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 = 'CF348C1' 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 = 'CF348C1' 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 ASOA201001393Floorbeam · corrodedFS 280.00 RT CROSSBEAM CORRODED. REMOVED RT FS280.00 FLOORBEAM IAW SRM 51-42-06 AND SRM 51-42-13. LOCATED AND DRILLED RT FS280 FLOORBEAM IAW SRM 51-24-36-001-001-A01 & 51-40-11-001-001-A01. INSTALLED RT FS 280.00 FLOORBEAM IAW SRM 51-42-06-001-001-A01 AND SSDR ASOA201001394Floorbeam · corrodedFS 280.00 COCKPIT FLOORBEAM CORRODED. REMOVED FS280 COCKPIT FLOORBEAM ANGLE REF SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND SRM 51-42-22-001-001-A01. INSTALLED NEW FS280 COCKPIT FLOORBEAM ANGLE REF SRM 51-42-06.SDR SWIA201024922Lamp · burned outEMERGENCY EXIT ROW LOWER LIGHT (12 C/D) INOPERATIVE. RELAMPED.SDR ASOA201001350Seat Track · corrodedSEAT TRACK 9R AT FS364 TO FS 485 CORRODED OUT OF LIMITS AND NEEDS TO BE REPLACED. SEAT TRACK 9R REMOVED IAW AMM 53-00-49-000-80. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.SDR ASOA201001398Frame · crackedLEFT AFT BELLY FAIRING 195DL AFT FRAME IS CRACKED AND HAS CHAFING DAMAGE. R & R C-CHANNEL FOR LT AFT BELLY FAIRING 195DL IAW SRM 51-41-02-001-001-A01 (PN CC670-39171-1) COMPLY WITH MODSUM IS670538200021. COMPLIED WITH EC/TC MOD SUM IS670538200021 AND MET ALLSDR QXEA2010091400535Angle · corrodedC-CHECK, THE PASSENGER DOOR SURROUND STRUCTURE MID CAP ANGLE HAS CORROSION AT FS 310 TO 349 AT WL 72. REMOVED MID CAP ANGLE TO ACCESS CORROSION AREAS. BLENDED CORROSION ON THE ANGLE AND FOUND SEVERAL AREAS OF .030 DEEP BLENDS AND ONE AREA WITH A BLEND OF 0.5SDR QXEA2010090900530Skin · damagedC-CHECK - LT MLG DOOR HAS 10 LOOSE RIVETS IN THE OUTER SKIN. REMOVED LT MLG DOOR IAWAMM 32-12-01-000-801. REMOVED 10 RIVETS IAW SRM 51-42-06-001-001-A01 AND INSTALLED NEW RIVETS IAW SRM 51-42-06-001-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-SDR QXEA2010090900531Skin · damagedC-CHECK - RT MLG DOOR HAS 5 LOOSE RIVET IN OUTER SKIN. REMOVED RT MLG DOOR IAW AMM 32-12-01-000-801. REMOVED 5 RIVETS IAW SRM 51-42-06-001-001-A01 AND INSTALLED NEW RIVETS IAW SRM 51-42-06-001-001-A01. TREATED, PRIMED AND PAINTED IAW SRM 51-21-11-001-001-A0SDR QXEA2010090900525Fitting · chafedC CHECK - LT MLG SIDE STAY FITTING HAS SMALL CHAFE. BLENDED OUT CHAFE IAW REO 670-57-11-043. BLENDED AREA IS .050" BY .050" CORNER BLEND 1.00" LENGTH. PERFORMED ECI ON LT SIDE STAY FITTING BLEND AREA. NO CRACKS NOTED AT THIS TIME, IAW NDTM ECI 51-20-006-250SDR QXEA2010090900526Seat Track · corrodedC-CHECK - RT SIDEWALL SEAT TRACK FS379-FS469 HAS CORROSION AND CHAFED. BLENDED AREAS OF CORROSION IAW SRM 51-12-00-001-001-A01 AND 51-21-06-001-001-A01. SEAT TRACK FOUND TO BE BEYOND LIMITS IAW REO 670-53-00-013. REMOVED SIDE SEAT TRACK IAW AMM 53-00-49-000SDR SIMA201025004Engine · vibrationON FLIGHT 3703 THE CREW REPORTED THAT DURING CRUISE THE LEFT ENGINE NR 1 VIBRATIONS WERE HIGH. THE CREW FOLLOWED THE AIRCRAFT OPERATION AS MANUAL PROCEDURE AND COULD NOT MAINTAIN ALTITUDE WITH THRUST SETTING. THE CAPTAIN DECLARED AN EMERGENCY AND DIVERTED TOSDR ASOA201001280Door · out of adjustLT OVERWING EMERGENCY EXIT DOOR HARD TO OPEN. ADJUSTED BOTH SHOOT BOLTS ON LT OVERWING EMERGENCY EXIT DOOR. OPS CHECK GOOD IAW AMM TASK 52-21-00-820-801.SDR SWIA201024840Engine · flamed outRIGHT ENGINE ITT EXCEEDED, FOLLOWED BY RIGHT ENGINE FLAMEOUT. (FLT 6828) REMOVED AND REPLACED THE RIGHT ENGINE ASSEMBLY PER AMM.SDR QXEA2010090100501Paint · chafedC-CHECK - LT WING SLATS NR1 & 2 SHOW EVIDENCE OF CHAFING. BLENDED AREA FOUND TO BE PAINT ONLY, WITH NO MATERIAL LOSS ON LOWER T/E SKIN, WITHIN LIMITS OF SRM 57-42-01-101-001-A01. CHAFED AREA FOUND ON WING L/E (UNDER AREA OF SLAT) BLENDED AREA IAW SRM 51-12-0SDR QXEA2010090100502Skin · gougedC-CHECK - GOUGE ON INBD FLAP AT TOP CTR OF FLAP BY L/E. BLENDED ON GOUGE ON UPPER SKIN OF RT INBD FLAP LOCATED BETWEEN 2 RIVETS AT FLS 84.20 IAW SRM 51-12-00-001-001-A01. SCRATCH MEASURES 0.5"L X .050W X .0025"D. GOUGE IS WITHIN LIMITS OF SRM 57-52-01-101-SDR QXEA2010090100503Structure · damagedC -CHECK - FWD BAG BAY DOOR FWD/AFT CORNERS OF INNER SKIN, INBD DAMAGED. REMOVED EDGE DAMAGE FROM FWD/AFT CORNERS OF INNER SKIN ON FWD BAGGAGE BAY DOOR. BLENDED DAMAGE IAW SRM 51-12-00-001-001-A01 AND FOUND TO BE IN LIMITS IAW SRM 53-00-00-101-001-A01. TREATSDR ASOA201001101Seat Track · corrodedLT SIDE WALL SEAT TRACK AT FS 797.00 TO 813.70 CORRODED. REMOVED CORROSION FROM SEAT TRACK BETWEEN FS 797.00 AND 813.70 ON LT SIDE WALL ALL WORK DONE IAW SRM 51-12-00-101-001-A01. SEAT TRACK FOUND TO BE IN SERVICEABLE LIMITS PER SRM 53-41-49-101-001-A01. ALOSDR ASOA201001097Strake · crackedAFT DORSAL STAKE FOUND WITH 1" CRACK DEFECT MARKED WITH RED TAPE. REPAIRED CRACK AT AFT DORSAL STRAKE IAW SRM 51-75-16-001-A01. REPAIR OF AFT DORSAL FULLY CURED IAW SRM 51-75-16-001-A01. PRIMED AND PAINTED IAW SRM 51-25-01-001-A01.SDR MASA2010080800856Engine · vibrationENG VIBE NR 2 ENG IN FLT. MX COMPLIED WITH TEMP RO.SDR QXEA2010081200481Fan · failedDISPLAY COOL CAUTION AFTER T/O, RETURN TO FIELD. LANDING UNEVENTFUL. REPLACED NR 1 