N451PA
Service difficulty reports · 216
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 = 'N451PA' 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 = 'N451PA' 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 P5CA2019092300199Doubler · delaminatedLT WING, O/B AFT FLAP, UPPER PNL, EXISTING REPAIR - DOUBLER FOUND DELAMINATED. PERFORMED PERMANENT REPAIR OF LT WING O/B AFT FLAP, UPPER O/B PANEL #588IT AS PER HX RI NR RI-57-00-13720 REV A.SDR P5CA2018112630356Engine · not reportedRTO RUNWAY 25L, @ 80 KTS. DOUBLE POP ON #3 ENGINE, EGT 736 AT IDLE, TAXI TO THE GATE. OIL PRESSURE NORMAL.(<P>REMOVED AND REPLACED #3 ENGINE IAW EO WORK CARDS 71-099-02-01, LEAK AND RUN UP CHECKS WERE NORMAL</P>)SDR P5CA201811200351Shaft · sheared#3 ENGINE OIL PRESSURE DECREASED TO 98 PSI IN FLIGHT, AND THEN 38 PSI AT IDLE. "ENG 3 OIL FILTER" EICAS MESSAGE. RAN QRH PROCEDURE, AND SHUT DOWN ENG 3. (<P>COMPLIED WITH POST WINDMILL INSPECTION IAW B747 AMM 72-00-00-206-059-J00, AND FIM TASK 71-00 A07 "ENG 3SDR P5CA2017083100304Fitting · corrodedFOUND MAIN DECK FITTING CORRODED BS 1500, LBL 81. REPLACED THE FITTING IAW AMM 20-51-01-912-008, REV 90. CONDITION CHECKED NORMAL.SDR P5CA2017083100306Bracket · corrodedCORROSION ON THE SUPPORT BRACKET LOWER FUSELAGE WING TO BODY FAIRING BS 920, BL 0. REMOVED THE PART IAW SRM 51-40-02-0G-0, REV 80. INSTALLED A NEW PART IAW SRM 51-40-02-0G-0, REV 80, DWG 65B06704, SHEET 2, REV F, AND DWG 142U0130, SHEET 1, REV A3. CONDITIOSDR P5CA2017083100293Floorbeam · corrodedCORROSION ON THE FLOORBEAM UPPER ANGLE OF MAIN DECK CARGO AT BS 460, NEAR LBL 105. ACCOMPLISHED EI T2017A53M-1839, REV 2.SDR P5CA2017083100294Skin · corrodedCORROSION ON THE INNER SKIN UPPER OF L5 DOOR. ACCOMPLISHED EI T2017A52M-1879, REV 1.SDR P5CA2017083100297Bulkhead · damagedAFT PRESSURE BULKHEAD FWD FACE HAD ONE DENT AND A SCRATCH BS 2376, WL 212, LBL 65. REPAIRED IAW SRM 53-80-08, REPAIR 7, REV 80. CONDITION CHECKED NORMAL.SDR P5CA2017083100298Seat Track · brokenFOUND SEAT TRACK BROKEN AT BS 1485, RBL 75.92. REPAIRED IAW SRM 53-00-52-2R-13, REPAIR 13, REV 80. CONDITION CHECKED NORMAL.SDR P5CA2017083100299Floorbeam · corrodedCORROSION ON THE FLOORBEAM UPPER ANGLE OF MAIN DECK CARGO AT BS 460, NEAR LBL 105. ACCOMPLISHED EI T2017A53M-1839, REV 2. CONDITION CHECKED NORMAL.SDR P5CA2017083100300Skin · corrodedCORROSION ON THE INNER SKIN UPPER OF LT SIDE NR 5 MAIN ENTRY DOOR. ACCOMPLISH EI T2017A52M-1879, REV 1. CONDITION CHECKED NORMAL.SDR P5CA2017083100301Floorbeam · corrodedFOUND FLOORBEAM CORRODED AT BS 2100, LBL 86.67. REPAIRED IAW SRM 53-00-51-2R-3, REPAIR 3, REV 80, DWG 65B38105, SHEET 10, REV -, AND DWG 65B21441, SHEET 8, REV C. CHECKED