Pratt & Whitney PW4158

Service difficulty reports · 689

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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"

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SDR IPXA10160802Skin · gougedINSPECTION TYPE:10YR, LT CTR FLAP UPPER SKIN REPAIR IS GOUGED IN SEVERAL PLACES. ACCOMPLISHED REPAIR IAW SRM 57-50-00 PARA 4E, FIG 205.Jun 9, 2010 · N121UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10160993Skin · chafedINSPECTION TYPE:10YR, LT INBD FLAP UPPER SKIN REPAIR DOUBLER IS CHAFED ACCOMPLISHED REPAIR IAW STA EA 300-5750-01-A2498, REV I/R AND EO A300-5750-38651-A.Jun 9, 2010 · N121UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10161027Skin · chafedINSPECTION TYPE:10YR, LT OTBD FLAP INBD L/E CHAFED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-50-00 PARA 4H FIG 208.Jun 9, 2010 · N121UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10160342Skin · crackedCRACKED SKIN AT RAT OPENING RT SIDE. REPAIRED WITH DOUBLER REPAIR IAW A300-5720-37427-D.Jun 8, 2010 · N124UP · Airbus A300F4622R · Wing, Plate/SkinSDR FDEA201006081869Clamp · failedSMOKE IN ACFT. APU AUTO SHUTDOWN. APU OIL QTY IS ZERO ON FLT DECK GUAGE & READING ZERO IN THE APU BAY. APU OIL QTY AT BLOCKING READING OVER HALF FULL. DUE TO SMOKE & ODOR OF OIL FROM BOTH PACKS. C/W MM 21-51-00-3 AND R & R BOTH PACK COALESCER BAGS. REFJun 8, 2010 · N746FD · Airbus A300B4622R · APU Oil SystemSDR IPXA10160537Floorboard · delaminatedINSPECTION TYPE:5YR, MAIN CABIN FLOORBOARD NR 241VK HAS DELAMINATED FABRICATED MAIN CABIN FLOORBOARD NR 241VK IAW EO A300-5320-16407-D APPENDIX B.Jun 8, 2010 · N167UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA10160327Skin · damagedRT WING INBD FLAP LOWER SURFACE DAMAGED. REPAIRED IAW EO A300-5750-36683-B.Jun 7, 2010 · N137UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10160445Floor Panel · damagedINSPECTION TYPE:10YR EDGE DAMAGE F/B NR 151UF AFT CARGO. FABRICATED AFT CARGO FLOOR PANEL NR 151UF IAW EO A300-5320-16407-D, APPENDIX C.Jun 7, 2010 · N121UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10160429Skin · gougedINSPECTION TYPE:5YR, REPAIR SURVEY SEQUENCE NR167-W3-02 REPAIR DOUBLER GOUGED IN 4 PLACES ON LT CTR FLAP UPPER SKIN BETWEEN RIBS 13-15 STGR 2.6 AND 2.7. REMOVED, FABRICATED AND INSTALLED NEW REPAIR DOUBLER IAW SRM 57-50-00 PB 201 PARA 4E, FIG 205 AND SRM 57-5Jun 5, 2010 · N167UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA0160648Skin · gougedINSPECTION TYPE:5YR, LT OTBD FLAP IB L/E TIP IS GOUGED. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-50-00 PARA. 4H FIG 208.Jun 4, 2010 · N167UP · Airbus A300F4622R · Trailing Edge FlapsSDR FDEA201006031784Panel · damagedBULK CARGO PIT SLANT PANEL 161CW HAS MULTIPLE DENTS AND THE BACK IS CORRODED. FABRICATED NEW BULK CARGO PIT SLANT PANEL 161 CW IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".Jun 3, 2010 · N730FD · Airbus A300B4622R · Cargo CompartmentsSDR FDEA201006031785Panel · damagedBULK CARGO PIT SLANT PANEL 161GW HAS MULTIPLE DENTS AND IS DELAMINATED. FABRICATED PANEL 161 CW IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".Jun 3, 2010 · N730FD · Airbus A300B4622R · Cargo CompartmentsSDR FDEA201006031786Panel · dentedBULK CARGO PIT SLANT PANEL 161AW HAS MULTIPLE DENTS. FABRICATED NEW BULK CARGO PIT SLANT PANEL 161 AW IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".Jun 3, 2010 · N730FD · Airbus A300B4622R · Cargo CompartmentsSDR