# Service difficulty reports: N582P, cancelled Dec 31, 2022

A list on [N582P, cancelled Dec 31, 2022](https://openairdocs.org/deregistered/N582P-2022-12-31.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 61 reports

- [SDR I5HA0858002](https://openairdocs.org/sdr/I5HA0858002.md): Skin · corroded · Apr 10, 2008 · N582P · Cvac 440 · Wing, Plate/Skin
  > DURING 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 I5HA0758007](https://openairdocs.org/sdr/I5HA0758007.md): Spring · loose · Apr 11, 2007 · N582P · Cvac 580 · Door Warning System
  > WHILE 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 HO
- [SDR 15HA0358005](https://openairdocs.org/sdr/15HA0358005.md): Smoke · detected · May 18, 2004 · N582P · Cvac 440 · Air Distribution System
  > CREW 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 15HA0458004](https://openairdocs.org/sdr/15HA0458004.md): Compressor · damaged · Feb 21, 2004 · N582P · Cvac 440 · Turbine Engine Compressor Section
  > DURING 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 PIEC
- [SDR 15HA0358007](https://openairdocs.org/sdr/15HA0358007.md): Quick Disconnect · worn · Jan 6, 2004 · N582P · Cvac 580 · Engine Fuel Distribution
  > IMMEDIATELY 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 WA
- [SDR I5HA0358006](https://openairdocs.org/sdr/I5HA0358006.md): Pump · malfunctioned · Dec 26, 2003 · N582P · Cvac 580 · Turbine Engine Oil System
  > WHILE 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-HA
- [SDR I5HA0358003](https://openairdocs.org/sdr/I5HA0358003.md): Engine · malfunctioned · May 7, 2003 · N582P · Cvac 440 · Engine (Turbine/Turboprop)
  > ON 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 DEFE
- [SDR 15HA0358002](https://openairdocs.org/sdr/15HA0358002.md): Line · broken · Apr 23, 2003 · N582P · Cvac 440 · Turbine Engine Oil System
  > WHILE 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 97ZZZX1570](https://openairdocs.org/sdr/97ZZZX1570.md): Frame · cracked · Jan 28, 1997 · N582P · Cvac 440 · Wing Miscellaneous Structure
  > LEFT WING STA 25 FRAME CRACKED UPPER 'Z'.
- [SDR 97ZZZX1569](https://openairdocs.org/sdr/97ZZZX1569.md): Beaver Tail Rib · corroded · Jan 28, 1997 · N582P · Cvac 440 · Trailing Edge Flaps
  > RIGHT WING BEAVER TAIL, NUMEROUS RIBS HAVE EXFOLIATION.
- [SDR 97ZZZX1568](https://openairdocs.org/sdr/97ZZZX1568.md): Skin · corroded · Jan 28, 1997 · N582P · Cvac 440 · Wing, Plate/Skin
  > LEFT WING UPPER SURFACE HAS CORROSION ON PLANK AND STRINGER BULKHEAD, STA 235 TO 28.5
- [SDR 97ZZZX1567](https://openairdocs.org/sdr/97ZZZX1567.md): Skin · cracked · Jan 28, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > FUSELAGE INNER SKIN SURFACE CRACKED STA 344, STR'S 13L-14L.
- [SDR 97ZZZX1566](https://openairdocs.org/sdr/97ZZZX1566.md): Skin · corroded · Jan 28, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > SKIN CORRODED IN FORWARD CARGO BAY AROUND BELT FRAME 193/210.
- [SDR 97ZZZX1565](https://openairdocs.org/sdr/97ZZZX1565.md): Shroud · cracked · Jan 28, 1997 · N582P · Cvac 440 · Wing Miscellaneous Structure
  > CRACK IN INNER SHROUD RT OTBD L/E STA 290.
- [SDR 97ZZZX1564](https://openairdocs.org/sdr/97ZZZX1564.md): Skin · cracked · Jan 28, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > AFT ADF ANTENNA SKIN CUT-OUT CRACKED.
