N2824R

Substantial
Minor

Socata TB9S/N: 1153

Accident Details

Date
Tuesday, September 17, 2019
NTSB Number
ERA19LA274
Location
Fort Meade, MD
Event ID
20190917X91309
Coordinates
39.083889, -76.762222
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
1
Total Aboard
2

Probable Cause and Findings

The failure of the carburetor intake scat tubing, which resulted in a partial loss of engine power.

Aircraft Information

Registration
N2824R
Make
SOCATA
Serial Number
1153
Engine Type
Reciprocating
Model / ICAO
TB9TAMP
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
1WORLD AERO LLC
Address
8408 HARTFORD AVE
Status
Deregistered
City
SILVER SPRING
State / Zip Code
MD 20910-5310
Country
United States

Analysis

On September 17, 2019, about 1800 eastern daylight time, a Socata Tampico TB9C, N2824R, was substantially damaged when it was involved in an accident near Fort Meade, Maryland. The flight instructor was not injured and the student pilot received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

According to the instructor, the purpose of the flight was to conduct practice takeoffs and landings. After a preflight inspection and normal engine run-up, they took off, remaining in the airport traffic pattern. While on the downwind leg, the student completed the before-landing checklist. The flight instructor noted that the engine rpm was low and applied additional power; however, engine power continued to decay. The instructor took the controls from the student and turned base toward runway 10. He switched fuel tanks and turned off the carburetor heat in an attempt to regain engine power, which had no effect. The airplane descended into the trees under partial power and came to rest in the treetops about 75 ft above the ground, resulting in substantial damage to both wings.

The engine sparkplugs were removed; the top electrodes were gray in color and exhibited normal wear signatures. The bottom plugs were darker than the top sparkplugs and were oil-soaked. The wires to the Nos. 1 and 3 cylinder top spark plugs were broken, but produced spark when the engine was manually rotated. All other sparkplug wires produced spark when the engine was rotated. Valve train continuity was established, and compression was observed on all cylinders during engine rotation. An undetermined amount of oil was observed in the sump. The carburetor was clear of debris. The intake scat tubing was found crushed on the airframe side. The airframe scat tubing fiberglass connection side was also found crushed. Examination of the interior of the scat tubing found the inner layer of the tubing collapsed. An examination of the engine did not reveal any anomalies that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA19LA274