- Date
- January 17, 1999, 13:30 local (21:30 UTC)
- Place
- No Las Vegas, NV
- Injuries
- 1 uninjured
- Damage
- Destroyed
- Phase of flight
- Maneuvering
- Aircraft
- N857JAAbraham J G II/Erickson K ONE Design
- Weather
- Visual (VMC) · Day
- Status
- Completed · report November 30, 2000
- Report
- Approved by Office Director
- FAA report
- 19990117000529A
- Case key
- 45665
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
The separation of the left rudder control cable from the rudder horn due to the improper installation of a nicopress fitting that secured the cable to the control horn.
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 indicated the purpose of the flight was to practice outside snap rolls. When he pressed on the left rudder pedal, it went all the way to the floor with no resistance. He reported that the airplane was in straight and level flight when he reached down to verify that the cable was detached, hoping to be able to control the airplane when he realized that the cable was slack from the rear of the airplane. He then informed the tower of the emergency. The airplane entered a right bank from which the pilot could not recover and he jumped out of the airplane and parachuted to safety. The airplane wreckage was examined. The right rudder cable was found continuous from the cockpit pedal to the rudder control horn, with the horn end of the cable secured with a nicopress fitting. The left rudder cable was attached to the cockpit pedal but was detached from the rudder horn. The left cable to horn nicopress fitting was not on the cable's horn end and the left rudder cable end exhibited long and even splaying. When the cable was stretched out, it went all the way back to the rudder horn and was nearly identical in length to the right cable. A search of the accident site failed to locate the missing nicopress fitting.
Factual narrative
On January 17, 1999, at 1330 hours Pacific standard time an experimental Abraham One Design airplane, N857JA, was destroyed when it impacted terrain while maneuvering approximately 14 miles north of the North Las Vegas Airport, Las Vegas, Nevada. The airplane was operated by the pilot under the provisions of 14 CFR Part 91. Visual meteorological conditions prevailed for the local flight and no flight plan was filed. The pilot/owner, the sole occupant, parachuted from the airplane and was not injured. The flight had departed the North Las Vegas airport at 1300.
In an interview with the Safety Board investigator, the pilot reported that he had gone out to the practice area to practice outside snap rolls. He stated that he had entered the snap roll at 5,500 feet mean sea level. The pilot reported that while in straight and level flight he "stomped" on the left rudder and reported that the rudder pedal went all the way to the floor. He reported that the airplane was in straight and level flight when he reached down to verify that the cable was detached, hoping to hand fly it when he realized that the cable was slack from the rear of the airplane. He then informed the tower of the emergency. The airplane entered a right bank from which the pilot could not recover and he jumped out of the airplane and parachuted to safety. The pilot reported that there were no further mechanical malfunctions noted with the airplane or engine beyond the rudder control system.
An officer from the North Las Vegas Police Department Aero Bureau unit responded to the accident site and examined the airplane wreckage. The right rudder cable was found continuous from the cockpit pedal to the rudder control horn, with the horn end of the cable secured with a nicopress fitting. The left rudder cable was attached to the cockpit pedal but was detached from the rudder horn. The left cable to horn nicopress fitting was not on the cable's horn end. He noted that the left rudder cable end exhibited long and even splaying. He reported that when the cable was stretched out, it went all the way back to the rudder horn and was nearly identical in length to the right cable. A search of the accident site failed to locate the missing nicopress fitting.
Aircraft
- Registration
- N857JA
- Reported as
- Abraham J G II/Erickson K ONE Design
- Category
- Airplane, amateur-built
- Serial number
- 0004
- Airframe hours
- 66
- Engine
- Lycoming IO-360, 210 horsepower, reciprocating
- Damage
- Destroyed
- Flight
- Personal · Part 91
- Registered owner
- James G Abraham II
- Airworthiness certificate
- Special, Experimental (Special)
- Departed
- VGT
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
- 41
- Certificate
- Commercial
- Airplane ratings
- Single-engine land
- Medical
- Class 3, Valid Medical--no waivers/lim.
- Seat
- Center
- Flight hours
- 640 total · 25 in this make and model · 525 as pilot in command · 50 in the last 90 days · 20 in the last 30 days · 3 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- Calm
- Visibility
- 20 statute miles
- Lowest ceiling
- 20,000 ft overcast
- Temperature
- 57 °F, dew point 28 °F
- Altimeter
- 30.00 inHg
- Observed at
- VGT, 14 nm away
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.