N9404E

Substantial
None

Aeronca 11BC S/N: 1041

Accident Details

Date
Saturday, August 28, 1999
NTSB Number
CHI99LA318
Location
WATERVLIET, MI
Event ID
20001212X19466
Coordinates
42.179012, -86.250411
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 not maintaining aircraft control during takeoff, and the pilot not correcting for the porpoise.

Aircraft Information

Registration
Make
AERONCA
Serial Number
1041
Engine Type
Reciprocating
Year Built
1946
Model / ICAO
11BC AB11
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
11AC

Registered Owner (Current)

Name
MALONEY EDWARD M
Address
7171 LAKE RD
City
COLOMA
State / Zip Code
MI 49038-9647
Country
United States

Analysis

On August 27, 1999, at 2015 eastern daylight time (edt), an Aeronca 11BC, N9404E, operated by a private pilot sustained substantial damage when on takeoff from runway 02 (2,600 feet by 200 feet, dry grass/turf) at the Watervliet Municipal Airport, Watervliet, Michigan, the airplane bounced, porpoised, and impacted on the runway. Visual meteorological conditions prevailed at the time of the accident. The personal flight was being conducted under 14 CFR Part 91. No flight plan was on file. The pilot and passenger on board the airplane reported no injuries. The local flight was originating at the time of the accident.

In his written statement, the pilot said that during takeoff, the airplane bounced 2-3 times on the runway, and then the landing gear and propeller broke.

The passenger on board the airplane stated that "upon liftoff, the airplane ballooned off of the runway. We came back down and bounced once, kind of porpoised twice, and came back down, and the landing gear collapsed."

A Federal Aviation Administration (FAA) inspector examined the airplane at the Watervliet Municipal Airport. The airplane's main landing gear was folded rearward underneath the airplane's fuselage. Both main gear struts were broken aft from the landing gear box, just behind the airplane's firewall. The lower portion of the firewall was bent aft. The bottom forward fuselage skin was crushed upward. The airplane's wood propeller was broken and splintered. Flight control continuity was confirmed. Examination of the airplane's engine, engine controls, and other airplane systems revealed no anomalies.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CHI99LA318