N224SC

Substantial
Serious

Learjet 24 S/N: 100

Accident Details

Date
Sunday, September 26, 1999
NTSB Number
MIA99FA267
Location
GAINESVILLE, GA
Event ID
20001212X19824
Coordinates
34.290786, -83.829887
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
2
Minor Injuries
3
Uninjured
0
Total Aboard
5

Probable Cause and Findings

The inadequate inspection of the main landing gear brake assemblies, which lead to operation of the aircraft with worn brakes that failed during the landing roll. Contributing factors were the descending terrain, roadway and ditch.

Aircraft Information

Registration
N224SC
Make
LEARJET
Serial Number
100
Engine Type
Turbo-jet
Year Built
1966
Model / ICAO
24 LJ24
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2

Registered Owner (Historical)

Name
DOLPHIN AVIATION INC
Address
8191 N TAMIAMI TRL STE 100
Status
Deregistered
City
SARASOTA
State / Zip Code
FL 34243-2023
Country
United States

Analysis

HISTORY OF FLIGHT

On September 26, 1999, about 0935 eastern daylight time, a Learjet 24, N224SC, registered to Dolphin Aviation, Inc., and operated as a Title 14 CFR Part 91 personal flight, overran runway 29 during landing at Lee Gilmer Memorial Airport, Gainesville, Georgia. Visual meteorological conditions prevailed at the time and an instrument flight rules flight plan was filed. The aircraft received substantial damage. The private-rated pilot and one passenger received serious injuries. The commercial-rated copilot and two passengers received minor injuries. The flight originated from Sarasota, Florida, the same day, about 0826.

The pilot stated that the flight was from Sarasota, Florida, to Gainesville, Georgia. Prior to departure, he performed a standard preflight inspection of the aircraft, which included a visual inspection of both the right and left main gear brakes and wheel well. When they were in visual contact with the Lee Gilmer Memorial Airport, the copilot cancelled the instrument flight rules clearance and called the airport UNICOM for local traffic and advisories. After receiving no response, they heard an aircraft announce departure from runway 29. After checking required runway length, the decision was made to use the active runway 29, because the winds favored this runway. They made a normal stabilized approach to runway 29. The Vref speed was 122 and he aimed for touchdown on the end of the runway, in the vicinity of the numbers. After touchdown he applied the brakes and deployed the spoilers. Shortly after applying the brakes, he felt what seemed like a malfunction in the brake system, at which time the brakes became ineffective and the expected decrease in forward motion did not materialize. The aircraft continued moving down the runway and ran off the end.

The copilot stated that the captain made a normal approach and touchdown to Lee Gilmer Memorial Airport. On rollout, 2,000 feet down the runway, the aircraft appeared to stop slowing down. The brakes appeared to become ineffective. The aircraft continued the landing roll off the departure end of the runway. One hundred feet from the end of the runway is a high ravine leading to a four lane highway and then a ditch, which is where the aircraft came to rest.

The passenger seated on the rear bench seat stated that the airplane seemed to be flying low on the downwind leg. From his vantage point, at the very rear of the aircraft, he had a clear view of everything going on in front of the aircraft. The airplane also appeared to be very low in the base leg and final turn and he could not believe how far up the runway they were prior to touchdown. It became apparent, since the forward speed did not significantly decrease that they were not going to stay on the runway. The airplane left the runway at considerable speed, continued across a highway, and seemed to become airborne again as it came to a violent stop, after striking objects, a utility pole among them.

The passenger seated on the left side of the aircraft just aft of the cabin door stated that the airplane was about 2.5 miles out from the runway at about 1,000 feet on the downwind leg. The airplane was turned onto final approach about 3 miles from the runway. The touchdown was firm and he is positive the airplane touched down about 1/3 down the runway. Touchdown was left main gear first, then right main gear, then nose gear. He looked out the right passenger window and saw the airplane was moving past hangars and airplanes at a very high rate of speed. He briefly remembers the brakes being applied and his father, who was seated on the rear bench seat, stating that they were going off the end of the runway. He observed the intersection with the other runway go by and the runway markers flash by. At this point the copilot told them to hold on , that they were going off the end of the runway, and that there was a hill. He felt a strain on his seat belt and encountered a negative G effect. The airplane then "slammed" onto and crossed a highway. The main landing gear made a loud crack and snapped off as the airplane hit the curb on the far side of the highway. He remembered the crushing and bending noise of the fuselage as the airplane slammed onto the ground and cut down a utility pole with its lines dropping on top of the airplane.

A witness stated he was working at the front desk of the fixed-base operator, located to the west of runway 4-22 and north of runway 11-29. He observed N224SC rolling out after landing on runway 29. The airplane appeared to be traveling at higher than normal speed and shortly thereafter, he saw smoke trailing from both main landing gear. He observed the airplane go off the end of the runway and disappear over a grassy slope, in a cloud of dust.

