Boeing 747-46NF

Service difficulty reports · 1,079

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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 = '74746NF'
  ORDER BY difficulty_date DESC"

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SDR UIEA2025070700848Seat Track · chafedM/D STA 646 TO STA 656 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:5" X W:0.3" X D:0.007", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070700849Seat Track · chafedM/D STA 1890 TO 1893 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND CHAFING SMOOTHED OUT AREA MEASURED AS PER SRM 53-00-52-1A-1. WITHIN ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DEJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070700850Seat Track · chafedM/D STA 1968 TO STA 1970 LBL 11 SEAT TRACK CROWN FOUND CHAFED. CHAFE AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:4" X W:03" X D:0.006", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070700851Seat Track · scratchedM/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1370, STA 1390, STA 1410. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, SMOOTHED AREA MEASURED L:4" X W:0.7" X D:0.008" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070700852Seat Track · corrodedM/D STA 780, 783 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L=5" X W=0.7", D=0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHER DJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070700854Seat Track · scratchedM/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1430, STA 1450 & STA 1470. SCRATCH AREAS SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED AREA MEASURED L:4" X W:0.7" X D:0.009", WITHIN SRM 53-00-52-1A-1 ALLOWJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800855Seat Track · corrodedM/D STA 606-STA 624 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=8" X W=0.7" X D=0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMTIS. NO FURTJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800856Seat Track · scratchedM/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11 STA 1611, STA 1631, STA 1772. SCRATCH AREAS SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED AREA MEASURED L:3" X W:0.7" X D:0.007", WITHIN SRM 53-00-52-1A-1 ALLOWAJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800857Seat Track · corrodedM/D STA 566-STA 592 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=15" X W=0.7" X D=0.008" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800858Seat Track · corrodedM/D STA 545-STA 559 LBL 11 SEAT TRACK CROWN CORRODED. CORRSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=8" X W=0.7" X D=0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800859Seat Track · corrodedM/D STA 872-STA 875 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=6" X W=0.7" X D=0.005" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800860Seat Track · corrodedM/D STA 750-STA 783 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED" L=4" X W=0.7" X D=0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800861Seat Track · scratchedM/D SEAT TRACK CTR GUIDE STUD AREA FOUND SCRATCHED AT LBL 11 STA 1430, STA 1450, STA 1470. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, BLENDED OUT AREA MEASURED L:4' X W:0.7" X D:0.008", WITHIN SRM 53-00-52-1A-1 ALLOWABLJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800862Seat Track · corrodedM/D STA 730-STA 752 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=6" X W=0.7" X D=0.005" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800863Seat Track · corrodedM/D SEAT TRACK CTR GUIDE STUD AREAS FOUND SCRATCHED AT RBL 11.33 STA 1853 AND STA 1913. SCRATCH AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED AREA MEASURED L:6" X W:0.7" X D:0.006", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800864Seat Track · corrodedM/D STA 687-STA 694 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED: L=8" X W=0.7" X D=0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURTHJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800865Guide · corrodedM/D STA 1920 - 1980 SCD AFT SIDE GUIDE FOUND CORROSION. CORROSION AREA REMOVED AS PER CMM 25-55-06 AND REPROTECTED AS PER SRM 51-20-01 AND CORROSION REMOVED AREA MEASURE L:13" X W:2" X D:0.028", ORG THICKNESS 0.152" WITHIN CMM 25-55-06 LIMITS. NO FURTHER DEFJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Miscellaneous StructureSDR UIEA2025070800868Seat Track · chafedM/D STA 1457 TO STA 1461 RBL 11 SEAT TRACK CROWN CHAFING. CHAFING AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:7" X W:0.3" X D:0.008", WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NOJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800869Seat Track · corrodedM/D STA 617 - STA 635 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:13" X W:0.7" X D:0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FUJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800870Seat Track · corrodedM/D STA 570 - STA 593 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:6" X W:0.7" X D:0.006" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800871Seat Track · corrodedM/D STA 546 TO STA 559 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:8 X W:0.7" X D:0.007" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FUJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800872Seat Track · corrodedM/D STA 2200 - STA 2210 LBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:4" X W:0.7" X D:0.005" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070800873Tee Angle · crackedNR 3 PYLON O/B INNER MOST LWR TEE CRACKED AT NAC STA 344 APPROX. TEE CRACK AREA REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Nacelle/Pylon Miscellaneous StructureSDR UIEA2025070900874Tee Angle · crackedNO. 2 PYLON - O/B MOST LOWER TEE CRACK FOUND AT NAC STA 332. TEE CRACK AREA REPAIRED AS PER SRM 54-51-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Nacelle/Pylon Miscellaneous StructureSDR UIEA2025070900875Beam · crackedNWW SIDE PANEL HAS 1EA CRACK FOUND AT BEAM LHS WL130 BETWEEN STA 320 AND STA 340. BEAM REPLACED AS PER BOEING DWG: 65B07942&PL AND NEW BEAM HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW BEAM INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, StructureSDR UIEA2025070900878Beam · crackedNWW SIDE PANEL HAS 1 EA CRACK FWD AT BEAM RHS WL180 BETWEEN STA 265 AND 280.