NORMAL.SDR P5CA2017083100303Fitting · corrodedFOUND MAIN DECK FITTING CORRODED BS 2060, LBL 81. REPLACED THE FITTING IAW AMM 20-51-01-912-008, REV 90. CONDITION CHECKED NORMAL.SDR P5CA2017083100305Fitting · corrodedFOUND MAIN DECK FITTING CORRODED BS 1640, LBL 39.69. REPLACED THE FITTING IAW AMM 20-51-01-912-008, REV 90. CONDITION CHECKED NORMAL.SDR P5CA2017083100307Plate · corrodedCORROSION ON PLATE, LT WING L/E TO FRONT SPAR CAVITY AT OLES 1425.31. REMOVED DAMAGED PART IAW SRM 51-40-02, REV 80. INSTALLED THE PLATE IAW SRM 51-40-02, REV 80, AND DWG 65B11862, SH2, REV F. CONDITION CHECKED NORMAL.SDR P5CA2017083100308Plate · corrodedCORROSION ON PLATE LT WING L/E TO FRONT SPAR CAVITY AT OLES 1305.14. REMOVED THE DAMAGED PART IAW SRM 51-40-02, REV 80. INSTALLED THE PLATE IAW SRM 51-40-02, REV 80, AND DWG 65B11862 SH2, REV F 3. CONDITION CHECKED NORMAL.SDR P5CA2017083100309Seat Track · brokenFOUND SEAT TRACK CRACKED AT BS 984 LBL 76.92. REPAIRED IAW SRM 53-00-52-2R-13, REPAIR 13, REV 80. CONDITION CHECKED NORMAL.SDR P5CA2017083100310Seat Track · brokenFOUND SEAT TRACK BROKEN AT BS 961, RBL 76.92 AND BS 980, RBL 75.92. REPAIRED IAW SRM 53-00-52-2R-13, REPAIR 13, REV 80. CONDITION CHECKED NORMAL.SDR P5CA2017083100311Seat Track · brokenFOUND SEAT TRACK BROKEN AT BS 1523, LBL 77. REPAIRED AREA IAW SRM 53-00-52-2R-13, REPAIR 13, REV 80. CONDITION CHECKED NORMAL.SDR P5CA2017083100312Floorbeam · corrodedCORROSION ON THE FLOORBEAM UPPER ANGLE NEAR BS 1500, RBL 23. ACCOMPLISHED EI T2017A53M-1890, REV 1 & 2. CONDITION CHECKED NORMAL.SDR P5CA2017083100313Floorbeam · corrodedCORROSION ON THE UPPER ANGLE OF MAIN DECK FLOORBEAM AT BS 980 NEAR LBL 85. ACCOMPLISH EI T2017A53M-1837, REV 2. CHECKED NORMAL.SDR P5CA2017083100314Skin · nickedFOUND A NICK IN SKIN BETWEEN STRINGERS 6L & 7L, BS 1034. REPAIRED IAW SRM 53-00-01-2R-9, REV 80. CHECKED NORMAL.SDR P5CA2016120200303Line · leakingEICAS MESSAGE NR 3 ENG OIL PRESSURE, QUANTITY READ ZERO. INSPECTED AND FOUND THAT OIL LEAK FROM THE NR 3 ENG MAIN FUEL PUMP DRAIN LINE. SERVICED THE OIL SYS AND CAPPED MAIN FUEL PUMP DRAIN LINE THEN NO OIL LEAK NOTED AND OIL QTY NORMAL AFTER ENG RUN CHECK IASDR P5CA2016091700259Hydraulic Line · leakingAFTER TAKEOFF, CREW OBSERVED STEADY HYDRAULIC FLUID LOSS IN SYSTEM NR 4. HYDRAULIC LOSS CONTINUED TO .67 WITH SYS DEPRESSURIZED. AFTER INSPECTION , MAINTENANCE NOTED NO FLUID LOSS IN NR 4 SYSTEM. QTY WAS FULL AFTER ACFT LANDED. MAINTENANCE FOUND THE PNEUMASDR P5CA2016060600128Warning Message · activatedLOW SPEED REJECT DUE TO ENGINE 2 REVERSER EICAS APPPLIED MEL 78-31-01A. CAT "C". MAINTENANCE PROCEDURE COMPLETED.SDR P5CA2015121200198Escape Reel · damagedCOCKPIT