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 FDEA201003160839Lock · wornBULK CARGO DOOR EXTERIOR HANDLE HAS EXCESSIVE PLAY. DISPLACED INTERNAL SKIN; REMOVED 3 EA WEBS AND REMOVED LOCKING MECHANISM IAW SRM 51-40-02, PARA 6 AND AMM 52-34-21-4. INSTALLED INTERNAL SKIN; INSTALLED 3 EA WEBS AND INSTALLED LOCKING MECHANISM IAW SRM 51Mar 16, 2010 · N718FD · Airbus A300B4622 · Cargo/Baggage DoorsSDR IPXA10158917Floor Panel · crackedINSPECTION TYPE:10YR, MCD FLOOR PANEL 251FM IS CRACKED. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 16, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158920Floorboard · crackedINSPECTION TYPE:10YR FLOORBOARD 251YJ IS CRACKED REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 16, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158921Floor Panel · crackedINSP TYPE:10YR, MAIN DECK COMP FLOOR PANEL 251UJ HAS A CRACK. REPAIRED IAW SRM 53-10-20, PARA 8B, FIG 203.Mar 16, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10159042Floor Panel · crackedINSPECTION TYPE:10YR, FLOOR PANEL 241 LJ IS CRACKED FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX.B.Mar 16, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10159045Floor Panel · crackedINSPECTION TYPE: 10YR, FLOOR PANEL 242JF IS CRACKED AT FABRICATED FLOOR PANEL IAW UPS EO A300-5320-16407-D, APPX B.Mar 16, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158849Lamp · inoperativeGLARE SHIELD EMERGENCY LIGHT INOP. RELAMPED. OPS CHECK GOOD IAW AMM 33-12-00-09.Mar 12, 2010 · N129UP · Airbus A300F4622R · Emergency LightingSDR IPXA10159024Floorboard · delaminatedINSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 251ZG IS DELAM AT LWR SURFACE FABBED FLOOR PANEL IAW SRM 53-10-20, PARA. 8B, FIG. 203, SHEE T 1.Mar 11, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10159044Floorboard · delaminatedINSPECTION TYPE:10YR FLOORBOARD 242TN AT MAIN CABIN IS DELAMED FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-D, APPX. B.Mar 10, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158798Floor Panel · damagedINSPECTION TYPE:5 YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231 RT PAINT MISSING SEVERAL AREAS WITH SMALL AREAS OF DELAMINATION. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. BMar 5, 2010 · N165UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158839Floorboard · damagedINSPECTION TYPE:5 YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231LJ PAIN MISSING SEVERAL AREAS WITH SMALL AREAS OF DELAMINATION. FABBED FLOORPANEL IAW UPS EO A300-5320-16407-D, APPX. B.Mar 5, 2010 · N165UP · Airbus A300F4622R · Fuselage Floor PanelSDR FDEA201003040641Slat System · malfunctionedDURING SLAT EXTENSION, SLATS STUCK AT 0 DEGREES. BOTH OVERHEAD SLAT FAULT LIGHTS CAME ON. CYCLED HANDLE AND SLATS STAYED STUCK. DURING TAXI IN CYCLED HANDLE AND SLATS WORKED NORMALLY. BITE TEST OF SFCC 1 SHOWED "MAIN CONT VLV" ON ARRIVAL, SLATS WORKING NORMar 4, 2010 · N721FD · Airbus A300B4622R · Leading Edge Slat Control SystemSDR IPXA10158832Floorboard · delaminatedINSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 232WG IS DELAMINATED. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.Mar 4, 2010 · N165UP · Airbus A300F4622R · Fuselage Floor PanelSDR FDEA201003040638Heat Exchanger · tornRT HEAT EXCHANGER INBD ROD ATTACH FLANGE IS TORN OUT. REMOVED AND REINSTALLED HEAT EXCHANGER IAW AMM 21-51-32-1. WELDED ATTACH FLANGE IAW CMM 21-53-24, PARAGRAPH 6-D. LEAK CHECK GOOD IAW AMM 21-51-00-5. OPS CHECK GOOD IAW AMM 21-51-00-5.Mar 4, 2010 · N718FD · Airbus A300F4622R · Heating SystemSDR FDEA201003030622Support Bracket · corrodedTHE SUPPORT BRACKET INSIDE THE AFT CARGO LOADING CONTROL ACCESS PANEL HAS EXFOLIATED CORROSION; LOCATED AT THE FWD/UPPER CORNER. CORROSION EXCEEDS 50 PERCENT ON THE ANGLE, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PG 6, TABLE 102, CODE "K". FABRICATED NEW AMar 3, 2010 · N718FD · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA10158824Floorboard · brokenINSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 241BF RT LOWER SIDE BROKEN. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.Mar 3, 2010 · N165UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158826Floorboard · brokenINSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 231SG IS BROKEN. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.Mar 3, 2010 · N165UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158828Floorboard · gougedINSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 241LJ LOWER RT SIDE GOUGED. ACCOMPLISHED REPAIR IAW SRM 53 10-20 PARA 8.B FIG 203.Mar 3, 2010 · N165UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158830Floorboard · delaminatedINSPECTION TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 262RF IS DELAMINATED AT AFT CORNER. ACCOMPLISHED REPAIR IAW SRM 53-10-20 PARA 8.B FIG 203.Mar 3, 2010 · N165UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10159043Floor Panel · damagedINSPECTION TYPE:10YR, BULK CARGO COMP FLOOR PANEL 162HF CORNER OF PANEL IS CRUSHED FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. D.Mar 2, 2010 · N120UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158822Skin · gougedINSPECTION TYPE:5 YR, RT INBD FLAP UPPER SKIN GOUGED IN SEVERAL PLACES APPROX 24 INCHES FWD OF RUB STRIP AN INBD OF NR 2 FLAP TRACK. REPAIRED IAW SRM 57-50-00, FIG. 205,Mar 1, 2010 · N165UP · Airbus A300F4622R · Trailing Edge FlapsSDR FDEA201002250527Floor Panel · damagedMAIN CABIN FLOOR PANEL 232VF I S BROKEN FABRICATED NEW FLOORBOARD 232 VF IAW DWG SRZ 25-005, REV "H".Feb 25, 2010 · N718FD · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158639Floor Panel · misrepairedINSPECTION TYPE:3C, PANEL 252SJ REQUIRES REPLACEMENT IAW EO A300-5100-30624C DUE TO REPAIRS DONE TO FLOORBOARD IAW SRM. FABRICATED FLOOR PANEL 252SJ IAW EO A300-5320-16407-D APPENDIX B.Feb 16, 2010 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158640Floorboard · damagedINSPECTION TYPE:3C, PANEL 262RF REQUIRES REPLACEMENT IAW EO A300-5100-30624-C DUE TO REPAIRS DONE TO FLOORBOARD IAW AMM. FABRICATED FLOORBOARD 262RF IAW EO A300-5320-16407-D APPENDIX B.Feb 15, 2010 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158641Floorboard · misrepairedINSPECTION TYPE:3C, PANEL NR 161MF REQUIRES REPLACEMENT IAW EO A300-5100-30624-C DUE TO REPAIRS DONE TO FLOORBOARD IAW AMM. FABRICATED FLOORBOARD NR 161MF IAW EO A300-5320-16407-D APPENDIX D.Feb 15, 2010 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158642Floorboard · misrepairedINSPECTION TYPE:3C, PANEL NR 161LF REQUIRES REPLACEMENT IAW EO A300-5100-30624-C DUE TO REPAIRS DONE TO FLOORBOARD IAW AMM. FABRICATED FLOORBOARD NR161LF IAW EO A300-5320-16407-D APPENDIX D.Feb 15, 2010 · N150UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158618Floor Panel · damagedINSP TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 252VJ DAMAGED. FABED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. B.Feb 14, 2010 · N166UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158591Skin · gougedINSP TYPE:3/C LT WING CTR FLAP UPPER SKIN GOUGED 12IN. FWD OF RUB STRIP ABOVE NR 4 FLAP TRACK. REPAIRED IAW SRM 57-50-00 FIG. 205, PARA 4E.Feb 12, 2010 · N150UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10158563Floor Panel · brokenINSP TYPE:5 YR MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231XG BROKEN. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX.B.Feb 11, 2010 · N166UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158565Floor Panel · brokenINSP TYPE:5 YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 262TF BROKEN. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. B.Feb 11, 2010 · N166UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158566Floor Panel · brokenINSPECTION TYPE:5 YR MAIN DECK CARGO COMPARTMENT FLOORBOARD 241MK BROKEN FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. B.Feb 11, 2010 · N166UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158593Floor Panel · brokenINSP TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOORBOARD 241YG BROKEN. FABBED IAW EO A300-5320-16407-D, APPX B.Feb 11, 2010 · N166UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158594Floor Panel · brokenINSP TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOOR PANEL 251UJ BROKEN. FABBED FLOOR PANEL IAW EO A300-5320-16407-D, APPX. B.Feb 11, 2010 · N166UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10158615Floor Panel · brokenINSP TYPE:5YR, MAIN DECK CARGO COMPARTMENT FLOOR PANEL 252UJ IS BROKEN. FABRICATED FLOOR PANEL 252UJ IAW EO A300-5320-16407D APPENDIX B.Feb 11, 2010 · N166UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA09157957Engine · unserviceableINSPECTION TYPE:N/A AT FL 330 ECAM ADVISORY-LOW OIL QTY NR 1 ENGINE. ECAM AND OIL QTY GAUGE BOTH INDICATED OIL QUANTITY 0 ON NR 1 ENGINE. NR 1 ENGINE PRES AND TEMP NORMAL THROUGHOUT FLIGHT. CONTINUED TO RUN ENGINE AND IT PERFORMED WITHIN LIMITS IN ALL PWR RNov 24, 2009 · N158UP · Airbus A300F4622R · Engine (Turbine/Turboprop)SDR FDEA200910083515Detector · failedON CLIMBOUT IN HEAVY RAIN AT 3000 FT, NR 1 ENG FIRE LIGHT ILLUMINATED. C/W EMERGENCY PROCEDURES. LANDED 23L. LIGHT STAYED ON AFTER LANDING. FIRE DEPT CONFIRMED VISUALLY AND INFRARED NO FIRE. TOWED IN. DISCONNECTED CONNECTOR D1909VC AT ENGINE NR 1 PYLON. Oct 8, 2009 · N716FD · Airbus A300B4622 · Fire DetectionSDR IPXA09157110Fan Blade · damagedINSPECTION TYPE:N/A CREW REPORTED POSSIBLE BIRD STRIKE WITH ASSOCIATED RT ENGINE VIBRATION REACHING 3.2. AFTER LANDING FOUND 2 FAN BLADES DAMAGED ON RT ENGINE. FOUND TWO BLADES DAMAGED BEYOND LIMITS. R&R BLADE SETS PER AMM. PERFORMED VIBE SURVEY.Aug 20, 2009 · N166UP · Airbus A300F4622R · Turbine Engine Compressor SectionSDR IPXA09156896Engine · overtempDURING CLIMB THROUGH FL250 NR 2 ENGINE SURGED WITH OVER TEMP. ENG SHUTDOWN & RETURNED TO VCE. REPLACED NR 2 ENGINE PER AMM 71-00-00-04 AND TC 710000-P1-1-400, TC 710001-P1-1-400.Jul 31, 2009 · N129UP · Airbus A300F4622R · Engine (Turbine/Turboprop)SDR FDEA200907292830Thrust Reverser · inoperativeON TAKEOFF PWR APPLICATION NR1 REV UNLOCK LIGHT ILLUMINATED. ABORTED TAKEOFF AT 23KTS. "MEL 78-30-01-C: ENGINE (IDENTIFY 1 OR 2) NR 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FWD