19981204039799A

Accident · Substantial damage

FAA accident report · Stnson 10ASTNSON · Nondalton, AK · December 4, 1998

Date
December 4, 1998 · 14:55 local
Place
Nondalton, AK
Airport
Nondalton
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
Air taxi and commuter (Part 135)
Operator
HXXC
Damage
Substantial damage
Aircraft
N36755
NTSB investigation
NTSBANC99LA015
Reported as
Stnson 10ASTNSON
Reported engine
Lycoming O320A2B
People aboard
2
Fatal injuries
0
Pilot’s flight hours
5,724 total26 in this make and model348 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 December 4, 1998, about 1455 Alaska standard time, a tundra tire equipped Stinson 10A airplane, N36755, sustained substantial damage during a forced landing, about 9 miles east of Nondalton, Alaska. The airplane was being operated as a visual flight rules (VFR) domestic on-demand passenger flight under title 14 CFR part 135 when the accident occurred. The airplane was operated by lake clark air inc., port alsworth, Alaska. The certificated commercial pilot, and the sole passenger, were not injured. Visual meteorological conditions prevailed. VFR company flight following procedures were in effect. The flight originated from a private airstrip at port alsworth, Alaska, at 1139. During a telephone conversation with the national transportation safety board (NTSB) investigator-in-charge (iic), on December 6, 1998, at 1000, the pilot reported the flight was conducted for the Alaska department of fish and game. The passenger was conducting a moose count. The pilot said that after departure with full fuel tanks, he flew for two hours with the left fuel tank selected. After two hours of flight, the fuel in the left tank was almost exhausted, and the pilot switched to the right fuel tank. He then flew for about 1.5 hours on the right tank before the engine suddenly quit. The pilot switched back to the left tank and climbed to about 1,000 feet above the ground. After about 6 minutes on the left tank, the engine quit running again. The pilot selected an emergency landing area on a small frozen pond. The surface of the pond contained slushy ice and drifted snow. During the landing roll, the airplane entered deep snow and nosed over. The airplane received damage to the left wing lift strut, the rudder, and the right wingtip. The operator reported the airplane is equipped with a 150 horsepower engine. The airplane has two wing mounted fuel tanks that contain 20 gallons each. Total useable fuel is 36 gallons. The fuel selector has positions for left, right, and off. Each fuel tank has an electric fuel gauge. The operator also reported that when the airplane was recovered from the accident site, evidence of fuel staining was observed on the upper surface of the right wing, adjacent to the right fuel cap. (.4) the certificated commercial pilot, and the sole passenger, departed for an on-demand air taxi flight over remote terrain. The passenger was conducting moose counting research for the Alaska department of fish and game. The airplane carried four hours of fuel divided between two wing mounted fuel tanks. Each fuel tank is equipped with an electric fuel gauge. After flying for two hours with the left tank selected, the fuel in the left tank was almost exhausted, and the pilot switched to the right fuel tank. He then flew for about 1.5 hours on the right tank before the engine suddenly quit. The pilot switched back to the left tank and climbed to about 1,000 feet above the ground. After about 6 minutes on the left tank, the engine quit runing again. The pilot selected an emergency landing area on a small, frozen pond. The surface of the pond contained slushy ice and drifted snow. During the landing roll, the airplane entered deep snow and nosed over. The passenger reported she flew in the accident airplane two days before the airplane was inoperative. During the accident flight, two days later, she again noticed the right fuel gauge was still inoperative. Following recovery of the airplane, evidence of fuel staining was observed on the upper surface of the right wing, adjacent to the right fuel cap. (-23) on December 4, 1998, at about 1455 local time, a wheel equipped Stinson 10A airplane N36755, sustained substantial damage during a forced landing due to fuel exhaustion. This occurred approximately eight miles southeast of Nondalton, Alaska. After touchdown, the aircraft rolled about 200 feet encountering a snowdrift, which caused the plane to nose over. The aircraft was operated by lake clark air, a FAR part 135 operation. This flight was conducting game surveys for the state of Alaska. VFR conditions prevailed at the time of the accident. The commercial pilot and the one passenger aboard, were not injured. The flight originated at port alsworth, Alaska.

