N454PA
Service difficulty reports · 176
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 = 'N454PA' 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 = 'N454PA' 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 P5CA2022012800026None · noneRHW O/B FORE FLAP L/E FOUND DELAMINATION (71" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)SDR P5CA2022012800027None · noneRHW O/B FORE FLAP L/E FOUND DELAMINATION (127" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A</P>)SDR P5CA2022012800028None · noneRHW O/B MID FLAP L/E FOUND DELAMINATION (116" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)SDR P5CA2022012800029None · noneRHW I/B FORE FLAP L/E CTR AREA FOUND DELAMINATION (155" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)SDR P5CA2022012800030None · noneRHW I/B MID FLAP L/E FOUND DELAMINATION (3" TO O/B, 18" TO AFT)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)SDR P5CA2022012800031None · noneLHW O/B MID FLAP CTR L/E FOUND DELAMINATION (127" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)SDR P5CA2022012800032None · noneLHW O/B FORE FLAP L/E FOUND DELAMINATION (77" TO O/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)SDR P5CA2022012800033None · noneLHW O/B MID FLAP L/E FOUND DELAMINATION (235" TO I/B)(<P>REPAIRED WITH COMPOSITE HOT BOND METHOD AS PER SRM 51-70-07 PAR 5A </P>)SDR P5CA2022012800034None · noneR/H BLG I/B W/W DOOR I/B EDGE FOUND DEFORMED(<P>R/H AFT MLG O/B AFT SECONDARY DOOR AFT BEAM DEFORMATION REPAIR</P>)SDR P5CA2022012800035None · noneNOSE NLG W/W FWD RH CORNER SKIN DOUBLER AREA 1EA FASTENER HOLE FOUND CRACKED ON THE NO.2 AND NO.3 LAYER (CHORD AND BULKHEAD CHORD)(COUNT FROM LOWER) STA 240(<P>NOSE NLG W/W FWD RH CORNER SKIN DOUBLER AREA ATTACH CHORD AND BULKHEAD CHORD 1EA FASTENER HOLE CRACKSDR P5CA2022012800036None · noneNOSE NLG W/W FWD L/H CORNER SKIN DOUBLER AREA 1EA FASTENER HOLE FOUND CRACKED ON THE SECOND LAYER (CHORD) (COUNT FROM LOWER) STA 240.(<P>NOSE NLG W/W FWD L/H CORNER SKIN DOUBLER AREA ATTACH CHORD 1EA FASTENER HOLE CRACK REPAIRED.</P>)SDR P5CA2022012800037None · noneNOSE NLG W/W FWD L/H AND R/H CORNER MOD DOUBLERS SHORT EDGE MARGINS(<P>NOSE NLG W/W FWD L/H AND R/H CORNER MOD DOUBLERS SHORT EDGE MARGINS REPAIRED</P>)SDR P5CA2021102000400None · noneAPU FIRE HANDLE LIGHT FLICKERS AND MAKES CLICKING NOISE WITH NO FIRE WARNING HORN.(<P>FOUND DAMAGED WIRE IN APU COMPARTMENT. APU FIRE DETECTION DEFERRED PER DDG 26-15-01-01B, MDDR 155418.