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 engine_model_key = 'CF66D' 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 engine_model_key = 'CF66D' 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 05FDEA01191Gearbox · crackedAT B - 9 CHECK TROUBLESHOOTING OIL LEAK ON NR 2 ENGINE S/N 451280, FOUND ACCESSORY GEARBOX, FUEL PUMP DRIVE PAD, HAD A 4 INCH CRACK, EMANATING FROM DRIVE PAD. DOCUMENTED ON B - 9 CHECK WORK PACKAGE, WORK ORDER 28833, NR 108. ENGINE REPLACED ON SEQ 324 WORK CSDR 05FDEA00912Engine · stalledENGINE NR 2 COMPRESSOR STALLS (SIGNIFICANT BANG-BANG) UPON THROTTLE REDUCTION, FL280- PERFORMANCE ENG SHUTDOWN PER QRH.SDR 05FDEA00332Engine · stalledON DESCENT FROM 36,000 TO 35,000 AND AGAIN DESCENT TO 34,000 FT NR 1 ENGINE COMPRESSOR STALLED AND N1, N2 WENT TO LESS THAN IDLE, RESTARTED EACH TIME AND HAD MUCH COMPRESSOR STALLS. ENGINE WAS THEN SHUT DOWN. BOROSCOPE INSPECTED NR 1 ENGINE FOR STALLS, FOUNDSDR 05FDEA00312Engine · vibrationON TAKEOFF NR 2 THROTTLE REQUIRED ONE KNOB WIDTH BEYOND 1 & 3 ON CLIMBOUT AT 3000 FT AGL RECEIVED AIR MANF 2 FAIL WITH NOTICEABLE AIRFRAME VIBRATION. ENG 2 OIL TEMP HIGH ALERT FOLLOWED WITH PEAK OIL TEMP OF 201 DEGREES C. ENGINE WAS SHUTDOWN AND NR 2 ENGINE SDR 05FDEA00144Engine · leakingNR 2 ENGINE OIL LEAK. ON CLIMBOUT NR 2 ENG OIL QTY DROPPED 18 QTS TO 9 QTS ON FINAL NR 2 OIL READ 3 QTS, AFTER LANDING NR 2 OIL QTY WAS 9 PTS. REMOVED & REPLACED B-SUMP SCAVENGE LINE IAW MM 79-00-01-1. FUEL SHROUD REMOVED AND REPLACED REF WRI 73-10/0359. RSDR ARWA20050104Engine · failedNR 2 ENGINE FAILED ON ROTATION. ENGINE SHUTDOWN IN ACCORDANCE WITH CHECKLIST. AIRCRAFT RETURNED TO MSLP WITHOUT ANY FURTHER INCIDENT. ACCOMPLISHED RED BORDER 019056; REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH ARROW AIR DC-10 WORK CARD 142R7101M. PSDR 04FDEA03189Bleed Valve · inoperativeON TAKEOFF AT1000' AGL GOT LEVEL 3"AIR MANF 1 FAIL. COMPLIED WITH QRH, RETURNED TO AN UNEVENTFUL LANDING. PERFORMED DECAY CHECK FOR PNEUMATIC SYS 1 PER MM. CHECKED NORMAL. WHILE T/S FOUND AIU 3 INTERNAL FAULT FAILED TEST. REMOVED AND REPLACED AIU. NO FSDR 05FDEA01771Skin Panel · crackedDURING MAINTENANCE INSPECTION, FOUND CRACK IN THE UPPER CONSTANT SECTION OF THE HORIZONTAL STABILIZER. THE CRACK WAS IN THE FLYABLE LIMITS. DUE TO SHORT INSPECTION REQUIREMENTS IT WAS DECIDED TO REPLACE ALL CRACKED PANELS IAW SB 55-16, IAW EA 8-5510-84843 (RSDR 04FDEA03136Fan Blade · looseCRACKED SEALANT/AXIAL AND RADIAL PLAY AT 29 EACH FAN DISCHARGE VANES, INSIDE NR 1 ENGINE, ON OUTER SHROUD. REMOVED AND REINSTALLED