- Date
- October 5, 1993, 17:15 local (21:15 UTC)
- Place
- Haines, AK
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Landing
- Aircraft
- N5285JPiper PA-18
- Weather
- Visual (VMC) · Night/dark
- Status
- Completed · report May 23, 1994
- Report
- Approved by Office Director
- NTSB office
- Alaska Regional Office
- FAA report
- 19931005040139A
- Case key
- 2469
From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.
On this page
Probable cause
Fatigue failure in a weld on the right main landing gear oleo strut tubing.
Sequence of events
NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.
Analysis
The pilot reported that he flared about 3 feet above the ground, then he 'cut' the throttle & the airplane 'dropped' onto the tundra. Both landing gear assemblies collapsed as the airplane touched down. The pilot reported there was a fracture in the welded section of the right oleo strut tubing. The airplane was equipped with 30 inch tundra tires.
Factual narrative
On October 5, 1993, at 1715 Alaska daylight time, a wheel equipped Piper PA-18 airplane, N5285J, owned and operated by the commercial rated pilot-in-command, crashed during a landing attempt at a remote landing site located approximately 4 miles north of Haines, Alaska. The pilot, the sole occupant, was not injured and the airplane sustained substantial damage. The personal flight, operating under 14 CFR Part 91, last departed Haines, Alaska, at 1700 and the destination was the remote landing site. Visual meteorological conditions prevailed and a VFR flight plan was not filed.
The pilot told the investigator-in-charge, during a telephone conversation, that he was surveying the area looking for mountain goats. During the landing attempt on the saddle back of the mountain, he flared too high and the airplane "dropped" onto the ground from a height estimated to be three to five feet. The airplane did not bounce. Both main landing gear structural assemblies collapsed. The airplane was equipped with 30 inch tundra tires. The pilot reported that his post accident inspection of the landing gear found a fracture in the welded section of the right oleo strut tubing. An inspection of the fuselage by the NTSB investigator-in-charge found a fracture in a longeron tube (a major structural member) in the area where the left forward landing gear ear attaches to the fuselage.
Aircraft
- Registration
- N5285J
- Reported as
- Piper PA-18
- Category
- Airplane
- Serial number
- 18-7143
- Airframe hours
- 694
- Engine
- Lycoming O-360, 180 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Registered owner
- Campbell, George R.
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · September 22, 1993 · 41 hours before
Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.
Flight crew
As NTSB recorded them. NTSB leaves out names.
- Role
- Pilot
- Age
- 26
- Certificate
- Commercial
- Airplane ratings
- Single-engine sea, Multi-engine land, Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, Valid Medical--w/ waivers/lim
- Seat
- Left
- Flight hours
- 1,350 total · 150 in this make and model · 1,120 as pilot in command · 140 in the last 90 days · 65 in the last 30 days · 3 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Night/dark
- Wind
- 330° at 3 knots
- Visibility
- 75 statute miles
- Lowest ceiling
- None
- Temperature
- 37 °F
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.
Other investigations on N5285J · 1
Matched to the same aircraft by N-number and date.