# Accident 20040616010149A: Amtr CB1, Nampa, ID, June 16, 2004

- Type: FAA accident report (Accident/Incident Data System), as reported
- Date: June 16, 2004, 12:40 local time
- Place: Nampa, ID
- Airport: Nampa Municipal Airport
- Damage: Substantial damage
- Phase of flight: Level Off Touchdown
- Operating rules: General operating rules (Part 91)
- Location: 43.5813° N, 116.5231° W: Placed by OpenAirDocs at NAMPA MUNI (MAN), within about a mile (OpenAirDocs)
- Nearby events: https://openairdocs.org/map.md?lat=43.5813&lon=-116.5231&mi=10
- Aircraft: N26WF, a cancelled registration (https://openairdocs.org/deregistered/N26WF-2005-03-22) (OpenAirDocs)
- Registry model: Fetherolf Will CB-1 (registry code 05606K4, https://openairdocs.org/model/fetherolf-will-cb-1) (OpenAirDocs)
- Registry engine: Lycoming 0-290 series (registry code 41506, https://openairdocs.org/engine/lycoming-0-290-series) (OpenAirDocs)
- Reported make and model: AMTR CB1
- People aboard: 1
- Fatal injuries: 0
- Pilot flight hours: 155 total, 39 in this make and model, 4 in the last 90 days
- FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/)
- Page: https://openairdocs.org/incident/20040616010149A

## Narrative

As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^.

(-23) PILOT STATED THAT HE DEPARTED RWY 29, NAMPA, FLEW LEFT PATTERN AND ATTEMPTED TO LAND RWY 29. HE STATED THAT AIRCRAFT FLOATED EXCESSIVELY AT APPROXIMATELY 5' AGL, THEN SUDDENLY DROPPED AND BOUNCED. AT THIS POINT HE STATED THAT HE ADDED FULL POWER, BUT THE AIRCRAFT CONTINUED TO DEPART THE LEFT SIDE OF THE RUNWAY. HIS RECOLLECTION OF EVENTS AFTER THIS POINT WERE NOT CLEAR. INVESTIGATION OF GROUND SCARS INDICATED THE AIRCRAFT DEPARTED THE LEFT SIDE OF RWY 29 APPROXIMATELY 2000' FROM THE APPROACH THRESHOLD. THE AIRCRAFT CONTINUED A GRADUAL DEPARTURE OF THE RUNWAY WITH ONLY THE LEFT GEAR CONTAING THE GROUND. THE RIGHT GEAR DESTROYED A RUNWAY LIGHT, THEN THE LEFT GEAR AND LOWER WING IMPACTED A SMALL EARTHEN BERM, WATER SYSTEM CONTROL VALVE, AND FENCE POST. PORTIONS OF THE LEFT MLG TUBULAR STRUCTURE AND WHEEL PANT DEPARTED THE AIRCRAFT AT THIS POINT. THE AIRCRAFT BECAME AIRBORNE AGAIN FOR APPROXIMATELY 40', AT WHICH POINT IT APPEARS THE AIRCRAFT IMPACTED THE GROUND AND CONTINUED TO SKID SIDEWAYS UNTIL COMING TO REST IN AN UPRIGHT POSITION AT AN APPROXIMATE HEADING OF 120 DEGREES. DAMAGE TO THE AIRCRAFT WAS SUBSTANTIAL.

## NTSB investigation

None matched to this report by aircraft and date. Search the NTSB's own records: https://data.ntsb.gov/carol-main-public/basic-search

## Other reports on N26WF (1)

Matched to the same aircraft by N-number and date.

- [Accident 20011102029929A](https://openairdocs.org/incident/20011102029929A), Nov 2, 2001: N26WF, Ontario, OR, No damage. (-23) Aircraft was built by pilot as a homebuilt kit. On landing, a weld on the landing gear broke and the right wheel detached from the frame. This caused the…

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. For accidents, the NTSB's own investigation is the fuller record.

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