FDEA201006031787Panel · dentedBULK CARGO PIT SLANT PANEL 161LW HAS MULTIPLE DENTS. FABRICATED NEW BULK CARGO PIT SLANT PANEL 161 LW IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201006031788Panel · damagedBULK CARGO PIT SLANT PANEL 162 LW IS CRACKED AND PUNCTURED. FABRICATED NEW BULK CARGO PIT SLANT PANEL 162 LW IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201006031789Panel · damagedMLG WHEEL WELL KEEL BEAM BOX CAT WALK PANEL LOCATED AT THE CTR OF THE KEEL BEAM HAS THE FWD LT AND RT FASTENER HOLES DAMAGED. FABRICATED NEW MLG W/W KEEL BEAM CAT WALK PANEL 147 BF IAW DWG SRZ 25-005, REV "H". PART MARKED PANEL REF DWG SRZ 25-005, REV "H". Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201006031790Floorboard · puncturedBULK CARGO COMPARTMENT FLOORBOARD 161 AF TOP SURFACE IS PUNCTURED, HAS MULTIPLE DENTS AND LARGE AREAS OF DELAMINATION. FABRICATED NEW BULK CARGO COMPARTMENT FLOORBOARD 161 AF IAW DWG SRZ 25- 005, REV "H" AND DWG SRZ 25-011, REV "C".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201006031791Floorboard · puncturedBULK CARGO COMPARTMENT FLOORBOARD 162 HF TOP SURFACE IS PUNCTURED, DENTED AND CORRODED. FABRICATED NEW BULK CARGO COMPARTMENT FLOOR BOARD 162 HF IAW DWG SRZ 25- 005, REV "H" AND DWG SRZ 25-011, REV "C".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201006031792Floorboard · puncturedBULK CARGO COMPARTMENT FLOORBOARD 161 JF TOP SURFACE HAS MULTIPLE DENTS AND DELAMINATION. FABRICATED NEW BULK CARGO COMPARTMENT FLOOR BOARD 161 AF IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201006031793Floorboard · brokenAFT CARGO COMPARTMENT FLOORBOARD 151 VF CORNER AND EDGE FILLER IS BROKEN. FABRICATED NEW AFT CARGO COMPARTMENT FLOORBOARD 151 VF IAW DWG SRZ 25- 005, REV "H".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201006031794Floorboard · damagedAFT CARGO COMPARTMENT FLOORBOARD 152 XF EDGE IS DAMAGED AND THE BOTTOM IS TORN. FABRICATED NEW AFT CARGO COMPARTMENT FLOORBOARD 152 XF IAW DWG SRZ 25-005, REV "H".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201006031795Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 132 HG HAS EDGE DAMAGE AND MULTIPLE PUNCTURES ON THE BOTTOM. FABRICATED NEW FWD CARGO COMPARTMENT FLOOR BOARD 132 HG IAW DWG SRZ 25- 005, REV "H".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201006031796Floorboard · crackedFWD CARGO COMPARTMENT FLOORBOARD 132 JG HAS MULTIPLE CRACKS. FABRICATED NEW FWD CARGO COMPARTMENT FLOORBOARD 132 JG IAW DWG SRZ 25- 005, REV "H".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201006031800Floor Panel · delaminatedWHEEL WELL FLOOR PANEL 147 DF IS DELAMINATED. FABRICATED NEW W/W FLOOR PANEL 147 DF IAW DWG SRZ 25-005, REV "H".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201006031808Floorboard · crackedAFT CARGO COMPARTMENT FLOORBOARD 151 XF IS CRACKED ACROSS THE CTR OF THE BOARD. FABRICATED FLOORBOARD 151 XF IAW DWG SRZ 25-005, REV "H" AND SRZ 25-011, REV "C".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201006031797Floor Panel · delaminatedWHEEL WELL FLOOR PANEL 143 CF IS DELAMINATED. FABRICATED NEW W/ W FLOOR PANEL 143 CF IAW DWG SRZ 25-005, REV "H".