N582P, cancelled Dec 31, 2022
Service difficulty reports · 61
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 = 'N582P' AND deregistration_id = 'N582P-2022-12-31' 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 = 'N582P' AND deregistration_id = 'N582P-2022-12-31' 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 I5HA0858002Skin · corrodedDURING A ROUTINE MAINT INSP THE UPPER RT OB WING SKIN TE WAS FOUND CORRODED WITH CRACKS COMING AROUND SEVERAL RIVETS. THE RT UPPER OB WING SKIN WAS REMOVED, ALL THE CORROSION WAS REMOVED, THE WING STRUCTURE INSPECTED, AND THE SKIN WAS REPLACED IAW THE SRM.SDR I5HA0758007Spring · looseWHILE EN-ROUTE, THE CABIN DOOR (OPEN) LIGHT ILLUMINATED. NO DOORS OPENED AND THERE WAS NO LOSS OF CABIN PRESSURE. THE AIRCRAFT LANDED UNEVENTFULLY WITH NO EMERGENCY OR PRECAUTIONARY PROCEDURES TAKEN. INSPECTION BY MAINTENANCE PERSONNEL, DISCOVERED A DOOR HOSDR 15HA0358005Smoke · detectedCREW NOTICED SMOKE IN THE COCKPIT AND CARGO COMPARTMENT JUST AFTER RT ENG WAS STARTED IN PREP FOR THE REGULARLY SCHEDULED FLIGHT. ENG WAS SHUTDOWN AND INSPECTED. NOTHING OUT OF ORDINARY WAS DISCOVERED. MECHANIC HAD CREW DISCONNECT EDC AND ENG WAS RESTARTED.SDR 15HA0458004Compressor · damagedDURING THE DESCENT, AT APPROX 12,000 FT, THE CREW HEARD A LOUD BANG A MOMENT LATER, THE LT FIRE WARNING LIGHT ILLUMINATED AND THE CREW (E) HANDLED THE ENGINE. THE AC MADE AN UNEVENTFUL LANDING. INSPECTION OF THE LT ENGINE HAS REVEALED THE PRESENCE OF A PIECSDR 15HA0358007Quick Disconnect · wornIMMEDIATELY AFTER TAKEOFF FROM CLE, EN ROUTE TO CVG, RIGHT ENGINE AUTO-FEATHERED. THE CREW RETURNED TO CLE WHERE THEY MADE AN UNEVENTFUL SINGLE ENGINE LANDING. INSPECTION REVEALED THE RIGHT ENGINE MAIN FUEL FEED LINE 'QUICK DISCONNECT' FITTING AT THE FIRE WASDR I5HA0358006Pump · malfunctionedWHILE EN ROUTE, RT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED WITH AN ASSOCIATED DROP IN REDUCTION GEARBOX OIL PRESSURE FROM APPROXIMATELY 150 PSI TO 100 PSI. NORMAL LIMITS ARE 130 PSI TO 250 PSI. CREW PERFORMED AN EMERGENCY IN FLT ENG SHUTDOWN USING THE E-HASDR I5HA0358003Engine · malfunctionedON THE TAKEOFF ROLL DEPARTING CVG, EN ROUTE TO CLE THE LEFT ENGINE WOULD ONLY PRODUCE 888 DEGREES, NOMINAL IS 971 DEGREES. THE PILOT ABORTED THE TAKEOFF. THE TEMPERATURE DATRUM (TD) SYSTEM WAS NULLED AND FULL POWER WAS THEN AVAILABLE. THE TD SYSTEM WAS DEFESDR 15HA0358002Line · brokenWHILE EN ROUTE BETWEEN CVG AND PIT, THE CAPTAIN NOTICED A DROP FROM 65 PSI TO 50 PSI IN THE LEFT POEWR SECTION OIL PRESSURE, FLUCTUATING REDUCTION GEARBOX OIL PRESSURE AND A THREE GALLON DROP IN OIL QTY. THE CAPTAIN PULLED THE LEFT 'E' HANDLE AND SECURED THE SDR 97ZZZX1570Frame · crackedLEFT WING STA 25 FRAME CRACKED UPPER 'Z'.SDR 97ZZZX1569Beaver Tail Rib · corrodedRIGHT WING BEAVER TAIL, NUMEROUS RIBS HAVE EXFOLIATION.SDR 97ZZZX1568Skin · corrodedLEFT WING UPPER SURFACE HAS CORROSION ON PLANK AND STRINGER BULKHEAD, STA 235 TO 28.5SDR 97ZZZX1567Skin · crackedFUSELAGE