N4787VBOEING E752009-05-17 NTSB Accident Report

Substantial
None

BOEING E75S/N: 75-5814

Summary

On May 17, 2009, a Boeing E75 (N4787V) was involved in an incident near Cottonwood, AZ. All 2 people aboard were uninjured. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this incident to be: The pilot's inadequate compensation for the crosswinds during the landing roll.

The pilot of the tailwheel-equipped airplane stated that during the landing roll the airplane began to drift to the left. The pilot applied right rudder and right aileron, and the airplane then encountered a gust of wind from the right. The left wing then struck the runway surface and the airplane departed the runway to the right, coming to rest in soft soil. The airplane sustained substantial damage to the lower wing spar during the accident sequence. The pilot reported that the airplane and engine had no mechanical failures or malfunctions prior to the accident.

This incident is documented in NTSB report WPR09CA265. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N4787V.

Accident Details

Date
Sunday, May 17, 2009
NTSB Number
WPR09CA265
Location
Cottonwood, AZ
Event ID
20090526X40613
Coordinates
34.729999, -112.035278
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The pilot's inadequate compensation for the crosswinds during the landing roll.

Aircraft Information

Registration
Make
BOEING
Serial Number
75-5814
Engine Type
Reciprocating
Year Built
1941
Model / ICAO
E75B752
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
E75

Registered Owner (Current)

Name
GOLD CAP LLC
Address
4871 AVIATOR LN NW
City
BREMERTON
State / Zip Code
WA 98312-9573
Country
United States

Analysis

The pilot of the tailwheel-equipped airplane stated that during the landing roll the airplane began to drift to the left. The pilot applied right rudder and right aileron, and the airplane then encountered a gust of wind from the right. The left wing then struck the runway surface and the airplane departed the runway to the right, coming to rest in soft soil. The airplane sustained substantial damage to the lower wing spar during the accident sequence. The pilot reported that the airplane and engine had no mechanical failures or malfunctions prior to the accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR09CA265