# N582P: 1957 Convair 440, registration cancelled 2022-12-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 31, 2022 - Status when cancelled: Registration expired, pending cancellation - Airframe: [Convair 440](https://openairdocs.org/model/convair-440) (registry code 2422902) - Engine: [Allison 501-D13 series](https://openairdocs.org/engine/allison-501-d13-series) (registry code 03004) - Data sheets: [TCDS 6A6](https://openairdocs.org/tcds/6A6), [TCDS E-282](https://openairdocs.org/tcds/E-282) (OpenAirDocs) - Serial number: 475 - Year built: 1957 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, transport - Airworthiness date: July 18, 1967 - Certificate issued: September 9, 2019 - Last registry action: September 9, 2019 - Mode S code: A77E9B - Owner when cancelled: [R&R Holdings Inc](https://openairdocs.org/faa-owner/R%26R%20HOLDINGS%20INC) - Location: [Spanaway, WA](https://openairdocs.org/faa-place/WA/Spanaway) - Owner type: Corporation - Owner's area on the map: 47.0609° N, 122.3889° W: Placed by OpenAirDocs at the center of ZIP code 98387, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N582P - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=582P - Page: https://openairdocs.org/deregistered/N582P-2022-12-31 From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Convair 440: https://openairdocs.org/model/convair-440.md ## Service difficulty reports (61, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR I5HA0858002](https://openairdocs.org/sdr/I5HA0858002), Apr 10, 2008: SKIN. CORRODED. 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 - [SDR I5HA0758007](https://openairdocs.org/sdr/I5HA0758007), Apr 11, 2007: SPRING. LOOSE. 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 EMERG - [SDR 15HA0358005](https://openairdocs.org/sdr/15HA0358005), May 18, 2004: SMOKE. DETECTED. 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 - [SDR 15HA0458004](https://openairdocs.org/sdr/15HA0458004), Feb 21, 2004: COMPRESSOR. DAMAGED. 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. T - [SDR 15HA0358007](https://openairdocs.org/sdr/15HA0358007), Jan 6, 2004: QUICK DISCONNECT. WORN. 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. - [SDR I5HA0358006](https://openairdocs.org/sdr/I5HA0358006), Dec 26, 2003: PUMP. MALFUNCTIONED. 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. NO - [SDR I5HA0358003](https://openairdocs.org/sdr/I5HA0358003), May 7, 2003: ENGINE. MALFUNCTIONED. 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 TE - [SDR 15HA0358002](https://openairdocs.org/sdr/15HA0358002), Apr 23, 2003: LINE. BROKEN. 