19980904046509A

Accident · Substantial damage

FAA accident report · Piper PA-28-181 · Oroville, CA · September 4, 1998

Date
September 4, 1998 · 19:20 local
Place
Oroville, CA
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2161G
NTSB investigation
NTSBLAX98LA284
Reported as
Piper PA28181
Reported engine
Lycoming O360A4M
People aboard
3
Fatal injuries
0
Pilot’s flight hours
230 total50 in this make and model29 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.

(.4)On September 4,1998, at 1915 pacific daylight time, a Piper PA-28-181, N2161G, sustained substantial damage while attempting to land on a road 3 nautical miles south of the airport at Oroville, California. The private pilot and two passengers sustained no injuries. Visual meteorological conditions prevailed for the pleasure flight to chico, which originated in long beach with an intermediate stop in santa paula, California. The pilot stated he was flying from long beach to redmond, Oregon for a fly-in at a kit plane manufacturer. The day before he departed, he asked that the airplane be filled with fuel, rather than to the tab markers as was normally done. The pilot's operating handbook (POH) indicated fuel capacity was 24 gallons per tank when full and 17 gallons when filled to the tabs. A review of the operator's records revealed the airplane completed a 1.4 hour flight 4 days earlier and was serviced with 14 gallons of fuel. Fuel receipts showed an additional 12.2 gallons were dispensed the day before the accident flight. The pilot stated he planned for 3.5 hours enroute to chico where he would stop for fuel. Departure from long beach was delayed until 1332 due to incleme nt weather. The pilot headed east past corona, CA., then flew toward lancaster, California. Dur to mountain obscuration, he said he could not proceed as planned and landed at santa paula. He said he personally filled the tanks to full capacity. The receipt indicated he dispensed 20.59 gallons. After departing santa paula, the pilot maintained an altitude of 1,000 feet (MSL) until past santa barbara, California. At gaviota VOR he climbed to 6,500 MSL. He maintained that altitude until paso robles, CA. Where he descended to 4,500 feet. When his global positioning system indicated he was 18 nautical miles from chico, he commenced a gradual descent. He maintained a power setting of 2,500 RPM in cruis flight. He leaned the mixture to 100 degrees rich of peak exhaust gas temperature (EGT). He stated that from takeoff at 1552, until 1650, he operated from the right fuel tank. Then he selected the left tank. At 1750, he switched to the right tank again. He noted the left fuel quantity gauge was slightly above the half tank mark. He switched back to the left tank at 1850. He observed that the right tank fuel quantityindicator was bobbing just above empty. About 1915, the engine RPM lowered the pilot turned the electric boost pump on and switched to the right tank. He observed the left tank was indicating empty. The fuel pressure came up and engine power was restored for approx. 1 minute before the engine again lost power. The pilot landed on a road with no traffic. The left wing tip contacted a road reflector. The airplane veered off the road, through a barbed wire fence, onto a rocky slope and the nose gear collapsed.

