Pratt & Whitney PW4060
Service difficulty reports · 7,186
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 = 'PW4060' 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 = 'PW4060' 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 DL76L010540Engine · malfunctionedON T/O GOT RT HP BLEED AND FOLLOWED POM. RETURNED TO CVG. REPLACED NBR 2 ENG HPSO VALVE PER MM 36-11-07-4-03 NO FURTHER FAULTS.SDR DL76L010542Wire · brokenRIGHT ENGINE HPSOV ON TAKEOFF ROLL, RETURN TO CVG. . REPAIRED BROKEN WIRE ON D4208P RAN ENGINE LEAK AND OPS CHECKS GOOD.SDR 2001UALA00333Motor · failedBOTH PRESSURE CONTROLLERS FAILED. DESCENDED TO FL180. OPERATED NORMALLY IN MAN MODE. *S/D* 3/27/01 AT LHR, AUTO PRESS SYSTEM NR 2 WAS DEFERRED INOP. ACFT FLEW TO ORD WITH NO PRESSURIZATION FAULTS. DURING ORD-IAD LEG, FLIGHT CREW REPORTED FAILURE OF BOTH SDR TWAA0105101Chip Detector · detachedTHE NUMBER 1 ENGINE EXPERIENCED AN OIL QUANTITY AND PRESSURE LOSS. ENGINE WAS SHUT DOWN AND FLIGHT LANDED AT IAD. THE CHIP DETECTOR FOR THE 1, 1.5, AND 2 BEARINGS WAS FOUND LAYING IN THE COWLING. THE ANGLE GEARBOX CHIP DETECTOR WAS NOT LOCKED IN PLACE. INSSDR 2001UALA00262Light · damagedLT EMERGENCY EXIT LIGHTING (EEL) IN FIRST CLASS IS DAMAGED.SDR 2001UALA00246Web · crackedNR 1 PYLON WEB CRACKED AT OUTBOARD DRAIN HOLE JUST FORWARD OF IDG CUTOUT INSIDE PANEL 441DT. INSTALLED REPAIR DOUBLER REF: SRM 54-53-02.SDR 2001UALA00250Web · crackedNR 1 PYLON UPPER WEB AT IDG CABLE HOLE ACCESS HAS 2 CRACKS AT NP HOLES. INSTALLED REPAIR DOUBLER REF: SRM 54-53-02.SDR 2001UALA00251Web · crackedNR 2 PYLON UPPER WEB AT IDG CABLE HOLE ACCESS HAS TO CRACKS. INSTALLED REPAIR DOUBLER REF: 54-53-02.SDR 2001UALA00252Web · corrodedAFT PIT BS 1280 RBL 18 FLOOR WEB CORRODED. INSTALLED REPAIR DOUBLER REF: SRM 51-70-13 FIGURE 01.SDR DL76L010382Pump · looseA/C DIV SNN DUE FUEL QTY DISCREPANCY BETWEEN FUEL TOTALIZER AND FMS FUEL REALITY. INCREASE THROUGH OUT FLT ACCOMPANIED BY INCREASING FUEL IMBALANCE WITH EXCESSIVE CONSUMPTION FROM RT WING. FOUND 2 EA FASTENER LOOSE AT FUEL PUMP FLANG FITTING AFT LINE TO FUEL SDR 2001UALA00190Frame · corrodedAFT CARGO PIT AT BS 1197 +132 AT LBL 22-26, FRAME T-CAP IS CORRODED. REPLACED T-CAP PER BAC DWG 146T1060 AND INSTALLED PER SRM53-00-07, FIG 101.SDR 2001UALA00142Ground Wire · damagedAPU BATTERY GROUND GD3072DC OVERHEATED. INSULATION BLANKETS HEAT DAMAGED. *S/D* ACCOMPLISHED DETAILED VISUAL INSPECTION OF ALL EFFECTED WIRE BUNDLES AND INSTALLATIONS LOCATED IN E6-1 SHELF AND P49 PANEL. ALL WIRING CHECKED OK, EXCEPT APU BATTERY GROUND WIRSDR 2001UALA00125Angle · crackedMAIN CABIN BS 