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 P - [SDR 97ZZZX1570](https://openairdocs.org/sdr/97ZZZX1570), Jan 28, 1997: FRAME. CRACKED. LEFT WING STA 25 FRAME CRACKED UPPER 'Z'. - [SDR 97ZZZX1569](https://openairdocs.org/sdr/97ZZZX1569), Jan 28, 1997: BEAVER TAIL RIB. CORRODED. RIGHT WING BEAVER TAIL, NUMEROUS RIBS HAVE EXFOLIATION. - [SDR 97ZZZX1568](https://openairdocs.org/sdr/97ZZZX1568), Jan 28, 1997: SKIN. CORRODED. LEFT WING UPPER SURFACE HAS CORROSION ON PLANK AND STRINGER BULKHEAD, STA 235 TO 28.5 - [SDR 97ZZZX1567](https://openairdocs.org/sdr/97ZZZX1567), Jan 28, 1997: SKIN. CRACKED. FUSELAGE INNER SKIN SURFACE CRACKED STA 344, STR'S 13L-14L. - [SDR 97ZZZX1566](https://openairdocs.org/sdr/97ZZZX1566), Jan 28, 1997: SKIN. CORRODED. SKIN CORRODED IN FORWARD CARGO BAY AROUND BELT FRAME 193/210. - [SDR 97ZZZX1565](https://openairdocs.org/sdr/97ZZZX1565), Jan 28, 1997: SHROUD. CRACKED. CRACK IN INNER SHROUD RT OTBD L/E STA 290. - [SDR 97ZZZX1564](https://openairdocs.org/sdr/97ZZZX1564), Jan 28, 1997: SKIN. CRACKED. AFT ADF ANTENNA SKIN CUT-OUT CRACKED. - [SDR 97ZZZX1563](https://openairdocs.org/sdr/97ZZZX1563), Jan 28, 1997: SKIN. CORRODED. SURFACE CORROSION RIGHT WING BAY WING PLANK STA 23 TO STA 29. - [SDR 97ZZZX1562](https://openairdocs.org/sdr/97ZZZX1562), Jan 28, 1997: SKIN. CORRODED. 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), Jan 28, 1997: FLOOR BEAM. CORRODED. FLOOR BEAM STA 681 CORRODED - [SDR 97ZZZX1559](https://openairdocs.org/sdr/97ZZZX1559), Jan 28, 1997: FITTING. CRACKED. RIGHT UPPER FORWARD HORIZONTAL STABILIZER ATTACH FITTING ATTACHED. - [SDR 97ZZZX1558](https://openairdocs.org/sdr/97ZZZX1558), Jan 28, 1997: FITTING. CRACKED. LEFT MLG INBOARD TRUNNION FITTING CRACKED. - [SDR 97ZZZX1580](https://openairdocs.org/sdr/97ZZZX1580), Jan 27, 1997: FITTING. CRACKED. RT UPPER FORWARD HORIZ STAB FITTING CRACKED. - [SDR 97ZZZX1579](https://openairdocs.org/sdr/97ZZZX1579), Jan 27, 1997: FLOOR BEAM. CRACKED. FLOOR BEAM CRACKED STA 718 RBL 8 AND 12. - [SDR 97ZZZX1578](https://openairdocs.org/sdr/97ZZZX1578), Jan 27, 1997: DOUBLER. CRACKED. DOUBLER CRACKED RT INBD NR 2 ENGINE TAILPIPE ACCESS. - [SDR 97ZZZX1577](https://openairdocs.org/sdr/97ZZZX1577), Jan 27, 1997: SKIN. CRACKED. LEFT MLG WHEELWELL AFT LOWER SKIN CRACKED. - [SDR 97ZZZX1576](https://openairdocs.org/sdr/97ZZZX1576), Jan 27, 1997: STRUCTURE. CORRODED. COCKPIT FLOOR STRUCTURE CORRODED STA 109 CENTER AREA. - [SDR 97ZZZX1575](https://openairdocs.org/sdr/97ZZZX1575), Jan 27, 1997: FLOOR BEAM. CORRODED. FLOOR BEAM CORRODED AT STA 712 RT. - [SDR 97ZZZX1574](https://openairdocs.org/sdr/97ZZZX1574), Jan 27, 1997: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED BETWEEN STA 681-712 RT. - [SDR 97ZZZX1573](https://openairdocs.org/sdr/97ZZZX1573), Jan 27, 1997: HAT SECTION. CORRODED. FUSELAGE HAT SECTION CORRODED STA 681, RT SIDE. - [SDR 97ZZZX1572](https://openairdocs.org/sdr/97ZZZX1572), Jan 27, 1997: STRINGER. CORRODED. FUSELAGE STRINGER CORRODED, STA 698 RT. - [SDR 97ZZZX1571](https://openairdocs.org/sdr/97ZZZX1571), Jan 27, 1997: STRINGER. CORRODED. FUSELAGE STRINGER 10 RIGHT, CORRODED STA 712. - [SDR 97ZZZX1560](https://openairdocs.org/sdr/97ZZZX1560), Jan 27, 1997: SKIN. CRACKED. SKIN CRACKED STA 140 STR 11R. - [SDR 97ZZZX1557](https://openairdocs.org/sdr/97ZZZX1557), Jan 