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 99UAL900087Tube · leakingSLIDE/RAFT FAILED AIR RETENTION TEST DUE TO SEAM SEPARATION IN TUBE ASSEMBLY. *S/D* SEAM SEPARATION IN INFLATABLE TUBE ASSEMBLY. UNIT IS BEYOND ECONOMICAL REPAIR AND WAS SCRAPPED.SDR HALA9900039Engine · failedHNL - FLT 21 - (LOG PAGE NR 4821636). DURING CRUISE, NR 1 ENGINE EXHIBITED CHARACTERISTICS OF COMPRESSOR STALLS. (RAISING EGT, AUDIBLE RUMBLES, AND N2 DECREASING). COMPLETED APPROPRIATE CHECKLIST AND SHUT DOWN ENGINE. (X)SDR 99UAL900070Light · inopEEL LIGHTING INOP AT MID LT LAV. REPLACED EEL LIGHT ASSEMBLY, OPS CHECK OK.SDR 99UAL900088Tube · leakingSLIDE/RAFT FAILED AIR RETENTION TEST DUE TO SEAM SEPARATION IN TUBE ASSEMBLY. *S/D* SEAM SEPARATION IN INFLATABLE TUBE ASSEMBLY. UNIT IS BEYOND ECONOMICAL REPAIR AND WAS SCRAPPED.SDR 99UAL900090Tube · leakingSLIDE/RAFT FAILED AIR RETENTION TEST DUE TO SEAM SEPARATION IN TUBE ASSEMBLY. *S/D* SEAM SEPARATION IN INFLATABLE TUBE ASSEMBLY. UNIT IS BEYOND ECONOMICAL REPAIR AND WAS SCRAPPED.SDR 99UAL900019Light · inopEEL STRIP LIGHTS INOP RIGHT SIDE IN FIRST CLASS SECTION. REPLACED EEL LIGHT STRIP SECTION.SDR 99UAL900003Coalescer · contaminatedSTRONG ODOR, POSSIBLY OF TURBINE OIL AFTER CLIMBOUT AND DESCENT. *S/D* ENG/APU OIL USAGE IS LOW, AND NO HYD FLUID LEAK OR FUEL LEAK WRITE-UPS. COALESCER BAGS REPLACED. OK ON SUBSEQUENT FLIGHTS.SDR 98UAL900600Wire · brokenEEL STRIP LIGHTING WIRE BROKEN AT DOOR 3R. EEL LIGHTS INOP AT DOOR 3 CROSS AISLE AND LAST HALF OF ZONE 3 ON RIGHT SIDE. REPLACED CABLE, BATTERY PACK, AND LEAD ASSEMBLY FOR 3R. ALL OPS CHECK GOOD.SDR 98UAL900592Retract Mech · malfunctionedTERRIFIC VIBRATION IN NOSE AREA AFTER GEAR RETRACTION. RETURNED TO SEA. *S/D* NOSE LANDING GEAR FORWARD DOORS WERE FOUND OPEN UPON ARRIVAL. ALL HINGE POINTS AND LINKS WERE CHECKED. NO DEFECT WAS FOUND. MANUALLY CLOSED AND LOCKED DOORS. NO FURTHER REPORTSDR 98UAL900573Line · leakingODOR IN CABIN AROUND DOOR 3 AREA ON TAKEOFF, CLIMB AND INTERMITTENTLY IN CRUISE. SMELLS LIKE HOT OIL. REPAIRED HYDRAULIC LEAK NEAR APU INLET, BURNED OUT ALL 3 PACKS. REPLACED ALL 3 COALESCER BAGS. THERE HAVE BEEN NO REOCCURANCES.SDR 98UAL900574Battery Pack · dischargedC ZONE EEL LIGHTS INOPERABLE ALONG BOTH AISLES. FOUND BATTERY PACKS DISCHARGED. REPLACED BATTERY PACKS AND CHECKS OKAY.SDR 98UAL900580Light · miswiredEEL LIGHTS INOP. NO POWER FROM OVERWING AND AFT CABIN BATTERY PACKS IN C ZONE. *S/D* FOUND WIRE L2712 K10 CONNECTED TO TERMINAL A1 OF R2-178. CONNECTED SAME WIRE TO R2-178 TERMINAL A3.SDR 98UAL900503Air Dist · odorENTIRE AIRPLANE HAS ODOR WHILE ON GROUND AND IN FLIGHT. PASSENGERS COMPLAINED OF OILY ODOR.SDR 98UAL900480Wire · failedEEL LIGHT STRIP OUT AT 1EF THROUGH DOOR 2R, 9AB