No fatalities

Landing Gear Failure and Power Loss During Ferry Flight Leads to Hard Landing (N3MU)

Denver-Stapleton, United States of AmericaLanding (descent or approach)

On October 12, 1986, a Mitsubishi MU-2 Marquise (registration N3MU) operated by Midway Aircraft Brokers was involved in an aviation accident near Denver-Stapleton, United States of America during landing or approach. No fatalities were reported. Investigators recorded the probable cause as: Occurrence #1: circuit breaker not engaged, maintenance inadequate, aircraft preflight inadequate, lack of familiarity with aircraft (pilot and copilot), landing gear inoperative, false indication. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 2026-06-11Data APIEditorial standards

A twin-engine aircraft on a ferry flight from Grand Junction to Chicago experienced landing gear retraction failure after takeoff from Denver. The pilot returned, but engine power loss occurred on approach, resulting in a hard landing that broke the left wing. Both occupants were uninjured.

Summary

A twin-engine aircraft being ferried from Grand Junction, Colorado, to Chicago, Illinois, with an en route stop at Denver, Colorado, experienced a landing gear malfunction after takeoff from Denver. During the return to Denver, the aircraft suffered partial engine power loss and made a hard landing, breaking the left wing. Both occupants escaped uninjured.

Incident Details

The pilot attempted to retract the landing gear after takeoff but was unsuccessful. After several attempts, he decided to return to Denver. On final approach, the right engine began surging, and the left engine failed to increase power. The aircraft made a hard landing on the runway, resulting in structural damage to the left wing.

Investigation Findings

Post-incident examination revealed that the speed levers on both engines were inoperative because the propeller governor and underspeed fuel governor reset arms were positioned on the opposite side of the speed lever actuating arms. The landing gear functioned normally during subsequent swing tests, indicating no mechanical fault with the gear itself. It was later learned that the right main tire had blown on takeoff three days earlier, requiring repair. At that time, maintenance personnel had opened the landing gear circuit breakers to prevent inadvertent gear retraction. The pilot stated that he checked the circuit breakers when the gear failed to retract.

Official findings identified multiple causes across three occurrences. In the first occurrence (takeoff), the circuit breakers were not engaged, maintenance was inadequate, the pilot's preflight was inadequate, both pilots lacked familiarity with the aircraft, the landing gear was inoperative, and the gear indicating system provided false indications. In the second occurrence (approach), the pilot did not follow the checklist, the propeller governor control linkage was incorrect, and maintenance personnel had not corrected this issue; other maintenance personnel provided inadequate service. In the third occurrence (landing), the pilot allowed the airspeed to drop below the reference speed, was diverted in attention, and inadvertently stalled the aircraft.

Probable cause

Occurrence #1: circuit breaker not engaged, maintenance inadequate, aircraft preflight inadequate, lack of familiarity with aircraft (pilot and copilot), landing gear inoperative, false indication. Occurrence #2: checklist not followed, propeller governor control linkage incorrect, maintenance not corrected, service inadequate. Occurrence #3: airspeed below Vref, diverted attention, inadvertent stall.