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 = 'V2528D5' 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 = 'V2528D5' 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 DALA1034269202Skin · crackedTHE LT SKIN AT STA 1494 BETWEEN LONGERON 2LT AND 3LT WAS FOUND CRACKED APPROX 3" LONG. DURING INSP IAW ERA 487106-14. DURING OPEN HOLE INSP MORE CRACKS WERE DETECTED AND A SECTION VERT STAB SKATE ANGLE WAS REMOVED. FINAL TRIM-OUT SIZE 4.3" X 5"A .063" DOUBLSDR DALA1034279202Skin · crackedTHE RT AFT FUSELAGE SKIN AT STA 1494 ABOVE LONGERON 3 RT AND JUST BELOW THE VERT STAB SKATE ANGLE WAS FOUND CRACKED. LENGTH OF CRACK APPROX 3.5 ". A REPAIR DOUBLER AND STRUCTURAL SHIM WERE INSTALLED.SDR 2010FA0001174Hub · damaged(Z3EY) THIS ENGINE IS UNDERGOING MX. DURING ROUTINE FPI, 11 LINEAR INDICATIONS WERE DETECTED ON THE FIR TREE ROOT PRESSURE FACES. THIS HAS BEEN DETECTED ON OTHER HUBS. THE ITEM HAS BEEN REMOVED FROM SERVICE.SDR DALA1023449208Frame · crackedFATIGUE CRACK IN FRAME FS 962 RT. R & R FRAME EO 02-460094-12AD REVA ME03 OPN0301.SDR DALA1023629206Actuator · intermittentACTION CLIMBING THROUGH 11,000 FT AND ACCELERATING THROUGH 310 KNOTS, NOSE GEAR DOOR CAME OPEN. SLOWED TO 250 KNOTS, DOOR APPEARED TO CLOSE. REPLACED NOSE GEAR DOOR LINK ACTUATOR AND RIGGED SAME IAW AMM. PERFORMED NOSE GEAR RETRACTION CHECK.SDR DALA1022599208Door Frame · crackedOVERWING EXIT FRAME 962 RT WAS FOUND CRACKED AND R & R IAW EA 02-460094-12AD.SDR DALA1021790904Lens · missingDURING LINE CHECK MX, FOUND EMERGENCY LIGHT INOPERATIVE AND MISSING LENS IN ROW 1. MX REPAIRED CRUSHED WIRING AND REPLACED MISSING LENS MODULE IN ROW 1. OPS CHECK OF LIGHT CHECKS OK.SDR DALA1020729216Lamp · inoperativeDURING LINE CHECK MX FOUND EMERGENCY PATH LIGHT INOP AND MODULE MISSING AT 15C. MX RE-LAMPED AND REPLACED MISSING MODULE. OPS OF LIGHT NOW CHECKS GOOD.SDR DALA1020739017Light · inoperativeMX FOUND THE EMERGENCY PATH LIGHT AT SEAT 26D TO BE INOPERATIVE. MX REPLACED THE EMERGENCY PATH LIGHT ASSY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.SDR DALA1020039212Wire · brokenDURING CHECK VIDEO CONTROL UNIT EMERGENCY LIGHTING FLOOR LIGHTS INOPERATIVE. ITEM WAS FWD TO MCO/PLACARD ON 16AUG10. THEN ON 18AUG10 MSP MX REPAIRED BROKEN WIRE AT 10CDE. ALL FLOOR PATH LIGHTS NOW OPERATE NORMAL AND THE MCO/PLACARD WAS REMOVED.SDR DLM90101290Wire · brokenON FLIGHT CHECK, MX FOUND CABIN EMERGENCY LIGHTS INOP FROM ROW 33 AND AFT. MX FOUND BROKEN WIRE AT SEAT ROW 35CDE. MX REPAIRED WIRE AND OPS CHECK OF LIGHTS NOW CHECK GOOD.SDR DLM90101300Light · inoperativeON 18MAY, THE INBOUND FLIGHT PILOT WROTE UP A FLOOR EMERGENCY ESCAPE PATH LIGHT AT SEAT 3C AS INOPERATIVE. MX FORWARDED THE LOG TO MX CONTROL WHO PLACARDED IT DUE TO PARTS NOT AVAILABLE . ON 26MAY, MX REPLACED RECEPTACLE AND LENS. OPS CHECK OF LIGHT, NOW CHSDR DLM90100845Light · inoperativeEMERGENCY