# N69RP: 1969 Beech D55, registration cancelled 2011-12-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 1, 2011
- Status when cancelled: Third renewal notice
- Airframe: [Beech D55](https://openairdocs.org/model/beech-d55) (registry code 1152730)
- Engine: [Continental IO-520 series](https://openairdocs.org/engine/continental-io-520-series) (registry code 17032)
- Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS E5CE](https://openairdocs.org/tcds/E5CE) (OpenAirDocs)
- Serial number: TE-766
- Year built: 1969
- Type of aircraft: Fixed wing multi engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: November 5, 1969
- Certificate issued: May 4, 2005
- Last registry action: October 25, 2007
- Mode S code: A929E2
- Owner when cancelled: [Gta Air Inc](https://openairdocs.org/faa-owner/GTA%20AIR%20INC)
- Location: [Addison, TX](https://openairdocs.org/faa-place/TX/Addison)
- Owner type: Corporation
- Owner's area on the map: 32.9600° N, 96.8372° W: Placed by OpenAirDocs at the center of ZIP code 75001, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N69RP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=69RP
- Page: https://openairdocs.org/deregistered/N69RP-2011-12-01

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 Beech D55: https://openairdocs.org/model/beech-d55.md

## Service difficulty reports (15)

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

- [SDR 2007FA0001029](https://openairdocs.org/sdr/2007FA0001029), Nov 13, 2007: CYLINDER HEAD. CRACKED. CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)
- [SDR 2007FA0001023](https://openairdocs.org/sdr/2007FA0001023), Nov 13, 2007: CYLINDER HEAD. CRACKED. CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)
- [SDR 2007FA0001022](https://openairdocs.org/sdr/2007FA0001022), Nov 13, 2007: CYLINDER HEAD. CRACKED. CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)
- [SDR 2007FA0001021](https://openairdocs.org/sdr/2007FA0001021), Nov 13, 2007: CYLINDER HEAD. CRACKED. CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)
- [SDR 2007FA0001020](https://openairdocs.org/sdr/2007FA0001020), Nov 13, 2007: CYLINDER HEAD. CRACKED. CRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)
- [SDR 2007FA0001019](https://openairdocs.org/sdr/2007FA0001019), Nov 13, 2007: CYLINDER HEAD. CRACKED. CRACKED CYL HEAD BEHIND INJECTOR BETWEEN FIN NR 12, NR 3. DEFECTIVE MFG PROCESS. (K)
- [SDR XGN2007F00025](https://openairdocs.org/sdr/XGN2007F00025), Jul 30, 2007: CYLINDER. CRACKED. NR 6 CYLINDER WAS NEW, REV 3, E SERIES, CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR. THIS IS 6TH REV 3, E SERIES TO CRACK IN THE SAME LOCATION. (K)
- [SDR XGN2007F00021](https://openairdocs.org/sdr/XGN2007F00021), Jul 30, 2007: CYLINDER HEAD. CRACKED. NR 6 CYLINDER WAS NEW ECI, REV 3, E SERIES, CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR. THIS IS 6TH ECI, REV 3, E SERIES, TO CRACK IN THE SAME LOCATION. (K)
- [SDR 2007FA0000698](https://openairdocs.org/sdr/2007FA0000698), Jul 30, 2007: CYLINDER. CRACKED. NR 6 CYLINDER WAS NEW ECI REV 3 E SERIES CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR. THIS IS 6TH ECI REV 3 E SERIES TO CARCK IN THE SAME LOCATION. (K)
- [SDR XGN2004F00001](https://openairdocs.org/sdr/XGN2004F00001), Dec 10, 2003: CAMSHAFT. BROKEN. AIRCRAFT WAS ENROUTE, PIC NOTICED THE AIRCRAFT YAWING WAY TO THE RIGHT. THERE WAS NOT ANY LOSS OF OIL OR FUEL PRESSURE NOR ANY VIBRATION. THE PILOT SHUT THE ENG
- [SDR XGN2002F00000](https://openairdocs.org/sdr/XGN2002F00000), Dec 31, 2001: CRANKCASE. CRACKED. HALF CIRCLE CRACKED AT NR 6 CYLINDER PAD. CRACK RUNS FROM UPPER PART OF CRANKCASE FROM CYLINDER BASE STUD AT 2 OCLOCK POSITION TO CYLINDER BASE STUD AT 10 OCLOC
- [SDR 20010411CW007](https://openairdocs.org/sdr/20010411CW007), Mar 6, 2001: COUNTERWEIGHT. SEPARATED. COUNTERWEIGHT DEPARTED LEFT PROP ON TAKEOFF ROLL. SPINNER AND BACKING PLATE WERE DESTROYED. PROP HUB WAS CRACKED IN TWO PLACES. NO OTHER DAMAGE TO AIRCRAFT OR E
- [SDR 95ZZZX6562](https://openairdocs.org/sdr/95ZZZX6562), Nov 14, 1995: FLAP. FAILED. UPON EXITING THE AIRCRAFT, THE WEIGHT OF THE PILOT STANDING ON THE RT FLAP, TORE THE ACTUATOR ATTACH BRACKET, RIPPED THE SKIN AND PULLED THE RIB ATTACHMENT OUT 
- [SDR 95ZZZX2261](https://openairdocs.org/sdr/95ZZZX2261), Apr 10, 1995: OIL PAN. CRACKED. DURING FLIGHT, PILOT NOTICED OIL STREAMING FROM RT COWLING. INSPECTION BY MAINTENANCE PERSONNEL REVEALED A 2 INCH CRACK IN THE OIL PAN AT LOWER RADIUS. SUSPECT 
- [SDR 95ZZZX1099](https://openairdocs.org/sdr/95ZZZX1099), Jan 19, 1995: CYLINDER. CRACKED. DURING A 200-HOUR INSPECTION ALL CYLINDERS OF LT ENGINE PASSED A DIFFERENTIAL COMPRESSION TEST. CLOSER INSPECTION OF CLYLINDER ASSYS REVEALED CRACKS BETWEEN COO

## 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 20000503020399I](https://openairdocs.org/incident/20000503020399I), May 3, 2000: Beech D55 (N69RP), Dallas, TX. (-23)Mechanic was repositining an aircraft, N69RP, to the signatur south FBO. Approaching runway 31L ATC instructed him to hold short. After 4-5 minutes he…

## Other aircraft with N69RP

- [Registered now](https://openairdocs.org/aircraft/N69RP): Cirrus Design SR22T, S/N 11773

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