Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Nov 1994)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.
THE PILOT'S INADEQUATE COMPENSATION FOR CROSSWIND. CROSSWIND CONDITIONS AND AN ICY RUNWAY SURFACE WERE FACTORS IN THE ACCIDENT.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC95LA013)
AFTER LOSS OF OIL PRESSURE THEN ENGINE FAILURE AT 2,800 FEET MSL, THE PILOT ELECTED TO MAKE AN EMERGENCY LANDING ALONG THE SHORE LINE. AFTER THE PILOT AND PASSENGERS EXITED THE AIRCRAFT, THE AIRPLANE SANK INTO 100 TO 150 FEET OF WATER. NEITHER THE AIRPLANE NOR THE ENGINE WAS RECOVERED.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC88LA106)
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 |
|---|---|---|---|
| 2023-05-16 | Reciprocating Engine Power Section | Mar 15, 2023 | Engine (IO-520-F) |
| 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-F)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.
CRACK IN FORWARD BULKHEAD OF HORIZONTAL STABILIZER, RIGHT HAND SIDE NEAR UPPER LIGHTNING HOLE. "REPLACED BULKHEAD WITH NEW BULKHEAD 1212136-14. SEE 337 DATED 1/23/25 FOR FURTHER DETAIL."
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND FLAP RIB AND SKIN CRACKS AT THE FORWARD NUTPLATE FOR THE INBOARD FLAP CONTROL BRACKET, STA 63.81. SUBMITTER RECOMMENDS CUTTING A 4.5 INCH DIAMETER ACCESS HOLE ON INBOARD SIDE OF RIB, REPAIRING RIB WITH A WELDED .032 INCH 4130 DOUBLER. THIS IS A COMMON PROBLEM ON THE 207 WITH ACTT 6,000 TO…
From FAA Service Difficulty Reports; matched by N-number and serial number.