Cessna 170B accident near Centralia, Washington, April 28, 2015
On April 28, 2015 at about 6:45 pm local time, a 1958 Cessna 170B, registered N1296D, was substantially damaged in an accident during enroute (climb to cruise) near Centralia, Washington. It was a personal flight under general aviation rules (Part 91). 1 person was seriously injured. The weather was visual conditions (good weather).
The NTSB's probable cause their words, unchanged
Maintenance personnel’s incorrect installation of the fuel selector valvehandle, which resulted in fuel starvation, a loss of engine power, and a forced hard landing. Contributing to the accident was the pilot's failure to follow the manufacturer's checklist.
Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.
What the record shows
- Date
- April 28, 2015 · about 6:45 pm local time
- Place
- Centralia, Washington · map
- Type
- Accident
- Injuries
- 1 person was seriously injured.
- Weather
- visual conditions (good weather)
- Aircraft
- Cessna 170B, built 1958 · all 170Bs on the register
- Registration
- N1296D · no longer on the register · serial 25424
- Damage
- Substantial damage
- Flight
- Personal flight · general aviation rules (Part 91)
The NTSB's narrative final · quoted from the NTSB record
The airline transport pilot reported that he intended to accomplish the engine manufacturer-recommended break-in procedures after repair work was completed while he was en route to another airport to fuel the airplane. The repair work had required that the fuel tanks be drained. Upon completion of the work, the recovered fuel was put in the left fuel tank. The pilot reported that he did not have an exact measurement of fuel but that he estimated that it was about 15 gallons. He also added about 6 1/4 gallons of fuel to the right fuel tank as a backup reserve. The pilot took off with the fuel selector valve (FSV) in the "left" tank position. During the climb to cruise flight, about 2,000 ft above ground level, the airplane experienced a loss of engine power. The pilot's attempts to restart the engine were unsuccessful. During the descent, the pilot switched the fuel selector to the "both" position; however, the engine would not restart. The pilot subsequently conducted a forced landing in a field; he pulled the airplane's nose up to clear some tall trees, which resulted in a stall and a subsequent hard landing in the field. Postaccident examination of the wreckage revealed that the FSV was properly installed but that the selector handle was slightly right of the forward, or the "both," position. Further examination of the FSV handle revealed that it was incorrectly indexed to the drive shaft that coupled the handle to the FSV, which allowed the handle to be installed 180 degrees from its correct position. The observed handle orientation resulted in the FSV being closed (or off) when the FSV handle was in the "both" position, right when in the "left" position, and left when in the "right" position. The FSV was verified to be open when positioned in all three feed positions, and closed when positioned to "off." The FSV handle had a hole drilled in it at manufacture that was angled to prevent incorrect orientation of the handle. Another hole was observed drilled through the operating arm and handle, which allowed for the incorrect installation of the handle. The investigation could not determine when this hole was drilled. The pilot reported that, during takeoff, he believed that the fuel selector was positioned to the fuller left tank; however, due to the incorrect indexing to the drive shaft that coupled the handle to the FSV, the fuel selector was actually positioned and drawing fuel from the reserve right fuel tank, and the fuel in that tank was subsequently exhausted, which resulted in the loss of engine power. When the pilot positioned the fuel selector to the "both" position during the emergency procedures, the fuel selector valve was actually in the "off" position. The Pilot's Operating Handbook specified that the FSV should be in the "both" position during takeoff.
The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.
The factual record from the NTSB's investigation tables, in plain English
What happened, in order
- Fuel starvation during enroute (climb to cruise) defining event
- Off-field or emergency landing during landing
- Hard landing during landing
The NTSB's findings
- cause Aircraft › Aircraft systems › Fuel system › Fuel distribution › Incorrect service/maintenance
- cause Aircraft › Fluids/misc hardware › Fluids › Fuel › Related maintenance info
- cause Aircraft › Fluids/misc hardware › Fluids › Fuel › Fluid level
- cause Personnel issues › Task performance › Maintenance › Installation › Maintenance personnel
- factor Personnel issues › Task performance › Use of equip/info › Use of checklist › Pilot
Pilot
- Certificate: airline transport pilot
- Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instrument: airplane
- Flight time: 2,688 hours in all; 512 in this make and model; 10 in the last 90 days; 0 in the last 30 days
- Medical certificate: Class 2 (with waivers/limitations)
- Seat: left
- Injury: serious injuries
The aircraft
- Airframe total time: 3,740 hours
- Last inspection: annual inspection, April 25, 2015
- Maximum gross weight: 1,451 lb
- Seats: 4
- Landing gear: fixed
- Engine: Lycoming O-360-A1A (piston); 1,615 hours total
The flight
- Departed from: 3B8 Spanaway WA at 6:40 pm
- Destination: CLS Chehalis WA
- Flight plan: none
Weather at the time
- Light: daylight
- Wind: from 330° at 8 knots
- Visibility: 3 statute miles
- Sky: broken clouds at 3,500 ft; scat at 2,700 ft
- Temperature: 55°F (13°C), dew point 48°F (9°C)
- Altimeter: 30.13 inHg
- Observation at 6:56 pm from KCLS, 5 miles away
Injuries
| Fatal | Serious | Minor | None | |
|---|---|---|---|---|
| Flight crew | 1 |
Documents from the investigation the NTSB's docket: the evidence folder behind the report
The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.
Other NTSB records under N1296D the same tail number, which may have belonged to a different aircraft at the time
Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.
