ATL95LA019

NTSB accident investigation · Weeks Glasair SH2F · Timmonsville, SC · November 27, 1994

Accident · FatalLimited investigationFinal report
Date
November 27, 1994, 11:10 local (16:10 UTC)
Place
Timmonsville, SC
Injuries
2 fatal
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N169DWWeeks Glasair SH2F
Weather
Instrument (IMC) · Day
Status
Completed · report May 18, 1995
Report
Approved by Office Director
FAA report
19941127039199A
Case key
3500

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The pilot's continued operation into known adverse weather conditions with a known aircraft deficiency, and his ensuing spatial disorientation, which resulted in ground impact during an uncontrolled descent.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - in flightManeuvering
Vacuum system - failure,totalCause
Operation with known deficiencies in equipment - continuedPilot in commandCause
Flight into known adverse weather - continuedPilot in commandCause
Spatial disorientationPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

A couple made a cross country flight to visit friends who were in another state. The husband had a private certificate with an instrument rating, and his wife had a private certificate. Both had an airplane single engine land rating. During the flight the vacuum pump failed, and it was not repaired during the visit. Following the weekend visit, they were returning home. Prior to departing, the husband obtained a weather briefing for a VFR flight. VFR was not recommended by the fss specialist because of forecasted instrument conditions at the destination airport, at the expected arrival time. The flight departed VFR, and when near the destination requested an IFR clarence for an approach. The husband made the radio calls to air traffic control, and stated that they were between cloud layers. After initiating the first vector for the instrument approach, the pilot reported that the 'gyros' had been lost. Shortly afterwards, the airplane disappeared from radar and radio contact. It impacted, out of control, into a densely wooded area.

Factual narrative

On November 27, 1994, about 1110 eastern standard time, a Weeks Stoddard-Hamilton SH2F Glasair, homebuilt airplane, N169DW, collided with the ground at Timmonsville, South Carolina. The airplane was operated by the pilots under 14 CFR Part 91, and visual flight rules (VFR). Instrument meteorological conditions prevailed. An instrument flight rules flight plan was filed for the personal flight. There were two pilots on the airplane, husband and wife. The husband had a private pilot certificate with airplane single engine and instrument ratings. His medical certificate had been denied in 1985 for cardiovascular disease. The wife had a private pilot certificate with airplane single engine land rating. Both pilots were fatally injured, and the airplane was destroyed. Origination of the flight was Melbourne, Florida about 0845 on the same day.

Prior to departing Melbourne, a male who identified himself as the pilot of N169DW, contacted the St. Petersburg, Florida, Automated Flight Service Station. The person received a weather briefing for a VFR flight to Florence, South Carolina. VFR flight was not recommended. Instrument meteorological conditions were forecasted for Florence, at the pilot's stated approximate arrival time.

At 1104, N169DW contacted Florence, South Carolina, approach control. A certified re-recording of the communications between the airplane and Florence air traffic control revealed that a male conducted the radio transmissions from the airplane. He stated that he was in visual conditions between cloud layers. Vectors to Florence for the instrument landing system approach were requested. A clearance was provided for vectors to Florence, for the instrument landing system runway 9 approach. As the airplane was being vectored, the pilot stated that the "gyro" was out. According to one of the controller's statements, the airplane appeared to be in a descent following this transmission. The radar target data tag indicated 400 feet, two seconds later 1400 feet, then "CST" (coast) mode. Radar contact was lost, and the disintegrated wreckage was later located by local law enforcement officers, about one mile north of the Huggins Memorial Airport, Timmonsville, South Carolina.

Pilot certification information for both pilots was obtained from the Federal Aviation Administration. Mr. Weeks received his private pilot certificate, with an airplane single engine land rating, on September 22, 1974. He was issued an instrument airplane rating on July 17, 1977. A total of 369.6 pilot-in-command flight hours was listed on his application for the instrument rating. A pilot log was not located, and his total flight hours could not be determined. According to an "Order Assessing Civil Penalty," contained in the certification information, Mr. Weeks was denied a medical certificate in 1985 because of having suffered a heart attack. A Repairman Certificate as an Experimental Aircraft Builder was issued to Mr. Weeks on February 14, 1992, for N169DW. Mrs. Weeks obtained a private certificate with an airplane single engine land rating on August 24, 1985. She listed 108.1 total flight hours on the certificate application. Her pilot log was not located, and her total flight hours could not be determined.

A statement was obtained from a friend of the pilots. The friend indicated that the Weeks had visited with he and his wife, on November 22 and 23, in Titusville, Florida. They visited with another couple in Melbourne, Florida, afterwards, leaving Melbourne about 0845 on November 27, 1994. According to the statement, the airplane's vacuum pump had failed on the trip from South Carolina to Florida, and was not repaired prior to departing Melbourne. According to aircraft records, Mr. Weeks purchased the engine on February 7, 1984. The engine log indicated that the overhauled vacuum pump was installed by Mr. Weeks on November 20, 1985. The engine was installed in N169DW on August 2, 1991. Total hours of operation by the vacuum pump could not be determined. Visual examination of the pump revealed that the internal vanes were intact, a portion of the rotor was broken off, and the engine to vacuum pump shear-connection was separated. There was no carbon powder inside the vacuum pump. The pump side of the shear-connection exhibited melted material and rotational scoring. The aircraft log listed the total hours as 109, as of May 12, 1994. the engine log listed 127.7 hours since major overhaul as of September 4, 1994.

Post mortem examinations of the pilots were conducted by the Medical University of South Carolina, Charleston, South Carolina. The cause of death was listed as multiple trauma. Mr. Weeks was found to have severe atherosclerosis of the aortic arch. Toxicological examinations were completed by the Armed Forces Institute of Pathology. Those examinations produced negative results for ethanol and other drugs.

Aircraft

Registration
N169DW
Reported as
Weeks Glasair SH2F (GLASAIR SH)
Category
Airplane, amateur-built
Serial number
169
Engine
Lycoming O-320-E2D, 160 horsepower, reciprocating
Damage
Destroyed
Flight
Personal · Part 91
Operator
Weeks, William D. & Norma, J.
Registered owner
Weeks, W.D.; Weeks, N.J.;Tart,
Airworthiness certificate
Special, Experimental (Special)
Last inspection
100 hour · May 12, 1994
Departed
MLB · Melbourne, FL
Destination
FLO · Florence, SC
Flight plan
IFR

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
65
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Toxicology
Performed
Flight hours
370 total

Weather

Conditions
Instrument (IMC) · Day
Wind
110° at 10 knots
Visibility
2 statute miles
Lowest ceiling
300 ft overcast
Temperature
48 °F, dew point 48 °F
Altimeter
30.00 inHg
Observed at
FLO, 10 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.

Other investigations on N169DW · 1

Matched to the same aircraft by N-number and date.