N452PA
Service difficulty reports · 208
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 = 'N452PA' 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 = 'N452PA' 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 P5CA2016051000105Floorbeam · crackedAFT CARGO COMPT RT BS 1840, RBL 1 FLOOR SUPPORT BEAM FOUND CRACK. AFT CARGO COMPARTMENT BS 1840, RBL 0 TO RBL 4 FLOORBEAM UPPER CAP IS REPAIRED IAW HX R1, NO R1-53-25-11337, REV A REPEAT INSPECTION IS REQUIRED IAW RT R1 NR R1-53-25-11337, REV A REPEAT INSPECTSDR P5CA2016051000104Floorbeam · crackedAFT CARGO BS 1900, LBL 41, FLOOR STRUCTURE FOUND CRACK. AFT CARGO COMPARTMENT BS 1900, LBL 39 TO LT OTBD FLOORBEAM UPPER CAP IS REPAIRED IAW SRM 53-60-07-2R, REPAIR 6 FIG 201, DETAIL I. ADJACENT INTERCOSTAL IS REPAIRED IAW SRM 51-70-12-06-0.SDR P5CA2016051000103Channel · crackedM/D BS 720 RT SIDE TENSION TIE END OF OTBD CHANNEL CORNER FOUND CRACK. M/DECK, BS 720 RT SIDE TENSION TIE CHANNEL ARE REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1. SUP: INSPECTION IS REQUIRED IAW SRM 53-20-30-2R-1, REPAIR 1 TABLE NR 3.SDR P5CA2016051000102Channel · crackedM/DECK BS 720 LT SIDE TENSION, THE END OF OTBD CHANNEL CORNER FOUND CRACK. M/DECK BS 720 LT SIDE TENSION THE CHANNELS ARE REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1. SUP: INSPECTION IS REQUIRED IAW SRM 53-20-30-2R-1, REPAIR 1, TABLE 203.SDR P5CA2016051000107Access Panel · damagedNR 1 PYLON 452EL ACCESS PANEL, PYLON V/V, LOWER AFT CORNER FASTENER HOLE ELONGATED. NR 1 PYLON 452EL ACCESS PANEL, PYLON V/V, LOWER AFT CORNER HOLE IS REPAIRED IAW HX R1 NR R1-54-00-11338, REV A.SDR P5CA2016051000109Support · crackedLEFT HORIZAONTAL STABILIZER OTBD FAIRING AFT PANEL SUPPORT CRACK. LT HORIZONTAL STABILIZER OTBD TIP FAIRING AFT T/E CHANNEL IS REPAIRED IAW HX RE NR R1-55-10-11322, REV A.SDR P5CA2016051000110Manifold · chafedNR 4 ENGINE, RT CORE COWL AIR COOLING MANIFOLD DEEP CHAFING. NR 4 ENGINE RT CORE COWL AIR COOLING MANIFOLD, PRE-COOLER EXIT DUCT FLANGE REPAIRED IAW ROHR SB TBC 80C2-NAC-71-032.SDR P5CA2016051000111Duct · chafedNR 1 ENGINE RT CORE COWL AIR COOLING DUCT INTERNAL EDGE AREA FOUND DEEP CHAFING. NR 1 ENGINE, RT CORE COWL AIR COOLING DUCT INTERNAL EDGE, PRE-COOLER EXIT DUCT. REPAIRED IAW ROHR SB TBC 80C2-NAC-71-032.SDR P5CA2016051000112Skin · damagedLEFT BLG INBD STRUT DOOR EXTERIOR SKIN HAS A SCRATCH MARK. LT BLG INBD STRUT DOOR SKIN IS REPAIRED AT BS 1416.5 AREA IAW SRM 52-80-01-2R-1, REPAIR 1, FIG 201.SDR P5CA2016051000113Fitting · crackedFS 1480 TO 1540, STR L32 TO L33 CRACK WAS FOUND AT LT LONGERON EXTENSION FITTING CRACK LENGTH .3750" APPROXIMATELY AT RADIUS AREA. FS 1480 TO 1540, STR L32 TO L33 LT LONGERON EXTENSION FITTING IS REPAIRED IAW EO NR 4453A818, PART 3, REV 12, POST MODIFICATION SDR P5CA2016051000114Fitting · crackedFS 1480 TO 1540, STR R32 TO R33 CRACK WAS FOUND AT RT LONGERON EXTENSION FITTING CRACK