20000805039989A

Accident · Substantial damage

FAA accident report · Cessna 140 · Post Mills, VT · August 5, 2000

Date
August 5, 2000 · 18:45 local
Place
Post Mills, VT
Airport
Post Mills Airport
Phase of flight
Go Round (Aborted VFR)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N73044
NTSB investigation
NTSBNYC00LA219
Reported as
Cessna 140
Reported engine
Continental C8512F
Fatal injuries
0
Pilot’s flight hours
23,677 total274 in this make and model30 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.

(-23)The pilot stated that on approach into Post Mills Vermont, he saw an ultra-light aircraft on the runway. He proceeded to conduct a go-around, however the engine lost power. Upon investigation of the aircraft, the left tank was found empty, fuel came out of the right tank when opened and when the fuel selector was selected to the right tnak, fuel flowed from the tank the fuel sump, which was broken, and the odor of fuel was detected. (.4)on August 5, 2000, about 1845 eastern daylight time, a Cessna 140, N73044, was substantially damaged after it experienced a power loss during a go-around at Post Mills Airport, Post Mills, Vermont. The certificated airline transport pilot received minor injuries. Visual meteorological conditions prevailed. No flight plan had been filed for the personal flight that was conducted under 14 CFR part 91. The pilot reported that he was returning home from rockland, Maine, and entered the traffic pattern at Post Mills for landing. The takeoff and en route phase of the flight had been conducted with the fuel selector on the left tank. While on base leg for runway 04, the fuel selector was repositioned to the right tank, which was full. On final approach, when the airplane was about 150 to 200 feet above the runway, an ultralight pulled in front of the pilot and he initiated a go-around. The pilot first turned to the right, to parallel the runway on the right side, after which, the engine lost power. The pilot stated that he turned the fuel selector, magneto switch, and master switch, each to off as the airplane began brushing the tops of the trees. The airplane descended through trees and came to rest on the ground in a nose low attitude. An inspector from the federal aviation administration (FAA) examined the airplane and reported the fuel selector was in the off position. There was no evidence of a fuel spill on the ground, and interviews with local fire department personnel, who initially responded to the accident site, revealed the odor of fuel was not detected. The left fuel tank was empty, and when the cap was loosened on the right tank, fuel gushed out around the edges of the cap. When the fuel selector was positioned to the right tank, fuel flowed from the right tank to the sump, which was broken, and the odor of fuel was detected in the air. According to the pilot, he had been airborne for 1 hour, 43 minutes. According to the Cessna 140 owner's manual, the capacity of the wing fuel tanks was 12.5 gallons each.

As the FAA filed it

(-23)THE PILOT STATED THAT ON APPROACH INTO POST MILLS VERMONT, HE SAW AN ULTRA-LIGHT AIRCRAFT ON THE RUNWAY. HE PROCEEDED TO CONDUCT A GO-AROUND, HOWEVER THE ENGINE LOST POWER. UPON INVESTIGATION OF THE AIRCRAFT, THE LEFT TANK WAS FOUND EMPTY, FUEL CAME OUT OF THE RIGHT TANK WHEN OPENED AND WHEN THE FUEL SELECTOR WAS SELECTED TO THE RIGHT TNAK, FUEL FLOWED FROM THE TANK THE FUEL SUMP, WHICH WAS BROKEN, AND THE ODOR OF FUEL WAS DETECTED. (.4)ON AUGUST 5, 2000, ABOUT 1845 EASTERN DAYLIGHT TIME, A CESSNA 140, N73044, WAS SUBSTANTIALLY DAMAGED AFTER IT EXPERIENCED A POWER LOSS DURING A GO-AROUND AT POST MILLS AIRPORT, POST MILLS, VERMONT. THE CERTIFICATED AIRLINE TRANSPORT PILOT RECEIVED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. NO FLIGHT PLAN HAD BEEN FILED FOR THE PERSONAL FLIGHT THAT WAS CONDUCTED UNDER 14 CFR PART 91. THE PILOT REPORTED THAT HE WAS RETURNING HOME FROM ROCKLAND, MAINE, AND ENTERED THE TRAFFIC PATTERN AT POST MILLS FOR LANDING. THE TAKEOFF AND EN ROUTE PHASE OF THE FLIGHT HAD BEEN CONDUCTED WITH THE FUEL SELECTOR ON THE LEFT TANK. WHILE ON BASE LEG FOR RUNWAY 04, THE FUEL SELECTOR WAS REPOSITIONED TO THE RIGHT TANK, WHICH WAS FULL. ON FINAL APPROACH, WHEN THE AIRPLANE WAS ABOUT 150 TO 200 FEET ABOVE THE RUNWAY, AN ULTRALIGHT PULLED IN FRONT OF THE PILOT AND HE INITIATED A GO-AROUND. THE PILOT FIRST TURNED TO THE RIGHT, TO PARALLEL THE RUNWAY ON THE RIGHT SIDE, AFTER WHICH, THE ENGINE LOST POWER. THE PILOT STATED THAT HE TURNED THE FUEL SELECTOR, MAGNETO SWITCH, AND MASTER SWITCH, EACH TO OFF AS THE AIRPLANE BEGAN BRUSHING THE TOPS OF THE TREES. THE AIRPLANE DESCENDED THROUGH TREES AND CAME TO REST ON THE GROUND IN A NOSE LOW ATTITUDE. AN INSPECTOR FROM THE FEDERAL AVIATION ADMINISTRATION (FAA) EXAMINED THE AIRPLANE AND REPORTED THE FUEL SELECTOR WAS IN THE OFF POSITION. THERE WAS NO EVIDENCE OF A FUEL SPILL ON THE GROUND, AND INTERVIEWS WITH LOCAL FIRE DEPARTMENT PERSONNEL, WHO INITIALLY RESPONDED TO THE ACCIDENT SITE, REVEALED THE ODOR OF FUEL WAS NOT DETECTED. THE LEFT FUEL TANK WAS EMPTY, AND WHEN THE CAP WAS LOOSENED ON THE RIGHT TANK, FUEL GUSHED OUT AROUND THE EDGES OF THE CAP. WHEN THE FUEL SELECTOR WAS POSITIONED TO THE RIGHT TANK, FUEL FLOWED FROM THE RIGHT TANK TO THE SUMP, WHICH WAS BROKEN, AND THE ODOR OF FUEL WAS DETECTED IN THE AIR. ACCORDING TO THE PILOT, HE HAD BEEN AIRBORNE FOR 1 HOUR, 43 MINUTES. ACCORDING TO THE CESSNA 140 OWNER'S MANUAL, THE CAPACITY OF THE WING FUEL TANKS WAS 12.5 GALLONS EACH.

NTSB investigation

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