- Date
- October 26, 2008, 12:30 local (19:30 UTC)
- Place
- Rialto, CA
- Injuries
- 1 uninjured
- Damage
- Substantial damage
- Phase of flight
- Initial climb
- Aircraft
- N44848Naval Aircraft Factory N3N-3
- Defining event
- Initial climb: Loss of engine power (total)
- Weather
- Visual (VMC) · Day
- Status
- Completed · report October 19, 2009
- Report
- Approved by Office Director
- NTSB office
- Western Pacific Region
- Parties
- Federal Aviation Administration
- FAA report
- 20081026851969A
- Case key
- 69359
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 NTSB’s determination of the probable cause, and any contributing factors.
A total loss of engine power during initial climb due to an interruption in fuel flow through an improperly assembled carburetor.
Findings · 2
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings.
Analysis
The pilot performed a preflight inspection of the company airplane in preparation for a local area round-robin flight. After all systems appeared to function normally, the pilot took off and flew to his first intended landing site. Then, the pilot took off for the return flight. According to the pilot, during the ensuing takeoff, the "engine power output and acceleration were normal." However, upon climbing about 150 feet above the runway, "the engine smoothly lost power....The power loss felt like the throttle lever [was] being smoothly closed from takeoff power to idle. There was no engine roughness, vibration, or perceived reduced power output preceding the loss of power, and no backfiring or sputtering [was] associated with the power loss." The pilot made a forced landing in an open field ahead of the airplane. The airplane collided with vegetation during the landing rollout. A teardown examination of the airplane's carburetor was performed, and internal anomalies were found regarding its assembly. The main fuel jets were found too small for the engine application, and the mixture shaft was improperly keyed and/or out of alignment with its respective track. This anomaly likely resulted in unreliable mixture settings and an interruption of fuel flow to the engine.
Factual narrative
The factual narrative543 words
On October 26, 2008 about 1230 Pacific daylight time, a Naval Aircraft Factory N3N-3, N44848, experienced a total loss of engine power seconds after takeoff from runway 24 at the Rialto Municipal Airport, Rialto, California. The airplane collided with vegetation during the forced landing in an open field about 1/2-mile southwest of the airport. The airplane was substantially damaged. The commercial certificated pilot was not injured. Visual meteorological conditions prevailed during the personal flight, and no flight plan was filed. The flight was performed under the provisions of 14 Code of Federal Regulations Part 91. The pilot reported to the National Transportation Safety Board investigator that the planned round-robin flight originated about 1205 from the Flabob Airport in Riverside. In pertinent part, the pilot reported to the Safety Board investigator that he performed a preflight inspection of the airplane, which was followed by a pretakeoff inspection. The single fuselage fuel tank was full of fuel. All systems appeared to function normally, and he initiated the planned hour-long local area flight. The pilot flew to the Rialto Municipal Airport, landed, and taxied back for takeoff. The accident occurred during the pilot's attempted return flight to Flabob. According to the pilot, during the ensuing takeoff, the "engine power output and acceleration were normal." However, upon climbing about 150 feet above the runway, "the engine smoothly lost power....The power loss felt like the throttle lever [was] being smoothly closed from takeoff power to idle. There was no engine roughness, vibration, or perceived reduced power output preceding the loss of power, and no backfiring or sputtering [was] associated with the power loss." The pilot made a forced landing in a nearby field. Seconds prior to landing, the engine "momentarily and smoothly regained power" for 5 to 7 seconds. Then, it "smoothly lost power a second time, again without roughness, backfiring, or sputtering." During rollout in the field, the airplane collided with a tree, which resulted in impact damage to the wings. Several hours later, the pilot recovered the airplane from the accident site under a police escort. The pilot reported that no fuel was added to the airplane's fuel tank. The pilot reported that he started the engine following normal procedures, and he taxied the airplane for about 15 minutes from the accident landing site to the airport, whereupon its engine was shut down. A company mechanic for the airplane's owner reported to the Safety Board investigator that when the owner purchased the airplane, it was equipped with the accident carburetor. Since the company's acquisition of the airplane, no maintenance had been performed to the carburetor. The Federal Aviation Administration coordinator reported to the Safety Board investigator that the airplane's engine was externally examined, and no evidence of any mechanical malfunction was apparent. Thereafter, theairplane's carburetor was removed and a teardown examination was performed by Aero Engines, Los Angeles, California. During the teardown examination, internal assembly anomalies were found. The owner's mechanic reported that the carburetor's "main jets were [found] too small for the engine application." This model carburetor may be installed on different models of engines. Also, the accident carburetor had been improperly assembled. The mixture shaft was improperly keyed and/or out of alignment with its respective track. This anomaly may result in unreliable mixture settings.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident.
Aircraft
- Registration
- N44848
- Reported as
- Naval Aircraft Factory N3N-3
- Category
- Airplane
- Serial number
- 4477
- Airframe hours
- 2,713
- Engine
- Lycoming R680, 300 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Personal · Part 91
- Airworthiness certificate
- Standard, Normal
- Last inspection
- Annual · September 26, 2008 · 3 hours before
- Departed
- L67 · Rialto, CA
- Destination
- RIR · Riverside, CA
- Airport
- L67 · Rialto Municipal, runway 24, 4,500 × 100 ft, asphalt
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
- 51
- Injuries
- None
- Certificate
- Commercial
- Airplane ratings
- Multi-engine land, Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, With waivers/limitations
- Last flight review
- October 8, 2007
- Seat
- Rear
- Flight hours
- 895 total · 21 in this make and model · 767 as pilot in command · 6 in the last 90 days · 3 in the last 30 days · 1 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 210° at 3 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 82 °F, dew point 25 °F
- Altimeter
- 30.07 inHg
- Observed at
- ONT, 10 nm away
Docket · 3
The files NTSB released with the investigation on August 28, 2009, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.4 MB in all.
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.