LENGTH .5" APPROXIMATELY AT RADIUS AREA. FS 1480 TO 1540, STR R32 TO R33, RT LONGERON EXTENSION FITTING IS REPAIRED IAW EO NR 4453A818, PART 3, REV 12, POST MODIFICATION INSDR P5CA2016051000116Battery Pack · no testU/D MERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED, LESS THAN 15 MINUTES,POWER PACK REPLACED IAW AMM33-51-04.SDR P5CA2016051000115Battery Pack · no testM/D EMERGENCY LIGHT BATTERY PACK CAPACITY CHECK FAILED, LESS THAN 15 MINUTES, POWER PACK REPLACED IAW AMM 33-51-04.SDR P5CA2016051000108Skin · corrodedLT WING OTBD T/E MID FLAP T/E TOP PANEL FOUND CORROSION. LT WING OTBD MID FLAP T/E THE TOP PANEL SUPT AT OTBD AREA CORROSION IS REMOVED. PROTECTED IAW SRM 51-10-02 & 51-20-01 WITHIN SRM 57-53-02-1A-1 ALLOWABLE DAMAGE 1, FIG 101, LIMITATION. BLEND OUT AREA 2SDR P5CA2016051000101Attach Fitting · crackedUPPER LOBE DOUBLER AT THE FUSELAGE AND VERTICAL STABILIZER ATTACH FITTING RT RADIUS UPPER LOBE DOUBLER FOUND CRACK APPROXIMATELY 80MM LONGERON STABILIZER 2403-2524. RT UPPER LOBE DOUBLER AT THE FUSELAGE AND VERTICAL STABILIZER ATTACH FITTING AREA IS REPAIRED SDR P5CA2016013100016Sensor · shortedHEATER RT TAT, FIM TASK 30-31, TASK 810. T/S FOUND RT TAT SENSOR HEATER INTERNALLY SHORTED TO GROUND. THE SENSOR WAS REPLACED IAW AMM 30-31-00 AND TEST PASSED AND MESSAGE CLEARED.SDR P5CA2015092700159Brake Assy · fireBRAKE/GREASE FIRE MOMENTARILY AFTER BLOCK IN. HOT BRAKE INSPECTION ACCOMPLISHED ON NR 9, NR 10, NR 11 BRAKES IAW MM 5-51-26. NO DEFECTS NOTED. AS PRECAUTION, REPLACED NR 9, NR 10, AND NR 11 TIRES AND NR 9 AND NR 10 BRAKES.SDR P5CA2015070800053Warning Message · illuminatedTAKEOFF ROLL, EICAS MESSAGE FOR NR 4 ENG THRUST REVERSER. REJECTED TAKEOFF AND RETURNED TO BLOCKS,SDR P5CA2015062000052Fire Warning · false activationMAIN DECK FIRE WARNING. QRH PROCEDURE AND ALL CHECK LISTS ACCOMPLISHED. PERFORMED EMERGENCY RETURN. AIRCRAFT LANDED NORMALLY. VISUAL INSPECTION OF MAIN DECK CARGO COMPARTMENT. NO EVIDENCE OF FIRE & SMOKE. AS PRECAUTION, REPLACED NR 8 LOOP A AND B SMOKE DETSDR P5CA2015060100046Adc · malfunctionedFLIGHT DIRECTORS ON BOTH SIDES FAILED DURING TAKEOFF AT 200 FT AGL. CYCLED BOTH SWITCHES AND FDS REGAINED OPERATION. FOUND CMC MESSAGE 22877 AND FOLLOWED FIM TASK 22-11, TASK C52. AIR DATA COMPUTER RT REPLACED IAW AMM 34-12-01/401 AND OPS CHECKED GOOD IAW SDR P5CA2015041600021Tire · failedAFTER LANDING, FOUND NR 9 TIRE MAIN WHEEL TIRE BURST, R & R NR 9 WHEEL ASSY IAW MM 32-45-01, ALSO PERFORMED A CHAPTER 5 INSPECTION ON LOG PAGE 692768, ITEM 7 IAW MM 05-51-34.SDR P5CA2014122900064Blade · damagedNR 2 ENGINE VIBRATION AT 5.0 DESCENDING THROUGH FL200. VIBE COULD BE FELT AND INCREASED WITH ENGINE POWER. LEVELING AT 16000' AND AS POWER CAME UP HEARD WHAT SOUNDED LIKE 2 ENGINE COMPRESSOR STALLS. ALL INDICATIONS NORMAL EXCEPT FOR NR 2 ENGINE VIBRATION 5.0 SDR P5CA2014072300021Bearing · migratedAUTOPILOT OSCILLATES AT 1500 