Loss of control Accident Cessna A185F Skywagon N243W,
ASN logo
ASN Wikibase Occurrence # 145301
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Wednesday 25 April 2012
Time:15:40
Type:Silhouette image of generic C185 model; specific model in this crash may look slightly different    
Cessna A185F Skywagon
Owner/operator:Private
Registration: N243W
MSN: 18503820
Year of manufacture:1979
Total airframe hrs:1364 hours
Engine model:Continental IO 520 SERIES
Fatalities:Fatalities: 3 / Occupants: 3
Aircraft damage: Substantial
Category:Accident
Location:Dark Canyon Wilderness Area near Blanding, UT -   United States of America
Phase: En route
Nature:Private
Departure airport:Hidden Splendor, UT (N/A)
Destination airport:Price, UT (PUC)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot departed in the airplane with his father and a flight instructor who had extensive experience flying in the local canyon areas. The intention was to perform a sightseeing flight, with multiple stops at backcountry airstrips. The flight instructor was carrying a personal locator device, which transmitted position data at 10-minute-intervals but no altitude information. This data revealed that the airplane landed at three airstrips. Shortly after the airplane departed the third airstrip about midafternoon, the instructor’s personal locator began a series of transmissions all from the same location, about 1.2 miles from an unused airstrip. These transmissions continued from that location for about the next 12 hours; however, no emergency or alert notifications were received from the personal locator or the airplane’s emergency locator transmitter (ELT) during that period. When the airplane had not returned to the original departure airport by nighttime, search and rescue efforts were initiated.

The wreckage was located in the early morning hours the next day on the edge of a plateau in remote wilderness, at an elevation of 6,900 feet mean sea level. The airplane wreckage came to rest on an uphill slope and was mostly consumed by postimpact fire. The terrain north and east of the accident site fell away to steep canyon walls, which descended to a confluence of rivers 1,500 feet below. Area weather conditions included low-level thermal activity, wind gusts, and light turbulence, which would have been further exasperated at the accident site due to the surrounding terrain.

The flight instructor and the aft seat passenger were fatally injured on impact; however, the pilot sustained serious injuries and was able to extricate himself from the airplane. However, he eventually succumbed to his injuries before the airplane was discovered. Although the airplane was equipped with a 406-MHz ELT and evidence suggests that it activated during the accident, it had become separated from the airplane’s structure (and thus its antenna) during the impact sequence, which limited its transmission range. As a result, no ELT transmissions were received by search and rescue (SAR) satellites. Had the ELT remained connected to its antenna, it would have effectively transmitted an alert signal, thereby providing SAR personnel with a rapid indication that an accident had occurred. Under such circumstances, the airplane would most likely have been discovered earlier, possibly during daylight hours. The pilot's injuries fell within the "severely" injured category, and analysis of emergency evacuation and trauma treatment resources revealed that with prompt ELT notification, medical response would have been greatly augmented, and he may have survived the accident. Furthermore, although a personal locator device survived the accident intact, it was ejected from the airplane during the accident sequence and was not within easy reach of the pilot.
Probable Cause: The pilot's failure to maintain airplane control during low-level maneuvering flight. Contributing to the pilot’s death was the lack of a timely emergency rescue response due to the lack of effective emergency signal transmissions from both the airplane’s emergency locator transmitter and the personal locator device, which were both ejected from the wreckage.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: WPR12FA184
Status: Investigation completed
Duration: 1 year and 7 months
Download report: Final report

Sources:

NTSB

Location

Revision history:

Date/timeContributorUpdates
26-Apr-2012 11:25 gerard57 Added
26-Apr-2012 17:48 RobertMB Updated [Time, Aircraft type, Registration, Cn, Operator, Location, Source, Narrative]
26-Apr-2012 17:50 RobertMB Updated [Narrative]
10-May-2012 19:13 Geno Updated [Time, Location, Departure airport, Destination airport, Source, Narrative]
10-May-2012 19:16 Geno Updated [Source]
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
27-Nov-2017 20:37 ASN Update Bot Updated [Other fatalities, Departure airport, Destination airport, Source, Narrative]

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org