# N898TA: 2000 Raytheon 400A, registration cancelled 2012-08-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 24, 2012
- Exported to: Czech Republic
- Status when cancelled: Valid registration
- Airframe: [Raytheon 400A](https://openairdocs.org/model/raytheon-400a) (registry code 7150010)
- Engine: [Williams FJ44-3A](https://openairdocs.org/engine/williams-fj44-3a) (registry code 66006)
- Data sheets: [TCDS A16SW](https://openairdocs.org/tcds/A16SW), [TCDS E3GL](https://openairdocs.org/tcds/E3GL) (OpenAirDocs)
- Serial number: RK-295
- Year built: 2000
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 8, 2012
- Certificate issued: January 13, 2012
- Last registry action: January 13, 2012
- Mode S code: AC64B6
- Owner when cancelled: [Flight Options LLC](https://openairdocs.org/faa-owner/FLIGHT%20OPTIONS%20LLC)
- Location: [Richmond Heights, OH](https://openairdocs.org/faa-place/OH/Richmond%20Heights)
- Owner type: Corporation
- Owner's area on the map: 41.5532° N, 81.4743° W: Placed by OpenAirDocs at the center of ZIP code 44143, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N898TA
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=898TA
- Page: https://openairdocs.org/deregistered/N898TA-2012-08-24

From the FAA registry file of October 29, 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 Raytheon 400A: https://openairdocs.org/model/raytheon-400a.md

## Service difficulty reports (9)

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

- [SDR DJFA2008089](https://openairdocs.org/sdr/DJFA2008089), Dec 30, 2008: WINDSHIELD. CRACKED. ON FINAL APPROACH PILOTS WINDSCREEN GLASS OUTER PLY CRACKED IN MULTIPLE LOCATIONS. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. 45 MINUTES AFTER LANDING, THE C
- [SDR DJFA2008082](https://openairdocs.org/sdr/DJFA2008082), Nov 22, 2008: RIB. CRACKED. DURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER INBD RIB AND BRACKET ASSEMBLIES, THE RT INBD RI
- [SDR DJFA2007019](https://openairdocs.org/sdr/DJFA2007019), Feb 13, 2007: SEAL. LEAKING. TRIP NR 1141843 CREW REPORTED A NOXIOUS OILY SMELL WHEN ENGINE IS AT HIGH POWER SETTINGS CONTINUING THROUGH CLIMB THEN DISSIPATING DURING CRUISE. MAINTENANCE FO
- [SDR DJFA2006307](https://openairdocs.org/sdr/DJFA2006307), Aug 27, 2006: PRINTED CKT BOARD. SHORTED. KRWI - WHILE ON CLIMBOUT THE NR 1 INVERTER FAILED AND WAS FOLLOWED BY PUNGENT FUMES FROM THE LOWER CIRCUIT BREAKER PANEL. THE AIRCRAFT WAS RETURNED TO KRWI WHER
- [SDR DJFA2006275](https://openairdocs.org/sdr/DJFA2006275), Jun 21, 2006: RIB. CRACKED. DURING A SCHEDULED MAINTENANCE VISIT A VERTICAL STABILIZER SUPPORT RIB WAS FOUND CRACKED. SUPPORT RIB PART NUMBER 45A23324-003 WAS REPLACED REFERENCING THE BEEC
- [SDR DJFA2006264](https://openairdocs.org/sdr/DJFA2006264), Jun 14, 2006: RIB. CRACKED. DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER BRACKET INSPECTION AS PART OF THE A / B LEVEL INSPECTION THE RIGHT INBOARD 
- [SDR DJFA2006213](https://openairdocs.org/sdr/DJFA2006213), Mar 7, 2006: UNKNOWN. UNKNOWN. NORMAL YOKE BACK PRESSURE WAS BEING APPLIED AT ROTATION, DID NOT SEEM TO RESPOND. FURTHER FORCE WAS APPLIED, STILL DID NOT RESPOND. PAST V1 SPEED, FELT CERTAIN 
- [SDR DJFA2005122](https://openairdocs.org/sdr/DJFA2005122), Jul 28, 2005: DOWNLOCK SWITCH. FALSE INDICATION. ON APPROACH, CREW RECEIVED 2 GREEN & NO RED GEAR INDICATIONS. NLG LIGHT WOULD NOT ILLUMINATE, BUT LIGHT WOULD TEST. NO CHANGE IN GEAR DOWN INDICATION WHEN CREW 
- [SDR DJFA2004031](https://openairdocs.org/sdr/DJFA2004031), Nov 9, 2004: BELLOWS. CRACKED. CREW REPORTED AIRCRAFT WOULD NOT INCREASE SPEED WITH INCREASED POWER AND AT 190 KTS STICK SHAKER WAS ENCOUNTERED. ABQ CENTER WAS ADVISED THAT AIRCRAFT HAD TO DE

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