# N9753D: 1959 Piper PA-22-160, registration cancelled 2017-10-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 10, 2017
- Status when cancelled: Valid registration
- Airframe: [Piper PA-22-160](https://openairdocs.org/model/piper-pa-22-160) (registry code 7102214)
- Engine: [Lycoming 0-320 series](https://openairdocs.org/engine/lycoming-0-320-series) (registry code 41508)
- Data sheets: [TCDS 1A6](https://openairdocs.org/tcds/1A6), [TCDS E-274](https://openairdocs.org/tcds/E-274) (OpenAirDocs)
- Serial number: 22-6667
- Year built: 1959
- Type of aircraft: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard
- Airworthiness date: March 5, 1959
- Certificate issued: August 15, 2017
- Last registry action: August 15, 2017
- Mode S code: AD98FD
- Owner when cancelled: [Thomas Daniel C](https://openairdocs.org/faa-owner/THOMAS%20DANIEL%20C)
- Location: [Issaquah, WA](https://openairdocs.org/faa-place/WA/Issaquah)
- Owner type: Individual
- Owner's area on the map: 47.5140° N, 121.9935° W: Placed by OpenAirDocs at the center of ZIP code 98027, within about 4 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N9753D
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=9753D
- Page: https://openairdocs.org/deregistered/N9753D-2017-10-10

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 Piper PA-22-160: https://openairdocs.org/model/piper-pa-22-160.md

## Service difficulty reports (3)

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

- [SDR 96ZZZX5238](https://openairdocs.org/sdr/96ZZZX5238), Oct 4, 1996: TUBE FRAME. CRACKED. INSTRUMENT PANEL CROSS-TUBE CRACKED AT BRAKE LEVER MOUNTING BRACKET WELD (MORE THAN ONE-FOURTH OF CIRCUMFERENCE). THE BRAKE LEVER PUTS A HIGH STRESS ON THE MOUN
- [SDR 96ZZZX5237](https://openairdocs.org/sdr/96ZZZX5237), Oct 4, 1996: FRAME. PITTED. A COMBINATION OF AN UNCORRECTED WATER LEAK AT A WINDOW AND DIRT HELD BETWEEN THE LONGERON/INTERIOR FABRIC RESULTED IN A BADLY PITTED LONGERON. SUBMITTER STATED 
- [SDR 96ZZZX5236](https://openairdocs.org/sdr/96ZZZX5236), Oct 4, 1996: TUBULAR FRAME. FATIGUE HOLE. MANUFACTURER USED A SMALL WELD DOT TO SNUB VIBRATION IN THE TOP OF THE LOWER FRONT DOOR CHANNEL. VIBRATION IN THE COWL WRAPPER/DOOR CHANNEL FATIGUED A .1250 INC

---
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.