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 P5CA2022022200073None · noneLHW O/B MID FLAP MIDDLE AREA UPPER PANEL 587MT AFT EDGE FOUND BUGLE UP (CORROSION)(<P>LHW O/B MID FLAP MIDDLE AREA UPPER PANEL 587MT AFT EDGE CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 57-53-02-1A-1 LIMIT</P>)SDR P5CA2022030100074None · noneM/D STA 1846 RBL 11.33" SEAT TRACK FOUND BROKEN(<P>M/D STA 1766.45 TO STA 1870.45 RBL 11.33" SEAT TRACK REPAIRED IAW SRM 53-00-52-2R-12 REPAIR 12 FIG 201 REV.94 DATE 20FEB 2022</P>)SDR P5CA2022030200075None · noneSTA 2598 L/H B/H LOWER CORNER 3EA FASTENER HOLE FOUND CRACK AT AFT INNER CHORD(<P>STA 2598 LOWER CORNER LH AFT INNER CHORD 3EA FASTENER HOLE CRACK AREA REPAIRED IAW RI NO: 53-80-15413 REV.A</P>)SDR P5CA2022030200076None · noneRHS CANTED HORIZONTAL FLANGE OF STA 1241 BULKHEAD FORGED FTG FOUND 2EA CRACK AT 3 O'CLOCK AND 9 O'CLOCK POSITION AND BOTH APPROX 3/16" IN DEPTH AT THE BOTTOM OF FIRST LAYER.(<P>FX - STA 1241 R/H CANTED HORIZONTAL FLANGE BULKHEAD FORGED FTG P/N: 65B07920-50 1EASDR P5CA2022030300077None · noneRHW O/B FORE FLAP O/B L/E AREA FOUND DELAM(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07 PAR.5.A REV.94 ,FEB20/2022 AND REFER TO HX PROCESS CARD CONTROL SEQUENCE NO. WO.637467 FOR REPAIR DETAILS</P>)SDR P5CA2022030300078None · noneLHW #11 KRUEGER FLAP O/B LWR CORNER FOUND DELAM(<P>PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-17 PAR.5.G REV.94.FEB20/2022 AND REFER TO HX PROCESS CARD SEQUENCE NO. WO.625865 FOR REPAIR DETAILS</P>)SDR P5CA2022030400079Shear Tie · none1EA CRACK WAS FOUND ON THE RBL 33.99 AND 1EA CRACK WAS FOUND ON THE RBL 57.5 SHEAR TIE AT 1000 FRONT SPAR(<P>STA 1000 RBL 33.99 AND RBL 57.5 SHEAR TIE REPLACED AND INSTALLED IAW EO 4453C024 PART 8 AND PART 9 AND RI 53-00-15419 REV.A, RI 53-00-15420 REV.A</P>)SDR P5CA2022030400080None · noneLH BLG W/W STA 1438-1460 STR 35L INTERCOSTAL FOUND CRACK(<P>LH BLG W/W STA 1438-1460 STR 35L INTERCOSTAL P/N: 65B16948-3 REPAIRED IAW RI-53-00-15421 REV.A</P>)SDR P5CA2022030500081None · noneNO.3 PYLON #472ER ACCESS PANEL 1EA FASTENER LOCK PLATE ATT RIVET FOUND BROKEN AND 1EA FASTENER HOLE FOUND WORN(<P>NO.3 PYLON ACCESS PANEL 472ER FASTENER HOLE ELONGATION AREA REPAIRED IAW RI-54-50-15409 REV.A</P>)SDR P5CA2022030500082None · noneNO.3 PYLON 472EL ACCESS PANEL 1EA FASTENER HOLE FOUND WORN(<P>NO.3 PYLON 472EL ACCESS PANEL FASTENER HOLE ELONGATION WORN AREA REPAIRED IAW RI-54-50-15410 REV.A</P>)SDR P5CA2022030500083None · noneNO.4 PYLON 482EL ACCESS PANEL 1EA FASTENER HOLE FOUND WORN(<P>NO.4 PYLON 482EL ACCESS PANEL FASTENER HOLE ELONGATION WORN AREA REPAIR IAW RI-54-50-15415 REV.A</P>)SDR P5CA2022030500084None · noneNO.2 PYLON 462EL ACCESS PANEL 2EA FASTENER HOLE FOUND WORN(<P>NO.2 PYLON 462EL ACCESS PANEL FASTENER HOLE ELONGATION WORN AREA REPAIRED IAW RI-54-50-15414 