FT, COUPLED APPROACH DISCONNECTED. GROUND TEST ELEVATOR SERVO PASS AND AUTOLAND & UNIQUE TEST PASS IAW AMM 22-10-00/501. ON INSPECTION IAW FIM 22-10, TASK 843, FOUND RT BEARING OF ELEVATOR CONTROL ROD AT AFT QUADRANT MIGRATED. SDR P5CA2014040400013Fan · failedE & E COOLING SUPPLY FAN MESSAGE WITH ASSOCIATED ELECTRICAL ODOR. REPLACED FAN AND SYSTEM TESTED NORMAL IAW AMM 21-58-06.SDR P5CA2014040100012Door · damagedLT MLG SHOCK STRUT INBD DOOR PANEL, HAS ELONGATED HOLES AND DAMAGED. REPAIRED IAW RI-52-80-10486, REV A.SDR P5CA2014040100011Skin · crackedBS 983, STR 38L, AT DRAG SPLICE FITTING AREA FOUND ONE FASTENER HOLE, FOUND A CRACK IN SKIN. SKIN REPAIRED IAW SRM 53-20-01-2R2 REPAIR 2, FIG 201.SDR P5CA2014040100010Floorbeam · crackedCABIN BS 1200, LBL 98 TO 127 FLOORBEAM WEB FOUND CRACKED. REPAIRED IAW RI-53-41-10487.SDR P5CA2013112600038Actuator · damagedGEAR MONITOR STATUS MESSAGE. DURING INSPECTION OF MAIN GEAR, MAINTENANCE FOUND THAT THE RT WING GEAR POSITION ACTUATOR ROD END REMOVED FROM SHAFT. R & R RT WING GEAR POSITIONING ACTUATOR IAW AMM 32-11-20. LEAK CHECK GOOD. INSPECTED WING GEAR AND TRUCK AND NOSDR P5CA2013031800006Nozzle · crackedDURING WALKAROUND MAINTENANCE FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, CRACK IS LOCATED AT THE 11 O'CLOCK POSITION ON THE NR 2 ENGINE. THE CRACK IS APPROXIMATELY 10" LONG. AS PER SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. DISPOSITION ISSDR P5CA2013010800001Web · crackedA CRACK WAS FOUND ON RIGHT BODY GEAR INBOARD AFT DOOR- AFT EDGE CLOSEOUT BEAM WEB. THE SRM 52-80-02 FIGURE 101 DETAIL IV - ALLOWABLE DAMAGE 3 DOESN'T ALLOW FOR A CRACK ON INBOARD AFT DOOR- AFT EDGE CLOSEOUT RIB WEB EO 4452A173 FAA 8110-3 DATED 07JAN13 ALSDR P5CA2012100700037Seat Track · damagedDAMAGE TO LOWER FORWARD CARGO COMPARTMENT SEAT TRACK AT BS 560, LBL 24.75. THE DAMAGE EXCEEDS THE ALLOWABLE DAMAGE LIMITS AS PER SRM 53-00-53-1A-1. PERFORMED A TIME LIMITED REPAIR AS DESCIBED IN PART 1 OF EO 4453A780 FAA 8110-3 DATED 06 OCT 12.SDR P5CA2012082800035Pdu · failedPDU 19L1 HOT AND SMOKING. REMOVED PDU. PDU REPLACED IAW AMM 25-57-01. SYSTEM OPS CHECKED GOOD.SDR P5CA2012082400034Structure · damagedDAMAGE FOUND TO MDSCD AREA - BS 1780 SIDEWALL TRIM GUTTER DEFORMED AND MOUNT FASTENERS MISSING, DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 OF EO 4425A315 AND FAA 8110-3 DATED 24AUG12 WORK INSTRUCTIONS. REPETITIVE DVIS REQUIRESDR P5CA2012040100023Relief Valve · faultyNRT TOWER OBSERVED FLUID STREAMING FROM UNDER THE RIGHT WING. NO NOTICEABLE REDUCTION IN FUEL, HYDRAULIC OR OIL QUANTITIES. (DURING MAINTENANCE WALK AROUND THE RIGHT INBOARD FUEL PRESSURE RELIEF VALVE WAS FOUND TO BE OPEN SLIGHTLY. REMOVED AND REPLACED THESDR P5CA2012030500022Seat Track · chafedFORWARD MAIN DECK SEAT TRACK WORN AND CHAFING DAMAGE AT SEVERAL LOCATIONS STA 1680 - 1800 RBL 11.33. (PERFORMED PERMANENT REPAIR TO SEAT TRACK PER SRM 