N26387

Substantial
None

GRUMMAN AMERICAN AVN. CORP. AA5AS/N: AA5A0555

Accident Details

Date
Tuesday, July 4, 2023
NTSB Number
ERA23LA286
Location
Redstone Arsenal, AL
Event ID
20230705192517
Coordinates
34.610070, -86.667690
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
2
Total Aboard
2

Probable Cause and Findings

The separation of the clamp assembly securing the throttle control cable outer housing, which resulted in the pilot’s inability to control the throttle.

Aircraft Information

Registration
Make
GRUMMAN AMERICAN AVN. CORP.
Serial Number
AA5A0555
Engine Type
Reciprocating
Year Built
1978
Model / ICAO
AA5AAA5
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
AA-5A

Registered Owner (Current)

Name
MASCO HOWARD N
Address
807 TANNAHILL DR SE
City
HUNTSVILLE
State / Zip Code
AL 35802-1935
Country
United States

Analysis

On July 4, 2023, about 1407 central daylight time, a Grumman American Aviation AA-5A, N26387, was substantially damaged when it was involved in an accident near Redstone Arsenal, Alabama. The private pilot and pilot-rated passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot stated that earlier that day he departed from the airplane’s home base, flew to Huntsville International Airport, Huntsville, Alabama, performed a RNAV approach, and then climbed to 3,500 ft mean sea level. While at that altitude en route to Guntersville Municipal Airport – Joe Starnes Field, Guntersville, Alabama, and while adjusting the engine power settings, the engine power decreased. He further described that the engine power was at high idle and would not respond to throttle control inputs. At that time, he declared an emergency and descended at slightly above best glide airspeed in an attempt to land at Redstone Arsenal, which he believed was the nearest airfield. When it was apparent that the airplane would be unable to reach the runway, he selected a nearby field with a paved road. After landing on the road, he applied maximum braking; however, the left wing impacted a metal pole, resulting in damage to the leading edge of the wing measuring 39 inches; the total wingspan was 31 ft 6 inches.

Postaccident inspection of the engine compartment by an FAA inspector revealed the throttle control cable assembly remained attached to the throttle control lever of the fuel injection servo, but the outer cable assembly was not secured in the engine compartment. Thus, movement of the throttle control in the cockpit did not result in movement of the throttle control lever. A clamp, shim, two screws, and two metal self-locking nuts that secured the outer cable assembly were not located, but a washer was found loose in the engine compartment.

A review of the maintenance records revealed the throttle cable was replaced at the airplane’s last annual inspection, which was completed on November 13, 2022. The airplane had been operated for about 15 hours since the annual inspection was completed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA23LA286