- [SDR 97ZZZX1563](https://openairdocs.org/sdr/97ZZZX1563.md): Skin · corroded · Jan 28, 1997 · N582P · Cvac 440 · Wing, Plate/Skin
  > SURFACE CORROSION RIGHT WING BAY WING PLANK STA 23 TO STA 29.
- [SDR 97ZZZX1562](https://openairdocs.org/sdr/97ZZZX1562.md): Skin · corroded · Jan 28, 1997 · N582P · Cvac 440 · Wing, Plate/Skin
  > WING SKIN, STRINGERS (4 EACH), FORWARD SPAR WEB, AND AFT SPAR WEB CORRODED FROM WET BAY TO WING TIP.
- [SDR 97ZZZX1561](https://openairdocs.org/sdr/97ZZZX1561.md): Floor Beam · corroded · Jan 28, 1997 · N582P · Cvac 440 · Fuselage Main, Floor Beam
  > FLOOR BEAM STA 681 CORRODED
- [SDR 97ZZZX1559](https://openairdocs.org/sdr/97ZZZX1559.md): Fitting · cracked · Jan 28, 1997 · N582P · Cvac 440 · Horizontal Stabilizer, Attach Fittings
  > RIGHT UPPER FORWARD HORIZONTAL STABILIZER ATTACH FITTING ATTACHED.
- [SDR 97ZZZX1558](https://openairdocs.org/sdr/97ZZZX1558.md): Fitting · cracked · Jan 28, 1997 · N582P · Cvac 440 · Main Landing Gear Attach Section
  > LEFT MLG INBOARD TRUNNION FITTING CRACKED.
- [SDR 97ZZZX1580](https://openairdocs.org/sdr/97ZZZX1580.md): Fitting · cracked · Jan 27, 1997 · N582P · Cvac 440 · Horizontal Stabilizer, Attach Fittings
  > RT UPPER FORWARD HORIZ STAB FITTING CRACKED.
- [SDR 97ZZZX1579](https://openairdocs.org/sdr/97ZZZX1579.md): Floor Beam · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Floor Beam
  > FLOOR BEAM CRACKED STA 718 RBL 8 AND 12.
- [SDR 97ZZZX1578](https://openairdocs.org/sdr/97ZZZX1578.md): Doubler · cracked · Jan 27, 1997 · N582P · Cvac 440 · Nacelle/Pylon Structure
  > DOUBLER CRACKED RT INBD NR 2 ENGINE TAILPIPE ACCESS.
- [SDR 97ZZZX1577](https://openairdocs.org/sdr/97ZZZX1577.md): Skin · cracked · Jan 27, 1997 · N582P · Cvac 440 · Wing, Plate/Skin
  > LEFT MLG WHEELWELL AFT LOWER SKIN CRACKED.
- [SDR 97ZZZX1576](https://openairdocs.org/sdr/97ZZZX1576.md): Structure · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Floor Panel
  > COCKPIT FLOOR STRUCTURE CORRODED STA 109 CENTER AREA.
- [SDR 97ZZZX1575](https://openairdocs.org/sdr/97ZZZX1575.md): Floor Beam · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Floor Beam
  > FLOOR BEAM CORRODED AT STA 712 RT.
- [SDR 97ZZZX1574](https://openairdocs.org/sdr/97ZZZX1574.md): Floor Support · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED BETWEEN STA 681-712 RT.
- [SDR 97ZZZX1573](https://openairdocs.org/sdr/97ZZZX1573.md): Hat Section · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Miscellaneous Structure
  > FUSELAGE HAT SECTION CORRODED STA 681, RT SIDE.
- [SDR 97ZZZX1572](https://openairdocs.org/sdr/97ZZZX1572.md): Stringer · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER CORRODED, STA 698 RT.
- [SDR 97ZZZX1571](https://openairdocs.org/sdr/97ZZZX1571.md): Stringer · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Longeron/Stringer
  > FUSELAGE STRINGER 10 RIGHT, CORRODED STA 712.
- [SDR 97ZZZX1560](https://openairdocs.org/sdr/97ZZZX1560.md): Skin · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > SKIN CRACKED STA 140 STR 11R.
