Pratt & Whitney PW4152

Service difficulty reports · 145

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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 = 'PW4152'
  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 FDEA201009143392Floor Panel · puncturedBULK PIT FLOOR PANEL 162 EF IS PUNCTURED. FABRICATED NEW PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND INSTALLED METAL PLATE IAW DWG SRZ 25-011, REV, "C"Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143393Floor Panel · puncturedBULK PIT FLOOR PANEL 162 DF IS PUNCTURED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND INSTALLED METAL PLATE IAW DWG SRZ 25-011, REV, "C"Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143394Floor Panel · puncturedBULK PIT FLOOR PANEL 161 GF IS PUNCTURED. FABRICATED NEW FLOOR PANEL, POTTED EDGES & INSTALLED INSERTS IAW SRZ 25-005, REV "H". TRIMMED & BONDED METAL PLATE IAW SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143395Floor Panel · puncturedBULK PIT FLOOR PANEL 161 BF IS PUNCTURED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND INSTALLED METAL PLATE IAW DWG SRZ 25-011, REV, "C"Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143396Floor Panel · crackedFWD CARGO COMPARTMENT FLOOR PANEL 132 RF IS CRACKED AND HAS EDGE DAMAGE IN NUMEROUS PLACES. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143398Floor Panel · delaminatedAFT PIT FLOOR PANEL 152 DF IS DELAMINATED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143399Floor Panel · delaminatedAFT PIT FLOOR PANEL 152 BF IS DELAMINATED. FABRICATED NEW FLOOR PANEL, IAW DWG SRZ 25-005, REV "H". POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143400Panel · delaminatedAFT PIT CEILING PANEL 152 DC IS DELAMINATED. REPAIRED AFT PIT CEILING PANEL BY REMOVING THE METAL DOUBLER DAMAGE, FIBERGLASS DAMAGE ON THE EXTERIOR AND INNER SURFACE, CLEANING, FABRICATING METAL DOUBLER, PREPPING AREA TO BOND METAL AND FIBERGLASS REPAIR PLIESSep 14, 2010 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201009143401Floor Panel · delaminatedBULK PIT FLOOR PANEL 161 HF IS DELAMINATED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND BONDED METAL PLATE IAW DWG SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143402Floor Panel · delaminatedBULK PIT FLOOR PANEL 161 AF IS DELAMINATED. FABRICATED NEW PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". FABRICATED, TRIMED AND BONDED A METAL PLATE IAW DWG SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143403Floor Panel · delaminatedBULK PIT FLOOR PANEL 162 HF IS DELAMINATED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMED AND BONDED A METAL PLATE IAW DWG SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143404Panel · dentedBULK PIT SIDEWALL PANEL 161 GW IS DENTED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND BONDED METAL PLATE IAW DWG SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201009143405Floor Panel · crackedMAIN CABIN FLOOR PANEL 252 BG IS CRACKED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143406Floor Panel · crackedMAIN CABIN FLOOR PANEL 251 EH HAS A CRACKED CORNER. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143407Floor Panel · crackedMAIN CABIN FLOOR PANEL 251 PH IS CRACKED ON THE BOTTOM SIDE. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143408Floor Panel · crackedMAIN CABIN FLOOR PANEL 252 BH HAS AN EAR CRACKED OFF THE AFT END OF THE PANEL. FABBED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143409Floor Panel · crackedMAIN CABIN FLOOR PANEL 232 MH IS CRACKED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143410Floor Panel · crackedMAIN CABIN FLOOR PANEL 241 ZJ IS CRACKED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143411Floor Panel · crackedMAIN CABIN FLOOR PANEL 241 PK IS CRACKED. FABRICATED NEW FLOOR PANEL, POTTED EDGES, INSTALLED INSERTS, APPLIED ANTI-SKID AND PART MARKED IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143412Floor Panel · crackedMAIN CABIN FLOOR PANEL 231 LG IS CRACKED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143413Floor Panel · puncturedMAIN CABIN FLOOR PANEL 231 QG IS PUNCTURED ON THE TOP SURFACE. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143397Floor Panel · delaminatedAFT PIT FLOOR PANEL 152 AF IS DELAMINATED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009103337Skin · corrodedRT WING BOTTOM SKIN, LOWER SURFACE IS CORRODED AT RIB 31. REAR SPAR AREA. REMOVED CORROSION. ORIGINAL MATERIAL 0.150. MATERIAL REMAINING 0.091. MATERIAL LOSS 0.059 OUT OF LIMITS IAW SRM 57-20-12. RERPAIR AREA IAW EA 6-5710-136708, "WINGS - RT WING LOWSep 10, 2010 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201008263146Pitot Head · contaminatedF/O A/S INOP DURING T/O ROLL ABORTED T/O. PVG U CHECKED F/O PITOT TUBE FOUND A BUG INSIDE, CLEARED PITOT TUBE AND PERFORMED THE PITOT TUBE INSP ALL OK IAW AMM 34-11-15-6, PERFORMED AUTO LAND SYS TEST PASSED IAW AMM 22-00-00, ACFT REMAINED CAT 3III, ACFT OKAug 26, 2010 · N804FD · Airbus A310324 · Pitot/Static SystemSDR FDEA201003160837Thrust Reverser · malfunctionedON TAKEOFF AT 60 KIAS, THE NR 2 THRUST REVERSER UNLOCKED LIGHT WITH ACCOMPANIED ECAM WARNING ILLUMINATED. TAKEOFF REJECTED, ECAM AND QRH CHECKLISTS COMPLETE. MEL 16MAR10 RELEASED FOR SERVICE PER MEL: 78-30-01-C CATEGORY: C EXPIRATION: 26MAR10, "MEL 78-30-Mar 16, 2010 · N815FD · Airbus A310324 · Engine Thrust ReverserSDR FDEA201003090706Indicator · intermittentSHORTLY AFTER LEVELOFF AT 380 LT OUTER FUEL INDICATED "XX" WITH TOTAL FUEL READING "XX" AND ALSO GW AND CG READING "XX" ON ECAM. LT OUTER FUEL QUANTITY ON OVERHEAD WAS BLANK. MEL 28-21-09 ALREADY HAD AUTO FUEL FEED SYSTEM DE-ACTIVATED FUEL ON LT INNER TANK Mar 9, 2010 · N803FD · Airbus A310324 · Fuel Indicating SystemSDR FDEA200911204097Anti-Ice System · faultedDURING T/O POWER APPLICATION, WHEN TOGA PWR WAS SELECTED THE GREEN A/THR LIGHT ILLUMINATED HOWEVER THE THROTTLES WOULD NOT MOVE. ACCOMPLISHED RTO AT 25 KTS. VERIFIED AT BLOCK IN NR1 ENGINE ANTI ICE WAS FAULTING IN ECAM. RELEASED FOR SERVICE IAW MEL: 22-30-01Nov 20, 2009 · N812FD · Airbus A310324 · Engine Anti-Icing SystemSDR 2011F00122Engine · shutdownIN FLIGHT SHUTDOWN OCCURS, LOUD BANG WAS HEARD AT CRUISE FL 360, N1 DROPPED 20 PERCENT, N2 DROPPED 20 PERCENT, EGT NOTED 400C, VIBRATION 3.2 UNIT. THROTTLE BROUGHT TO IDLE EGT SHOOT UP AGAIN (RED LIGHT).Apr 25, 2007 · Airbus A310324 · Engine (Turbine/Turboprop)SDR 07FDEA01454Fairing · crackedCRACK FOUND AT INNER SKIN OF NR 4 LT FLAP MOVABLE FAIRING. REPAIR PERFORMED BY BONDING IAW SRM 57-20-35 AND EA 6-5720-99236 AND RAS/FOK/126/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310 · Wing Miscellaneous StructureSDR 07FDEA01455Skin · wornELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF LT WING SKIN. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW. EA 6-5720-101304 AND RAS/BAE/1002914/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310 · Wing, Center BoxSDR 07FDEA01456Skin · wornELONGATED HOLES AT PYLON SUPPORT BRACKET AND BOTTOM OF RT WING SKIN. REPAIR PERFORMED BY REAM UP AND BUSHING INSTALLATION IAW. EA 6-5720-101304 AND RAS/BAE/1002914/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310 · Wing, Plate/SkinSDR 07FDEA01457Panel · delaminatedDELAMINATION AT VERTICAL STABILIZER L/E PANEL NR 3. REPAIR WAS PERFORMED BY WET LAY-UP REPAIR IAW. SRM 51-77-12 / FIG.211, APPROVED BY EA 6-5532-101302 AND RAS/DAHAM/4020826/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310 · Vertical Stabilizer, Plate/SkinSDR 07FDEA01459Longeron · corrodedCORROSION FOUND ON LONGERON A536-11644-220, C11-C14, Y 770. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Longeron/StringerSDR 07FDEA01460Seat Track · corrodedCORROSION ON SEAT TRACK, C15A-C19, Y-953. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 71-52-10.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA01462Longeron · corrodedCORROSION ON LONGERON C11-C15A, Y-1456. REPAIR PERFORMED BY T-SPLICE REPAIR IAW SRM 53-12-15 / FIG.207.