THRUST POSITION." REMOVED AND REPLACED THE THRUST REVERSER PRJul 29, 2009 · N743FD · Airbus A300B4622R · Engine Thrust ReverserSDR IPXA09156352Engine · bird ingestionATB DUE TO SUSPECTED COMPRESSOR STALL ON TAKEOFF. HEARD LOUD BANG AND A LARGE SHUDDER DURING ROTATION. THE F/O THOUGHT HE SAW A FLASH OF LIGHT ON THE RT SIDE. ALSO HAD AUTO THROTTLE ANOMALIES. FOUND EVIDENCE OF BIRD STRIKE TRAILING SIDE OF FAN AND COMPRESSJun 16, 2009 · N122UP · Airbus A300F4622R · Engine (Turbine/Turboprop)SDR FDEA200906041922Frame · gougedFOUND A GOUGE IN OUTER FLANGE OF FRAME 47 NEAR P26 LT. REPAIR PERFORMED BY REWORK OUTER FLANGE AT RUN OUT TO ELIMINATE THE GOUGE AND NDT FOR CRACK FREE CONDITION IAW. RAS/EFW/9000182/2009 ISS. A, APPROVED BY EA 6-5310-131203.Jun 4, 2009 · N751FD · Airbus A300B4622R · Fuselage Main, FrameSDR IPXA09155026Warning System · activatedRECEIVED NR 1 THRUST REVERSER UNLOCK LIGHT IN CRUISE. CREW ELECTED TO DIVERT TO LIT. DEFERRED NR 1 THRUST REVERSER PER MEL 70-30-01 AND DMP 70-30-01.Mar 15, 2009 · N149UP · Airbus A300F4622R · Engine Thrust ReverserSDR FDEA200902100499Shutoff Valve · malfunctionedGOT REVERSER UNLOCK ON NR 1 ENG AT 60 KTS. ATTEMPTED SECOND T/O SAME RESULTS. R&R PRSOV PER AMM 78-32-11-5Feb 10, 2009 · N721FD · Airbus A300B4622R · Engine Thrust ReverserSDR UPS08152643Light · malfunctionedEMERGENCY EXIT LIGHTS FLICKER WHEN SUPPOSE TO BE ON. COMPLIED WITH OPERATIONAL TEST OF EMERGENCY LIGHTING IAW AMM 33-51-00- 05. OPS CHECK GOOD.Jul 4, 2008 · N156UP · Airbus A300F4622R · Emergency LightingSDR 08FDEA00261Connector · damagedON DESCENT NR 1 ENG THRUST WOULD NOT INCREASE, FOLLOWED BY OIL PRESS LOW WARNING. PRESS SHOWED NEAR ZERO, S/D ENG NR 1, ENG NR 1 WINDMILL APPROX 10 MIN, PER CREW DEBRIEF, ON DESCENT WITH THROTTLES AT IDLE. ADVANCED THROTTLES TO LEVEL OFF, NR 1 ENG W/N RESPONJan 23, 2008 · N725FD · Airbus A300B4622R · Engine Oil System WiringSDR UPS07150557Indicator · fluctuatesINSPECTION TYPE:N/A DURING CLIMBOUT RIGHT ENGINE OIL PRESSURE INDICATION WENT TO XX ON BOTH ECAM & GAUGE, AFTER A COUPLE OF MINUTES INDICATION CAME BACK BUT WAS FLUCUATING, CREW REDUCED ENGINE POWER BUT DID NOT SHUTDOWN ENGINE, ON DESCENT EVERYTHING RETURNED TAug 30, 2007 · N138UP · Airbus A300F4622R · Engine Oil PressureSDR UPS07150343Panel · crackedDURING REMOVAL AND REPLACEMENT OF AFT LOWER CARGO CEILING PANEL FOUND SUPPORTING STRUCTURE CRACKED AND DENTED. REMOVED DAMAGE AND REPAIRED IAW EO A300-5320-27329-A AND RESTORED FINISH IAW SRM 51-23-10.Jul 29, 2007 · N152UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR UPS07150347Floorboard · puncturedINSPECTION TYPE: N/A (2) PUNCTURES IN FLOOR BOARD AS POSITION 1. REPAIRED (2) HOLES IAW SRM 53-10-20.Jun 21, 2007 · N127UP · Airbus A300F4622R · Fuselage Floor PanelSDR 06FDEA03630Computer · malfunctionedPDIS 728 77-10 0804 13OCT06 GSO RECD ENG 2 N1 MODE. ONLY MAINTENANCE - CLEARED ITSELF ON T/O ROLL RECD SAME WARNING. REFECT T/O AT 60KTS. FOLLOWED ALL ECAM/RED TABS. FADEC WAS SELECTED TO N1 MODE FOR BOTH ENGINES. FACT 13OCT06 04:47 GSO R REMOVED AND REPLAOct 13, 2006 · N728FD · Airbus A300F4622R · Central ComputersSDR 06FDEA03631Module · malfunctionedPDIS 720 34-11 0002739 13OCT06 ORD CLOSE R 1ST RTO OF 2 F/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. OFF MFG 404Oct 13, 2006 · N720FD · Airbus A300F4622R · Pitot/Static System
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