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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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)SDR 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 24840SDR 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 SDR UIEA2025110701293Wheel · damagedNR 3 MAIN TIRE DAMAGED. REPLACED NR 3 AND 4 MLG WHEEL ASSY IAW AMM 32-45-01/401. PRESS & LEAK CHK OK.SDR 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, APSDR 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 & AIPSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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. NSDR 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 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. NSDR 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 DESDR 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. NSDR 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 DSDR 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 DSDR 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 ALLOWSDR 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 FURTSDR 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 ALLOWASDR 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 FURSDR 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 FURTHSDR 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 FURTSDR 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 FURTSDR 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 ALLOWABLSDR 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 FURTSDR 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 DSDR 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 FURTHSDR 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 DEFSDR 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. NOSDR 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 FUSDR 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 FURSDR 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 FUSDR 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 FSDR 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.SDR 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.SDR 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.SDR 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-SDR 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.
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