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 DL76P070498Actuator · activatedTHREE HOURS INTO FLIGHT, JUST PRIOR TO DESCENT. ATTEMPTED 3 APU START ATTEMPTS AT FL330. THE MAJORITY OF THE FLIGHT WAS FLOWN AT FL390. NONE OF THE ATTEMPTS WERE SUCCESSFUL WITH AN APU DOOR STATUS MSG ON EICAS ABOUT A MINUTE INTO EACH ATTEMPT. NO SSDR DL76L070479Engine · leakingDUE NUMBER 2 ENG EXCESSIVE HIGH OIL CONSUMPTION, PERFORMED EXT INSPECTION. NO OIL LEAK NOTED AFTER ENG RUN UP. AIRCRAFT POSITIONED FERRY TO ATL ON FLT 9903 DUE TO EXISTING PROBLEM WITH THE NR 3 BEARING LEAK INTO THE TAILPIPE. LEAK HAS PROGRESSED PAST OIL COSDR DL76P070497Actuator · inoperative3 APU START ATTEMPTS AT 39000/ 35000/ AND 23000 NO RPMS A APU DOOR STATUS MSG DISPLAYED APU INOP. FOUND APU DOOR ACTUATOR C/B POPPED. RESET C/B APU STARTED NORMAL.SDR 2007UALA01416Plate · crackedFWD PIT, FWD CARGO DOOR CUTOUT, LOWER MAIN SILL AREA, STA 642, UPPER BEAM CHORD PLATE HAS CRACK INDICATIONS, RBL 60. [SUP 06-01-07] VERIFIED CRACK INDICATIONS PER HFEC INSPECTION. FOUND SILL CRACKED APPROX. 4.5 INCHES LONG. REMOVED LOWER DOOR SILL AND REPLSDR 2007UALA01417Door Frame · puncturedAFT PIT DOOR CUTOUT FRAME AFT SIDE JUST UNDER THE APU BATTERY DOOR FRAME WEB PUNCTURED. MAJOR REPAIR ACCOMPLISHED: CUTOUT FRAME WEB DAMAGE. FABRICATED & INSTALLED DOUBLER, SHIMS & FILLER REPAIR.SDR 2007UALA01428Circuit Breaker · faultyTHE EVAC SIGNAL CIRCUIT BREAKER ON THE P6- 1 (F2) POPS WHEN THE EMERGENCY EVAC SWITCH IS HIT. [SUP 06-01-07] REPLACED EMER. EVAC MODULE AT AFT RT PANEL 22. OP CHECKS NORMALLY.SDR 2007UALA01429Hose · kinkedMAIN CABIN O2 MASK HOSES KINKED SEAT ROWS 2 CENTER, 1 EA 2 RT 1 EA 35 RT 1 EA 35 CENTER, 2 EA 1 EA AT 18C AND R, 29C AND R, AND 17C AND R. REPLACED MASKS WITH KINKED HOSES PER MM35-21-04. CLOSED PSU'S PER MM35-21-04. A/C READY FOR SERVICE. SUSPECT KINKING CASDR 2007UALA01430Light · brokenEEL LIGHT BAR AT THE AFT GALLEY AREA IS BROKEN. REPLACED LIGHT BAR. OPS CHECKS NORMAL.SDR 2007UALA01388Chiller · dirtySMOKE ODOR REPORTED IN BUSINESS CLASS GALLEY CHILLER AREA. [SUP 05-29-07] REPLACED AIR CHILLER AS PER AMM 25-33-04. CLEANED DIRTY VENTS. CHECKED OKAY FOR SERVICE. SUSPECT CHILLER MOTOR OVERHEATED AS VENT BECAME RESTRICTED BY DEBRIS.SDR 2007UALA01349Cable · out of positionEMERGENCY FLOOR LIGHTING STRIP NEAR 1B COMING UP. POSITIONED CABLE IN THE CORRECT PLACE.SDR 2007UALA01354Engine · surgesGROUP 3 SURGE ON TAKE OFF 1.33 EPR. PASSENGER COMFIRMED FLAMES FROM RT SIDE OF ACFT. ENGINE RECOVERED NO OTHER LIMITS EXCEEDED AND RESPONSE OK. SUPPLEMENTAL DATA UPDATE REPLACED #2 ENGINE. #2 ENG-RUN UP ENGINE PER AMM71-00-56-201 ACCT OF ENG REPLACEMENT. SDR 2007UALA01340Tail Cone · puncturedTAIL CONE 18 INCH PUNCTURE AT STA 1898. [SUP 05-16-07] MAJOR REPAIR ACCOMPLISHED: MANUFACTURED & INSTALLED STRUCTURAL FILLERS AND DOUBLER REPAIR.SDR 2007UALA01350Floorbeam · crackedSTA 246 FLOORBEAM LBL 11 AFT SIDE MID CHORD CRACKED AT LWR RADIUS NEAR FASTENER. MAJOR REPAIR ACCOMPLISHED: CUT OUT CHORD DAMAGE FROM LBL 59 TO RBL 49. FABRICATED & INSTALLED REPAIR ANGLE, STRAPS & MID CHORD.SDR 2007UALA01351Floorbeam · crackedSTA 246 FLOORBEAM UPPER WEB CRACKED OUT OF LWR FASTENER AT LBL 21. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED DOUBLER REPAIR.SDR 2007UALA01352Frame · corrodedAFT CARGO PIT FRAME UPPER CHORD CORRODED AROUND FASTENER HOLES STA 1197, LBL 42 TO RBL 42. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION. FABRICATED & INSTALLED ANGLE REPAIR.SDR 2007UALA01353Floorbeam · crackedMAIN CABIN FLOORBEAM INTERCOSTAL UPPER ANGLE CRACKED AT STA 337, LBL 41. MAJOR REPAIR ACCOMPLISHED: REMOVED CRACKED ANGLE. FABRICATED & INSTALLED NEW ANGLE.SDR 2007UALA01318Skin · crackedNR 2 ENG PYLON PNL CUT OUT CRACKED AT UPR FWD CORNER LOCATED ON I-B PYLON SKIN ACCESS HOLE CUT OUT JUST FWD OF HYD BAY. MAJOR REPAIR ACCOMPLISHED: STOP DRILLED CRACK. FABRICATED & INSTALLED DOUBLER REPAIRS.SDR 2007UALA01319Cable · disengagedLT AFT MED SLIDE RELEASE CABLE DISENGAGED. [SUP 05-18-07] RE-ENGAGED SLIDE RELEASE CABLE PER MM 25-66-00. READY FOR SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT CABLE DISENGAGED BY CONTACT WITH CABIN SERVICE EQUIPMENT DURING LOADING/UNLOADING.SDR 2007UALA01303Intercostal · crackedCABIN UNDER FLOORBOARD #P23, INTERCOSTAL UPPER ANGLE IS CRACKED AT STA 293, RBL 36. MAJOR REPAIR ACCOMPLISHED: REMOVED LINE REPAIR. FABRICATED & INSTALLED FILLER & EXTERNAL DOUBLER REPAIR.SDR 2007UALA01304Skin · damagedLIGHTNING STRIKE AT STA 760, BELOW STR 4L. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE. INSTALLED FILLER AND DOUBLER.SDR DL76L070362Engine · oil consumptionRT ENGINE HIGH OIL COMSUMPTION. REPLACED NR 2 ENG PER TRANS 1T149.SDR 2007UALA01271Engine · surgesNR 2 ENGINE SILENT SURGE. [SUP 05-18-07] REPLACED NR 2 ENG ELECTRONIC ENGINE CONTROL PER AMM 73 -21-04. RT ENG PIMU HAD 'EEC CH-A T29 RNG FAIL' REF SMC 2. REF LOG 1 DURING ENG RUN AFTER REPLACE OF EEC FOUND PIMU FAULT 'EEC CH-A T29 RNG FAIL'. REPLACED NR 2 SDR 2007UALA01265Seat Track · damagedCABIN SEAT TRACK AT BS 770 AND LBL 54 IS EXFOLIATED. MAJOR REPAIR ACCOMPLISHED: REMOVED CORROSION & DAMAGED SECTION OF SEAT TRACK. FABRICATED & INSTALLED SEAT TRACK SECTION, SPLICE PLATE & SPLICE CHANNEL.SDR 2007UALA01272Slide · out of limitsDOOR 1L SLIDE IS OUT OF LIMITS. [SUP 05-18-07] SLIDE SHOULD READ NO LESS THAN 2975 AT 70 DFG, IT IS CURRENTLY READING 2500. REPLACED SLIDE. A/C RETURNED TO SERVICE. SLIDE PROBLEM ROOT CAUSE: SUSPECT SEAL DETERIORATION AT FILL VALVE PRESSURE HOSE CONNECTIOSDR 2007UALA01248Support Bracket · crackedMAIN CABIN FLOOR BEAM INTERCOSTAL SUPPORT BRACKET CRACKED STA 1503, LBL 67. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED NEW BRACKET.SDR 2007UALA01285Engine · surgesNR 2 ENG SURGED DURING GROUND RUN FOR BLEED T-S. [SUP 05-18-07] ACCOMPLISHED NR 2 ENGINE VISUAL CHK. REPLACED IDG OIL AND SCAV. OIL FILTER. INSPECTED MAG CHIP DET. PER MM79-21-1 0 601. NR 2 ENGINE REQUIRES BORESCOPE PER TROUBLESHOOTING OF SMC2. BORESCOPED C5SDR 2007UALA01240Transformer · shortedELECTRICAL POWER PROBS CAUSED RTFL. REPLACED CURRENT TRANSFORMER T9000. REF WDM25-31-12, WDM25-31-13, WDM33-31-13 & WDM33-27-12. RELUGGED WIRE (32-16) AT C9010 W12 DUE TO HEAT DAMAGE. PERFORMED LOAD TEST AND LOAD SHED TEST OPS CHECKS NORMAL REF GNMM02-0-21SDR 2007UALA01231Slide · wrong partDOOR 1R SLIDE IS THE WRONG PART. [SUP 05-18-07] REPLACED DOOR 1R SLIDE ASSY PER AMM 25-66-01 WITH THE CORRECT SLIDE P/N. NEW SLIDE INSTALLED IS MR25708 (649-9059).SDR 2007UALA01216Generator · unknownCREW REPORTS LOSS OF LEFT GENERATOR. [SUP 05-04-07] REPLACED LEFT ENGINE INTEGRATED DRIVE GENERATOR. RAN UP ENG PER JRH 2-6-1, IDG OPERATED NORMALLY. OUTBOUND TRIP DID VERIFICATION TEST AND IDG OPERATED OK. SUSPECT INTERNAL WEAR LED TO FAULTY HERTZ OUTPUT SDR DL76L070366Acoustic Panel · crackedFOUND DURING HMV AT GSO, NR 1 ENG FAN COWL ACOUSTICAL PANEL HAS A CRACK INSIDE OF A DENT AT THE 4 O`CLOCK POSITION JUST FWD OF THE FAN BLADES. REPAIRED BY REMOVING CRACKED AREA AND POTTING AREA IAW B 767 SRM 51-00-01 REPAIR NR 1 ENGINE 201.SDR DL76L070367Acoustic Panel · delaminatedNR 2 ENGINE AFT ACOUSTIC PANEL AT APPROX 3:30 POSITION IS DELAMINATED. REPAIRED BY REMOVING DELAM AREA AND POTTING AREA IAW B767 - 300 SRM 54-00-01 REPAIR AND FIG 201. WORKED ON N/R20439 DURING HMV IN GSO.SDR 2007UALA01237Blades · damagedBIRD STRIKE TO NR 1 ENGINE. ACCOMPLISHED BOROSCOPE INSP OF NR 1 ENG HPC 5TH, 6TH, 10TH AND 11TH STG BLADES PER MM 72-00-00. FOUND 1 EA 6TH STG BLADE WITH LARGE TEAR IN AREA C OF L/E BEYOND FLYBACK LIMITS, 18 EA 10TH STG BLADES WITH DAMAGE BEYOND LIMITS IN ARSDR DL76G070328Actuator · leakingFLT 128/15 NOTIFIED MTC AT APPROX 2300E THAT RT SYS HYD WAS DOWN TO .43 AND FALLING. HAD CREW TURN OFF RT HYD AND FLUID LOSS STOPPED. CREW DECIDED TO DIVERT TO BOS. AFTER BOS MTC INSPECTED AIRCRAFT FOUND THE LEFT ELEVATOR-RT SYS PCA LEAKING HYD FLUID. REMOSDR DL76L070320Starter · sparksDURING TAXI AND START OF RT ENG, HAD NO ROTATION AND SPARKS FROM STARTER AREA AFTER START VALVE OPENED. STARTER FAILED AND ALSO DAMAGED THE START VALVE. REPLACED STARTER AND START VALVE.SDR DL76L070321Relay · unknownLT ENG EEC MODE STATUS. REPLACED K402 RELAY FOR THE LT ENG PROBE HEAT. RAN ENG, OP CKS GOOD.SDR DL76L070322Coffeemaker · smokeAFT COFFEE MAKER ON CAPT'S SIDE PRODUCED SMOKE WHEN TURNED ON. SMOKE QUIT WHEN COFFEE MAKER WAS TURNED OFF. CB'S WERE PULLED. RESET C/B FOR AFT COFFEE MAKER. MADE A POT OF COFFEE FROM EACH. ALL CKS OK. NO SMOKE NOTED AT ANY TIME.SDR DL76L070323Circuit Card · unknownAFTER STARTING, THE RIGHT CENTER PUMP PRESS LIGHT ILLUMINATED WITH THE RIGHT CTR PUMP ON. REMOVED AND REPLACED THE RT ENG SPEED CARD.SDR DL76L070325Engine · unknownL ENGINE WOULD NOT START. MANUAL OVERRIDE START PROCEDURE PERFORMED. FWD TO MCO PER MEL 80-00-02. CREW REPORTS GOOD