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 IPXA11164042Floor Panel · damagedINSPECTION TYPE:5 YR, REPAIR VALIDATION SURVEY, REPAIR OF BULK CARGO FLOOR PANEL 162HF. REPAIR OF BULK CARGO FLOOR PANEL 162HF BY FABRICATION ACCOMPLISHED IAW EO A300-5320-16407-E, APPX D.Dec 26, 2010 · N172UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA1164217Floorboard · damagedINSPECTION TYPE:3C, REPAIR VALIDATION SURVEY, REPAIR OF AFT BULK PIT FLOOR APPROX 2FT INBD OF DOOR THRESHOLD. FABRICATED BULK PIT FLOORBOARD NR161LF IAW EO A300-5320-16407-E, APPENDIX D.Dec 26, 2010 · N154UP · Airbus A300F4622R · Fuselage Floor PanelSDR FDEA201012224736Valve · malfunctionedAFTER T/O ECAM INDICATED SLATS SYS 2 FAULT AND OVER-HEAD INDICATED SLATS SYS 2 FAULT LIGHT ILLUMINATED. CREW CYCLED SLATS TWICE - SLATS AND FLAPS WERE NORMAL AFTER SECOND CYCLE - LIGHT REMAINED ILLUMINATED. NR 2 SFCC FAULTED HIGH SPEED VALVE. REPLACED SLAT Dec 22, 2010 · N726FD · Airbus A300B4622R · Leading Edge Slat Control SystemSDR IPXA10163905Warning System · no testCREW REPORTED EVACUATION SLIDE WARNING SYS LIGHT DID NOT TEST, BUZZER IS GOOD. TS IAW FIM 52-73-00, FIG 102. R & R ESCAPE SLIDE IND LIGHT IAW AMM 52-73 -11-04. OPS CK GOOD. C/W WAN NR1703356. THIS CLEARS DEFERRAL M442679.Dec 21, 2010 · N122UP · Airbus A300F4622R · Escape SlideSDR IPXA0163869Controller · inoperativeAFTER T/O, FLAPS 15/20 DEGREES WOULD NOT RETRACT. FLAP SYS 1 & 2 FAULT, DIVERTED. NR1 SFCC SHOWS ALL 5 FLAPS FAIL IND ILLUM INDICATING SFCC FAILURE REPLACED NR1 SFCC IAW FIM 27-50-10, FIG 101, AMM 27-51-18-04. FOUND LT FLAP TORQUE LIMITER IND TRIPPED. LUBDec 16, 2010 · N130UP · Airbus A300F4622R · Trailing Edge Flap Control SystemSDR IPXA0163859Module · inoperativeLANDING GEAR WOULD NOT RETRACT. ECAM MESSAGE LANDING GEAR RETRACT INOP. SWITCHED FROM SYS 2 TO SYS 1. NO HELP. HANDLE WOULD NOT MOVE FROM MIDDLE POSITION. C/W FIM 32-30-00 BLOCK 1, 2 AND 5. FOUND BAD LEVER MODULE ASSY. TSM 32-30-00 C/W TESTS/OPS CK C/W REFDec 15, 2010 · N120UP · Airbus A300F4622R · Landing Gear Retraction/Extension SystemSDR IPXA10163810Slide · unwanted deployCREW INADVERTENTLY DEPLOYED DOOR SLIDE. DOOR SLIDE REMOVED AND DEF 441338 ASSIGNED. SUPPLEMENTAL ETOPS REPORT, INSTALLED SERVICEABLE SLIDE, GIRTBAR, SLIDERS AND COVER IAW AMM 25-61-21-04. OK FOR SERVICE. STICKER REMOVED. M441338 CLEARED.Dec 9, 2010 · N120UP · Airbus A300F4622R · Escape SlideSDR IPXA10163770Skin · dentedRR INBD FLAP HAS DAMAGE CONSISTING OF A DENT IN LWR MAIN SKIN ASSY WITH A GOUGE. REPAIRED REF EO-A300-5750-37685-B.Dec 6, 2010 · N128UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA10163793Skin · dentedRT INBD FLAP LOWER SKIN DENT 18" FROM FWD EDGE. THIS IS CLASSIFIED AS A MAJOR REPAIR. TRANSFERRED TO NR 355102. COMPLETED REPAIR IAW EO A300-5750-37685-B. THIS IS A PERMANENT REPAIR AND CLEARS D424774.Dec 6, 2010 · N128UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA0163740Computer · inoperativeAFTER ROTATION GOT A MASSIVE VIBRATION IN THE CAPT & F/O YOKE. CREW DID AIR TURN BACK. NO INDICATIONS ON ECAM OR ROUND DIALS. DURING RETURN NUMEROUS ECAM MESSAGES WITH STICK SHAKER. AFTER LANDING ROLLOUT STICK SHAKER REMAINED ON. REPLACED 48FU1 RELAY. Nov 30, 2010 · N139UP · Airbus A300F4622R · Stall Warning SystemSDR FDEA201011264495Valve · malfunctionedDURING SLAT RETRACTION ECAM IND SLAT SYS 2 FAULT WITH OVERHEAD LIGHT