N450PA

Service difficulty reports · 307

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N450PA' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UIEA2026071300593Circuit Card · faultedMAIN DECK FIRE WARNING - NO EICAS MSG. SWAPED THE A4 WITH A29 CIRCURT CARD & PFMD GND TEST ,TEST PASSED IAW AMM 26-10-01 (NOW D00132 IN A4 POSITION,D00883 IN A29 POSITION)Jul 12, 2026 · N450PA · Boeing 74746NF · Fire DetectionSDR UIEA2026022600069Valve · inoperativeEQUIPMENT COOLING MESSAGE. SUSPECT FLT DECK FLOW REG VALVE INOP. OPENED FLOOR PANEL AND MANUALLY MOVED VALVE TO OPEN. TRANSFER TO DMI 248403 PER MEL 21-61-13 CAT C. R & R FD FLOW REG VALVE AS PER AMM 21-61-09 & AIPC 21-21-06. OPS AND LEAK CHK GOOD. DMI 24840Feb 26, 2026 · N450PA · Boeing 74746NF · Air Distribution SystemSDR UIEA2025111001295Tire · failed#8 MLG BLEW OUT TOWER REPORTED SMOKE & TIRE DEBRIS ON RUNWAY. R & R NR 8 MWA IAW AMM 32-45-01 & IPC 32-45-03-02. C/W BLOWN TIRE CHAP 5 INSP IAW AMM 05-51-25. R & R NR 7 MWA IAW AMM 32-45-01. R & R NLG STEERING CYLINDER IAW AMM 32-53-11. OPS CHKD NORMAL. NO Nov 11, 2025 · N450PA · Boeing 74746NF · TireSDR UIEA2025110701293Wheel · damagedNR 3 MAIN TIRE DAMAGED. REPLACED NR 3 AND 4 MLG WHEEL ASSY IAW AMM 32-45-01/401. PRESS & LEAK CHK OK.Nov 7, 2025 · N450PA · Boeing 74746NF · Wheel/Ski/FloatSDR UIEA2025101001267Indication Sys · faultedFLIGHT CREW REPORTED NR 4 HYD QTY INDICATION ERRATIC IN FLIGHT. PERFORMED WIRING CHECK BETWEEN DW 3112C PIN 2 AND DM7838EA PIN G15, DM 7838BA PIN D15, CHECKS NORMAL. R & R NR 4 HYD IM AND GROUND TEST PASS IAW AMM 29-11-42, WDM 27-62-11 & AIPC 29-11-42-01B, APOct 10, 2025 · N450PA · Boeing 74746NF · Hydraulic Indicating SystemSDR UIEA2025081001118Tire · failedAT LANDING, #1 TIRE BLEW. FLAT SPOT FOUND. CREW HAD AUTOBRAKE SET AT 4 MINIMUM LEVEL DUE TO NO AUTOSPOILER AND BRAKE ROD. ONCE DISENGAGED, CREW MANUAL BRAKE DID NOT EXCEED LEVEL 2. A/C TAXIED & TOWED IN WITH BLOWN TIRE. R & R #1 MWA IAW AMM 32-45-01/401 & AIPAug 10, 2025 · N450PA · Boeing 74746NF · TireSDR UIEA2025062800817Longeron Fitting · crackedLEFT BS 1480 LONGERON EXTENSION FITTING FOUND CRACKED. CRACK LONGERON EXTENSION FITTING REPAIRED AS PER ATLAS AIR EO 4453A818 REV 20 PART 7. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, StructureSDR UIEA2025062800818Doubler · crackedMAIN DECK - L1 ENTRY DR UPR HINGE DOUBLER FND CRACKED. DOUBLER REPLACED AS PER SRM 51-10-02 AND NEW DOUBLER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW DOUBLER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Passenger/Crew DoorsSDR UIEA2025063000819Lug · cracked1 EA CRACK WAS FOUND ON BS 1000 RBL 11.33 INTERCOSTAL LUG FITTING. INTERCOSTAL LUG FITTING REPLACED AS PER ATLAS AIR EO 4453C024 REV.4 PART 7 STEP 3. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, Attach FittingsSDR UIEA2025063000820Lug · cracked1 EA CRACK WAS FOUND ON BS 1000 LBL 11.33" INTERCOSTAL LUG FITTING. INTERCOSTAL LUG FITTING REPLACED AS PER ATLAS AIR EO 4453C024 REV.4 PART 3 STEP 3. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, Attach FittingsSDR UIEA2025070100821Fairing · delaminatedRIGHT WING I/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 13". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge FlapsSDR UIEA2025070100822Fairing · delaminatedRIGHT WING I/B AFT FLAP MID L/E FAIRING FOUND DELAMINATION AT O/B 180". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge FlapsSDR UIEA2025070100823Fairing · delaminatedLEFT WING I/B MID FLAP L/E FAIRING FOUND DELAMINATION AT O/B 70". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge FlapsSDR UIEA2025070100824Fairing · delaminatedRIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 39". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge FlapsSDR UIEA2025070100825Fairing · delaminatedRIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT I/B 12". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge FlapsSDR UIEA2025070100826Fairing · puncturedLEFT WING I/B FORE FLAP MID L/E FAIRING FOUND PUNCH HOLE FROM I/B 133". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. C. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge FlapsSDR UIEA2025070100827Fairing · delaminatedRIGHT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION AT O/B 180". PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5. A. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge FlapsSDR UIEA2025070100828Fairing · chafedRHW I/B AFT FLAP I/B L/E FAIRING FOUND CHAFING. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5.G. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge FlapsSDR UIEA2025070300830Power Supply · no testFUNCTIONAL TEST EMERGENCY LIGHTS BATTERY PACKS FOR CAPACITY (15 MIN. MINIMUM). FOUND EMERGENCY LT L1533, L5733, L5767 & M4915 WENT OFF IN LESS THAN 15 MINUTES. EMERGENCY LT POWER PACK M5169 REPLACED AND OPERATION CHECKED NORMAL IAW AMM 33-51-04.Jul 14, 2025 · N450PA · Boeing 74746NF · Emergency LightingSDR UIEA2025070500835Lamp · inoperativeDOOR L1 FWD EMERGENCY SILL LT L1853 FOUND INOP. DOOR L1 FWD EMERGENCY SILL LT L1853 LAMP REPLACED AND TEST NORMAL IAW AMM 33-51-05.Jul 14, 2025 · N450PA · Boeing 74746NF · Emergency LightingSDR UIEA2025070700844Seat Track · crackedM/D STA753 TO STA757 LBL11" SEAT TRACK FOUND CRACKED. SEAT TRACK CRACK AREA REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR12 FIG 201. NO FURTHER DEFECTS NOTED.Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2025070700846Seat Track · chafedM/D STA 1980 TO STA 1985 RBL 11.33" SEAT TRACK CROWN CHAFED. CHAFED AREA SMOOTHED OUT AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND SMOOTHED OUT AREA MEASURED L:6" 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 UIEA2025070700847Seat Track · chafedM/D STA 2020 TO STA 2026 RBL 11 SEAT TRACK CROWN CHAFED. CHAFED 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. NO Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach FittingsSDR 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 Fittings
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