# Service difficulty reports: N450PA

A list on [N450PA](https://openairdocs.org/aircraft/N450PA.md).

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

Page 1 of 7 · 307 reports

- [SDR UIEA2026071300593](https://openairdocs.org/sdr/UIEA2026071300593.md): Circuit Card · faulted · Jul 12, 2026 · N450PA · Boeing 74746NF · Fire Detection
  > MAIN 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)
- [SDR UIEA2026022600069](https://openairdocs.org/sdr/UIEA2026022600069.md): Valve · inoperative · Feb 26, 2026 · N450PA · Boeing 74746NF · Air Distribution System
  > EQUIPMENT 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 24840
- [SDR UIEA2025111001295](https://openairdocs.org/sdr/UIEA2025111001295.md): Tire · failed · Nov 11, 2025 · N450PA · Boeing 74746NF · Tire
  > #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
- [SDR UIEA2025110701293](https://openairdocs.org/sdr/UIEA2025110701293.md): Wheel · damaged · Nov 7, 2025 · N450PA · Boeing 74746NF · Wheel/Ski/Float
  > NR 3 MAIN TIRE DAMAGED. REPLACED NR 3 AND 4 MLG WHEEL ASSY IAW AMM 32-45-01/401. PRESS & LEAK CHK OK.
- [SDR UIEA2025101001267](https://openairdocs.org/sdr/UIEA2025101001267.md): Indication Sys · faulted · Oct 10, 2025 · N450PA · Boeing 74746NF · Hydraulic Indicating System
  > FLIGHT 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, AP
- [SDR UIEA2025081001118](https://openairdocs.org/sdr/UIEA2025081001118.md): Tire · failed · Aug 10, 2025 · N450PA · Boeing 74746NF · Tire
  > AT 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 & AIP
- [SDR UIEA2025062800817](https://openairdocs.org/sdr/UIEA2025062800817.md): Longeron Fitting · cracked · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, Structure
  > LEFT 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.
- [SDR UIEA2025062800818](https://openairdocs.org/sdr/UIEA2025062800818.md): Doubler · cracked · Jul 14, 2025 · N450PA · Boeing 74746NF · Passenger/Crew Doors
  > MAIN 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.
- [SDR UIEA2025063000819](https://openairdocs.org/sdr/UIEA2025063000819.md): Lug · cracked · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, Attach Fittings
  > 1 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.
- [SDR UIEA2025063000820](https://openairdocs.org/sdr/UIEA2025063000820.md): Lug · cracked · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, Attach Fittings
  > 1 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.
- [SDR UIEA2025070100821](https://openairdocs.org/sdr/UIEA2025070100821.md): Fairing · delaminated · Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge Flaps
  > RIGHT 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.
- [SDR UIEA2025070100822](https://openairdocs.org/sdr/UIEA2025070100822.md): Fairing · delaminated · Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge Flaps
  > RIGHT 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.
- [SDR UIEA2025070100823](https://openairdocs.org/sdr/UIEA2025070100823.md): Fairing · delaminated · Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge Flaps
  > LEFT 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.
- [SDR UIEA2025070100824](https://openairdocs.org/sdr/UIEA2025070100824.md): Fairing · delaminated · Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge Flaps
  > RIGHT 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.
- [SDR UIEA2025070100825](https://openairdocs.org/sdr/UIEA2025070100825.md): Fairing · delaminated · Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge Flaps
  > RIGHT 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.
- [SDR UIEA2025070100826](https://openairdocs.org/sdr/UIEA2025070100826.md): Fairing · punctured · Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge Flaps
  > LEFT 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.
- [SDR UIEA2025070100827](https://openairdocs.org/sdr/UIEA2025070100827.md): Fairing · delaminated · Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge Flaps
  > RIGHT 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.
- [SDR UIEA2025070100828](https://openairdocs.org/sdr/UIEA2025070100828.md): Fairing · chafed · Jul 14, 2025 · N450PA · Boeing 74746NF · Trailing Edge Flaps
  > RHW 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.
- [SDR UIEA2025070300830](https://openairdocs.org/sdr/UIEA2025070300830.md): Power Supply · no test · Jul 14, 2025 · N450PA · Boeing 74746NF · Emergency Lighting
  > FUNCTIONAL 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.
- [SDR UIEA2025070500835](https://openairdocs.org/sdr/UIEA2025070500835.md): Lamp · inoperative · Jul 14, 2025 · N450PA · Boeing 74746NF · Emergency Lighting
  > DOOR 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.
- [SDR UIEA2025070700844](https://openairdocs.org/sdr/UIEA2025070700844.md): Seat Track · cracked · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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.
- [SDR UIEA2025070700846](https://openairdocs.org/sdr/UIEA2025070700846.md): Seat Track · chafed · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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. N
