Pratt & Whitney PW4158

Service difficulty reports · 689

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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 = 'PW4158'
  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.

SDR 06FDEA03634Module · malfunctionedF/O'S PFD AIRSPEED LAGGED CAPT. PFD AND BOTH STBY AIRSPEED GAUGES BY 40 KTS, THEN STOPPED INCREASING AT 200 KIAS, LATER CAPT PFD AIRSPEED READ 300 KIAS, F/O' PFD AIRSPEED READ 200. FACT 13OCT06 06:02 ORD R REPLACED F/O ADC AND CHECK PER MM 34-11-34-4 Oct 13, 2006 · N720FD · Airbus A300F4622R · Pitot/Static SystemSDR UPS06148224Indication Sys · malfunctionedLANDING GEAR SYSTEM 1 AND 2 SHOWS BOTH RED AND GREEN LIGHTS. THE CREW INFORMED FLT CONTROL OF POSSIBLE GEAR DOWN INDICATION PROBLEM AND DECLARED AN EMERGENCY. THE FLT LANDED SHORTLY AFTER THAT WITH NO FURTHER INCIDENT. R&R LANDING GEAR CONTROL MODULE IAW MM Oct 11, 2006 · N171UP · Airbus A300F4622R · Landing Gear Position and WarningSDR 06FDEA03265Engine · smokeON CLIMBOUT DEPARTURE CONTROL INFORMED US THAT TOWER SAID WE WERE EMITTING BLACK SMOKE OUT OF NR 1 ENGINE. ALL ENGINE PARAMETERS INDICATED NORMAL. ELECTED TO MAKE A PRECAUTIONARY LANDING. PER CREW DEBRIEF- CAPT REPORTED ALL NORMAL INDICATIONS, ON INBND LEGSep 12, 2006 · N719FD · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR UPS06147833Compressor · stalledINSPECTION TYPE: N/A AIR DIVERT, INITIAL DESCENT COMPRESSOR STALL WITH NO SECONDARIES. ON SUBSEQUENT DESCENTS NUMEROUS COMPRESSOR STALLS ON NR 1 ENGINE. NO FLUCTUATIONS ON ANY OF THE ENGINE INSTRUMENTS. PERFORMED ENGINE STALL PROCEDURES. DECLARED EMERGENCY BECAug 29, 2006 · N150UP · Airbus A300F4622R · Turbine Engine Compressor SectionSDR 06FDEA3002Engine · smokeAIR TURN BACK, AFTER TOWER REPORTED HEAVY SMOKE OUT OF THE RIGHT ENGINE. DECLARED EMERGENCY AND RETURNED TO LAND. THE ENGINE INSTRUMENTS APPEARED NORMAL. NORMAL LANDING AT 284000 LBS (NOT OVERWEIGHT. OBSERVED ON LANDING NO SMOKE NOTED. ON TAXI IN TO GATE,Aug 17, 2006 · N728FD · Airbus A300B4622R · Engine (Turbine/Turboprop)SDR UPS06146089Flap System · failedON APPROACH TO CGN, FLAPS W/N EXTEND PAST 15. A/C DIVERTED. EMERGENCY DECLARED. UPON APPRIVAL AT EDDK THE SLATS EXTENDED FULLY AND THE FLAP GAUGE INDICATED LESS THAN 15 FLAPS. WE SEQUENCED THE FLAP HANDLE THROUGH AGAIN GETTING THE SAME INDICATIONS. ON APPROACHFeb 1, 2006 · N155UP · Airbus A300F4622R · Trailing Edge Flap Control SystemSDR UPS06146047Curtain · tornFWD BARRIER CURTAIN IN LWR CARGO BULK COMPARTMENT IS BADLY TORN. REMOVED AND REPLACED BULK COMPARTMENT BARRIER CURTAIN.Jan 25, 2006 · N143UP · Airbus