Pratt & Whitney PW4062
Service difficulty reports · 206
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 = 'PW4062' 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 = 'PW4062' 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 HALA2012073100188Pump · leakingFOUND NR 1 ENG HYD PUMP LEAKING. R & R NR 1 HYD EDP IAW AMM 29-11-05, LEAK & OPS CHECKED OK.SDR HALA2012071800176Relief Valve · leakingRIGHT FUEL TANK QUANTITY DECREASED 1500 LBS DURING CLIMB WHILE BOTH CENTER TANK PUMPS ARE ON AND OPERATING. FOUND PRESSURE RELIEF VALVE LEAKING. REPLACED PRESSURE RELIEF VALVE IAW AMM 28-21-08. OK TO CLOSE RT MAIN TANK ACCESS DOOR 541HB. LEAK CHECK OF PANELSDR HALA2012071000170Bypass Valve · leakingAPU AUTO SHUTDOWN AT GATE. BITE APU IAW FIM HIGH OIL TEMP FAULT IAW FIM 49-11-00, FIG 110. NO OTHER FAULTS FOUND. IAW FIM REPLACED OIL COOLER BYPASS VALVE IAW AMM 49-27-10. LEAK CHECKED FAILED. REPLACED OIL COOLER BYPASS VALVE WITH ANOTHER NEW VALVE LEAKSDR HALA2012050900134Blade · damagedON WALKAROUND FOUND RT ENGINE NR 6 FAN BLADE HAS FOD DAMAGE, APPROXIMATELY TWELVE INCHES FROM BLADE ROOT (AREA F). BLENDED DAMAGED AREA WITHIN LIMITS IAW AMM 72-31-02, NO CRACKS NOTED ON EDDY CURRENT. OK FOR SERVICE.SDR HALA2012011900045Engine · malfunctionedETOPS SIGNIFICANT SYSTEM - LEFT ENGINE STARTED NORMALLY TILL 50 PERCENT, THEN REMAINED AT 50 PERCENT FOR 50 SECOUNDS BEFORE SLOWLY ACCELERATING - TOTAL TIME FROM FUEL ON TILL ENGINE STABLE TOOK 110 SECONDS, PEAK TEMP EGT WAS 397. TROUBLESHOT IAW FIM 73-21-00/SDR HALA2011112800546Eec · malfunctionedETOPS SIGNIFICANT SYSTEM - LEFT ENGINE EEC C1 STATUS MESSAGE DISPLAYED. BITE CHECKED PIMU & FOUND EEC CHANNELS A & B FMU CR- CHECK FAILED. TROUBLESHOT PER FIM. PIMU MESSAGE INDEX FOUND RESISTANCES WITHIN LIMITS OF FIM & PINS B,A,E,C,D DO NOT GO TO GROUND. SDR HALA2011113000512Engine · malfunctionedETOPS SIGNIFICANT SYS - LEFT ENGINE HESITATED AT 50 PERCENT N2 DURING ENGINE START AFTER START VALVE CLOSED AND STARTER CUTOUT WITH SELECTOR BACK IN AUTO. OTHER PARAMETERS NORMAL. GROUND RAN LT ENGINE, FOUND WITHIN LIMITS OF AMM 71-00-00. OK FOR SERVICE.SDR HALA2011102300484Warning System · false activationETOPS SIGNIFICANT SYS - EICAS STATUS MESSAGE LT ENG EEC C1 DISPLAYED ON LOWER EICAS. TROUBLE SHOT IAW FIM 73-21-00. PIMU CHECKED AND HAD RNG FAIL-CLEARED MESSAGE. RAN ENGINE, NO FAULTS ON PIMU OR EICAS-OK