FTW97LA201

NTSB accident investigation · Centrair 101C · Santa Fe, NM · May 25, 1997

Accident · No injuriesLimited investigationFinal report
Date
May 25, 1997, 14:00 local (20:00 UTC)
Place
Santa Fe, NM
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N991JBCentrair 101C
Weather
Visual (VMC) · Day
Status
Completed · report December 15, 1997
Report
Approved by Office Director
FAA report
19970525012909A
Case key
20227

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

the pilot's improper planning/decison. Factors relating to the accident were: lack of thermal lift, which resulted in an off-airport landing, and the lack of suitable terrain for the landing.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Miscellaneous/otherCruise
Weather condition - no thermal liftFactor
On ground/water collision with objectLanding
Planning/decision - improperPilot in commandCause
Terrain condition - none suitableFactor
Terrain condition - roadway/highway
Object - wall/barricadeFactor

Analysis

Initially, strong thermal conditions prevailed on the proposed 500 km cross-country glider flight; however, conditions began to weaken, and the pilot amended his destination twice. The conditions continued to deteriorate, and when the glider reached an altitude of 1,500 feet agl, the pilot determined that an off-airport landing was inevitable. He selected a highway as the only available landing area due to numerous trees in the surrounding terrain. The glider touched down, and during rolled-out, the wings settled onto the highway guardrails. At a speed of about 10 mph, the glider's nose turned left, and the fuselage contacted the left guardrail.

Factual narrative

On May 25, 1997, about 1400 mountain daylight time, a Centrair 101C glider, N991JB, was substantially damaged when it collided with a guardrail during a forced landing on a highway approximately 21 miles southeast of Santa Fe, New Mexico. The private pilot, sole occupant of the glider, was not injured. The glider was registered to and operated by the pilot under Title 14 CFR Part 91. Visual meteorological conditions prevailed and no flight plan was filed for the personal flight that originated from Moriarty, New Mexico, about 1230.

In a written statement, the pilot reported that he planned a 500 km trip to Colorado. Initially, the flight encountered thermal conditions in the Moriarty area that were "extremely strong, showing thermal strength in the range from 1000 to 1500 feet per minute." However, upon reaching a point approximately 30 miles north of Moriarty, the pilot "noticed a considerable weakening of conditions" and decided to make his destination the Santa Fe County Municipal Airport in Santa Fe, New Mexico, located "about 20 miles away."

The pilot "attempted several times to penetrate towards" Santa Fe, but "encountered strong sink" each time. While making these attempts, the glider was "blown east" by westerly winds. Thermal "conditions to the east looked acceptable" to the pilot, and he elected to "have the wind drift" the glider towards the Las Vegas Municipal Airport in Las Vegas, New Mexico, located "[approximately] 40 miles east."

As the glider drifted east, the pilot "noticed that the average lift was gradually decreasing and the top of the lift was slowly coming down." As he "fought the deteriorating conditions," the pilot "looked for suitable land out areas." When the glider reached an altitude of 1,500 feet agl, the pilot "decided that a land-out might be inevitable" and began planning an approach to land on the southbound lanes of Interstate 25. According to the pilot, he selected the highway as the only available landing area due to numerous trees in the surrounding terrain. The glider touched down in a gap in traffic and "settled with both wings on the guardrails sliding forward." At a speed of "about 10 mph," the nose of the glider turned left, and the "fuselage slid slowly into the left guard rail."

The FAA inspector who examined the glider reported that a crack midway between the canopy and the empennage extended around 3/4 of the fuselage's circumference, and the trailing edge of the left wing was delaminated.

Aircraft

Registration
N991JB
Reported as
Centrair 101C
Category
Glider
Serial number
101901
Airframe hours
1,035
Engine
unknown
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Egbert Kahl
Airworthiness certificate
Special, Experimental (Special)
Departed
0E0 · Moriarty, NM
Destination
LVS · Las Vegas, NM

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
48
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Center
Flight hours
323 total · 200 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
270° at 20 knots, gusting 25
Visibility
10 statute miles
Lowest ceiling
4,000 ft broken
Temperature
75 °F

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N991JB · 1

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