(<P>CRACKED BEAM REPLACED AS PER BOEING DWG NO.65B07942 & PL & EO 4453A043 REV 11 PART 2 ITEM 3 AND NEW BEAM HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW BEAM INSTALLED AS PER SRM 51-Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, StructureSDR UIEA2025070900879Seat Track · crackedM/D STA 981 TO 983 LBL 75" SUBSTITUTE TRACK FOUND CRACKED. SUBSTITUTE TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-13 REPAIR 13 FIG 201. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070900880Seat Track · corrodedM/D STA 650 - STA 654 RBL 11 SEAT TRACK CROWN CORRODED. CORROSION AREA REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CORROSION REMOVED AREA MEASURED L:9' X W:0.7" X D:0.008" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS. NO FURJul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070900881Frame · crackedNR 4 ENG NACELLE LT CORE COWL FRAME NR 2 FOUND CHAFED. FRAME CHAFE AREA REPAIRED IAW SRM 54-45-02-2R-1 REPAIR FIG 201. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Nacelle/Pylon, Frame/Spar/RibSDR UIEA2025070900883Frame · cracked#4 ENG R/H CORE COWL FRAME #5 (COUNT FROM FWD) FOUND CRACKED. FRAME CRACK AREA REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Nacelle/Pylon, Frame/Spar/RibSDR UIEA2025070900884Floor Support · crackedMDC - STA 1160 - 1180 LH O/B FLOOR SUPPORT CRACK. FLOOR SUPPORT CRACK AREA REPAIRED AS PER RI-53-40-17764 REV A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Miscellaneous StructureSDR UIEA2025070900885Skin · crackedLEFT WING #10 VC FLAP BULLNOSE O/B EDGE FOUND DEFORMED AND CRACKED. O/B EDGE DAMAGE AREA REPAIRED AS PER RI-57-40-17758 REV A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge FlapsSDR UIEA2025071000886Duct · chafedNR 4 ENG RH C-DUCT FWD BLOWOUT DOOR L/E FOUND CHAFING. CHAFING AREA REPAIRED AS PER ST ENGINEERING CMM 78-32-09 REPAIR 5. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Engine Collector/Tailpipe/NozzleSDR UIEA2025071000887Skin · crackedAPU RIGHT DOOR SKIN AT NR 1 LATCH OPENING AND FWD LOWER FOUND CRACKED AND CHAFING. NR 1 LATCH CUTOUT CRACK & FWD LWR SKIN CHAFING AREA REPAIRED AS PER RI-52-48-17747 REV A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Auxiliary Power Unit (APU) DoorsSDR UIEA2025071000888Bulkhead · cracked1 EA CRACK FOUND ON BS2598 BULKHEAD LH AFT INNER CHORD CRACK AT 3 O'CLOCK POSITION VIEW LOOKING FWD, CRACK DEPTH APPROX 0.080" FROM FORWARD SURFACE. INNER CHORD CRACK AREA REPAIRED AS PER RI-80-17737 REV A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, BulkheadSDR UIEA2025071000893Bulkhead · cracked1 EA CRACK FOUND ON BS 2598 BULKHEAD RH AFT INNER CHORD CRACK AT 3 O'CLOCK POSITION (VIEW LOOKING FWD) CRACK DEPTH APPROX 0.015" FROM FORWARD SURFACE. INNER CHORD CRACK AREA REPAIRED AS PER RI-53-80-17738 REV A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, BulkheadSDR UIEA2025071000895Duct · crackedNO. 2 ENG - RH C-DUCT OUTER GROOVE UPPER AREA CRACK FOUND. FRAME CRACK AREA REPAIRED AS PER ATLAS AIR EA NO.EA-1978A227 REV.0. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Engine Collector/Tailpipe/NozzleSDR UIEA2025071100901Web · crackedM/D STA 1180 L/H O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-8 FIG 8. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Miscellaneous StructureSDR UIEA2025071100902Web · crackedM/D STA 1180 RH O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-8 REPAIR 8. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Miscellaneous StructureSDR UIEA2025071100903Web · crackedM/D STA 1220 L/H O/B BELOW FLOOR INTERCOSTAL WEB CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-5 REPAIR 5. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Miscellaneous StructureSDR UIEA2025071100904Web · crackedM/D STA 1200 L/H O/B BELOW FLOOR INTERCOSTAL WEB FOUND CRACKED. INTERCOSTAL WEB CRACK AREA REPAIRED AS PER SRM 53-40-51-2R-9 REPAIR 9. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Miscellaneous StructureSDR UIEA2025071100905Failsafe · crackedUPPER DECK LH BS820 TENSION TIE FAIL SAFE CHORD 1EA CRACK FOUND. FAIL SAFE CHORD CRACK AREA REPAIRED AS PER SRM 51-70-11-0G-0. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, StructureSDR UIEA2025071100926Plate · damagedSTEEL PLATE FOUND 4EA FASTENER HOLES SEM AT UPR DECK R/H STA 760 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, StructureSDR UIEA2025071100927Plate · damagedSTEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK RH STA800 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, StructureSDR UIEA2025071100928Plate · damagedSTEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK RH STA840 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, StructureSDR UIEA2025071100929Plate · damagedSTEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK RH STA860 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, StructureSDR UIEA2025071100930Plate · damagedSTEEL PLATE FOUND 2 EA FASTENER HOLE SEM AT UPR DECK LH STA860 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, StructureSDR UIEA2025071100931Plate · damagedSTEEL PLATE FOUND 1 EA FASTENER HOLE SEM AT UPR DECK LH STA880 TENSION TIE AREA. STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, StructureSDR UIEA2025071100932Plate · damagedSTEEL PLATE FOUND 3 EA FASTENER HOLE SEM AT UPR DECK LH STA840 TENSION TIE AREA.(<P>STEEL PLATE REPLACED CARRIED OUT AS PER RI-53-20-17745 REV.A. NO FURTHER DEFECTS NOTED.</P>)Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, StructureSDR UIEA2025071100933Frame · crackedUPPER DECK TENSION TIE AT RH BS860 1 EA CRACK FOUND. FRAME REPLACED CARRIED OUT AS PER SRM 51-10-02 AND NEW FRAME HOLES AS PER SRM 51-40-05 AND NEW FRAME INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, Frame
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