As the FAA filed it

(.4)ON SEPTEMBER 4,1998, AT 1915 PACIFIC DAYLIGHT TIME, A PIPER PA-28-181, N2161G, SUSTAINED SUBSTANTIAL DAMAGE WHILE ATTEMPTING TO LAND ON A ROAD 3 NAUTICAL MILES SOUTH OF THE AIRPORT AT OROVILLE, CALIFORNIA. THE PRIVATE PILOT AND TWO PASSENGERS SUSTAINED NO INJURIES. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE PLEASURE FLIGHT TO CHICO, WHICH ORIGINATED IN LONG BEACH WITH AN INTERMEDIATE STOP IN SANTA PAULA, CALIFORNIA. THE PILOT STATED HE WAS FLYING FROM LONG BEACH TO REDMOND, OREGON FOR A FLY-IN AT A KIT PLANE MANUFACTURER. THE DAY BEFORE HE DEPARTED, HE ASKED THAT THE AIRPLANE BE FILLED WITH FUEL, RATHER THAN TO THE TAB MARKERS AS WAS NORMALLY DONE. THE PILOT'S OPERATING HANDBOOK (POH) INDICATED FUEL CAPACITY WAS 24 GALLONS PER TANK WHEN FULL AND 17 GALLONS WHEN FILLED TO THE TABS. A REVIEW OF THE OPERATOR'S RECORDS REVEALED THE AIRPLANE COMPLETED A 1.4 HOUR FLIGHT 4 DAYS EARLIER AND WAS SERVICED WITH 14 GALLONS OF FUEL. FUEL RECEIPTS SHOWED AN ADDITIONAL 12.2 GALLONS WERE DISPENSED THE DAY BEFORE THE ACCIDENT FLIGHT. THE PILOT STATED HE PLANNED FOR 3.5 HOURS ENROUTE TO CHICO WHERE HE WOULD STOP FOR FUEL. DEPARTURE FROM LONG BEACH WAS DELAYED UNTIL 1332 DUE TO INCLEME NT WEATHER. THE PILOT HEADED EAST PAST CORONA, CA., THEN FLEW TOWARD LANCASTER, CALIFORNIA. DUR TO MOUNTAIN OBSCURATION, HE SAID HE COULD NOT PROCEED AS PLANNED AND LANDED AT SANTA PAULA. HE SAID HE PERSONALLY FILLED THE TANKS TO FULL CAPACITY. THE RECEIPT INDICATED HE DISPENSED 20.59 GALLONS. AFTER DEPARTING SANTA PAULA, THE PILOT MAINTAINED AN ALTITUDE OF 1,000 FEET (MSL) UNTIL PAST SANTA BARBARA, CALIFORNIA. AT GAVIOTA VOR HE CLIMBED TO 6,500 MSL. HE MAINTAINED THAT ALTITUDE UNTIL PASO ROBLES, CA. WHERE HE DESCENDED TO 4,500 FEET. WHEN HIS GLOBAL POSITIONING SYSTEM INDICATED HE WAS 18 NAUTICAL MILES FROM CHICO, HE COMMENCED A GRADUAL DESCENT. HE MAINTAINED A POWER SETTING OF 2,500 RPM IN CRUIS FLIGHT. HE LEANED THE MIXTURE TO 100 DEGREES RICH OF PEAK EXHAUST GAS TEMPERATURE (EGT). HE STATED THAT FROM TAKEOFF AT 1552, UNTIL 1650, HE OPERATED FROM THE RIGHT FUEL TANK. THEN HE SELECTED THE LEFT TANK. AT 1750, HE SWITCHED TO THE RIGHT TANK AGAIN. HE NOTED THE LEFT FUEL QUANTITY GAUGE WAS SLIGHTLY ABOVE THE HALF TANK MARK. HE SWITCHED BACK TO THE LEFT TANK AT 1850. HE OBSERVED THAT THE RIGHT TANK FUEL QUANTITYINDICATOR WAS BOBBING JUST ABOVE EMPTY. ABOUT 1915, THE ENGINE RPM LOWERED THE PILOT TURNED THE ELECTRIC BOOST PUMP ON AND SWITCHED TO THE RIGHT TANK. HE OBSERVED THE LEFT TANK WAS INDICATING EMPTY. THE FUEL PRESSURE CAME UP AND ENGINE POWER WAS RESTORED FOR APPROX. 1 MINUTE BEFORE THE ENGINE AGAIN LOST POWER. THE PILOT LANDED ON A ROAD WITH NO TRAFFIC. THE LEFT WING TIP CONTACTED A ROAD REFLECTOR. THE AIRPLANE VEERED OFF THE ROAD, THROUGH A BARBED WIRE FENCE, ONTO A ROCKY SLOPE AND THE NOSE GEAR COLLAPSED.

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 N2161G · 1

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