# N1195X: 1975 Piper PA-28-151, registration cancelled 2010-11-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: November 2, 2010
- Exported to: Argentina
- Status when cancelled: Triennial form not returned
- Airframe: [Piper PA-28-151](https://openairdocs.org/model/piper-pa-28-151) (registry code 7102805)
- Engine: [Lycoming 0-320 series](https://openairdocs.org/engine/lycoming-0-320-series) (registry code 41508)
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS E-274](https://openairdocs.org/tcds/E-274) (OpenAirDocs)
- Serial number: 28-7515324
- Year built: 1975
- Type of aircraft: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal
- Airworthiness date: May 27, 1975
- Certificate issued: June 19, 1987
- Last registry action: June 17, 2008
- Mode S code: A050BF
- Owner when cancelled: [Remmers Aviation Inc](https://openairdocs.org/faa-owner/REMMERS%20AVIATION%20INC)
- Location: [Burlington, IA](https://openairdocs.org/faa-place/IA/Burlington)
- Owner type: Corporation
- Owner's area on the map: 40.8561° N, 91.1298° W: Placed by OpenAirDocs at the center of ZIP code 52601, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N1195X
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=1195X
- Page: https://openairdocs.org/deregistered/N1195X-2010-11-02

From the FAA registry file of November 5, 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-28-151: https://openairdocs.org/model/piper-pa-28-151.md

## Service difficulty reports (6)

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

- [SDR RMM2001F00000](https://openairdocs.org/sdr/RMM2001F00000), Oct 23, 2001: STRUT. CRACKED. DURING A SCHEDULED INSPECTION A CRACK WAS FOUND IN ONE LEFT GEAR LOWER TORQUE LINK ATTACHMENT EAR. THIS CONDITION HAS BEEN FOUND PREVIOUSLY OVERHAULED MID TO HI
- [SDR 20000817SH019](https://openairdocs.org/sdr/20000817SH019), Aug 9, 2000: CYLINDER. CRACKED. DURING OTHER MAINTENANCE TO LANDING GEAR, THE TORQUE LINKS WERE REMOVED AND UPPER STRUT CYLINDER CLEANED. CRACKS WERE FOUND AT THE BOTTOM OF THE MACHINED AREA F
- [SDR 20000821SH007](https://openairdocs.org/sdr/20000821SH007), Aug 4, 2000: CYLINDER. ELONGATED. ON SEVERAL OCCASIONS DURING INSPECTIONS, THE LT LANDING GEAR TO WING SPAR CAP LOWER BOLTS WAS FOUND BROKEN, USUALLY ONE BOLT. LESS FREQUENTLY, AN UPPER BOLT COU
- [SDR 96ZZZX3216](https://openairdocs.org/sdr/96ZZZX3216), May 8, 1996: SKIN. CRACKED. DURING NORMAL INSPECTION, CRACKS WERE FOUND IN STIFFENER CORRIGATION ENDS IN DOUBLER SKIN UNDER WING WALK. WING WALK WAS SOFT (SPRUNG DOWN) WHEN IT WAS STEPPED 
- [SDR 96ZZZX3215](https://openairdocs.org/sdr/96ZZZX3215), May 8, 1996: SKIN. CRACKED. DURING NORMAL INSPECTION, CRACKS WERE FOUND IN STIFFENER CORRIGATION ENDS IN DOUBLER SKIN UNDER WING WALK. WING WALK WAS SOFT (SPRUNG DOWN) WHEN IT WAS STEPPED 
- [SDR 96ZZZX199](https://openairdocs.org/sdr/96ZZZX199), Dec 15, 1995: TUBE. SEPARATED. ENGINE WAS ROUGH AT IDLE, AND WOULD SMOKE. IDLE ADJUSTMENT WOULD NOT HELP. CARBURETOR WAS DISASSEMBLED. THE IDLE TUBE WAS FOUND SEPARATED FROM THE THREADED PORT

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