20030718036109A

Accident · Substantial damage

FAA accident report · Beech 35-A33 · Fort Worth, TX · July 18, 2003

Date
July 18, 2003 · 15:15 local
Place
Fort Worth, TX
Airport
Hicks Airfield Airport
Phase of flight
Go Round (Aborted VFR)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N44CN
NTSB investigation
NTSBFTW03LA189
Reported as
Beech 35A33
Reported engine
Continental IO470*
Fatal injuries
0

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Inspector's statement: on July 18, 2003 I investigated an accident involving the operation of a Beech 35-A33 single-engine airplane, N44CN. The aircraft was operated by roger latham and had three passengers onboard. The following information was obtained during interviews with Mr. Latham and two of the passengers. The aircraft departed nacogdoches, Texas enroute to Hicks airport in Fort Worth, Texas on a 14 CFR 91 pleasure flight with four occupants onboard. Soon after departing nacogcoches, Mr. Latham began to experience radio problems. The flight continued to Hicks airport where Mr. Latham intended to land. During the approach to Hicks, the flaps were extended, however when the gear was selected in the down position the landing gear failed to extend. Mr. Latham recognized the unsafe gear condition and attempted a go-around. When power was appled, the engine sputtered and would not develop adequate power to continue flight. The aircraft settled to the ground north west of the runway between the railroad tracks. The aircraft was substantially damaged, three occupants received minor injuries, and one received serious injuries. During the investigation of the aircraft on site, it was noted that the landing gear was still retracted, the flaps were extended, and the mixture control was not in a full rich position. Many of the switches were in the off position, including the alternator field switch, however it was not possible to determine the position of these switches at the time of the accident. With the aircraft lifted and a jump battery connected, the landing gear extended normally. A specific gravity test was conducted on the battery removed from the aircraft and it was determined that the battery lacked adequate charge to operate the electric landing gear motor. The alternator was removed and tested for proper operation with no discrepancies noted. The weather at the time of the accident was 10-statue miles visibility, few clouds at 7500 feet, and temperature was 37 c. privacy data omitted

As the FAA filed it

(-23) INSPECTOR'S STATEMENT: ON JULY 18, 2003 I INVESTIGATED AN ACCIDENT INVOLVING THE OPERATION OF A BEECH 35-A33 SINGLE-ENGINE AIRPLANE, N44CN. THE AIRCRAFT WAS OPERATED BY ROGER LATHAM AND HAD THREE PASSENGERS ONBOARD. THE FOLLOWING INFORMATION WAS OBTAINED DURING INTERVIEWS WITH MR. LATHAM AND TWO OF THE PASSENGERS. THE AIRCRAFT DEPARTED NACOGDOCHES, TEXAS ENROUTE TO HICKS AIRPORT IN FORT WORTH, TEXAS ON A 14 CFR 91 PLEASURE FLIGHT WITH FOUR OCCUPANTS ONBOARD. SOON AFTER DEPARTING NACOGCOCHES, MR. LATHAM BEGAN TO EXPERIENCE RADIO PROBLEMS. THE FLIGHT CONTINUED TO HICKS AIRPORT WHERE MR. LATHAM INTENDED TO LAND. DURING THE APPROACH TO HICKS, THE FLAPS WERE EXTENDED, HOWEVER WHEN THE GEAR WAS SELECTED IN THE DOWN POSITION THE LANDING GEAR FAILED TO EXTEND. MR. LATHAM RECOGNIZED THE UNSAFE GEAR CONDITION AND ATTEMPTED A GO-AROUND. WHEN POWER WAS APPLED, THE ENGINE SPUTTERED AND WOULD NOT DEVELOP ADEQUATE POWER TO CONTINUE FLIGHT. THE AIRCRAFT SETTLED TO THE GROUND NORTH WEST OF THE RUNWAY BETWEEN THE RAILROAD TRACKS. THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED, THREE OCCUPANTS RECEIVED MINOR INJURIES, AND ONE RECEIVED SERIOUS INJURIES. DURING THE INVESTIGATION OF THE AIRCRAFT ON SITE, IT WAS NOTED THAT THE LANDING GEAR WAS STILL RETRACTED, THE FLAPS WERE EXTENDED, AND THE MIXTURE CONTROL WAS NOT IN A FULL RICH POSITION. MANY OF THE SWITCHES WERE IN THE OFF POSITION, INCLUDING THE ALTERNATOR FIELD SWITCH, HOWEVER IT WAS NOT POSSIBLE TO DETERMINE THE POSITION OF THESE SWITCHES AT THE TIME OF THE ACCIDENT. WITH THE AIRCRAFT LIFTED AND A JUMP BATTERY CONNECTED, THE LANDING GEAR EXTENDED NORMALLY. A SPECIFIC GRAVITY TEST WAS CONDUCTED ON THE BATTERY REMOVED FROM THE AIRCRAFT AND IT WAS DETERMINED THAT THE BATTERY LACKED ADEQUATE CHARGE TO OPERATE THE ELECTRIC LANDING GEAR MOTOR. THE ALTERNATOR WAS REMOVED AND TESTED FOR PROPER OPERATION WITH NO DISCREPANCIES NOTED. THE WEATHER AT THE TIME OF THE ACCIDENT WAS 10-STATUE MILES VISIBILITY, FEW CLOUDS AT 7500 FEET, AND TEMPERATURE WAS 37 C. ^PRIVACY DATA OMITTED^

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.