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 = 'CF650C2' 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 = 'CF650C2' 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 CA120504008Connector · sheared(CAN) IN CRUISE, CREW EXPERIENCED MULTIPLE POWER INTERRUPTIONS CAUSING, BUSS OFF. LIGHTS TO ILLUMINATE. CREW LANDED AT NEAREST SUITABLE AIRPORT WHERE MAINTENANCE DISCOVERED THE T1 TERMINAL ON THE NR 1 GENERATOR LOOSE. TERMINAL WAS RE-SECURED AND THE ACFT RETSDR CA130702005Acm · failed(CAN) NR 1 ACM COOLING TURBINE WHEEL SHAFT FAILED DURING GROUND RUNS, TURBINE EXITED ACFT THROUGH EXHAUST DOOR. THE ACM WAS REPLACED AND THE ACFT RETURNED TO SERVICE.SDR FDEA201202130567Engine · stalledON TAKEOFF ROLL AT APPROX 60 KTS LARGE COMPRESSOR STALL FROM 1 MOTOR WITH YAW AND LARGE VIBRATION. REJECTED TAKE-OFF. NR 1 SHOWED EGT EXCEEDANCE AND N1 WITH (X)- NO ROTATION. SHUTDOWN ENGINE, PULLED FIRE HANDLE. RETURNED TO RAMP. ENGINE REPLACED. DUE TSDR CA120211001Blocker Door · damaged(CAN) AFTER LANDING, CREW OBSERVED THE NR 3 REVERSER, UNLOCK AND PRESSURE, LIGHTS REMAINED ILLUMINATED. MAINTENANCE DISCOVERED THAT THE BLOCKER DOORS AND THE BRACKETS THAT ATTACH THE JACKSCREWS TO THE SLIDING PANEL HAD BECOME DAMAGED/BROKEN POSSIBLY DUE TO OSDR CNMA20110034Engine · failed2000 FT FROM LEVEL OFF NR1 ENGINE SHUTDOWN, EGT RED FLAG WITH NO N1 OR N2. PREFORMED QRH PROCEEDURE. METAL IN TAILPIPE & EXCESSIVE DAMAGE TO LPT. R & R NR1 ENG IAW WC 10UN-101. ACHIEVED ENG PARAMETERS IAW MM 71-00.SDR FDEA201105031709Warning Light · false activationAT 98 KTS GOT A NR 2 ENG EXCEEDANCE ALERT REJECT TAKEOFF. PERFORMED FAN (N1) OVERSPEED INSP, FAN BLADES MOTOR FREE FOR ROTATION FIRST STAGE FAN SHROUD WITHOUT RUB TRACES AND INLET AND EXHAUST NOZZLES FREE FROM PARTICLES IAW AMM 72-00-00-6-2. ACFT OK FOR SESDR FDEA201104261625Engine · malfunctionedON TAKEOFF ROLL. MAX POWER AT 90KIAS THE ENGINE FAIL LIGHT, ENGINE 2 N1 EXCEEDANCE 120.1 (T/O LIMIT 115.8) REJECTED T/O. PERFORMED FAN (N1) OVERSPEED INSP, FAN ROTOR FREE FOR ROTATION, FIRST STAGE FAN SHROUD WITHOUT RUB TRACES AND INLET AND EXHAUST NOZZLES FSDR FDEA201104021298Skin · corrodedRT FUSELAGE AT APPROX STA 1887, L47R HAS BULGING SKIN. REMOVED FASTENERS AND SPOT FACED 5 EA, 1 IN CIRCLE AREAS TO ACCESS CORROSION AREAS REF SRM 53-20-00 FIG 6, SH 5 CUT OUT CORROSION REF SRM 53-20-00, VOL 1. FABRICATED REPAIR FILLER REF SRM 53-20-00, VOL 1SDR FDEA201102120547Strap · malfunctionedUNABLE TO DEPLOY CAPTS LEFT SHOULDER STRAP. NO DEFECTS NOTED IAW MM 25-11-01-8-0. OK