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Atlas / NTSB / CEN11LA365

NTSB CAROL · Event

Event CEN11LA365

2011-05-27 Freemont, Michigan, United States Airport · FFX Minor 1 aircraft Status: Completed

Registry · N60147

FAA Aircraft Registry record.

Make / Model

BOEING A75N1(PT17)

Year of manufacture

1941 · 70 years old at event

Engine

CONT MOTOR W670 SERIES (250 hp)

Seats / Engines

2 seats · 1 engine

Last airworthiness date

19600324

ADS-B equipped

Yes — Mode-S A7CDFA

Registrant of record

MCGUIRE ZACH T

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The pilot’s failure to attain a positive climb rate following takeoff for reasons that could not be determined because the propeller was not provided for further examination. Contributing to the accident was the pilot's impairment from alcohol.

Factual narrative

On May 27, 2011, about 1500 eastern daylight time, a Boeing A75NA (PT17), N60147, descended and impacted terrain while turning crosswind after takeoff from Fremont Municipal Airport Fremont (FFX), Michigan. The airplane transport pilot sustained minor injuries and the pilot-rated passenger was uninjured. The airplane sustained substantial damage to both wings. The airplane was registered to and operated by the pilot as a personal flight under the provisions of 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed and no flight plan had been filed for the flight that was to remain in the airport traffic pattern of FFX. The flight originated from FFX about 1430. The pilot-rated passenger did not have a tailwheel endorsement and had received flight instruction from the pilot prior to the day of the accident. On the day of the accident, the passenger performed the first takeoff and landing which was to be followed by the pilot performing the second takeoff and landing while remaining in the airport traffic pattern. The passenger stated that the airplane was running fine and it did not sound differently prior to the accident. The pilot-rated passenger stated that he did not realize anything was wrong until all he could see was tree branches which was followed by the impact. The pilot stated that airplane seemed to stop climbing after it entered the crosswind leg of the departure. The airplane then started to settle and descended into trees. The Michigan Department of State Police administered a preliminary breath test (PBT) to the pilot at 1610. The PBT results were 0.188 blood alcohol content (BAC). The State of Michigan Department of State Police Forensic Science Division Laboratory Report, Results of Analysis,of the pilot stated: 0.15 grams alcohol per 100 milliliters blood. According to the Federal Aviation Administration (FAA) inspector, the propeller was a McCauley, D1093 Navy hub, serial number MC-45-249. One propeller blade was bent backwards and had impact marks on the back side of the blade but not on the leading edge. The engine case was cracked. The FFX airport manager said that the pilot disassembled and inspected the propeller and noted the presence of light corrosion within the hub. The pilot then threw the hub in the garbage. The airport manager said that the propeller blades had been damaged from their impact with trees. He said the pilot did not think that there was anything wrong with the propeller and did not want to provide the propeller for examination, which was requested by the Federal Aviation Administration inspector and National Transportation Safety Board Investigator-In-Charge. According to the Federal Aviation Administration brochure "Alcohol and Flying," effects of a BAC of .18% - .30% can include confusion, dizziness, exaggerated emotions (anger, fear, grief) impaired visual perception, decreased pain sensation, impaired balance, staggering gait, slurred speech, and moderate muscular incoordination. Effects of a BAC of .09% - .25% can include emotional instability, loss of critical judgment, impairment of memory and comprehension, decreased sensory response, and mild muscular incoordination. It advises that "The number of serious errors committed by pilots dramatically increases at or above concentrations of 0.04% blood alcohol. This is not to say that problems don’t occur below this value. Some studies have shown decrements in pilot performance with blood alcohol concentrations as low as 0.025%." The airplane began to descend after takeoff and while on the crosswind leg of the airport traffic pattern. The pilot stated that he could not stop the airplane from descending before the airplane impacted trees. The passenger stated that the airplane was running fine and that it did not sound different before the accident. The pilot did not provide the propeller assembly for further examination to determine what may have reduced the airplane’s climb performance. The Michigan Department of State Police administered a preliminary breath test to the pilot after the accident; the pilot’s blood alcohol concentration (BAC) was 0.18%. The State Police Forensic Science Division’s laboratory report analyzed the pilot’s blood, which had a BAC of 0.15%. According to the Federal Aviation Administration (FAA), effects of a BAC of .18% can include confusion, dizziness, impaired visual perception, impaired balance, and moderate muscular incoordination. 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 oper/perf/capability-Performance/control parameters-Climb rate-Not attained/maintained - C
  • C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
  • F Personnel issues-Physical-Impairment/incapacitation-Alcohol-Pilot - F

Verbatim from NTSB's published report. Source file NTSB_2011_CEN11LA365.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.