FOR SERVICE.SDR HALA2011101400458Carbon Seal · leakingETOPS SIGNIFICANT SYS - UPON ARRIVAL A SMALL AMOUNT OF OIL WAS NOTED LEAKING FROM COMPRESSOR SECTION ON NR1 ENG BEHIND FAN STAGE. NO OIL ADDED MX CONTROL ADVISED. OIL USAGE BELOW ETOPS LIMITS REF AMM 71-00-00-795-003-D-10, SMALL AMOUNTS OF OIL LEAKAGE PERMITSDR HALA2011092000413Oil System · leakingETOPS SIGNIFICAT SYS - ON CREW WALK AROUND FOUND RT ENGINE LEAKING OIL ON FAN BLADE. PERFORMED INSPECTION OF RT ENGINE FAN BLADE FOR OIL LEAK. LEAK WITHIN LIMIT. LEAK FROM WEEP LOCATION IAW FIM 71-08-00PB101, FIG 113, SHEET 113.SDR HALA2011092000414Oil System · leakingETOPS SIGNIFICANT SYS - ON CREW WALK AROUND FOUND OIL POOLING BEHIND NR 2 ENG N1 FAN BLADES. SYS OK IAW AM71-00-00-795-003-NOV00 OIL PUDDLE, OK FOR SVC.SDR HALA2011091700405Oil System · leakingETOPS SIGNIFICANT SYS - OIL FOUND IN LT ENGINE FAN COWL. OIL LEAKAGE BELOW IDLE SPEED IS WITHIN LIMITS IAW AMM 71-00-00-795-003-N00. OK FOR SERVICE.SDR HALA2011090800399Blade · bentETOPS SIGNIFICANT SYS - NR 2 ENGINE 1 FAN BLADE BENT ON L/E .3750" FROM TIP, 2" LONG. BEND IS .1250" IN DEFLECTION AFT. R & R NR 5 AND 24 FAN BLADE IAW AMM 72-31-02-004-001 N00. PERFORMED TEST 8 VIBRATION SURVEY IAW AMM 71-00-00-725-008-N00. NO TROUBLE FOUNSDR HALA2011082700390Latch · dirtyLEFT WING SLIDE EICAS MESSAGE ON TAKEOFF ROLL. PERFORMED HIGH ENERGY STOP INSP IAW AMM 05-51-14-212-089. ACCOMPLISHED FIM 52-71-00, FIG 107, BITE PESU OK. IAW FIM INDEX INSPECTED AND CLEARED BLOCKAGES ON OFF WING SLIDE COMPT, LATCHES. BITE PSEU AGAIN-NO DSDR HALA2011082500387Warning Light · illuminatedETOPS SIGNIFICANT SYS -ENROUTE STATUS MESSAGE "AFT EQ EXH FAN 1" DISPLAYED. ACCOMPLISHED FIM 21-26-00. NO MESSAGE DISPLAYED. OK FOR SERVICE.SDR HALA2011081400365B-Nut · looseETOPS SIGNIFICANT SYS - NR 1 ENG TOOK 6 PINT DURING SERVICING. TIGHTENED OIL INLET TUBE B-NUT IAW 79-21-01, LEAK CHECKED GOOD. (AT OIL COOLER) (ACFT M/M 79-21-011).SDR HALA2011080900356Seal · leakingETOPS SIGNIFICANT SYS - ON CREW WALKAROUND, FOUND RT ENG LEAKING OIL ON FAN BLADE IAW AMM 71-08-00-1, OIL LEAK WITHIN LIMITS FROM NR2 ENGINE. FRONT BEARING SEAL, MOC NOTIFIED.SDR HALA2011072400331Blade · damagedETOPS SIGNIFICANT SYS - RT ENG BLADE NR 36 HAS NICK ABOUT 4.5" FROM BLADE TIP. BLENDED RT ENG NR 36 BLADE IAW AMM 72-31-02. WITHIN LIMITS IAW AMM (AREA A). NO CRACKS NOTED DURING EDDY