TO CONTINUE.SDR CNMA20110002Engine · failedNR 2 ENG SHUTDOWN DURING CLIMB ACCOMPLISHED QRH PROCEDURE. REPLACED NR 2 ENGINE PER CARD 10UN-201 OPS CHECK NORMAL LEAK CHECKED OK POWER ASSURANCE OK.SDR CA110209015Sensor · misriggedAFTER DEPARTURE THE LANDING GEAR WOULD NOT RETRACT NORMALLY, HAD TO USE THE OVERRIDE. LANDING GEAR ANTI-RETRACTION PUSH/PULL CABLES ADJUSTED IAW AMM 32-31-01 AND LANDING GEAR GND SENSE CONTROL MECH ADJUATED IAW AMM 32-24-01. LANDING GEAR GND SENSE CONTROL ADJSDR FDEA201101080076Engine · bird ingestionMULTIPLE BIRD STRIKES, FRONT WINDSCREEN AND NR 3 ENGINE. MODERATE VIBRATION, DECLARED AN EMERGENCY, COMPLIED WITH QRH, DIVERTED. (DEPARTED 16R BIRD STRIKE AT 2,500 FT MSL) FIRED BOTH BOTTLES INTO NR 3 ENGINE. LOST "B" LOOPS.SDR CNMA20100035Strainer · cloggedENG 3 OIL STRAINER CLOG LIGHT ILLUMINATED STEADY IN FLIGHT, ACCOMPLISHED QRH PROCEDURE NR3 ENGINE SHUTDOWN. C/A: REPLACED ENGINE.SDR CNMA20100036Scavenge Pump · leakingNR 3 ENG OIL QTY WENT TO ZERO IN FLIGHT, VERIFIED BY LOSS OF OIL PRESS & LOW OIL PRESS LIGHT. TROUBLESHOT DOWN TO NR 3 ENGINE OIL LUBE AND SCAVENGE PUMP ASSY. R & R PUMP ASSY IAW MM 79-20-04, SERVICED 25 QTS OF OIL IN ENGINE LEAK CKS AND OPS CKS GOOD.SDR FDEA201012214733Bleed Valve · overheatedBLEED AIR 1, HI TEMP LEVEL 3, ALERT. REPLACED NR 1 ENG FAN VALVE IAW MM36-13-04-4 AND RAN ENG NO FAULTS FOUND.SDR FDEA201012204719Switch · looseDURING TAXI OUT, TURNED OFF NOSE LIGHT AND FLASH OF LIGHT AND LOUD POP WAS HEARD COMING FROM NOSE LIGHT SWITCH. OBSERVED RT NOSE LIGHT CB POPPED. RETURNED TO GATE. FOUND NOSE LIGHT SWITCH LOOSE. TIGHTEN NOSE GEAR TAXI LIGHT SW AND OPS NORMAL REF SWP, CHAP SDR FDEA201012084621Fire Warning · false activationDURING POWER UP/START OF APU, GOT FLASHING "AGENT DISCH" SW; NO LEVEL 3 CARGO FIRE ALERT, BUT CARGO DOOR (LOWER FWD) WAS CLOSED ALREADY AND COULD NOT BE INSPECTED UNTIL OPEN. PUSHED AGENT DISCHARGE SWITCH FOR LOWER FWD CARGO, BUT ON RETURN TO COCKPIT, HASDR FDEA201010134033Warning Light · illuminatedDURING PREFLIGHT ACTVITIES STARTED APU. AFTER APU START AND WAITING FOR ELECTRICAL SWITCH OVER, GOT A LEVEL 3 CARGO FIRE LWR1 ALERT. FOLLOWED QRH AND DISCHARGED FIRE BOTTLE (FLASHING DISCHARGE SWITCH). REMOVED AND INSTALLED LOWER CARGO COMPTMENT FIRE EXTINSDR 2010FA0001115Frame · damagedDURING SHOP VISIT, SUBJECT ENGINE EXHIBITED SEVERE TURBINE MID FRAME LINER CLOCKING, DESPITE SUCCESSFULLY PASSING ON WING INSPECTION APPROX 70 CYCLES PAST. MAINTENANCE ORGANIZATION PERFORMING INSPECTION USED BOROSCOPE, AND