860 - 870 LBL 89 FLOORBEAM L-ANGLE BETWEEN UPPER CHORD TO SEAT TRACK CRACKED. C-CHECK. REPLACED L-ANGLE, REF SRM 51-40-02 FOR FASTENER INSTALLATION PROCEDURES.SDR 2001UALA00115Skin · dentedEXTERIOR FUSELAGE SKIN DENT STATION 445, BETWEEN STRINGERS 24L AND 26L. *S/D* SKIN REPAIR PER SRM 53-00-01 FIGURE 206 WAS ACCOMPLISHED AT OSV TIMCO.SDR 2001UALA00094Handle · stuckUNABLE TO RAISE GEAR HANDLE WITHOUT USING OVERRIDE.SDR 2001UALA00095Circuit Board · failedON DEPARTURE FROM SFO AT APPROX 1500 FT FORWARD CARGO DOOR EICAS MESSAGE ILLUMINATED. WENT OFF AFTER APPROX FIVE MINUTES. DID NOT CHECK CARGO LIGHTS. *S/D* REPEAT NUISANCE MESSAGE WAS CORRECTED BY VERIFYING ADJUSTMENT OF FORWARD CARGO DOOR LOCK SENSOR, CLOSDR 2001UALA00136Frame · corrodedAFT CARGO PIT AT BS 1197 AT LBL 5 - 26 FRAME T-CAP HAS AREAS OF CORROSION. REPLACED T-CAP PER SRM.SDR DL76L010185Engine · failedAT 400 FT RIGHT ENGINE COMPRESSOR STALL. BOTH TOWER AND PASSENGERS REPORTED SMOKE FROM RIGHT ENGINE. THROTTLE RETARDED TO IDLE AND RETURNED FOR LANDING IN SFO. REPLACED ENGINE.SDR ANCF200100006Hose · leakingDURING CLIMB, PASSING 25,000 FT, THE STANDBY ALTIMETER SHOWED 17,000 FT AND THE AIRSPEED INDICATORS SHOWED 320 KNTS WHILE THE STANDBY AIRSPEED INDICATOR SHOWED 220 KNTS. WITH 28,000 FT IN THE CAPTAIN AND F/O ALTIMETER THE STANDBY ALTIMETER SHOWED 18,000 FT. SDR 2001UALA00069Idg · contaminatedLEFT AND RIGHT IDG AND STARTER OIL FOUND CONTAMINATED.SDR CA010301019Window · failed(CAN) ON CLIMBOUT A VERY LOUD SQUEAL FROM VICINITY OF CAPTS SLIDING WINDOW. FLIGHT RETURNED. INVESTIGATION FOUND A LOOSE DUCT IN LEFT TUNNEL OF THE AVIONICS COMPARTMENT. DUCTING REPOSITIONED AND SECURED. FLIGHT DEPARTED. ON CLIMBOUT AGAIN EXCESSIVE NOISE FROM SDR DL76L010153Engine · stalledRT ENG AUDIBLE STALL ON T/O AT MAD. ACFT ATB. ENG WAS NOT SHUTDOWN IN FLIGHT. ENGINE TO BE REPLACED AT MAD.SDR DLM11010105Blade · failedNR 3 ENG COMPRESSOR STALL AND PERFORMED REJECTED T/O AT APPROX 160. ENGINE SHUT DOWN BY FLT CREW. BLADE FAILED. POSSIBLY DUE TO SOFT FOD.SDR 2001UALA00042Battery Pack · inoperativeEMERGENCY LIGHTING INOP FIRST CLASS, LEFT RIGHT AND CROSS AISLE. *S/D* BATTERY PACK REPLACED FOR LT EEL LIGHTS. REPLACED POWER SUPPLY STRIP FOR RT F/C EEL AND ACCOMPLISHED PERMANENT REPAIR OF EEL STRIP.SDR 2001UALA00044Battery Pack · dischargedRIGHT OVERWING EXIT LOWER EEL EXIT SIGN COMES ON AND OFF BY ITSELF. *S/D* REPLACED BATTERY PACK, OPS CHECK GOOD.SDR CA010308004Bolt · sheared(CAN) ONE BOLT FOUND SHEARED ATTACHING WHEEL HUN HALVES OF NR 3 MAIN WHEEL TIRE ASSEMBLE. MAIN WHEEL TIRE ASSEMBLE REPLACED AS PER MAINTENANCE