# NTSB ATL04CA145: Cessna 172 RG, N6321R, Fernandina, FL, July 8, 2004

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Data collection · Final report
- Date: July 8, 2004, 10:45 local (14:45 UTC)
- Place: Fernandina, FL
- Coordinates: 30.611665, -81.462219
- Nearby events: https://openairdocs.org/map.md?lat=30.6117&lon=-81.4622&mi=10
- Phase of flight: [Landing](https://openairdocs.org/ntsb-phases/550) (OpenAirDocs' grouping)
- Highest injury: No injuries
- Injuries: 2 uninjured
- Status: Completed, report June 28, 2006
- Report: Approved by Office Director
- Parties: ASO FSDO 15
- NTSB case key (mKey): 59777
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=ATL04CA145
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/59777/pdf
- Page: https://openairdocs.org/ntsb/ATL04CA145

## Probable cause

The pilot's failure to follow the checklist and lower the landing gear prior to landing.

## Sequence of events

In NTSB's coding before 2008 (https://www.ntsb.gov/GILS/Documents/codman.pdf).

- Wheels up landing, landing
  - checklist - not followed, pilot in command (cause)

## Analysis

According to the pilot, "while I was plotting my course to make sure that [I] was going to make the runway I was calling out the items on the checklist.  I was trying to take the first half of the runway and I was high on the approach. I was trying to concentrate on getting down before the point that he (check airman) pointed out. I finally was getting [down] and I had my point made until we heard a horrendous noise which was the prop hitting the pavement."   Examination of the airplane revealed engine and propeller damage, firewall damage, underbelly fuselage damage as well as front doors and skin being cracked and buckled.  The landing gear system, all three wheels, were still in the wheel wells. The subsequent functional test of the landing gear system failed to disclose a mechanical problem. The functional test also determined that the landing gear warning horn was operational.

## Factual narrative

On July 8th, 2004, at 1045 eastern daylight time, a Cessna 172 RG, N6321R, registered to and operated by Delta Flight Connection, landed wheels-up at Fernandina Beach Municipal Airport, Fernandina Beach, Florida. The airplane was being flown by the pilot during a Commercial Single Engine check ride under the provisions of Title 14, CFR Part 91, when the accident occurred. The private pilot and check-airman were not injured. Visual meteorological conditions prevailed and no flight plan was filed for the local flight. The airplane sustained substantial damage. The flight originated from Fernandina Beach, Florida at 0930.

According to the check airman, he initiated single engine failure by pulling the carburator heat out and reducing the throttle to idle.  The applicant performed the emergency items and called "gear down", "flaps down" and "something like 1st landing configuration complete".  On short final, the check airman stated that he called out certain final items as a safety reminder such as gear down, mixture rich, props forward, cleared to land. " I can not recall if he acknowledged/double-checked these items."

According to the Pilot in Command, "while I was plotting my course to make sure that was going to make the runway I was calling out the items on the checklist.  I was trying to take the first half of the runway and I was high on the approach. I was trying to concentrate on getting down before the point that he (check airman) pointed out. I finally was getting done and I had my point made until we heard a horrendous noise which was the prop hitting the pavement."

Examination of the airplane revealed engine and propeller damage, firewall damage, underbelly of fuselage damage as well as front doors and skin being cracked and buckled.  The landing gear, all three wheels, was still in the wheel well. The subsequent functional test of the landing gear system failed to disclose a mechanical problem. The functional test also determined that the landing gear warning horn was properly working.

## Aircraft

- Registration: [N6321R](https://openairdocs.org/deregistered/N6321R-2006-05-19), registration cancelled 2006-05-19, S/N 172RG0164, built 1979 (OpenAirDocs)
- Reported make and model: Cessna 172 RG
- Registry model: [Cessna 172RG](https://openairdocs.org/model/cessna-172rg) (registry code 2072438) (OpenAirDocs)
- Registry engine: [Lycoming O&VO-360 series](https://openairdocs.org/engine/lycoming-o-vo-360-series) (registry code 41514, reciprocating) (OpenAirDocs)
- Category: Airplane
- Serial number: 172rg0164
- Engines: Lycoming O-360 reciprocating
- Damage: Substantial damage
- Flight: Instructional, Part 91
- Registered owner: Delta Flight Connection Academy
- Airworthiness certificate: Standard, Normal
- Departed: 55J, FERNANDINA BEAC, FL
- Destination: Fernandina, FL

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 20; injuries: none; private; airplane ratings: single-engine land; instrument ratings: airplane; medical: class 3, valid medical--no waivers/lim.; seat: front; flight hours: 160 total, 0 in this make and model

## Weather

- Conditions: Visual (VMC), Day
- Wind: 270° at 5 knots
- Lowest ceiling: 200 ft broken
- Temperature: 82 °F, dew point 72 °F
- Altimeter: 30.03 inHg
- Observed at: JAX

## FAA reports on this event (1)

The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs).

- [Accident 20040708012639A](https://openairdocs.org/incident/20040708012639A), Jul 8, 2004: Cessna 172RG, Fernandina Beac, FL, Minor damage. (-23) PIC failed to lower landing gear. Aircraft landed gear up causing minor damage to aircraft, the PIC and DPE were not injured.

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

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