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 IPXA2025021901235Skin · crackedCRACK - SKIN , STA 2658 BETWEEN S-11L AND S-12L (REPAIR). REPAIR DAMAGE AREA I.A.W UPS EO-92807-REQ1 REV.1 AND SRM 53-80-01-2R-4 REV.102 EGAT WORK SHEET NO.50053. JOB COMPLETED.Jan 21, 2025 · N580UP · Boeing 747428F · Fuselage Main, Plate/SkinSDR IPXA2025021801198Cargo Track · corrodedCORROSION - CARGO TRACK , AFT CGO COMPARTMENT STA 1890~1920 RBL 11 OF MAIN DECK FLOOR STRUCTURE. (REPAIR). I.A.W AMM 53-21-02-404-006 REV.112 INSTALL MAIN DECK CARGO FLOOR PANEL AT STA 1890 ~ 1920 LBL11 AND CONDITION CHECK NORMAL. REPAIR DAMAGE AREA I.A.W SRMJan 21, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025021800339Cargo Track · corrodedCORROSION - TRACK , AFT CGO COMPARTMENT STA 1772 LBL 35 OF MAIN DECK FLOOR STRUCTURE. REMOVE DAMAGE PART I.A.W SRM 51-40-02-0G REV.102. FABRICATE P/N:69B04257-1 PER BOEING DWG NO.69B04257 SH1 REV."E", PL REV."A" AND EGAT WORK SHEET NO.50056 AND ORIGINAL PART Jan 21, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025021600257Plate · corrodedCORROSION - PLATE , AFT CGO COMPARTMENT STA 1780 LBL 98 OF MAIN DECK FLOOR STRUCTURE. IAW AMM 20-51-01-912-008 REV 112 REPLACE STA 1780 LBL 98 PLATE. I.A.W AMM 51-24-13-607-010 REV 112 APPLY CORROSION PREVENTIVE COMPOUND AND CONDITION CHECK NORMAL.Jan 21, 2025 · N580UP · Boeing 747428F · Fuselage Miscellaneous StructureSDR IPXA2025021304224Angle · corrodedCORROSION OF ZEE ANGLE ON UPPER DECK AT STA 480 LBL 28 (REPLACE). NSTALLED FABRICATED PART I.A.W SRM 51-40-02-0G REV.102 AND BOEING DWG NO:141U5420 SH 4 REV.F.Jan 21, 2025 · N580UP · Boeing 747428F · Fuselage Miscellaneous StructureSDR IPXA2025021304257Web · corrodedCORROSION, WEB OF FLOOR STRUCTURE ( UPPER DECK ) BETWEEN STA 480 - 500 LBL 28. (REPAIR). FABRICATE P/N:141U5422-5 PER BOEING DWG NO.141U5422 SH 1 REV."B";PL REV."B" AND P/N:141U5421-3 PER BOEING DWG NO.141U5421 SH 1 REV."B",PL REV."B" AND P/N:141U5422-4 PER BOJan 21, 2025 · N580UP · Boeing 747428F · Fuselage Miscellaneous StructureSDR IPXA2025021301228Keelbeam · corrodedCORROSION - LEFT KEEL BEAM SKIN BETWEEN STA 1060 TO STA 1080 (REPAIR). REWORK AREA DETAIL DATA AND DIMENSION REFER TO DATA SHEET CONTROL NO.T3F18E005YFJB-1. IT IS WITHIN ALLOWABLE DAMAGE LIMIT I.A.W SRM 53-40-12-1A-1 REV.102. RE-INSTALL FASTENERS I.A.W SRM 51Jan 21, 2025 · N580UP · Boeing 747428F · Fuselage Main, KeelSDR IPXA2025021100801Cargo Track · corrodedCARGO TRACK , BULK CGO COMPARTMENT STA 1958 LBL 11 OF MAIN DECK FLOOR STRUCTURE. (REPAIR) COMPLETED EGAT WORK SHEET NO.50061 (SRM 