19980711016479A

Accident · Substantial damage

FAA accident report · Amtr Wagabond · Wasilla, AK · July 11, 1998

Date
July 11, 1998 · 13:00 local
Place
Wasilla, AK
Airport
Wasilla Airport
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N36GM
NTSB investigation
NTSBANC98LA094
Reported as
Amtr Wagabond
Reported engine
Lycoming O235C2C
Fatal injuries
0
Pilot’s flight hours
25,000 total500 in this make and model80 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.

Rough engine power loss on climbout. Landed on road. Struck road sign. Rust debris in carb bowl. Possible water. (.4) on July 11, 1998, about 1300 Alaska daylight time, a n experimental/homebuilt meeuwsen Wagabond airplane, N36GM, sustained substantial damage during a forced landing on a roadway, about 5 miles northeast of Wasilla, Alaska. The tailwheel equipped airplane was being operated as a visual flight rules (VFR) local area personal flight when the accident occurred. The airplane was registered to, and operated by, the pilot. The certificated airline transport pilot, the sole occupant, received minor injuries. Visual meteorological conditions prevailed. During a telephone conversation with the national transportation safety board (NTSB) investigator-in-charge (iic), on July 13, 1998, at 1105, the pilot reported the following: he recently completed a flight from California, through Canada, to Wasilla. During the trip through Canada, the pilot encountered rust deposits in the fuel supply. He drained the airplane fuel sump before each flight until no rust deposits were observed. The airplane has two, metal wing mounted fuel tanks. The tanks do not have an individual sump. The only fuel sump is an airframe gascolator. Prior to departing on the accident flight, the pilot said he drained about a quart of fuel from the sump, and did not notice any contamination. The pilot said he departed a private airstrip adjacent to cottonwood lake in Wasilla. The airplane climbed to about 50 feet above the lake, and suddenly began to run rough. The engine was producing popping and banging noises, and began losing RPM. The pilot said he applied carburetor heat, and leaned the fuel mixture. The engine speed recovered to about 2200 RPM, but continued to run rough. The pilot reported he attempted several carburetor heat and mixture combinations, but the airplane did not gain any altitude. After traveling about 1 mile over the lake, the airplane was approaching an area of trees and a roadway with adjacent electrical power lines. The pilot said he selected an emergency landing area on the roadway and dove the airplane toward the ground between several sets of power lines. The airplane landed on the roadway, and the right wing struck a stop sign. The pilot said he then applied right rudder to intentionally swerve the airplane into a ditch. A federal aviation administration(FAA) airworthiness inspector, anchorage flight standards district office (FSDO), anchorage, Alaska, examined the airplane wreckage after the pilot/owner recovered the airplane. The inspector indicated the pilot had fueled the airplane with automotive gasoline from gas cans. The carburetor and the airframe gascolator had been disassembled by the pilot. The inspector noted the gascolator appeared to be clean. The interior of the carburetor bowl exhibited evidence of rust. (-23) on July 11, 1998, experimental/amateur built aircraft N36GM departed a private airstrip located between cottonwood lake and mud lake near Wasilla, Alaska. On climb-out over cottonwood lake, the engine began to run rough, the pilot attempted several carb heat/mixture combinations. The engine did not respond and the pilot elected to make a forced landing on a subdivision road that was free of traffic. On landing, the aircraft struck a road sign, the left main gear collapsed and the plane came to rest in the ditch. The pilot received minor cuts and bruises. When the carburetor and gascolator were disassembled and inspected, the carb was dry of fuel at the time but was noted that the bowl had rusty metal flakes in it and the mixture control shaft was rusty indicating that there might have been standing water in it. The gascolator was found clean.

