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 ASAA0580543Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)SDR ASAA0580544Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)SDR ASAA0580545Floor Panel · corrodedC-CHECK, CABIN FLOOR PANEL HAS CORRODED INSERTS AND IS DELAMINATED AROUND INSERTS. REPLACED FLOOR PANEL. (K)SDR ASAA0580546Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)SDR ASAA0580547Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)SDR ASAA0580548Floor Panel · delaminatedC-CHECK, CABIN FLOOR PANEL IS DELAMINATED. REPLACED FLOOR PANEL. (K)SDR ASAA0580549Track · corrodedC-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K)SDR ASAA0580550Track · corrodedC-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K)SDR ASAA0580551Track · corrodedC-CHECK, CABIN FLOOR TRACK CORRODED. REPLACED FLOOR TRACK. (K)SDR ASAA0580552Web · crackedC-CHECK, CABIN FLOOR WEB CRACKED. REMOVED DAMAGED WEB SECTION. INSTALLED REPAIR DOUBLER. (K)SDR ASAA0580553Skin · dentedC-CHECK, FUSELAGE SKIN DENTED. COLD-WORKED TO ORIGINAL CONTOUR. INSTALLED REPAIR DOUBLER. (K)SDR ASAA0580554Skin · dentedC-CHECK, FUSELAGE SKIN DENTED. COLD WORKED TO ORIGINAL CONTOUR. INSTALLED REPAIR DOUBLER. (K)SDR ASAA0580555Vane · gougedC-CHECK, LT WING OB FLAP IB VANE IS GOUGED. BLENDED GOUGE. INSTALLED REPAIR DOUBLER. (K)SDR ASAA0580556Vane · puncturedC-CHECK, LT WING NR 1 FLAP VANE IS PUNCTURED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (K)SDR ASAA0580557Vane · dentedC-CHECK, LT WING NR 1 FLAP VANE IS DENTED. REMOVED DAMAGED SECTION. INSTALLED REPAIR FILLER AND DOUBLER. (K)SDR GTIA050285Unknown · unknownON RUNWAY CLEARED FOR TAKEOFF THE LT ENGINE WOULD NOT RESPOND TO THROTTLE ADVANCE THE LT ENGINE REMAINED AT IDLE POWER THEN SLOWLY WOUND DOWN TO 44 PERCENT N2, AIRCRAFT TAIL SWAP WITH 803NK. INSPECTED THROTTLE LINKAGE AT FUEL CONTROL. NO DEFECTS NOTED. INSPSDR GTIA050286Bleed Valve · malfunctionedLT ENGINE N2 DROPS BELOW 45 PERCENT WHEN LOAD APPLIED. REPLACED A/C WITH 832NK ON LINE. REMOVED NR1 ENGINE FUEL CONTROL. OPS AND LEAK CHECK GOOD. REMOVED AND REPLACED START BLEED CONTROL VALVE, PERFORMED IDLE CHECK, ENGINE ACCELERATION CHECK. OPS CHECK GOOSDR ASMF200512009Csd · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING LT ENGINE STARTING, THE LT CSD TEMPERATURE INCREASED AND WENT OUT OF RANGE AND LOAD AC WITH 7. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE LT CSD AND HEAT EXCHANGER AIR/OIL ASSY WERESDR ASMF200512011Engine · fodDURING TRANSIT CHECK, THE RT ENGINE BLADES FIRST STAGE WERE DETECTED WITH AND THE NOISE SUPPRESSOR HAD INCRUSTED A FOD. INSPECTION WAS PERFORMED, DETECTING 20 COMPRESSOR BLADES OF FIRST STAGE WITH DAMAGE OUT OF LIMITS IAW MM 72-00-00. AIRCRAFT WAS SENT TO THE SDR ASMF200512008Bungee Cylinder · leakingDURING TRANSIT CHECK, TECHNICAL PERSONNEL DETECTED A HYDRAULIC LIQUID LEAK IN THE RT MAIN LANDING GEAR. BUNGEE CYLINDER WAS REPLACED IAW MM 32-32-02, TESTED CORRECT.SDR GTIA050284Ahrs · malfunctionedAHARS NR2 CIRCUIT BREAKER POPPED, PFD AND ND OUT. AIRCRAFT TAIL SWAP WITH 808NK. REMOVED AND REPLACED NR2 AHRU. OPS CHECK GOOD. (K)SDR GTIA050283Landing Gear · vibrationAC SHIMMY VERY EXTREME ON LANDING ROLL OUT WHEN BRAKING BETWEEN 60-65 KTS, AC TAIL SWAP WITH 832NK. BLED