Safety record in brief:1 NTSB accident (substantial damage, Jun 1993)1 AD may apply1 service difficulty report
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-IN-COMMAND WAS OPERATING THE AIRPLANE AT AN EXCESSIVE TAXI SPEED, AND DID NOT MAINTAIN VISUAL SEPARATION WITH THE TIED DOWN AIRPLANE. FACTORS CONTRIBUTING TO THE ACCIDENT WERE A LIGHT RAIN AND FOG CONDITION, AND A FOGGY INTERIOR WINDOW.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI93LA188)
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 |
|---|---|---|---|
| 99-05-13 | Raytheon Aircraft Company 17, 18, 19, 23, 24, 33, 35, 36/A36, A36TC/B36TC, 45, 50, 55… | Apr 19, 1999 | Airframe (C23)Certain serial numbers: F33A CE-290–CE-1791; E33C CJ-26–CJ-179; F33C CJ-26–CJ-179; A36 E-185–E-3046; B36TC EA-242–EA-591; 58 TH-1–TH-1798 |
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 STABILATOR MAIN SPAR ADJACENT TO FUSELAGE HINGE ATTACH FITTINGS AIRCRAFT USED FOR FLIGHT TRAINING. CRACK DUE TO FATIGUE. SUBMITTER RECOMMENDED DETAILED INSPECTION OF THIS AREA AT EACH INSPECTION INTERVAL.
From FAA Service Difficulty Reports; matched by N-number and serial number.