PERSONNEL INFORMATION

Records from the Federal Aviation Administration, Airman Certification Branch, Oklahoma City, Oklahoma, show the pilot holds a private pilot certificate with airplane single engine land, airplane multiengine land, and instrument airplane ratings, and type ratings for Cessna 500 and Learjet. The certificate was last issued on August 26, 1994, when the Learjet type rating was added. The pilot holds a FAA Class 3 medical certificate, issued on March 12, 1998, with the restriction that the pilot must wear correcting lenses while exercising the privileges of the certificate. The pilot reported on the NTSB Pilot/Operator Aircraft Accident Report that he received a biennial flight review on June 4, 1999, in a Beech Baron. Documents the pilot supplied to NTSB show he received a 12/24 month pilot proficiency check in the Learjet on February 18, 1999. The pilot reported he has 4,800 total flight hours, with 600 flight hours in the Learjet. He reported he flew 22 total flight hours in the last 90 days, and 8 total flight hours in the last 30 days, all in the Learjet.

Records from the Federal Aviation Administration, Airman Certification Branch, Oklahoma City, Oklahoma, show the copilot holds a commercial pilot certificate with airplane single engine land, airplane multiengine land, airplane single engine sea, and instrument airplane ratings, and a type rating for Learjet. The certificate was last issued on October 3, 1993, when the Learjet type rating was added. The copilot holds a FAA Class 2 medical certificate, issued on September 22, 1999, with the restriction that the pilot must wear correcting lenses while exercising the privileges of the certificate. Documents the copilot supplied to NTSB show he received a biennial flight review and instrument proficiency check on May 2, 1999, and he completed a second in command proficiency check in the Learjet model 25B on June 6, 1999. The copilot reported he has 6,675 total flight hours, with 675 flight hours in the Learjet. He reported he flew 0 total flight hours in the last 90 days and last 30 days. AIRCRAFT INFORMATION

The aircraft was a Learjet model 24, serial number 100. Records show that at the time of the accident the aircraft had accumulated 12,868 total flight hours and 12,805 cycles. The aircraft was last inspected on September 24, 1999, 1 flight hour before the accident. This inspection was a Phase A-1 through A-6, 300 hour inspection. Phase A-5 calls for inspection of the landing gear brake assemblies for wear, cracks, hydraulic leaks, and release. This item on the inspection was signed off by a mechanic on September 20, 1999. The item was not signed off by an inspector.

At the time of the accident the aircraft was displaying FAA registration number N224SC. Documents in the aircraft showed this registration number was assigned to the aircraft on March 11, 1999, and the FAA Certificate of Aircraft Registration reflected this registration number. The FAA Standard Airworthiness Certificate, last issued on April 1, 1998, reflected the previous FAA registration number, N427LJ.

METEOROLOGICAL INFORMATION

The Lee Gilmer Memorial Airport, 0953 surface weather observation was clear skies, visibility 10 sm, temperature 68 degrees F, dew point temperature 61 degrees F, wind from 060 degrees at 7 knots, altimeter setting 30.18.

FLIGHT RECORDERS

The aircraft was not equipped with a flight data recorder or a cockpit voice recorder. Title 14 CFR Part 91.609(e), states "Unless otherwise authorized by the Administrator, after October 11, 1991, no person may operate a U.S. Civil registered multiengine, turbine-powered airplane or rotorcraft having a passenger seating configuration of six passengers or more and for which two pilots are required by type certification or operating rule unless it is equipped with an approved cockpit voice recorder...." N224SC was equipped with two individual passenger seats, a potty seat, and a rear bench seat that had seat belts for three passengers, for a total passenger seating capacity of six seats.

WRECKAGE AND IMPACT INFORMATION

The airplane landed on runway 29 and overran the departure end of the runway. After over running the runway, the airplane traveled down an embankment, crossed over 4 lane Aviation Boulevard, and came to rest in a drainage ditch. The GPS position at the point the airplane came to rest was 34 degrees, 16.435 north latitude and 83 degrees, 50.124 west longitude. Elevation at the point the aircraft came to rest was about 1,250 feet, based on the captain's altimeter.

Examination of runway 29 showed that about 1,500 feet from the arrival end, marks are visible from heavy braking of the outboard right main tire and inboard left main tire of N224SC. At 3,000 feet from the arrival end, marks are visible showing the outboard right main tire had gone flat and marks are visible from the other three main tires. The marks continue down the runway and about 500 feet from the departure end of runway 29, the tire marks veer to the left and continue until they go off the runway surface at the left edge of the runway at the end. The marks continue through the grass until the airpl...

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA99FA267