20230528008739A

Accident · Substantial damage

FAA accident report · Cessna 175A · Enterprise, UT · May 28, 2023

Date
May 28, 2023 · 16:43 local
Place
Enterprise, UT
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5089
NTSB investigation
NTSBWPR23LA204
Reported as
Cessna 175A
Reported engine
Continental GO-300 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor, private pilot
Pilot’s flight hours
350 total95 in this make and model25 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

The pilot in command (PIC) departed from a private airstrip at mackie ranch (UT91) approximately 6 miles sw of Enterprise Utah. The PIC planned a route of flight from UT91 to las vegas. The airman stated he had planned and flown this route in the past. The airfield is at an elevation of 5642 feet. The sheriff reported the temperature to be approximately 85 degrees fahrenheit at the site of the crash. The altitude of the crash was approximately 6900 feet. The outside conditions were VMC. The PIC departed the field and started a normal climb out. He was flying a heading of approximately 266 degrees towards a saddle in the mountains to the wsw of UT91. As the aircraft was approaching the saddle the aircraft started to lose performance and was only able to continue climbing at less than 50’ per minute. The airman had chosen to fly up the left side of the saddle which he stated did not leave the aircraft enough room to turn around. The PIC stated from the perspective inside the aircraft it appeared as though the aircraft would clear the trees and saddle of the mountain. At the time the aircraft reached the saddle of the mountain it was not above tree top level. The aircraft first stuck the tops of trees before losing further altitude where the aircraft struck the side of the mountain which caused to aircraft to flip upside down with the wing tops down. The aircraft did not have the necessary climb performance for the route chosen. Due to high density altitude and downdrafts near the saddle of the mountain. The aircraft made a controlled flight into terrain (cfit) due to insufficient altitude.

As the FAA filed it

THE PILOT IN COMMAND (PIC) DEPARTED FROM A PRIVATE AIRSTRIP AT MACKIE RANCH (UT91) APPROXIMATELY 6 MILES SW OF ENTERPRISE UTAH. THE PIC PLANNED A ROUTE OF FLIGHT FROM UT91 TO LAS VEGAS. THE AIRMAN STATED HE HAD PLANNED AND FLOWN THIS ROUTE IN THE PAST. THE AIRFIELD IS AT AN ELEVATION OF 5642 FEET. THE SHERIFF REPORTED THE TEMPERATURE TO BE APPROXIMATELY 85 DEGREES FAHRENHEIT AT THE SITE OF THE CRASH. THE ALTITUDE OF THE CRASH WAS APPROXIMATELY 6900 FEET. THE OUTSIDE CONDITIONS WERE VMC. THE PIC DEPARTED THE FIELD AND STARTED A NORMAL CLIMB OUT. HE WAS FLYING A HEADING OF APPROXIMATELY 266 DEGREES TOWARDS A SADDLE IN THE MOUNTAINS TO THE WSW OF UT91. AS THE AIRCRAFT WAS APPROACHING THE SADDLE THE AIRCRAFT STARTED TO LOSE PERFORMANCE AND WAS ONLY ABLE TO CONTINUE CLIMBING AT LESS THAN 50’ PER MINUTE. THE AIRMAN HAD CHOSEN TO FLY UP THE LEFT SIDE OF THE SADDLE WHICH HE STATED DID NOT LEAVE THE AIRCRAFT ENOUGH ROOM TO TURN AROUND. THE PIC STATED FROM THE PERSPECTIVE INSIDE THE AIRCRAFT IT APPEARED AS THOUGH THE AIRCRAFT WOULD CLEAR THE TREES AND SADDLE OF THE MOUNTAIN. AT THE TIME THE AIRCRAFT REACHED THE SADDLE OF THE MOUNTAIN IT WAS NOT ABOVE TREE TOP LEVEL. THE AIRCRAFT FIRST STUCK THE TOPS OF TREES BEFORE LOSING FURTHER ALTITUDE WHERE THE AIRCRAFT STRUCK THE SIDE OF THE MOUNTAIN WHICH CAUSED TO AIRCRAFT TO FLIP UPSIDE DOWN WITH THE WING TOPS DOWN. THE AIRCRAFT DID NOT HAVE THE NECESSARY CLIMB PERFORMANCE FOR THE ROUTE CHOSEN. DUE TO HIGH DENSITY ALTITUDE AND DOWNDRAFTS NEAR THE SADDLE OF THE MOUNTAIN. THE AIRCRAFT MADE A CONTROLLED FLIGHT INTO TERRAIN (CFIT) DUE TO INSUFFICIENT ALTITUDE.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N5089 · 1

Matched to the same aircraft by N-number and date.