20020113001849A

Accident · Substantial damage

FAA accident report · Univar 108-2 · Bayou La Batre, AL · January 13, 2002

Date
January 13, 2002 · 18:00 local
Place
Bayou La Batre, AL
Airport
Roy E Ray Airport
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9315K
NTSB investigation
NTSBATL02LA037
Reported as
Univar 1082
Reported engine
Lycoming O360A1A
Fatal injuries
0
Pilot’s flight hours
400 total95 in this make and model40 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.

(.19) On January 13, 2002, at 1700 central standard time, a Stinson 108M, N9315K, operated by a private pilot, under the provisions of title 14 CFR part 91, experienced a loss of engine power on the intitial takeoff/climb from roy e. ray airport in Bayou la barte, Alabama. The personal flight was enroute from Bayou la barte, Alabama to st. elmo, Alabama. Visual meteorological conditions prevailed at the time of the accident and no flight plan was filed. The private pilot received serious injuries. The accident occured during the takeoff from Bayou la barte airport. The airplane sustained substantial damage. Reportedly, the engine lost power at 400 feet above the ground during the climbout. The pilot executed a left turn and collided with power lines. The airplane subsequently came to rest in a nearby ditch about 400 feet from the end of the departure runway 36. (-23) on take off aircraft lost power at approx 200'. Pilot made a left turn trying to land on a road. Aircraft hit a small tree with right wing then went thru 2 power lines, impacted ground in a nose down position, then flipped over on its back. (.4) on January 13, 2002, at 1700 central standard time, a Stinson 108M, N9315K, experienced a loss of engine power on the initial takeoff/climb from roy e. ray airport in Bayou La Batre, Alabama. The airplane, registered to consolidated-vultee, was operated by the pilot under the provisions of title 14 CFR part 91. The personal flight was enroute from Bayou La Batre, Alabama to st. elmo, Alabama. Visual meteorological conditions prevailed at the time of the accident and no flight plan was filed. The private pilot received serious injuries and the airplane sustained substantial damage. The pilot stated there were 20 gallons of fuel on board at takeoff. According to the pilot, the engine lost power at 400 feet above the ground during the climb out. The pilot stated that he established glide at 65-70MPH and attempted an engine restart unsuccessfully. The pilot executed a left turn and collided with power lines approximately 35 above ground. The airplane subsequently came to rest in a nearby ditch about 400 feet from the end of the departure runway 36. A review of weather data showed conditions favorable for the formation of carburetor icing; the temperature was 57 degrees fahrenheit. Tests were performed on both magnetos, they both operated within normal parameters. A functional check of the engine was performed; the power was checked at 2700 RPM and results indicated that the engine ran smoothly at full power and at idle. Oil pressure was normal during the functional check. The functional check of the engine failed to disclose a mechanical malfunction or component failure.

As the FAA filed it

(.19) ON JANUARY 13, 2002, AT 1700 CENTRAL STANDARD TIME, A STINSON 108M, N9315K, OPERATED BY A PRIVATE PILOT, UNDER THE PROVISIONS OF TITLE 14 CFR PART 91, EXPERIENCED A LOSS OF ENGINE POWER ON THE INTITIAL TAKEOFF/CLIMB FROM ROY E. RAY AIRPORT IN BAYOU LA BARTE, ALABAMA. THE PERSONAL FLIGHT WAS ENROUTE FROM BAYOU LA BARTE, ALABAMA TO ST. ELMO, ALABAMA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT AND NO FLIGHT PLAN WAS FILED. THE PRIVATE PILOT RECEIVED SERIOUS INJURIES. THE ACCIDENT OCCURED DURING THE TAKEOFF FROM BAYOU LA BARTE AIRPORT. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE. REPORTEDLY, THE ENGINE LOST POWER AT 400 FEET ABOVE THE GROUND DURING THE CLIMBOUT. THE PILOT EXECUTED A LEFT TURN AND COLLIDED WITH POWER LINES. THE AIRPLANE SUBSEQUENTLY CAME TO REST IN A NEARBY DITCH ABOUT 400 FEET FROM THE END OF THE DEPARTURE RUNWAY 36. (-23) ON TAKE OFF AIRCRAFT LOST POWER AT APPROX 200'. PILOT MADE A LEFT TURN TRYING TO LAND ON A ROAD. AIRCRAFT HIT A SMALL TREE WITH RIGHT WING THEN WENT THRU 2 POWER LINES, IMPACTED GROUND IN A NOSE DOWN POSITION, THEN FLIPPED OVER ON ITS BACK. (.4) ON JANUARY 13, 2002, AT 1700 CENTRAL STANDARD TIME, A STINSON 108M, N9315K, EXPERIENCED A LOSS OF ENGINE POWER ON THE INITIAL TAKEOFF/CLIMB FROM ROY E. RAY AIRPORT IN BAYOU LA BATRE, ALABAMA. THE AIRPLANE, REGISTERED TO CONSOLIDATED-VULTEE, WAS OPERATED BY THE PILOT UNDER THE PROVISIONS OF TITLE 14 CFR PART 91. THE PERSONAL FLIGHT WAS ENROUTE FROM BAYOU LA BATRE, ALABAMA TO ST. ELMO, ALABAMA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT AND NO FLIGHT PLAN WAS FILED. THE PRIVATE PILOT RECEIVED SERIOUS INJURIES AND THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE. THE PILOT STATED THERE WERE 20 GALLONS OF FUEL ON BOARD AT TAKEOFF. ACCORDING TO THE PILOT, THE ENGINE LOST POWER AT 400 FEET ABOVE THE GROUND DURING THE CLIMB OUT. THE PILOT STATED THAT HE ESTABLISHED GLIDE AT 65-70MPH AND ATTEMPTED AN ENGINE RESTART UNSUCCESSFULLY. THE PILOT EXECUTED A LEFT TURN AND COLLIDED WITH POWER LINES APPROXIMATELY 35 ABOVE GROUND. THE AIRPLANE SUBSEQUENTLY CAME TO REST IN A NEARBY DITCH ABOUT 400 FEET FROM THE END OF THE DEPARTURE RUNWAY 36. A REVIEW OF WEATHER DATA SHOWED CONDITIONS FAVORABLE FOR THE FORMATION OF CARBURETOR ICING; THE TEMPERATURE WAS 57 DEGREES FAHRENHEIT.TESTS WERE PERFORMED ON BOTH MAGNETOS, THEY BOTH OPERATED WITHIN NORMAL PARAMETERS. A FUNCTIONAL CHECK OF THE ENGINE WAS PERFORMED; THE POWER WAS CHECKED AT 2700 RPM AND RESULTS INDICATED THAT THE ENGINE RAN SMOOTHLY AT FULL POWER AND AT IDLE. OIL PRESSURE WAS NORMAL DURING THE FUNCTIONAL CHECK. THE FUNCTIONAL CHECK OF THE ENGINE FAILED TO DISCLOSE A MECHANICAL MALFUNCTION OR COMPONENT FAILURE.

NTSB investigation

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