Runway excursion Accident Cessna TR182 Turbo Skylane RG N5JB,
ASN logo
ASN Wikibase Occurrence # 226701
 
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:Sunday 30 June 2019
Time:10:00 LT
Type:Silhouette image of generic C82R model; specific model in this crash may look slightly different    
Cessna TR182 Turbo Skylane RG
Owner/operator:Private
Registration: N5JB
MSN: R18201283
Year of manufacture:1979
Total airframe hrs:2767 hours
Engine model:Lycoming O-540
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Lincoln Airport (S69), Lincoln, MT -   United States of America
Phase: Landing
Nature:Private
Departure airport:Deer Lodge, MT (38S)
Destination airport:Lincoln, MT (S69)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot was landing the airplane in gusting wind conditions with the wing flaps extended to 40°. During the landing flare, the airplane encountered a gust and the pilot applied full engine power for a go-around; however, the airplane 'did not respond' and the pilot then chose to land on the remaining runway. The airplane landed hard and bounced, resulting in a nose landing gear collapse and a runway excursion.
The wing flaps were found extended to about 35° following the accident, and the flap selector was in the fully extended (40°) position. The airplane's pilot operating handbook (POH) stated that a flap setting less than 40° would improve airplane handling characteristics in gusting wind conditions. Additionally, the POH procedure for a go-around stated that the wing flaps should be retracted to 20° after applying engine power. It is likely that the airplane did not climb during the attempted go-around due to the pilot's failure to retract the wing flaps; however, the airplane was not examined after the accident and whether a mechanical anomaly contributed could not be determined. Similarly, whether there were any mechanical malfunctions or anomalies that contributed to the loss of control following the bounced landing could not be determined.

Probable Cause: A loss of control during landing, which resulted in a nose landing gear collapse and runway excursion.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: WPR19LA184
Status: Investigation completed
Duration: 2 years and 9 months
Download report: Final report

Sources:

NTSB WPR19LA184
FAA register: https://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=5JB

Location

Revision history:

Date/timeContributorUpdates
30-Jun-2019 23:18 Geno Added
01-Jul-2019 02:49 RobertMB Updated [Aircraft type, Phase, Nature, Destination airport, Narrative]
01-Jul-2019 18:02 TG Updated [Source]
02-Jul-2019 15:39 Geno Updated [Aircraft type, Registration, Cn, Operator, Source, Narrative]
04-Jul-2019 17:49 RobertMB Updated [Aircraft type]
02-Jul-2022 07:26 ASN Update Bot Updated [Time, Other fatalities, Departure airport, Destination airport, Source, Narrative, Category, Accident report]

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