</P> / <P>LP 1488596 - FOUND WIRE DAMAGE AT APU COMPT INSIDE WIRE # W720-SDR CNF5REV/2021/07Sleeve · dimON 06TH OCTOBER 2021, WE HAVE FOUND ON OUR ASSEMBLY SHOP AN OVERSIZE SLEEVE ITEM 600 ON ATTACHED SKETCH , THIS SLEEVE P/N 65B19933-1 S/N R2018-75406 IS MATCHED SET WITH THE OUTER CYLINDER P/N 161U1505-10 S/N BFG3300 INSTALLED ON THE FRESH OVERHAUL GEAR WLG RH SDR P5CA2021100300374Module · faultedINTERMITTENT FIRE BELL/MASTER WARNING IN CLIMB, CRUISE AND DESCENT, NO OTHER INDICATIONS. REMOVED AND REPLACED MAWEA MASTER MODULE A, AND MASTER MODULE B, OPS CHECK GOOD IAW AMM 31-51-00.SDR P5CA2020072310267Probe · malfunctioned#2 EGT INDICATION ON UPPER EICAS ERRATIC AND CONSTANTLY FLUCTUATING AND GOING BLANK. ENGINE #2 ALL 8 EGT PROBES REPLACED. ENG NR 2 W13 HARNESS ALSO REPLACED. ENG NR 2 RUN TESTED NORMAL IAW AMM 77-21-02.SDR P5CA2020021300025Skin · chafedCHAFING AILERON, R/H WING INBD AILERON OTBD SIDE WBL 515 AREA.(<P>REMOVE THE CHAFING MATERIAL AND CLEAN. MEASURE THE DAMAGE AREA (L = 0.8", W = 0.2" AT AFT EDGE, AT OTBD EDGE, AT R/H WING INBD AILERON UPPER SKIN PNL) BOND REPAIR PLIES USE WET LAYUP WITH RESIN.SDR P5CA2020021300028Connector · damagedDAMAGE: FOUND THE CONNECTOR DAMAGE OF MOTOR -OVRD/JTSN 3 AFT, EQUIPMENT NO:M226.(<P>1) IAW SWPM 20-61-11 REV 72 AND WDM 28-31-26 REV 27, REPLACED MOTOR-OVRD/JTSN 3 AFT CONNECTOR DM226 AT R/H W/W AND THE CONDITION CHECKED NORMAL.</P><P>2) IAW WDM 28-31-26 REV SDR P5CA2020021300029Skin · dentedDENT - SKIN, V. STAB LEFT UPPER RUDDER EXTERNAL SURFACE SKIN DENT AT RUD STA 282.(<P>CUT OUT THE DAMAGED MATERIAL AND CLEAN. MEASURE THE DAMAGED AREA (L = 1.5", W = 0.7", D =3, PLIES. 52.5" FROM AFT EDGE. 22.5" FROM UPPER EDGE AT RUD STA 282) BOND THE REPAIR PSDR P5CA2020021300030Floorbeam · corrodedFOUND CORROSION AT STA 1740 LBL 110. M/D FLOOR STRUCTURE UPPER CAP.(<P>REMOVE DAMAGED PART IAW SRM 51-40-02 REV. 87. INSTALL NEW PART IAW SRM 51-40-02 REV. 87 AND EI NO. T2020A53M-262 REV.1 AND DWG NO. 65B17764 SHEET 4, REV. E AND DWG NO. 14641941 SHEET 79, RESDR P5CA2020021300031Shear Tie · corrodedFOUND SHEAR TIE CORROSION AT STA 1777, LBL 107 AND LBL 110.(<P>ACCOMPLISHED EI NO. T2020A53M-146 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR P5CA2020021300032Floorbeam · wornWORN DAMAGE IN FASTENER HOLES OF MAIN DECK FLOOR BEAM UPPER CHORDS AND INTERCOSTAL AT STA 1380, RBL 11.(<P>ACCOMPLISHED EI NO. T2020A53M-154 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR P5CA2020021300033Battery Pack · no testTEST FAIL: FOUND EMERGENCY BATTERY PACK M5168 CAN NOT STAY ON 15 MINS.(<P>1) IAW AMM 33-51-04-002-009-001 REV 97, REMOVED EMERGENCY BATTERY POWER PACK ASSY M5168.</P><P>2) IAW AMM 33-51-04-402-012-001 REV 97, INSTALLED EMERGENCY BATTERY POWER PACK ASSY M5168.<SDR P5CA2020021300034Seat Track · crackedFOUND SEAT TRACK CRACK AT STA 1920 RBL 98, M/D FLOOR.