19990918028429A

Accident · Substantial damage

FAA accident report · Cessna 180 · Palmer, AK · September 18, 1999

Date
September 18, 1999 · 11:30 local
Place
Palmer, AK
Phase of flight
Ground Taxi, Other Airplane
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2294C
NTSB investigation
NTSBANC99LA157
Reported as
Cessna 180
Reported engine
Continental O470J
People aboard
1
Fatal injuries
0
Pilot’s flight hours
2,000 total1,000 in this make and model

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 September 18, 1999, about 1200 Alaska daylight time, a Cessna 180 airplane, N2294C, sustained substantial damage during landing at an off airport landing site about 25 miles east of Palmer, Alaska, at 61 degrees 19 minutes north latitude, 148 degrees 28 minutes west longitude. The solo commercial pilot was not injured. The personal flight was conducted under 14 CFR part 91. The flight departed the Palmer airport, Palmer, about 1140 on the second trip that day to the pilot's hunting camp. Visual meteorological conditions prevailed at the time of the accident, and no flight plan was filed. During a telephone interview with the NTSB investigator-in-charge (iic) on October 13, the pilot stated that he was taxiing after landing on a gravel bar. He said the ground was soft and muddy, so he kept the airplane moving so the airplane would not become stuck. The pilot said the wheels bogged down during the taxi, and the airplane nosed over. The vertical stabilizer and the right wing outboard of the lift strut sustained substantial damage. The pilot stated the ceiling was about 5,500 feet overcast, and the visibility was 5 miles in rain. He indicated the winds had increased f rom his earlier trip to the same location, and were blowing from the northwest at 30 knots, with gusts to 50 knots. (-23) during taxi after landing the pilot said he added power to keep the aircraft moving because the ground was soft & muddy, as the wheels bogged down the airplane nosed over, then the wind blew the aircraft over on its back. Airman has not provided hours last 90 days or date of last regulatory checkride. (.4) the pilot was taxiing the airplane after landing on a gravel and clay bar the second time that day. He said the ground was soft and muddy, so he kept the airplane moving so it would not become stuck. The wheels bogged down during the taxi, the airplane nosed down, and the wind carried the airplane over onto its back. The vertical stabilizer and the right wing outboard of the lift strut sustained substantial damage. The pilot said the visibility was 5 miles in rain, and the winds had increased from the first trip, and were 25 knots, with gusts to 40 knots.

As the FAA filed it

(.19) ON SEPTEMBER 18, 1999, ABOUT 1200 ALASKA DAYLIGHT TIME, A CESSNA 180 AIRPLANE, N2294C, SUSTAINED SUBSTANTIAL DAMAGE DURING LANDING AT AN OFF AIRPORT LANDING SITE ABOUT 25 MILES EAST OF PALMER, ALASKA, AT 61 DEGREES 19 MINUTES NORTH LATITUDE, 148 DEGREES 28 MINUTES WEST LONGITUDE. THE SOLO COMMERCIAL PILOT WAS NOT INJURED. THE PERSONAL FLIGHT WAS CONDUCTED UNDER 14 CFR PART 91. THE FLIGHT DEPARTED THE PALMER AIRPORT, PALMER, ABOUT 1140 ON THE SECOND TRIP THAT DAY TO THE PILOT'S HUNTING CAMP. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME OF THE ACCIDENT, AND NO FLIGHT PLAN WAS FILED. DURING A TELEPHONE INTERVIEW WITH THE NTSB INVESTIGATOR-IN-CHARGE (IIC) ON OCTOBER 13, THE PILOT STATED THAT HE WAS TAXIING AFTER LANDING ON A GRAVEL BAR. HE SAID THE GROUND WAS SOFT AND MUDDY, SO HE KEPT THE AIRPLANE MOVING SO THE AIRPLANE WOULD NOT BECOME STUCK. THE PILOT SAID THE WHEELS BOGGED DOWN DURING THE TAXI, AND THE AIRPLANE NOSED OVER. THE VERTICAL STABILIZER AND THE RIGHT WING OUTBOARD OF THE LIFT STRUT SUSTAINED SUBSTANTIAL DAMAGE. THE PILOT STATED THE CEILING WAS ABOUT 5,500 FEET OVERCAST, AND THE VISIBILITY WAS 5 MILES IN RAIN. HE INDICATED THE WINDS HAD INCREASED F ROM HIS EARLIER TRIP TO THE SAME LOCATION, AND WERE BLOWING FROM THE NORTHWEST AT 30 KNOTS, WITH GUSTS TO 50 KNOTS. (-23) DURING TAXI AFTER LANDING THE PILOT SAID HE ADDED POWER TO KEEP THE AIRCRAFT MOVING BECAUSE THE GROUND WAS SOFT & MUDDY, AS THE WHEELS BOGGED DOWN THE AIRPLANE NOSED OVER, THEN THE WIND BLEW THE AIRCRAFT OVER ON ITS BACK. AIRMAN HAS NOT PROVIDED HOURS LAST 90 DAYS OR DATE OF LAST REGULATORY CHECKRIDE. (.4) THE PILOT WAS TAXIING THE AIRPLANE AFTER LANDING ON A GRAVEL AND CLAY BAR THE SECOND TIME THAT DAY. HE SAID THE GROUND WAS SOFT AND MUDDY, SO HE KEPT THE AIRPLANE MOVING SO IT WOULD NOT BECOME STUCK. THE WHEELS BOGGED DOWN DURING THE TAXI, THE AIRPLANE NOSED DOWN, AND THE WIND CARRIED THE AIRPLANE OVER ONTO ITS BACK. THE VERTICAL STABILIZER AND THE RIGHT WING OUTBOARD OF THE LIFT STRUT SUSTAINED SUBSTANTIAL DAMAGE. THE PILOT SAID THE VISIBILITY WAS 5 MILES IN RAIN, AND THE WINDS HAD INCREASED FROM THE FIRST TRIP, AND WERE 25 KNOTS, WITH GUSTS TO 40 KNOTS.

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 N2294C · 2

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