This N-number isn't registered right now. Below is its last known registration, canceled Jul 17, 2020.
Safety record in brief:1 NTSB accident (substantial damage, Dec 2017)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 flight instructor’s inadequate preflight inspection, during which he failed to ensure that water was sufficiently drained from the fuel system, which resulted in total loss of engine power and a subsequent forced landing and impact with objects.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for WPR18LA042)
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 |
|---|---|---|---|
| 2009-10-09 R2 | Rudder Control System | Sep 12, 2011 | Airframe (152)Certain serial numbers: 150F 15061533–15064532; 150G 15064533–15064969; 150G 15064971–15067198; 150H 15067199–15069308; 150H 649; 150J 15069309–15071128; …. Only with: FA150L S/N FA1500121-FA1500261 and FA150M S/N FA1500262-FA1500336 only when equipped with FKA150-2311 and FKA150-2316. |
| 2011-10-09 | Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190… | Jun 17, 2011 | Airframe (152) |
| 2008-22-18 | Cessna Aircraft Company 150 Series Airplanes | Dec 9, 2008 | Airframe (152)Only with: BRS-150 Parachute System with serial number 50001 through 50006 installed via STC SA64CH. |
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.
DURING ROUTINE 100 HR INSPECTION, MINOR CORROSION WS FOUND ON BOTH LEFT AND RIGHT VERTICAL STABILIZER ATTACH FITTINGS, APPROX BS 200.4. UPON REMOVAL OF CORROSION, A CRACK WS FOUND IN THE RADIUS OF THE RIGHT FITTING APPROXIMENTLY .7500 OF THE WAY ACROSS AND APPROX .50 PERCENT OF THE THICKNESS DEEP.…
From FAA Service Difficulty Reports; matched by N-number and serial number.