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Longeron/StringerSDR 07FDEA01463Longeron · corrodedCORRODED LONGERON C12A-C14, Y1959. REPAIR PERFORMED BY T-SPLICE REPAIR IAW. SRM 53-12-15 / FIG 207.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Longeron/StringerSDR 07FDEA01464Longeron · corrodedCORRODED LONGERON C11-C15A, Y-450. REPAIR PERFORMED BY T-SPLICE REPAIR IAW. SRM 53-12-15 / FIG.207.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Longeron/StringerSDR 07FDEA01466Floorbeam · corrodedCORRODED TOP CAP FLOORBEAM AT C33 LT. REPAIR PERFORMED BY SPLICING IAW SRM 53-10-15 / FIG.207.Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Floor BeamSDR 07FDEA01468Stringer · corrodedCORRODED STRINGER P44 LT AND RT, C16A-C17. STRINGER REPAIR PERFORMED IAW. SRM 53-12-14 / FIG.201. (RUN OUT FITTING INSTALLATION; PN A536-10607-206, -207)Apr 12, 2007 · N810FD · Airbus A310 · Fuselage Main, Longeron/StringerSDR 07FDEA01470Skin · dentedOLD DENT ON BULK CARGO DOOR LOWER LT CORNER WITH RAS/DATLS/0002170/2004 WITH TEMPORARY LIMIT OF ONE UNPRESSURIZED FERRY FLIGHT. PERMANENT REPAIR PERFORMED BY DOUBLER INSTALLATION IAW. EA 6-5234-101283 AND RAS/DABRE/7006682/2006 ISSUE (A).Apr 12, 2007 · N810FD · Airbus A310 · Cargo/Baggage DoorsSDR 07FDEA01477Attach Fitting · corrodedCORROSION ON PYLON NR 2 BEARING HOLE ON RIB 18 LOWER ATTACH FITTING. REPAIR PERFORMED BY REAM UP HOLE AND CHAMFER ON EACH SIDE IAW SB: A310-54-2021 AND EA 6-5451-103241.Apr 12, 2007 · N810FD · Airbus A310 · Nacelle/Pylon, Attach FittingsSDR 07FDEA00492Engine · unknownNR 2 ENG DOES NOT RESPOND TO THROTTLE MOVEMENT, ATS LEVER OFF. REPLACED NR 2 EEC PER MM 73-21-01-4-06 AND WAS NO HELP. CHECKED FADEC FAULTS AND HAD NONE. RAN ENGINE WITH NO EPR MODE FAULTS OR COMMAND POINT, ER FAULTS, ALL ENGINE INDICATIONS GOOD. INSTALLEFeb 15, 2007 · N806FD · Airbus A310324 · Engine (Turbine/Turboprop)SDR 06FDEA03607Thrust Reverser · inoperativeNR 2 T/R UNLOCK WHEN POWER ADDED FOR T/O ACN RELEASED FOR SERVICE IAW MEL/CDL: 78-30-01-C THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION. REMOVED AND REPLACED NR 2 ENG T/R PRSOV AS REQUIRED PER A310-300MM78-31-05-4.OPS CHECK GOOD.Oct 10, 2006 · N806FD · Airbus A310324 · Engine Thrust ReverserSDR 06FDEA0372Converter · no testREMOVED AND REPLACED SDAC IAW AMM 31-55-22-4. OPERATIONAL TEST FOUND SATISFACTORY. A/C OK TO CONTINUE. PREMATURE REMOVAL/INSTALLATION.Jan 24, 2006 · N802FD · Airbus A310 · DC Rectifier/ConverterSDR 06FDEA0240Structure · contaminatedPILOT REPORT ACFT WILL TAKE AN ATTITUDE OF 3 DEGREES NOSE UP AT ALL PHASES OF FLIGHT ANY TIME. THE AUTO PILOT IS DISCONECTED. OPEN T.H.S ACCESS PANEL AND NOTICED ACCUMULATION OF WATER ABOUT 14 INCHES HIGH RIGHT BEHIND PRESSURE BULKHEAD. UNPLUGED DRAIN IN Jan 17, 2006 · N804FD · Airbus A310 · Aircraft StructuresSDR 04FDEA03453Engine · malfunctionedAT 1200 FT ON T/O, NR 2 ENGINE SEVERE COMPRESSOR STALLS. TOWER REPORTED FLAME FROM RIGHT ENGINE IN FLIGHT. PERFORMED ENGINE FIRE CHECKLIST NR 2. RETURNED TO LAND, IND WEIGHT 216.0. FIRE HANDLE PULLED, 1ST AGENT DISCHARGED. EPR/EGT EXCEEDENCE MESSAGES ON EDec 20, 2004 · N801FD · Airbus A310324 · Engine (Turbine/Turboprop)SDR 03FDEA02299Engine · inoperativeHEARD LOUD BANG, NOSE MOVED TO RT SHARPLY. FOLLOWED REJECTED TAKEOFF PROCEDURE. ALL ENGINE INSTRUMENTS NORMAL AT 105 KTS. IAW TROUBLESHOOTING MANUAL AND POWERPLANT ENGINEERING CONCURRENCE, ENGINE WILL BE CHANGED. SHIPPING INFO TENATIVE FOR REPLACEMENT ENGIDec 29, 2003 · N801FD · Airbus A310 · Engine (Turbine/Turboprop)SDR AUS20020584Skin · debonded(AUS) RT INBOARD TRAILING EDGE FLAP DISBONDED.Mar 6, 2002 · Airbus A310324 · Trailing Edge FlapsSDR AUS20020586Cable · worn(AUS) RUDDER CABLE WORN.Mar 6, 2002 · Airbus A310324 · Rudder Control SystemSDR AUS20020587Cable · worn(AUS) ELEVATOR CABLES PNO A2737114500000 AND PNO A2737114000000 WORN.Mar 6, 2002 · Airbus A310324 · Elevator Control System
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