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Accidents · NTSB DEN06LA058 · Final report

Amateur-built NXT accident near Glenwood, New Mexico, April 11, 2006

On April 11, 2006 at about 4:00 pm local time, a amateur-built NXT, registered N42XT, was substantially damaged in an accident near Glenwood, New Mexico (Glenwood-Catron County airport). It was a personal flight 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 the partial failure of the crankcase nose seal for undetermined reasons. A contributing factor was the pilot's diminished visibility during the forced landing due to oil on the windscreen, resulting in a runway excursion and subsequent impact with rocks and terrain.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
April 11, 2006 · about 4:00 pm local time
Place
Glenwood, New Mexico · Glenwood-Catron County · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
Amateur-built NXT
Registration
N42XT · registry record · serial 004
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

While cruising at an airspeed of 300 knots at an altitude of 12,500 feet, the airplane "hit a pocket of wind shear." Shortly thereafter, the pilot noticed smoke entering the cockpit. When the pilot noticed an increase in engine oil temperature, he reduced the engine power. The pilot attempted to locate an area to execute a forced landing and declared a "mayday" to air traffic control. In an attempt to reduce the smoke continuing to enter the cockpit, the pilot shut down the engine, and feathered the propeller. The smoke in the cockpit dissipated, and the pilot attempted a forced landing to a dirt runway. Due to oil on the windshield, the pilot's visibility was reduced during the approach and landing. During the landing, the airplane departed the dirt runway surface and impacted rocks and terrain. Examination of the engine revealed that the crankshaft oil seal was partially extruded at the six o'clock position. No additional anomalies were noted with the engine that would have precluded engine operation. The aircraft was equipped with a Christen air/oil separator. No evidence of improper installation was noted, and all of the lines were secure at their respective fittings. The separator was removed and the ball check valve within the separator was free to move and no obstructions were noted. An alternate warm air source (whistle slot) was located in the crankcase vent line and mounted on the left side of the firewall. The oil breather tube exited the airframe on the lower left side of the fuselage.

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: commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 90 in this make and model; 50 in the last 90 days; 20 in the last 30 days
  • Last flight review: August 1, 2004
  • Medical certificate: Class 2 (without waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 90 hours
  • Last inspection: annual inspection, September 1, 2005; 90 hours since
  • Maximum gross weight: 2,600 lb
  • Seats: 2
  • Landing gear: retractable
  • Engine: Lycoming TIO-540-X186 (piston); 0 hours total

The flight

  • Departed from: LRU Las Cruces NM at 3:30 pm
  • Destination: PMD Palmdale CA
  • Flight plan: VFR
  • Runway 1, 3,700 ft by 84 ft

Weather at the time

  • Light: daylight
  • Wind: from 310° at 20 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 61°F (16°C), dew point 0°F (-18°C)

Injuries

FatalSeriousMinorNone
Crew1

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.