REV.A</P>)SDR P5CA2022030700086None · noneBS 2231 1EA CRACK WAS FOUND ON THE FASTENER HOLE AT S25L RUNNING FWD AT 4 O'CLOCK POSITION APPROX 0.040"(<P> STA 2231 STR 25L FRAME STRAP LAYER 1EA FASTENER HOLE OVERSIZE REPAIRED IAW RI-53-60-15406 REV.A</P>)SDR P5CA2022030700087None · noneBS 2231 2EA CRACK WERE FOUND ON THE FASTENER HOLE AT STR 17L RUNNING AFT AT 9 O'CLOCK POSITION APPROX 0.040"(<P>M/D - STA 2231 STA 17L FRAME STRAP LAYER CRACK AREA REPAIRED IAW RI-53-60-15406 REV.A</P>)SDR P5CA2022031000089Web · noneSECT 44 - MAIN DECK FOUND CRACK ON THE WEB OF PRESSURE DECK AT STA 1241 RHS AND LHS 106, CAT C TIME - LIMITED REPAIR(<P>SECT 44 - MAIN DECK PRESSURE DECK AT STA 1241 TO STA 1265 LBL 98- LBL 127 P/N: 65B26630-11 AND STA 1241 TO STA 1265 RBL98-RBL127 WEB P/N: 65SDR P5CA2022031000090None · noneLHS CANTED HORI FLANGE OF STA 1241 BULKHEAD FORGED FITTING FOUND CRACK RUNNING I/B AT 3 O/C POSITION AND APPROX 7/8 IN LENGTH AT UPPER SURFACE(<P>FX - STA 1241 L/H O/B CANTED HORI FLANGE OF BULKHEAD FORGED FTG P/N: 65B07920-49 CRACK AREA REPAIRED IAW RI-53-00-SDR P5CA2022030800088Duct · noneNO.4 ENG R/H C-DUCT OPEN ACTUATOR ATT FITTING BOLT HOLE FOUND ELONGATED.(<P>NO.4 ENG R/H C-DUCT REPLACED IAW AMM 78-31-01. T/R COWL P/N 683L177G13 CONVERSION TO P/N 683L179G09 REF TO CARD NO. CR.636372</P>)SDR P5CA2021061100236Door · damagedDURING WALK AOUND INSP FOUND TAIL SKID MARKS ON BOTH APU DOORS(<P>REPLACED RH/LH APU DOORS. PERFORMED REPAIR OF TAILCONE AREA PER BOEING SR AND E.O. (OFF PART: PN 65B02771-209, SN TLS23687)</P>)SDR P5CA2021033000076Skin · damagedDURING A-CHECK FUSELAGE SKIN DAMAGE, SIZE 10"L X 5.1"W, AND STRINGER DAMAGED SIZE 1.5" L X 0.3" W. REFER TO RAM FORM N453PA-21-01 AND N453PA-21-02. ACCOMPLISHED A PERMANENT REPAIR TO / THE DAMAGED SKIN (PN: 65B23900-1) BETWEEN STA 2577 TO BSTA 2598 AND STRISDR P5CA2021031500070Compressor · damagedDEPARTING KLAX ENG #1 COMPRESSOR STALLED 4 TIMES CLIMING OUT OF APPROX 1000'. QRH PROCEDURES FOLLOWED RESULTING IN NORMAL ENGINE OPERATION.(<P>PERFORMED STALL INSPECTION WITH BOROSCOPE AT HPC 1,6,12,13,14. FOUND DAMAGE AT 12,13,14 BLADES SO DECIDED ENGINE REPLSDR P5CA2021011000011Bleed Valve · malfunctionedBLEED NR 3 EICAS MESSAGE ON TAKE OFF ROLL. FWD TO MEL 36-11-03, MDDR 140670, CAT C. DEACT NR 3 HP BLEED. REMOVED AND REPLACED HPC (OFF PART: PN 773289-18, SN 200002037) AND HPV, IAW B747 AMM 36-11-00. OPERATIONS CHECK GOOD. THIS CLEARS MDDR 140670.SDR P5CA2020071300264B-Nut · leakingIN FLIGHT HYD QTY LOW, NR 4 INDICATING .34. AFTER LANDING .74. FIM 29-11/884. EXTERNAL LEAK CHECKED IAW AMM 29-11-00 AND FOUND RUNNING LEAK AT GROUND SPOILER CONTROL VALVE B-NUT. TIGHTENED THE B-NUT AND LEAK CHECKED OK. SYSTEM NR 4 SERVICED IAW AMM 12-12-01. SDR P5CA2020052100162Smoke Detector · false activationEICAS WARNING "FIRE MN DK MID" DURING CRUISE. VISUALLY VERIFIED FALSE. ITEM 2: CARGO "CGO DET 8 MN DK" STATUS MESSAGE. (<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>ITEM 1: ITEM UNABLE TO DUPLICATE, / PLEASDR P5CA2020031600060Frame · damagedFWD CARGO STA 620 LBL 45 FRAME UPPER CHORD DAMAGED.