STAGE ONE FAN BLADES TO FACILITATE INSPECTION/REPAIR OF OUTLET GUIDE VANES. INSPECTED 29 OUTLET GUIDE VANES. NO METAL TO METALSDR 04FDEA02990Skin · damagedDURING AIRPLANE CONVERSION FROM P-F/ACF HAVING REPLACE SKIN P/N AGA3108-1 FRAME AND SHEAR TIE AT STA 1986 ,PN AGA3783-3/-25 FRAME ,SHEAR TIE AT STA 1975 P/N, AGA3183-3/-23. REWORK INVOLVED AREA IAW EA 8-5310-77036.SDR 04FDEA02987Panel · crackedN12347, DURING PASSENGER TO FREIGHT COVERSION: ON PANEL 7208-1 RT SIDE, FOUND BY ULTRASONIC INSPECTION NR 1 HOLE WITH CRACK L .2500 INCH AT 1INCH FROM BOTTOM. POSITION NR 3, SHORE AIRCRAFT AS REQUIRED IAW SB 55-16, REPLACE CRACKED PANEL IAW SB 55-16 FIG 4 GRSDR 04FDEA02988Longeron · corrodedDURING PAX TO FREIGHT CONVERSION FOUND INTERNAL FUSELAGE STA 791-808, STR 27, RT VANE DOOR WITH CORROSION AND EXFOLATION. REMOVE SCUFF PLATE FOR ACCESS OPEN SKIN, REPLACE DAMAGE SECTION OF LONGERON 27 AND REINSTALL SKIN IAW SRM 51-33-01 PAG 34-47;AND SCUFF PSDR 04FDEA02989Longeron · corrodedDURING PAX TO FREIGHT CONVERSION FOUND INTERNAL FUSELAGE STA 791-808, STR 27, RT VANE DOOR WITH CORROSION AND EXFOLATION REMOVED SCUFF PLATE FOR ACCESS OPEN SKIN, REPLACE DAMAGE SECTION OF LONG 27 AND REINSTALL SKIN IAW SRM 51-33-01 PAGE 34-47; AND SCUFF PSDR 04FDEA02981Roller · wornRT WING FLAP SIDE LOAD ROLLER FITTING LOWER LUG FLAT SPOTTED AND HOLES HAVE EVIDENCE OF PITTING. REMOVED PITTING AND CORROSION FROM LUG AND BORE. FABBED AND INSTALLED 2 EACH REPAIR BUSHINGS IAW SRM 57-20-00 VOL. I PAGE 16. BLENDED FLAT SPOTTED AREA IAW EA8-SDR 04FDEA02950Frame · crackedNR 2 ENGINE RT THRUST REVERSER TRAILING EDGE AFT FLANGE CRACKED APPROXIMATELY 6 INCHES FROM BOTTOM. COMPLIED WITH MFG EA 8-7830-81496SDR 04FDEA02951Panel · misalignedNR 1 PYLON PRECOOLER VENTILATOR PANEL ASSY PN AUB7054-501 FASTENER HOLES DO NOT ALIGN TO PYLON STRUCTURE. COMPLIED WITH EA 8-5480-81485 REV. A, NR 1 ENGINE VENTILATOR PANEL REPAIR.SDR 04FDEA02952Lavatory · not seatedLAVATORY PAPER AND WASTE RECEPTACLE DOES NOT SEAL CORRECTLY. RESEALED LAVATORY PAPER AND WASTE RECEPTALE IAW MD10-10 SRM 51-41-01 VOL II AND EA 8-2540- 82478, SEALING OF FORWARD LAVATORY TRASH SHOUT.SDR 04FDEA02929Fitting · corrodedCOMPLY WITH EA 8-5750-82057. WINGS LT IB FLAP VANE ASSY, REPAIR OF O SIZED HOLES IN CHANNEL FITTINGS CLOSING ACTION ON 10/12/04.ON N/R S00010. COMPLIED WITH EA 8-5750-82059.SDR 04FDEA02909Stop · brokenCOMPLY WITH E.A.8-5210-82059.REWORK OF ABA7188-1 FITTING TO REPLACE ABA7156-501 FOR R1 DOOR. CLOSING ACTION ON 10/11/04. ON N/R S00024. COMPLIED WITH EA 8-5210-82059SDR 04FDEA02914Hinge · corrodedLT IB FLAP OB HINGE PIVOT BORE FACE PITTED AND GOUGED (AIRFRAME SIDE) LOCATION NR 3. REMOVED BUSHING, REMOVED CORROSION, AND COMPLIED WITH EA 8-5750-81473 REF NR N00295.SDR 04FDEA02873Hinge · gougedCOMPLY WITH EA 8-5240-82048. TAILCONE-PATIO DOOR HINGE REPAIR P/N AKC7011. CLOSING ACTI0N ON 10/05/04. ON N/R S00019 COMPLIED WITH EA 8-5240-82048.SDR 04FDEA02874Support · corrodedLT/RT OB FLAPS-FLAP VANE SUPPORTS CORROSION REWORK. CLOSING ACTION ON 10/04/04. ON N/R S00018. COMPLIED WITH EA 8-5750-82049.SDR 04FDEA02879Hinge · corrodedLT WING OB FLAP IB HINGE, LOCATION NR 6, OB BORE IS CORRODED. REMOVED CORROSION, BEGINNING BORE DIAMETER 1.240, FINAL 1.266, MATERIAL LOSS 0.026 IAW DAC CMM 57-44-08, ETCH INSPECTED IAW DAC CMM 57-44-08 AND 20-11-02. PEENED IAW DAC CMM 57-44-08 AND 20-11-01.SDR 04FDEA02676Warning Light · illuminatedAFTER T/O AT 800 FT, HAD FLAP DISAGREE LIGHT ILLUMINATE . RUN RED TABS AND THE LIGHT DID NOT GO OUT. DUMPED APPROX. 20K OF FUEL. FLAPS EXTENDED THE LIGHT GOES OUT. THERE WERE NO ABNORMAL FLT CHARACTERISTICS WITH FLAPS CYCLING OR EXTENDED. T/S PER TAFI 2SDR 04FDEA02685Proximity Switch · inoperativeAFTER TAKEOFF, ALL GEAR INDICATIONS REMAINED UNSAFE AFTER GEAR HANDLE WAS RAISED AND CHECKED IN, BOTH FRONT AND BACK PANELS. FOLLOWED QRH, CYCLED THE GEAR AND ALL LIGHTS WENT OUT. CONTINUED FLIGHT. TROUBLESHOT IAW DC10 TAFI CHAPTER 32-30-00, FAULT CODE-AA. SDR 04FDEA02644Pan · gougedNR 2 ENGINE RT FAN COWL INTERIOR HAS RUBBING APPROXIMATELY 8 INCHES ABOVE CENTER U-BOLT. REMOVED CENTER U-BOLT FITTING TO FOM. REMOVED DAMAGED SECTION OF PAN IAW SRM 51-35-01, VOL II. WELD REPAIRD IAW EA 8-5410-81450. INSTALLED PAN IAW SRM 51-31-01 VOL II. SDR 04FDEA02538Floorbeam · corrodedAFT PIT, FLOORBEAM CAP BEAM AT STATION 1887.0 HAS EXFOLIATION. REMOVED FLOORBEAM IAW SRM 51-33-01 VOL II. INSTALLED NEW FLOORBEAM AGA 3849-15, (FABRICATED ON NON-ROUTINE N01875) IAW DWG AGA 3849 AND SRM 51-33-01 VOL II. REFERENCE NON-ROUTINE N01814.SDR 04FDEA02346Fitting · corrodedCORROSION AT THE INTERIOR OF AFT CARGO DOOR UPPER BOX AT LONGERON 27L FITTING AND SEVERAL HARDWARE, STA 1787 TO STA 1841, LONGERON 27L, LBL 101.0 TO LBL 106.0. REMOVED CORROSION, EXCEEDS LIMITS IAW DC10 SRM 53-00-01 VOL I, REMOVED AND REPLACED HEADER BEAM,SDR 04FDEA02347Fitting · crackedCRACKED FITTING, CENTER WING SECTION TO FUSELAGE SPLICE, STATION 1157, LEFT HAND SIDE AT LONGERON 37L, EXTERNAL FITTING. REMOVED DAMAGED FITTING IAW DC10 SRM 51-33-01 VOL II. NEW FITTING FABBED ON FEDEX CARD N00880. LOCATED AND DRILLED FITTING IAW DC10 SRM 51SDR 04FDEA02103Engine · stalledAT FL330, SELECTED ENGINE AND WING ANTI-ICE ON, ENGINE 3 ANTI-ICE DISAGREE AND COMPRESSOR STALL AT SAME TIME. N1 ROLLED BACK TO 67 PERCENT. RAN COMPRESSOR STALL CHECKLIST. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN APPROXIMATELY 1+05 FLIGHT TIME REMAINING (WINSDR 04FDEA01853Mount Bracket · wornCOMPLY WITH EA 8-7222-77876 POWER PLANT FAN SECTION ACCESSORY GEARBOX MOUNT BRACKET WEAR REPAIR. COMPLIED WITH EA 8-7222-77876 POWER PLANT FAN SECTION ACCESSORY GEARBOX MOUNT BRACKET AT MAE.SDR 04FDEA01493Fitting · corrodedCOMPLY WITH EA 8-5750-77424 WINGS LT IB FLAP-OB HINGE BRACKET SIDE BRACE REPAIR (P/N ARC0182-1) COMPLIED WITH EA 8-5750-77424 (WINGS-LT IB FLAP- OB HINGE BRACKET SIDE BRACE REPAIR (PN ARC 018 2-1) AT MAE.SDR 04FDEA01495Hinge Bracket · corrodedCOMPLY WITH EA 8-5740-77418 WINGS RT INBD FLAP, FWD HINGE ASSY PIVOT BORE CORROSION. COMPLIED WITH EA NR 8-5740-77418 WINGS-LT IB FLAP, FWD HINGE ASSY PIVOT BORE CORROSION, PART 1 ONLY. COMPLIED WITH AS STATED IN UPDATE.SDR 04FDEA01500Valve · faultyNR 2 ENGINE FAILURE WARNINGS APPEARED ON ECAM ON TAKEOFF AT 70 KTS. REJECTED TAKEOFF. TRIED ANOTHER TAKEOFF, SAME PROBLEM, REJECTED TAKEOFF AGAIN. NR 2 ENGINE WOULD NOT SHUT DOWN IN BLOCKS WITH FUEL LEVER. PULLED NR 2 FIRE HANDLE AND ENGINE WOULD NOT SHUT SDR 04FDEA01492Fitting · corrodedCOMPLY WITH EA 8-5750-77425 WINGS-LT IB FLAP, ROLLER FITTING ATTACH HOLES CORRODED AT MAE(PART 1 INTIAL IS COMPLIED WITH AND WILL REQUIRE A FOLLOW UP ACTION TO BE COMPLIED WITH. COMPLIED WITH AS STATED IN UPDATE.SDR 04FDEA01165Case · gougedCOMPLY WITH EA 8-7220-77402 ENGINE - GOUGES IN EXTERIOR OF NR 3 ENGINE AFT STATOR CASE. NO RESTRICTION NR 3 ENGINE AFT STATOR CASE HAS GOUGES, OK PER EA 8-7220-77402 IAW EA AFTER 50 FLIGHT CYCLES ACCOMPLISH AN INITIAL INSPECTION TO VERIFY THAT NO CRACKS EXISSDR 04FDEA00395Housing · gougedCOMPLY WITH EA 8-7260-75573. ENGINE DRAIN - TRANSFER GEARBOX HOUSING DAMAGE INTERIM REPAIR. COMPLIED WITH EA 8-7260-75573.SDR 03FDEA02244Case · splitDURING TO AT 300 FT, NR 3 EGT "X'ED" OUT. EAD SHOWED ENG NR 3 EXCEEDANCE. EGT X WENT AWAY AND SHOWED NORMAL EGT. EGT THEN SPIKED INTO THE RED SHOWING 1027 EGT. THROTTLE WAS RETARDED AND ALL INDICATIONS (N1, EGT, N2, AND FUEL FLOW) WERE NORMAL, NO OTHER INDISDR 04FDEA01496Skin Panel · crackedHORIZONTAL STABILIZER - LT UPPER AFT SKIN PANEL CRACKED. CRACKED PANEL PORTION REPLACEMENT IAW SB 55-18 IAW EA 8-5510-70172. (REF FEDEX NRC N1102) *S/D COMING*SDR 04FDEA01497Skin Panel · crackedHORIZ STABILIZER - LT UPPER AFT SKIN PANEL CRACKED. CRACKED