DESCENT DEVICE NR 4 HAS CABLE EXTENDED. R & R NR 4 COCKPIT DESCENT DEVICE IAW AMM 25-61-01.SDR P5CA2015121200199Escape Reel · damagedCOCKPIT DESCENT DEVICE NR 6 HAS CABLE EXTENDED. R & R COCKPIT DESCENT DEVICE IAW AMM 25-61-01.SDR P5CA2015121200200Escape Reel · damagedCOCKPIT DESCENT DEVICE NR 5 HAS CABLE EXTENDED. R & R DESCENT DEVICE IAW AMM 25-61-01.SDR P5CA2015121200201Escape Reel · damagedCOCKPIT DESCENT DEVICE NR 7 HAS CABLE EXTENDED. R & R NR 7 DESCENT DEVICE IAW 25-61-01.SDR P5CA2015121200202Escape Reel · damagedCOCKPIT DESCENT DEVICE NR 8 HAS CABLE EXTENDED. R & R COCKPIT DESCENT DEVICE IAW AMM 25-61-01.SDR P5CA2015100100162Unknown · odorODOR FROM INSIDE COCKPIT, LIKE VINYL BURNED. INSPECTED INSIDE, E1, E2 RACK BOTH SIDE TUNNEL, SUPPLY FAN, EXHAUST FAN, INSIDE COCKPIT, INSIDE LT PFD AND RT PFD, UPPER AND LOWER EICAS ALL CDU OK IAW MM 05-51-56-200-801, ENGINE RUN CHECKED IAW MM 71-00-00-862-00SDR P5CA2015081100083Frame · damagedNR 2 ENGINE LT CORE COWL FRAME HOLD OPEN ROD BRACKET MOUNT HOLE 3 EA ELONGATED. NR 2 ENGINE LT CORE COWL FRAME HOLD OPEN ROD BRACKET, MOUNT HOLE ELONGATED AREAS. REPAIRED IAW SRM 51-70-11: EO 4471A153, REV 0.SDR P5CA2015081100082Panel · damagedNR 3 PYLON, RT EXHAUST NOZZLE UPPER SKIRT PANEL 1 EA HOLE FOUND ELONGATED, NR 3 PYLON RT SKIRT FAIRING SKIN ELONGATED FASTENER HOLE REPAIRED IAW R1-54-50-11007.SDR P5CA2015081100081Skin · dentedRIGHT MLG INBD AFT STRUT DOOR EXTERNAL OUTER SKIN FOUND DENT, RT BLG INBD AFT STRUT DOOR EXTERNAL OUTER SKIN DENT AREAS AND DAMAGED RIB REPAIRED IAW R1-52-80-11002, REV B.SDR P5CA2015081100080Support Fitting · crackedLEFT WING - NR 6 SPOILER ACTUATOR SUPPORT FITTING FOUND CRACKED AT OTBD LOWER FLANGE, LT WING - NR 6 SPOILER ACTUATOR SUPPORT FITTING OTBD LOWER FLANGE CRACK AREA REPAIRED IAW SRM 57-51-13-2R-1, REPAIR 1.SDR P5CA2015081100078Shear Tie · crackedFWD CARGO -BS 980, STR 37R -STR 38R FWD FRAME SHEAR TIE FOUND CRACKED AT RADIUS, FWD CARGO COMPARTMENT BS 980 RIGHT BETWEEN STR 37R TO STR 38R FRAME SHEAR TIE IS REPAIRED IAW R1: R1-53-22-11018.SDR P5CA2015081100077Skin · crackedRT SIDE BS 980 DRAG SPLICE LOWER FITTING AT STR 38R CRACK FOUND ON SKIN LAYER UNDER FITTING, CRACK RUNNING DOWNWARD AT 6 O'CLOCK POSITION THROUGH THICKNESS, FUSELAGE SKIN IS REPAIRED IAW SRM 53-20-01-2R-2. REPAIR 2 AT BS 939.5 TO 991.5 BETWEEN STR 37R-39R ARESDR P5CA2015081100076Hinge Fitting · crackedRT WING REAR SPAR NR 7 SPOILER MID HINGE FITTING OTBD LOWER 3EA RIVET HEAD CRACKED. RT WING REAR SPAR NR 7 SPOILER ACTUATOR SUPPORT FITTING CRACKED AREA REPAIRED IAW R1-57-51-11009.SDR P5CA2015081100075Access Panel · chafedNR 3 PYLON, ACCESS PANEL NR 472EL, 2EA FASTENER HOLES FOUND