N8115V

Substantial
None

Grumman S2F-1 S/N: 144725

Accident Details

Date
Thursday, September 24, 1998
NTSB Number
ANC98LA164
Location
WASILLA, AK
Event ID
20001211X10994
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the recently overhauled right brake seal resulting in a total loss of brake fluid, failure of the right brake system, and subsequent inability of the pilot to utilize the brake. A contributing factor was the soft terrain.

Aircraft Information

Registration
N8115V
Make
GRUMMAN
Serial Number
144725
Engine Type
Reciprocating
Model / ICAO
S2F-1 G21
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
GENERAL AVIATION SYSTEM ACFT SLS INC
Address
1575 W COMMERCIAL BLVD HANGAR 35A
Status
Deregistered
City
FT LAUDERDALE
State / Zip Code
FL 33309
Country
United States

Analysis

On September 24, 1998, about 1240 Alaska daylight time, a Grumman S2F-1 airplane, N8115V, sustained substantial damage when it departed runway 21 during landing at the New Wasilla airport, Wasilla, Alaska. The solo airline transport pilot was not injured. The airplane was owned and operated by the pilot under 14 CFR Part 91 as a local, personal flight. The airplane was being operated under an FAA letter of authorization, leading to an experimental category airworthiness certificate. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed.

The pilot told the NTSB investigator-in-charge during a telephone interview on September 29, and wrote in his NTSB Pilot / Operator report, that during landing the right brake failed and the airplane began to drift to the left. The pilot said that soft earth on the left side of the runway compounded the left drift, and that differential power did not swing the nose of the airplane back to the right. The airplane departed the left side of the 3,700 feet long by 75 feet wide gravel runway, and the nose landing gear collapsed.

Subsequent inspection of the airplane by an FAA Flight Standards District Office inspector revealed that the right brake seal failed, releasing the hydraulic fluid. A review of records showed that the right main landing gear had been overhauled, and the right brake seal replaced on June 8, 1998, at 7,363 airframe total hours, 15 hours prior to the accident. A review of work orders submitted by the overhaul facility listed the following repairs (in part):

Remove R/H Wheel & Repair Leak 1.8 hours Overhaul Brakes 3.3 hours Install Tire & Set Brakes 0.8 hours Install R/H Brake 2.2 hours Install Brakes 4.3 hours

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ANC98LA164