REPORTED NIL FINDINGS.SDR FDEA201009053299Cylinder · inoperativeCTR LANDING GEAR FAIL TO DEPLOY USING ALTERNATE EXTENSION CABLE. BOTH NORMAL AND CONFIG LANDIG GEAR IN DICATION SHOW CTR LANDING GEAR RED. JACKED AND DOWNJACKED ACFT, DISCONNECTED AND RECONNECTED FWD CENTERLINE GEAR DOORS FROM STRUT, FOUND MAIN GEAR INTERLOSDR FDEA201009013230Frame · damagedMAIN CABIN INTERIOR LINER ATTACH BRACKET HAS A FASTENER THRU THE RADIUS OF FRAME 1159; BETWEEN STRINGER 11R - STRINGER 12R. COMPLIED WITH EA 8-5310-136699.SDR FDEA201008273166Floor Panel · damagedMCC FLOOR PANEL NR 357 GC IS BROKEN. FABRICATED NEW FLOORBOARD IAW DWG SRZ 25-005, REV "H".SDR FDEA201008253131Floor Panel · crackedMCC FLOOR PANEL FROM STA 1259-1299, RBL 70-107 IS CRACKED AND DELAMINATED. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV "H".SDR FDEA201008233108Seat Track · wornMAIN CABIN SEAT TRACK SCALLOPS ARE WORN AT BS 1623; LBL 48. REMOVED DAMAGED SECTION OF SEAT TRACK AND INSTALLED NEW SECTION IAW SRM 53-70-00, FIG 1, SHEET 2, VOL I. ALODINED AND PRIMED NEW SECTION IAW SRM 51-21-01, VOL II. FABBED AND INSTALLED SPLICE SECTIONSDR FDEA201008193050Skin · damagedFOUND A REPAIR DOUBLER ON THE R/W TIP UPPER SURFACE ON THE INBD END OF THE SPLICE STRAP THAT REQUIRES A MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED WING TIP IAW SRM 51-31-01, VOL II. REMOVED AND REPLACED TESDR FDEA201008183038Motor · failedL-1 DOOR DOES NOT OPEN WHEN PNEUMATIC EMERGENCY OPS CHECK IS PERFORMED. REMOVED AND REPLACED L-1 DOOR AIR MOTOR IAW AMM 52-11-02-2. PERFORMED AIR MOTOR FUNCTIONAL CHECK IAW AMM 52-10-01/201.SDR FDEA201008173017Floor Panel · delaminatedTAIL CONE LT UPPER WORK PLATFORM ACCESS DOOR FLOOR PANEL IS DELAMINATED. CRACKED AND MISSING EDGE MATERIAL. FABRICATED NEW TAIL CONE ACCESS FLOOR PANEL IAW DWG SRZ 25-005, REV "H". REMOVED AND INSTALLED ACCESS FLOOR PANEL IAW SRM 51-31-01, VOL II.SDR FDEA201008122964Angle · corrodedLOWER CTR CARGO PIT CLOSEOUT ANGLE HAS CORROSION AT STA 1781; RBL 36-56. REMOVED CORROSION. ORIGINAL THICKNESS 0.063. REMAINING THICKNESS 0.033. 0.030 REMOVED - OUT OF LIMITS PER SRM 53-00-01, FIG 1-B, VOL I. LOCATED, DRILLED, DEBURRED AND COUNTERSUNKSDR FDEA201008122961Seat Track · wornMAIN CABIN SEAT TRACK SCALLOPS ARE WORN AT BS 1059; LBL 48. CHECKED SEAT TRACK AT BS 1059, LBL 48 AND FOUND OUT OF LIMITS IAW SRM 35-70-00, FIG 5 GENERAL NOTE 7. REPAIRED AREA IAW SRM 53-70-00, FIG 1, VOL I.SDR FDEA201008112929Skin · scratchedFUSELAGE EXTERNAL SKIN HAS A SERIES OF SCRATCHES FROM FS 465-FS 535; LONGERON 