FTW99LA198

NTSB accident investigation · Boeing A75L3 · Fort Worth, TX · July 23, 1999

Accident · Minor injuriesLimited investigationFinal report
Date
July 23, 1999, 11:15 local (16:15 UTC)
Place
Fort Worth, TX
Injuries
1 minor, 2 uninjured; on the ground: 1 minor
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N59646Boeing A75L3
Weather
Visual (VMC) · Day
Status
Completed · report June 23, 2000
Report
Approved by Office Director
FAA report
19990723009629A
Case key
46854

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 loss of engine power for an undetermined reason. A factor was the lack of suitable terrain for the forced landing.

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 engine powerTakeoff - initial climb
Reason for occurrence undeterminedCause
Forced landingEmergency landing after takeoff
On ground/water collision with objectEmergency landing after takeoff
Object - vehicle
On ground/water encounter with terrain/waterEmergency landing after takeoff
Terrain condition - rough/uneven
Terrain condition - none suitableFactor

Analysis

The airplane impacted a golf cart and terrain during a forced landing following a loss of engine power during the initial takeoff climb. The commercial pilot reported that a 'slow gradual loss of engine power' occurred shortly after takeoff, and he initiated a forced landing to a golf course fairway. The airplane touched down approximately 150 feet short of the fairway, impacted a moving golf cart, struck a curb, nosed over, and came to rest inverted on the fairway. Examination of the fuel system and engine did not reveal the reason for the loss of engine power.

Factual narrative

On July 23, 1999, at 1115 central daylight time, a Boeing A75L3 airplane, N59646, was substantially damaged when it impacted a golf cart and terrain during a forced landing following a loss of engine power during the initial takeoff climb from Spinks Airport, Fort Worth, Texas. The two occupants, a commercial pilot and a private pilot, were not injured, and the driver of the golf cart sustained minor injuries. No flight plan was filed and visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 91 personal flight. The flight's intended destination was the Arlington Municipal Airport in Arlington, Texas.

During interviews conducted by an FAA inspector and in written statements submitted to the NTSB, the two pilots reported that they made a series of touch-and-go landings at Spinks Airport, refueled the airplane with 19.3 gallons of 100LL aviation fuel, and then performed several more touch-and-go landings. A decision was made by the pilots to return to the Arlington Municipal Airport. The private pilot, who was occupying the rear seat, performed the takeoff with the smoke system on. The airplane "started to gradually lose power." When the airplane reached an altitude of 50 to 100 feet agl, the private pilot turned left to an easterly heading. The commercial pilot noticed that the airplane was not climbing and used hand signals to communicate his observation to the private pilot. The private pilot then transferred control of the airplane to the commercial pilot. The "slow gradual loss of engine power" continued, and the commercial pilot initiated a forced landing to a fairway of the Southern Oaks Golf Course. The airplane touched down approximately 150 feet short of the fairway, impacted a moving golf cart, struck a curb, nosed over, and came to rest inverted on the fairway.

According to the FAA inspector, who responded to the accident site, the main landing gear separated, and the upper and lower right wings sustained structural damage.

On November 5, 1999, under the supervision of the NTSB investigator-in-charge, the Lycoming R680 engine and the airframe fuel system were examined at the facilities of Air Salvage of Dallas, Lancaster, Texas. The fuel tank was found to be approximately 1/2 full with blue colored fuel. No water was noted in a fuel sample drained from the tank. The fuel vent line was unobstructed, and fuel flowed freely from the tank to the main fuel strainer mounted on the firewall. Disassembly of the carburetor revealed that the inlet screen and bowl were free of debris, the float and needle valve assembly moved freely, and the venturi was coated with carbon deposits.

Engine continuity was confirmed to all cylinders and to the magnetos by manually rotating the propeller. Thumb compression was verified on all cylinders except cylinder #1. Cylinder #1 was removed, and carbon particles were found between the intake valve head and the valve seat. Examination of the intake system supplying fresh air to the carburetor revealed no obstructions to airflow. Examination of the intake system supplying heated air to the carburetor revealed the presence of a 1-inch by 3-inch piece of sheet metal in the plenum. It was noted that a screen covering the base of the carburetor would have prevented this piece of metal from entering the venturi. Additionally, it was noted that when the piece of metal was positioned on the screen, it covered approximately one-third of the screen.

Aircraft

Registration
N59646
Reported as
Boeing A75L3
Category
Airplane
Serial number
75-1732
Engine
Lycoming R680, 225 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Robert R. Robinson
Airworthiness certificate
Standard, Normal
Last inspection
Annual · July 2, 1998
Departed
FWS
Destination
GKY · Arlington, TX
Airport
FWS · Fort Worth Spinks

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
26
Certificates
Flight instructor, Commercial
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Seat
Front
Flight hours
2,008 total · 8 in this make and model · 1,786 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
190° at 10 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
84 °F

FAA reports on this event · 1

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