Boeing 747-428F

Service difficulty reports · 284

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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 aircraft_model_key = '747428F'
  ORDER BY difficulty_date DESC"

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SDR WRNA201511200002Fan · overheatedAT TOP OF CLIMB ELECTRONIC EQUIPMENT COOLING GROUND EXHAUST VALVE FAIL MESSAGE. WHEN SWITCHED ELECTRONIC EQUIPMENT COOLING TO OVERRIDE POSITION, CONTINUED TO HAVE THE OVERHEAT PROBLEM CAUSING A RETURN TO DEPARTURE.Nov 18, 2015 · N904AR · Boeing 747428F · Air Distribution FanSDR IPXA2015110195371Skin · not reportedRT T/E FLAP 1.25" DIA CUTOUT FULL CORE DEPTH FROM LOWER SKIN REPAIRED IAW EOB747-5750-59109-A, SRM REV 75, CHP 57-53-01. REPAIR 1 AND SRM, REV 75, CHP 51-70-10-2R, REPAIR 2.Nov 1, 2015 · N580UP · Boeing 747428F · Trailing Edge FlapsSDR IPXA2015082492654Floor Panel · damagedMAIN DECK FLOOR PANEL DAMAGED AT BS 460. COMPLETED NR 578425. MAJOR REPAIR.Aug 24, 2015 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA2015072291416Controller · inoperativeDIVERSION, RECEIVED BLEED 1 ADVISORY EICAS MSG AND BLEED OVERPRESS 1 STATUS LVL MESSAGE. FOUND CMC FAULT MSG 36226, PRV & CONTROLLER FAIL. R & R WITH NEW PRV & CONTROLLER IAW AMM 36-11-13 & 36-11-20. THEN OPS TEST OF NR 1 ENGINE PRV WITH ENGINE IDLE RUN . WJul 17, 2015 · N580UP · Boeing 747428F · Pneumatic Distribution SystemSDR IPXA2015041988200Floor Panel · damagedFLOOR PANEL, DAMAGED. FABRICATED A NEW FLOOR PANEL.Apr 19, 2015 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR WRNA201504020004Engine · vibrationDURING DECENT THE NR 1 ENGINE, N2 VIBRATION PEAKED AT 4.5, 15,000 FEET, INDICATED AIRSPEED 300 KNOTS, FLIGHT IDLE POWER.Mar 31, 2015 · N902AR · Boeing 747428F · Engine (Turbine/Turboprop)SDR IPXA2015022586443Relay · inoperativeC/B FOR STANDBY POWER TRANSFER RELAY POPPING ON P6-6 PANEL. ONLY IF STBY POWER IN AUTO POS. R & R STANDBY POWER TRANS RELAY IAW AMM 24-29-03-004 & 404. STBY POWER SYSTEM TEST GOOD.Feb 25, 2015 · N580UP · Boeing 747428F · AC Power Distribution SystemSDR IPXA2015011985338Frame · crackedINSPECTION TYPE: CM, BS 2231 FRAME ANGLE AT S16L WAS FOUND CRACKED. REPAIRED IAW RI-53-60-10809 REV A & EO 5310-56475-A.Jan 9, 2015 · N580UP · Boeing 747428F · Fuselage Main, FrameSDR IPXA2015011985339Frame · crackedINSPECTION TYPE: CM, BS 2231, S17L FOUND CRACKED AT FRAME INNER ANGLE. REPAIRED IAW RI-53-60-10809 REV A AND EO B747-5310-56475-A.Jan 8, 2015 · N580UP · Boeing 747428F · Fuselage Main, FrameSDR IPXA2015011985336Frame · crackedINSPECTION TYPE:CM, DECK BS 2231, CRACKS WERE FOUND AT 2 EA HOLE BETWEEN S24 & S25 CRACK LOCATED AT FRAME INNER CHORD, UPPER HOLE RUNNING FORWARD WITH 0.060" AND LOWER HOLE WITH 0.040" LONG. M/DECK BS2231 STR 24L TO STR 25L FRAME FWD INNER CHORD IS REPAIRED IJan 8, 2015 · N580UP · Boeing 747428F · Fuselage Main, FrameSDR IPXA2015011985335Frame · crackedINSPECTION TYPE: CM. BS 2231 S25L, ONE HOLE WAS FOUND CRACKED AT FRAME INNER ANGLE, CRACK RUNNING FORWARD 0.060" LONG APPROXIMATELY. REPAIRED IAW SRM 53-60-15-2R-2, FIG 201, REV 71 ORIGINAL MATERIAL 65B01849-7 WITH CRACK LENGTH 0.060" RUNNING FWD. FINAL TRIJan 8, 2015 · N580UP · Boeing 747428F · Fuselage Main, FrameSDR