Accident · substantial damage
Aug 15, 2007 · Coeur D'Alene, IDthe instructor's misjudged landing flare.
- Damage
- Substantial
- Injuries
- None
- Report
- LAX07CA251
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX07CA251)
Safety record in brief:1 NTSB accident (substantial damage, Aug 2007)2 ADs may apply2 service difficulty reports
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the instructor's misjudged landing flare.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX07CA251)
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 (R182) |
| 2008-10-02 | Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series… | May 12, 2008 | Airframe (R182)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007. |
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.
RECENTLY INSTALLED ELECTROAIR ELECTRONIC IGNITION SYSTEM EIS-61000-5M AND EIS-61000-5C. WHILE TROUBLE SHOOTING ERRONEOUS RPM INDICATIONS WE OPENED THE COVER OF THE MAGNETO TIMING HOUSING (MTH) AND FOUND SIGNIFICANT SHAVINGS IN THE CASE. BORESCOPE INSPECTION SHOWED DAMAGE TO BOTH PLASTIC GEARS…
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACK IN WIRING HARNESS CUTOUT IN BULKHEAD AT STA 124, DUE TO IMPROPER REINFORCEMENT OF BULKHEAD AND FUSELAGE FLEXING IN FLIGHT. RECOMMEND REMANFACTURE OF BULKHEAD WITH THICKER MATERIAL TO WITHSTAND IN-FLIGHT STRESS OR ENSURE THAT BULKHEAD IS PROPERLY SUPPORTED TO PREVENT FLEXING OR CHANGE THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.