INNER SKIN SURFACE CRACKED STA 344, STR'S 13L-14L.SDR 97ZZZX1566Skin · corrodedSKIN CORRODED IN FORWARD CARGO BAY AROUND BELT FRAME 193/210.SDR 97ZZZX1565Shroud · crackedCRACK IN INNER SHROUD RT OTBD L/E STA 290.SDR 97ZZZX1564Skin · crackedAFT ADF ANTENNA SKIN CUT-OUT CRACKED.SDR 97ZZZX1563Skin · corrodedSURFACE CORROSION RIGHT WING BAY WING PLANK STA 23 TO STA 29.SDR 97ZZZX1562Skin · corrodedWING SKIN, STRINGERS (4 EACH), FORWARD SPAR WEB, AND AFT SPAR WEB CORRODED FROM WET BAY TO WING TIP.SDR 97ZZZX1561Floor Beam · corrodedFLOOR BEAM STA 681 CORRODEDSDR 97ZZZX1559Fitting · crackedRIGHT UPPER FORWARD HORIZONTAL STABILIZER ATTACH FITTING ATTACHED.SDR 97ZZZX1558Fitting · crackedLEFT MLG INBOARD TRUNNION FITTING CRACKED.SDR 97ZZZX1580Fitting · crackedRT UPPER FORWARD HORIZ STAB FITTING CRACKED.SDR 97ZZZX1579Floor Beam · crackedFLOOR BEAM CRACKED STA 718 RBL 8 AND 12.SDR 97ZZZX1578Doubler · crackedDOUBLER CRACKED RT INBD NR 2 ENGINE TAILPIPE ACCESS.SDR 97ZZZX1577Skin · crackedLEFT MLG WHEELWELL AFT LOWER SKIN CRACKED.SDR 97ZZZX1576Structure · corrodedCOCKPIT FLOOR STRUCTURE CORRODED STA 109 CENTER AREA.SDR 97ZZZX1575Floor Beam · corrodedFLOOR BEAM CORRODED AT STA 712 RT.SDR 97ZZZX1574Floor Support · corrodedFLOOR SUPPORT CORRODED BETWEEN STA 681-712 RT.SDR 97ZZZX1573Hat Section · corrodedFUSELAGE HAT SECTION CORRODED STA 681, RT SIDE.SDR 97ZZZX1572Stringer · corrodedFUSELAGE STRINGER CORRODED, STA 698 RT.SDR 97ZZZX1571Stringer · corrodedFUSELAGE STRINGER 10 RIGHT, CORRODED STA 712.SDR 97ZZZX1560Skin · crackedSKIN CRACKED STA 140 STR 11R.SDR 97ZZZX1557Frame · crackedFRAME FLANGE CRACKED STA 641 OUTBOARD AT STR 25L.SDR 97ZZZX1556Belt Frame · corrodedBELT FRAME AT STA 698 CORRODED RT SIDE.SDR 97ZZZX1555Stringer · crackedSTRINGER 29R CRACKED STA 760.SDR 97ZZZX1554Skin · crackedSKIN CRACKED STR 29R, STA 798.SDR 97ZZZX1553Skin · crackedFUSELAGE INNER SKIN CRACKED STA 344 BETWEEN STR 13 AND 14R.SDR 97ZZZX1552Skin · crackedFUSELAGE SKIN INNER SURFACE CRACKED STA 420, STR'S 13, 14L.SDR 97ZZZX1551Skin · crackedFUSELAGE INNER SKIN CRACKED STA 420 STR'S 13 AND 14RSDR 97ZZZX1550Skin · crackedSKIN AT STR 29R CRACKED BETWEEN STA 730 TO STA 745.SDR 97ZZZX1549Intercostal · gougedINTERCOSTAL AT STA 210 GOUGED.SDR 97ZZZX1548Stringer · crackedSTR 13R CRACKED AND DISTORTED STA 92.SDR 97ZZZX1547Angle · corrodedANGLE FORWARD OF CAPTAIN'S INSTRUMENT PANEL CORRODEDSDR 97ZZZX1546Intercostal · gougedINTERCOSTAL GOUGED AT BELT FRAME FLANGE STA 210 TO STA 227.SDR 97ZZZX1545Skin · dentedSKIN DENTED STA 937 STR 4L.SDR 97ZZZX1544Skin · corrodedSTR 21L LAP SEAM CORRODED STA 413 TO STA 435.SDR 97ZZZX1543Skin · corrodedLAP SEAM CORRODED AT STA 435.23, STR 21R.SDR 97ZZZX1542Skin · corrodedLAP SEAM CORRODED AT 21R STA 509 TO STA 526.SDR 97ZZZX1541Skin · crackedCROWN SKIN CRACKED STA 760.SDR 97ZZZX1540Skin · crackedCROWN SKIN CRACKED STA 730 TO STR 745.SDR 97ZZZX1539Angle · corrodedAFT BULKHEAD L-ANGLE CORRODED AT FLOOR LEVEL.
Back to N582P, cancelled Dec 31, 2022