IPXA2015011985340Skin · crackedINSPECTION TYPE: C, BS 980 SKIN FOUND CRACKED . REPAIRED SRM 53-20-01-2R-2, FIG 201 & RI-53-20-10804 REV A & EO 5330-56459-A.Jan 6, 2015 · N580UP · Boeing 747428F · Fuselage Main, Plate/SkinSDR WRNA201501080028Control Unit · malfunctionedTHE CREW REPORTED TAKEOFF WAS SMOOTH AND UNEVENTFUL. NOTICED AN OUT OF TRIM AND OPPOSITE RUDDER TRIM. RT INBD AILERON DEFLECTED TO FULL DOWN POSITION DURING FLIGHT AND WAS UNABLE TO ENGAGE AUTOPILOT. DIVERTED AND DUMPED APPROXIMATELY 25 MINUTES OF FUEL PJan 5, 2015 · N902AR · Boeing 747428F · Aileron Control SystemSDR IPXA2014102484700Warning Message · activatedINDOOR F/D OVHD EICAS MESSAGE. PRESSURE GOOD. CLEANED AND EXERCISED FWD OVERHEAD HATCH, SWITCH S02312, INDICATIONS NORMAL WHEN DOOR CYCLED OPEN/CLOSED.Oct 24, 2014 · N580UP · Boeing 747428F · Door Warning SystemSDR IPXA2014100684521Priority Valve · inoperativeBLEED 3 EICAS CAUTION MESSAGE, TURNED NR 3 BLEED OFF IAW CHECKLIST REVIEWED CMC AND FOUND NR 3 BLEED DURING THE CLIMB STATUS, ENGINE DUCT PRESSURE UP TO 110 PSI, BLEED AIR PRESSURE WARNING COMING UP, CMC MSG 36228 BLEED-3 PRV/CONTROLLER FAIL OPEN, REFER TO FIMOct 3, 2014 · N580UP · Boeing 747428F · Pneumatic Distribution SystemSDR IPXA2014081383974Fire Detector · malfunctionedAFT CARGO FIRE EICAS WARNING ANNUNICATED AFTER LEVELING OFF AT FL 340. DECLARED EMERGENCY, JETTISONED FUEL, RETURNED TO DEPARTURE. AFT CARGO FIRE LOOP A FAILED TEST. FOUND FAILED DUE TO MOISTURE AND FOG. SWAPPED SMOKE DETECTOR TO FWD CARGO LOOP AND BOTH DAug 12, 2014 · N580UP · Boeing 747428F · Smoke DetectionSDR IPXA2014033182461Skin · dentedRT WING INBD MID FLAP HAS TWO DENTS ON LWR SURFACE OTBD END. COMPLETED MAJOR REPAIR OF RT WING INBD MID FLAP IAW EOB747-5750-53923-A.Mar 30, 2014 · N580UP · Boeing 747428F · Trailing Edge FlapsSDR IPXA2013121801075Handle · out of positionPASSING FL200 EICAS MSG "DOOR F/D OVHD" QRH CHECKLIST COMPLETED. FOUND F/D HATCH HANDLE WAS A LITTLE OFF THE LINE, HATCH OPEN AND CLOSE. OPS CHECK, COND NORMAL, NO FAULT FOUND IAW AMM 52-21-00.Dec 16, 2013 · N580UP · Boeing 747428F · Emergency ExitsSDR IPXA3B79306Seat Track · corrodedINSPECTION TYPE: D, MAIN DECK BS 995 LBL 33, SEAT TRACK FLANGE FOUND CORRODED BS 970 TO 1000 LBL 33. SEAT TRACK IS REPAIRED IAW SRM 53-00-52-2R-6, FIG 201, REV 66 ALTERNATIVE 1.Jul 9, 2013 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA3B79351Floorbeam · crackedINSPECTION TYPE:D, RT UPPER DECK BS 340 ONE HOLE FOUND CRACKED ONE FLOORBEAM WEB. FLOORBEAM REPAIRED IAW RI-53-12-10238, REV A & 5310-31309-A IS CLASSIFIED A MAJOR REPAIR.Jun 26, 2013 · N580UP · Boeing 747428F · Fuselage Main, Floor BeamSDR IPXA3B79349Floorbeam · damagedINSPECTION TYPE: D, DURING EO, ACCOMPLISHED LT BS 520 STRAP AND EXISTING FLOORBEAM FOUND AT OTBD AREA 2EA HOLES AREA LESS THAN DWG SHOWN ONE EXISTING HOLE IS ALREADY OVERSIZED TO 0.0250" DIA. REPAIRED IAW RI-53-15-10220, REV A & B747-5310-51295-A. CLASSIFIEDJun 25, 2013 · N580UP · Boeing 747428F · Fuselage Main, Floor BeamSDR IPXA3B79281Floor Panel · damagedINSPECTION TYPE: D, MAIN DECK BS 860-980, LBL 11-33, FLOOR PANEL FOUND CRACK AND BROKEN. FLOOR PANEL FABRICATED IAW DWG 65B23341-29 AND INSTALLED IAW AMM 53-21-02.Jun 24, 2013 