53-00-52-2R-12 REV.102) STEP 5-11. COMPLETED EGAT WORK SHEET NO.50061(SRM 53-00-52-2R-12 REV.102) STEP 12,13,14,15. RII COMPLETED Jan 21, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025021100198Cargo Track · corrodedCARGO TRACK , AFT CGO COMPARTMENT STA 1700~1720 RBL 11 OF MAIN DECK FLOOR STRUCTURE. (REPAIR) RII COMPLETED & NO FAULT FOUND FOR EGAT WORK SHEET NO.50060(SRM 53-00-52-2R-12 REV.102) STEP 12,13,14,15. OPENJan 21, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025021100325Cargo Track · corrodedCARGO TRACK , AFT CGO COMPARTMENT STA 1853 LBL 11 OF MAIN DECK FLOOR STRUCTURE. (REPAIR) COMPLETED EGAT WORK SHEET NO.50059 (SRM 53-00-52-2R-12 REV.102) STEP 5-11. COMPLETED EGAT WORK SHEET NO.50059(SRM 53-00-52-2R-12 REV.102) STEP 12,13,14,15. RII COMPLETED &Jan 21, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025021100298Cargo Track · corrodedCARGO TRACK , AFT CGO COMPARTMENT STA 1732 LBL 98 OF MAIN DECK FLOOR STRUCTURE. (REPAIR) 1. I.A.W. EGAT WORK SHEET NO:50067 (SRM 53-00-52-2R-6 REV.102.) STEP 6 AND FIGURE 201. COMPLETED MACHINING CHAFER 0.125" BY 45-DEGREE FOR REPAIR ANGLE. 2. I.A.W. EGAT WORKJan 21, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025021100264Cargo Track · corrodedCARGO TRACK , AFT CGO COMPARTMENT STA 1660~1680 LBL 98 OF MAIN DECK FLOOR STRUCTURE. (REPAIR) OK TO WORK OPENJan 21, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025021100227Cargo Track · corrodedCARGO TRACK , AFT CGO COMPARTMENT STA 1755 LBL 98 OF MAIN DECK FLOOR STRUCTURE. (REPAIR) I.A.W. EGAT WORK SHEET NO:50067 (SRM 53-00-52-2R-6 REV.102.) STEP 6 AND FIGURE 201. COMPLETED MACHINING CARGO TRACK CROWN HOLES. OPENJan 21, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025021100170Cargo Track · corrodedAFT CGO COMPARTMENT STA 1640~1660 LBL 98 OF MAIN DECK FLOOR CARGO TRACK STRUCTURE. (REPAIR) RII COMPLETED & NO FAULT FOUND FOR EGAT EI NO. F2025A53M-247 SEQUENCE A STEP 15 & STEP 16Jan 21, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025021100112Seat Track · corrodedTRACK , AFT CGO COMPARTMENT STA 1505 LBL 98 OF MAIN DECK FLOOR STRUCTURE. (REPAIR) 1. I.A.W. EGAT WORK SHEET NO:50064 (SRM 53-00-52-2R-6 REV.102.) STEP 6 AND FIGURE 201. COMPLETED MACHINING CHAFER 0.125" BY 45-DEGREE FOR REPAIR ANGLE. 2. I.A.W. EGAT WORK SHEETJan 21, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025021969635Seat Track · corrodedCORROSION - SEAT TRACK, MAIN DECK STA 480 LBL 33.9. (REPLACE). REMOVE DAMAGE PART I.A.W SRM 51-40-02-0G REV.102. FABRICATE P/N:65B11244-7 PER BOEING DWG NO.65B11244 SH3 REV."-", PL 65B11244-7 REV."B", PSDL REV."