ON. CYCLED HANDLE NO JOY. SPFI INDICATED SLATS UP. ZIPPER AND HOOK WORKED NORMALLY, CONSULTED QRH, DID NOT COVER FAULT WITH SLATS ACTUALLY UP. WITH BOTH VISUAL AND SPFI INDICATING FLAPSNov 26, 2010 · N726FD · Airbus A300B4622R · Leading Edge Slat Control SystemSDR FDEA201011234477Warning Light · false activationAVIONICS SMOKE LIGHT ILLUMINATED AND WENT OUT 3 TIMES BEFORE WE COULD LAND. NO SMOKE NOTED IN COCKPIT OR IN SNIFFER FAN. TEMP INSTALLED 13WA PARTS ON ORDER R & R 11WA REF MM 26-15-12-04. PREMATURE REMOVAL/INSTALLATION.Nov 23, 2010 · N730FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201011234474Smoke Detector · failedAVIONICS SMOKE INDICATION PASSING 13000'. CHECKED AVIONICS COMPARTMENT SMOKE DETECTION USING MM-26-15-00-05 OPS NORMAL. AS A PRECAUTION R&R COCKPIT AND AVIONICS SMOKE DETECTORS. USING MM-26-15-12-04. ALSO OPS NORMAL. ACFT OK FOR SERVICE.Nov 23, 2010 · N741FD · Airbus A300B4622R · Fire DetectionSDR FDEA201011234476Smoke Detector · false activationAVIONICS SMOKE LIGHT ILLUMINATED AND WENT OUT 3 TIMES BEFORE WE COULD LAND. NO SMOKE NOTED IN COCKPIT OR IN SNIFFER FAN. MEM R DET 13WA NEEDS NEW CLAMP REF IPC 26-15-01-07 ITEM 40. QTY 1 CLAMP, TEMP INSTALLED 13WA PARTS ON ORDER R & R 11WA REF MM 26-15-12-Nov 23, 2010 · N730FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201011174405Control Handle · inoperativeSELECTED THE LANDING GEAR LEVER DOWN WITH THE POSITION DET IN SYS 1. RECEIVED 3 GREEN DOWN INDICATIONS AND 3 RED UNLK INDICATIONS ON THE FWD PNL INDICATING SYS. THE INDICATING SYSTEMS ON THE OVERHEAD PNL WERE ALL GREEN. RELEASED FOR SERVICE IAW MEL: 32-61-01Nov 17, 2010 · N726FD · Airbus A300B4622R · Landing Gear SelectorSDR IPXA0163613Skin · damagedREF LOG PAGE 434115 ITEM 1, REF D412751 FUSELAGE EXTERNAL REPAIR DOUBLER DMG ADJACENT TO FR85 AND L45. REPAIRED IAW EO A300-5330-35623D.Nov 16, 2010 · N138UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA0163604Skin · damagedFUSELAGE SKIN DAMAGED FR 85. REPAIRED IAW EO A300-5330-35623-C.Nov 15, 2010 · N138UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR FDEA201011114317Landing Gear · malfunctionedLG WOULD NOT RETRACT. HANDLE WENT TO RETRACT POSITION BUT LG NEVER CAME UP. COMPLIED WITH TEST OF PROXIMITY DETECTOR PROCESSING UNIT (54GB) IAW TSM 32-61-00. NO FAULTS NOTED AT THIS TIME. GEAR PINS INSTALLED. PERFORMED TEST OF LANDING GEAR ELECTROVALVE (3GANov 11, 2010 · N750FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR FDEA201011104316Selector Valve · inoperativeLG WOULD NOT RETRACT. HANDLE WENT TO RETRACT POSITION BUT LG NEVER CAME UP. JACKED A/C VERIFIED VALVE 3GA FAULTY REMOVED AND REPLACED VALVE IAW MM 32-31-12-04. ALSO REMOVED AND REPLACED MODULE LANDING GEAR CONTROL HANDLE (2GA) IAW MM 32-32-11-04-0. PERFORMNov 10, 2010 · N750FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR IPXA0163593Light · inoperativeLAVATORY AUXILIARY LIGHT IS INOP. RELAMPED LAVATORY AUXILIARY LIGHT ASSY IAW AMM 33-24-00-00. OPS CHECK GOOD IAW AMM 33-51-00-05. OK FOR SERVICE.Nov 9, 2010 · N134UP · Airbus A300F4622R · Emergency LightingSDR IPXA10163564Solenoid Valve · inoperativeON TAKEOFF, SLAT SYS 2 FAULT LIGHT ECAM SLAT SYS 2 FAULT ILLUMINATED OVERHEAD PANEL. R & R SOLENOID VALVE ON VALVE BLOCK 26CV REF MM 27-84-33-04. FOLLOWED FIM 27-80-05, STEP 1 TO A2-6-13. ENABLE SOLENOID VALVE HAD RESISTANCE VALVE OF 69 OHMS. OPS CK OF SYS 2Nov 