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 DLM88100828Support · corrodedEXFOLIATION CORROSION ON SUPPORT UNDER LOWER DOOR JAMB OF VENTRAL DOOR BTW X=4 TO X=10VAT STA Y=1350. DAMAGE WAS REMOVED AND REPAIR PARTS WERE FABRICATED, TREATED, AND INSTALLED IAW ERA 480767-14 REV ORIG.SDR DLM88100827Skin · damagedLIGHTNING STRIKE DAMAGE ON LT ELEVATOR GEARED TAB T/E. LT ELEVATOR GEARED TAB T/E WAS REPAIRED IAW SRM 55-04 PAR 34 AND OPN 1031 CARD 1213-1221.SDR DLM88100705Beam · corrodedCORROSION ON LOWER BEAM STA Y=370-247 AT FWD CARGO COMP DOOR JAMB. RE-WRITE; SEVERAL RIVETS IMPROPERLY INSTALLED AND INCORRECT WASHERS INSTALLED UNDER HI-LOCK NUTS. RIVETS AND WASHERS WERE REPLACED IAW SRM'S 51-30-2 AND 51-30-5.SDR DLM88100786Floorbeam · corrodedMAIN PASS CABIN STA 241 LBL42 FLOOR SUPPORT CORRODED/ FABRICATED NEW FRAME SECTION USING EXT S2929169 IAW SRM 53-01 AND 51-10-03.SDR DLM88100787Intercostal · crackedMAIN CABIN STA 1295 TO 1306, BL0 INTERCOSTAL BETWEEN BEAM CRACKED IN 4 PLACES.SDR DLM88100590Light · damagedEMERGENCY LIGHT AT SEAT 25D INOP. FOUND LIGHT ASSY DAMAGED. R & R EMERGENCY LIGHT ASSY AT SEAT 25D. OPS CK NML.SDR DLM88100594Skin · dentedACFT RECEIVED DAMAGED AT FS 1300 LONGERON 26L. THE ACFT WAS REPAIRED IAW ERA 480472-14.SDR DLM88100754Strap · corrodedDURING HMV3, AFT CARGO BETWEEN STATION 1231-1271, L23L STRAP IN CENTER OF LONGERON IS EXFOLIATED OUT OF LIMITS. REMOVED STRAP IAW SRM 51-30-02 MATERIAL USED FOR NEW STRAP 7075T6 .250, FAB OF -75 STRAP ACCOMPLISHED ON TRAVELER NR 1943N01202 IAW DWG 5911423. POSDR DLM88100823Beam · corrodedEXFOLIATION CORROSION OVER BEAM OF C2 LOWER DOOR JAMB. FASTENERS WERE REMOVED IAW SRM 51-30-5. CORROSION REMOVED IAW SRM 51-10-3 PAR 26. THICKNESS FOUND OUT OF LIMITS IAW SRM 53-05 FIG 123 SHEET 2. REPAIR DOUBLERS, FILLER AND SPACER WERE FABRICATED AND INSSDR DLM88100824Beam · corrodedEXFOLIATION CORROSION ON UPPER SURFACE OF AFT CARGO COMPARTMENT DOOR JAMB BEAM. CORROSION WAS REMOVED IAW SRM 51-10-3 PAR 26 AND AREA WAS FOUND OUT OF LIMITS IAW SRM 53-05 FIG 123 SHEET 2. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM'S 53-05 FIG 123 ASDR DLM88100825Fitting · corrodedPITTING CORROSION ON LT GEAR SUPPORT FITTING BUSHING BORE. LT GEAR SUPPORT FITTING BUSHING BORE WAS MACHINED TO CLEAN UP CORROSION IAW ERA 480222-14AD REV ORIG. FINAL SIZE ID 2.535. FLOURESCENT DYE INSP PERFORMED IAW EA 09-093855-03 AD OPN 0104 PAR J NOTE ASDR DLM88100826Support · scratchedSCRATCHES ON TRANSITION STEP OF RT GEAR SUPPORT BUSHING BORE. RT MLG SUPPORT BUSHING BORE WAS MACHINED AT TRANSITION STEP TO CLEAN UP DAMAGED SURFACE IAW ERA 480222-14AD REV ORIG. REMAINING WALL THICKNESS BETWEEN BUSHING AND BEARING 1.223, BEARING BORE ID 2.3SDR DLM88100511Wire · brokenFOUND ON CHECK - EMERGENCY TRACK LIGHT