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Atlas / NTSB / WPR12CA311

NTSB CAROL · Event

Event WPR12CA311

2012-07-11 Idaho Falls, Idaho, United States Airport · IDA None 1 aircraft Status: Completed

Registry · N787AE

FAA Aircraft Registry record.

Make / Model

CESSNA T210L

Year of manufacture

1972 · 40 years old at event

Engine

CONT MOTOR TSIO-520 SER (300 hp)

Seats / Engines

6 seats · 1 engine

Last airworthiness date

19730119

ADS-B equipped

Yes — Mode-S AAAA8C

Registrant of record

COORDINATE PRODUCTIONS LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s failure to extend the landing gear before landing. Contributing to the accident was an uncorrected malfunction of the landing gear warning horn system.

Factual narrative

The pilot reported that in anticipation of a difficult approach and landing due to reported winds he configured the airplane early with the mixture-rich, propeller-high rpm, and the fuel selected to the fullest tank. He did not extend the landing gear due to the distance from the airport. The pilot entered the traffic pattern on a normal 45-degree entry for landing. On final approach he failed to perform the pre-landing checklist and confirm the landing gear was down. The airplane touched down on the runway surface with the landing gear retracted, which caused substantial damage to the fuselage structure. The pilot stated that during the annual inspection there had been an anomaly in the gear warning horn system and it was noted to be out of adjustment and had not been resolved. The pilot reported no other preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. The pilot reported that, in anticipation of a difficult approach and landing due to the reported wind, he configured the airplane early with the mixture rich, propeller at high rpm, and the fuel selected to the fullest tank. He did not extend the landing gear due to the distance from the airport. The pilot entered the traffic pattern on a normal 45-degree entry for landing. On final approach, he failed to perform the prelanding checklist and to confirm that the landing gear was down. The airplane touched down on the runway with the landing gear retracted, which resulted in substantial damage to the fuselage structure. The pilot stated that, during the annual inspection, the gear warning horn system was noted to be out of adjustment, and this had not been resolved. The pilot reported no other preimpact mechanical malfunctions or failures with the airplane that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • C Aircraft-Aircraft systems-Landing gear system-(general)-Not used/operated - C
  • C Personnel issues-Action/decision-Action-Forgotten action/omission-Pilot - C
  • F Aircraft-Aircraft systems-Landing gear system-Gear position and warning-Not serviced/maintained - F

Verbatim from NTSB's published report. Source file NTSB_2012_WPR12CA311.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.