Pratt & Whitney JT8D-219
Service difficulty reports · 1,944
Newest first. General aviation reporting is voluntary.
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 = 'JT8D219' 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 = 'JT8D219' 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 DALA1051439012Frame · unknownFUSLEAGE MAIN FRAME LT LOWER NOSE LONGERON 22-26 AND ATTACH FRAME REPAIRED IAW EA 09-069225-12, ME01.SDR DALA1022620982Wire · brokenDURING LINE CHECK MX FOUND EMERGENCY PATH LIGHTS FROM ROW 24-30 INOPERATIVE. MX REPAIRED BROKEN WIRE AT SEAT 30D AND LIGHT HARNESS. ALSO REPLACED POWER SUPPLY B5-211. OPERATION OF LIGHTS NOW CHECK OK.SDR DALA1022630942Wire · damagedDURING LINE CHECK MX FOUND EMERGENCY LIGHT AT 2C INOPERATIVE. MX SECURED PULLED WIRES FROM CONNECTOR AND REPLACED LIGHT ASSY IAW AMM 33-53-01. OPS OF LIGHT NOW CHECK OK.SDR DALA1022640909Light · inoperativeDURING LINE CHECK MX FOUND EMERGENCY LIGHT AT 17D INOPERATIVE. MX REPLACED LIGHT ASSY AT SEAT 17D IAW AMM 33-53-01. OPS OF LIGHT CHECKS OK.SDR DALA1022660922Connector · unsecureDURING LINE CHECK, MX FOUND FIRST CLASS LAVATORY EMERGENCY FLOOR LIGHTS INOPERATIVE. MX SECURED CONNECTOR. OPS OF LIGHT NOW CHECKS OK.SDR WX0A070603Battery Pack · inoperativeIT HAS BEEN REPORTED BY THE FLIGHT CREW, THE EMERGENCY EVACUATION LIGHTING SYSTEM HAS BEEN FOUND TO BE DEFECTIVE. MX R & R THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS. OPS CHECK WAS ACCOMPLISHED IAW AMM 33-50-0SDR DALA1022650950Battery · inoperativeDURING LINE CHECK, MX FOUND EMERGENCY LIGHTS IN TAIL COMPARTMENT AND L2 DOOR INOPERATIVE. MX REPLACED BATTERY IN AFT LAVATORY CEILING AND FUSE IN POWER SUPPLY R5-212. OPS OF LIGHTS NOW CHECK OK.SDR DALA1022050932Engine · failedDURING CLIMB APPROACHING FL360, THE FLIGHT CREW REPORTED THAT THE NR 1 ENGINE "POPPED" AND THE EGT CLIMBED TO 800 DEGREES. FLIGHT CREW SECURED THE NR 1 ENG BY SHUTTING OFF THE FUEL FLOW AND DIVERTED THE ACFT TO A SAFE LANDING. CREW REMARKED THAT THEY DID NOTSDR DALA1022060998Wire Harness · damagedDURING LINE CHECK MX FOUND EMERGENCY LIGHT AT 27D TO BE INOPERATIVE. MX RE-SECURED PULLED WIRE FROM HARNESS. OPS OF THE LIGHT NOW CHECKS OK.SDR DALA1022070998Wire Harness · inoperativeDURING LINE CHECK MX FOUND ALL ESCAPE PATH LIGHTS INOPERATIVE AFT OF ROW 31. MX RE-SECURED PULLED WIRE FROM SEAT 36F AND REPLACED FUSE IN BATTERY PACK BS-212. OPS OF LIGHTS NOW CHECKS GOOD.SDR WX0A070601Battery Pack · inoperativeDURING A ROUTINE OVERNIGHT SERVICE CHECK INSP MX REPORTED A PORTION OF THE EMERGENCY EVACUATION LIGHTING SYS WOULD NOT TEST. MX R & R THE APPROPRIATE BATTERIES IN THE POWER SUPPLY BATTERY PACK AND MADE ALL REQUIRED CORRECTIONS AND OPS CHECK WAS ACCOMPLISHED ISDR DALA1021810900Wire · brokenDURING LINE CHECK MX FOUND EMERGENCY LIGHT AT SEAT 20D INOPERATIVE. MX REPAIRED BROKEN WIRING AT SEAT. OPS OF LIGHT NOW CHECKS GOOD.SDR DALA1021780996ASlide · partial deployDOOR 4L OPENED PARTIALLY