OUT AT 28CD. FND BROKEN WIRE AT SEAT CONNECTOR OTBD SIDE OF SEAT ASSY. NO PARTS AVAIL TO CORRECT. FWD TO MCO AND PLAC IAW MEL33-00-24 ONLY ONE LIGHT INOP AT THIS SEAT LOCATION.SDR DLM88100513Battery Pack · inoperativeF/C CEILING EMERGENCY LIGHT INOP AT 2 AND 3 NO HELP AND ROW 10 NO HELP. REPLACED BATTERIES. OPS NORMAL.SDR DLM88100514Light · inoperativeEMERGENCY TRACK LIGHT OUT SEAT 38DE. RELAMP NO HELP. REPLACED LIGHT ASSY OPS NORMAL.SDR DLM88100515Light · inoperativeDURING L/O FOUND ROW 25 ED EMERGENCY TRACK LIGHT AFT RED LIGHT ASSY INOP. REPLACED LIGHT ASSY. RED LENS INSTALLED. OPS NORMAL.SDR DLM88100516Wire Harness · damagedSEAT 24DE FWD RED EMERGENCY PATH LIGHT INOP. T/S FOUND SEAT HARNESS CUT AT ZIP TIE NEEDS DAL PN 334202640, SHOULHAN 712232. REPLACE HARNESS AT SEAT 24DE. OPS CKS GOOD.SDR DLM88100510Connector · brokenFOUND ON CHECK EMER LIGHT OUT AT 34CD. FND WIRE BROKEN AT SEAT TRACK CONNECTOR. REPLACED CONNECTOR AND PINS. OPS CK OK.SDR DLM88100700Access Door · damagedELONGATED SCREW HOLE AND FRETTING CORROSION ON SLAT TRACK ACCESS DOOR NR 1132C AND 1165C OF LT WING LW. ACCESS DOOR WAS REPAIRED IAW ERA 480223-14 REV, ORIG AND SRM 51-10-3.SDR DLM88100697Beam · corrodedEXFOLIATION CORROSION ON LOWER BEAM STA Y=370-427 AT FWD CARGO COMP DOOR JAMB. DOOR JAMB WAS REPAIRED IAW SRM'S 51-30-2, 53-05D, AND 51-10-3.SDR DLM88100698Beam · corrodedEXFOLIATION CORROSION ON LOWER BEAM STA Y=1155-1212 AT AFT CARGO COMP DOOR JAMB. BEAM WAS REPAIRED IAW SRM'S 51-30-5, 51-10-3, AND 53-05 FIG 123.SDR DLM88100699Beam · corrodedCORROSION ON LOWER BEAM STA Y=636-693 AT MID CARGO COMP DOOR JAMB. BEAM WAS REPAIRED IAW SRM'S 51-30-1, 51-30-2, 51-10-3 PAR 2B, AND 53-05 FIG 123.SDR DLM88100693Tube · dentedWORN FUSELAGE TUBE OF TAILCONE RELEASE CONTROL CABLE STA 1510 CANT 5 O'CLOCK POSITION. TUBE WAS REPLACED IAW AMM 20-30-01-201. TAIL CONE RELEASE CONTROL CABLE WILL BE ADJUSTED ON NR T0164941.SDR DLM88100694Release Cable · frayedBROKEN STRANDS ON TAILCONE RELEASE CABLE STA 1510 CANT 11 O'CLOCK POSITION. CABLE WAS REPLACED IAW AMM 20-10-17-201. CABLE WAS ADJUSTED AND OPS CHECKED IAW AMM 53-53-00-501.SDR DLM88100696Link · wornBENT LINK AND WORN ARM OF VENTRAL CATWALK CONTROL MECHANISM STA 1485 CANT X=-10. LINK, ARM AND HARDWARE OF VENTRAL CATWALK CONTROL MECHANISM WAS REPLACED IAW AMM 20-30-01-201.SDR RYNA2010002170004Fan Blade · bentRIGHT ENGINE HAD 3 COMPRESSOR STALLS DURING CLIMB THROUGH 16,000 TO 17,000 FT. DURING TROUBLESHOOTING FOR COMPRESSOR STALL FOUND DAMAGED 1ST STAGE FAN BLADE. PERFORMED VISUAL INSP OF BLADE DAMAGE, BLADE BENT 1 ¼ (L/E TO T/E) AND 1 24/32 (TIP TO SHANK) WITH NSDR DLM88100689Stiffener · crackedCRACK ON STIFFENER AT STA Y=1350 AND X=0 AT P-DOME UPPER SIDE. CRACKED STIFFENER WAS REPALCED IAW SRM'S 51-30-2 AND 51-30-5 