19980805019779A

Accident · Substantial damage

FAA accident report · Univar 108-1 · Delta Junction, AK · August 5, 1998

Date
August 5, 1998 · 10:30 local
Place
Delta Junction, AK
Phase of flight
Takeoff Ground Roll
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N8835K
NTSB investigation
NTSBANC98LA117
Reported as
Univar 1081
Reported engine
Franklin 6A4150B3
People aboard
2
Fatal injuries
0
Pilot’s flight hours
20,000 total85 in this make and model260 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.

Acft crashed on takeoff. (.4) on August 5, 1998, about 1030 Alaska daylight time, a wheel equipped Stinson 108-1 airplane, N8835K, sustained substantial damage during takeoff from an off airport site located about 70 miles southwest of Delta Junction, Alaska. The airplane was being operated as a visual flight rules (VFR) personal flight under title 14, CFR part 91, when the accident occurred. The certificated airline transport pilot, and the one passenger aboard were not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The flight was returning to Delta Junction, where it had departed on August 3. In his written statement to the national transportation safety board (NTSB), the pilot noted that he was attempting a southwesterly departure from a 750 feet long dry creek bed. He stated that during the takeoff roll, and about 700 feet down the creek bed, he applied 25 degrees of flaps. He said that the airplane became airborne, but failed to gain sufficient altitude to clear rising terrain. The airplane's right wing collided with a stand of trees, pivoting the airplane to the right, and the left wing struck the ground. The airplane's wings, and l ower left longeron sustained substantial damage. The pilot reported that the wind conditions at the time of the accident were light and variable, favoring a southwesterly departure.

As the FAA filed it

ACFT CRASHED ON TAKEOFF. (.4) ON AUGUST 5, 1998, ABOUT 1030 ALASKA DAYLIGHT TIME, A WHEEL EQUIPPED STINSON 108-1 AIRPLANE, N8835K, SUSTAINED SUBSTANTIAL DAMAGE DURING TAKEOFF FROM AN OFF AIRPORT SITE LOCATED ABOUT 70 MILES SOUTHWEST OF DELTA JUNCTION, ALASKA. THE AIRPLANE WAS BEING OPERATED AS A VISUAL FLIGHT RULES (VFR) PERSONAL FLIGHT UNDER TITLE 14, CFR PART 91, WHEN THE ACCIDENT OCCURRED. THE CERTIFICATED AIRLINE TRANSPORT PILOT, AND THE ONE PASSENGER ABOARD WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND NO FLIGHT PLAN WAS FILED. THE FLIGHT WAS RETURNING TO DELTA JUNCTION, WHERE IT HAD DEPARTED ON AUGUST 3. IN HIS WRITTEN STATEMENT TO THE NATIONAL TRANSPORTATION SAFETY BOARD (NTSB), THE PILOT NOTED THAT HE WAS ATTEMPTING A SOUTHWESTERLY DEPARTURE FROM A 750 FEET LONG DRY CREEK BED. HE STATED THAT DURING THE TAKEOFF ROLL, AND ABOUT 700 FEET DOWN THE CREEK BED, HE APPLIED 25 DEGREES OF FLAPS. HE SAID THAT THE AIRPLANE BECAME AIRBORNE, BUT FAILED TO GAIN SUFFICIENT ALTITUDE TO CLEAR RISING TERRAIN. THE AIRPLANE'S RIGHT WING COLLIDED WITH A STAND OF TREES, PIVOTING THE AIRPLANE TO THE RIGHT, AND THE LEFT WING STRUCK THE GROUND. THE AIRPLANE'S WINGS, AND L OWER LEFT LONGERON SUSTAINED SUBSTANTIAL DAMAGE. THE PILOT REPORTED THAT THE WIND CONDITIONS AT THE TIME OF THE ACCIDENT WERE LIGHT AND VARIABLE, FAVORING A SOUTHWESTERLY DEPARTURE.

NTSB investigation

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