19970611013779A

Accident · Destroyed

FAA accident report · Luscom 8A · Annapolis, MD · June 11, 1997

Date
June 11, 1997 · 11:00 local
Place
Annapolis, MD
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N37095
NTSB investigation
NTSBIAD97LA086
Reported as
Luscom 8A
Reported engine
Continental A658F
People aboard
1
Fatal injuries
0
Pilot’s flight hours
5,000 total50 in this make and model90 in the last 90 days

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.

On June 11, 1997, at 1100 eastern daylight time, a Luscombe LL-8-A, N37095, was destroyed when it collided with trees during a forced landing near Annapolis, Maryland. The certificated private pilot was not injured while the passenger sustained minor injuries. Visual meteorological conditions prevailed and a flight plan was not filed. The personal flight was conducted under 14 CFR part 91. The local flight had originated from severn river, Maryland, at approximately 1030. According to a federal aviation admninistration (FAA) inspector, the pilot was perforning an aerial survey between 500 and 1000 feet above the ground, when the engine lost power. The pilot reported that as he approached one of the creeks , the initiated a turn so that the passenger could take a picture of the seagrass, when the airplane started to lose altitude. He stated that his efforts to maintain altitude by adding full power was unsuccessful. Despite a full forward throttle setting, the airplane continued to lose altitude and power. The pilot performed a forced landing to a wooded area where the right wing struck a 20 feet tall tree. The airplane was examined at the accident site by the FAA inspector. According to the inspector's report, there was about 6 to 7 gallons of fuel in the fuel tanks, and no water or contamination was found in the fuel system. Examination of the wreckage did not disclose any evidence of mechanical malfunction with the airplane or engine, and the carburetor heat switch was in the off position. The reported temperature and dew point at the time of accident was 82 degrees fahrenheit (f), and 59 degrees f respectively. According to carburetor icing charts, conditions were conducive for carburetor ice.

As the FAA filed it

ON JUNE 11, 1997, AT 1100 EASTERN DAYLIGHT TIME, A LUSCOMBE LL-8-A, N37095, WAS DESTROYED WHEN IT COLLIDED WITH TREES DURING A FORCED LANDING NEAR ANNAPOLIS, MARYLAND. THE CERTIFICATED PRIVATE PILOT WAS NOT INJURED WHILE THE PASSENGER SUSTAINED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND A FLIGHT PLAN WAS NOT FILED. THE PERSONAL FLIGHT WAS CONDUCTED UNDER 14 CFR PART 91. THE LOCAL FLIGHT HAD ORIGINATED FROM SEVERN RIVER, MARYLAND, AT APPROXIMATELY 1030. ACCORDING TO A FEDERAL AVIATION ADMNINISTRATION (FAA) INSPECTOR, THE PILOT WAS PERFORNING AN AERIAL SURVEY BETWEEN 500 AND 1000 FEET ABOVE THE GROUND, WHEN THE ENGINE LOST POWER. THE PILOT REPORTED THAT AS HE APPROACHED ONE OF THE CREEKS , THE INITIATED A TURN SO THAT THE PASSENGER COULD TAKE A PICTURE OF THE SEAGRASS, WHEN THE AIRPLANE STARTED TO LOSE ALTITUDE. HE STATED THAT HIS EFFORTS TO MAINTAIN ALTITUDE BY ADDING FULL POWER WAS UNSUCCESSFUL. DESPITE A FULL FORWARD THROTTLE SETTING, THE AIRPLANE CONTINUED TO LOSE ALTITUDE AND POWER. THE PILOT PERFORMED A FORCED LANDING TO A WOODED AREA WHERE THE RIGHT WING STRUCK A 20 FEET TALL TREE. THE AIRPLANE WAS EXAMINED AT THE ACCIDENT SITE BY THE FAA INSPECTOR. ACCORDING TO THE INSPECTOR'S REPORT, THERE WAS ABOUT 6 TO 7 GALLONS OF FUEL IN THE FUEL TANKS, AND NO WATER OR CONTAMINATION WAS FOUND IN THE FUEL SYSTEM. EXAMINATION OF THE WRECKAGE DID NOT DISCLOSE ANY EVIDENCE OF MECHANICAL MALFUNCTION WITH THE AIRPLANE OR ENGINE, AND THE CARBURETOR HEAT SWITCH WAS IN THE OFF POSITION. THE REPORTED TEMPERATURE AND DEW POINT AT THE TIME OF ACCIDENT WAS 82 DEGREES FAHRENHEIT (F), AND 59 DEGREES F RESPECTIVELY. ACCORDING TO CARBURETOR ICING CHARTS, CONDITIONS WERE CONDUCIVE FOR CARBURETOR ICE.

NTSB investigation

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