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DFW05CA001

2004-10-09 · Hearne, Texas, United States · Minor · 1 aircraft · Status: Completed

Airport LHB

Current FAA registration · N5529K

Make / Model
BELLANCA 7ECA
Year of manufacture
1978 · 26 years old at event
Engine
LYCOMING 0-235 SERIES (115 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19780517
ADS-B equipped
Yes — Mode-S A70A76

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The excessive taxi speed by the pilot in command resulting in the pilot's loss of control. A contributing factor was the quartering tailwind.

Factual narrative

On October 9, 2004, approximately 1100 central daylight time, a Bellanca 7ECA tail-wheel equipped airplane, N5529K, was substantially damaged when it collided with a bail of hay at the Hearne Municipal Airport (LHB) near Hearne, Texas. The commercial pilot was not injured, and one passenger sustained minor injuries. The single-engine airplane was owned and operated by Tailwinds Aviation of Grand Prairie, Texas. Instrument meteorological conditions prevailed, and a flight plan was not filed for the personal flight conducted under 14 Code of Federal Regulations Part 91. In a telephone interview with an NTSB representative, the 420-hour pilot reported that he made a 180-degree turn after landing on runway 36 at LHB, and was taxiing to the main ramp at a speed of approximately 30 knots with an 8-knot quartering tailwind. When the ramp was approximately 500-600 feet ahead, the pilot decreased power, and the airplane began to veer off to the left. Subsequently, the pilot applied right rudder and tapped on the left brake. When the airplane continued to veer to the left, the pilot pulled the stick toward himself to force the tail wheel on to the ground. The pilot then applied pressure to both brakes and reported that they were not effective. The airplane collided with a bail of hay approximately 200 feet to the left of the runway. Upon impact, the airplane nosed over and came to rest in an inverted position. Examination of the airplane by an NTSB representative revealed that the rudder and left wing brace were structurally damaged. Additionally, the propeller assembly was detached from the aircraft. On October 14, 2004, a representative from the NTSB performed an examination of the brake system and found that the brake fluid lines were empty of fluid; however, the airplane had come to rest in an inverted position, and the red, oily brake fluid had leaked from the vent of the fluid reservoir and was found in the cockpit above the reservoir, leaking from the engine cowling. A substantial amount of brake fluid was also reported to be found on the ground beneath the engine cowling at the site of the accident. When brake fluid was added through the fluid ports, the brakes worked properly and no leaks were found in the lines. The brake pads were worn to approximately 1/4-inch in thickness, and the left brake rotor exhibited grooves; however, the brakes were fully effective when pressure was applied. At 1049, the automated weather observing system at LHB reported wind from 340 degrees at 7 knots, 10 statute miles visibility, an overcast sky at 900 feet, temperature 70 degrees Fahrenheit, dew point 62 degrees Fahrenheit, and a barometric pressure setting of 29.93 inches of Mercury. The 420-hour commercial pilot was taxiing at approximately 30 knots in a tail-wheel eqipped airplane with an 8-knot quartering tailwind. The airplane veered off to the left of the runway and collided with a bail of hay. The impact forced the airplane to nose-over and come to rest in an inverted position. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2004_DFW05CA001.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

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