- [SDR UIEA2025070700847](https://openairdocs.org/sdr/UIEA2025070700847.md): Seat Track · chafed · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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
- [SDR UIEA2025070700848](https://openairdocs.org/sdr/UIEA2025070700848.md): Seat Track · chafed · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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. N
- [SDR UIEA2025070700849](https://openairdocs.org/sdr/UIEA2025070700849.md): Seat Track · chafed · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 DE
- [SDR UIEA2025070700850](https://openairdocs.org/sdr/UIEA2025070700850.md): Seat Track · chafed · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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. N
- [SDR UIEA2025070700851](https://openairdocs.org/sdr/UIEA2025070700851.md): Seat Track · scratched · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 D
- [SDR UIEA2025070700852](https://openairdocs.org/sdr/UIEA2025070700852.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 D
- [SDR UIEA2025070700854](https://openairdocs.org/sdr/UIEA2025070700854.md): Seat Track · scratched · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 ALLOW
- [SDR UIEA2025070800855](https://openairdocs.org/sdr/UIEA2025070800855.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 FURT
- [SDR UIEA2025070800856](https://openairdocs.org/sdr/UIEA2025070800856.md): Seat Track · scratched · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 ALLOWA
- [SDR UIEA2025070800857](https://openairdocs.org/sdr/UIEA2025070800857.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 FUR
- [SDR UIEA2025070800858](https://openairdocs.org/sdr/UIEA2025070800858.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 FURTH
- [SDR UIEA2025070800859](https://openairdocs.org/sdr/UIEA2025070800859.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 FURT
- [SDR UIEA2025070800860](https://openairdocs.org/sdr/UIEA2025070800860.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 FURT
- [SDR UIEA2025070800861](https://openairdocs.org/sdr/UIEA2025070800861.md): Seat Track · scratched · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 ALLOWABL
- [SDR UIEA2025070800862](https://openairdocs.org/sdr/UIEA2025070800862.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 FURT
- [SDR UIEA2025070800863](https://openairdocs.org/sdr/UIEA2025070800863.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 D
- [SDR UIEA2025070800864](https://openairdocs.org/sdr/UIEA2025070800864.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 FURTH
- [SDR UIEA2025070800865](https://openairdocs.org/sdr/UIEA2025070800865.md): Guide · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Miscellaneous Structure
  > M/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 DEF
- [SDR UIEA2025070800868](https://openairdocs.org/sdr/UIEA2025070800868.md): Seat Track · chafed · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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. NO
- [SDR UIEA2025070800869](https://openairdocs.org/sdr/UIEA2025070800869.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 FU
- [SDR UIEA2025070800870](https://openairdocs.org/sdr/UIEA2025070800870.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 FUR
- [SDR UIEA2025070800871](https://openairdocs.org/sdr/UIEA2025070800871.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 FU
- [SDR UIEA2025070800872](https://openairdocs.org/sdr/UIEA2025070800872.md): Seat Track · corroded · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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 F
- [SDR UIEA2025070800873](https://openairdocs.org/sdr/UIEA2025070800873.md): Tee Angle · cracked · Jul 14, 2025 · N450PA · Boeing 74746NF · Nacelle/Pylon Miscellaneous Structure
  > NR 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.
- [SDR UIEA2025070900874](https://openairdocs.org/sdr/UIEA2025070900874.md): Tee Angle · cracked · Jul 14, 2025 · N450PA · Boeing 74746NF · Nacelle/Pylon Miscellaneous Structure
  > NO. 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.
- [SDR UIEA2025070900875](https://openairdocs.org/sdr/UIEA2025070900875.md): Beam · cracked · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, Structure
  > NWW 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.
- [SDR UIEA2025070900878](https://openairdocs.org/sdr/UIEA2025070900878.md): Beam · cracked · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage Main, Structure
  > NWW 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-
- [SDR UIEA2025070900879](https://openairdocs.org/sdr/UIEA2025070900879.md): Seat Track · cracked · Jul 14, 2025 · N450PA · Boeing 74746NF · Fuselage, Seat/Cargo Attach Fittings
  > M/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.

Next page: https://openairdocs.org/aircraft/N450PA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N450PA/reports

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