THROUGH 16AB AND 30HJ THROUGH 38HJ. SPLICED NEW RIBBON BY BULKHEAD 1R, 2L AND REPLACED LEADER CABLE ASSY, CHECKS OK.SDR 98UAL900465Battery Pack · dischargedALL EEL LIGHTS IN C-ZONE ARE INOP. REPLACED 3 BATTERY PACKS IN FORWARD C ZONE AND 3 BATTERY PACKS IN AFT C ZONE. CHECKS OK.SDR 98UAL900466Battery Pack · dischargedEMERGENCY OVERHEAD AND EXIT LIGHTS ON DOORS 2L, 2R AND SEVERAL LT AND RT THROUGH LIGHTS IN B ZONE ARE INOP. REPLACED BATTERY PACK AND BATTERY CONTROL BOX. CHECKS OK.SDR 98UAL900417Compressor · failedCAPT ADVISED AT 80KT EXPERIENCED LOUD EXPLOSION WITH MINOR AIRCRAFT SWERVE AND NR 3 EGT EXCEEDING MAX TEMP. CAPT ABORTED TAKEOFF AT 90KT WITH NO FURTHER PROBLEMS AND TAXIIED TO THE GATE. BORESCOPE INDICATES FAILURE INITIATED AT STAGE 7 HPC BLADE. REPLACED ESDR 98UAL900315Fan · failedELECTRICAL BURNING SMELL AND SMOKE REPORTED AT ROW 15. ALSO A GRINDING NOISE HEARD. NR 4 RECIRCULATING FAN TRIPPED OFF AND THE ODOR DISSIPATED. THE FAN WAS RESET AND FLIGHT CONTINUED TO IAD.SDR 98UAL900286Oil Pressure · lostLANDED ORD UNDER AMBER ALERT WITH NR 2 ENGINE SHUT DOWN DUE TO LOSS OF OIL PRESSURE.SDR 98UAL900282Bulkhead · crackedBS 1156 PRESSURE BULKHEAD FORWARD LEFT HAND SIDE AT L40 LONGERON HAS A CRACK. MANUFACTURED AND INSTALLED NEW REPAIR ANGLE.SDR 98UAL900262Lights · malfunctionedRED WARNING LIGHTS ILLUMINATED WHEN GEAR HANDLE SELECTED TO GEAR DOWN POSITION. CYCLED GEAR ONCE RED LIGHTS STILL ON. JIGGLED GEAR HANDLE GREEN LIGHTS CAME ON. LANDING NORMAL.SDR 98UAL900229Fuel Pump · failedSHORTLY AFTER TAKEOFF, NR 1 ENGINE THRUST WENT TO 85 PERCENT N1, THEN UNABLE TO INCREASE OR DECREASE THRUST. OPENED FUEL CROSS FEED VALVE AND THEN ABLE TO CONTROL ENGINE POWER. RETURNED TO SFO. REPLACED THE MAIN FUEL PUMP AND THE MEC. RAN ENGINE AT HIGH POSDR 98UAL900209Gear · failedNR 2 ENGINE FLAMED OUT AND WAS SHUT DOWN. FLIGHT CONTINUED TO SFO UNDER AMBER ALERT. ENGINE WAS CHANGED FROM AIRCRAFT. UPON TEAR DOWN OF THE INLET GEARBOX, A MAIN BEVEL GEAR WAS FOUND FAILED.SDR 98UAL900171Battery · discharged1L DOOR EMERGENCY SLIDE LIGHT IS INOP. REPLACED BATTERY.SDR 98UAL900165Wire · failedEEL LIGHTS AT 19-20H INOP. POWER FEED TO EEL 20H. REPLACED, CHECKS OK.SDR 98UAL900134Retract Mech · lack of lubeAFTER TAKEOFF, LEFT MAIN GEAR DID NOT RETRACT. DURING FLIGHT GEAR CAME UP. NORMAL LANDING AT ORD. *S/D* LEFT MAIN LANDING GEAR WAS FOUND WITH INADEQUATE LUBRICANT. THE GEAR WAS LUBED AND WAS OPERATED SEVERAL TIMES TO CONFIRM A NORMAL OPERATION.SDR 98UAL900122Tire · failedA LEFT MAIN GEAR TIRE BLEW ON TAKEOFF FROM DEN. DUMPED FUEL AND RETURNED TO DEN. AFTER NORMAL LANDING NR 1 ENGINE SHUTDOWN AND FIRE HANDLE PULLED. *S/D* NR 1 FORWARD MAIN LANDING GEAR TIRE WAS REPLACED. TASK ACCOMPLISHED TO CHECK THE