AND 51-10-4. EMERGENCY EXIT MECHANISM ARM ASSY WAS REMOVED AND REINSTALLED TO FACILITATE MX IAW CMM 52-22-02.SDR DLM88100686Skin · dentedDENT ON FUSELAGE SKIN STA Y=232 LONGERONS 17 AND 18 LT. DAMAGED AREA WAS R & R IAW SRM 53-04 FIG 12B, SRM 51-10-4 AND SRM 51-10-3. REPAIR WAS IDENTIFIED IAW PS 900-5-1 NR 4.SDR DLM88100284Indicator · stuck2H EPR STUCK AT APPROX 1.5 ON T/O ROLL- RTO AT 30 KTS. FLIGHT CREW PLACARD INSTALLED IAW MEL 77-00-01A.SDR DLM88100174Fuel Control · malfunctionedAT FL 35 LT ENG EPR, N1 AND N2 STARTED TO ROLL BACK. RT ENG STAYED AT 2.0 EPR. LT WENT DOWN TO 1.1 EPR. F/A HEARD LOUD NOISE OR BANGING FROM ENG. ANTIICE ON IN MO TURBULANCE DURING DESCENT LOST PRESSURIZATION. LT ENG STARTED TO RESPOND AROUND FL 20 AND BYSDR DLM88091969Engine · failedRT ENG PWR LOSS AFTER TAKEOFF. FOUND METAL IN TAIL PIPE, REQUIRES ENGINE CHANGE. REPLACED RT ENG.SDR DL76P091971Indicator · malfunctionedRTB DUE TO INOPERATIVE SPEED FLAG ON ADIS RESET TMC C/BS. FLAGS CLEARED - NO ADC FAULTS. TMC TESTS GOOD. A/T SERVO TESTS GOOD.SDR DL76L091935Transmitter · inoperativeLT ELEVATOR POSITION INDICATION INOP AFTER TAXI OUT. FWD TO MCO AND PLACARD IAW MEL 27-08-01. RESET ELEV POS IND C/B NO HELP. VERIFIED LT ELEV MOVEMENT. REMOVED & REPLACED LT ELEV POSITION TRANSMITTER IAW AMM CKS GOOD MCO AND PLACARD REMOVED. ETOPS CATEGOSDR DLM88091934Gcu · faultedRT ENG GEN FAULT ON T/O ROLL AT 40KIAS. REPLACED RT GCU IAW MM. RAN RT ENG WITH GEN LOADED SEVERAL TIMES. OPS CK NML. VOLTS AND FREQS NML. MCO/PLAC RMVD.SDR DLM88091853Turbine · failedRT ENG FAILURE ON T/O CLIMB POWER. SPD 250 ALT 3000 LOUD BANG- EPR ROLLED BACK- TEMP RISE TO 800- SOME ROTATION UNTIL FUEL SHUT OFF. NO FIRE INDICATION. RTN TO FLL. AT GATE MTC FOUND TURBINE FAILURE. METAL IN TAILPIPE. WILL REQUIRE ENGINE CHANGE. REPLACSDR DL76L091854Pressure Panel · gougedPRESSURE WEB GOUGED UPPER SURFACE AT APPROX STA 970R AND RBL 90. REPAIR IN ACCORDANCE WITH ERA 478288-14.SDR WX0A070480Engine · failedUPON CLIMBOUT IN A RIGHT TURN A LOUD POP WAS HEARD AND THE ACFT LURCHED. NR 1 ENGINE N1 AND N2 SPOOLED DOWN AND EGT ROSE TO JUST UNDER 800 DEGREES. PERFORMED EQRH, SEVERE ENGINE DAMAGE CHECKLIST. MAINTENANCE DEPARTMENT PERSONNEL REMOVED AND REPLACED THE 31 SDR AALA20091116ORD01Engine · failedON FINAL NUMBER ONE ENGINE BEGAN TO VIBRATE AND SURGE. MOVED THROTTLE TO IDLE. LANDED WITHOUT INCIDENT. FOUND METAL IN TAILPIPE. REPLACED NUMBER ONE ENGINE ON 17 NOV 2009 AT ORD.SDR DALA1052240623Structure · crackedNR 2 PYLON RT SIDE UPPER CHORD CRACK REPAIRED IAW ERA 477880-14.SDR DLM88091631Engine · failedAT APPRX 1700 FT, HEARD LOUD BANG FOLLOWED BY RT ENG ROLLING BACK AND EGT ROCKETING THRU 600 DEG. CREW SHUT THE FUEL OFF. C/W ENGINE CHANGE NR 2 IAW TRANSMITTAL NR 9T102 AD.SDR DL76L091632Indicator · failedON CLIMB OUT RECEIVED RT ADF FLAG WITH FUMES IN COCKPIT. F/O HSI ALSO LOST COLOR AND FLICKERED. ALSO RECEIVED CABIN AUTO INOP 1 AND 2. STILL TROUBLE AT THIS TIME. THE ODOR HAS GONE AWAY AT THIS TIME. CHECKED BEHIND P11 AND P6 CB PANELS-NTF. REMOVED AND RSDR DLM88091630Engine · bird ingestionCREW REPORTS FLYING THRU A FLOCK OF BIRDS ON TAKEOFF. FOLLOWED BY REPEATED COMPRESSOR STALLS AND ENG ROLLED TO WINDMILL SPEED. CREW SHUT THE FUEL LEVER OFF. THEY DID NOT NOTICE THE OIL PRESSURE AFTER SHUTDOWN. WINDMILL APPRX 10MINC/W TRANSMITAL 9T102 NR 1 ESDR DLM88091580Transmitter · malfunctionedLT ENG OIL PRESS PEAKED HIGH AT CRUISE TO 70 PSI, THROTTLES MOVED BACK TO IDLE AND PRESSURE DOWN TO 45 PSI. OIL PRESS FOLLOWING THROTTLES, ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED NR 1 ENG OIL PRESS RELIEF VALVE AND OIL PRESSURE TXMTR PER AMM. ALSSDR DLM88091518Engine · malfunctionedIRR - DURING CLIMBOUT OF FL 290 A/C EXPERIENCED A LOUD BANG, SHUDDER LEFT ENGINE. SHUT DOWN INSTANTLY, COMPLETED ALL CHECKLISTS AND RETURNED TO KFLL. LANDING WEIGHT WAS 122,900LBS. REPLACED NR 1 ENGINE.SDR DLM88091491Case · failedON ENGINE START GOOD PRESSURE AND START VALVE BUT NO ENGINE ROTATION. FOUND LT STARTER CASE FAILED. REMOVED AND REPLACED LEFT ENGINE STARTER ASSY, CHECKS GOOD.SDR YYFA20090003Line · leakingDURING CRUISE , RT ENGINE OIL QUANTITY DROPPED TO ZERO , SHORTLY AFTER THE RIGHT OIL PRESSURE DROPPED BELLOW 35 PSI AND OIL TEMPERATURE ROSE , INFLIGHT RIGHT ENGINE WAS SHUTDOWN BY CREW. AIRCRAFT LANDED SAFELY , MAINTENANCE FOUND AN OIL LINE LEAKING FROM RIGHTSDR AALA20090821TUL09Engine · malfunctionedTUL - INFLIGHT ORD-DFW. CREW REPORTED ENGINE OIL FILTER CLOG LIGHT ON AND LEFT ENGINE COMPRESSOR STALL. LEFT ENGINE PULLED TO IDLE BUT WAS NOT SHUT DOWN. EMERGENCY DECLARED, LANDED TUL WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE SDR AALA20090811DFW01Engine · malfunctionedDFW - LEFT ENGINE OIL PRESSURE LIGHT CAME ON WITH PRESSURE SHOWING ZERO. CREW SHUT DOWN LEFT ENGINE. SINGLE ENGINE TIME 10 MINUTES. EMERGENCY DECLARED RETURNED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LEFT ENGINE DUE TO OISDR WX0A070375Engine · failedSEIZURE OF THE NR 2 (RIGHT) ENGINE AT 1200FT. PERFORMED EQRH, TRIED TO RELIGHT WITH NO SUCCESS. SECURED THE ENGINE AND LANDED AT FLL. MAINTENANCE DEPARTMENT PERSONNEL PERFORMED ALLEGIANT AIR TASK CARD R0807101, MD80, JT8D ENGINE REMOVAL AND REPLACEMENT. OK FSDR AALA20090729STL01Fan Blade · damagedAT 1100" AGL BIRD STRIKE RIGHT ENGINE. INITIAL EPR DROP OF .60, RECOVERED AFTER DELAY OF 10 SECONDS (COMPRESSOR STALL). SMOOTH OVERWEIGHT LANDING AT 152,500. ENGINE WAS OPERATED AT IDLE. PRELIMINARY VISUAL 13 FAN BLADES BENT/DAMAGED. INSPECTION TO COMPLET
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