START AT JFK. INSPECTED VLV AND CONNECTOR CHKS GOOD. RAN AND SPUN ENG SEVERAL TIMES CHKS OK MCO AND P REMOVED.SDR 2007UALA01181Unknown · odorON FINAL APPROACH, STRONGER ELECTRICAL ODOR RETURNED THROUGHOUT ACFT ALONG WITH HAZE IN CABIN. [SUP 05-04-07] REPLACED LEFT RECIRC FILTER AND LEFT RECIRC FAN. SMELL GONE A & NO HAZE. A/C RETURNED TO SERVICE. SUSPECT WEAR IN RECIRC FAN LED TO SHORT CIRCUISDR NOCA08307Fire Bottle · dischargedAPU FIRE BOTTLE ACCIDENTALLY DISCHARGED IN LEJ. REMOVED AND REPLACED APU FIRE BOTTLE IAW AMM 26-22-02. SYSTEM CHECKS NORMAL.SDR 2007UALA01182Indication Sys · malfunctionedRTFL DUE TO RIGHT AND CENTER HYDRAULIC SYSTEMS QUANTITY INDICATION PROBLEMS. [SUP 05-16-07] REPLACED HYD. QTY. MONITOR UNIT PER MM 29-33-01. OP CHECKS NORMALLY. A/C RETURNED TO SERVICE.SDR DLM88070318Battery · dischargedFWD O/WING EXITS INT EXIT SIGNS LIGHTS INOP. REPLACED BATTERIES IN CHARGER PACK.SDR HALA0700168Fan Blade · damagedNR 1 ENG 1ST STAGE FAN BLADE NR 8 HAS A NICK IN THE LEADING EDGE 17" FROM BLADE TIP 1/16" DP BY 1/8" WD. REPAIRED NR 8 FIRST STAGE FAN BLADE BY BLENDING PERAMM 72-31-02.SDR DL76G070317Projector · overheatedMID CABIN PROJ OVERHEATED WITH WHITE SMOKE AND ELECTRICAL ODOR. INSTALLED FWD VIDEO PROJ. MID PROJ PREVIOUSLY REPLACED WITH PROJ PER EA 01-461217-14, AND FWD POSITION EMPTY. MCO AND P REMOVED.SDR HALA0700164Pressure Switch · unknownETOPS SIGNIFICANT SYSTEM, "R. ENG FUEL FILT" DISPLAYED ON STATUS PAGE. T/S PER FIM 73-11-00 FIG 103, REPLACED FUEL FILTER PER AMM 73-11-02/401. FOUND FUEL FILTER CLEAN REPLACED DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-01/401, RAN ENGINE, NO MSG NO LEAKS NOSDR HALA0700159Guide Vane · missingETOPS SIGNIFICANT SYSTEM, LEFT ENGINE EXIT GUIDE VANE MISSING AT 1000 O'CLOCK POSITION. INFO NOTED, OK TO CONT PER AMM 72-33-02 TABLE 602 A MAXIMUM OF 3 GUIDE VANE CAN BE MISSING OK FOR SERVICE.SDR DL76L070308Oil Filter · unknownAFTER ENGINE START R OIL FILTER CAUTION AND R OIL FILTER STATUS MSG, OIL QTY INDICATED 2QTS, SHUTDOWN ENGINE. REPLACED RT ENGINE MAIN OIL FILTER PER AMM 79-21-05. RAN ENGINE. LEAK CHECK OK.SDR HALA0700157Fmu · malfunctionedETOPS SIGNIFICANT SYSTEM, ENG VALVE LIGHT ILLUMNIATED WITH FUEL CONTROL SWITCH IN RUN. T/S USING FIM 73 11 00 NO EICAS MSGS VERIFIED 28 VDC TO FMU SO SOLENOID WDM 76 11 11 BLK 41 REPLACE FMU BLK 3 VERIFIED 300 PSIG FUEL PRESSURE FIM 71 08 00FIG101 REMOVED ANDSDR 2007UALA01062Engine · oil consumptionNR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. [SUP 05-08-07] PRECAUTIONARY REPORT. NO OIL LEAKS DISCOVERED. SUSPECT OVER SERVICING.SDR ANCF200600050Servo · malfunctionedDURING DESCENT AT 15.000 FT, SPEED 290 EICAS MSG AUTOPILOT COME ON WITH CAUTION LIGHT, AUTOPILOT WAS DISENGAGED BY IT SELF. DURING APP THE ELEVATOR WAS VERY HARD TO OPERATE, BEING NECESSARY, EXCESSIVE FORCE CONTROL BY THE PILOT. PILOT FLYING. DURING FLARE TH
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