This N-number isn't registered right now. Below is its last known registration, canceled Aug 30, 2004.
Safety record in brief:3 NTSB accidents (substantial damage at worst, latest Nov 1993)2 ADs may apply
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 fatigue failure of the torsion-tension bar pin due to fretting corrosion. A factor in this accident was an inadequate quality of material utilized in the manufacture of the pin.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX94LA054)
WHILE CRUISING DURING AN AG FLIGHT THE ACFT'S ENG BEGAN LOSING PWR. AT THE TIME THE ACFT WAS ABOUT 50 FT AGL & WAS TRAVELLING AT 50 MPH. THE PLT MADE A FORCED LDG ONTO A NEARBY PLOWED FLD. UPON TOUCHDOWN THE RT SKID DUG INTO A FURROW & THE ACFT ROLLED OVER. EXAM OF THE ACFT REVEALED THAT AN AIR LEAK HAD DEVELOPED AT THE FUEL FEED LINE INLET TO THE ELECTRIC BOOST PUMP. THE CONNECTOR INLET BUSHING…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX85LA305)
THE ACFT COLLIDED WITH TERRAIN WHILE ON AN AERIAL APPLICATION FLT. THE PLT STATED HE, 'HEARD A LOUD BANG' WHILE SPRAYING. THEN THE 'NOSE OF THE HELICOPTER DOVE RADICALLY DOWN', AND HE CRASHED INTO THE FIELD. EXAMINATION OF THE SITE REVEALED THAT ONE OF THE SPRAY BOOM EXTENSION WAS FOUND ABOUT 50 YDS FROM THE CRASH LOCATION. COTTON PLANT STALKS WERE ENTWINED ABOUT THE TIP OF THE BOOM & IN ITS…
From NTSB records; matched by serial number.Read NTSB report (search CAROL for LAX85LA002)
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-12E) |
| 97-10-16 | Hiller Aircraft Corporation Model UH- 12, UH-12A, UH-12B, UH-12C, UH-12D, UH-12E… | Jun 27, 1997 | Airframe (UH-12E)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.