MANUAL TASK 32-45-08-400.SDR ANCF200100003Computer · looseDURING TAKE OFF ROLL CAPT'S ADI AND HSI SCREENS WENT BLANK WHEN AIRCRAFT ROLLED OVER IRREGULARITIES ON RUNWAY, DURING TAXI BACK TO GATE INSTRUMENTS WENT BACK TO NORMALCORRECTIVE ACTIONTHE EICAS COMPUTER AND LH SYMBOL GENERATOR WERE ADJUSTED ON RACK, ALSO WERE SDR 2000UALA00823Controller · inoperativeRUDDER TRIM INOP. JETISONED FUEL, RTF.SDR 2000UALA00802Warning System · activatedRTF GSO WITH LEFT ENGINE FUEL FILTER INDICATION. NORMAL LANDING. NO EMERGENCY DECLARED.SDR CA010105004Control Unit · failed(CAN) DURING CRUISE, FL350, CENTER HYDRAULIC QUANTITY EICAS WARNING ILLUMINATED. HYDRAULIC QUANTITY ON STATUS PAGE INDICATED IT WAS 0.40. CENTER HYDRAULIC PUMPS WERE SHUTDOWN FOR REMAINDER OF FLIGHT. YVR ATC ADVISED AND AN EMERGENCY WAS DECLARED. LANDED AT YVRSDR DL76L002514Cover · missingON ARRIVAL MCO FOUND OIL DRIPPING FROM ENGINE. FURTHER INSPECTION FOUND N2 MANUAL CRANK PAD COVER MISSING. REPLACED PAD COVER.SDR 2000UALA00778Oil System · dryNR 2 ENGINE OIL QUANTITY WENT TO ZERO DURING CRUISE.SDR 2000UALA00770Oven · fireFIRE IN MID GALLEY OVEN, LOCATION R31 RECON-OVEN. HAND HELD EXTINGUISHER USED. DIVERTED PHL. OVERWEIGHT LANDING. *S/D* FOUND PAPER BURNED BETWEEN TOP OF OVEN RACK AND EXHAUST FAN OPENING. THE OVEN WAS REMOVED AND THE ELECTRICAL CONNECTORS WERE INSPECTED.SDR 2000UALA00704Battery Pack · failedEMERGENCY LIGHTS AT ROWS 20 - 26 ON THE RIGHT SIDE ON INTERMITTENTLY. SUPPLEMENTAL DATA UPDATE REPLACED BATTERY PACK PER MM33-51-07. TESTED GOOD.SDR 2000UALA00702Engine · leakingON ROLLOUT, FLIGHT ATTENDANTS IN MID SECTION SMELLED SMOKE IN GALLEY / LAVATORY AREA. AIRCRAFT RETURNED TO FIELD. SUPPLEMENTAL DATA UPDATE CHECKED CARBON FILTERS IN FWD CARGO PIT AND MIXER AREA, NO FAULTS NOTED. ACCOMPLISHED HIGH POWER ENGINE RUN AND NO SMOSDR CA001212013Fcu · failed(CAN) ON APPROACH AT SPEED 170K, SELECTED FLAPS FROM 20 TO 25, FLAPS STOPPED AT 23 DEGREES, CAUTION LIGHT TRAILING EDGE FLAP DISAGREE. GO AROUND CARRIED OUT. CHANGED FLAP SLAT ELECTRONIC CONTROL UNIT (FSCU). OPERATION CHECK NORMAL.SDR 2000UALA00662Oven · dirtyAFTER T-O GALLEY PWR TURNED ON AT MID GALLEY AND ELECTRICAL ODOR SMELLED. NO SMOKE NOTED. CIRCUIT BREAKER U-6 PULLED. SUPPLEMENTAL DATA UPDATE AFTER CIRCUIT BREAKER U-6 WAS PULLED, THE ODOR DISSIPATED. CREW REPORTED THE ODOR ONLY DURING THE OPENING OF THE SDR 2000UALA00651Charger · inoperativeEMERGENCY EXIT SIGN LIGHTS AT DOOR 2R AND 2L ARE INOP. *S/D* REPLACED EXIT SIGN LIGHTS BATTERY CHARGER FOR EXIT SIGN 2L AND 2R, PER MM 33-51-07, OP CHECK OK.SDR CA001129033Inverter · failed(CAN) CREW