BRAKE ACCUMULATORS, BSDR 98UAL900110Mid Shaft · failedSHUT DOWN NR 3 ENGINE DUE TO AIRCRAFT VIBRATION AND HIGH TEMPERATURE INDICATION. DIVERTED TO HNL LANDED UNDER AMBER ALERT. *S/D* THE FAN MID-SHAFT IN THE ENGINE SEPARATED. THE PRIMARY CAUSE OF FAILURE IS STILL UNDER INVESTIGATION BY GENERAL ELECTRIC.SDR 98UAL900097Lights · inoperativeSMALL RECTANGULAR LIGHTS ARE 1L AND 1R NOT OPERATIONAL DURING CHECK. *S/D* REPLACED EEL STRIP AT RIGHT GALLEY FORWARD OF CROSS AISLE 2 AND PUSHED BACK SOCKET AT DOOR IL EXIT SIGN PLUG. ALL EEL LIGHTS CHECK OK.SDR 98UAL900092Pressurization · malfunctionedAFTER TAKEOFF, PRESSURIZATION DID NOT OPERATE IN AUTO. SELECTED SEMI-AUTO, OK TO FL340 THEN SEMI-AUTO FAILED. SELECTED STBY, OK FOR ONE HOUR. ON CLIMB TO FL360, CABIN DEPRESSURIZED. SELECTED MANUAL BUT UNABLE TO CONTROL PRESSURIZATION. DESCENDED TO 15,000SDR 98UAL900069Coalescer Bag · dirtySTRONG PUNGENT ODOR REPORTED BY CABIN CREW NEAR FORWARD GALLEY AREA. *S/D* REPLACED ALL THREE COALESCER BAGS, NO RECURRENCE.SDR 98UAL900064Apu · malfunctionedNR 2 PNEUMATIC INOP AC OIL SMELL IN CABIN. *S/D* BURNED OUT NR 2 PACK. REPLACED COALESCER BAG. ALSO, REPLACED APU AS PRECAUTIONARY MEASURE.SDR 98UAL900044Nozzle · crackedNR 2 ENGINE HAS VIBRATION AND HUM THAT FOLLOWED THE THROTTLE. ENGINE REDUCED TO IDLE POWER AND DIVERTED TO LAS. *S/D* PRIMARY CAUSE OF ENGINE FAILURE WAS THE CRACKING OF THE HIGH PRESSURE TURBINE STAGE 1 NOZZLE. ON SEVERAL ADJACENT NOZZLES, THE CRACKS WRAPSDR 98UAL900004Rib · crackedA CRACK WAS FOUND ON THE CENTER WING SECTION RIBS LOCATED AT RBL 29.0. THE CRACK RUNS FWD AND AFT DIAGONALLY AND MEASURES APPROXIMATELY 4.00 INCHES IN LENGTH. A DOUBLER WAS INSTALLED IN THE AREA.SDR 97UAL900892Duct · rupturedON CLIMBOUT, NR 3 ENGINE FIRE INDICATION. INDICATION STOPPED WHEN ENGINE WAS SHUT DOWN. ENGINE EGT WENT TO 953C MOMENTARILY. *S/D* THE 16TH STAGE PNEUMATIC SUPPLY DUCT FAILED AND RUPTURED AT ONE OF THE ATTACHMENT LUGS. ABNORMAL VIBRATION CONDITION WAS CONSDR 98UAL900006Structure · damagedFUSELAGE SKIN AND UNDERLYING CIRCUMFERENTIAL FRAMES DAMAGED DURING PUSHBACK. DAMAGE OCCURRED ALONG A HORIZONTAL REFERENCE LINE APPROX 6 INCHES BELOW AND PARALLEL TO THE LOWER EDGE OF THE L1 DOOR CUTOUT. SKIN PANEL BETWEEN STA 304 AND STA 401 BUTT JOINTS AND SDR 97UAL900873Oil Temp Sensor · malfunctionedSHUT DOWN NR 1 ENGINE UPON LANDING TO HONOLULU DUE TO LOW OIL PRESSURE. *S/D* THE OIL TEMP SENSOR AND INDICATOR WERE REPLACED, OP CHECKED OK.SDR 97UAL900876O-Ring · erodedEVACUATION SLIDE AT DOOR 1L SELF DEPLOYED WITHIN A STORED AIRPLANE. O-RING (P/N 1A2313-3) IN THE BOTTLE VALVE FAILED DUE TO EROSION.SDR 97UAL900864Bulkhead Angle · corrodedNUMBER 3 PYLON LOWER FIREWALL AND ATTACH ANGLE FOR YN 315.5 BULKHEAD