Amateur-built CAPELLA XS accident near Leander, Texas, November 8, 1997
On November 8, 1997 at about 10:00 pm local time, a amateur-built CAPELLA XS, registered N89FW, was substantially damaged in an accident near Leander, Texas (Kitty Hill airport). It was a flight of an unrecorded kind under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
The loss of engine power due to an undetermined reason. A factor was the lack of suitable terrain for the forced landing.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- November 8, 1997 · about 10:00 pm local time
- Place
- Leander, Texas · Kitty Hill · map
- Type
- Accident
- Injuries
- No one was hurt; 1 person was on board or involved.
- Weather
- visual conditions (good weather)
- Aircraft
- Amateur-built CAPELLA XS
- Registration
- N89FW · no longer on the register · serial FW2C651
- Damage
- Substantial damage
- Flight
- Flight of an unrecorded kind · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The pilot initiated a forced landing to a field, following a loss of engine power, at the downwind-to-base leg position for the runway. During the landing flare, the airplane struck a fence. The owner reported that the fuel system and ignition system operated properly; however, upon disassembly of the cylinders, the rear cylinder exhibited scoring, evidence of overheating, and a seized piston ring. The owner reported sending the components for inspection by a Rotex authorized technician; who, according to the owner confirmed that the engine had seized and that the oil injector was the cause. The person to whom the engine was sent for examination stated that he 'did not confirm that the oil injector was the cause.' He further stated that a differential air flow to the engine, an improper fuel air ratio, an improper fuel oil mixture, and/or overheating could have contributed to the loss of engine power. This is not a certified aircraft engine and conforms to no aircraft standards. It is for use in experimental, uncertificated aircraft and vehicles only in which an engine failure will not compromise safety.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
Pilot
- Certificate: private
- Ratings: single-engine land
- Flight time: 1,400 hours in all; 10 in this make and model
- Medical certificate: Class 3 (valid medical--w/ waivers/lim.)
- Seat: left
The aircraft
- Airframe total time: 56 hours
- Last inspection: annual inspection, June 28, 1997; 10 hours since
- Maximum gross weight: 950 lb
- Seats: 2
- Landing gear: fixed
- Engine: Rotax 582-66 (piston); 0 hours total
The flight
- Departed from: 77T at 8:00 pm
- Flight plan: none
- Runway 17, 2,350 ft by 60 ft
Weather at the time
- Light: daylight
- Wind: from 170° at 5 knots
- Visibility: 10 statute miles
- Sky: clear
- Temperature: 75°F (24°C), dew point 0°F (-18°C)
- Altimeter: 29.00 inHg
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