- [SDR 97ZZZX1557](https://openairdocs.org/sdr/97ZZZX1557.md): Frame · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Frame
  > FRAME FLANGE CRACKED STA 641 OUTBOARD AT STR 25L.
- [SDR 97ZZZX1556](https://openairdocs.org/sdr/97ZZZX1556.md): Belt Frame · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Frame
  > BELT FRAME AT STA 698 CORRODED RT SIDE.
- [SDR 97ZZZX1555](https://openairdocs.org/sdr/97ZZZX1555.md): Stringer · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Longeron/Stringer
  > STRINGER 29R CRACKED STA 760.
- [SDR 97ZZZX1554](https://openairdocs.org/sdr/97ZZZX1554.md): Skin · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > SKIN CRACKED STR 29R, STA 798.
- [SDR 97ZZZX1553](https://openairdocs.org/sdr/97ZZZX1553.md): Skin · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > FUSELAGE INNER SKIN CRACKED STA 344 BETWEEN STR 13 AND 14R.
- [SDR 97ZZZX1552](https://openairdocs.org/sdr/97ZZZX1552.md): Skin · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN INNER SURFACE CRACKED STA 420, STR'S 13, 14L.
- [SDR 97ZZZX1551](https://openairdocs.org/sdr/97ZZZX1551.md): Skin · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > FUSELAGE INNER SKIN CRACKED STA 420 STR'S 13 AND 14R
- [SDR 97ZZZX1550](https://openairdocs.org/sdr/97ZZZX1550.md): Skin · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > SKIN AT STR 29R CRACKED BETWEEN STA 730 TO STA 745.
- [SDR 97ZZZX1549](https://openairdocs.org/sdr/97ZZZX1549.md): Intercostal · gouged · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STA 210 GOUGED.
- [SDR 97ZZZX1548](https://openairdocs.org/sdr/97ZZZX1548.md): Stringer · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Longeron/Stringer
  > STR 13R CRACKED AND DISTORTED STA 92.
- [SDR 97ZZZX1547](https://openairdocs.org/sdr/97ZZZX1547.md): Angle · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Miscellaneous Structure
  > ANGLE FORWARD OF CAPTAIN'S INSTRUMENT PANEL CORRODED
- [SDR 97ZZZX1546](https://openairdocs.org/sdr/97ZZZX1546.md): Intercostal · gouged · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Miscellaneous Structure
  > INTERCOSTAL GOUGED AT BELT FRAME FLANGE STA 210 TO STA 227.
- [SDR 97ZZZX1545](https://openairdocs.org/sdr/97ZZZX1545.md): Skin · dented · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > SKIN DENTED STA 937 STR 4L.
- [SDR 97ZZZX1544](https://openairdocs.org/sdr/97ZZZX1544.md): Skin · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > STR 21L LAP SEAM CORRODED STA 413 TO STA 435.
- [SDR 97ZZZX1543](https://openairdocs.org/sdr/97ZZZX1543.md): Skin · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > LAP SEAM CORRODED AT STA 435.23, STR 21R.
- [SDR 97ZZZX1542](https://openairdocs.org/sdr/97ZZZX1542.md): Skin · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > LAP SEAM CORRODED AT 21R STA 509 TO STA 526.
- [SDR 97ZZZX1541](https://openairdocs.org/sdr/97ZZZX1541.md): Skin · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > CROWN SKIN CRACKED STA 760.
- [SDR 97ZZZX1540](https://openairdocs.org/sdr/97ZZZX1540.md): Skin · cracked · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Main, Plate/Skin
  > CROWN SKIN CRACKED STA 730 TO STR 745.
- [SDR 97ZZZX1539](https://openairdocs.org/sdr/97ZZZX1539.md): Angle · corroded · Jan 27, 1997 · N582P · Cvac 440 · Fuselage Miscellaneous Structure
  > AFT BULKHEAD L-ANGLE CORRODED AT FLOOR LEVEL.

Next page: https://openairdocs.org/deregistered/N582P-2022-12-31/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N582P-2022-12-31/reports

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