(<P>ACCOMPLISHED REPAIR IAW SRM 53-60-52-01-1 REV. 87 AND EI NO. T2020A53M-164 REV. 1 AND BOEING DWG NO. 65B38251 SH 62 REV. A, SH 66 REV. -, SH 67 REV. A. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR P5CA2020021300035Connector · damagedFOUND FUEL BOOST PUMP TANK NO. 3-AFT M31 CONNECTOR DAMAGE AT R/H W/W.(<P>1) IAW SWPM 20-61-11 REV. 72 AND WDM 28-22-34 REV. 27, REPLACED FUEL BOOST PUMP TANK NO. 3-AFT CONNECTOR DM31 AT R/H W/W AND CONDITION CHECKED NORMAL.</P><P>2) IAW WDM 28-22-34 REV 27, PESDR P5CA2020021300036Floorbeam · dentedDENT - WEB, AFT CARGO FLOOR STRUCTURE AT STA 1673 RBL 16.(<P>ACCOMPLISHED JOB IAW EI NO. T2020A53M-111 REV. 2. CONDITION CHECK NORMAL AND JOB COMPLETED. </P>)SDR P5CA2020021300037Floorbeam · corrodedCORROSION ON THE ANGLE OF FLOOR BEAM CAP AT STA 2300, NEAR LBL 11.(<P>ACCOMPLISHED EI NO. T2020A53M-265 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)SDR P5CA2020021300038Connector · damagedDAMAGE: FOUND THE CONNECTOR DAMAGE OF MOTOR-OVRD/JTSN 2 AFT, EQUIPMENT NO. M223.(<P>1) IAW SWPM 20-61-11 REV 72 AND WDM 28-31-25 REV 27, REPLACED MOTOR-OVRD/JTSN AFT CONNECTOR (DM223) AT L/H WING W/W.</P><P>2) IAW WDM 28-31-25 REV 27, PERFORM WIRE CONTINUITY CSDR P5CA2020021300039Connector · crackedCRACK - FOUND JTSN/OVRD CTR RH (M225) PUMP CONNECTOR CRACK.(<P>1) IAW SWPM 20-61-11 REV 22 AND WDM 28-31-21 REV 27, REPLACED CONNECTOR DM225 OF JTSN/OVRD CTR RH W/W AND THE CONDITION CHECKED NORMAL.</P><P>2) IAW WDM 28-31-21 REV 29, PERFORM WIRE CONTINUITY CHKSDR P5CA2020021300040Connector · damagedFOUND FUEL BOOST PUMP TANK NO.2-AFT M23 CONNECTOR DAMAGE AT LH W/W.(<P>1) IAW SWPM 20-61-11 REV 72 AND WDM 28-22-33 REV 27, REPLACED FUEL BOOST PUMP TANK NO.2 AFT CONNECTOR (DM23) AT LH WING W/W.</P><P>2) IAW WDM 28-22-33 REV 27, PERFORMED WIRE CONTINUITY CHK SDR P5CA2020021300041Connector · damagedCRACK: FOUND JTSN/OVRD CTR LH (M224) PUMP CONNECTOR CRACK.(<P>1) IAW SWPM 20-61-11 REV 72 AND WDM 28-31-22 REV 27, REPLACED JTSN/OVRD CTR LH PUMP CONNNECTOR (DM224) AT LH W/W.</P><P>2) IAW WDM 28-31-22 REV 27, PERFORMED WIRE CONTINUITY CHK AND RESULT IS SATISFSDR P5CA2020021300042Connector · damagedDAMAGE: FOUND THE CONNECTOR DAMAGE OF MOTOR-OVRD/JTSN 2 FWD, EQUIPMENT NO. 222.(<P>1) IAW SWPM 20-61-11 REV 72 AND WDM 28-31-23 REV 27, REPLACED MOTOR-OVRD/JTSN 2 FWD CONNECTOR (DM222) AT LH WING W/W.</P><P>2) IAW WDM 28-31-23 REV 27, PERFORM WIRE CONTINUITY CSDR P5CA2020021300043Connector · damagedDAMAGE: FOUND THE CONNECTOR DAMAGE OF MOTOR-OVRD/JTSN 3 FWD EQUIPMENT NO.M227.(<P>1) IAW SWPM 20-61-11 REV 72 AND WDM 28-31-2 REV 27, REPLACED MOTOR-OVRD/JTSN 3 FWD CONNECTOR DM227 AT RH W/W AND CONDITION CHECKED NORMAL.