOILER #3 DUE TO DELAMINATION.SDR 06FDEA00028Structure · crackedLT WING NR 1 SPOILER TRAILING EDGE CRACKED LATERALLY OB AND AFT OF ACTUATOR. REMOVED AND REPLACED LT WING NR 1 SPOILER PANEL IAW MD10MM 27-60-01-4. CHECKED CLEARANCES IAW MD10-MM 27-60-01-6. SEE SNRM N00298 OF WORK ORDER NR 00031297.SDR SWAA060035Hinge Fitting · brokenDURING SCHEDULED C2 CHECK, FOUND LT WING NR 4 SPOILER OUTBD ACTUATOR ATTACH HINGE FITTING BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER MM.SDR SWAA054164Casting · crackedDURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 SPOILER INBOARD ACTUATOR ATTACH POINT SUPPORT CASTING CRACKED. REMOVED AND REPLACED CASTING PER SRM.SDR SWAA054058Skin · delaminatedDURING SCHEDULED A2 CHECK, FOUND LEFT WING NR 2 SPOILER DELAMINATED. REMOVED AND REPLACED NR 2 SPOILER PER MM.SDR SWAA054051Skin · delaminatedDURING SCHEDULED C4 CHECK, FOUND LT WING SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.SDR 05FDEA04363Skin · damagedRT WING 1 SPOILER HAS PENETRATION DAMAGE 3" BY 1". REPAIRED NR 1 SPOILER IAW A310-200 SRM 57-70-00 REPAIR.SDR QXEA200600260Shroud · brokenYYC - RT WING BOTTOM TRAILING EDGE. MULTI FUNCTION SPOILER SHROUD HAS MULTIPLE BROKEN AND LOOSE FASTENERS BETWEEN WS 170.83 TO WS 231.23. FASTENERS REPLACED (MS20426T) IAW CRJ700 SRM 51-02-06-001-001-A01.SDR QXEA200600215Skin · crackedYYC- RT WING OUTBD MULTIFUNCTION SPOILER UPPER CENTER HINGE SKIN CRACKED. SPOILER UPPER CENTER HINGE SKIN REPAIRED IAW CRJ 700 EA R-57-136 AND REO 670-57-73-011 REV STEPS 1 AND 2. NDT HFEC CARRIED OUT IAW NDTM PART 1 51-20-006 NO CRACKS NOTED. ROTARY FLAP PSDR AWXA200600093Skin · debondedMCN - DURING C16 CHECK DISCOVERED TWO SPOTS OF DISBOND ON THE NR 6 SPOILER, LOWER SURFACE, FROM WBL 228.53R TO WBL 330.53R. MAINTENANCE REMOVED DISBONDED SKIN AND CORE IAW BOEING 737-300 SRM 51-70-10-2R4 FIG 203. FABRICATED REPLACEMENT CORE AND DOUBLER IAW BSDR DEBA401PP2Switch · malfunctionedON ACCELERATION FOR TAKEOFF THE CREW RECEIVED A TAKEOFF CONFIGURATION WARNING HORN AT 100KTS, PRIOR TO ROTATION. TAKEOFF WAS ABORTED WITHOUT INCIDENT. THE AIRCRAFT RETURNED TO THE RAMP. WHILE TROUBLESHOOTING THE PROBLEM CORRECTED ITSELF. DETERMINED THAT TSDR SWAA053878Casting · crackedDURING SCHEDULED C1 CHECK, FOUND RT WING NR 5 SPOILER OTBD HINGE CASTING CRACKED. REMOVED AND REPLACED NR 5 SPOILER PER MM.SDR 0601054Spoiler · delaminatedREPAIRED LEFT WING NR 3 SPOILER DUE TO DELAMINATION.SDR SWAA053816Rod End · brokenFOUND LT WING NR 4 GROUND SPOILER OTBD ACTUATOR ROD END BROKEN. REMOVED AND REPLACED GROUND SPOILER OTBD ACTUATOR PER MM.SDR QXEA200501732Bolt · damagedDURING HIGH SPEED CLIMB & CRUISE, AUTOPILOT ON 'MISTRIM RT WING DOWN' DISCONNECTED AP. MANUALLY RETRIM A/C TO HALF SCALE RT WING DOWN DURING APPROACH WITH FLAPS 15 DEG NEEDED TO START TAKING OUT THAT TRIM UNTIL FLAPS AT 35. NO RT WING DOWN NEEDED. MX PERFORSDR UPS06M46389Skin · corrodedINSPECTION TYPE:C RT WING TOP SIDE FIXED T/E PANEL XORS 683.4 FWD OF NR 4 SPOILER FOUND CORROSION UNDERNEATH PNL. CORROSION REMOVAL C/OUT FOUND MAT REMOVED EXCEEDED LIMIT. HFEC C/OUT FOUND NO EVIDENT OF CRACK. FLAP PEENING C/OUT ON REWORK AREA PER EN1039-0 SDR 05FDEA03868Repair · unknownRT WING SPOILER NR 3 FOUND DOUBLER REPAIR ON LOWER SKIN DIMENSION 