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 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 FURSDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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>)SDR 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.SDR UIEA2025071200935Tension Tie · crackedUPPER DECK LH BS900 TENSON TIE FWD CHANNEL 1 EA CRACK FOUND. TENSION TIE FWD CHANNEL PERFORMED INTERIM REPAIR AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.SDR UIEA2025071200936Tension Tie · crackedUPPER DECK LH BS940 TENSION TIE FWD CHANNEL 1 EA CRACK FOUND. TENSION TIE FWD CHANNEL PERFORMED INTERIM REPAIR AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.SDR UIEA2025071200938Tension Tie · crackedUPPER DECK LH BS820 TENSION TIE FWD CHANNEL 1 EA CRACK FOUND. TENSION TIE CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED.SDR UIEA2025071200939Skin · damagedNR 4 NACELLE NOSE COWL LIP SKIN INTERIOR SURFACE 1 EA FASTENER HOLE ELONGATED. ELONGATE FASTENER HOLE AREA REPAIRED AS PER ATLAS EA-1971A218 REV. 0. NO FURTHER DEFECTS NOTED.SDR UIEA2025071200940Skin · damagedLEFT WING L/E FIXED FAIRING BETWEEN INBD ILES 630.46 TO ILES 693.5 SEVERAL FASTENER HOLES FOUND ELONGATED. L/E SKIN REPAIRED AS PER RI-57-41-17749 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071300942Web · crackedLEFT WING L/E FIXED INTERNAL AT INBD ILES 693.5 WEB CRACKED. WEB CRACK AREA REPAIRE AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071300943Beam · crackedLEFT WING L/E FIXED INTERNAL AT INBD ILES 693.5 UPPER CHORD CRACKED. UPR CHORD CRACK AREA REPAIRED AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071300944Beam · crackedLEFT WING L/E FIXED LOWER BEAM CRACK L/E ILES 693.5 AREA. BEAM REPAIRED AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025071300945Splice Strap · crackedLEFT WING L/E FIXED SPLICE STRAP-LOWER CRACK AT INBD ILES 693.5 AREA. SPLICE STRAP-LOWER CRACK AREA REPAIRED AS PER RI-57-41-17749 REV A. NO FURTHER DEFECTS NOTED.SDR UIEA2025040300427Pseu · faultedAFTER TAKE OFF, GEAR TILT MESSAGE & GEAR HANDLE WOULD NOT MOVE PAST OFF.(<P>ADJUSTED LT BLG PROX SWITCH AND TARGET PER B747 AMM 32-61-12-822-019. BODY GEAR OPS CHECK GOOD PER B747 AMM 32-33-715-071. REPLACED PSEU PER B747 AMM 32-09-03-004-001 AND 32-09-03-404-SDR UIEA2024081600834Fairing · delaminatedLHW I/B MID FLAP I/B L/E FAIRING FOUND DELAMINATION(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED.</SPAN></P>)SDR UIEA2024081600833Lamp · inoperativeMAIN DECK L1 DR STILL FWD EMER LT INOP.(<P>MAIN DECK L1 DR STILL FWD EMER LT LAMP REPLACED & OPERATION TEST NORMAL IAW AMM 33-51-05.</P>)SDR UIEA2024080900819Engine · faulted#1 ENGINE IN FLIGHT SHUTDOWN DIVERTED TO ICN.(<P>ACCOMPLISHED WO 134669. R/R #1 ENG IAW WC 71-099-02-01 & OPS & LEAK CHECK GOOD IAW AMM 71-00-02.</P>)SDR UIEA2024072900759None · noneATB PERFORMED DUE TO COLLAPSED PALLET OF BATTERIES AT POSITION GL.(<P>PER AMM 05-51-15 INSPECTED MCD POSITION GL AREA FOR CHEMICAL SPILL AND FOUND NO SPILLAGE. BATTERIES FOUND TO BE LITHIUM BATTERIES AND NO DEFECTS NOTED. NO DAMAGE OR DEFECTS TO A/C PER AMM 25SDR UIEA2024071700682Brake Assy · failed#12 BRAKE FAILED ON LANDING(<P>REPLACED #12 BRAKE ASSY PER AMM 32-41-15. OPS & LEAK CHECK OK</P>)SDR UIEA2024071200645Flap System · faultedUPON DEPARTURE, FLAPS DRIVE. OUTBOARD FLAPS LOCKED AT APPROX F5 POSITION.