(<P>FWD CARGO STA 620 LBL 45 FRAME UPPER CHORD REPAIRED AS PER SRM 53-20-07-2R REPAIR 11.</P>)SDR P5CA2020031600061Seat Track · corrodedM/D - STA 900 - 920 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 900 - 920 RBL SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52 FIG 101.</P>)SDR P5CA2020031600062Seat Track · corrodedM/D - STA 1120 TO 1140 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D - STA 1120 TO 1140 LBL 11 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52 FIG 101</P>)SDR P5CA2020031600063Seat Track · corrodedM/D - STA 1840 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D - STA 1840 LBL 11 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52 FIG 101.</P>)SDR P5CA2020031600064Seat Track · corrodedM/D - STA 980 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D - STA 980 LBL 11 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52 FIG 101.</P>)SDR P5CA2020031600065Skin · damagedFX STA 1840 - 1900 S-42L TO S-43L SKIN DAMAGED.(<P>FX STA 1840 - 1900 S-42L TO S-43L SKIN REPAIRED AS PER SRM 53-00-01-2R-1 AND RI 53-60-13958 REV A.</P>)SDR P5CA2020031600066Seat Track · corrodedM/D - STA 1480 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1480 RBL 11 SEAT TRACK REPAIRED AS PER RI 53-60-13947 REV A.</P>)SDR P5CA2020031600067Seat Track · corrodedM/D STA 830 - 950 LBL 11" SEAT TRACK FOUND CORROSION.(<P>M/D STA 830 - 950 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)SDR P5CA2020031600071Seat Track · corrodedM/D - STA 2150 - 2190 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 2150 - 2190 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)SDR P5CA2020031600072Seat Track · corrodedM/D - STA 1480 - 1590 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1480 - 1590 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12.</P>)SDR P5CA2020031600073Doubler · crackedTAIL SECTION STA 2520 RH LOBE DOUBLER FOUND CRACK.(<P>TAIL SECTION STA 2520 RH LOBE DOUBLER CRACK AREA REPAIRED AS PER RI 53-00-13952 REV A.</P>)SDR P5CA2020031600077Light · inoperativeL/H DOOR 1 FWD DOOR SILL EMERGENCY LIGHT FOUND INOP (L1853).(<P>L/H DOOR 1 FWD DOOR SILL EMERGENCY LIGHT LAMP REPLACED AND OPERATION TEST NORMAL IAW AMM 33-51-05.</P>)SDR P5CA2020031600078Light · inoperativeL/H DOOR 1 FWD ENTRANCE CEILING EMERGENCY LIGHT FOUND INOP.(<P>L/H DOOR 1 FWD ENTRANCE CEILING EMERGENCY LIGHT LAMP REPLACED AND LAMP TEST NORMAL IAW AMM 33-51-07.</P>)SDR P5CA2020031600080Web · crackedSTA 1241 L/H B/H WEB FOUND CRACK.(<P>STA 1241 L/H B/H WEB CRACK AREA REPAIRED AS PER RI-53-00-13943 REV A.</P>)SDR P5CA2020031600081Web · crackedSTA 1241 RH B/H WEB FOUND CRACK.