WHILE ARMED. SLIDE DID NOT FULLY DEPLOY AND DOOR DID NOT FULLY OPEN DUE TO SURVIVAL KIT LANYARD TANGLED IN GIRT BAR. REPLACED 4L DOOR SLIDE AND INFLATOR BOTTLE.SDR DALA1021780996Light · inoperativeDURING LINE CHECK MX FOUND EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. MX REPLACED LIGHT ASSY IN ROW 23D. OPS CHECK OF LIGHT, CHECKS OK IAW AMM.SDR DALA1020370911Skin · corrodedFUSELAGE C-3 DOOR SURROUND SKIN INTERNAL DOUBLER CORROSION. REPAIRED IAW ERA 484722-14.SDR DALA1020430954Wire · brokenDURING LAYOVER, MX FOUND THE NR 10 SEAT EMERGENCY LIGHT WIRE BROKEN MX REWIRED THE NR10 SEAT EMERGENCY LIGHT WIRE. OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.SDR DALA1020600976Panel · missingPANEL MISSING ONTOP OF RT AILERON CA-INSTALLED RT WING PANEL TOP OF RT AILERON. OK FOR SVC.SDR DALA1020060942Power Supply · inoperativeMX FOUND THE FWD ESCAPE PATH LIGHTING TO BE INOPERATIVE. MX REPLACED THE POWER SUPPLY AND THE F/A EMERGENCY LIGHT SWITCH. AN OPS TEST WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.SDR DALA1020590928Skin · corrodedFOUND 3 AREAS OF CORROSION, 1 AT APPROX STA 256 AND STR 29L ONE AT APPROX STA 256 AND STR 30 AND ONE AT STA 292 AND STR 30. REPLACED AFFECTED SKIN FROM FACTORY SPLICE TO STA 303 IAW ERA 484936-14 REV ORIG PERMANENT REPAIR.SDR 2WAA20101110AEngine · oil consumptionLT ENGINE LOST 11 QRTS OIL, REMAINING OIL 3 QRTS. NORMAL INDICATIONS PSI/TEMP.SDR DALA1020050912Battery Pack · inoperativeMX FOUND THE AFT LT AND RT OVERWING EXIT UPPER EMERGENCY LIGHTS TO BE INOPERATIVE. MX REPLACED THE BATTERIES FOR B5-105. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.SDR WX0A070588Engine · failedFLIGHT PERSONNEL REPORTED ON TAKEOFF ROLL JUST AT 30 KNOTS, HARD SHUDDER ON RIGHT ENGINE. THE "ART" FIRED AND POWER LOSS RIGHT SIDE. UPON INSPECTION SEVERAL ENGINE PARTS BLEW AFT AND SOME PARTS VISIBLE IN AFT SECTION. SMALL, FIRE CONTAINED, BURNED ABOVE 600 SDR DALA1018760921Compressor · stalledFLIGHT CREW RETURNED THE AIRCRAFT TO DEPARTURE AIRPORT DUE TO THE NR 1 ENGINE EXPERIENCING A COMPRESSOR STALL AND AN UNCOMMANDED SHUTDOWN. MAINTENANCE REPORTED METAL IN THE TAILPIPE SO THE NR 1 ENGINE WAS REPLACED (2010-D0955) (DLM88102118).SDR DALA1019200933Fuse · failedMX FOUND THE EMERGENCY LIGHTS FROM SEAT ROW 24 TO BE INOPERATIVE. MX CHECKED THE WIRING AND BATTERY PACKS AND ALL CHECKS GOOD. REPLACED POWER SUPPLY FUSES. A SYSTEM CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.SDR DALA1019329011Light · brokenMX FOUND THE EMERGENCY LIGHT AT 4C TO BE BROKEN. MX REPLACED THE LIGHT ASSY AT 4C. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.SDR 2010FA0000827Disk · crackedDURING DISASSEMBLY OF THE TURBINE MODULE IT WAS NOTICED THAT THE DISK (PN 777603) WAS CRACKED AT THE FIR TREE. ALSO NOTED, WERE (2) CRACKED BLADES (PN 798403), BOTH LOCATED NEAR (WITHIN (1) FIR TREE) OF THE DISC CRACK. THIS IS A KNOWN PROBLEM AND HAS BEEN PRSDR 2010FA0000828Blade · crackedDURING DISASSEMBLY OF THE TURBINE MODULE IT WAS NOTICED THAT THE DISK (PN 777603) WAS CRACKED AT THE FIR TREE. ALSO NOTED, WERE (2) CRACKED BLADES (PN 798403), BOTH LOCATED NEAR (WITHIN (1) FIR TREE) OF THE DISC CRACK. THIS IS A KNOWN PROBLEM AND HAS BEEN PRSDR 2ARF201008001Generator · faultyACFT PERFORMED AN UNSCHEDULED LANDING DUE TO APU OUT SERVICE IN FLIGHT. MX PERFORMED A SWAP BETWEEN RT GCU AND GCU OF THE APU IAW AMM 24-20-02. DURING TRANSIT CHECK, THE CSD AND OIL COOLER OF THE RT SIDE WERE REPLACED IAW AMM 24-10-03, ALL CORRECT.SDR DALA101787840975Light · inoperativeMX FOUND THE EMERGENCY LIGHT AT SEAT 3C TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.SDR DALA1017850954Seat · mislocatedWHEN MX TRIED TO GAIN ACCESS TO THE WING SURFACE FROM THE CABIN, THEY FOUND THE EMERGENCY EXIT DOOR WOULD NOT OPEN BECAUSE IT WAS BLOCKED BY THE ARMREST OF THE SEAT. THIS WAS IN ROW 24DE. IT WAS DETERMINED THAT THE SEATS IN ROW 23DE AND IN ROW 24DE WERE IN TSDR WX0A070580Engine · malfunctionedFLIGHT DECK PERSONNEL REPORTED EN ROUTE, RIGHT AC CROSSTIE LOCK OUT LIGHT ILLUMINATED. RIGHT AC ELECTRICAL FAILURE, PER QRH CONTINUED, APPROXIMATELY 20 MINUTES LATER, RIGHT ENGINE FIRE INDICATION, PER QRH SECURED RIGHT ENGINE AND LANDED AT NEAREST SUITABLE AISDR DALA1019649001Floor Support · corrodedMAIN PAX ABIN FLOOR SUPPORT HAS CORROSION AT LBL 48, BETWEEN BS 157 AND BS 200. 100 MATERIAL LOSS. R & R FLOOR SUPPORT IAW SRM 51-10-4, 51-30-1 AND 51-30-5.SDR DALA1020139004Beam · corrodedEXFOLIATION CORROSION ON LOWER DOOR JAMB BEAM REPAIR MRB 53-017-02. LOWER DOOR BEAM REPAIR PARTS WERE REMOVED IAW SRM 51-30-2 AND SRM 51-30-2. CORROSION WAS REPAIRED IAW SRM 53-05, FIG 804. NEW DOUBLERS WERE INSTALLED IAW SRM 53-05, FIG 804.SDR DALA1020149004Clamp · wornWORN CLAMP TAILCONE RELEASE CONTROL CABLE LT SIDE. REMOVED CLAMP IAW AMM 53-53-00-501 AND NEW CLAMP INSTALLED IAW AMM 53-53-00-501. OPS CHECK WAS DONE.SDR DALA1020159004Support Fitting · corrodedCORROSION ON LT GEAR SUPPORT FITTING BEARING BORE OTBD FACE LT WING. PITTING CORROSION WAS BLENDED OUT IAW SRM 51-02 D, EA 09-093855-03, AD 0104 AND TREATED IAW SRM 51-10-3.SDR DALA1020179004Support · damagedSCRATCHES ON LT GEAR SUPPORT FITTING BEARING BORE. SCRATCHES ON BORE WHERE CLEANED UP IAW EA 09-093855-03AD SRM 51-02 PARA 1A (6)(A)AND TREATED IAW SRM 51-10-3.SDR DALA1020189004Support · damagedSCRATCHES AND PITTING CORROSION ON THE GEAR SUPPORT FITTING BUSHING BORE AND THE BOTTOM BUSHING BORE AREA LW. SCRATCHES AND PITTING WERE BLENDED OUT IAW 51-02D PARA 1 A(6),PS900-2-4-1 NO 01,AMR 0957306 REV2, AMR 0957306, REV 3 STEP 4B AND TREATED IAW 51-10-3.SDR DALA1020169004Support Fitting · corrodedSCRATCHES AND PITTING CORROSION ON RT GEAR SUPPORT FITTING BUSHING BORE ALSO DEEP DEPRESSION ON AFT MID SECTION OF SAME BUSHING BORE. BORE HOLE REWORKED IAW AMR 0957306, REV 2, REPAIR INST 2. FINAL DIAMETER 2.4560", BOTTOM FLANGE THICKNESS 1.1110". BEARINGSDR