ALL 4 BRAKES, CHECKED TORQUE VALUES OF ALL 4 MAIN TIRE AXLE NUTS. ALL CHECKED GOOD. NOTE: NR2 BRAKE AFT BLEEDER EMITTING AIR BUBBLES, PURGED AIR FROM SYSDR ASMF200512002Shutoff Valve · leakingAIRCRAFT RETURNED TO PLATFORM, DURING TAXING, THE RT PRESSURE AND QUANTITY HYDRAULIC SYSTEM WAS LOST. DURING MAINTENANCE REVISION, THE RUDDER SHUTOFF VALVE WAS LEAKED AND IT WAS REPLACED IAW MM 27-20-08, TESTED CORRECT.SDR ASMF200512001Hose · leakingDURING TRANSIT CHECK, THE LT HYDRAULIC BRAKE ACCUMULATOR HOSE WAS LEAKING. THE HOSE WAS REMOVED AND REPLACED BY FLEXIBLE HOSE IAW MM 32-42-04. THE LT HYDRAULIC BRAKE ACCUMULATOR FLEXIBLE HOSE WAS REPLACED BY ORIGINAL HOSE IAW MM 32-42-04, TESTED CORRECT.SDR ANCF200400062Engine · malfunctionedDURING TAKEOFF AND AFTER TAKEOFF THRUST WAS APPLIED, RT ENGINE ACCELERATION WAS VERY SLOW AND STOPPED AT 1.7 EPR. ACCELERATION TO 2 EPR WAS REACHED MOVING RT POWER LEVER MANUALLY. WHEN RT ENGINE REACHED 2 EPR N1 INDICATION STARTED FLASHING AND INDICATION WAS 1SDR GTIA050275Seat Track · corrodedRT OB SEAT TRACK FS 493 BOTTOM OF TRACK OUT OF LIMITS, CORROSION. REMOVED CORRODED SEAT TRACK SECTION, DRILLED NEW SEAT TRACK, FABRICATED SPLICE AND PLATE, TREATED, PRIMED AND INSTALLED REPAIR. (K)SDR GTIA050282Doubler · corrodedFWD SERVICE DOOR HAS CORROSION ON FLOOR WEB BETWEEN STA 1460 TO 218. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED DOUBLER AND FABRICATED NEW ONE, TREATED PRIMED AND INSTALLED REPAIR DOUBLER. (K)SDR ANCF200400063Engine · unknownDURING CRUISE FLIGHT AT FL 310, LT OIL PRESS LIGHT CAME (ON) ON EOAP. LT OIL PRESS INDICATION FELL TO 0 WITH (35) AND (40) LIGHTS ON. LT OIL QUANTITY WAS NORMAL INDICATING 16 QTS. LT OIL TEMPERATURE REACHED 131. LT ENGINE WAS SHUTDOWN, FOLLOWING THE CHECKLSDR GTIA050273Seat Track · corrodedSTA 1136, SEAT TRACK HAS CORROSION. FABRICATED, TREATED AND INSTALLED SECTION OF SEAT TRACK AT STA 1136. (K)SDR GTIA050278Floor Support · corrodedFLOOR SUPPORT AT STA 198 BETWEEN LT SEAT TRACKS IS CORRODED. REMOVED FLOOR SUPPORT, FABRICATED NEW SUPPORT TREATED AND PRIMED, INSTALLED REPAIR. (K)SDR GTIA050279Floor Support · corrodedFORE AND AFT FLOOR SUPPORTS AT STA 170-195 ON OB LT SEAT TRACK HAS SPOTS OF CORROSION ALONG LENGTH. REMOVED CORROSION ON SUPPORTS FOUND TO BE OUT OF LIMITS, FABRICATED NEW FLOOR SUPPORT ANGLE, TREATED PRIMED AND INSTALLED SUPPORT. (K)SDR GTIA050280Floor Support · corrodedFLOOR SUPPORT LBL 5, STA 195-200 HAS CORROSION ALONG LENGTH. REMOVED CORROSION AND FOUND ADDITIONAL CORROSION ON UNDERSIDE OF FLOOR SUPPORT TO BE OUT OF LIMITS, FABRICATED NEW SUPPORT, TREATED PRIMED AND INSTALLED NEW SUPPORT. (K)SDR GTIA050281Diaphragm · corrodedFWD GALLEY AFT CORNER IB HAS A 6 INCH HOLE CORRODED THROUGH SUBFLOOR WEB. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED DIAPHRAGM AND FABRICATED NEW DIAPHRAGM, TREATED PRIMED AND INSTALLED. (K)SDR AALA20050761Engine · failedINFLIGHT, SHORTLY AFTER LEVEL OFF AT FL320, RIGHT ENGINE FAILED. RIGHT HAND ENGINE OIL QUANTITY AND PRESSURE WERE NORMAL. EXHAUST GAS TEMPERATURE REACHED 800 DEGREES BEFORE SHUTDOWN. NO FIRE INDICATION OCCURRED. LANDED ORD WITHOUT INCIDENT. REPLACED NUMBESDR ASMF200511008Starter · failedAIRCRAFT RETURNED TO PLATFORM, RT ENGINE DID NOT START. DURING MAINTENANCE