10 X 6 INCHES. INSPECTED, REMOVED AND INSTALLED SPOILER NR 3 RT WITH NEW HARDWARE IAW MM 27-60-01-4. PERFORMED FUNCTIONAL TEST IAW MM 27-60-01-4.SDR SWAA053554Ski · delaminatedDURING SCHEDULED C3 CHECK, FOUND RT WING NR 6 SPOILER DELAMINATED. REMOVED AND REPLACED SPOILER PER MM.SDR DHL2005749022Spoiler · delaminatedNR 5 SPOILER UPPER IB FWD CORNER TAPS SOFT. CUT OUT DELAMINATED AREA ON NR 5 SPOILER UPPER IB FWD CORNER APPROX 5 INCHES BY 6 INCHES FABBED FILLER 5 INCHES BY 6 INCHES AND DOUBLER APPROX 6 1/2 INCHES BY 7 12/2 INCHES FROM 7075T6 .020 PO526029 CLEANED PREPPED SDR AWXA200501473Panel · debondedDURING C19 CHECK DISCOVERED DEBONDED AREA ON THE UPPER AND LOWER SURFACE OF THE NR 3 SPOILER PANEL FROM WBL 229.0L TO WBL 304.5L. MAINTENANCE REMOVED DAMAGED AREA ON THE NR 3 SPOILER PANEL IAW SRM 51-70-10-2R4. FABRICATED REPAIR DOUBLER AND REPAIR CORE IAW SSDR DHL2005749003Hinge · crackedFOUND NR 1 SPOILER 2ND HINGE CUTOUT HAS 1" CRACK. STOP DRILLED CRACK IAW 727 SRM 51-10-1. VERIFIED CRACK TERMINATION IN STOP DRILL HOLE IAW B727 NDT PT 6 51-00-00 FIG 23. FABRICATED REPAIR DOUBLER FROM MAT 70-75-T6 071 - PO NR 9002507 DIMS 5 3/4" BY 4 1/4" SDR AWXA200501340Skin · crackedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED THE NR 6 SPOILER ON UPPER SURFACE BULGING WITH CRACK, .5 INCHES LONG, WS 228R. MAINTENANCE REMOVED SPOILER AND REMOVED DAMAGE IAW BOEING 737-300 SRM 57-70-01-2R4 FIG 201. FABRICATED AND INSTALLED DOUBLER ON THSDR 05FDEA03402Skin · chafedLEFT WING SPOILER NR 2 O/B FWD EDGE 2 EA AREAS THAT ARE CHAFED. COMPLIED WITH EA 6-5750-92961 N00044.SDR AWXA200501301Spoiler · debondedMCN - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE NR 8 SPOILER UPPER AND LOWER SURFACE, 15.5" FROM OUTBOARD END AND 6" FROM THE AFT EDGE, FROM WL 430.97 TO WBL 432.97. MAINTENANCE CUT OUT AND REMOVED DAMAGED SKIN AND CORE FROM THE NR 8 SPOILER IAW BOEING SDR ABXA050251Fitting · crackedLEFT INBOARD SPOILER HAD AN APPROXIMATE .1562 INCH CRACK IN THE CENTER DOUBLER ABOVE THE CENTER DRIVE FITTING. BLENDED CRACK IAW REA D957-52510.SDR ASAA0580525Panel · gougedOKC - DURING HV-CHECK, LEFT INBOARD SPOILER PANEL GOUGED ON UPPER SURFACE AT TRAILING EDGE. REPLACED DAMAGED PLIES. (M)SDR EIA2005160Hinge Fitting · failedNR 7 SPOILER HINGE FITTING FAILED CAUSED DAMAGE TO NR 7 SPOILER AND LEADING EDGE OF INBOARD FORE FLAP. ACCOMPLISHED ECRA 486-57-046-1 BEFORE FLIGHT. REPLACED NR 7 SPOILER PANEL, REWORKED HINGE AND REPAIRED FLAP AS PER INSTRUCTIONS OF ECRA PART 1.SDR AWXA200501203Skin · debondedMCN - MAJOR REPAIR - DURING C18 CHECK DISCOVERED DISBOND AREA ON THE LOWER SURFACE OF THE NR 1 SPOILER, APPROXIMATELY 6 INCHES FROM INBOARD EDGE, FROM WBL 398.50L TO WBL 408.50L. MAINTENANCE REMOVED DISBOND AREA AND CORE FROM NR 1 SPOILER LOWER SURFACE IAW BOSDR P5CA0501402Panel · crackedLEFT WING NR 3 O/B SPOILER HAS A CRACK AT UPPER SURFACE (NEAR HINGE FITTING SUPPORT). REMOVED AND REPLACED NR 3 SPOILER PER MM 27-61-02.SDR P5CA0501404Panel · crackedLT WING NR 3 O/B SPOILER HAS A CRACK AT UPPER SURFACE (NEAR HINGE FITTING SUPPORT). REPLACED NR 3 SPOILER ASSEMBLY IAW AMM 27-61-02.SDR USAA200508005Fitting · chafedFOUND 3/8" BY .045" CIRCULAR WEAR AT OUTBOARD HINGE BRACKET FOR NR 5 SPOILER BOARD, WBL 169.25R. DEFECTIVE