A300F4622R · Cargo CompartmentsSDR UPS06146046Slide · will not armESCAPE SLIDE ON CABIN DOOR WILL NOT MOVE TO THE ARMED POSITION. REMOVED AND REINSTALLED GIRT BAR IAW MM 25-61-21-4. SLIDE ARM AND DISARM OPERATION GOOD. THIS CLEARS M318706.Jan 24, 2006 · N150UP · Airbus A300F4622R · Escape SlideSDR UPS06146035Shear Plate · crackedMAIN CABIN FR 79 RT, CRACK IN INTERCOSTAL. REMOVED AND REPLACED INTERCOSTAL AT FR 79 RT IAW SRM 51-40-00.Jan 10, 2006 · N139UP · Airbus A300F4622R · Fuselage Main, StructureSDR UPS06146036Crossbeam · crackedMAIN CABIN FLOOR CROSSBEAM AT FR 51 BETWEEN SEAT TRACKS 1 AND 2 RT IS CRACKED. REMOVED AND REPLACED CROSSBEAM AT FR 51 BETWEEN SEAT TRACK 1 AND 2 RT IAW SRM 51-40-00.Jan 9, 2006 · N139UP · Airbus A300F4622R · Fuselage Main, StructureSDR UPS06145909Windshield · crackedFO'S WINDSHIELD CRACKED. R&R'D F/O WINDSHIELD WITH REF TO MM 56-11-11-4. OPS CKS OK.Jan 4, 2006 · N122UP · Airbus A300F4622R · Flight Compartment WindowsSDR UPS06146038Support Channel · crackedSUPPORT CHANNEL CRACKED APPROX 1.5 INCHES ON AFT CARGO COMPT LT SIDE STA 3354. REMOVED AND REPLACED SUPPORT CHANNEL IAW SRM 51-40-00.Jan 3, 2006 · N139UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR UPS06146000Structure · cracked5YR N2 ENG AFT LWR PYLON MEMBER SECTION IS CRACKED IN 2 EA PLACES RT AND LT AT JOGGLE. REMOVED AND REPLACED RT AND LT MEMBER SECTIONS IAW SRM 51-40-00.Dec 28, 2005 · N137UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR UPS05145893Hydraulic Line · leakingNOTED HYDRAULIC FLUID COMING OUT OF LT PYLON, DRY MOTORED ENG TO PIN POINT PROPER PANEL TO REMOVED LT AFT PYLON OB ENG PANEL AFTER REMOVAL FOUND HARD LINE CHAFFED ON BRADED LINK HARDLINE HAS FAILED AND CAUSED LEAK. REPLACED FLEX LINE WITH PERM RIGID HYDRAULICDec 23, 2005 · N129UP · Airbus A300F4622R · Hydraulic System, MainSDR 05FDEA03492Indicator · inaccurateDURING TAKEOFF ROLL, NR 2 PRIMARY AIRSPEED INDICATOR CONTINUED TO INDICATE 30 KIAS WHILE NR 1 INDICATED 80 KIAS. TAKEOFF ABORTED AT 90 KIAS. ENT BY: 275418 RPT BY: 056042 FACT 25OCT05 06:18 ONT R AS PRECAUTIONARY USING DRY NITROGEN BLEW OUT NR 2 PITOT Oct 25, 2005 · N718FD · Airbus A300F4605R · Altimeter, Barometric/EncoderSDR 05FDEA02580Fuel Control · fluctuatesON INITIAL CLIMB-OUT, PASSING APPROX 11000 FT MSL, A/T SYSTEM DISENGAGED. WHEN THAT HAPPENED, NOTICED A FLUCTUATION IN NR 1 FUEL FLOW. CONTINUED CLIMB WHILE EVALUATING PROBLEM. NR 2 FUEL FLOW WAS APPROX 12000PPH NR 1 WAS FLUCTUATING BETWEEN 7000 PPH AND 15Aug 21, 2005 · N654FE · Airbus A300F4605R · Fuel Controlling SystemSDR 05FDEA02544Bleed Valve · failedSHORTLY AFTER T/O NR 