As the FAA filed it

ROUGH ENGINE POWER LOSS ON CLIMBOUT. LANDED ON ROAD. STRUCK ROAD SIGN. RUST DEBRIS IN CARB BOWL. POSSIBLE WATER. (.4) ON JULY 11, 1998, ABOUT 1300 ALASKA DAYLIGHT TIME, A N EXPERIMENTAL/HOMEBUILT MEEUWSEN WAGABOND AIRPLANE, N36GM, SUSTAINED SUBSTANTIAL DAMAGE DURING A FORCED LANDING ON A ROADWAY, ABOUT 5 MILES NORTHEAST OF WASILLA, ALASKA. THE TAILWHEEL EQUIPPED AIRPLANE WAS BEING OPERATED AS A VISUAL FLIGHT RULES (VFR) LOCAL AREA PERSONAL FLIGHT WHEN THE ACCIDENT OCCURRED. THE AIRPLANE WAS REGISTERED TO, AND OPERATED BY, THE PILOT. THE CERTIFICATED AIRLINE TRANSPORT PILOT, THE SOLE OCCUPANT, RECEIVED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. DURING A TELEPHONE CONVERSATION WITH THE NATIONAL TRANSPORTATION SAFETY BOARD (NTSB) INVESTIGATOR-IN-CHARGE (IIC), ON JULY 13, 1998, AT 1105, THE PILOT REPORTED THE FOLLOWING: HE RECENTLY COMPLETED A FLIGHT FROM CALIFORNIA, THROUGH CANADA, TO WASILLA. DURING THE TRIP THROUGH CANADA, THE PILOT ENCOUNTERED RUST DEPOSITS IN THE FUEL SUPPLY. HE DRAINED THE AIRPLANE FUEL SUMP BEFORE EACH FLIGHT UNTIL NO RUST DEPOSITS WERE OBSERVED. THE AIRPLANE HAS TWO, METAL WING MOUNTED FUEL TANKS. THE TANKS DO NOT HAVE AN INDIVIDUAL SUMP. THE ONLY FUEL SUMP IS AN AIRFRAME GASCOLATOR. PRIOR TO DEPARTING ON THE ACCIDENT FLIGHT, THE PILOT SAID HE DRAINED ABOUT A QUART OF FUEL FROM THE SUMP, AND DID NOT NOTICE ANY CONTAMINATION. THE PILOT SAID HE DEPARTED A PRIVATE AIRSTRIP ADJACENT TO COTTONWOOD LAKE IN WASILLA. THE AIRPLANE CLIMBED TO ABOUT 50 FEET ABOVE THE LAKE, AND SUDDENLY BEGAN TO RUN ROUGH. THE ENGINE WAS PRODUCING POPPING AND BANGING NOISES, AND BEGAN LOSING RPM. THE PILOT SAID HE APPLIED CARBURETOR HEAT, AND LEANED THE FUEL MIXTURE. THE ENGINE SPEED RECOVERED TO ABOUT 2200 RPM, BUT CONTINUED TO RUN ROUGH. THE PILOT REPORTED HE ATTEMPTED SEVERAL CARBURETOR HEAT AND MIXTURE COMBINATIONS, BUT THE AIRPLANE DID NOT GAIN ANY ALTITUDE. AFTER TRAVELING ABOUT 1 MILE OVER THE LAKE, THE AIRPLANE WAS APPROACHING AN AREA OF TREES AND A ROADWAY WITH ADJACENT ELECTRICAL POWER LINES. THE PILOT SAID HE SELECTED AN EMERGENCY LANDING AREA ON THE ROADWAY AND DOVE THE AIRPLANE TOWARD THE GROUND BETWEEN SEVERAL SETS OF POWER LINES. THE AIRPLANE LANDED ON THE ROADWAY, AND THE RIGHT WING STRUCK A STOP SIGN. THE PILOT SAID HE THEN APPLIED RIGHT RUDDER TO INTENTIONALLY SWERVE THE AIRPLANE INTO A DITCH. A FEDERAL AVIATION ADMINISTRATION(FAA) AIRWORTHINESS INSPECTOR, ANCHORAGE FLIGHT STANDARDS DISTRICT OFFICE (FSDO), ANCHORAGE, ALASKA, EXAMINED THE AIRPLANE WRECKAGE AFTER THE PILOT/OWNER RECOVERED THE AIRPLANE. THE INSPECTOR INDICATED THE PILOT HAD FUELED THE AIRPLANE WITH AUTOMOTIVE GASOLINE FROM GAS CANS. THE CARBURETOR AND THE AIRFRAME GASCOLATOR HAD BEEN DISASSEMBLED BY THE PILOT. THE INSPECTOR NOTED THE GASCOLATOR APPEARED TO BE CLEAN. THE INTERIOR OF THE CARBURETOR BOWL EXHIBITED EVIDENCE OF RUST. (-23) ON JULY 11, 1998, EXPERIMENTAL/AMATEUR BUILT AIRCRAFT N36GM DEPARTED A PRIVATE AIRSTRIP LOCATED BETWEEN COTTONWOOD LAKE AND MUD LAKE NEAR WASILLA, ALASKA. ON CLIMB-OUT OVER COTTONWOOD LAKE, THE ENGINE BEGAN TO RUN ROUGH, THE PILOT ATTEMPTED SEVERAL CARB HEAT/MIXTURE COMBINATIONS. THE ENGINE DID NOT RESPOND AND THE PILOT ELECTED TO MAKE A FORCED LANDING ON A SUBDIVISION ROAD THAT WAS FREE OF TRAFFIC. ON LANDING, THE AIRCRAFT STRUCK A ROAD SIGN, THE LEFT MAIN GEAR COLLAPSED AND THE PLANE CAME TO REST IN THE DITCH. THE PILOT RECEIVED MINOR CUTS AND BRUISES. WHEN THE CARBURETOR AND GASCOLATOR WERE DISASSEMBLED AND INSPECTED, THE CARB WAS DRY OF FUEL AT THE TIME BUT WAS NOTED THAT THE BOWL HAD RUSTY METAL FLAKES IN IT AND THE MIXTURE CONTROL SHAFT WAS RUSTY INDICATING THAT THERE MIGHT HAVE BEEN STANDING WATER IN IT. THE GASCOLATOR WAS FOUND CLEAN.

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 N36GM · 3

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