DISPLAY SUPPLY FAN AND CHECK VALVE IAW AMM TASKS 21-24-12-000-801 & 21-24-12-400-801, OPS CHECK GOOD. RETURNED TO SERVICE.SDR QXEA2010071500413Cowling · chafedC CHECK - RT ENGINE UPPER FAN COWL CHAFE UNDER T/R TRANSMISSION FLEX LINE. BLENDED CHAFED AREAS ON FAN COWL SKIN AND REINFORCING ANGLE. SENT TO MFG FOR ENGINEERING. PERFORMED ECI ON RT ENGINE UPPER FAN COWL REINFORCING ANGLE WHERE AREA WAS BLENDED. NO CRACKSDR QXEA2010070800384Seat Track · corrodedC-CHECK - RT SIDE SEAT TRACK HAS CORROSION BETWEEN FS 677-708. BLENDED CORROSION ON RT SIDE SEAT TRACK, ORIGINAL THICKNESS .260. REMOVED .042 MAX ALLOWABLE IS .035, REMAINING MATERIAL IS .218. BLEND IS OUT OF LIMITS IAW REO 670-53-00-013. R & R RT SIDE SEASDR QXEA2010070800385Seat Track · corrodedC-CHECK - RT FLOOR SEAT TRACK HAS CORROSION NEAR FASTENER COUNTERSINK BETWEEN FS 485-581. BLENDED CORROSION ON RT FLOOR SEAT TRACK, ORIGINAL THICKNESS .110, REMOVED .038, MAX ALLOWABLE IS .035, REMAINING MATERIAL IS .072. BLEND IS OUT OF LIMITS IAW REO 670-5SDR ASOA201001088Dimmer · failedF/A REPORTS A POPPING SOUND FOLLOWED BY A FAINT ELECTICAL SMELL STRONGEST AT THE TOP OF FIRST CLASS CABIN. R & R DIMMER PS49 IAW AMM 33-21-03. OPS CK GOOD. ACFT OK FOR SERVICE. (CLOSED)SDR ASOA201000977Flashlight · inoperativeF/A REPORT FWD F/A STATION FLASHLIGHT NOT ILLUMINATING WHEN SELECTED ON. REPLACED FLASH LIGHT IAW AMM 25-00-00. (CLOSED)SDR CA100707010Connector · looseCREW REPORTED A LOUD BANG IN THE CABIN UPON LANDING & EICAS OXYGEN PRESSURE INDICATION DASHED. THE CIRCUIT BREAKER CBP2-P11 WAS FOUND POPPET OUT. TECHNICIAN INSPECTED THE AVIONICS BAY AND FOUND THE PRESSURE TRANSDUCER EXPLODED (SEE ATTACHED PICTURES THE WIRINGSDR ASOA201000933Floor Support · crackedFLOOR PANEL 221ALF LT SUPPORT ANGLE CRACKED. REMOVED LT FLOOR SUPPORT ANGLE FOR FLOOR PANEL 221ALF IAW SRM 51-42-06-001-001-A01. NEW FLOOR SUPPORT ANGLE NEEDS TO BE INSTALLED. DRILLED NEW SERVICEABLE FLOOR SUPPORT ANGLE, INSTALLED CAM LOC RECEPTICALS IAW SRMSDR QXEA201006110043Floorbeam · corrodedC-CHECK-COCKPIT FLOOR SUPPORT ANGLE ATTACHING FWD SIDE OF FS280 BEAM IS CORRODED. BLENDED .005" MATERIAL FROM ANGLE, ORIGINAL THICKNESS IS .063', MATERIAL REMAINING IS .058". BLEND IS WITHIN LIMITS IAW SRM 53-21-43-001-A01 PG 103. TREATED AND PRIMED IAW SRMSDR QXEA2010061100339Floor Support · corrodedC-CHECK FOUND CORROSION ON FLOOR ANGLE UNDER PANEL 141 ALF AT FS 280. BLENDED CORROSION FROM LOWER ANGLE FOR PANEL 141ALF. BLENDED .005 MATERIAL FROM ANGLE. ORIGINAL THICKNESS OF ANGLE IS .063, .058 MATERIAL REMAINING. BLEND IS