53-00-52 REPAIR 12 AND INSTRUCTION CONTAINED IN EO 4453A702 AND BOEING REPAIR AND DEVIATION RECORD (RDR) ASDR P5CA2012030500021Skate Angle · crackedCRACK ON SKATE ANGLE OF NR 3 PYLON INBOARD FAIRING AT NACELLE STATION 457. (ACCOMPLISHED TIME LIMITED REPAIR PER EO 4454A142 AND BOEING SR 2112722461 AND REPAIR AND DEVIATION RECORD. PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO 24 MONTHS).SDR P5CA2012030500020Frame · crackedCRACK ON THE FUSELAGE FRAME OF MAIN DECK CARGO COMPARTMENT AT STA 1900, S-12R - S-13R. (PERFORMED REPAIR PER EO 4453A690 WHICH REFERS TO VENDOR ENGINEERING INSTRUCTIONS AND APPROVAL PER BOEING SR SR 1-2110434060 AND FAA 8100-9 FORM).SDR P5CA2012030500019Skin · wornTHREE EA FASTENER HOLES WORN ON LT WING LEADING EDGE SKIN AT ILES 653.39. (PERFORMED INTERNAL FLUSH PERMANENT REPAIR PER INSTRUCTIONS IN EO 4457A406 AND BOEING SR 1-2110443013 AND REPAIR AND DEVIATION RECORD RDR).SDR P5CA2012030500018Intercostal · crackedCRACK ON THE INTERCOSTAL OF FLOOR STRUCTURE AT STATION 990.5 RBL 99.08 AND WL 200. (PERFORMED PERMANENT REPAIR PER INSTRUCTIONS IN EO 4453A700 AND BOEING SR 1-2111730438 AND REPAIR DEVIATION RECORD).SDR P5CA2012030500017Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 145, LOWER SIDE. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030500016Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 131. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030500015Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 145 UPPER SIDE. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030500012Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 484. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030500014Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 151 UPPER SIDE. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM RDR).SDR P5CA2012030500013Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 159. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM RDR).SDR P5CA2012030200011Rib · crackedCRACK ON RIB OF LT HORIZONTAL STABILIZER LEADING EDGE AT STA 151. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030200010Rib · crackedCRACK ON RIB OF RT HORIZONTAL STABILIZER LEADING EDGE AT STA 518. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030100009Rib · crackedCRACK ON RIB OF RT HORIZONTAL STABILIZER LEADING EDGE AT STA 510. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4455A075 AND SRM 55-10-09 REPAIR 2 AND OEM REPAIR DEVIATION RECORD).SDR P5CA2012030100007Skin · dentedREPAIR DENT ON LT FUSELAGE SKIN AT STA 710, S-29L & NBSP. DENT MEASURES 8.0" X 1.5" AND IS .210" DEEP. (PERMANENT REPAIR ACCOMPLISHED PER INSTRUCTIONS IN EO 4453A321 WITH APPROVAL PER 8100-9).SDR P5CA2012030100005Skin · nickedFOUND SKIN NICK/DAMAGE 1.8" X 2.1" AT STA 2592, S-38R TO S-42R NEAR AFT JACK POINT AREA. (REPAIRED PER EO 4453A699 APPROVED BY 8100-9).
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