CURRENT INSP. OK FOR SVC.SDR HALA2011070800319Indicator · malfunctionedETOPS SIGNIFICANT SYS - UNABLE TO ALIGN NAV'S 3 ATTEMPTS. REALIGNED LT, CTR & RT IRU'S OPS CHECKED OK IAW FIM 34-21-00 FIG 105D.SDR HALA2011041900161Engine · slowETOPS SIGNIFICANT SYS - LT ENG SLOW TO ACCEL TO IDLE F/F AND DUCT PRESS WERE NORMAL. T/S IAW AMM 71-00-00-712-021-N00 - NO FAULTS ON PIMU BITS - RAN ENG, STARTED WITHIN 80 SEC - LIMITS IAW AMM 120 SEC OK FOR SERVICE.SDR HALA2011022100104Warning Message · false activationETOPS SIGNIFICANT SYS - ON ACFT ARRIVAL, FOUND ENG A/O VALVE & EEC C1 MESSAGE. REGARDING THE MESSAGE, PIMU BITE TEST CARRIED OUT IAW FIM 71-PIMU BITE PROCEDURE AND PIMU GROUND TEST CARRIED OUT IAW AMM 77-35-00. NO FAULT DETECTED AND FAULT MESSAGES ARE ERASEDSDR HALA2011021300091Oil System · leakingETOPS SIGNIFICANT SYS - ON WALKAROUND FOUND EVIDENCE OIL LEAK ON LOWER COWL AREA OF NR1 ENGINE. OPENED NR 1 ENG AND CLEANED, RAN NR 1 ENG AT IDLE POWER, NO LEAKS NOTED, OK FOR SERVICE.SDR HALA2011020600078Pump · leakingETOPS SIGNIFICANT SYS - HYD FLUID LEAKING FROM NR 1 ENG. R & R NR 1 ENG HYD PUMP IAW AMM29-11-05, OPS & LEAK CHECK GOOD.SDR HALA2011020600079Line · leakingETOPS SIGNIFICANT SYS - FOUND HYD FLUID LEAKING FROM AFT FLEX HYD SUPPLY LINE AT TOP OF ENG. SECURED AFT FLEX HYD SUPPLY LINE AT TOP OF ENG.SDR HALA2010121600586Trim System · slowETOPS SIGNIFNICANT SYS - RT RUDDER TRIM OPERATION SLOW OR UNRESPONSIVE SOMETIMES. NO MOVEMENT OR VERY SLOW OCCASIONALLY NORMAL PARKED AT GATE. PERFORMED FIM 27-21-00/ FIG 106 FOUND RUDDER TRIM CONTROLS TO OPERATE NORMAL, OK FOR CONT SERVICE.SDR HALA2010121600591Seal · tornOUT OF FL 340 EXPERIENCED LOUD AIR LEAK IN COCKPIT DIFFERIENTIAL PRESSURE WAS IN AT MAX. AIR LEAK SEEMED TO COME FROM F/O 2R OR 3R WINDOWS. PRESSURIZED ACFT ON GROUND, FOUND 2R WINDOW LEAKING. FOUND 2R WINDOW PRESSURE SEAL TORN AT TOP AFT CORNER. R & R 2R WISDR HALA2010121600592Warning Light · illuminatedETOPS SIGNIFICANT SYS - "L IRS FAULT" LGT ILLUMINATED AFTER TOUCHDOWN. RAN LT IRS SYS IAW AMM34-21-00, OPS CK GOOD.SDR UALA2010121304533Adc · faultyCAPTAIN ALT CONSTANTLY MOVES UP AND DOWN 60' AT CRUISE. ALSO TEMPORARILY WENT UP IN DESCENT. ALL FLIGHT CONTROLS FELT UNUSUALLY HEAVY ON FINAL AND LANDING. IAW CREW HEAVY FORCES WERE NOTICED ON AIL AND ELEV. LT ADC REPLACED. ACP BITE CHK OF ALL CSEU UNITSSDR HALA2010121200581Transceiver · malfunctionedETOPS SIGNIFICANT SYS - F/O HF RADIO WILL NOT TUNE. RERACKED BOTH HF XCVR. GND OPS CK OK 23-11-03.SDR HALA2010111500538Transmitter · malfunctionedETOPS SIGNIFICANT SYS - HF RADIO NR 2 WHEN TUNING TRANSMITTER, TUNING IS INTERMITTANT. SOMETIMES TUNING LASTS FOR 30 SEC OR RADIO DOES NOT TUNE AT ALL. IAW ACARS FROM FLT CREW, OPS CHECKED NORMAL. PEFORMED AMM 23-11-10 OPS TEST, NR2 HF RADIO OPS CHECKED NORSDR HALA2010111500540Wave Guide · splitETOPS SIGNIFICANT SYS - WEATHER RADAR WAVE GUIDE SPLITTING APART. REMOVED WX RADAR WAVE GUIDE FROM BULKHEAD IN RADOME TO WX RADAR ANT IAW AMM34-43-04. INSTALLED WAVEGUIDE FROM RADOME BULKHEAD TO ANTENNA & OPS CK OK IAW AMM34-43-04.SDR HALA2010111300539Indicator · failedETOPS SIGNIFICANT SYS - RT FUEL GAUGE FAILED ON FINAL APPROACH. PERFORMED FIM 28-41-00-1, FIG 110, IAW FIM, SYS IS OK, RT FUEL GAUGE DISPLAY NORMAL.SDR HALA2010110800523Light · illuminatedETOPS SIGNIFICANT SYS - RT GEN FIELD LIGHT IS ON. ACCOMPLISHED AMM 24-11-00, OPS CK.SDR HALA2010110800524Heat Exchanger · leakingETOPS SIGNIFICANT SYS - ON OVERNIGHT CHECK, FOUND NR2 ENG EVIDENCE OF OIL LEAK IN BYPASS AREA. REMOVED NR2 ENG AIR/OIL HEAT EXCHANGER AND VALVE ASSY IAW AMM 79-21-09 (HA11068), INSTALLED AIR/OIL HEAT EXCHANGER IAW AMM 79-21-09. OPS AND LEAK CHECK PENDING. GROSDR HALA2010102900504Intercostal · crackedINTERCOSTAL BS 742-764, LBL 39 CRACKED. INTERCOSTAL RELACED IAW SRM51-40-02, REV.84.SDR HALA2010102600494Generator · malfunctionedETOPS SIGNIFICANT SYS- RT GENENERATOR NEEDED TO BE RESET AFTER ENG START. ACCOMPLISHED RT ENGINE GENERATOR CHECK ON BPCU BITE. NO FAULTS NOTED RT. GENERATOR SYS CHECK GOOD IAW FIM 24-20-00 OK FOR SVC.SDR HALA2010102500490Stringer Splice · corrodedLEVEL 2 CORROSION ON STRINGER SPLICE AT BS 434, S18L. SPLICE R & R IAW SRM 51-40-02 REV 84 AND DWG 140T0115.SDR HALA2010102500491Stringer Splice · corrodedLEVEL 2 CORROSION ON STRINGER SPLICE AT BS 434, S17L. SPLICE REPLACED IAW SRM 51-40-02, REV 84 AND DWG 140T0115.SDR HALA2010101400465Transceiver · weakETOPS SIGNIFICANT SYS - NO DATA LINK FOR THE WHOLE FLIGHT WHILE IN HF. DATA WORKED IN VHF RANGE ONLY. FOUND RT AND LT HF FAULTING REF LOG PAGE 368301 ITEM NR15 FOR RT AND LT HF SIGN OFF. ASSURANCE CHECK FOR DATA LINK REQUIRED. FOUND LT HF TRANCEIVER WEAK REPSDR HALA2010101400467Starter · failedETOPS SIGNIFICANT SYS - APU