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201006031798Floor Panel · delaminatedWHEEL WELL FLOOR PANEL 147 AF IS DELAMINATED. FABBED NEW FLOOR PANEL USING THE OLD PANEL AS A TEMPLATE. KNOCKED BACK CORE EDGES, POTTED, CURED AND INSTALLED INSERTS IN PANEL 147 AF. INSTALLED NON-SKID AND PART MARKED IAW DWG SRZ 25-005, REV "H".Jun 3, 2010 · N730FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201006021766Shaft · corrodedRUDDER VARABLE STOP LEVER ATTACHMENT SHAFT IS CORRODED AND THE PLATING IS PEELING - RT SIDE. REMOVED RUDDER VARIABLE STOP UNIT IAW AMM 27-23-22-4. REMOVED SHAFT IAW CMM 27-23-22, PG 3010. REMOVED CORROSION FROM SHAFT IAW CMM 27-23-22. MEASURED WALL THICKNEJun 2, 2010 · N730FD · Airbus A300B4622R · Rudder Control SystemSDR FDEA201005281692Profile · corrodedFWD.CARGO COMPARTMENT BALLMAT 131YG AFT PROFILE IS CORRODED. (PARTS RACK) REMOVED PROFILE IAW SRM 51-40-21 PARA 6 AND 51-72-10, LOCATED AND DRILLED IAW SRM 51-72-10, INSTALLED NEW PROFILE PN A2577186320600 PO 683083.1 IAW SRM 51-40-21 PARA 6,13 AND 51-72-10 ANMay 28, 2010 · N730FD · Airbus A300B4622R · Cargo CompartmentsSDR FDEA201005281693Seal Depressor · corrodedAFT CARGO COMPT. LOWER DOOR SILL SEAL DEPRESSOR ABOVE NR 2 CARGO DOOR LOCK FITTING IS CORRODED. REMOVED SEAL DEPRESSOR IAW SRM 51-40-21, PARA 5. INSTALLED NEW SEAL DEPRESSOR PN A5397822421600 IAW SRM 51-40-21, PARA 5.May 28, 2010 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201005281702Hmu · unknownON TAKEOFF ROLL, NR 1 ENGINE NEVER WENT PAST 80 PERCENT. RTO WAS AT 80KTS. OMA R BITE CHECK FADEC, REF TSM, NO FAULTS NOTED. INSPECTED BURNER BYPASS LINE, NO LEAKS NOTED. INSPECTED AND CHANGED FUEL FILTER REF MM. R & R FUEL PUMP AND HMU. LEAK CHECK GOOD. May 28, 2010 · N680FE · Airbus A300B4622R · Engine Fuel DistributionSDR FDEA201005271687Probe · dirtyON T/O ROLL AT 80 KNTS CALL, F/O AIRSPEED INDICATED 50 KNTS. CAPTAINS AND STBY AIRSPEED INDICATED 80 KNTS. REJECTED TAKEOFF AT 90 KNTS. R & R F/O'S PITOT PROBE IAW MM 34-11-15-4. OPS CHECKED GOOD IAW MM 34-10-00-5 (FLIGHT ENVIRONMENT DATA TEST). F/O'S LEAK TESMay 27, 2010 · N740FD · Airbus A300B4622R · Pitot/Static SystemSDR FDEA201005261696Flange · corrodedLOWER FUSELAGE FRESH WATER SERVICE PANEL CAVITY WATER PRESSURE GAGE FRAME CORRODED FR.38.1 - FR.38.2, STGR. 45 - STGR. 47. REMOVED PRESSURE GAGE FLANGE IAW SRM 51-40-21, PARA 5, PG 7. RECEIVED EA NR 6-3810-136658. REMOVED CORROSION IAW SRM 51-74-10, PARA B May 26, 2010 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201005261697Flange · corrodedLOWER FUSELAGE FRESH WATER SERVICE PANEL CAVITY WATER QUANTITY GAGE FRAME, CORRODED FR 38.1 - FR 38.2, STGR. 45 - STGR. 47 REMOVED PRESSURE GAGE FLANGE IAW SRM 51-40-21, PARA 5, PG 7. RECEIVED EA NR 6-3810-136658. REMOVED CORROSION IAW SRM 51-74-10, PARA B May 26, 2010 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201005251635Stringer · corrodedCORROSION ON FUSELAGE INTERNAL STRUCTURE BETWEEN FRAME 38.2 AND FRAME 39; BELOW THE OTBD HOT AIR VALVE. (STR 44R TO STR 44R) REMOVED CORRODED STRINGER IAW SRM 51-40-21, PARA 6 & 7. FABBED STRINGER AND COUPLING IAW SRM 53-10-14, FIG 201, PGS 203 / 204. ALMay 25, 2010 · N730FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA201005251636Angle · corrodedAFT CARGO COMPARTMENT FWD LOWER CORNER DOOR SILL ANGLE SEAL DEPRESSOR IS CORRODED. R & R LOWER FWD CORNER SEAL DEPRESSOR, PO 682786.1 IAW SRM 51-72-10, PG 2 AND SRM 51-40-21, PARA 5. ALODINED AND PRIMED AREA IAW SRM 51-71-10, PG 1 AND PAINTED IAW SRM 51-75-10May 25, 2010 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201005241620Attach Angle · crackedAVIONICS COMPARTMENT ATTACH ANGLE IS CRACKED AT FRAME 10; RBL 30. REMOVED ANGLE AND INSTALLED NEW ANGLE PN A5361235620100, PO 682607.2 IAW SRM 51-40-21, PARA 6 & 7.May 