This N-number isn't registered right now. Below is its last known registration, canceled Aug 27, 2018.
Safety record in brief:3 NTSB accidents (substantial damage at worst, latest Aug 2008)2 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.
The pilot of the other airplane's excessive taxi speed while taxiing to the runway, and his failure to see the stopped airplane ahead of him in time to avoid a collision.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC08LA106)
The pilot's failure to maintain control of the airplane during the landing flare/touchdown.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC08CA036)
The pilot's inadequate compensation for the wind conditions, and an inadvertent stall. A factor in the accident was the presence of a tail wind.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC98LA150)
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 (207A) |
| 2009-16-03 | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating… | Sep 9, 2009 | Engine (IO 520 SERIES)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed. |
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.
PILOT REPORTS SUCTION READING NIL. REMOVED VACUUM PUMP & SHAFT WAS SHEARED.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING ANNUAL INSPECTION, OIL STREAK DISCOVERED ON AFT HALF OF PROPELLER HUB CASTING. A DYE PENETRANT INSPECTION PERFORMED AND REVEALED HUB TO BE CRACKED. CRACK WAS APPROXIMATELY 1.50 INCHES LONG HAIR LINE. AWAITING TEAR-DOWN REPORT FROM OVERHAUL SHOP. (X)
From FAA Service Difficulty Reports; matched by N-number and serial number.