FLOOR LIGHTING INOP AT 35C. REPLACED FLOOR TRACK LIGHT ASSY AND RED LENS. OPS CHECK OF LIGHT NOW OK.SDR DLM90100796Light · damagedEMERGENCY TRACK LIGHT LENS AND LIGHT DAMAGED AT SEAT 3C. REPAIRED AS REQD.SDR DLM90100797Light · damagedDAMAGED SECTION OF EMERGENCY TRACK LIGHTING AT SEAT 32C.SDR DLM90100798Bulb · burned outEMERG FLOOR PROX ESCAPE PATH LIGHTING BY SEAT 03C LOOSE, 2 ADJACENT WHITE LIGHTS INOP. FOUND BOTH BULBS BURNED OUT. RELAMPED SAME. OPS NORMAL AT THIS TIME. MCO AND PLACARD REMOVED.SDR DLM90100743Bulb · inoperativeEMERGENCY RED LIGHT AT 28C INOPERATIVE. REPLACED BULB AND LIGHT SOCKET ASSY. SYS CHECKS GOOD.SDR DLM90100512Coalescer Bag · dirtyCABIN EXUDES STRONG EXHAUST FUMES REPORTED BY INBOUND CREW. CHECKED RECIRC FAN AND FILTER ALL OK REPLACED LT AND RT WATER BAGS LEAK CHECKS OK RAN PACKS NO ODOR.SDR DLM90091208Actuator · malfunctionedDESCENT AT 15000 FT TO LEVEL OFF POWER INCREASE GOT STATUS MSG "L" STATOR VANE FAIL. THEN CREW NOTIFICATION OF LOAD POPPING NOISES ON LEFT AFT SIDE, THE LEFT ENGINE RPM DECREASED TO ~35% N1 AND EGT NEAR 600C. OIL PRESS AT 85 PSI. SHUT DOWN ENGINE AS EGT STASDR DLM90091212Engine · dirtyDESCENT AT 15000 TO LEVEL OFF POWER INCREASE GOT STATUS MSG LT STATOR VANE FAIL THEN CREW NOTIFICATION OF LOUD POPPING NOISES ON LEFT AFT SIDE, THEN LEFT ENGINE RPM DECREASED TO 35 PCT N1 AND EGT NEAR 600C. OIL PRESS AT 85 PSI. SHUTDOWN WAS 620C NO OTHER ABNSDR DLM90091086Connector · damagedL ENGINE GENERATOR OVERHEAT MESSAGE APPEARED IN FLIGHT THEN EXTINGNISHED. FOUND OIL COOLING LINE LEAKING AND GENERATOR FAILED.REPLACED OIL COOLING LINE AND GENERATOR. CONNECTORS DAMAGED. WILL NEED HARNESS ASSY MFG P/N 290W5211-509 DPN 242710080. DUE TO HASDR DLM90090330Fastener · looseENGINE AFT MOUNT SUPPORT FITTING FASTENER INSPECTION PER EA 02-469466-12AD. UPPER AFT FASTENER (AFT FASTENER ON ROW A) FAILED INSPECTION. REPLACED ALL 8 FASTENERS IN FITTING PER EA INSTRUCTIONS. REPLACEMENT OF DISCREPANT FASTENERS CONSTITUTES A MAJOR REPAIR SDR DLM90081435Engine · bird ingestionHIT BIRD AT ABOUT 135 KTS. HIGH SPEED ABORT ACCOMPLISHED AND PARKED WITH HOT BRAKES. RT ENGINE FLUCTUATED AND HAD NOTICABLE POWER LOSS WITH THE BIRD STRIKE. BRAKE TEMP REACHED 650. REPLACED NR 2 ENGINE.SDR DLM90080399Actuator · malfunctionedLEFT ENGINE SHUT ITSELF DOWN ON APPROACH INTO SEA. LEFT ENG RESTARTED. REPLACED L ENG STATOR VANE ACTUATOR PER AMM, STILL NEEDS L CHECK AND ENG TEST NR 3 AND 11, DC 690463. LEAK CHECKS E AND C/W TEST NR 3 AND NR 11.SDR DLM90080053Proximity Sensor · malfunctionedLT MAIN GEAR RED LIGHT WAS SLOW TO EXTINGUISH AFTER TAKEOFF. ASSOCIATED OAP MESSAGE AUTO SPOILER FAIL. QRH PROCEDURE FOR AUTOSPOILER FAIL MESSAGE DID NOT EXTINGUISH MESSAGE. RETURN SLC AS DIRECTED BY COMPANY. CHECKED NOSE GEAR PROX SENSORS WIRES AND TARGETSDR DLM90080045Converter · faultedLT AC PWR FAULT. REMOVED