26L - LONGERON 27L. COMPLIED WITH EA 8-5330-123553.SDR FDEA201008112940Hinge · corrodedCTR CARGO DOOR HINGE INNER SURFACE HAS RUST. FOUND 4 HINGE SEGMENTS OUT OF LIMITS ON DOOR IAW SRM 52-10-00, FIG 8, VOL I. R & R HINGE SEGMENTS IAW SRM 51-33-01, VOL II AND DWG ACA0012, REV "M". BLENDED CORROSION IAW SRM 51-21-01, VOL II. R & R CTR CARGO DOSDR FDEA201008112919Engine · inoperativeMANUAL FUEL/PUMPS ON HAD PROBLEM STARTING NR2. 1ST ATTEMPT-ENGINE ROLLED BACK AFTER 40 PERCENT, N1. SECOND ATTEMPT SLOW BUT STARTED OK. CHECKED POWER SEVERAL TIMES ON TAXI-ALL OK. PASSING 19K ENG 2 FLAMED OUT. RAN CHECKLIST,RECYCLED PUMP SWITCHES, RESTARTESDR FDEA201008102906Former · chafedNR 1 PYLON, PANEL 437EL, AFT SUPPORT HAS FRETTED AREAS. REMOVED DAMAGED STIFFENER AND DOUBLER IAW SRM 51-31-01, VOL II. RECEIVED NEW STIFFENER, PO 689690.1 AND FABRICATED NEW DOUBLER IAW DWG AUB7070, REV "F". ALODINED AND PRIMED IAW SRM 51- 21-01, VOL II. SDR WRLA20100810431Slide Raft · deployedL 1 DOOR SLIDE WAS FOUND TO BE PARTIALLY DEPLOYED WHILE STILL ATTACHED TO THE DOOR. THE GIRT BAR WAS NOT ENGAGED. THE DOOR ASSIST BOTTLE WAS FULL. THE SLIDE/RAFT BOTTLE WAS FULLY DISCHARGED. THE SLIDE SHROUD WAS DAMAGED. NO EVIDENCE OF DAMAGE TO THE DOOR SDR FDEA201008092877Support Bracket · gougedLT WING, NR 2 SPOILER, INBD SUPPORT BRACKET IS GOUGED BY THE FLAP. REPAIRED GOUGED SUPPORT BRACKET IAW EA 8-5740-136702,SDR FDEA201008092883Beam · crackedLT OVERWING DOOR HAS A CRACKED UPPER BEAM PN ADA 0006-1. LT OVERWING DOOR IS BEING REPLACED ON N/R N01074. NO FURTHER MX REQUIRED ON THIS N/R.SDR FDEA201008092878Skin · delaminatedRT WING, OTBD AILERON, LOWER SKIN, FWD L/E IS DELAMINATED. TRIMMED OUT DELAMINATED EDGE IAW SRM 57-00-01, FIG 1A, VOL I. CHECKED EDGE BLENDOUT AND MAINTAINED 2D FROM ALL ATTACH FASTENERS IAW SRM 57-00-01, FIG 1A, SHEET 1, VOL I. ALODINED AND PRIMED IAW SRSDR FDEA201008062852Case · chafedNR 3 ENGINE OTBD SIDE, A CONNECTOR BACK SHELL IS CHAFING THE STRUCTURE AT 1:00 O'CLOCK POSITION. REPAIRED CHAFED AREA IAW EM 72-23-01, REPAIR 001. RESTORED AREA IAW EM 72-23-01, REPAIR 001.SDR FDEA201008062863Spar · damagedNR 3 PYLON UPPER SPAR AT THE AFT BULKHEAD HAS (4 EA) BOLTS SPINNING (NR 5,6,7 & 9) GOING INBD TO OTBD. R & R 1 EA FASTENER AT ACCESSIBLE LOCATION IAW DWG AUB 7025, REV "AZ". R & R NUTS AT 3 EA TRAPPED FASTENERS IAW EA 8-5450-136697.SDR FDEA201008062864Fastener · looseNR 1 PYLON INTERIOR UPPER SPAR FASTENERS ARE LOOSE BELOW THE AFT PYLON SUPPORT LUG. (18 PLACES) R & R FASTENERS AT ACCESSIBLE LOCATION