ATL04CA162
2004-07-11 · Chamblee, Georgia, United States · None · 1 aircraft · Status: Completed
Airport PDK
Aircraft involved
Probable cause & findings
The pilot's improper landing flare that resulted in a hard landing. A factor was a tailwind condition.
Factual narrative
On July 11, 2004, at 1215 eastern daylight time, a Cessna 172, N6555D, registered to and operated by Aviation Atlanta, Inc., collided with the runway during an attempted landing on runway 20L at DeKalb-Peachtree Airport, Chamblee, Georgia. The solo instructional flight was conducted under Title 14 CFR Part 91, and visual flight rules (VFR). Visual meteorological conditions prevailed at the time of the accident, and a VFR flight plan was filed and activated. The student pilot was not injured and the airplane sustained substantial damage. The flight originated at Letourneau Field, Toccoa, Georgia, on July 11, 2004 at 1125. According to the pilot, the flight was a solo cross country flight originating at DeKalb-Peachtree Airport (PDK) with intermediate stops in Andersen, South Carolina and Toccoa, Georgia. The pilot stated that upon returning to the PDK terminal area, he listened to the current weather information, which reported the winds to be from 330 degrees at 11 knots, and contacted the PDK control tower. He stated that over the runway surface, he may have "flared too high", resulting in a high sink rate and the airplane bounced on the runway three times. He stated he was able to taxi the airplane to the ramp for assistance, and during the post-flight inspection of the airplane, he noticed the damage to the airplane. Examination of the wreckage revealed that the right lower and left upper engine firewall were buckled and the right lower engine mount was separated from the firewall. The pilot and passenger floor panels were buckled and the right side of the fuselage, engine cowling, and bottom forward pilot compartment were buckled. The propeller was bent on both tips. Neither flight control yoke was able to travel forward, aft, left, or right. The pilot further stated that it had been more than 4 months since he had practiced crosswind landings. The pilot stated that while approaching the destination , he listened to the current weather information, which reported the winds to be from 330 degrees at 11 knots. He stated that during the landing on runway 20L, he may have "flared too high", resulting in a high sink rate and the airplane bounced on the runway three times. He stated he was able to taxi the airplane to the ramp for assistance, and during the post-flight inspection of the airplane, he noticed the damage to the airplane. Examination of the wreckage revealed that the right lower and left upper engine firewall were buckled and the right lower engine mount was separated from the firewall. The pilot and passenger floor panels were buckled and the right side of the fuselage, engine cowling, and bottom forward pilot compartment were buckled. The propeller was bent on both tips. Neither flight control yoke was able to travel forward, aft, left, or right. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_ATL04CA162.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type. All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
The NASA Emergency Locator Transmitter Survivability and Reliability project was initiated in 2013 to assess the crash performance standards for the next generation of emergency locator transmitter (E…
- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- Embry-Riddle Scholarly Commons 2023 · Conference paper Validation of Training Satisfaction Survey
The Training Satisfaction Survey (TSS) was developed as part of a larger project to examine the features of Virtual Reality software and supporting devices as a training program on visual illusions an…
- Semantic Scholar 2021 · Article (Data in Brief) Cockpit voice recorder transcript data: Capturing safety voice and safety listening during historic aviation accidents
Cockpit Voice Recorder (CVR) transcripts capture audio data within cockpit environments. This aids the investigation of causal factors contributing to aviation accidents by revealing communication and…
- Semantic Scholar 2021 · Article (Safety Science) Safety voice and safety listening during aviation accidents: Cockpit voice recordings reveal that speaking-up to power is not enough
Abstract Safety voice is theorised as an important factor for mitigating accidents, but behavioural research during actual hazards has been scant.