Safety record in brief:1 NTSB accident (substantial damage, Sep 2021)6 ADs may apply
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The pilot’s failure to maintain control of the helicopter during an out-of-ground effect hover in a gusty wind, due to loss of tail rotor effectiveness.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA21LA357)
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 |
|---|---|---|---|
| 2018-02-01 | The Enstrom Helicopter Corporation Helicopters | Feb 21, 2018 | Airframe (F-28C)Certain serial numbers: 480 5001–5006. Only with: With main rotor spindle P/N 28-14282-11 or 28-14282-13 installed. |
| 2017-26-03 | The Enstrom Helicopter Corporation Helicopters | Jan 4, 2018 | Airframe (F-28C)Only with: Rod end bearing assembly P/N 01-824-08E-011, 09455-01-824-08E-011, ECD091-1, ASMK8T, M81935/1-08K, MS21242S8K, or MTK8 installed. |
| 2012-11-05 | Enstrom Helicopter Corporation Helicopters | Jul 3, 2012 | Airframe (F-28C)Only with: Helicopters with trim relay P/N KUP14D55-24, KUP14D55-472, M83536/10-015M, or M83536/10-024M installed; does not apply to helicopters with reversible trim motor P/N 28-16621 or P/N AD1R-10. |
| 2011-26-10 | Enstrom Helicopter Corporation Helicopters | Jan 23, 2012 | Airframe (F-28C)Only with: Helicopters with a trim relay P/N KUP14D55-472, M83536/10-015M, or M83536/10-024M installed; does not apply to helicopters with reversible trim motor P/N 28-16621 or AD1R-10. |
| 2002-08-03 | Enstrom Helicopter Corporation Model F-28, F-28A, F-28C, F-28F, 280, 280C, 280F, and… | May 2, 2002 | Airframe (F-28C) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 96-06-03 | The Enstrom Helicopter Corporation Model F-28, F-28A, F-28C, F-28C-2, F-28F, 280, 280C… | Mar 19, 1996 | Airframe (F-28C) |
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.