CEN11LA365

NTSB accident investigation · Boeing A75N1 (PT17) · Freemont, MI · May 27, 2011

Accident · Minor injuriesLimited investigationFinal report
Date
May 27, 2011, 15:00 local (19:00 UTC)
Place
Freemont, MI
Injuries
1 minor, 1 uninjured
Damage
Substantial damage
Phase of flight
Other
Aircraft
N60147Boeing A75N1 (PT17)
Defining event
Other: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed · report November 27, 2012
Report
Approved by Office Director
NTSB office
Central Region
Parties
Federal Aviation Administration, McCauley Propeller Systems
FAA report
20110527012899A
Case key
79278

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

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.

Findings · 3

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Performance/control parameters: climb rateAircraft › Aircraft oper/perf/capability · Not attained/maintainedBoeing A75N1(PT17): 1 caseAll aircraft: 265 casesProbable cause
Not determinedNot determined › Not determined · Unknown/Not determinedBoeing A75N1(PT17): 8 casesAll aircraft: 2,247 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

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.

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 muscularincoordination. 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%."

Aircraft

Registration
N60147
Reported as
Boeing A75N1 (PT17)
Category
Airplane
Serial number
75-1951
Airframe hours
3,885
Engine
Continental W670, 220 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Pilot
Registered owner
Pilot
Airworthiness certificate
Standard, Aerobatic
Last inspection
Annual · October 1, 2010
Departed
FFX · Freemont, MI
Destination
Freemont, MI
Airport
FFX · Fremont Municipal Airport, runway 09, 3,502 × 75 ft, asphalt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew · 2

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
67
Injuries
Minor
Certificates
Airline transport, Flight instructor
Airplane ratings
Single-engine sea, Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
May 24, 2011
Seat
Front
Toxicology
Performed
Flight hours
18,925 total · 1,218 in this make and model · 17,266 as pilot in command · 50 in the last 90 days · 1 in the last 30 days · 0 in the last 24 hours
Role
Pilot
Age
46
Injuries
None
Certificates
Private, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Seat
Rear

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 10 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
167 °F
Observed at
FFX, 2 nm away

Docket · 5

The files NTSB released with the investigation on September 26, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.3 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.