As the FAA filed it

(.19) ON DECEMBER 4, 1998, ABOUT 1455 ALASKA STANDARD TIME, A TUNDRA TIRE EQUIPPED STINSON 10A AIRPLANE, N36755, SUSTAINED SUBSTANTIAL DAMAGE DURING A FORCED LANDING, ABOUT 9 MILES EAST OF NONDALTON, ALASKA. THE AIRPLANE WAS BEING OPERATED AS A VISUAL FLIGHT RULES (VFR) DOMESTIC ON-DEMAND PASSENGER FLIGHT UNDER TITLE 14 CFR PART 135 WHEN THE ACCIDENT OCCURRED. THE AIRPLANE WAS OPERATED BY LAKE CLARK AIR INC., PORT ALSWORTH, ALASKA. THE CERTIFICATED COMMERCIAL PILOT, AND THE SOLE PASSENGER, WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. VFR COMPANY FLIGHT FOLLOWING PROCEDURES WERE IN EFFECT. THE FLIGHT ORIGINATED FROM A PRIVATE AIRSTRIP AT PORT ALSWORTH, ALASKA, AT 1139. DURING A TELEPHONE CONVERSATION WITH THE NATIONAL TRANSPORTATION SAFETY BOARD (NTSB) INVESTIGATOR-IN-CHARGE (IIC), ON DECEMBER 6, 1998, AT 1000, THE PILOT REPORTED THE FLIGHT WAS CONDUCTED FOR THE ALASKA DEPARTMENT OF FISH AND GAME. THE PASSENGER WAS CONDUCTING A MOOSE COUNT. THE PILOT SAID THAT AFTER DEPARTURE WITH FULL FUEL TANKS, HE FLEW FOR TWO HOURS WITH THE LEFT FUEL TANK SELECTED. AFTER TWO HOURS OF FLIGHT, THE FUEL IN THE LEFT TANK WAS ALMOST EXHAUSTED, AND THE PILOT SWITCHED TO THE RIGHT FUEL TANK. HE THEN FLEW FOR ABOUT 1.5 HOURS ON THE RIGHT TANK BEFORE THE ENGINE SUDDENLY QUIT. THE PILOT SWITCHED BACK TO THE LEFT TANK AND CLIMBED TO ABOUT 1,000 FEET ABOVE THE GROUND. AFTER ABOUT 6 MINUTES ON THE LEFT TANK, THE ENGINE QUIT RUNNING AGAIN. THE PILOT SELECTED AN EMERGENCY LANDING AREA ON A SMALL FROZEN POND. THE SURFACE OF THE POND CONTAINED SLUSHY ICE AND DRIFTED SNOW. DURING THE LANDING ROLL, THE AIRPLANE ENTERED DEEP SNOW AND NOSED OVER. THE AIRPLANE RECEIVED DAMAGE TO THE LEFT WING LIFT STRUT, THE RUDDER, AND THE RIGHT WINGTIP. THE OPERATOR REPORTED THE AIRPLANE IS EQUIPPED WITH A 150 HORSEPOWER ENGINE. THE AIRPLANE HAS TWO WING MOUNTED FUEL TANKS THAT CONTAIN 20 GALLONS EACH. TOTAL USEABLE FUEL IS 36 GALLONS. THE FUEL SELECTOR HAS POSITIONS FOR LEFT, RIGHT, AND OFF. EACH FUEL TANK HAS AN ELECTRIC FUEL GAUGE. THE OPERATOR ALSO REPORTED THAT WHEN THE AIRPLANE WAS RECOVERED FROM THE ACCIDENT SITE, EVIDENCE OF FUEL STAINING WAS OBSERVED ON THE UPPER SURFACE OF THE RIGHT WING, ADJACENT TO THE RIGHT FUEL CAP. (.4) THE CERTIFICATED COMMERCIAL PILOT, AND THE SOLE PASSENGER, DEPARTED FOR AN ON-DEMAND AIR TAXI FLIGHT OVER REMOTE TERRAIN. THE PASSENGER WAS CONDUCTING MOOSE COUNTING RESEARCH FOR THE ALASKA DEPARTMENT OF FISH AND GAME. THE AIRPLANE CARRIED FOUR HOURS OF FUEL DIVIDED BETWEEN TWO WING MOUNTED FUEL TANKS. EACH FUEL TANK IS EQUIPPED WITH AN ELECTRIC FUEL GAUGE. AFTER FLYING FOR TWO HOURS WITH THE LEFT TANK SELECTED, THE FUEL IN THE LEFT TANK WAS ALMOST EXHAUSTED, AND THE PILOT SWITCHED TO THE RIGHT FUEL TANK. HE THEN FLEW FOR ABOUT 1.5 HOURS ON THE RIGHT TANK BEFORE THE ENGINE SUDDENLY QUIT. THE PILOT SWITCHED BACK TO THE LEFT TANK AND CLIMBED TO ABOUT 1,000 FEET ABOVE THE GROUND. AFTER ABOUT 6 MINUTES ON THE LEFT TANK, THE ENGINE QUIT RUNING AGAIN. THE PILOT SELECTED AN EMERGENCY LANDING AREA ON A SMALL, FROZEN POND. THE SURFACE OF THE POND CONTAINED SLUSHY ICE AND DRIFTED SNOW. DURING THE LANDING ROLL, THE AIRPLANE ENTERED DEEP SNOW AND NOSED OVER. THE PASSENGER REPORTED SHE FLEW IN THE ACCIDENT AIRPLANE TWO DAYS BEFORE THE AIRPLANE WAS INOPERATIVE. DURING THE ACCIDENT FLIGHT, TWO DAYS LATER, SHE AGAIN NOTICED THE RIGHT FUEL GAUGE WAS STILL INOPERATIVE. FOLLOWING RECOVERY OF THE AIRPLANE, EVIDENCE OF FUEL STAINING WAS OBSERVED ON THE UPPER SURFACE OF THE RIGHT WING, ADJACENT TO THE RIGHT FUEL CAP. (-23) ON DECEMBER 4, 1998, AT ABOUT 1455 LOCAL TIME, A WHEEL EQUIPPED STINSON 10A AIRPLANE N36755, SUSTAINED SUBSTANTIAL DAMAGE DURING A FORCED LANDING DUE TO FUEL EXHAUSTION. THIS OCCURRED APPROXIMATELY EIGHT MILES SOUTHEAST OF NONDALTON, ALASKA. AFTER TOUCHDOWN, THE AIRCRAFT ROLLED ABOUT 200 FEET ENCOUNTERING A SNOWDRIFT, WHICH CAUSED THE PLANE TO NOSE OVER. THE AIRCRAFT WAS OPERATED BY LAKE CLARK AIR, A FAR PART 135 OPERATION. THIS FLIGHT WAS CONDUCTING GAME SURVEYS FOR THE STATE OF ALASKA. VFR CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT. THE COMMERCIAL PILOT AND THE ONE PASSENGER ABOARD, WERE NOT INJURED. THE FLIGHT ORIGINATED AT PORT ALSWORTH, ALASKA.

NTSB investigation

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

Other reports on N36755 · 1

Matched to the same aircraft by N-number and date.