LAX02LA010

NTSB accident investigation · Rhoades Jodel D-9 · Waialua, HI · October 21, 2001

Accident · FatalLimited investigationFinal report
Date
October 21, 2001, 12:57 local (22:57 UTC)
Place
Waialua, HI
Injuries
1 fatal
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N43RRRhoades Jodel D-9
Weather
Visual (VMC) · Day
Status
Completed · report May 1, 2003
Report
Approved by Office Director
Parties
FEDERAL AVIATION ADMINISTRATION
FAA report
20011021028859A
Case key
53648

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

Loss of engine power for unknown reasons. A factor was the inadvertent stall the pilot encountered while maneuvering to make a forced landing in an open taro field.

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.

Loss of engine powerCruise
Reason for occurrence undeterminedCause
Forced landingDescent - emergency
Loss of control - in flightManeuvering - turn to reverse direction
Airspeed - not maintainedPilot in commandCause
Stall - encounteredPilot in commandFactor
In flight collision with terrain/waterManeuvering - turn to reverse direction
Terrain condition - ground

Analysis

The pilot maneuvered to make an off-airport landing due to a loss of engine power. During the turn to land the airplane's wing dropped, the airplane stalled and spun into the ground. There were no radio communications from the accident pilot indicating that he had a problem. During the on-scene inspection the FAA did not observe fuel or smell evidence of fuel on the ground or around the airplane. There were no discrepancies noted with the engine.

Factual narrative

History of flight

On October 21, 2001, at 1257 Hawaiian standard time, an experimental Rhoades Jodel D-9, N43RR, experienced a loss of engine power and crashed into a taro field near Waialua, Hawaii, approximately 2 miles east of the Dillingham Airfield Airport, Mokuleia, Hawaii. The airplane, owned and operated by the pilot under the provisions of 14 CFR Part 91, sustained substantial damage. The airline transport pilot, the sole occupant, sustained fatal injuries. Visual meteorological conditions prevailed for the personal flight to the Honolulu International Airport, Honolulu, Hawaii, and a visual flight rules (VFR) flight plan had been filed. The flight had departed the Dillingham Airfield Airport at 1246.

The wreckage was examined at the accident site. One wooden propeller blade was fractured near the hub. The blade did not exhibit any tip damage. There was no evidence of fuel on the ground or around the airplane.

Witness information

A ground witness stated that earlier in the day the airplane had taxied past him on the taxiway three times. The first two times the engine stopped and then started again. The witness reported that it sounded like the pilot "played with the throttle" to get the airplane started again. On the third taxi the witness stated that the engine stopped; the pilot restarted the engine and taxied back to his hangar.

Another ground witness stated that he saw the pilot prior to departure from Dillingham. The accident pilot performed a preflight, and the witness hand-propped the engine to start it. There was no starter for the airplane, so hand propping was the only way to start it. The witness observed the pilot taxi down the runway and takeoff. The accident pilot went around the pattern a few times and then landed and taxied back to the hangar area. The witness stated that he did not see or hear anything unusual with the airplane, and the pilot seemed satisfied with the flight. The witness observed the pilot adding fuel to the airplane. The witness and another individual then followed the accident airplane to the runway in another airplane. The purpose was to follow the accident airplane to Honolulu.

The witness stated that after departure from Dillingham he lost sight of the accident airplane. When he saw the accident airplane again it was headed in the opposite direction back towards Dillingham. He thought there was a problem and that the accident pilot was intending to land back at the airport. The witness observed the airplane at a low altitude and indicated that the airplane appeared to be under control. The witness thought that the pilot was looking for somewhere to land. At the last minute he saw the wing drop and the airplane start to spin. The witness stated that the airplane impacted the ground in a nose down attitude.

The Safety Board investigator interviewed a witness who was trailing the accident airplane and acting as an escort. He was about 1/2 mile behind the airplane, and then lost sight of it. He initiated a turn in the opposite direction to look for the accident airplane. He saw the airplane headed back towards Dillingham, at a low altitude, apparently looking for a place to land. The witness stated that as the pilot turned left, the airplane appeared to "snap roll" to the right and into the ground.

Personnel information

Review of Airman Certification records disclosed that the pilot held an airline transport pilot certificate with a multiengine land rating, and private pilot single engine land rating. He also held an airframe and power plant certificate. The pilot's personal logbooks were not available for review. The most recent first-class medical was issued on July 13, 2001, with a restriction for corrective lenses.

Aircraft information

Review of the airplane logbook disclosed that the airplane had been disassembled in Burbank, California, on October 31, 1999, and shipped to Honolulu. On May 25, 2001, the airplane was inspected and found to comply with the requirements of FAR Part 91. The Experimental - Amateur Built Standard Operating Limitations were also dated May 25, 2001.

Tests and research

A visual inspection of the engine was conducted with all components found intact and in place. There was no obvious external damage to the engine. The magneto was inspected due to a prior incident where the magneto had lifted out of its holding slot. The owner had remedied the situation by clamping down the magneto. The magneto was found secure on its mounting pad. The magneto was removed for further examination with no signs of failure or wear of the internal wear. No further discrepancies were noted with the engine.

Medical and pathological information

A toxicological analysis was performed by the Federal Aviation Administration Civil Aeromedical Institute, Oklahoma City, Oklahoma, from samples obtained during the autopsy. The results of the analysis were negative for carbon monoxide, cyanide, ethanol, and drugs.

Aircraft

Registration
N43RR
Reported as
Rhoades Jodel D-9
Category
Airplane, amateur-built
Serial number
JODEL D-9-R-1
Airframe hours
372
Engine
Volkswagen Conversion, 36 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Ronald K. Haenel
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · May 25, 2001
Departed
HDH · Mokuleia, HI
Destination
HNL · Honolulu, HI
Flight plan
VFR
Airport
HDH · Dillingham Airfield

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
39
Injuries
Fatal
Certificate
Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--w/ waivers/lim
Seat
Front
Toxicology
Performed
Flight hours
2,700 total

Weather

Conditions
Visual (VMC) · Day
Wind
30° at 13 knots, gusting 23
Visibility
10 statute miles
Lowest ceiling
None
Temperature
84 °F, dew point 63 °F
Altimeter
29.96 inHg
Observed at
HNL, 44 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.