REPORT OF BURNING SMELL/SMOKE IN COCKPIT, STANDBY POWER INVERTER MESSAGE CAME ON ENGINE INDICATING AND CREW ALERT SYSTEM.CIRCUIT BREAKER PULLED FOR STANDBY INVERTER AND BEGAN SMOKE EVACUATION PROCEDURE. WHEN SWITCHES TO NORMAL, SMELL RETURNED. AIRCRSDR 2000UALA00649Light · inoperativeEMERGENCY EEL STRIP LIGHTING ON AT ROWS 20 TO 28 RIGHT SIDE. REMOVED AND RECONNECTED, COMES ON WITH SWITCH. WATCHED FOR 10 MINUTES DID NOT COME ON, WHEN ON GROUND.SDR 2000UALA00629Rudder · bindingRUDDER BINDING.SDR 2000UALA00628Relay · failedEICAS MSG FWD EQPT VAL DISPLAYED.EQUIPMENT COOLING ''VALVE'' LIGHT ILLUMINATED. STBY SELECTED & VALVE LIGHT REMAINED. DUMPED 35.8 FUEL. DIVERTED MIA SUPPLEMENTAL DATA UPDATE RELAY K1043 AIR/GROUND WAS FOUND STUCK IN THE GROUND POSITION. WHEN RELAY WAS REMSDR 2000UALA00611Squib · will not testLEFT WING EMERGENCY EXIT SQUIB WILL NOT TEST.SDR 2000UALA00612Switch · malfunctionedALL SEAT BELT AND ALL LAV RETURN TO SEAT LIGHTS STAY ON WITH SEAT BELT SWITCH IN AUTO, AND FLAPS AND GEAR UP. *S/D* ISOLATED PROBLEM TO ALT PRESSURE SWITCH S467. REPLACED SWITCH, GROUND OPS CK SYSTEM NORMAL PER MM 33-24-00.SDR 2000UALA00605Video Unit · damagedSLIGHT ELECTICAL ODOR ABOUT ROW 18. *S/D* REPLACE UNDER SEAT VIDEO BOX AT SEAT 17AB. SHOP FOUND LEAKING CAPACITORS FOR THE POWER SUPPLY IN THE VIDEO DISTRIBUTION BOX, CAUSING C12 AND L3 TO SHORT OUT.SDR DL76P001987Chip Detector · leakingON T/O AT 3000 FT MSL, LT ENG OIL PRESS DROPPED TO RED BOX, OIL QTY WENT TO ZERO. FOUND LEAK AT OIL TANK CHIP DETECTOR. REPLACED ENGINE.SDR DL76L001869Wire · chafedLEFT PRV EICAS MSG AT 80 KTS. TAKEOFF DISCONTINUED. REPAIRED CHAFED WIRING TO TERM 3 OF PRV AND REPLACED TERM 1 TO PRV. ALSO REPLACED PRV. PERFORMED HI-PWR RUNUP. NOTE; PRV CONTROLLER ALSO REPLACED IN COURSE OF T/S.SDR DL76L001883Engine · malfunctionedHIGH OIL CONSUMPTION HISTORY ON NUMBER 1 ENGINE. NUMEROUS ATTEMPTS TO CORRECT HAVE NOT YIELDED SATISFACTORY RESULTS. REPLACED ENGINE.SDR 2000UALA00558Engine · leakingNR 2 ENGINE OIL QTY DECREASED TO 0 IN FLIGHT OIL TEMP & PRESSURE OK. LOGBOOK READS LOST 2 QTS AN HOUR, THE LAST 2.5 HOURS OF FLT. ON DESCENT WITH THROTTLES RETARDED OIL TEMP BEGAN TO RISE AND ENGINE VIBRATION WAS AT 1.7. AFTER ENGINE SHUTDOWN AT THE GATE OILSDR 2000UALA00479Video Unit · odorON FINAL DESCENT, FLT ATT REPORTED ELECTRICAL SMELLORIGINATING FROM ROWS 6, 7 & 8 SEATS E & F. *S/D* REPLACED VIDEO DISPLAY UNITS (VDU) AT SEATS 7 E & F, REPLACED VIDEO DISPLAY BOX (VDB) AND SEAT CABLE AT SEAT 7E. SHOP FOUND VDB POWER SUPPLY BAD, C6 AND C7
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