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ERA13CA377

2013-08-24 · Mitchellville, Maryland, United States · None · 1 aircraft · Status: Completed

Airport W00

Current FAA registration · N98923

Make / Model
CESSNA 172P
Year of manufacture
1985 · 28 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19850422
ADS-B equipped
Yes — Mode-S ADCF4D

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s decision to depart with a known deficiency following a hard landing. Contributing to the accident was an anomaly of the airplane’s nosewheel steering that could not be replicated during post-accident examination.

Factual narrative

The pilot reported that while taxiing for takeoff for a local flight with passengers, the right rudder felt “stiff.” Once in the air, the rudder operated normally; however, the pilot’s first landing was “hard.” After picking up a second set of passengers, the pilot noticed that while taxiing back to the runway, the right rudder felt even more stiff. At one point during the taxi, the pilot “stomped” on the rudder to steer the airplane right, but did not think much of the anomaly, as the airplane seemed to move normally after applying additional engine power. During the subsequent takeoff, the pilot noticed that the right rudder pedal continued to feel stiffer than it had during the previous takeoff.   During the second landing, the airplane veered immediately left upon touchdown and departed the runway. The pilot attempted to correct the airplane’s course, but the right rudder pedal was unresponsive. The pilot then attempted to abort the landing, but once in the air, he realized the airplane would not be able to climb above approaching trees and decided to land the airplane in a farm field. During the landing the nose landing gear collapsed and the airplane nosed over, resulting in substantial damage. A Federal Aviation Administration inspector examined the airframe and flight controls following the accident and confirmed that the rudder was free to move, but that the nose steering system of the airplane had been compromised during the accident and its pre-impact functionality could not be determined. When asked how the accident could have been prevented the pilot stated, “After a hard land[ing] have the plane inspected – Don’t takeoff even if it seems normal.” The pilot reported that while taxiing for takeoff for a local flight with passengers, the right rudder felt “stiff.” Once in the air, the rudder operated normally; however, the pilot’s first landing was “hard.” After picking up a second set of passengers, the pilot noticed that while taxiing back to the runway, the right rudder felt even more stiff. At one point during the taxi, the pilot “stomped” on the rudder to steer the airplane right, but did not think much of the anomaly, as the airplane seemed to move normally after applying additional engine power. During the subsequent takeoff, the pilot noticed that the right rudder pedal continued to feel stiffer than it had during the previous takeoff.   During the second landing, the airplane veered immediately left upon touchdown and departed the runway. The pilot attempted to correct the airplane’s course, but the right rudder pedal was unresponsive. The pilot then attempted to abort the landing, but once in the air, he realized the airplane would not be able to climb above approaching trees and decided to land the airplane in a farm field. During the landing the nose landing gear collapsed and the airplane nosed over, resulting in substantial damage. A Federal Aviation Administration inspector examined the airframe and flight controls following the accident and confirmed that the rudder was free to move, but that the nose steering system of the airplane had been compromised during the accident and its pre-impact functionality could not be determined. When asked how the accident could have been prevented the pilot stated, “After a hard land[ing] have the plane inspected – Don’t takeoff even if it seems normal.” Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

FAA avdata. C = Cause, F = Factor.

  • C Aircraft-Aircraft systems-Landing gear system-Nose/tail landing gear-Malfunction - C
  • C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C

Verbatim from NTSB's published report. Source file NTSB_2013_ERA13CA377.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.