REVISION, IT WAS DETECTED THE RT ENGINE WITHOUT TURN IN N2. THE RT ENGINE STARTER WAS REPLACED IAW MM 80-10-01, TESTED CORRECT.SDR GTIA050277Angle · crackedANGLE IS CRCKED IN LT MLG WHEEL WELL FWD DOOR JAMB STRUCTURE STA 946. REMOVED CRACKED ANGLE, FORMED NEW ANGLE, TREATED PRIMED AND INSTALLED REPAIR. (K)SDR GTIA050271Windshield · leakingFRONT CENTER WINDSHIELD LEAKING WATER, AIRCRAFT TAIL SWAP WITH N808NK. WINDSHIELD SEALANT FOUND DELAPIDATED, RE SEALED WINDSHIELD, LEAK CHECKS GOOD. (K)SDR GTIA050276Pan · corrodedCORROSION AROUND CEILING PAN WHERE DRAIN GOES THROUGH AFT CARGO ABOVE STRINGER L-18 AT FS 1155. FABRICATED REPAIR FILLER AND DOUBLER, TREATED AND PRIMED FILLER AND DOUBLER, INSTALLED REPAIR AND NEW FLOOR SUPPORT BRACKET. (K)SDR GTIA050265Actuator · leakingRT MLG ACTUATOR SWIVEL GLAND LEAKING, AC TAIL SWAP WITH N815NK. RESEALED RT MLG ACTUATOR SWIVEL GLAND, NO LEAKS NOTED. (K)SDR ASAA0580534Skin · dentedLINE CHECK, FUSELAGE DENTED AFT OF L-1 (FWD PAX) DOOR. REMOVED DAMAGED SECTION SECTION. INSTALLED EXTERNAL DOUBLER WITH BLIND RIVETS IAW EA. (K)SDR ASAA0580535Skin · damagedSEA LINE CHK, FUSELAGE DAMAGED BY LIGHTNING STRIKE ON LT SIDE. REPAIRED IAW SRM AND EA.(K)SDR GTIA050268Pressure Blkhd · damagedTEAR ON AFT PRESSURE BULKHEAD IN NOSE WHEEL WELL, LOWER LT CORNER STA 110. REMOVED DAMAGED AREA, CLEANED SHARP EDGES, FAB FILLER AND DOUBLER FROM 7075-T6, TREATED PRIMED AND INSTALLED REPAIR IAW EA. (K)SDR GTIA050270Skin · damagedFUSELAGE SKIN DAMAGE AT FORWARD AND AFT LOWER CORNERS OF FORWARD GALLEY SERVICE DOOR CUTOUT. REMOVED DAMAGE AT FORWARD AND AFT LOWER CORNER OF GALLEY SERVICE DOOR CUTOUT IAW SRM, TREATED AND PRIMED AFFECTED AREA. (K)SDR GTIA050269Seat Track · crackedRT OB SEAT TRACK SWOLLEN AND CRACKED IN 2 PLACES AT APPROX FS465. CLEANED 2 SPOTS AND REMOVED SUSPECTED CRACK IAW SRM. PERFORMED HFEC OF RT OB SEAT TRACK AT FS 465 NO OTHER DEFECTS NOTED. PERFORMED ULTRASONIC THICKNESS OF SEAT TRACK WITHIN LIMITS, TREATED ASDR AALA20050698Engine · making metalBUF INFLIGHT T305/23OCT - RIGHT ENGINE WAS SHUT DOWN BY CREW DUE TO OIL FILTER CLOG LIGHT ILLUMINATING. FOUND METAL IN SCREEN AND FILTER AND OIL TANK. REPLACED ENGINE. FLIGHT DATA RECORDER DOWNLOAD REQUESTED BY ENGINEERING. SYSTEM GROUND CHECKED NORMAL OPSDR GTIA050263Frame · crackedL-2 DOOR FRAME IS CRACKED JUST BELOW BAYONET. INSTALLED SERVICEABLE DOOR AT L-2 POSITION IAW MM FOR ROG AND LEAK CHECK. (K)SDR DLM88050627Engine · failedNR 2 ENG FAILED DURING CLIMB-OUT AT 19,800 FT MSL, LOUD BANG, MODERATE VIBRATION FOLLOWED. REPLACED ENGINE.SDR DLM88050620Line · crackedLEFT HYD SYS PRESSURE AND QUANTITY DROPPED TO ZERO IN FLIGHT. REPLACED HYD SUPPLY LINE TO NUMBER 1 ENGINE HYD PUMP.SDR ASMF200510007Indicator · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT ENGINE EPR’S INDICATOR REMAINED ON 1.00 WHEN APPLYING TAKEOFF POWER. THE EPR INDICATOR WAS REPLACED IAW MM 77-11-02, TESTED CORRECT. DURING OVERNIGHT CHECK, THE LEFT ENGINE TRIM WAS PERFORMED IAW MM 71-0SDR GTIA050262Relay · malfunctionedDC BUSS (OFF) LIGHT ILLUMINATED DURING TAXI, LOAD METER NORMAL, AIRCRAFT TAIL SWAP 811NK. FOUND DC EMERGENCY POWER TRANSFER RELAY BAD, REMOVED AND REPLACED RELAY. OPS CHECK GOOD. (K)
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