# N556SS: Diamond Aircraft Ind DA20-A1, registration cancelled 2001-08-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 10, 2001
- Exported to: Austria
- Status when cancelled: Triennial form not returned
- Airframe: [Diamond Aircraft Ind DA20-A1](https://openairdocs.org/model/diamond-aircraft-ind-da20-a1) (registry code 2990000)
- Data sheets: [TCDS TA4CH](https://openairdocs.org/tcds/TA4CH) (OpenAirDocs)
- Serial number: 10127
- Type of aircraft: Fixed wing single engine
- Certificate issued: May 23, 1996
- Last registry action: July 6, 2001
- Mode S code: A71756
- Owner when cancelled: [Bcc Equipment Leasing Corp](https://openairdocs.org/faa-owner/BCC%20EQUIPMENT%20LEASING%20CORP)
- Location: [Long Beach, CA](https://openairdocs.org/faa-place/CA/Long%20Beach)
- Owner type: Corporation
- Owner's area on the map: 33.8239° N, 118.1113° W: Placed by OpenAirDocs at the center of ZIP code 90808, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N556SS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=556SS
- Page: https://openairdocs.org/deregistered/N556SS-2001-08-10

From the FAA registry file of November 12, 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 Diamond Aircraft Ind DA20-A1: https://openairdocs.org/model/diamond-aircraft-ind-da20-a1.md

## Service difficulty reports (2)

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

- [SDR 99ZZZX281](https://openairdocs.org/sdr/99ZZZX281), Dec 16, 1998: WASHER. WRONG PART. UPON INSPECTION OF THE WING ATTACH A-BOLT, NOTED THE WASHER LISTED IN THE PARTS MANUAL, AN 960-C616, PAGE I-53-2, IS INCORRECT IN SIZE AND WILL ALLOW THE BOLT T
- [SDR 99ZZZX280](https://openairdocs.org/sdr/99ZZZX280), Dec 16, 1998: FUEL CELL. CRACKED. UPON REMOVAL OF FUEL CELL TO RIG RUDDER CABLES, NOTED THE INTERNAL BAFFLE SPOT WELDS WERE CRACKING THROUGH TO THE TANK OUTER SKIN. LEAKS WERE DETECTED AND REPAI

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