This N-number isn't registered right now. Below is its last known registration, canceled Jan 18, 2018.
Safety record in brief:1 NTSB accident (substantial damage, Jun 2008)2 ADs may apply3 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.
A total loss of engine power due to fuel exhaustion as a result of the flight instructor's inadequate preflight planning.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for NYC08LA199)
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 (172H) |
| 2011-06-02 | Cessna Aircraft Company (Cessna) Model 172 Airplanes Modified by Supplemental Type… | May 26, 2011 | Airframe (172H)Only with: Modified by STC SA01303WI (installation of TAE 125-01 or TAE 125-02-99 engine). |
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.
NR 3 CYLINDER CONNECTING ROD AND CAP FAILED AT THE CRANKSHAFT. CONNECTING ROD FELL TO BOTTOM OF CYLINDER BORE AND WAS REPEATEDLY STRUCK BY THE CRANKSHAFT UNTIL ENGINE WAS SHUT DOWN. THE FAILURE OCCURRED AFTER FINAL POWER REDUCTION DURING A ROUTINE LANDING. PILOT REPORTED HEARING A LOUD BANG…
From FAA Service Difficulty Reports; matched by N-number and serial number.NUMBER THREE CYLINDER CONNECTING ROD AND CAP FAILED AT CRANKSHAFT. THE CONNECTING ROD THEN FELL DOWN TO THE BOTTOM OF THE CYLINDER BORE AND WAS STRUCK REPEATEDLY BY THE CRANKSHAFT UNTIL ENGINE WAS SHUTDOWN. THE FAILURE OCCURRED AFTER FINAL POWER REDUCTION DURING A ROUTINE LANDING. THE PILOT…
From FAA Service Difficulty Reports; matched by N-number and serial number.ELEVATOR BELLCRANK BRACKET FOUND BROKEN IN NUMEROUS SPOTS WHERE IT ATTACHES TO FUSELAGE CROSS RIBS, STA 22 UNDER FLOORBOARD PANEL. DETERMINED POSSIBLE CAUSE AS NO GUSTLOCK INSTALLED DURING HIGH WINDS.
From FAA Service Difficulty Reports; matched by N-number and serial number.