DFW05CA050

NTSB accident investigation · Reinhart GP-4 · Fort Worth, TX · January 9, 2005

Accident · No injuriesData collectionFinal report
Date
January 9, 2005, 12:30 local (18:30 UTC)
Place
Fort Worth, TX
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N233CRReinhart GP-4
Weather
Visual (VMC) · Day
Status
Completed · report March 30, 2005
Report
Approved by Office Director
Parties
Fort Worth FSDO
FAA report
20050109033959A
Case key
60823

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 failure to compensate for the prevailing crosswind. A contributing factor was the crosswind.

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.

Loss of control - on ground/waterLanding - roll
Compensation for wind conditions - inadequatePilot in commandCause
Weather condition - crosswindFactor
Gear collapsedLanding - roll

Analysis

The 742-hour private pilot reported that during his departure from runway 17, the wind was from approximately 200 degrees at 10 knots. When he returned about an hour later, the wind had shifted to approximately 250-260 degrees at 15-20 knots with gusts. The pilot made two attempts at a crosswind landing on runway 17, each time striking a runway light with the airplane and initiating a go-around. The pilot reported that the right flap was damaged during the first attempt, and the landing gear retract link was damaged during the second landing attempt. During the third landing attempt, the pilot "used a forward slip technique to land, then kicked the nose around, and made what appeared to be a good landing." The left main landing gear then collapsed. The pilot reported that he held "hard right aileron to keep the left wing up as the airplane slid off to the left side of the runway." The airplane continued down into a ravine, and the propeller dug into the ground as the airplane made a 180-degree turn and came to rest upright.

Factual narrative

On January 9, 2005, approximately 1230 central standard time, a home-built Reinhart GP-4 single-engine airplane, N233CR, sustained substantial damage following a loss of control during landing at the Bourland Field Airport (50F), near Fort Worth, Texas. The private pilot, sole occupant and owner of the airplane, was not injured. Visual meteorological conditions prevailed, and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The local flight originated from 50F, approximately 1130.

In a written statement, the 742-hour private pilot reported that during his departure from 50F, the wind was from approximately 200 degrees at 10 knots. When he returned about an hour later, the wind had shifted to approximately 250-260 degrees at 15-20 knots with gusts. The pilot made two attempts at a crosswind landing on runway 17, each time striking a runway light with the airplane and initiating a go-around. The pilot reported that the right flap was damaged during the first attempt, and the landing gear retract link was damaged during the second landing attempt.

During the third landing attempt, the pilot "used a forward slip technique to land, then kicked the nose around, and made what appeared to be a good landing," but the left main landing gear collapsed, and the pilot "held hard right aileron to keep the left wing up as the airplane slid off to the left side of the runway." The airplane continued down into a ravine, and the propeller dug into the ground as the airplane made a 180-degree turn and came to rest upright.

According to the pilot and Federal Aviation Administration (FAA) inspector who responded to the accident site, aircraft hangars were located on the northwest corner of the field, adjacent to the departure end of runway 17. The pilot reported that turbulence was created by the wind contacting these hangars.

The FAA inspector reported structural damage to the spar of the horizontal stabilizer and damage to the right flap. All three of the landing gear collapsed, and there were holes in the engine cowling and fuselage of the airplane.

At 1225, the automated weather observing system at the Granbury Municipal Airport (GDJ), near Granbury, Texas, located approximately 14 nautical miles southwest of the accident site, reported wind from 200 degrees at 15 knots, clear skies, 10 statute miles visibility, temperature 70 degrees Fahrenheit, dew point 54 degrees Fahrenheit, and an barometric pressure setting of 30.22 inches of Mercury.

Aircraft

Registration
N233CR
Reported as
Reinhart GP-4
Category
Airplane, amateur-built
Serial number
001
Airframe hours
47.9
Engine
Lycoming IO-360-AIB6D, 200 lbs thrust, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Angeleno Aviation, LLC
Airworthiness certificate
Special, Experimental (Special)
Last inspection
100 hour · August 4, 2004 · 19.4 hours before
Departed
50F · Fort Worth, TX
Airport
50F · Bourland Field Airport, runway 17, 4,092 × 60 ft, asphalt

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
60
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land, Multi-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Last flight review
January 17, 2003
Seat
Left
Flight hours
742 total · 63 in this make and model · 14 in the last 90 days · 4 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
200° at 15 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
70 °F, dew point 54 °F
Altimeter
30.21 inHg
Observed at
GDJ, 14 nm away

FAA reports on this event · 1

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