1 ENGINE HP BLEED VALVE FAULTED. TEMP ON ECAM BLEED PAGE SHOWED 255-260 DEGREES. WITHIN 30 SECONDS REGULAR BLEED VALVE FAULTED. REMOVED AND REPLACED NR 1 ENGINE FAN AIR VALVE, ALL CHECKS NORMAL PER MM 36-11-16-4-03. ACCOMPLISHED NR 1 EAug 18, 2005 · N716FD · Airbus A300B4622 · Compressor Bleed ValveSDR UPS05145259Cowling · damagedNR 2 ENG OTBD FAN COWL HAS HEAT DAMAGE. REMOVED AND REPLACED NR 2 ENG OTBD FAN COWL REF MM 71-13-02-4.Jul 17, 2005 · N131UP · Airbus A300F4622R · Engine Air Intake SystemSDR UPS05143914Engine · crackedNR 1 ENGINE INLET SKIN CRACKS. R&R LT ENGINE NOSE COWL IAW A300 MM THRU STEP 3B (10). INSTALLED LT NOSE COWL LEAK CHECK GOOD REF MM. THIS CLEARS D296652 INSPECTION.Feb 20, 2005 · N160UP · Airbus A300F4622R · Engine (Turbine/Turboprop)SDR UPS04143335Light · inoperativeLAV EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHT.Oct 8, 2004 · N149UP · Airbus A300F4622R · Emergency LightingSDR UPS04143325Light · inoperativeDURING PREFLIGHT TEST OF EMERGENCY EVACUATION SLIDE, THE AURAL SOUND WORKS BUT THE LIGHT DOES NOT ILLUMINATE. RESET ASPSU IAW MM 52-73-18-4. DEFERRAL CLEARED.Oct 7, 2004 · N126UP · Airbus A300F4622R · Escape SlideSDR UPS04143049Oxygen Mask · inoperativeF/O 02 MASK WILL NOT TEST PROPERLY. REINSTALLED F/O 02 MASK. TEST OKAY.Sep 3, 2004 · N122UP · Airbus A300F4622R · Crew Oxygen SystemSDR UPS04143048Slide · inoperativeREF M287110 ESCAPE SLIDE DEPLOYED. REPLACED ESCAPE SLIDE ASSY IAW MM 25-61-21-4. OKAY FOR SERVICE. CLEARED DMI M287110.Sep 3, 2004 · N129UP · Airbus A300F4622R · Escape SlideSDR 04FDEA02463Pump · leakingLOST NEARLY ALL GREEN HYDRAULIC QUANITY DURING CRUISE AT FL 290. FOUND LT HYD PUMP SHAFT SEAL LEAKING. REMOVED AND REPLACED LT OR FWD HYD PUMP ON NR 2 ENG ISW M/M 29-11-32-4-1, OPS AND LEAK CHECK, GOOD.Aug 12, 2004 · N719FD · Airbus A300B4622R · Hydraulic Pump (Electric/Engine), MainSDR UPS04142899Brake · fireDURING BLOCK IN NR 4 BRAKE WAS SEEN TO BE ON FIRE. SMALL AREA OFF BRAKE ONLY. WHEEL ASSY AND GEAR AREA NOT AFFECTED. REMOVED AND REPLACED NR 4 BRAKE UNIT IAW MM 32-42-27-4.Aug 10, 2004 · N125UP · Airbus A300F4622R · BrakeSDR USA2004F00072Epsu · will not testEPSU R2 WOULD NOT TEST. MAINTENANCE REPLACED THE EPSU. OPERATIONAL CHECK GOOD.Jun 5, 2004 · N678US · Airbus A330323 · Emergency LightingSDR USA2004F00073Switch · failedEPSU (ESCAPE SLIDE LT SW EPSU R2) FAULTED DURING TEST. MAINTENANCE FOUND THE R2 SLIDE LIGHT SWITCH BAD. REMOVED AND REPLACED R2 SLIDE ASSY IAW MM. ALL TESTS OK.Jun 5, 2004 · N678US · Airbus A330323 · Escape SlideSDR UPS03141228Light · inoperativeCREW DISCOVERED EVAC SLIDE LIGHT (WARNING