# N409ER: 2002 Cessna 172S, registration cancelled 2009-03-04

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 4, 2009
- Status when cancelled: Triennial form not returned
- Airframe: [Cessna 172S](https://openairdocs.org/model/cessna-172s) (registry code 2072439)
- Engine: [Lycoming IO-360-L2A](https://openairdocs.org/engine/lycoming-io-360-l2a) (registry code 41597)
- Data sheets: [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 1E10](https://openairdocs.org/tcds/1E10) (OpenAirDocs)
- Serial number: 172S9158
- Year built: 2002
- Type of aircraft: Fixed wing single engine
- Engine type: Reciprocating
- Airworthiness: Standard, normal, utility
- Airworthiness date: September 10, 2002
- Certificate issued: July 14, 2004
- Last registry action: July 17, 2007
- Mode S code: A4CE84
- Owner when cancelled: [Cef 2002 Aircraft LLC](https://openairdocs.org/faa-owner/CEF%202002%20AIRCRAFT%20LLC)
- Location: [Danbury, CT](https://openairdocs.org/faa-place/CT/Danbury)
- Owner type: Corporation
- Owner's area on the map: 41.3778° N, 73.4575° W: Placed by OpenAirDocs at the center of ZIP code 06810, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N409ER
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=409ER
- Page: https://openairdocs.org/deregistered/N409ER-2009-03-04

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 Cessna 172S: https://openairdocs.org/model/cessna-172s.md

## Service difficulty reports (5)

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

- [SDR 2003FA0000416](https://openairdocs.org/sdr/2003FA0000416), Apr 21, 2003: FUEL CONTROL. INACCURATE. DURING PRE TAKEOFF CHECK, THE IDLE WAS TOO LOW TO CONTINUE. THIS ENGINE/FUEL CONTROL COMBINATION REQUIRES SUBSTANTIAL ADJUSTMENT TO MAINTAIN THE CORRECT IDLE.
- [SDR 2003FA0000415](https://openairdocs.org/sdr/2003FA0000415), Apr 21, 2003: SPINNER. CRACKED. PILOT WROTE UP MISSING SCREW. UPON EXAMINATION THE SPNNER AND BULKHEAD WERE FOUND CRACKED.
- [SDR 2003FA0000258](https://openairdocs.org/sdr/2003FA0000258), Feb 10, 2003: FLOW DIVIDER. STICKING. DURING CRUISE THE CREW REPORTED A ROUGH ENGINE. AFTER INSPECTING APPLICABLE SYSTEMS, THE FUEL FLOW DIVIDER WAS CHANGED AFTER HAVING BEEN FOUND STICKING INTERNAL
- [SDR 2003FA0000257](https://openairdocs.org/sdr/2003FA0000257), Feb 10, 2003: FLOW DIVIDER. STICKING. DURING CRUISE THE CREW REPORTED AROUGH ENGINE. AFTER INSPECTING APPLICABLE SYSTEMS, THE FUEL FLOW DIVIDER WAS CHANGED AFTER HAVING BEEN FOUND STICKING INTERNALL
- [SDR 2003FA0000256](https://openairdocs.org/sdr/2003FA0000256), Feb 10, 2003: FLOW DIVIDER. STICKING. DURING CRUISE THE CREW REPORTED AROUGH ENGINE. AFTER INSPECTING APPLICABLE SYSTEMS, THE FUEL FLOW DIVIDER WAS CHANGED AFTER HAVING BEEN FOUND STICKING INTERNALL

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