- Date
- June 20, 2011, 12:40 local (18:40 UTC)
- Place
- Caldwell, ID
- Injuries
- 2 minor, 7 uninjured
- Damage
- Substantial damage
- Phase of flight
- Takeoff
- Aircraft
- N3278QCessna 402
- Defining event
- Takeoff: Loss of engine power (total)
- Weather
- Visual (VMC) · Day
- Status
- Completed · report November 7, 2012
- Report
- Approved by Office Director
- NTSB office
- Western Pacific Region
- Parties
- Boise FSDO, Continental Motors
- FAA report
- 20110620013869A
- Case key
- 80830
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 total loss of power in one engine during takeoff due to the blockage of fuel flow by a foreign object in the fuel tank.
Findings · 2
NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.
Sequence of events
The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.
Analysis
The pilot of the skydiving airplane was performing the first takeoff of the day, and he had just raised the landing gear when the airplane experienced a complete loss of power in one of its two engines. There was still runway remaining, and the pilot made the decision to abort the takeoff. Because the airplane was at a very low altitude, the pilot was not sure that all three landing gear would fully extend before the airplane touched down. Therefore, he elected to keep the landing gear retracted, and the airplane touched down on the soft/rough terrain adjacent to the runway. Although no anomalies related to the engine were found, three pieces of poly-isoprene (synthetic rubber) were found in the fuel tank associated with the engine that lost power. Each individual piece was large enough to plug the orifice to the fuel boost pump, and it is likely that one or more of the pieces interrupted the fuel flow to the engine and resulted in the loss of power.
Factual narrative
On June 20, 2011, about 1240 mountain daylight time, a Cessna 402, N3278Q, impacted the terrain after a rejected takeoff at Caldwell Independent Airport, Caldwell, Idaho. The commercial pilot and one of his passengers received minor injuries, and the remaining seven passengers were not injured. The airplane, which was owned and operated by the pilot, sustained substantial damage to its fuselage. The local 14 Code of Federal Regulations Part 91 skydiving flight, which was in the takeoff sequence at the time of the accident, was being operated in visual meteorological conditions. No flight plan had been filed. According to the pilot, he taxied from the location where the airplane was normally kept, to the location where he picked up eight skydivers for the first drop of the day. After picking up the skydivers he taxied to the active runway where he completed the pre-takeoff checklist and engine run-up. He then initiated the takeoff roll, lifted off, and raised the landing gear. Just after he retracted the landing gear, the airplane's right engine experienced a complete loss of power. At that point, because there was still runway remaining, the pilot elected to abort the takeoff, and in order to keep the airplane upright, he pulled the throttle for the left engine to the idle position. Because he was very low over the ground, and he could not be assured of the timely extension of all three landing gear, the pilot decided not to extend the landing gear prior to the airplane settling back to the grass and dirt runway. During the process of touching down and sliding over the rough/soft terrain, the airplane's airframe became substantially damaged. After the accident the right engine was examined, to include the exhaust assembly, air induction assembly, magnetos and ignition assembly, spark plugs, fuel pump, fuel manifold valve, fuel lines and injection nozzles, air throttle assembly, fuel metering unit, lubrication system, oil filter, cylinders, rocker assemblies, accessory drive gear, alternator, and turbocharger. The examination did not reveal any anomalies that would have prevented the engine from operating and producing rated horsepower. After the removal of the drain plug from the right fuel tank in order to drain all of the remaining fuel, three pieces of what appeared to be latex-like thin film material were drained from the tank. One piece was cylindrical in shape, and the other two were flat sheets. All were irregular in shape, and all were seamless. All were translucent and light green/grey in color and very flexible. Each of the pieces was large enough by itself to block the 1.375 inch wide fuel boost pump inlet screen orifice, and all three pieces, when placed in a jar of 100 low-lead aviation fuel, sank to the bottom. It was not determined when or how the material had entered the fuel tank. After the initial on-scene examination, two of the three pieces were sent to the NTSB Materials Laboratory for further examination. The laboratorydetermined that the thickness of the material was 0.002 inches, and a Fourier Transform Infrared Spectrometer analysis determined that the material was most likely poly-isoprene. Poly-isoprene is also known as synthetic rubber.
Aircraft
- Registration
- N3278Q
- Reported as
- Cessna 402
- Category
- Airplane
- Serial number
- 402-0078
- Engines
- Cont Motor TSIO-520-E, 300 horsepower, reciprocatingCont Motor TSIO-520-E, 300 horsepower, reciprocating
- Damage
- Substantial damage
- Flight
- Skydiving · Part 91
- Operator
- Janes Denise M
- Registered owner
- Janes Denise M
- Airworthiness certificate
- Special, Restricted (Special)
- Last inspection
- Annual · May 17, 2011
- Departed
- KEUL · Caldwell, ID
- Destination
- KEUL · Caldwell, ID
- Airport
- KEUL · Caldwell Independent Airport, runway 30, 5,500 × 100 ft, grass/turf
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
- 56
- Injuries
- Minor
- Certificate
- Commercial
- Airplane ratings
- Single-engine land, Multi-engine land
- Medical
- Class 2, With waivers/limitations
- Last flight review
- November 7, 2010
- Seat
- Left
- Flight hours
- 6,100 total · 100 in the last 90 days
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 290° at 8 knots
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 81 °F
Docket · 7
The files NTSB released with the investigation on August 13, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 9.4 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.