6, 2010 · N138UP · Airbus A300F4622R · Leading Edge Slat Control SystemSDR IPXA10163515Floor Panel · puncturedDAMAGED BULK PIT FLOOR PANEL. REPAIRED IAW SRM 53-10-20, FIG 207.Nov 2, 2010 · N127UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163391Isolation Valve · failedRIGHT INNER ISOLATION VALVE WOULD NOT OPEN IN FLIGHT. DIVERTED, OPS CHECKED AUTO FEED SYS IAW MM 28-21-00-05, PARA 2. THIS CLEARS M437998. PLACARD REMOVED.Oct 27, 2010 · N141UP · Airbus A300F4622R · Aircraft Fuel Distribution SystemSDR IPXA10163366Light · inoperativeEXIT LIGHT OVER CREW ENTRY DOOR INOP. ACCOMPLISHED SUPERNUMARY AREA EMERGENCY LIGHTING ADJ/TEST. ALL LIGHTS CHECKED GOOD IAW MM 33-51-00-05.Oct 26, 2010 · N128UP · Airbus A300F4622R · Emergency LightingSDR IPXA10163368Gauge · out of positionAFTER LANDING NOTICED EMERGENCY SLIDE GAUGE IS NO LONGER VISIBLE IN THE CREW ENTRANCE DOOR. CLOSED FWD ENTRY DOOR AND INSPECTED SLIDE GAUGE THRU ENTRY DOOR SIGHT GLASS. EMERGENCY SLIDE GAUGE IS VISIBLE & READABLE.Oct 26, 2010 · N143UP · Airbus A300F4622R · Escape SlideSDR IPXA10163315Skin · damagedDAMAGE ON FUSELAGE SKIN FR58 STR 36R AND 37R. REPAIRED IAW EO A300-5330-33844-C.Oct 24, 2010 · N145UP · Airbus A300F4622R · Fuselage Main, Plate/SkinSDR IPXA10163279Fitting · dirtyCABIN DOOR SLIDE DISARMING LEVER FELT UNUSUAL WHEN DISARMING SLIDE. FOUND AND CLEANED DEBRIS AT AFT GIRT BAR FITTING. OPERATED ARM SLIDE HANDLE, OPS CK NORMAL IAW MM 52-10-30-06.Oct 21, 2010 · N146UP · Airbus A300F4622R · Emergency EquipmentSDR IPXA10163345Floor Panel · crackedINSPECTION TYPE:1C, MCD FLOOR PANEL 232LF IS CRACKED AT LOWER SURVACE AS MARKED. REPAIRED CRACK IAW SRM 53-10-20, FIG 203. SHEET 2 AND EO A300-5320-38221-B.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163346Floorboard · puncturedINSPECTION TYPE:5 YR, MAIN CABIN FLOORBOARD 231AH HAS A PUNCTURE. REPAIRED FLOORBOARD IAW SRM 53-10-20, PARA 8B, FIG 102. AND EO A300-5320-38221-B.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163355Floorboard · delaminatedINSPECTION TYPE:5 YR, MAIN CABIN FLOORBOARD NR 232 AH IS DELAMINATED. REPAIRED FLOORBOARD IAW SRM 53-10-20 PARA 8B, FIG 203, AND EO A300-5320-38221-B.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163393Floor Panel · crackedINSPECTION TYPE:5 YR, MCD FLOOR PANEL 241HF IS CRACKED AT EDGE. FABRICATED NEW FLOOR PANEL IAW EO A300-5320-16407-E.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163398Floor Panel · delaminatedINSPECTION TYPE:5 YR, MDC FLOOR PANEL 231PJ DELAMINATED. FABRICATED FLOOR PANEL IAW A300-5320-16407-E.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163400Floorboard · delaminatedINSPECTION TYPE:5 YR, MAIN CABIN FLOORBOARD 231QJ IS DELAMINATED. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163403Floor Panel · crackedINSPECTION TYPE:5YR, MCD FLOOR PANEL 252VJ IS CRACKED AT LOWER SURFACE REPAIRED FLOOR PANEL IAW A300 SRM 53-10-20 PARA 8B, FIG. 203Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163409Floorboard · crackedINSPECTION TYPE:5YR, MAIN CABIN FLOORBOARD NR 231XG HAS A CRACK. REPAIRED FLOORBOARD IAW SRM 53-10-20, PARA 8B, FIG 203 AND EO A300-5230-38221-B.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163412Floorboard · crackedINSPECTION TYPE:5YR, MAIN CABIN FLOORBOARD 231WG HAS A CRACK. REPAIRED FLOORBOARD IAW SRM 53-10-20 8B FIG 203 AND EO A300-5320-38221-B.