PANEL PORTION REPLACEMENT IAW SB 55-18 IAW EA 8-5510-70172. (REF NRC N1102)SDR 03FDEA01804Hinge Bracket · corrodedNR S 9 COMPLY WITH EA8-5750-73194. WINGS-RT IB FLAP-OB HINGE BRACKET, CORROSION REPAIR P/N ARC0154-2. CLOSING ACTION ON 10/22/03. COMPLIED WITH EA 8-5750-73194.SDR 03FDEA01681Switch · inoperativeAIR CONDITIONING DOORS LIGHT ON S/O PANEL BEGAN FLICKERING INFLIGHT. FUEL WAS DUMPED AND LANDING ACCOMPLISHED AT SLC IAW RED TABS. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-04-04 CATEGORY: C EXPIRATION: 11OCT03, FACT 03OCT03 07:58 EWR R . REMOVED AND REPLASDR 03FDEA01459Case · gougedGOUGES IN EXTERIOR OF NR 2 FAN FRAME CASE. COMPLIED WITH E.A. 8-7220-72285 ENGINES-DISPOSITION OF GOUGES IN EXTERIOR OF NR 2 ENGINE FAN FRAME CASE.SDR 03FDEA01387Support · crackedCOMPLY WITH E.A. 8-7210-72270- ENGINE-BASIC- FAN STATOR SUPPORT HALF, CRACK REPAIR. ENGINE-BASIC FAN STATOR SUPPORT HALF CRACK REPAIR. CLOSED ON 08/25/2003 FEDEX .SDR 03FDEA01123Engine · malfunctionedNR 3 ENG HUNG DURING HIGH ALTITUDE SHUT DOWN. RELIGHT AND FAILED TO RECOVER DURING DESCENT RESULTING IN NR 3 ENG SHUT DOWN.SDR 03FDEA00780Engine · malfunctionedCRUISE ALT (FL370) ANC -- SEA 2+19 ENROUTE TIME "ENG NR 3 OIL PRESS LOW" ALERT. FOLLOWED APPROPRIATE CHECKLIST & LANDED AT DESTINATION. EMERGENCY DECLARED. FOUND ANGLE GEARBOX LOOSE ON HORIZONTAL SHAFT ANGLE GEARBOX CASE SEALS BLOWN, SEVERAL OIL LINES SHSDR 03FDEA00578Engine · flamed outNR 3 ENGINE OIL STRAINER CLOG LIGHT CAME ON AT FL 330. AS WE WERE ABOUT TO START THE RED TABS CHECK LIST FOR THIS PROBLEM NR 3 ENGINE FLAMED OUT. AT TIME OF FLAME OUT ALL ENGINE INDICATIONS WERE NORMAL. RED TABS COMPLETED. AIRCRAFT DIVERTED TO KDEN FOR PRESDR 03FDEA00390Door · gougedRT MLG DOOR AFT OUTBOARD PAN HAS 6 INCH LONG GOUGE. LONG GOUGE HAS CRACK, REMOVED CORNER PAN. RECEIVED NEW PAN DRILLED HOLES TREATED PRIMED AND PAINTED AND INSTALLED IAW SRM 52-10-00, 51-35-01,51-35-02,51-31-01 AND 51-21-01.SDR 03FDEA00389Pylon · damagedNR 1 ENGINE PYLON RIGHT SIDE CLOSE OUT ON LOWER WING BROKEN ABOVE PANEL 437ER. CLOSING ACTION ON 04/05/03. ON NR N00313. REMOVED CLOSE-OUT PANEL ROUTED TO FAB IAW SRM 51-31-01. T/R NR T2/322652 AND 1 PANEL ON T2/322695, LOCATED AND DRILLED IAW SRM 51-31-0SDR 03FDEA00388Seal · bentNR 662 NR 3 PYLON PANEL 488CR RAIN SEALS (2) EA BENT AND TORN. CLOSING ACTION ON 04/05/03. REMOVED 2EA RAIN SEALS ON NR 3 PYLON PANEL 488CR, IAW SRM 51-31-01. FAB NEW RAIN SEALS ON TRAVELER NR T2/324415. DRILLED DEBURED IAW SRM 51-31-01. INSTALLED RAIN
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