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA13B79232Floor Panel · brokenINSPECTION TYPE:D UPPER DECK BS 380-384, RBL 11-40 FLOOR PANEL FOUND BROKEN. FLOOR PANEL FABRICATED IAW DWG 141U5876-15 AND INSTALLED IAW AMM 53-21-02.Jun 24, 2013 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA13B79173Fairing · delaminatedINSPECTION TYPE:D, LEFT WING OTBD MID FLAP L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 66 .Jun 24, 2013 · N580UP · Boeing 747428F · Trailing Edge FlapsSDR IPXA3B79287Splice Plate · crackedINSPECTION TYPE: D, BS 400, S44-45L NLG WW LT AFT CORNER TWO FASTENERS CRACKED, FOUND AT SPLICE PLATE. SPLICE PLATE REPLACED AND INSTALLED IAW HS RI-53-11-10214, REV A & EO B747-5330-51303-A, REPAIR CLASSIFIED AS MAJOR.Jun 22, 2013 · N580UP · Boeing 747428F · Fuselage Miscellaneous StructureSDR IPXA13B79172Panel · delaminatedINSPECTION TYPE:D, RT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 66.Jun 21, 2013 · N580UP · Boeing 747428F · Trailing Edge FlapsSDR IPXA3B79353Floorbeam · crackedINSPECTION TYPE: D, BS 380, UPPER DECK FLOORBEAM, ONE FASTENER HOLE FOUND CRACKED. FLOORBEAM REPAIRED IAW RI-53-15-10232, REV A & B747-5310-51314-A. REPAIR CLASSIFIED AS A MAJOR REPAIR.Jun 20, 2013 · N580UP · Boeing 747428F · Fuselage Main, Floor BeamSDR IPXA3B79348Floorbeam · crackedINSPECTION TYPE: D, BS 380 LT UPPER DECK FLOORBEAM ONE FASTENER HOLE FOUND CRACKED AT 4TH LAYER FROM AFT. BS 380 FLOORBEAM WEB REPAIRED IAW RI53-15-10232, REV A & 5310-51314-A, CLASSIFIED AS A MAJOR REPAIR.Jun 20, 2013 · N580UP · Boeing 747428F · Fuselage Main, Floor BeamSDR IPXA3B79307Skin · crackedINSPECTION TYPE:D, FX LT SIDE SKIN PANEL AT AFT CORNER OF NLG W/W FOUND CRACKED. FX LT SIDE SKIN PANEL AT BS400 AFT CORNER OF NLG W/W AREA IS REPAIRED IAW HX RI-53-11-10214 REV.A & EO B747-5330-51303-A, REPAIR CLASSIFIED AS MAJOR.Jun 20, 2013 · N580UP · Boeing 747428F · Fuselage Main, Plate/SkinSDR IPXA13B79175Skin · delaminatedINSPECTION TYPE:D, LEFT WING OTBD MID FLAP OTBD L/E AREA DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 66.Jun 20, 2013 · N580UP · Boeing 747428F · Trailing Edge FlapsSDR IPXA13B79174Skin · delaminatedINSPECTION TYPE: D, LEFT WING OTBD FORE FLAP OTBD L/E AREA DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR PERFORMED IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 66.Jun 20, 2013 · N580UP · Boeing 747428F · Trailing Edge FlapsSDR IPXA3B79352Floorbeam · crackedINSPECTION TYPE: D, RT BS 340 UPPER DECK FLOORBEAM, ONE FASTENER HOLE FOUND CRACKED. FLOORBEAM REPAIRED IAW RI-53-12-10238, REV A & 5310-51309-A, REPAIR CLASSIFIED A MAJOR REPAIR.Jun 19, 2013 · N580UP · Boeing 747428F · Fuselage Main, Floor BeamSDR IPXA3B79309Floorbeam · crackedINSPECTION TYPE: D, BS 380 FLOORBEAM, ONE FASTENER HOLE FOUND CRACKED AT FRAME WEB. REPAIRED IAW HX RI-53-12-10234, REV A & EO B747-5310-51312-A, REPAIR CLASSIFIED AS MAJOR.Jun 19, 2013 · N580UP · Boeing 747428F · Fuselage Main, Floor BeamSDR IPXA13B79171Fairing · damagedINSPECTION TYPE:D, LEFT WING INBD AFT FLAP L/E FAIRING PUNCH HOLE FIBERGLASS PREPREG LAY UP REPAIR. PERFORMED IAW SRM 51-70-07, PAR 5A (1), FIG 5, REV 66.Jun 18, 2013 · N580UP · Boeing 747428F · Trailing Edge FlapsSDR IPXA13B79231Floor Panel · delaminatedINSPECTION