27, 1997: FRAME. CRACKED. FRAME FLANGE CRACKED STA 641 OUTBOARD AT STR 25L. - [SDR 97ZZZX1556](https://openairdocs.org/sdr/97ZZZX1556), Jan 27, 1997: BELT FRAME. CORRODED. BELT FRAME AT STA 698 CORRODED RT SIDE. - [SDR 97ZZZX1555](https://openairdocs.org/sdr/97ZZZX1555), Jan 27, 1997: STRINGER. CRACKED. STRINGER 29R CRACKED STA 760. - [SDR 97ZZZX1554](https://openairdocs.org/sdr/97ZZZX1554), Jan 27, 1997: SKIN. CRACKED. SKIN CRACKED STR 29R, STA 798. - [SDR 97ZZZX1553](https://openairdocs.org/sdr/97ZZZX1553), Jan 27, 1997: SKIN. CRACKED. FUSELAGE INNER SKIN CRACKED STA 344 BETWEEN STR 13 AND 14R. - [SDR 97ZZZX1552](https://openairdocs.org/sdr/97ZZZX1552), Jan 27, 1997: SKIN. CRACKED. FUSELAGE SKIN INNER SURFACE CRACKED STA 420, STR'S 13, 14L. - [SDR 97ZZZX1551](https://openairdocs.org/sdr/97ZZZX1551), Jan 27, 1997: SKIN. CRACKED. FUSELAGE INNER SKIN CRACKED STA 420 STR'S 13 AND 14R - [SDR 97ZZZX1550](https://openairdocs.org/sdr/97ZZZX1550), Jan 27, 1997: SKIN. CRACKED. SKIN AT STR 29R CRACKED BETWEEN STA 730 TO STA 745. - [SDR 97ZZZX1549](https://openairdocs.org/sdr/97ZZZX1549), Jan 27, 1997: INTERCOSTAL. GOUGED. INTERCOSTAL AT STA 210 GOUGED. - [SDR 97ZZZX1548](https://openairdocs.org/sdr/97ZZZX1548), Jan 27, 1997: STRINGER. CRACKED. STR 13R CRACKED AND DISTORTED STA 92. - [SDR 97ZZZX1547](https://openairdocs.org/sdr/97ZZZX1547), Jan 27, 1997: ANGLE. CORRODED. ANGLE FORWARD OF CAPTAIN'S INSTRUMENT PANEL CORRODED - [SDR 97ZZZX1546](https://openairdocs.org/sdr/97ZZZX1546), Jan 27, 1997: INTERCOSTAL. GOUGED. INTERCOSTAL GOUGED AT BELT FRAME FLANGE STA 210 TO STA 227. - [SDR 97ZZZX1545](https://openairdocs.org/sdr/97ZZZX1545), Jan 27, 1997: SKIN. DENTED. SKIN DENTED STA 937 STR 4L. - [SDR 97ZZZX1544](https://openairdocs.org/sdr/97ZZZX1544), Jan 27, 1997: SKIN. CORRODED. STR 21L LAP SEAM CORRODED STA 413 TO STA 435. - [SDR 97ZZZX1543](https://openairdocs.org/sdr/97ZZZX1543), Jan 27, 1997: SKIN. CORRODED. LAP SEAM CORRODED AT STA 435.23, STR 21R. - [SDR 97ZZZX1542](https://openairdocs.org/sdr/97ZZZX1542), Jan 27, 1997: SKIN. CORRODED. LAP SEAM CORRODED AT 21R STA 509 TO STA 526. - [SDR 97ZZZX1541](https://openairdocs.org/sdr/97ZZZX1541), Jan 27, 1997: SKIN. CRACKED. CROWN SKIN CRACKED STA 760. - [SDR 97ZZZX1540](https://openairdocs.org/sdr/97ZZZX1540), Jan 27, 1997: SKIN. CRACKED. CROWN SKIN CRACKED STA 730 TO STR 745. - [SDR 97ZZZX1539](https://openairdocs.org/sdr/97ZZZX1539), Jan 27, 1997: ANGLE. CORRODED. AFT BULKHEAD L-ANGLE CORRODED AT FLOOR LEVEL. All 61: https://openairdocs.org/deregistered/N582P-2022-12-31/reports.md ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20031226034199I](https://openairdocs.org/incident/20031226034199I), Dec 26, 2003: Cvac 440 (N582P), Pittsburgh, PA. (-23) On December 26, 2003, air tahoma flight #484 a convair 440 (CV-580) ws enroute from cincinnati (cvg) to Pittsburgh (pit) when the number two engine low… --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.