Safety record in brief:1 NTSB accident (substantial damage, Sep 1995)1 AD may apply2 service difficulty reports
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THE LOSS OF ENGINE POWER FOR UNDETERMINED REASONS. FACTORS WERE THE PILOT'S INABILITY TO INITIATE A FLARE DUE TO THE FRACTURE OF THE YOKE ASSEMBLY, AND THE LACK OF SUITABLE TERRAIN FOR THE FORCED LANDING.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW95LA391)
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 (172D) |
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.
AFTER 40 MINUTES OF CRUISE FLIGHT TO 3,000 FEET MSL, THE ENGINE LOST POWER. ABOUT 80 FEET ABOVE THE GROUND, ON SHORT FINAL TO A HAY FIELD, THE CONTROL WHEEL BROKE. THE PILOT GRABBED THE CONTROL WHEEL TUBE AND STARTED TO FLARE FOR LANDING WHEN THE AIRCAFT STRUCT THE GROUND IN A NOSE-LOW ATTITUDE.…
From FAA Service Difficulty Reports; matched by N-number and serial number.AFTER 40 MINUTES OF CRUISE FLIGHT TO 3,000 FEET MSL, THE ENGINE LOST POWER. ABOUT 80 FEET ABOVE THE GROUND, ON SHORT FINAL TO A HAY FIELD, THE CONTROL WHEEL BROKE. THE PILOT GRABBED THE CONTROL WHEEL TUBE AND STARTED TO FLARE FOR LANDING WHEN THE AIRCAFT STRUCT THE GROUND IN A NOSE-LOW ATTITUDE.…
From FAA Service Difficulty Reports; matched by N-number and serial number.