AND REPLACED VSC CONVERTER PER AMM. OPS GOOD PART NO 1B189-5.SDR DLM90071167Engine · intermittentLT ENG STRAINER CLOG ILLUMINATED DURING INITIAL CLIMB COMPLETED WITH CK LIST AND RETURNED TO LAND. ENG WAS NOT SHUT DOWN AND LANDING WAS NOT OVERWEIGHT. INSP/CLEANED SCAVENGE OIL FILTER PER MEL REF. NO DEPOSITS NOTED. FWD TO MCO AND PLAC PER MEL 79-36-01.SDR DLM90071060Engine · vibrationAT FL300 THE LT STATOR VANE MSG ILLUMINATED, THE CREW DISCONNECTED THE AUTOTHROTTLES AND KEPT THE LT ENG ABOVE IDLE AS PER THE QRH. WITH INCREASING VIBS AND EGT CLIMBING THE CREW REDUCED THE THROTTLE TO IDLE AND SHUT DOWN THE ENGINE. LT ENG WINDMILLED FOR LESDR DLM90070287Engine · fodAT FL310, LEFT ENGINE SHUT DOWN IN FLT HEARD BANG AND FELT SHUTTER N1 RAPIDLY DECREASED, EGT INCREASED TO 730 OIL PRESS WENT TO -0-. C/W BORESCOPE INSP FOUND FOD BEYOND M/M LIMITS. DAMAGE STA AT 3RD STG HPC. STG 2.5 LPC BLADES ARE CLEAN ENG CHANGE REQUIRED. SDR DLM90070048Fire Loop · malfunctionedLEFT ENGINE FIRE DETECT FAULT ILLUMIINATED ON OAP. REPLACED LT ENG DET. PERFORMED HIGH VOLTAGE MEG OHM CHECK ON ALL LT ENG A LOOP WIRES NO FAULTS FOUND FROM CONDUCTOR TO GROUND. REPLACED FAN FIRE DET LOOP A D1-910. REPLACED LOOP D1-911D1-912D1-914D1-915 NESDR DLM90060937Line · leakingRIGHT ELECTRICAL SYSTEM FAIL WITH RIGHT GEN OIL PRESSURE MESSAGE ON OAP. FIVE MINUTES LATER RIGHT GEN FAIL. ON ARRIVAL LAS, FOUND NO OIL IN GENERATOR. FOUND OIL OUT LINE LEAKING. REPLACED LINE AND GENERATOR. SERVICED WITH OIL. OPS CHKS GOOD PER AMM. OIL SDR DL76L060430Bleed Valve · malfunctionedLT ENG PRV MSG IN FLT WITH ASSOCIATED BLEED LIGHT. REPLACED PRV CONTROLLER AND PRV PER MM ENGINE RUN, OPS GOOD.SDR DLM90060417Engine · malfunctionedON APPROACH INTO PHX, LOST OIL PRESSURE ZERO INDICATION WITH LOW OIL PRESSURE MESSAGE ON EOAP WITH BOTH OIL PRESSURE CAUTION AND WARNING LTS ILLUMINATED. ENGINE SHUTDOWN ACCOMPLISHED PER QRH. OIL TEMP AND ALL OTHER PARAMETERS WERE NORMAL PRIOR TO SHUTDOWN. SDR DL757060351Tire · failedNR 3 MAIN TIRE FAILED DURING RTO. RT SIDE BRAKE TEMP AT 3 HIGHEST. REPLACED NR 3 WHEEL ASSY BRAKE TEMP AT 3 DOES NOT REQUIRE HIGH ENERGY STOP INSP.SDR DLM90060350Hydraulic System · unknownRIGHT SYSTEM HYDRAULIC PRESSURE LOW AFTER TAKEOFF FROM SLC. REPLACED RIGHT SYSTEM RESERVOIR SERVICED THE RIGHT HYD SYSTEM. BLEED SYSTEM PERFORMED OP AND LEAK CHECK OF THE RIGHT ELEC AUX PUMP AND RIGHT ENGINE DRIVE PUMP. ALL CHECK GOOD AND NO LEAKS NOTED.SDR DLM88060352Line · leakingLT HYD SYS LOST HYD PRESS FOLLOWED BY LT SYS HYD LOSS. FOUND FLEX PRESSURE LINE INBD OF LEFT PYLON LEAKING. REPLACED SAME. REPLACED NR 1 EDP. LEFT ENG LK CK OK PER MM. REPLACED CASE DRAIN AN PRESSURE FILTERS FOR LEFT ENGINE. LK CK GOOD. C/W IN FLIGHT FLSDR DLM90060287Converter · inoperativeLEFT ENGINE GEN FAILED AFTER TAKEOFF. REPLACED NR 1 ENGINE GEN CONVERTOR UNIT. GEN CHECKED OK.SDR