Safety record in brief:2 NTSB accidents (destroyed damage at worst, latest Apr 1994)2 ADs may apply
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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 FAILURE TO MAINTAIN ROTOR SPEED, DELAY OF THE FLARE, AND THE IMPROPER TOUCHDOWN. A FACTOR WAS THE LOSS OF ENGINE POWER FOR UNDETERMINED REASONS.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for FTW94LA125)
THE PLT REPORTED NOTICING THE FUEL GAGE WAS NEARING EMPTY SHORTLY BEFORE THE ENG QUIT. THE ACFT CRASHED DURING AN ATTEMPTED FORCED LANDING ON A ROAD. THE PLT STATED HE WAS FLYING THE ACFT TO HIS RESIDENCE WHERE IT WAS BASED. INVESTIGATION REVEALED LITTLE FUEL REMAINED WITHIN THE FUEL SYSTEM AND NO SIGNS OF FUEL LEAKAGE DURING THE ACCIDENT.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for SEA86FA139)
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 |
|---|---|---|---|
| 97-20-15 | Hiller Aircraft Corporation Model UH- 12A, UH-12B, UH-12C, UH-12D, and UH-12E Helicopters | Nov 12, 1997 | Airframe (UH-12B) |
| 97-10-16 | Hiller Aircraft Corporation Model UH- 12, UH-12A, UH-12B, UH-12C, UH-12D, UH-12E… | Jun 27, 1997 | Airframe (UH-12B)Only with: Having control rotor blade spar tube P/N 36003, 36006, 36129, 36129-25, 36203, 36203-15, 36203-21, or 36209-3, or cuff P/N 36101-1, 36101-4, 36108, 36115-1, 36115-4, 36115-6, 36115-8, or 36124 installed; includes UH-12D and UH-12E converted to turbine power per STC SH177WE and SH178WE. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
No Service Difficulty Reports found for this airframe since 1995.