Loss of control Accident Cessna 177B N34508,
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ASN Wikibase Occurrence # 286870
 
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Date:Tuesday 23 June 2009
Time:18:00 LT
Type:Silhouette image of generic C177 model; specific model in this crash may look slightly different    
Cessna 177B
Owner/operator:
Registration: N34508
MSN: 17701847
Total airframe hrs:1791 hours
Engine model:Lycoming O-360-A1F6
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Elyria, Ohio -   United States of America
Phase: Landing
Nature:Training
Departure airport:Elyria, OH (1G1)
Destination airport:Elyria, OH (1G1)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The accident occurred during the student pilot's second landing on her first solo flight. She stated that the airplane began to porpoise immediately after the nose landing gear touched down. The airplane completed several porpoise cycles before she decided to abort the landing. After increasing engine power and becoming airborne, the airplane began to veer left toward some trees situated alongside the runway. To correct for the left veer, she applied right rudder and, in an attempt to decrease drag, reduced the flap setting from 20 to 10 degrees. The airplane stalled during a right turn, about 20 to 30 feet above the ground, and entered a nose-down attitude. She was able to level the airplane before it landed hard on all three landing gear off the left side of the runway. The engine firewall and fuselage were substantially damaged during the event. The student pilot stated that asymmetric loading of the propeller (P-Factor) caused the airplane to veer left after she increased engine power for the aborted landing. She noted that she had not received flight instruction demonstrating the airplane's flight characteristics while in ground effect at airspeeds at or near stall speed.

Probable Cause: The student pilot's failure to maintain aircraft control and adequate airspeed during the aborted landing, which resulted in an aerodynamic stall at a low altitude.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN09CA381
Status: Investigation completed
Duration: 4 months
Download report: Final report

Sources:

NTSB CEN09CA381

Location

Revision history:

Date/timeContributorUpdates
03-Oct-2022 17:20 ASN Update Bot Added

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