DLM90060263Engine · malfunctionedLEFT ENGINE BEGAN TO SHUDDER FOLLOWED BY A COMPRESSOR STALL AND PARAMETER ROLLBACK AND EGT INCREASE. C/W BORESCOPE INSPECTION OF THE HPC AS PER AMM. FOUND NUMBER STAGES DAMAGED AND OUT OF LIMITS. REPLACED ENGINE PER TRANS 2T102.SDR DLM90060238Generator · lack of lubeAT CRUISE POWER DISRUPTED W/L AC PWR FAULT AND L GEN OFF MSG GEN WOULD NOT RESET. ACCOMPLISHED QRH PROCEDURE. LEFT BUS RECEIVED PWR FROM APU GEN BUT APU FAULT MSG ILLUMINATED. L ELEC SYS FAIL AND L GEN OIL PRESS MSGS APPEAR WHEN STATUS BUTTON PUSHED. (ATL SDR DLM90060194Generator · failedRIGHT GEN INOP ON MCO, APU LOW ON OIL, MSG IN FLIGHT. RETURN TO GATE. REPLACED RIGHT GEN, CHECKS GOOD. SERVICED APU, CHECKS GOOD. NO LEAKS.SDR DLM90060169Engine · hot startON DESCENT, NR 1 ENGINE EGT PEGGED AT TOP OF RED RANGE 881 DEG WITH OIL PRESS AT 260 PSI AND OIL TEMP 96 DEG. NO OTHER UNUSUAL INDICATIONS. RETARDED TO IDLE WITH NO IMPROVEMENT. SHUT ENGINE DOWN IAW QRH. REPLACED ENGINE.SDR DLM90060047Warning Light · illuminatedON TAKEOFF AT KOAK, EOAP DISPLAYED RT EECEDP BUSS FAIL. TROUBLESHOT PER FIM, MESSAGE CLEARED.SDR DLM90050472Tru · failedAPPROX 10 MINS AFTER T/O LEFT GENERATOR TRIPPED OFF LINE AND WOULD NOT RESET. APU WAS STARTED IAW PROCEDURE. LOSS OF CAPTS FLT DIRECTOR, NR 1 VOR, AND ALL ENGINE INSTRUMENTS WERE CONTINUALLY FLICKERING AND DISPLAYING ERRONEOUS DATA. GROUND PROXIMITY C/B WASSDR DLM90041056Electrical Sys · failedLEFT ELEC SYSTEM FAILED EN ROUTE. REPLACED LEFT ECU.SDR DLM90040565Fire Loop · malfunctionedPASSING 3000 FT RT ENGINE FIRE DETECTOR FAULT MESSAGE ILLUM IT STAYED ON FOR APPROX 1 MIN AND THEN WENT OUT. FIRE DET FAULT MESSAGE CAME ON WITH RT ENG B-LOOP LIGHT. LIGHT INTERMITTENT CAME ON AND OFF WITH WITH -B- LOOP. PERFORM FAULT TEST PER T/S MANUAL. SDR DLM90040391Engine · malfunctionedACS REPORTED TAIL PIPE FIRE NR 2 ENGINE AFTER ENGINE SHUTDOWN. REPLACED ENGINE.SDR DLM90040265Generator · brokenLT GEN FAILED IN CLIMB WITH GEN OFF, LIGHT ILLUMINATED. RESET ONCE UNSUCCESSFUL. VERBAL FROM CREW VIBRATION FELT IN A/C AND YOKE. FOUND GENERATOR BROKEN IN 2 PIECES WITH GEARBOX CONTAMINATED WITH METAL MATERIAL. WILL REQUIRE ENGINE REPLACEMENT.SDR DLM90031090Warning Light · inoperativeAFTER ARRIVAL AT GATE AND DURING PASSENGER NORMAL EXIT, RAMP STATED, A TAILPIPE FIRE IN NR 2 ENG. NO FIRE INDICATION OR LIMIT EXCEEDENCE NOTED. TAILPIPE FIM PROCEDURE ACCOMPLISHED IAW POM. ENG WAS ALREADY SHUT DOWN. CLEANED NR 5 BEARING CAVITY AND RAN ENGISDR DLM90030819Bearing · cokedNUMBER ONE ENGINE HAD TAIL PIPE FIRE ON SHUT DOWN. NUMBER 1 ENGINE BEING CHANGED DUE TO EXCESSIVE COKING IN NUMBER 5 BEARING COMPARTMENT PER IAE.SDR DLM90030795Engine · fireRAMP AND FLEET SERVICE REPORT NR 1 ENG TAIL PIPE FIRE ON SHUTDOWN. REF ERA087224-14 NO COKING FOUND IN NR 5 BEARING SCAV TUBE ENG, LEAK AND OPS NORM PER PFHB.
Back to IAE V2528-D5