24, 2010 · N730FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA201005211606Coupling · corrodedCORROSION ON FUSELAGE INTERNAL STRUCTURE AT THE END FITTING AND BASE OF FRAME 39, PRESSURE BULKHEAD BELOW THE INBD COLD AIR MANIFOLD CHECK VALVE. REMOVED PROFILE IAW SRM 51-40-21. REMOVED 2 EA COUPLINGS IAW SRM 51-40-21, PARA 6&7. REMOVED CORROSION IAW SRM May 21, 2010 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR IPXA10159912Control Unit · inoperativeAFTER T/O L/G WOULD NOT RETRACT. TRIED BOTH POS DET 1&2 L/G LEVER WOULD NOT MOVE PAST OFF POSITION. DIVERTED, IAW FLT CONTROL. FAILURE CODE "65" DETECTED ON PROXIMITY DETECTOR PROCESSING UNIT WHILE PERFORMING T/S IAW FIM 32-30-00. PG. 105 FIG 108. R & R PRMay 18, 2010 · N120UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR IPXA10159913Web · damagedSHEAR WEB DAMAGED. REPAIRED IAW EO A300-5310-37837-A.May 18, 2010 · N160UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA10159914Skin · damagedSKIN DAMAGED. REPAIRED IAW EO A300-5330-37219-B.May 18, 2010 · N160UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR FDEA201005171552Skin · crackedLT WING T/E AREA BOTTOM SKIN IS CRACKED FROM RIB 8 TO RIB 9. PERFORMED REPAIR IAW DWG R57340199, EA 6-5710-136653.May 17, 2010 · N730FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA201005171553Skin · damagedRT WING, (2) HOLES INBD OF RIB 9 SKIN PANEL THAT ARE COMMON TO THE ATTACH ANGLE SHOW CRACK INDICATIONS IN THE FWD AND AFT DIRECTIONS. PERFORMED REPAIR IAW DWG R57340199, EA 6-5710-136653.May 17, 2010 · N730FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA201005171555Support Fitting · crackedMAIN CABIN LT SIDE UNDER FLOOR SUPPORT FITTING IS CRACKED AT FRAME 49, LBL 57. REMOVED CRACKED LINK AND INSTALLED NEW LINK IAW SRM 51-72-10, PARA 6, PG 2.May 17, 2010 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201005171556Support Fitting · crackedMAIN CABIN LT SIDE UNDER FLOOR SUPPORT FITTING IS CRACKED AT FRAME 48, LBL 57. REMOVED CRACKED LINK AND INSTALLED NEW LINK IAW SRM 51-72-10, PARA 6, PG 2.May 17, 2010 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201005171557Fitting · crackedMAIN CABIN UNDER FLOOR PANEL FLOOR SUPPORT FITTING IS CRACKED AT FRAME 49, RBL 57. REPLACED FLOOR SUPPORT LINK IAW SRM 51-72-10, PGS 1-4.May 17, 2010 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR IPXA10159887Wedge · damaged.725 HOLE LOCATED RT INNER FLAP T/E WEDGE. REPAIRED IAW EO A300-5750-33456-B.May 17, 2010 · N124UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10159802Lever · sticksCREW ENTRY DOOR ARM/DISARM LEVER STICKS HALFWAY BETWEEN ARM AND DISARM. TAKES FORCE TO MOVE IT TO DISARM. DEFERRED IAW DMP M425049 ASSIGNED. R & R FWD GIRT BAR SLIDER BELLCRANK IAW MM 52-10 -30. OPS CHECKS GOOD. THIS CLEARS M425049.May 11, 2010 · N143UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA10159731Girt Bar · bentDURING TROUBLESHOOTING OF A DEFERRED ITEM FOUND GIRT BAR TO BE BENT CAUSING ORIGINAL PROBLEM OF DEFERRAL. REPLACED SLIDE PACK AND GIRT BAR ASSY OPS CHECKS GOOD RII OK.May 7, 2010 · N149UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA10159704Slide · inoperativeSLIDE WILL NOT ARM WITH DOOR CLOSED. R & R CREW DOOR SLIDE AND GIRT BAR IAW AMM 25-61-21-04. SLIDE PN ON/OFF D31023-101 SN NO 0543, OFF 0539. GIRT BAR PN 5217044000000 SN ON TAG 01092303. PLACARD REMOVED.May 6, 2010 · N149UP · Airbus A300F4622R · Escape Slide
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