IAW DAC DWG AUB 7025, REV "AZ". R & R NUTS AT 2 EA TRAPPED FASTENERS IAW EA 8-5450-136697.SDR FDEA201008052839Floor Panel · crackedCENTER CARGO COMPARTMENT FLOOR PANEL 183 MF HAS A MISSING INSERT AND PANEL IS CRACKED. FABBED NEW FLOOR PANEL 183 MF IAW IAW DWG SRZ 25-005, REV "H".SDR WRLA20100621395Web · crackedWHILE IN ATL DURING A-5 CHECK A SPECIAL INSPECTION (SI) WAS PERFORMED ON THE NR 3 PYLON AND THE UPPER WEB WAS FOUND CRACKED AT THE CORNER OF THE GENERATOR FEEDER CABLE PASS THROUGH CUTOUT LOCATED AT YUS 338. FOUND BY ATLANTA INSPECTOR. PERMANENT REPAIR MADE SDR WRLA20100422353Fitting · corrodedREF DELTA N/R 93 CENTER LINE LANDING GEAR LT ATTACH FITTING CENTER BORE PITTED IN FITTING. REWORK CTR LANDING GEAR LT TRUNNION FITTING IAW DELTA ERA 481717-14.SDR FDEA201004131170Panel · delaminatedRT WING UPPER SURFACE T/E. REMOVING WING PANEL ARC0340-504 WITH N00458. FOUND DELAMINATION ON AFT EDGE. (REMOVED PART). REPAIRED DELAMINATION IAW SRM 51-71-00 PAR.16 VOL.2SDR FDEA201004061086Stringer · corrodedCTR CARGO BILGE AREA BETWEEN BS1701-1721 AND STRINGER 48R. STRINGER HAS EXFOLIATION CORROSION. R & R STRINGER SPLICE IAW SRM 51-31-01. STRINGER SPLICE FABRICATED ON TRAVELER T10/825356. CLASSIFIED AS MAJOR REPAIR.SDR 22AA201000067AControl Cable · brokenACFT ROLLS WHEN SPEED BRAKE IS EXTENDED. DIFFERENCE SHOWS ON SPI. DURING INSP FOUND RT/LT INBD AILERONS OUT OF RIGGING. ALSO ON PRE/FLT FOUND LT WING GROUND SPOILERS NOT DEPLOYING FULLY & SPOILER HANDLE NOT RETRACTING AUTOMATICALLY. ALSO SPOILER PANEL 1 & 2 NOSDR FDEA201003130808Fairing · chafedRT WING FIXED L/E FAIRING LOWER SURFACE HAS CHAFED MARK AT INBD FAIRING TO NR 3 PYLON. REPAIRED RT WING FIXED L/E FAIRING LOWER SURFACE IAW SRM 57-10-00 AND SRM 51-31-01, REPAIR CLASSIFIED AS MAJOR.SDR FDEA201003020593Skin · corrodedRT WING OTBD AILERON SKIN LOWER SURFACE HAS CORROSION. R & R RT OTBD AILERON IAW AMM 27-10-02-4. OP CHECKED AILERON IAW AMM 27-10-02-4. OPS CHECK GOOD.SDR FDEA201003020594Skin · corrodedLT WING OTBD AILERON LOWER SURFACE HAS FASTENERS UNDER PAINT PULLING THROUGH SKIN AND CORROSION FORMING UNDER PAINT. R & R LT OTBD AILERON IAW AMM 27-10-02-4. OPS CHECKED AILERON IAW AMM 27-10-02-4. OPS CHECK GOOD.SDR 22AA201000049Longeron · crackedDURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND CRACK. NON-ROUTINE NR 0123, CRACK AREA AT NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIR IAW EN 1016-10 AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.
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