This N-number isn't registered right now. Below is its last known registration, canceled May 8, 2007.
Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Aug 2005)3 ADs may apply1 service difficulty report
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
the loss of engine power for reasons undetermined. Contributing factors include the lack of suitable terrain for a forced landing, and the soft dirt.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DEN05LA127)
the pilot's in-flight decision/planning which resulted in fuel exhaustion. The fence and night conditions were contributing factors.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DEN04LA045)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (172N) |
| 2011-06-02 | Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type… | May 26, 2011 | Airframe (172N)Only with: Modified by STC SA01303WI (installation of TAE 125-01 or TAE 125-02-99 engine). |
| 2001-23-03 | Cessna Aircraft Company Models 172N, 172P, R172K, 172RG, F172N, F172P, FR172J, and… | Dec 27, 2001 | Airframe (172N)Certain serial numbers: 172N 17267585–17270049; 172N 17270051–17274009; 172N 17261445; 172N 17261578; 172N 17270050; 172P 17274010–17276654; … |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
ENGINE STOPPAGE DUE TO ABNORMALLY HIGH WEAR TO THE LIFTING BLOCKS OF THE CONTACT POINTS OF BOTH THE LT AND RT SIDES OF A COMMON MAGNETO. BOTH CONTACT POINTS WERE REMOVED AND INSPECTED FOR BOGUS PARTS; REINSTALLED, LUBRICATED, RE-GAPPED AND TIMED. THE AIRCRAFT WAS RETURNED TO SERVICE AFTER GROUND…
From FAA Service Difficulty Reports; matched by N-number and serial number.