TYPE:D, BS 660-760, RBL 33-75 FLOOR PANEL FOUND SEVERAL PUNCTURES DENTS AND SURROUNDING EDGE DELAMINATION. FLOOR PANEL REPLACED IAW DWG 65B38454-16 AND INSTALL IAW AMM 53-21-02.Jun 15, 2013 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA13B79230Floor Panel · delaminatedINSPECTION TYPE:D, BS 760-860, RBL 33 - 75, FLOOR PANEL FOUND SEVERAL PUNCTURES DENTS AND SURROUNDING EDGE DELAMINATION. FLOOR PANEL REPLACED IAW DWG 65B38459-6 AND INSTALLED IAW AMM 53-21-02.Jun 15, 2013 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA12B76575Skin · wornLT OTBD AILERON UPPER SKIN AT INBD END NEAR T/E WEDGE. REPAIRED IAW EO B747-5750-49455-A.Dec 31, 2012 · N580UP · Boeing 747428F · AileronsSDR IPXA2B76530Floor Panel · damagedONE INCH HOLE IN MAIN CARGO DECK FLOOR PANEL FS 700, LBL 114. REPAIRED IAW SRM 53-00-50-2R-1.Dec 25, 2012 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA2B76529Floor Panel · damaged1 X .5 INCH, HOLE MAIN CARGO DECK FLOOR PANEL AT BS 285, RBL 24. REPAIRED IAW SRM 53-00-50-2R-1.Dec 25, 2012 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA2B76523Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL FS 1719-1797 DAMAGED, FABRICATED IAW EO B747-5320-49386-A.Dec 24, 2012 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA2B76522Floorboard · damagedTOP SKIN DAMAGED ONLY TO MAIN CARGO DECK FLOORBOARD. REPAIRED REF SRM B747-53-00-50-2R-1.Dec 24, 2012 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA12B75943Battery Pack · inoperativeMAIN DECK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IAW MM 33-51-04-902. OPS NORMAL.Oct 16, 2012 · N580UP · Boeing 747428F · Emergency LightingSDR IPXA12B75942Power Supply · inoperativeEMERGENCY LIGHTS AT L1 DOOR ARE INOPERATIVE. TROUBLESHOT IAW WDM 33-51-72. REPLACED POWER SUPPLY M-5170.Oct 16, 2012 · N580UP · Boeing 747428F · Emergency LightingSDR IPXA2B72324Skin · damagedINSPECTION TYPE: C, LEFT WING OTBD AFT FLAP LWR SURFACE FOUND DAMAGED HOLE METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 2, REV 60.Mar 6, 2012 · N580UP · Boeing 747428F · Trailing Edge FlapsSDR IPXA12B71836Bottle · lowSLIDE BOTTLE PRESSURE READS IN YELLOW RANGE ON GAUGE. OPENFeb 17, 2012 · N580UP · Boeing 747428F · Escape SlideSDR IPXA1B66675Floor Panel · damagedMCD HOLE IN FLOOR PANEL AT APPROX STA 1860, CTR BETWEEN CTR PDU'S RBL 7. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-42712A.May 16, 2011 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA1B66674Floor Panel · damagedMCD HOLE IN FLOOR PANEL AT APPROX STA 1840, RBL 7. FABRICATED NEW FLOOR PANEL IAW EO B747-5320-42712-A.May 16, 2011 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA1B66673Floor Panel · damagedMC DECK HOLE IN FLOOR INBD OF LT AFT EMERGENCY DOOR AT ST 2280L, LBL 5. REPAIRED IAW SRM 53-00-50, R1.May 16, 2011 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA1B66672Floor Panel · damagedMC DECK HOLE IN FLOOR 1B OF LT/FWD ENTRY DOOR LBL 88.5. REPAIRED IAW SRM 53-00-50, R1.May 16, 2011 · N580UP · Boeing 747428F · Fuselage Floor PanelSDR IPXA1B66671Floor Panel · damagedHOLE IN FLOOR STA 390, LBL 35. REPAIRED IAW SRM 53-00-50.May 16, 2011 · N580UP · Boeing 747428F · Fuselage Floor Panel
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