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MIA95LA002

1994-10-03 · STUART, Florida, United States · None · 1 aircraft · Status: Completed

Airport SUA

Current FAA registration · N701AM

Make / Model
CESSNA 421B
Year of manufacture
1973 · 21 years old at event
Engine
CONT MOTOR GTSI0-520-F-K (435 hp)
Seats / Engines
8 seats · 2 engines
Last airworthiness date
19850531
ADS-B equipped
Yes — Mode-S A95851

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

THE IMPROPER RIGGING OF THE LANDING GEAR SAFETY SQUAT SWITCH BY OTHER MAINTENANCE PERSONNEL. CONTRIBUTING TO THE ACCIDENT WAS THE CONTAMINATION OF THE GEAR SQUAT SWITCH WITH CORROSION AND WATER.

Factual narrative

On October 3, 1994, about 0753, eastern daylight time, N701AM, a Cessna C-421B, registered to and operated by Air Mobile Ministries, experienced an all-landing gears collapse on landing at Whitman Field, Stuart, Florida. The flight was a 14 CFR Part 91 personal flight. The planned destination was Port-au-Prince, Haiti. Visual meteorological conditions prevailed at the time and a VFR flight plan was filed. The airplane was substantially damaged and the pilot and six passengers reported no injuries. The flight was originating at the time of the accident. The pilot stated that after takeoff the landing gear would not come up so he placed the gear handle in the down position and observed three green lights. On landing roll the gear collapsed. The one passenger who was on board was an FAA employee in a duty travel status, from the San Juan, Puerto Rico, Flight Standards District Office. Examination of the landing gear safety switch [Squat] by FAA personnel revealed that the switch was corroded, full of water and was improperly rigged. FAA personnel also reported the airplane weight and balance data used by the pilot for takeoff computations was in error, and the airplane was about 200 pounds over gross weight on departure. AFTER TAKEOFF TOWER CONTROLLERS TOLD THE PILOT THAT THEY SAW SMOKE TRAILING FROM THE RIGHT ENGINE. THE PILOT ELECTED TO RETURN TO THE FIELD FOR LANDING, AND LOWERED THE LANDING GEAR AND OBSERVED THE GEAR DOWN INDICATIONS. ON LANDING ROLL THE GEAR COLLAPSED. AFTER THE AIRPLANE WAS RECOVERED AND PLACED ON JACKS IT WAS DISCOVERED THAT THE LANDING GEAR SAFETY SWITCH WAS CONTAMINATED WITH WATER, CORRODED AND IMPROPERLY RIGGED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1994_MIA95LA002.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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