-" AND EGAT WORK SHEET NO.50048 AND ORIGINAL PARTJan 18, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025022365090Spar · corrodedFAULT - CORROSION - LOWER CHORD, RIGHT WING OUTBOARD FRONT SPAR AT FSSO / OLES 1510 (AGING A/C INSPECTION)PERFORMED REPAIR I.A.W EO-92809-REQ1 REV.1Jan 18, 2025 · N580UP · Boeing 747428F · Wing SparSDR IPXA2025021867103Floorbeam · corrodedCORROSION FLOOR BEAM, FWD CGO COMPARTMENT STA 980 LBL 74 OF MAIN DECK FLOOR STRUCTURE. (REPAIR). I.A.W AMM 53-21-02-404-006 REV.112 INSTALL MAIN DECK CARGO FLOOR PANEL AT STA 980 LBL74 AND CONDITION CHECK NORMAL. REPAIR DAMAGE AREA I.A.W SRM 53-00-51-2R-3 REJan 18, 2025 · N580UP · Boeing 747428F · Fuselage Main, Floor BeamSDR IPXA2025021567101Support Bracket · corrodedCORROSION SUPPORT BRACKET, WING TO BODY FAIRING INTERNAL STA 1078 LBL 9. (REPLACE). FABRICATE P/N:149U1070-47 PER BOEING DWG NO.149U7010 SH6 REV."A", PL REV."AC" AND EGAT WORK SHEET NO.50109 AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH9.08 REV.10 REQUIREMENJan 18, 2025 · N580UP · Boeing 747428F · Aerodynamic FairingsSDR IPXA2025021169635Seat Track · corrodedSEAT TRACK, MAIN DECK STA 480 LBL 33.9. (REPLACE) PERFORMED CHROMIC ACID ANODIZE I.A.W. EGAT WORK SHEET NO.:50048 STEP 7 AND SPWPS-AN-004 REV.25 AND SPDS-AN-001 REV.41 (REFER TO SHOP LOG NO:2025-0016) OPENJan 18, 2025 · N580UP · Boeing 747428F · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2025020665218Fastener · brokenFASTENER HEAD, R/H H.S.T. LE STA 544. (AGING A/C INSPECTION) (REPLACE) 1.REMOVE DAMAGE FASTENER I.A.W SRM 51-40-02-0G REV.102. 2.INSTALL NEW FASTENER I.A.W SRM 51-40-02-0G REV.102 AND BOEING DWG NO.65B23604 SH4 REV.-. 3.JOB COMPLETED.Jan 18, 2025 · N580UP · Boeing 747428F · Horizontal Stabilizer StructureSDR IPXA2025021652637Web · crackedCRACK - WEB , RIGHT WING INBOARD LEADING EDGE CAVITY UPPER EDGE AT ILES 411 (AGING A/C INSPECTION). (REPLACE). REMOVE DAMAGE PART I.A.W SRM 51-40-02-0G REV.102. INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.102 AND UPS EO-92868-REQ1 REV.1 AND BOEING DWG NO:65B13Jan 17, 2025 · N580UP · Boeing 747428F · Wing Miscellaneous StructureSDR IPXA2025021652509Splice Plate · corrodedPLATE , LEFT WING LEADING EDGE CAVITY LOWER SIDE OLES 1545 (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV 102 AND BOEING DWG NO.65B11862 SHEET 2 REV F.Jan 17, 2025 · N580UP · Boeing 747428F · Wing Miscellaneous StructureSDR IPXA2025021652064Retainer · corrodedCORROSION - RETAINER , R/H WING LOWER T/E FIX PANEL INTERNAL SURFACE INBD FWD CORNER , WBL 128 (AGING A/C