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DFW08CA033

2007-10-20 · Lufkin, Texas, United States · None · 1 aircraft · Status: Completed

Airport KLFK

Current FAA registration · N172GH

Make / Model
CESSNA 172R
Year of manufacture
1997 · 10 years old at event
Engine
LYCOMING I0360 SER A&C (200 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19971003
ADS-B equipped
Yes — Mode-S A12139

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot's improper recovery from a bounced landing.

Factual narrative

The 64-hour student pilot lost control of the airplane when the airplane bounced during a hard landing on runway 15. The pilot deployed full flaps soon after turning final approach; however, he believed that the airplane was too high on final approach to elected to slip the airplane to increase his rate of descent while he attempted to maintain 70 knots on final approach. As the airplane approached the runway the pilot discontinued the landing slip; however, a high rate of descent had developed and the airplane landed hard. following the hard landing, the airplane bounced and porpoise developed. Examination of the airplane reveled that the nose gear tire had been blown during the hard landing. Further examination revealed that the engine firewall had sustained structural damage. The winds at the time of the mishap were reported from 190 degrees at 18 knots. The 64-hour student pilot lost control of the airplane when the airplane bounced during a hard landing on runway 15. The pilot deployed full flaps soon after turning final approach; however, he believed that the airplane was too high on final approach so he elected to slip the airplane to increase his rate of descent while he attempted to maintain 70 knots on final approach. As the airplane approached the runway the pilot discontinued the landing slip; however, a high rate of descent had developed and the airplane landed hard. Following the hard landing, the airplane bounced and a porpoise developed. Examination of the airplane reveled that the nose gear tire had been blown during the hard landing. Further examination revealed that the engine firewall had sustained structural damage. The winds at the time of the mishap were reported from 190 degrees at 18 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_2007_DFW08CA033.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.