CHAFED. NR 3 PYLON, ACCESS PANEL NR 472EL DAMAGED. FASTENER HOLES REPAIRED IAW R1-54-57-11017, REV A.SDR P5CA2015081100074Access Panel · chafedNR 3 PYLON, ACCESS PANEL NR 472ER, 2EA FASTENER HOLES FOUND CHAFED. NR 3 PYLON - ACCESS PANEL NR 472ER, 2EA DAMAGED HOLE REPAIRED IAW R1-54-57-11016, REV A.SDR P5CA2015081100073Skin · crackedRIGHT WING LOWER L/E TIP AT NR 15 K-FLAP OTBD ARM CUTOUT FOUND CRACK, RT WING L/E INBD ILES 514 HOSE BEAM LOWER BEAM CRACK AREA REPAIRED IAW R1-57-41-11011.SDR P5CA2015081000072Support Beam · chafedNR 1 PYLON, NR 3 FAN COWL SUPPORT BEAM RT LOWER SURFACE FOUND DEEP CHAFING, NR 1 PYLON, NR 3 FAN COWL SUPPORT BEAM, RT LOWER SURFACE DEEP CHAFING AREAS REPAIRED IAW R1-54-50-11008.SDR P5CA2015081000071Door Sill · crackedSCD FWD DOOR SILL FOUND CRACKED, M/D-SCD FWD DOOR SILL WALKWAY PANEL CRACKED AREA, REPAIRED IAW R1-25-55-10998.SDR P5CA2015081000070Door Sill · crackedAFT DOOR SILL FOUND CRACK, M/D SIDE CARGO AFT DOOR SILL PANEL CRACK AREAS REPAIRED IAW R1-25-55-10997.SDR P5CA2015081000069Channel · crackedU/D BS 760, LT TENSION TIE FWD CHANNEL 1 EA FASTENER HOLES FOUND CRACKED IN 6 AND 12 O/C POSITION, BOTH 0.030" LENGTH. U/D BS 760, LT TENSION TIE FWD CHANNEL AND AFT CHANNEL CRACK AREAS REPAIRED IAW SRM 53-20-30-2R-1, REPAIR. THIS REPAIR IS CLASSIFIED AS A CASDR P5CA2015081000068Channel · crackedU/D BS 760 RT TENSION TIE AFT CHANNEL, 2 EA FASTENER HOLES FOUND CRACK. U/D BS 760, RT TENSION TIE FWD CHANNEL AND AFT CHANNEL CRACK AREAS REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. THIS REPAIR IS CLASSIFIED AS A CATEGORY B REPAIR.SDR P5CA2015081000067Channel · crackedU/D BS 720, LT TENSION TIE FWD CHANNEL CRACKED AT RADIUS APPROXIMATELY 0.375" LONG. U/D BS 720, LT TENSION TIE FWD CHANNEL AND AFT CHANNEL CRACK AREAS. REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1. THIS REPAIR IS CLASSIFIED AS A CATEGORY B REPAIR.SDR P5CA2015081000066Channel · crackedU/D BS 720 RT TENSION TIE FWD CHANNEL CRACKED AT RADIUS APPROX 0.375" LONG. U/D BS 720 RT TENSION TIE FWD CHANNEL AND AFT CHANNEL CRACK AREAS REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1. THIS REPAIR IS CLASSIFIED AS A CATEGORY B.SDR P5CA2015021100008Actuator · brokenON POST FLIGHT WALK AROUND, FOUND LT WING LANDING GEAR TRUCK POSITION ACTUATOR BROKEN AT BOTH ENDS. R & R LT WING GEAR TRUCK POSITION ACTUATOR IAW AMM 32-11-20-404-010.SDR P5CA2015020900007Oven · failedOVEN CONTROL PANEL HOT WITH C/B PULLED. ODOR OF BURNED PLASTIC. PERFORMED OVEN OPS CHECK AND CHECKED OK. NO PLASTIC ODOR IAW AMM 25-32-00. ACCOMPLISHED CONDITIONAL INSPECTION IAW AMM 05-51-56. NO OTHER ITEMS FOUND.
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