WITHIN LIMITS IAW CSRM TASSDR ASOA201000878Fitting · crackedWHILE PERFORMING THE EDDY CURRENT OF THE RT BULKHEAD BATHTUB FITTING RECEIVED A RELAVANT CRACK INDICATION AROUND THE RETURN LINE OPENING. FINISHED DRILLING AND FINAL SIZED ALL FASTENER HOLES. APPLIED PRIMER & WET INSTALLED NEW FITTING. ABOVE WORK DONE REF SDR ASOA201000884Angle · crackedSUPPORT ANGLE LT SIDE FOR COCKPIT PANEL 221ALF CRACKED. BEGAN REMOVING FASTENERS ON LT SIDE FLOOR SUPPORT ANGLE FOR COCKPIT PANEL 221ALF. IAW SRM 51-42-06-001-001-A01. R & R LT SIDE COCKPIT FLOOR SUPPORT ANGLE WITH SERVICEABLE PART ALL WORK DONE IAW SRM 51SDR ASOA201000871Unknown · odorF/A REPORTED ELECTRIC SMOKE TYPE ODOR IN THE GALLEY AREA W/NO VISABLE INDICATIONS NOTED. CW GVI TO GALLEY OPERATED ALL GALLEY COMPONENTS/ LIGHTS NO DEFECTS NOTED IAW AMM 38-10-00, 33-26-00. (CLOSED)SDR ASOA201000872Floorbeam · corrodedBS 280 BEAM REQUIRES REPLACEMENT DUE TO CORROSION, REPAIRED. PRIMED AND PAINTED BARE AREAS AT CTR EATHING, INSTALLED NEW 280 CROSS BEAM IAW SRM 51-42-06, 51-42-20. 5. DRIP TRAYS AND FLOOR PANEL NUTPLATES REQUIRES INSTALLATION AND 280 BEAM NEEDS TO BE SEALED ASDR ASOA201000868Placard · deterioratedPAX DOOR OPEN AND EXIT PLACARD DETERIORATED. R & R RT MLG SIDE STAY ACTUATOR IAW AMM 32-32-01. OPS AND LEAK CK GOOD. (CLOSED)SDR ASOA201000860Seat Track · corrodedMAIN CABIN CORROSION ON RT INBD SEAT TRACK STA 349-364 AND 374 TO 379. RT INBD SEAT TRACKS AT FS 349-583 100 PERCENT MATERIAL LOSS. R & R 2 EA SEAT TRACK PN SH670-52159-1 & SH670-33426-1 IAW SRM 51-40-02R. (CLOSED)SDR ASOA201000861Lens · crackedMAIN CABIN G1 GALLEY- EMERGENCY LIGHT LENS CRACKED. R & R LIGHT LENS ASSY IAW AMM 33-51-05.SDR ASOA201000862Lens · crackedFWD GALLEY AREA FWD F/A PANEL EMERGENCY LIGHT LENS CRACKED. R & R FWD GALLEY AREA FWD F/A PANEL EMERGENCY LIGHT ASSY IAW MM 33-51-05. OPS CHECK GOOD IAW MM 33-51-05.SDR ASOA201000863Connector · disconnectedMAIN CABIN- SEAT ROW 11 CEILING PANEL, EMERGENCY LIGHT INOP. REINSTALLED LOOSE CONNECTOR AND OPS CHECKED OK IAW AMM 33-51-09.SDR ASOA201000850Power Supply · inoperativeFOUND NUMEROUS EMERGENCY LIGHTS INOP INCLUDING LIGHT FWD OF SERVICE DOOR AND UPPER EMER LIGHT AT PAX DOOR SUSPECT BAD BATTERY PACK. R & R NR 1 EMERGENCY POWER SUPPLY UNIT CHARGER IAW AMM 33-51-17-000-801 AND AMM 33-51-17-400-801. OPS TEST GOOD IAW AMM 33-51-SDR QXEA2010052800310Door Frame · corrodedC CHECK - CORROSION FOUND ON INNER PAX DOOR LOWER FRAME UNDER REMOVED RESIN BETWEEN DOOR FRAME 327.7 - 338.9. REMOVED RIVETS TO ALLOW ACCESS IAW SRM 51-42-06-001-001-A01. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. DAMAGE FOUND TO BE WITHIN LIMITS IAW SDR ASOA201000798Seat Track · corrodedRT FLOOR INBD SEAT TRACK HAS CORROSION. REMOVED CORROSION ON RT INBD SEAT TRACK STA 485-549 IAW SRM 51-20-06 MAX MAT .035 REMOVED .040 FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED 3 EA TRACK RT INBD STA 485-549 IAW SRM 51-41-02. NEW SEAT TRACK POSH670SDR ASOA201000881Threshold · corrodedASD THRESHOLD CORRODED AT CTR JUST AFT OF DOOR HARNESS ADEL CLAMP. BLENDED ANGLE AT ASD THRESHOLD FOUND TO BE OUT OF LIMITS REF SRM 51-21-06-001-001, WA161715 6/4/10. RECEIVED & STARTED DRILLING NEW ANGLE AND INSTALLED NUT PLATES ON NEW ANGLE REF SRM 51-42-0SDR ASOA201000789Fuse · inoperativeMAIN CABIN INTERIOR AISLE EXIT SIGN AND EXIT LIGHTS INOP AT OVERWING EMERGENCY EXITS. REPLACED FUSE AT PL124 BATTERY PACK NR2 OPS CHECK GOOD IAW MM 33-51-17.SDR ASOA201000736Angle · corrodedMAIN CABIN-L1 DOOR THRESHOLD ANGLE HAS CORROSION. R & R ANGLE PART NR SH670-31825-7 IAW SRM 51-41-02 OPS CHECK GOOD IAW SRM MM 52-11-00.SDR ASOA201000711Seat Track · corrodedMAIN PASSENGER CABIN RT FLOOR SEAT TRACK STA 364 TO 549 HAS CORROSION. SEAT TRACK FOUND TO BE OUT OF LIMITS REMOVED SEAT TRACK RT STA 364 TO STA 485 RCVD NEW RT SEAT TRACK PN SHO670-32159-1, PO 30340005 AND INSTALLED RT SEAT TRACK IAW SRM 51-41-02. BLENDED RTSDR ASOA201000712Seat Track · corrodedMAIN PASSENGER CABIN RT SEAT TRACK STA 364 TO 549 HAS CORROSION. REMOVED CORROSION FROM FS 485-549 RT INBD SEAT TRACK IAW SRM 51-21-06 ORIGINAL MAT .150. REMOVED .031 REMOVING MAT .119 USING CAL A1-116272 DUE DATE 20JUL10 AND GAUGE NR H3708 DUE DATE 15JUN1SDR ASOA201000713Floorbeam · corrodedBS 280 BEAM LT AND RT SIDE BADLY CORRODED. COMPLIED WITH EC/TC SB 670BA-53-026 REV.B.SDR QXEA2010051700303Bpsu · failedUPON FLAPS 20 SELECTION DURING APPROACH, GOT A FLAPS FAIL CAUTION MESSAGE. PERFORMED CHECKLIST WITH NO CHANGE. FLT CTRL SYNOPITIC PAGE INDICATED L FLAPS AT 16 DEG AND NO INDICATION ( 2 DASHES )FOR RT FLAPS. SLATS INDICATED 20 DEG. DIVERTED AND LANDING WAS USDR QXEA2010051100300Servo · bindingON SHORT FINAL, AT 500 AGL, HARD RT UNCOMMANDED V ROLL REQUIRING PILOT TO OVER POWER WITH HIGH CONTROL PRESSURE. AILERON TRIM INDICATOR ALWAYS NEUTRAL. AUTOPILOT OFF AT THE TIME, ACFT BEING HAND FLOWN. LANDING UNEVENTFUL. PERFORMED GVI OF ROLL CONTROL SYS/CABSDR ASOA201000705Cover · brokenGALLEY NR 2 FLOOR LEVEL EMERGENCY FLOOD LIGHT COVER BROKE. R & R GALLEY NR 2 FLOOR LEVEL EMERGENCY FLOOD LIGHT COVER IAW AMM 33-51-11.
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