DALA1020129004Frame · crackedCRACK WAS FOUND ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAM AT STA 886 RT REF EA 09-460094-12, AD OPN NR 0104. CRACKED FRAME WAS REMOVED IAW SRM 51-30-2 AND NEW FRAME WAS INSTALLED IAW SR09530282, REV ORG REF ALL AM NRCS T0180442,T0181246,AND T01812SDR YYFA201000022Door · malfunctionedON TAKEOFF NOSE GEAR DOORS APPARENTLY DID NOT CLOSE PROPERLY ACCOMPANIED BY LOUD AIR NOISE AND VIBRATION.SDR DALA1020109004Skin · corrodedCORROSION ON BARREL NUT 2EA OF RT HORIZONTAL STABILIZER UPPER SKIN STA XH=27 REF NRC T0180054 VHS MRB 55-056-02. REPAIR WAS ACCOMPLISHED IAW AMR 0955139, REV1 AND ERA 483916-14 REV ORIG.SDR DALA1020119004Fastener · improper partLOCK FASTENER INSTALLED ON POSITION 48 IS NOT PN HLT 427-6 AS STATED ON VA 71126AD OF EA 09-460094-12AD, REV A ME-03 OPN 0302 STEP 15. INCORRECT FASTENERS WERE REMOVED IAW SRM 51-30-5 PAR 8 AND CORRECT FASTENERS WERE INSTALLED IAW 51-30-5 PAR7.SDR AALA20100715DFW03Turbine Blades · damagedDFW - CREW REPORTED ON TAKEOFF THERE WAS A LOUD BANG AND THE RIGHT ENGINE BEGAN TO SPOOL DOWN. ENGINE AND AIRFRAME VIBES WERE FELT. RIGHT ENGINE SHUTDOWN ON ITS OWN. EXAMINATION OF THE RIGHT ENGINE ON THE GROUND SHOWED AFT SECTION OF TURBINE BLADES MISSING.SDR DALA1020099004Tab · damagedNICK ON LT ELEVATOR TAB T/E APROX XHS=35 (VHS). NICK ON LT ELEVATOR TAB WAS REPAIRED IAW AM OPN NR 1031, 1337 TO 1345 AND SRM 55-04 PARA 3 (3).SDR AALA20100705DFW01Relay · faultyDFW - CREW REPORTED RIGHT ENGINE OVERHEAT VALVE WAS NOT WORKING AND ENGINE OIL TEMPERATURE STAYED IN CAUTION RANGE. RIGHT ENGINE WAS SHUT DOWN AND SINGLE ENGINE TIME WAS EIGHT MINUTES. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVESDR DALA1019799001Skin · chafedVERTICAL STAB STR LT SIDE LOWER AFT SIDE OF CUTOUT, SKIN PANEL CHAFED. BLENDED CHAFED AREA, FOUND TO BE BEYOND SRM LIMITS. REPAIRED IAW SRM 55-01, FIG 4.SDR DALA1015450949Engine · damagedCLIMBING THROUGH 12000 RT ENGINE LOOP B ILLUMINATED FOLLOWED BY LOOP 1 AND FIRE HANDLE LIGHT FOR RT ENGINE. ENGINE WAS SHUT DOWN AND RTB SINGLE ENGINE EMERGENCY. INFLIGHT SHUTDOWN REPORT COMPLETED. FOUND 13TH STG DUCT TO EXIT CASE BLOWN. REPLACED NR 2 ENGISDR DALA1019699001Cargo Track · corrodedAFT CARGO BETWEEN STA 1007 AND 1155 RT SIDE, TIE DOWN TRACK HAS CORROSION (MRB 53-100-17). REMOVED CORROSION, BEYOND SRM LIMITS. REPLACED CARGO TIE DOWN TRACK IAW SRM 51-30-1 AND SRM 51-30-5.SDR DALA1018889005Support Fitting · damagedSCRATCHES ON LT MLG SUPPORT FITTING BEARING BORE. DAMAGE REMOVED IAW EA 09-093855-03AD, REV B, ME01, OPN 0103 AND BORE WAS FOUND TO BE IN LIMITS. BEARING BORE WAS TREATED IAW SRM 51-10-3 PAR 34.SDR DALA1018899005Beam · corrodedEXFOLIATION CORROSION ON AFT COMPARTMENT DOOR JAMB LOWER BEAM REPAIR DOUBLER STA Y=1168-1198 (C3). REMOVED DOUBLER IAW SRM 51-30-5. FAB NEW DOULBER IAW SRM 53-05, FIG 123. INSTALLED NEW DOUBLER IAW SRM 51-30-5 AND 53-05 FIG 123.
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