FAILED TO START UPON ARRIVAL. APU ECU BITE IAW FIM 49-11-00. NO FAULTS, NO FLAGS. TRIED APU START ATTEMPT UNSUCCESSFUL, RPM ONLY 20 PERCENT. R & R APU START ASSY. OPS CK GOOD. AMM 49-41-01. SECURED APU DOOR. APU STARTED SUCCSDR HALA2010101400532Structure · corrodedGALLEY A1 UPPER AND LOWER UNITS HAVE NUMEROUS DEFECTS AND EXTENSIVE CORROSION IN EXTRUSIONS. EXTRUSIONS FABRICATED AND REPLACED IAW SELL CMM 25-38-73, REV 4, SRM 25-32-03 AND SRM D634T210 REV 84, AND AIR NZ TI190136349-0001, HAL M105 FILE NR 585167 TO UPPER FSDR HALA2010101300464Transceiver · weakETOPS SIGNIFICANT SYS - TRANSMISSION AND RECEPTION ON HF NR2 R WEAK. R & R RT HF TRANSCEIVER IAW AMM 23-11-03. OPS CK GOOD. FIM 23-11-00 ACCOMP, NO FAULTS NOTED. OK FOR SVC.SDR HALA2010101000461Relay · malfunctionedETOPS SIGNIFICANT SYS - L IDG VALVE ILLUMINATED ON STATUS PAGE. R & R RELAY K01033 IAW WDM 24-11-11. OPS CHECK OK IAW AMM 71-00-00.SDR HALA2010101000504Bracket · corrodedLEVEL 2 CORROSION FOUND ON BRACKET AT BS 544, S17R. FABRICATED REPLACEMENT BRACKET PN 143T8006-R, IAW DWG 143T8006, AND INSTALLED IAW SRM 51-40-02. CPC APPLIED.SDR HALA2010093000477Seat Track · corrodedLEVEL 2 CORROSION SEAT TRACK AT STA 1435, RBL 88.5 BEYOND LIMITS. SEAT TRACK REPLACED IAW SRM 51-40-02, REV. 84 AT RBL 88.5, STA 1324 - STA 1444. ALODINED, PRIMED, PAINTED, AND APPLIED CPC.SDR HALA2010092900447Seat Track · corrodedLEVEL 2 CORROSION AT SEAT TRACK LBL 88.5, STA.1370. SEAT TRACK SECTION PN 146T5215-3 FABRICATED IAW DWG 146T5215. SEAT TRACK INSTALLED IAW SRM 51-40-02, REV 84.SDR HALA2010092900446Seat Track · corrodedLEVEL 2 CORROSION ON END OF TRACK AT STA 346 LBL 88.5. REMOVED FABRICATED AND REPLACED TRACK IAW SRM 53-00-51-2R1, REPAIR 1.SDR HALA2010092100482Strap · corrodedLEVEL 2, CORROSION ON STRAP AT STA 927, S20R. REPLACED STRAP IAW SRM 51-40-02 REV.84 AT STA 927,S20R.SDR HALA2010092000426Warning Light · false activationETOPS SIGNIFICANT SYS - FMC LIGHT STAYED ON ENTIRE FLIGHT. FINALLY WENT OUT WHEN ENGINES SHUTDOWN AT GATE. INBOUND FLT CREW REPORTED NO FMC PROBLEMS DURING FLIGHT. DID MCDP LAST FLT AND PREVIOUS FLT FAULTS AND TEST 30 IAW FIM 22-00-03-1. NO FMC FAULTS. T/S SDR HALA2010092000483Mount · corrodedLEVEL 2 CORROSION ON GALLEY FEET MOUNTS AT STA 1588, LBL76,STA.1592 LBL45, AND RBL 45, STA.1614, RBL45. R & R FEET IAW SRM 51-10-02, REV 84.
Back to Pratt & Whitney PW4062