</P><P>2) IAW WDM 28-31-24 REV 27, PERFOSDR P5CA2020021300044Battery Pack · no testFOUND EMERGENCY LIGHT POWER PACK FUNCTIONAL FAIL.(<P>IAW AMM 33-51-04-902-001-001 REV 97, REPLACED EMERGENCY LIGHT POWER PACK M5170 AND PERFORMED POWER SUPPLY TEST, THE RESULT WAS SATISFACTORY. </P>)SDR P5CA2019080650162Oil System · lowLOW OIL QUANTITY NR 1 ENGINE. REMOVED AND REPLACED THE NR 1 ENGINE. C/W PER WORK CARD 71044-02-01. OPS CK NORMAL.SDR P5CA2019040900050Window · crackedRIGHT SIDE CREW REST PASSENGER WINDOW CRACKED. (<P>REMOVED AND REPLACED RIGHT SIDE CREW REST PASSENGER WINDOW, OUTER PANE IAW AMM 56-21-01. </P>)SDR P5CA201805220076Jumper · damagedEQUIPMENT COOLING MESSAGE. INSTALLED A JUMPER IAW DDG 21-58-07A, MESSAGE CLEARED.SDR P5CA2018013000018Seat Track · deformedM/D BALL MAT STA 1780 TO 1840 RBL 13 TO 31 FWD LH REPAIRED AREA FOUND DEFORM(<P>M/D STA 1780 TO STA 1840 RBL 13" TO RBL 31" BALL MAT PANEL LHS SUBJECT RAIL REPLACED IAW SRM 51-10-02</P>)SDR P5CA2018013000019Cargo Net · tornBULK CARGO, BS 1980, LT CARGO NET TORN REPAIRED IAW CMM 25-50-00, REV 33, AND RI-25-50-12411, REV A.SDR P5CA2018013000020Splice · chafedFUSELAGE SPLICE FITTING AT BS 1230 FOUND CHAFED. REPAIRED IAW RI-53-00-12422, REV B.SDR P5CA2018013000021Torque Box · puncturedAFT CARGO BETWEEN BS 1660 AND 1680, LT FLOOR TORQUE BOX METAL PANEL PUNCTURED. REPAIRED IAW RI-51-00-12419, REV A.SDR P5CA2018013000022Splice · chafedFUSELAGE BS 1232 FOUND CHAFED. REPAIRED IAW RI-53-00-12422, REV B.SDR P5CA2018013000023Caster · damagedMAIN DECK CARGO BALL MAT CASTER SUPPORT BASE FOUND BROKEN AT BS 1780 TO 1840, RBL 31 TO 56, THE CASTER SUPPORT BASE WAS REPAIRED IAW EO 4425A500, REV 1.SDR P5CA2018013000025Frame · chafedNR 2 ENGINE RT CORE COWL INNER WALL FRAME FOUND CHAFED. REPAIRED IAW E0-1971A169.SDR P5CA2018013000026Stiffener · crackedAPU FIREWALL FWD FACE NR 2 STIFFENER, RBL 32 FOUND CRACKED AT BS 2658. THE STIFFENER WAS REPAIRED IAW RL-53-83-12420, REV A.SDR P5CA2018013000027Skin · dentedRIGHT HORIZONTAL STAB LWR HSS 327 FOUND DENTED. THE SKIN WAS BLENDED AND REWORKED IAW HX-55-10-12428, REV A.SDR P5CA2018013000028Skin · chafedNR 2 ENGINE, RT CORE COWL PRECOOLER EXHAUST DUCT INLET CASE FOUND CHAFED. REPAIRED IAW EO 4471A029, REV 4.SDR P5CA2018013000029Frame · crackedAPU BAY FRAME AT BS 2669.52 CRACKED. THE FRAME WAS REPAIRED IAW SRM 51-70-11, FIG 1.SDR P5CA2018013000030Housing · damagedMAIN DECK CARGO DOOR SILL HANDLING CASTER HOUSING FOUND DAMAGED. REPAIRED.SDR P5CA2018013000031Skin · scratchedEXTERNAL SKIN AT BS 1860 BETWEEN STRINGERS 46L & 47L SCRATCHED. THE SKIN WAS REPAIRED.
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