N7584M

Substantial
Fatal

CESSNA 175S/N: 55884

Accident Details

Date
Friday, October 15, 2021
NTSB Number
WPR22FA011
Location
Reserve, NM
Event ID
20211015104107
Coordinates
33.596478, -108.721550
Aircraft Damage
Substantial
Highest Injury
Fatal
Fatalities
1
Serious Injuries
2
Minor Injuries
0
Uninjured
0
Total Aboard
3

Probable Cause and Findings

The pilot’s failure to maintain clearance from terrain while maneuvering at a low altitude. Contributing to the accident was the pilot’s reduced forward visibility due to the sun.

Aircraft Information

Registration
Make
CESSNA
Serial Number
55884
Engine Type
Reciprocating
Year Built
1959
Model / ICAO
175C175
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
175

Registered Owner (Current)

Name
PECOTTE HARRY A
Address
810 E APACHE ST
City
SILVER CITY
State / Zip Code
NM 88061-6646
Country
United States

Analysis

HISTORY OF FLIGHTOn October 15, 2021, about 0959 mountain daylight time, a Cessna 175, N7584M, was substantially damaged when it was involved in an accident near Reserve, New Mexico. The pilot was fatally injured, and the two passengers were seriously injured. The aircraft was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

A summary of combined statements obtained from the two passengers, was provided by their attorney. In that summary, the passengers stated that they recall that the weather was cold and clear on the day of the accident flight, and that the purpose of the flight was to scout areas to hunt. When they reached a planned hunting area, they pointed out to the pilot where they wanted to look, and the pilot turned toward that area. They recall a turn to the northeast that was “a sharp turn and then the airplane started to go down quickly.” They thought it sounded like the engine had lost power and the pilot “was having a hard time.” The airplane leveled off and the pilot did not make a distress call, but the mountains kept getting closer. They recall that it was difficult to see out of the windshield, the airplane was “tilted up”, and they impacted trees.

Data downloaded from a handheld GPS showed that the airplane departed Grant County Airport, near Silver City, New Mexico about 0907. The airplane flew north-northwest for 21 minutes, then west-northwest for another 17 minutes. In the final 9 minutes of the flight, the data showed that the airplane turned to a northerly heading, before it turned to the southeast. During the last 2 minutes of the flight, the airplane remained on a southeasterly heading and ascended from 6,732 ft mean sea level (msl) to 7,530 ft msl. The last recorded GPS data point was located about 95 ft south of the accident site, at an altitude of 7,523 ft msl. METEOROLOGICAL INFORMATIONA review of astronomical data from the National Oceanic and Atmospheric Administration revealed that, at the time and location of the accident, the sun was located at an azimuth of 126.2° true (117.2° magnetic), and an elevation of 29.29° above the horizon.

The calculated density altitude at the accident site around the time of the accident was 8,564 ft and the calculated pressure altitude was 7,151 ft. WRECKAGE AND IMPACT INFORMATIONExamination of the accident site revealed the airplane impacted mountainous terrain at an elevation of 7,521 ft msl. The first identifiable point of contact was the top of a pine tree located about 100 ft downhill from the wreckage. Branches from damaged trees were found on the ground and displayed signatures consistent with propeller strikes.

The airplane came to rest on its left side. The left wing was folded upward and remained attached by the control cables. Both wings exhibited impact damage along their leading edges. The horizontal and vertical stabilizers remained attached to the empennage, and the elevator and rudder remained attached at their respective attachment points. Flight control continuity was established for all flight control surfaces.

Examination of the recovered engine revealed that when the crankshaft was rotated by hand using the propeller, rotational continuity was established throughout the engine and valvetrain, and thumb compression was obtained on all cylinders.

The engine was started and ran at various power settings with no anomalies noted.

The propeller remained attached to the crankshaft flange and the propeller blades remained attached to the hub. The propeller blades displayed leading edge gouging, torsional twisting, chordwise striations across the cambered surface, and trailing edge “S” bending.

No evidence of preexisting mechanical malfunction was observed with the airframe or engine that would have precluded normal operation. MEDICAL AND PATHOLOGICAL INFORMATIONToxicology testing performed at the Federal Aviation Administration Forensic Sciences Laboratory found Losartan, Rosuvastatin, and Diphenhydramine in the pilot’s blood and urine. Losartan is a prescription medication used to treat high blood pressure, and Rosuvastatin is a prescription cholesterol medication. Neither of these medications are known to adversely affect performance. Diphenhydramine is an over-the-counter antihistamine and can impair performance, depending on the circumstances of use. Carboxyhemoglobin, Ethanol, Glucose, and drugs of abuse were not detected.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR22FA011