INSPECTION) (REPLACE). INSTALL NEW PART I.A.W SRM 51-40-02-0G REV.102 AND BOEING DWG NO.65B11631 SH2 REV.J. ALL PAPERWORK REVIEWED AND C/WJan 17, 2025 · N580UP · Boeing 747428F · Wing Main, Frame StructureSDR IPXA2025022028499Hose · damagedFOUND MAIN DECK SMOKE SAMPLING TUBE HOSE DAMAGED AT STA 760 LH & RH. (REPLACE). .I.A.W AMM 26-14-05-706-008 REV 112 PERFORM MAIN DECK SMOKE SAMPLING TUBE HOSE REPLACE AT STA 760 LH & RH.Jan 16, 2025 · N580UP · Boeing 747428F · Fire Protection SystemSDR IPXA2025021628458Web · corrodedAFT CARGO COMPARTMENT FLOOR WEB CORROSION AT STA 1845. (REPLACE). I.A.W AMM20-51-01-912-008 REV112 REPLACE DOOR ASSEMBLY WITH NEW PARTS. IPC VERIFIED AND SERVICEABLE TAG N0.112451. ATTACHMENT ARE UPLOADED. JOB COMPLETED AND CONDITION CHECK NORMAL.Jan 16, 2025 · N580UP · Boeing 747428F · Fuselage Miscellaneous StructureSDR IPXA2025011628499Hose · damagedFOUND MAIN DECK SMOKE SAMPLING TUBE HOSE DAMAGED AT STA 760 LH & RH. (REPLACE) OK TO WORKJan 16, 2025 · N580UP · Boeing 747428F · Smoke DetectionSDR IPXA2025021600826Tension Tie · crackedDURING PERFORM EO-26856-JIC001 FOUND TENSION T/E CHANNEL CRACK FWD SIDE & AFT SIDE AT STA 720 L/H (REPAIR) 1. REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.50047 AND SRM 53-20-30-2R-1 REV.102 2. JOB COMPLETED. OPENJan 15, 2025 · N580UP · Boeing 747428F · Fuselage Miscellaneous StructureSDR IPXA2025021600809Tension Tie · crackedDURING PERFORM EO-26856-JIC002 FOUND TENSION TIE CHANNEL CRACK AFT SIDE AT STA 840 R/H (REPAIR) 1. REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.50037 AND SRM 53-20-30-2R-2 REV.102 2. JOB COMPLETED. OPENJan 15, 2025 · N580UP · Boeing 747428F · Fuselage Miscellaneous StructureSDR IPXA2025022074648Lens · cracked**SUPPLEMENTAL SDR** FAULT - FOUND L1 ENTRY " EXIT " SIGN CRACK (REPLACE). I.A.W AMM 33-51-01-002-005 REV 112 AND AMM 33-51-01-402-012 REV 112 REPLACED L1 ENTRY "EXIT" SIGN. ALL PAPERWORK REVIEWED AND C/WJan 14, 2025 · N580UP · Boeing 747428F · Emergency LightingSDR IPXA2025011474648Sign · cracked**SDR FILED OPEN** FAULT - FOUND L1 ENTRY " EXIT " SIGN CRACK (REPLACE) OK TO WORKJan 14, 2025 · N580UP · Boeing 747428F · Emergency LightingSDR IPXA2025022350042Structure · corrodedFAULT - CORROSION - CHORD, LEFT WING LEADING EDGE CAVITY OLES 1507.PERFORMED REPAIR I.A.W EO-92783-REQ1 REV.1Jan 12, 2025 · N580UP · Boeing 747428F · Wing Miscellaneous StructureSDR IPXA2025020350546Lens · crackedFOUND COCKPIT EMERGENCY LIGHT L01382 COVER LENS CRACK. (REPLACE). I.A.W WDM 33-51-72-2 REV.44 AND AIPC 33-51-00-20 REV.57 REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY (L01382).Jan 12, 2025 · N580UP · Boeing 747428F · Emergency LightingSDR IPXA2025011350546Lens · crackedFOUND COCKPIT EMERGENCY LIGHT L01382 COVER LENS CRACK. (REPLACE) OK TO WORKJan 12, 2025 · N580UP · Boeing 747428F · Emergency LightingSDR IPXA2025021616832Tension Tie · cracked**SDR FILED OPEN** FAULT - CRACK, TENSION TIE FWD CHANNEL AT STA 820 L/H SIDE. (REPAIR) 1. REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.50022 AND SRM 53-20-30-2R-2 REV.102 2. JOB COMPLETED. ATTACHMENT ARE UPLOADEDJan 10, 2025 · N580UP · Boeing 747428F · Fuselage Main, Attach FittingsSDR IPXA2025021616859Tension Tie · crackedCRACK, TENSION TIE FWD CHANNEL AT STA 760 R/H SIDE. (REPAIR) 1. REPAIR DAMAGE AREA I.A.W EGAT WORK SHEET NO.50021 AND SRM 53-20-30-2R-2 REV.102 2. JOB COMPLETED.Jan 10, 2025 · N580UP · Boeing 747428F · Fuselage Main, Attach FittingsSDR U2RA2025011300070Wire Harness · chafedDURING A-CHECK AT LEVEL 5 KCNW, IT WAS DISCOVERED THAT A WIRE BUNDLE WAS CHAFFING WITH POST P/N: 65B14087-3 LOCATED AT FRAME STA. 460, LBL 87. THE DAMAGE WAS MEASURED AS 4MM X 5MM, WHICH IS OUT OF LIMITS. PERMANENT REPAIR ACCOMPLISHED IN ACCORDANCE WITH FVCI EJan 5, 2025 · N952CA · Boeing 747428F · Fuselage Main, Bulkhead Fuselage wiringSDR U2RA2025011100069Reservoir · low pressureDURING A-CHECK INSPECTION AT LEVEL 5 AEROSPACE KCNW, IT WAS FOUND THAT EMERGENCY POWER RESERVOIR P/N: 1270156-4 S/N: ALT183-3683 HAS LOW PRESSURE. EMERGENCY POWER RESERVOIR P/N: 1270156-4 S/N: ALT183-3683 WAS REMOVED AND REPLACED ON NR 0072 UNDER LEVEL 5 AEROSJan 5, 2025 · N952CA · Boeing 747428F · DoorsSDR IPXA2024101761016Hose · chafedATB, ON TAKE OFF GEAR WOULD NOT RETRACT €ŒGEAR TILT €Œ EICAS MSG AIR TURN BACK FOLLOWED FIM 32-31 FAULT TREE FIG 105 TO BLOCK 4 FOUND R/H BG TRUCK FLEX LINE LEADING TO TILT ACTUATOR CHAFED AND LEAKING SEVERELY, PER BLOCK 33 REMOVED AND REPLACED FLEX LINE WIOct 16, 2024 · N580UP · Boeing 747428F · Hydraulic System, MainSDR IPXA202410161016Landing Gear · faulted*SDR FILED OPEN* *AIR TURN BACK* ON TAKE OFF GEAR WOULD NOT RETRACT €ŒGEAR TILT €Œ EICAS MSG AIR TURN BACKOct 16, 2024 · N580UP · Boeing 747428F · Landing Gear Retraction/Extension SystemSDR WRNA202409040687Limiter · brokenDURING POST FLIGHT FOUND # 3 BRAKE TORQUE LIMITER BROKEN.Sep 4, 2024 · N904AR · Boeing 747428F · BrakeSDR IPXA2024082771819Battery · inoperativeFOUND THE L1 DOOR EMERGENCY LIGHT INOP.I.A.W AMM 33-51-04-902-001-001 REV.111 REPLACED THE EMERGENCY LIGHT BATTERY (M5170) AND PERFORMED L1 DOOR EMERGENCY LIGHT OPERATIONAL TEST , RESULT WAS