PART REPLACED WITH IDENTICAL PART.SDR AWXA200501050Panel · debondedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE UPPER AND LOWER SURFACE OF THE NR 3 SPOILER PANEL AT INBOARD AFT CORNER FROM WING STATIONS 291L TO WING STATIONS 297L. MAINTENANCE REMOVED DISBOND AREA FROM THE NR 3 SPOILER PANEL IAW BOEINGSDR AWXA200501047Skin · debondedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED DISBOND AREA ON THE UPPER AND LOWER SURFACE OF THE NR 2 SPOILER. SEVENTEEN INCHES FROM THE INBOARD END AND FIVE INCHES FROM THE AFT EDGE FROM WING STATIONS 354.75L TO WING STATIONS 359.2L. MAINTENANCE REMOVED SDR 05FDEA02238Depressor · crackedLEFT WING UPPER T/E ACCESS PANEL SUPPORT PLATE O/B OF NR 5 SPOILER IS CRACKED. REMOVED AND REPLACED PLATE IAW SRM 51-30-2.SDR 05FDEA02218Skin · corrodedRIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER SKIN BULGE AT XORS 536 STRINGER 1. RHW UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER XORS 536 STRINGER 1 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED: 0.032"; ORIG. THICKNESS: 0SDR 05FDEA02217Skin · corrodedRIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER SKIN BULGE AT XORS 538.49 STRINGER 1. RT WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER XORS 538.49 STRINGER 1 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED: 0.035"; ORIG. THICKNSDR 05FDEA02216Skin · corrodedRIGHT HAND WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER SKIN BULGE AT XORS 538.49 STRINGER 4. RT WING UPPER SURFACE TRAILING EDGE FORWARD OF NR 2 SPOILER XORS 538.49 STRINGER 4 SKIN BULGE AREA CORROSION REMOVED. MAT'L REMOVED: 0.024"; ORIG. TSDR HNAA0500072Actuator · leakingNR 1 HYDRAULIC ISOLATION VALVE CAUTION LIGHT ILLUMINATED WHEN TAKING RUNWAY FOR TAKEOFF. NR 1 HYDRAULIC QUANTITY WENT TO 1.0 NORMAL BRAKING FAILED. CREW SHUT DOWN NR 1 ENGINE AND RETURNED TO GATE. REMOVED AND REPLACED THE LEFT WING INBOARD ROLL SPOILER PER SDR AWXA200500924Spoiler · debondedDURING C18 CHECK FOUND A DISBOND AREA ON THE UPPER SURFACE OF THE NR 4 SPOILER, 36" FROM INBOARD END FROM WBL 123.75 TO WBL 135.75. MAINTENANCE REMOVED DISBOND AREA FROM THE UPPER SURFACE OF THE NR 4 SPOILER, 36" FROM INBOARD END IAW BOEING 737-300 SRM. FABRSDR AWXA200500840Bracket · crackedMCN - MAJOR REPAIR - DURING C16 CHECK DISCOVERED SMALL CRACK LOCATED ON RIGHT WING INBOARD HINGE BRACKET FOR INBOARD GROUND SPOILER. MAINTENANCE REMOVED CRACKED HINGE BRACKET FROM RT WING INBOARD GROUND SPOILER IAW BOEING 737-300 SRM 51-40-02-0 FIG 8. PREPPESDR SWAA051898Hinge · brokenDURING SCHEDULED RON CHECK, FOUND LT WING INBOARD T/E GROUND SPOILER BROKEN AT HINGE CASTING. REMOVED AND REPLACED SPOILER PER MM.SDR 05FDEA01662Angle · crackedNR 2 SPOILER UPPER SURFACE CRACKED AT 2 CENTER ATTACHMENTS. REMOVED AND REPLACED LT NR 2 SPOILER HINGE CUTOUT ANGLE IAW SRM 51-30-2.SDR 05FDEA01619Attach Angle · damagedNR 2 SPOILER ACTUATOR LWR ATTACH ANGLE HOLES ARE ELONGATED. *S/D* REPLACED NR 2 SPOILER ACTUATOR SUPPORT FITTING PER SRM 51-30-2.SDR COMA0570070Hinge Fitting · crackedRT MULTI-FUNCTION SPOILER CENTER HINGE FITTING CRACKED IN HALF. REMOVED CRACKED FITTING AND INSTALLED NEW FITTING P/N CC670-17113-5 IAW CRJ AMM 57-73-27-400-801-A01.
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