NYC05LA009

NTSB accident investigation · Beech BE-200 · Dulles, VA · October 26, 2004

Accident · No injuriesLimited investigationFinal report
Date
October 26, 2004, 09:43 local (13:43 UTC)
Place
Dulles, VA
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N888TRBeech BE-200
Weather
Visual (VMC)
Status
Completed · report July 31, 2006
Report
Approved by Office Director
Parties
FAA/FSDO
FAA report
20041026031219A
Case key
60436

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 improper in-flight decision to continue the instrument approach and landing, which resulted in a collision with a sign. A factor was the below instrument approach landing minimum weather conditions.

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.

In flight collision with objectMissed approach (ifr)
Object - sign
In-flight planning/decision - improperPilot in commandCause
Weather condition - below approach/landing minimumsFactor
Gear collapsedLanding - roll

Analysis

The pilot approached the destination airport and entered a holding pattern to wait for the weather to improve. After about 20 minutes, the weather seemed to improve, and because the pilot could occasionally see the ground, he decided to conduct an instrument approach. About 50 feet above decision height, the pilot had the runway environment in sight, and estimated the in-flight visibility was about 1/2 mile. During the landing, the pilot lost all forward visibility and executed a missed approach, but before a positive rate of climb could be established, the airplane touched down left of the runway on grass, and the left main landing gear struck a taxiway sign. About 10 feet past the sign, the airplane became airborne, and the pilot continued the missed approach. The pilot then diverted to an alternate airport, and during the landing the left main landing gear collapsed, resulting in substantial damage. The automated surface observation system and a witness both reported that the weather at the time of the accident was below the minimums prescribed in the instrument approach procedure.

Factual narrative

On October 26, 2004, at 0943 eastern daylight time, a Beech BE-200, N888TR, was substantially damaged during landing at the Washington Dulles International Airport (IAD), Dulles, Virginia. The certificated airline transport pilot and the two passengers were not injured. Day instrument meteorological conditions prevailed for the business flight that departed Piedmont Triad International Airport (GSO), Greensboro, North Carolina, destined for Eastern WV Regional Airport (MRB), Martinsburg, West Virginia. An instrument flight rules (IFR) flight plan was filed for the flight conducted under 14 CFR Part 91.

According to the pilot, after departing Greensboro, the flight progressed without incident until reaching the Martinsburg area. He then completed several holding circuits to allow the weather to improve. While holding, the pilot checked the automated surface observing system, which reported 1/4 mile visibility in fog, and 100 feet of vertical visibility. After about 20 minutes, the weather seemed to improve, and because the pilot could occasionally see the ground, he requested an approach clearance.

The flight was subsequently cleared for the ILS RWY 26 approach. About 50 feet above the decision height, the pilot had the runway environment in sight, and reported that the in-flight visibility was about 1/2-mile. He then maneuvered the airplane, and initiated a flare for landing; however, prior to touching down, the pilot lost all forward visibility and initiated a missed approach. He advanced the power levers, and as the engines responded, he felt the airplane contact "something." The airplane continued to accelerate and climb, but when the pilot selected the landing gear handle to the up position, only the nose wheel and right main landing gear indicators indicated gear up, while the left main landing gear remained in a transient condition.

The pilot declared a missed approach and diverted to Dulles. There, he executed a "low-pass" so the tower controller could inspect the landing gear. The controller advised the pilot that it appeared the left landing gear was damaged, and issued a landing clearance. The airplane touched down on runway 1 and began to roll-out, but at approximately 40 knots, the left main landing gear collapsed. The airplane skidded to a stop on the runway, and the pilot, along with the passengers, exited without further incident.

According to a Federal Aviation Administration inspector, examination of the wreckage revealed damage to the left engine firewall and forward pressure bulkhead.

A weather observation taken about 13 minutes before the accident at the Martinsburg Airport recorded the wind as calm, visibility 1/4 mile in fog, vertical visibility 100 feet, temperature 45 degrees Fahrenheit, dew point 45 degrees Fahrenheit, and an altimeter setting of 30.22 inches of mercury.

A witness, who was holding short of runway 26 in a vehicle at Martinsburg, stated that after the pilot of the accident airplane declared a missed approach, he was cleared by the control tower to conduct a runway sweep. During the sweep, forward visibility was limited to "two to three runway lights," which equated to between 400 and 600 feet. About halfway down the runway, the witness found debris from a taxiway sign and various aircraft parts. Because of poor visibility, he could not see the source of the debris, so he parked his vehicle and began to search on foot. He found that a taxiway sign on the left side of the runway had been struck, and there were three tire marks in the grass that paralleled the runway. The marks were approximately 100 feet long, and ended approximately 10 feet past the base of the sign. In addition, the left and center tire marks transitioned over the 6-inch high concrete base the sign was mounted on.

According to the instrument approach procedure for the ILS RWY 26 approach at Martinsburg Airport, decision height was 200 feet agl, and required visibility was at least 1/2 mile.

Aircraft

Registration
N888TR
Reported as
Beech BE-200
Category
Airplane
Engines
Pratt & Whitney PT6A-41, 850 horsepower, turbo propPratt & Whitney PT6A-41, 850 horsepower, turbo prop
Damage
Substantial damage
Flight
Business · Part 91
Operator
Twin County Aviation LLC
Registered owner
Twin County Aviation LLC
Airworthiness certificate
Standard, Normal
Departed
GSO · Greensboro, NC
Destination
MRB · Martinsburg, WV
Flight plan
IFR
Airport
IAD · Washington Dulles Internationa, runway 010, 11,500 × 150 ft, concrete

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
55
Injuries
None
Certificates
Airline transport, Commercial, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
September 1, 2004
Seat
Left
Flight hours
3,630 total · 120 in this make and model · 3,092 as pilot in command · 108 in the last 90 days · 10 in the last 30 days

Weather

Conditions
Visual (VMC)
Wind
340° at 4 knots
Visibility
6 statute miles
Lowest ceiling
250 ft broken
Temperature
55 °F, dew point 50 °F
Altimeter
30.20 inHg
Observed at
IAD

FAA reports on this event · 1

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