LIGHT) INOPERATIVE. DEFERRED UNDER MEL 52-73-01 01 W/CONTROL NR M266526 PLACARD INSTALLED.Sep 15, 2003 · N136UP · Airbus A300F4622R · Escape SlideSDR UPS05145889Hydraulic Line · brokenINSPECTION TYPE: N/A GREEN SYS RSVR LOW LEVEL WARNING CAME ON IN FLT FOLLOWED ALL ECAM PROCEDURES AND CHECK LIST. **** SUPPLEMENTAL MRR **** REPAIRED HYD LINE NEAR GREEN SYS SERVO CONTROL UNIT IAW M/M 20-23-11-0. LEAK CHECKS OK. SERVICED GREEN SYSTEM RES.Dec 22, 2002 · N121UP · Airbus A300F4622R · Hydraulic System, MainSDR USAABA02020Battery · dischargedEPSU AT L2 DOOR FAILED THE BATTERY TEST. MAINTENANCE REPLACED THE EPSU BATTERY.Sep 27, 2002 · N677UW · Airbus A330323 · Emergency LightingSDR S01629020Hydraulic SystemB-18573 DURING T/O,GEAR RETRACT ECAM WARNING MSG SJun 13, 2001 · Airbus A300F4622R · Hydraulic Power SystemSDR AU000056Fire Detector · faulty(AUS) NR 1 ENGINE FIRE WARNING SYSTEM FAULTY.Jan 15, 2000 · Airbus A300B4622R · Fire DetectionSDR 98ZZZX3948Engine · leakingCI-151 NGO-TPE. AIRCRACFT AIR TURN BACK DUE TO NR 2 ENGINE OIL LOSS. NR 2 ENGINE REPLACED IN NGO BY AOG TEAM. S/N OFF 724877. S/N ON 728513. ENGINE TSO: 8,766:48 HOURS. ENGINE TC: 3,785.Aug 25, 1998 · N88881 · Airbus A300B4622R · Turbine Engine Oil SystemSDR AU970226Switch · failed(AUS) LH MAIN LANDING GEAR UPLOCK SWITCH FAULTYMar 12, 1997 · Airbus A300B4622R · Landing Gear Position and WarningSDR 97ZZZX1016Air Seal · crackedINSPECTED 2ND STAGE HPTR AIR SEAL AND FOUND CRACK INDICATION AS DESCRIBED IN PW4000 ALL OPER WIRE NOV 14, 1996 NR C301G961114XFR. MFG RECOMMENDATIONS SEE ASB PW4 ENGA72-628.Dec 12, 1996 · Turbine SectionSDR 97ZZZX1017Air Seal · crackedINSPECTED 2ND STAGE HPTR AIR SEAL AND FOUND CRACK INDICATION AS DESCRIBED IN PW4000 ALL OPER WIRE NOV 14, 1996 NR C301G961114XFR. MFG RECOMMENDATIONS SEE ASB PW4 ENGA72-628.Dec 12, 1996 · Turbine SectionSDR 97ZZZX1018Air Seal · crackedINSPECTED 2ND STAGE HPTR AIR SEAL AND FOUND CRACK INDICATION AS DESCRIBED IN PW4000 ALL OPER WIRE NOV 14, 1996 NR C301G961114XFR. MFG RECOMMENDATIONS SEE ASB PW4 ENGA72-628.Dec 12, 1996 · Turbine SectionSDR 97ZZZX1019Air Seal · crackedINSPECTED 2ND STAGE HPTR AIR SEAL AND FOUND CRACK INDICATION AS DESCRIBED IN PW4000 ALL OPER WIRE NOV 14, 1996 NR C301G961114XFR. MFG RECOMMENDATIONS SEE ASB PW4ENG172-628.Dec 12, 1996 · Turbine SectionSDR 97ZZZX1020Air Seal · crackedINSPECTED 2ND STAGE HPTR AIR SEAL AND FOUND CRACK INDICATION AS DESCRIBED IN PW4000 ALL OPER WIRE NOV 14, 1996 NR C301G961114XFR. MFG RECOMMENDATIONS SEE ASB PW4 ENGA72-628.Dec 12, 1996 · Turbine Section
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