SATISFACTORY.Aug 27, 2024 · N580UP · Boeing 747428F · Emergency LightingSDR IPXA2024082634635Battery · inoperativeFOUND THE UPPER DECK AISLE EMERGENCY LIGHT L5733 AND CREW 3REST EMERGENCY LIGHT L5767 INOP..I.A.W AMM 33-51-04-902-001-001 REV.111 REPLACED THE EMERGENCY LIGHT BATTERY (M5169) AND PERFORMED UPPER DECK EMERGENCY LIGHT OPERATIONAL TEST , RESULT WAS SATISFACTORY.Aug 24, 2024 · N580UP · Boeing 747428F · Emergency LightingSDR IPXA2024072473659Duct · leakingNO €ŒFIRE TEST PASS€? MESSAGE AS PER MEL 26-16-1-2-1-1 OPS PROCEDURES DUCT LEAK WHEEL WELL CTL CARD REPLACED IAW AMM 26-10-01-404-006, REV. 111 P/N ON/OFF 35008-33 S/N ON B1396 S/N OFF 2212Jul 24, 2024 · N580UP · Boeing 747428F · Detection SystemSDR IPXA2024040293945Actuator · corroded*** EMERGENCY DECLARED *** #1ENG FAILURE SHORT FINAL SECURED . ON GND _N1 ROLLED BACK ACTUATOR INSTALLATION CHECK OK AS RII INSPECTORApr 2, 2024 · N580UP · Boeing 747428F · Engine Bleed Air SystemSDR IPXA2024010589797Unknown · unknown*** SDR FILED OPEN *** DAMAGE FOUND #6 TE FLAP FIXED FAIRING CROSS REF T3F18E001YCTM.***SM EVAL REQ*** VISIBLE DAMAGE SIZE 0.75€?X0.10€? DEPTH 0.10€? SEALED THE DAMAGE AREA WITH ALUMINUM FOIL TAPE<BR>DEFERRED PER SRM 51-70-02-1A.Jan 5, 2024 · N580UP · Boeing 747428F · Trailing Flap Position Indicating SystemSDR IPXA2023121826244Door · noisy*** SUPPLEMENTAL SDR *** DURING CLIMB THRU FL280 A LOUD METALLIC POP WAS HEARD AND FELT THRU FLIGHT DECK FLOOR. SUSPECT OVERHEAD DOOR, INSPECTED DOOR MECHANISM REF M/M 52-21-00 NO FAULTS NOTED.Dec 15, 2023 · N580UP · Boeing 747428F · Emergency ExitsSDR IPXA2023121526244None · none*SDR FILED OPEN* DURING CLIMB THRU FL280 A LOUD METALLIC POP WAS HEARD AND FELT THRU FLIGHT DECK FLOOR. SUSPECT OVERHEAD DOOR, INSPECTED DOOR MECHANISM REF M/M 52-21-00 NO FAULTS NOTED.Dec 15, 2023 · N580UP · Boeing 747428F · Standard Practices/StructuresSDR IPXA2023121526184Door · warning messageDOOR FD OVHD EICAS ILLUMINATED CLIMBING THRU FL290. ACCOMPLISHED DOOR FD OVHD CHECKLIST AND PUT DOOR IN SAFE CONFIGURATION. THE DOOR LOCK MOVED FROM LOCKED TO UNLOCKED BY ITSELF DURING TURBULENCE. PRESSURIZED A/C TO 4.0 FOR 20 MINUTES, UNABLE TO MOVE LATCH WITDec 15, 2023 · N580UP · Boeing 747428F · Emergency ExitsSDR IPXA2023112731028Bleed Air Sys · warning message*ATB* BLEED 2 EICAS MSG ILLUMINATED ON T/O R/R #2 HPSOV PER M/M 36-11-05-400-802-001 , OPS CHECKED GOOD. REVERSED DMP 36-11-3 . REVERSED DMP 78-31-1-1 THIS CLEARS 2803594 +2803591.Nov 23, 2023 · N580UP · Boeing 747428F · Engine Bleed Air System
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