Pratt & Whitney JT8D-15
Service difficulty reports · 2,710
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 = 'JT8D15' 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 = 'JT8D15' 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 2001UALA00721Smoke · detectedFORWARD GALLEY HAS ELECTRICAL SMOKE AND SMELL. NOT ENOUGH INFORMATION TO DETERMINE CAUSE. FORWARD GALLEY HOT FOOD UNIT WAS DISCONNECTED AND REPLACED BY GATES GOURMET. NEW UNIT INSTALLED AND OPERATION CHECKS NORMAL.SDR 2001UALA00719Fire Warning · malfunctionedDURING CLIMB, THE FLIGHT CREW HEARD A FIRE WARNING BELL WITH NO INDICATION OF THE SOURCE. THE AIRCRAFT CONTINUED TO ORD. CREW REPORTED THAT ON CLIMBOUT THRU FL200, FIRE BELL SOUNDED WITH NO OTHER INDICATIONS. RESET SYS, TESTED ENG'S AND CARGO SYS'S, ALL TESTEDSDR 2001UALA00720Battery · dischargedRH OVER WING EMERGENCY EXIT SIGNS ARE INOPERABLE. BATTERY PACK AND CHARGER FAILED. REPLACED BATTERY PACK AND CHARGER.SDR 2001UALA00656Rib · crackedNR 6 SLAT ACTUATOR ATTACHMENT INBOARD AND OUTBOARD RIBS ARE CRACKED. REPAIRED ATTACHMENT RIBS PER SM-0R 70-57-56-01-AR5.SDR 2001UALA00652Window · crackedDURING CRUISE PASSENGER OUTER WINDOW PANE AT ROW 17 SHATTERED. AIRCRAFT DIVERTED TO SFO. *S/D* AN IMPROPER SEAL DURING INSTALLATION RESULTED IN FAILURE OF OUTER PANE. REPLACED ROW 17A OUTER AND MIDDLE WINDOW PANES PER MAINTENANCE MANUAL AND BOEING DRAWING SDR 2001UALA00653Indicator · failedLANDED UNDER AMBER ALERT DUE TO SPLIT TRAILING EDGE FLAP INDICATION. *S/D* THE FLAP POSITION INDICATOR FAILED. REMOVED AND REPLACED BOTH INBOARD AND OUTBOARD FLAP POSITION INDICATOR. CYCLED FLAPS SEVERAL TIMES, OPERATION CHECKS NORMAL.SDR 2001UALA00722Skin · damagedRT ELEVATOR UPPER SURFACE HAS SEVERAL LOOSE WORKING FASTENERS AT THE TRAILING EDGE JUST OUTBOARD OF THE ELEVATOR TAB. REPAIRED ELEVATOR PER SRM 55-20-03. WEIGHT OF REPAIR MATERIALS CALCULATED PER SRM 51-80-07, AND IS WITHIN LIMITS. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00654Controller · failedAUTO PRESSURIZATION FAILED DURING DESCENT.SDR 2001UALA00655Actuator · leakingDURING TAXI LOST HYDRAULIC SYSTEM-A. *S/D* LT NR 3 SLAT ACTUATOR WAS LEAKING. REMOVED AND REPLACED LT NR 3 SLAT ACTUATOR IN ACCORDANCE WITH MAINTENANCE MANUAL. OPERATIONAL CHECKS NORMAL.SDR 2001UALA00640Pump · failedAIRCRAFT DIVERTED TO MSP DUE TO NUMBER THREE ENGINE SHUTDOWN. *S/D* THE ENGINE DRIVEN FUEL PUMP LOST FUEL FLOW CAUSING THE ENGINE TO FLAME OUT. REPLACED THE FUEL CONTROL UNIT AND THE FUEL PUMP.SDR ABXA010212Engine · failedTHE RIGHT ENGINE (NR 2) EXPERIENCED AN UNCOMMANDED SHUT DOWN DURING THE LANDING FLARE. MAINTENANCE COMPLETED VISUAL INSPECTIONS OF THE INTAKE AND EXHAUST. NO DEFECTS WERE NOTED. THE RIGHT ENGINE FUEL FILTER WAS REPLACED AS A PRECAUTION. NO DEFECTS WERE NOTSDR 2001UALA00622Rib · damagedNR 6 SLAT INBOARD END DAMAGED REMOVED AND REPLACED RIB PER SRM 51-30-3SDR 2001UALA00617Frame · crackedFUSELAGE FRAME AT BS 420 IS CRACKED ALONG THE RADIUS BETWEEN STRINGER 20R AND 21R.. INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 AND 53-10-2 DUE TO SKIN CRACKINGSDR 2001UALA00618Shear Tie · corrodedFORWARD PIT STATION 580 BETWEEN STR 28L AND 28R FRAME SHEAR TIE CORRODED BEYOND LIMIIT. REPLACED SHEAR TIE.SDR 2001UALA00621Clip · crackedSTRINGER 21R CLIP CRACKED AND BUCKLED AT BS 460 