This N-number isn't registered right now. Below is its last known registration, canceled Aug 27, 2002.
Safety record in brief:1 NTSB accident (substantial damage, May 2002)3 ADs may apply2 service difficulty reports
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.
Failure of the pilot to ensure the seat was set properly prior to engine start, and not using the parking brake when adjustment of seat was necessary, which resulted in the inadvertent deactivation of the brakes and subsequent collision with the fuel trucks.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for LAX02LA154)
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.
UPON INSPECTION OF AIRFRAME, DISCOVERED THAT LOWER RIGHT AFT VERTICAL STABILIZER ATTACH FITTING WAS CRACKED, AND LEFT HAND SIDE CORRODED. SUBMITTER STATED CAUSE APPEARS TO BE AGE RELATED.
From FAA Service Difficulty Reports; matched by N-number and serial number.UPON 100-HOUR INSPECTION TO DETERMINE APPLICABILITY TO AD 80-25-02 R2, NOTED THAT NR 4 CYLINDER INTAKE PUSH ROD P/N 73806T-T WHICH DOES NOT APPLY TO AD, WAS FOUND CRACKED AT END OF ALUMINUM TUBE THAT SWAGES ONTO BALL END OF PUSH ROD, TWO CRACKS WERE OBVIOUS VISUALLY. A FURTHER INSPECTION OF ALL…
From FAA Service Difficulty Reports; matched by N-number and serial number.