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163436Floor Panel · delaminatedINSP TYPE:5 YR MCD FLOOR PANEL 231GH DELAMINATED. FABRICATED MAIN CARGO DECK FLOOR PANEL 231GH REF EO A300-5320- 16407-E APPX A AND B.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163438Floor Panel · crackedINSPECTION TYPE:5 YR, FWD PIT FLOORBOARD PANEL 131BH HAS A CRACK. FABRICATED LOWER, FWD CARGO COMPT FLOOR PANEL 131BH REF EO A300-5320-16407-E APPX A AND C.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163455Floor Panel · delaminatedINSPECTION TYPE:5YR, FLOOR PANEL 231KJ DELAMINATED. FABRICATED MAIN DECK FLOOR PANEL 231KJ REF EO A300-5320-16407, APPX A AND B.Oct 21, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163394Floor Panel · brokenINSPECTION TYPE:5 YR, MDC FLOOR PANEL 241YR BROKEN. FABRICATED FLOOR PANEL IAW EO A300-5320-16407-E.Oct 20, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163401Floorboard · crackedINSPECTION TYPE:5 YR, MAIN CABIN FLOORBOARD 241BQ HAS A CRACK. REPAIRED FLOORBOARD IAW SRM 53-10-20 PARA 8B, FIG. 203 AND EO A300-5320-38221-B.Oct 20, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163404Floorboard · crackedINSPECTION TYPE:5YR, MAIN CABIN FLOORBOARD NR 242VM IS CRACKED UNDER SURFACE REPAIRED FLOORBOARD IAW SRM 53-10-20, PARA 8B, FIG 203 AND EO A300-5320-38221-B.Oct 20, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163405Floor Panel · crackedINSPECTION TYPE:5YR, MCD FLOOR PANEL 242TK IS CRACKED AT LOWER SURFACE AS MARKED. REPAIRED MCD FLOOR PANEL IAW 53-10-20, PARA 8B, FIG 203 AND EO A300-5320-38221-B.Oct 20, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163406Floor Panel · crackedINSPECTION TYPE:5YR, MDC FLOOR PANEL 241UK CRACKED UNDER SURFACE. REPAIRED FLOOR PANEL IAW EO A300-5320-3221-B AND SRM 53-10-20 PARA 8B, FIG 203.Oct 20, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163408Floorboard · crackedINSPECTION TYPE:5YR, MAIN CABIN FLOORBOARD 242YK HAS 3 EA CRACKS. REPAIRED FLOORBOARD IAW SRM 53-10-20 8B FIG 203, EO A300-5320-38221-B, SRM 53-10-20 PARA 8A, FIG 201 & 202, AND EO A300-5320-38334-A.Oct 20, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163336Floor Panel · crackedINSPECTION TYPE:5YR, MAIN CARGO FLOOR PANEL 251CH IS CRACKED AT LOWER SURFACE. FABRICATED MAIN CARGO FLOOR PANEL 251CH IAW EO A300-5320-16407-E, APPENDIX A/B.Oct 19, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163337Floor Panel · brokenINSPECTION TYPE:5YR, MAIN CABIN FLOOR PANEL 252KM BROKEN. FABRICATED MAIN CABIN FLOOR PANEL 252KM IAW EO A300-5320-16407-E, APPENDIX A/B.Oct 19, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163338Floor Panel · brokenINSPECTION TYPE:5YR, MAIN CARGO FLOOR PANEL 252FM IS BROKEN. FABRICATED MAIN CABIN FLOOR PANEL 252FM IAW EO A300-5320-16407-E, APPENDIX A/B.Oct 19, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163347Floor Panel · crackedINSPECTION TYPE:5 YR, MCD FLOOR PANEL 251J IS PEELED AND CRACKED AT LOWER SURFACE AS MARK. REPAIRED DAMAGE FLOOR PANEL IAW A300 53-10-20 PARA 8B, FIG. 203,Oct 19, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA10163349Floor Panel · crackedINSPECTION TYPE:5 YR, MCD FLOOR PANEL 251ZG IS CRACKED AT LOWER SURFACE AS MARKED. REPAIRED DAMAGE IAW 53-10-20 PARA 8B AND FIG 203, AND EO A300-5320-38221-B.Oct 19, 2010 · N170UP · Airbus A300F4622R · Fuselage Floor Panel
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