ATTACHMENT. REPLACED STRINGER CLIP AT STRINGER 21R PER SRM 53-10-3SDR 2001UALA00619B-Nut · looseDURING TAKEOFF ROLL THERE WAS NO FIRST OFFICER''S AIRSPEED INDICATION. RETURNED TO BLOCKS FOUND LOOSE B-NUT ON PITOT AND STATIC LINE ON F/O AIRSPEED INDICATOR. TIGHTENED B-NUT AND PERFORMED A LOW LEVEL LEAK CHECK.SDR 2001UALA00628Indicator · failedABORTED TAKEOFF AT 80 KNOTS DUE TO FAILURE OF THE FIRST OFFICERS AIRSPEED INDICATOR.SDR 2001UALA00629Pump · failedAIRCRAFT RETURNED TO DEN DUE TO LOSS OF THE SECOND FUEL BOOST PUMP IN THE CENTER TANK. BOOST PUMP FAILED. REPLACED THE BOOST PUMP.SDR 2001UALA00606Controller · malfunctionedAIRCRAFT RETURNED TO DEN DUE TO PRESSURIZATION PROBLEM. CABIN PRESSURE CONTROLLER FAILED. REPLACED CONTROLLER.SDR 2001UALA00572Skin · damagedRT ELEVATOR OUTBOARD TRAILING EDGE HAS LIGHTNING DAMAGE. SKIN IS CRACKED, MELTED, PUNCTURED AND STATIC WICK IS MISSING. REPAIRED ELEVATOR PER SM OR 70-55-20-03-JD, AND INSTALLED REPAIR PER SRM 51-30-02. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00575Wire · shortedFIRST CLASS FLOOR EMERGENCY LIGHTS ARE INOPERABLE. *S/D* LIGHT ASSY CABLE SHORTED. TROUBLESHOT AND FOUND EEL STRIP SHORTED. REPLACED LIGHT ASSY CABLE.SDR 2001UALA00574Power Supply · inoperativeFUEL FLOW INDICATION FOR ALL ENGINES WENT TO ZERO TWICE IN FLIGHT. AIRCRAFT DIVERTED TO MCI. *S/D* THE CAUSE OF THE FUEL FLOW INDICATION TO READ ZERO IS THE FUEL FLOW POWER SUPPLY UNIT. THERE IS ONLY ONE POWER SUPPLY UNIT FOR ALL THREE INDICATORS. THE FUSDR 2001UALA00571Rib · crackedNR 3 SLAT ACTUATOR INBOARD RIB IS CRACKED. REPAIRED PER SM OR 70-57-56-01-AR5. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA00570Battery Pack · dischargedBOTH LT ESCAPE HATCH EMERGENCY EXIT SIGNS ARE INOPERABLE. *S/D* BATTERY PACK FAILED. REPLACED BATTERY PACK. OPERATIONS CHECK NORMAL.SDR 2001UALA00569Altimeter · fluctuatesCAPTAIN'S ALTIMETER FLUCTUATES INTERMITTENTLY -20 TO +40. SUPPLEMENTAL DATA UPDATE CAPTAIN'S ALTIMETER. REPLACE CAPTAIN'S ALTIMETER . OPS CHK NORMAL.SDR 2001UALA00568Bushing · wornAIRCRAFT RETURNED TO GSO DUE TO AIRFRAME VIBRATION. SUPPLEMENTAL DATA UPDATE UPPER RUDDER TRAILING EDGE PLAY OUT OF LIMIT. REPLACED BOLTS, AND BUSHING. RUDDER TRAILING EDGE PLAY WITHIN LIMIT.SDR 2001UALA00547Hydraulic Line · leakingCREW REPORTED THAT B HYDRAULIC SYSTEM QUANTITY READ ZERO. NO LOW PRESSURE LIGHTS ILLUMINATED. SUPPLEMENTAL DATA UPDATE REPLACED B SYSTEM HYDRAULIC TUBE ON FILTER MODULE. SERVICED HYDRAULIC SYSTEM. CHECKS OK.SDR 2001UALA00543Exhaust Pipe · crackedNR 1 ENGINE TAILPIPE CRACKED JUST AFT OF FORWARD FLANGE AT 9 O''CLOCK POSITION. *S/D* THE CAUSE OF THE CRACKING IS STILL UNDER INVESTIGATION WITH THE MANUFACTURE OF THE TAILPIPE. THE CORRECTIVE ACTION WAS THE REPLACEMENT OF THE TAILPIPE.SDR 2001UALA00520Clamp · leakingNR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON AFTER ENGINE WAS RUNNING FOR 4 MINUTES AT 1.90 EPR WITH BLEED OFF. LIGHT GOES OFF IF THROTTLE RETARDED TO 1.60. *S/D* THE 13TH STAGE PNEUMATIC DUCT WAS LEAKING AT A CLAMP. THE CLAMP WAS REPLACED AND ENGINE TESTED WISDR 2001UALA00521Exhaust Pipe · crackedNR 2 ENGINE EXHAUST TAILPIPE HAS A 16 INCH CRACK AT THE 6 OCLOCK POSITION NEAR THE ACOUSTIC PANEL. *S/D* THE CAUSE OF THE CRACKING IS STILL UNDER INVESTIGATION WITH THE MANUFACTURE OF THE TAILPIPE. THE TAILPIPES HAVE BEEN MODIFIED BY A STC FOR THE STAGE 3 HSDR 2001UALA00509Skin · damagedEXTERNAL FUSELAGE SKIN HAS EXCESSIVE MATERIAL REMOVED . STATION 219.818 INCHES BELOW STRINGER 25L. