N9430J

Substantial
Minor

PIPER PA-28-180S/N: 28-3541

Accident Details

Date
Tuesday, September 6, 2011
NTSB Number
CEN11CA678
Location
Buena Vista, CO
Event ID
20110930X40215
Coordinates
38.813610, -106.123336
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
2
Total Aboard
3

Probable Cause and Findings

The airplane’s diminished climb performance due to the pilot not leaning the engine mixture enough prior to takeoff in high density altitude conditions and at nearly maximum gross takeoff weight.

Aircraft Information

Registration
N9430J
Make
PIPER
Serial Number
28-3541
Engine Type
Reciprocating
Year Built
1966
Model / ICAO
PA-28-180P28A
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
635 AIRPORT RD
Status
Deregistered
City
GREELEY
State / Zip Code
CO 80631-9148
Country
United States

Analysis

The pilot reported that he rolled down the runway for takeoff a little over 60 knots. He stated that just after liftoff, the airplane was initially sluggish to climb so he lowered the nose to gain more speed in ground effect (about 70 knots). The airplane started to gain some altitude, so the pilot continued his departure. Shortly after clearing the end of the runway, there was a loss of power and climb performance. With trees and houses ahead and insufficient altitude to clear them, the pilot decided to land in a field with deep grass just north of the airport. Upon landing in the field the nose landing gear collapsed resulting in substantial damage to the front of the fuselage. The pilot and both passengers exited the airplane without significant injuries.

After the accident the pilot said he believed that he may not have leaned the engine enough during run up resulting in less than 100 percent available power for the climbout. He also reported that the spark plugs may have been fowled due to the mixture setting resulting in the loss of available power immediately after takeoff. The pilot stated that the airplane was loaded to within 65 pounds of its maximum gross weight and with a calculated density altitude of 10,400 feet, the anticipated climb rate of 300 feet per minute required full power as outlined in the Pilot Operating Handbook. He stated that if there was not deep grass in the landing field, he could have landed the airplane without incident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN11CA678