(<P>PERFORMED FLAPS OPS TEST SEVERAL TIMES PER AMM 27-58-01, CAN'T DUPLICATE FAULT ON GROUND. COMPLETED AP 28370 FOR TE FLAP SYS, FLAP SYS OPS TEST NORMALSDR UIEA2024052200400Rvdt · faultedDURING FLAP RETRACTION AFTER DEPARTURE, FLAP DRIVE CAME ON EICAS. FLAPS WOULD NOT RETRACT PAST 5DEG ON OUTBOARD FLAPS(<P>R/R RH OUTBOARD RVDT PER AMM 27-58-01. NO FURTHER DEFECTS NOTED. </P>)SDR UIEA2024041400274Engine · leakingNR 4 ENGINE OIL QUANTITY DROPPED TO 2 QTS IN FLIGHT. C/W WO #128800, R & R NR 4 ENGINE, OPS & LEAK CHECKED NORMAL IAW W/C # 71-099-02-01.SDR UIEA2024012300018Gcu · failedAC 1 BUS FAILED(<P>REMOVED AND REPLACED THE GCU 1 IAW AMM 24-23-01/401. OPS CHK IS GOOD</P>)SDR UIEA2023091500835Seal · unknown#4 OIL QTY DECREASING IN FLIGHT 1 QUART PER 20 MIN(<P>PERFORMED ENGINE DRAIN INSPECTION IAW AMM 71-71-00, FOUND OIL LEAKING FROM HMM DRAIN LINE. R/R CARBON SEAL AT AGB IAW AMM 72-64-02. R/R HHM IAW AMM 73-21-14. PERFORMED IDLE LEAK CHECK TEST #3 & #12 EEC ACTUSDR UIEA2023070600723Actuator · unknownFOUND FUNCTION FAIL AT RH BLG ALTERNATE EXTENSION ROTARY ACTUATOR(<P>1) IAW AMM 32-35-01-004-001 REV 107 AND AMM 32-35-01-404-007 REV 107 R/R RH BLG ALTERNATE EXTENSION ACTUATOR. 2) IAW AMM 32-35-00-715-059 REV 107 PERFORM RH BLG ALTERNATE EXTENSION SYSTEM OPESDR UIEA2023070600722Battery · unknownFOUND EMERGENCY LT POWER SUPPLY BATTERY (M5170) AT STA 550 WL323 LBL 83 FUNCTIONAL FAIL(<P>IAW AMM 33-51-04-902-001-001 REV 107 REMOVED AND SENT THE BATTERY FOR REPAIR, AFTER THAT, INSTALLED THE BATTERY AND PERFORMED POWER SUPPLY TEST. THE TEST RESULT WAS GOODSDR UIEA2023070600721Bracket · unknownFWD LWR WING TO BODY FAIRING PANEL SUPPORT BRACKET SKIN CORROSION STA 920 BL0(<P>1) REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 97. 2) INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 97, DWG 65B06704 SH2 REV F AND DWG 142U0130 SH1 REV A. 3) JOB COMPLETED AND CSDR UIEA2023070600720Doubler · unknownWATER FILL CONNECTION AREA DOUBLER CORROSION AT STA 980 S45R - S46R(<P>1) REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 97. 2) INSTALL NEW PARTS SRM 51-40-02-0G-0 REV 97, DWG 142U3780 SHEET 12 REV F, DWG 140U0999 SHEET 30 REV -, DWG 142U0130 SHEET 1 REV A AND SDR UIEA2023070600719Unknown · unknownCRACK - WEB AND STIFFENER, LH WING INBD FIXED T/E BEAM OUTBD END WBL 429.47(<P>1) PERFORM EI T2023A57M-1568 REV 0. 2) ACCOMPLISHED IAW EI T2023A57M-1568 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL. PN 65B10865-3</P>)SDR UIEA2023070600718Unknown · unknownDEVIATION - DURING PERFORMING TASK CARD 4453A087 PART 2, THE EXISTING CONDITION IS DIFFERENT WITH DWG AT STA 440 LH SIDE(<P>1) ACCOMPLISHED JOB IAW EI T2023A53M-1564 REV 0. 2) ACCOMPLISHED IAW EI T2023A53M-1564 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMASDR UIEA2023070600717Unknown · unknownDEVIATION - DURING PERFORMING TASK CARD 4453A087 PART 2 EXISTING CONDITION IS DIFFERENT WITH DWG AT STA 340 RH SIDE(<P>1) ACCOMPLISHED JOB IAW EI T2023A53M-1571 REV 0. 2) ACCOMPLISHED IAW EI T2023A53M-1571 REV 1. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>
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