This N-number isn't registered right now. Below is its last known registration, canceled Feb 20, 2004.
Safety record in brief:1 NTSB accident (substantial damage, Nov 2003)3 ADs may apply4 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.
the pilot's failure to maintain adequate airspeed which resulted in an inadvertent stall.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW04LA020)
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.
PROBLEM WITH HIGH OIL TEMP ON TEST FLIGHT. AT 280.3 OIL CONSUMPTION INCREASED AND ENG STARTED RUNNING ROUGH, WHEN CHECKING SPARK PLUGS FOUND OIL ON NR 3 CYL PLUG. REMOVED NR 3 CYLINDER FOUND OIL CONTROL RING BROKEN, METAL IN OIL SYS. ON 12/27/02 REPLACED ALL 4 CYLINDERS AND CONNECTING ROD ASSY.…
From FAA Service Difficulty Reports; matched by N-number and serial number.A CRACK WAS FOUND IN THE HUB AREA. CRACK RADIATED FROM INSIDE THE HUB THROUGH THE FACE OF THE HUB TO THE MOUNTING SURFACE ENDING IN THE BOLT HOLE ADJACENT TO THE NR 1 BLADE. COMPLIANCE WITH MCCAULEY SB 169C AND AD 89-26-10 WAS ACCOMPLISHED AT 3229.7 TOTAL HOURS WHERE NO DEFECTS WERE FOUND. A…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING COMPLIANCE WITH SEB 95-3, THE RIB ASSY FLAP SUPPORT ARMS, PN 0523901-13 LT, OR PN 0523901-14 RT, FOUND WEAR GROOVES WHICH EXCEED THE MAXIMUM DEPTH OF 0.020 INCH. AT LEAST ONE OR BOTH ARMS WORN BEYOND LIMIT.
From FAA Service Difficulty Reports; matched by N-number and serial number.PROPELLER TOTAL TIME: 5815.0. A CRACK WAS FOUND IN THE HUB AREA. CRACK RADIATED FROM INSIDE THE HUB THROUGH THE FACE OF THE HUB TO THE MOUNTING SURFACE ENDING IN THE BOLT HOLE ADJACENT TO THE NR 1 BLADE. COMPLIANCE WITH MCCAULEY SB 169C AND AD 89-26-10 WAS ACCOMPLISHED AT 3229.7 TOTAL WHERE NO…
From FAA Service Difficulty Reports; matched by N-number and serial number.