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED PER SAM 53-30-3, FIGURE 1.SDR 2001UALA00508Valve · failedNR 3 ENGINE STRUT OVERHEAT LIGHT CLIMBING THROUGH 8000 FEET FROM MIA. *S/D* REPLACED NR 3 13TH STAGE MOD VALVE. OPERATIONS CHECK NORMAL, NO FURTHER PROBLEMS REPORTED.SDR CA010504023Bracket · worn(CAN) CAREW REPORTED A VIBRATION IN CLIMB THRU 10,000 FEET THEN RECURRED ON DESCENT. AS THE AIRCRAFT DESCENDS BELOW 10,000 FEET. THE PROBLEM DID NOT OCCUR AFTER THE ELEVATOR TAIL HINE BRACKET WAS REPLACED.SDR 2001UALA00458Controller · malfunctionedAIRCRAFT RETURNED TO DEN DUE TO PRESSURIZATION PROBLEMS. SUPPLEMENTAL DATA UPDATE AIRCRAFT FAILED HULL LEAK CHECK.REPAIRED LEAKS AND TESTED OK PER MM 21-30-05.SDR 2001UALA00451Receiver · failedAIRCRAFT DIVERTED TO STL DUE TO NAVIGATION SYSTEM FAILURE IN ROUTE. STATIC WICKS AND NAV RECEIVER FAILED. FOUND TWO BAD STATIC DISCHARGE WICKS AND NR 1 VOR RECEIVER TO BE WEAK. REPLACED STATIC WICKS AND NR 1 VOR RECEIVER. SYSTEM CHECKS NORMAL PER MAINTENANCESDR COOSDR010005Skin · corrodedSECTION 43-STA720E+11/STA720D+3, S26R AND ST720E+5.25 S26L. INTERNAL FUSELAGE SKIN CORRODED.SDR COOSDR010006Floorbeam · corrodedMAIN CARGO CABIN BS 720A FLOOR BEAM UPPER CHORD CORRODED, BETWEEN RBL 60 INCHES AND LBL 60 INCHES, WL 208.SDR COOSDR010007Skin · corrodedLOWER FUSELAGE, SKIN CORRODED BETWEEN BS 117B TO BS 1183 BETWEEN STR 25L AND STR 26L.SDR COOSDR010008Stringer · crackedAFT CARGO COMPARTMENT, STRINGER 30 CRACKED AT BS 950.SDR COOSDR010009Floorbeam · corrodedMAIN CARGO CABIN, BS 950F, FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62 IN AND LBL 62 IN, WL 208.SDR COOSDR010010Floorbeam · corrodedMAIN CARGO CABIN BS 1030 FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62IN AND LBL 62 IN, WL 208.SDR COOSDR010011Floorbeam · corrodedMAIN CARGO CABIN BS 1110 FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 61 IN AND LBL 61 INCHES, WL 208.SDR COOSDR010012Floorbeam · corrodedMAIN CARGO CABIN BS 1130 FLOOR BEAM LOWER CHORD CORRODED, BETWEEN RBL 45 INCHES AND LBL 45 INCHES.SDR COOSDR010013Floorbeam · corrodedMAIN CARGO CABIN BS 950C FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62 IN AND LBL 62 IN.SDR COOSDR010014Floorbeam · corrodedMAIN CARGO CABIN BS 380 FLOORBEAM UPPER CHORD CORRODED, BETWEEN RBL 62 IN AND LBL 62 IN, WL 208.SDR COOSDR010015Floorbeam · corrodedMAIN CARGO CABIN BS 720D FLOORBEAM UPPER CHORD CORRODED, BETWEEN 45 IN AND LBL 60 IN, WL 208.SDR COOSDR010016Floorbeam · corrodedMAIN CARGO CABIN BS 1070, FLOORBEAM UPPER AND LOWER CHORD CORRODED, BETWEEN RBL 61 IN AND LBL 61 IN, WL 208.SDR COOSDR010018Skin · corrodedRT WING, LOWER SURFACE AT WS 320, STRINGER 8 SKIN CORRODED.SDR 2001UALA00430Controller · failedDURING DESCENT CABIN PRESSURE WAS ERRATIC. SUPPLEMENTAL DATA UPDATE SUSPECT CABIN PRESSURE CONTROLLER FAILED. REPLACED CABIN PRESSURE CONTROLLER.SDR 2001UALA00428Frame · crackedFUSELAGE FRAME BS 783 RT HAS A CRACK AT FIRST HOLE BELOW CABIN FLOOR LINE. INSTALLED DOUBLER AND ANGLE REPAIR PER SRM 53-11-05 AND MM 53-11-08. MAJOR REPAIR ACCOMPLISHED.
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