(<P>STA 1241 R/H B/H WEB CRACK AREA REPAIRED AS PER RI-53-00-13943 REV A.</P>)SDR P5CA2020031600083Light · dimCOCKPIT - AISLE EMER LT FOUND DIM.(<P>COCKPIT AISLE EMER LT REPLACED AND TEST NORMAL IAW AMM 33-51-00.</P>)SDR P5CA2019122740233Scavenge Pump · contaminatedSHUT DOWN THE NR 1 ENGINE DUE TO LOW OIL QUANTITY. MAINTENANCE NOTED THAT UPON ARRIVAL, OIL QUANTITY RETURNED TO 18 QUARTS. NO LEAKS FOUND. PERFORMED AN INSPECTION OF THE SCAVENGE SYSTEM FILTERS, FOUND DEBRIS IN THE TRANSFER GEARBOX INLET SCREEN TO THE SSDR P5CA2019122300229Engine · failedNR 1 ENGINE FAILED AT 3500 FT MESSAGE ON APPROACH IN RAIN WITH NAI ON ENGINE RESTARTED AUTOMATICALLY. FOLLOWED FIM 71-00 FIGURE 114 FOR AUTO SHUTDOWN EVENT. ALSO FOLLOWED POWERPLANT ENGINEERING GUIDANCE TO ACCOMPLISH BORESCOPE / INSPECTION FOR INTERNAL DAMAGESDR P5CA2019112090217Actuator · malfunctionedFUEL X-FEED 2 STATUS MESSAGE.(<P>FOUND #2 FUEL X-FEED C/B POPPED OUT, C/B RESET AND POPPED AGAIN. REMOVED AND REPLACED #2 FUEL X-FEED ACTUATOR IAW AMM 28-22-01. </P>)SDR P5CA201904043046Actuator · malfunctionedFLIGHT CREW ABORTED TAKE-OFF DUE TO BODY GEAR STEERING MESSAGE. AIRCRAFT RETURNED TO BLOCKS. (<P>LH BODY GEAR RH STEERING ACTUATOR CHECKED IN LOCKED IN CMC BUT WAS FOUND TO BE EXTENDED. REMOVED AND REPLACED LH BODY GEAR RH STEERING ACTUATOR PER AMM 32-53-11. VSDR P5CA201904010042Warning Message · false activationFLIGHT CREW ABORTED TAKE OFF IN ANC DUE TO BODY GEAR STEERING WARNING DURING TAKE OFF ROLL. DURING DEBRIEF OF CREW THEY ADVISED THAT MESSAGE DISAPPEARED AFTER THE ABORT. THEY CONTINUED WITH A SUCCESSFUL TAKEOFF WHEN MESSAGE RE-APPEARED SHORTLY AFTER. FLIGHTSDR P5CA2017063000215Extinguisher · leakingUPPER DECK WATER FIRE EXTINGUISHER LEAKING. REMOVED AND REPLACED THE WATER FIRE EXTINGUISHER IAW AMM 26-26-02.SDR P5CA2017061600199Depressor · tornFOUND LOWER AFT CARGO DOOR DEPRESSOR SEAL TORN LEFT SIDE OF DOOR CUT OUT 10OCLOCK POS. PERFORMED TIME LIMITED REPAIR IAW SRM 53-00-15-2.SDR P5CA2016120900316Escape Reel · damagedCOCKPIT DESCENT DEVICE NR 8, CABLE DAMAGED AND EXTENDED. REMOVED AND REPLACED THE DESCENT DEVICE IAW AMM 25-61-01.SDR P5CA2016093000274Unknown · odorDURING APPROACH, SMELL OF SMOKE AND LOW HUMMING SOUND NOTED. TURNED OFF PACK 1 AND CONDITION CEASED. FOUND CMC MSG 21189. T/S SUSPECT PACK 1 ACM AT FAULT. DEFERRAL AS PER MEL 21-51-01-02. DUE TO PACK 1 INOP FWD CARGO REMAINS EMPTY PER MEL 26-16-01-02-01B.SDR P5CA2016080100179Warning System · activatedABORTED TAKEOFF LOW SPEED 70 KNOTS DUE TO EICAS MESSAGE ELECTRIC DRIVE 3. TRANSFER TO MDDR 68827 IAW MEL 24-11-01A, CAT B.SDR P5CA2016051000106Panel · damagedNR 2 PYLON V/V PANEL 462ER FASTENER HOLE ELONGATED. NR 2 PYLON V/V PANEL 462ER IS REPAIRED IAW HX R1 R1-54-00-11339, REV A.
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