STIFFENER HAS FASTENERS CORRODED AND SHEARED UNDER FIRE BLANKET. OVERSIZE HOLES FOR NEW FASTENER TO FIRST OVER SIZE AND EDDY CURRENT NEW HOLES FOR CRACKS.SDR 97UAL900871Drain Holes · obstructedRUDDERS LOCKED ON FINAL. CREW FIRST OPERATED RUDDER BELOW 10,000 FEET. RUDDER FELT STIFF. AFTER TOUCHDOWN RUDDER PEDALS WERE STUCK IN NEUTRAL POSITION. *S/D* STANDING WATER FOUND IN FORWARD DIVERTER COMPARTMENT BELOW NR 2 ENGINE. AT ALTITUDE, WATER FROZESDR 97UAL900843Power Supply · inoperativeEMERGENCY LIGHTS FAIL TEST. FOUND CONNECTION ON POWER SUPPLY DAMAGED. REPLACED CONNECTION, POWER SUPPLY AND BATTERY PACK, OPS CHECK GOOD.SDR 97UAL900848Bulkhead Web · crackedTHE CENTER WING BOX BULKHEAD WEB AT STATION XCW=46.5 IS CRACKED. THE CRACK IS LOCATED BETWEEN APB7038-52 STIFFENERS AND APB7038-68 ANGLE AND APB 7038-60 TEE. THE CRACK LENGTH IS APPROXIMATELY 8 INCHES LONG. THE CRACK WAS TRIM-OUT AND A PREMANENT REPAIR WAS SDR CALA9701661Bolt · shearedTHE NR 1 ENG FAILED DURING CLIMBOUT AT FL 190. THE ACFT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENG WAS REMOVED AND REPLACED. *S/D* DISASSEMBLY OF THE ENG FOUND ONE HPT STAGE 1 NOZZLE SUPPORT BOLT LIBERATED. THE LIBERATED BOLT MOST SDR 97UAL900798Coalescer Bag · dirtySTRONG ACRID ODOR THROUGHOUT CABIN (STRONGEST IN THE AFT CABIN) WITH ALL PACKS ON. DISSIPATES WHEN RECIRCULATING FANS ARE TURNED OFF. *S/D* FOUND OIL, GYCOL, WATER AND HYDRAULIC FLUID IN AREA OF APU INLET. CLEANED UP FLUIDS AND BURNED OUT PACKS. REPLACED SDR 97UAL900802Bulkhead Angle · crackedAT STA Y=1156, TWO CRACKS WERE FOUND IN THE NYB6042-5 FWD PRESSURE BLKHD ANGLE. ONE CRACK IS AT X=+5.54 AND MEASURES APPROX. 1.2 INCHES. SECOND CRACK IS BETWEEN X=-5.54 AND X=-9.9 AND EXTENDED FROM UNDER AN EXISTING REPAIR DOUBLER. DOUBLER WAS REMOVED AND CSDR 97UAL900791Rib · crackedRIB WAS FOUND CRACKED AT THE UPPER CAP ATTACHMENT AT LT STA XFS=106.834 DURING HORIZONTAL STABILIZER LEADING EDGE RIB CAP INSPECTION. *S/D* RIB WAS REPLACED.SDR 97UAL900753Rib · crackedDURING C-CHECK EDDY CURRENT INSPECTION, CRACKS WERE FOUND IN THE RIGHT OUTBOARD FLAP CLOSING RIB ASSEMBLY.SDR 97UAL900754Battery Pack · dischargedEMERGENCY FLOOR LIGHTS WERE ILLUMINATED BETWEEN SEATS 17 AND 30. REPLACED BATTERY PACK FOR EEL LIGHTS. LIGHTS CHECKED OKAY.SDR 97UAL900749Battery · dischargedLEFT AISLE AND FORWARD FLOOR EMERGENCY LIGHTING IN ZONE B REMAINS ON WHILE SWITCH IN COCKPIT WAS SELECTED TO ANY POSITION. REPLACED EEL BATTERY. OP CHECK OF EMERGENCY LIGHTS ARE NORMAL.SDR 97UAL900719Rub Block · wornTAKEOFF WARNING HORN HEARD AND SLAT DISAGREE LIGHT CAME ON. ABORTED TAKEOFF AT APPROXIMATELY 140 KTS. REPLACED RIGHT NR 10 SLAT TRACK RUB BLOCKS AND RE-TENSIONED RIGHT OUTBOARD SLAT DRIVE CABLES.
Back to GE CF6-6D