- Date
- September 7, 2020, 13:00 local (20:00 UTC)
- Place
- Whitmore, AZ
- Injuries
- 8 uninjured
- Damage
- Substantial damage
- Phase of flight
- Landing
- Aircraft
- N186GCCessna 208
- Defining event
- Landing-landing roll: Sys/Comp malf/fail (non-power)
- Weather
- Visual (VMC) · Day
- Status
- Completed
- Report
- Approved by Office Director
- Investigation class
- Class 4 - Basic report with no Prelim publish
- NTSB office
- Western Pacific Region
- Parties
- FAA - FSDO
- FAA report
- 20200907014369A
- Case key
- 101931
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
A loss of directional control during landing due to a flat main landing gear tire, which resulted in a lateral runway excursion and impact with terrain.
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
**This report was modified on December 5, 2024. Please see the docket for this accident to view the original report.** The pilot reported that, during the landing ground roll, the airplane started to veer left. He applied right rudder input, but the airplane continued to “drag” left. As the pilot repositioned his feet to apply the brakes, the airplane “turned harder to the left,” exited the runway, and impacted terrain. The right wing was substantially damaged. The pilot thought that “a left main tire malfunction on or before landing” had occurred. An examination of the left wheel and tire assembly (by the Federal Aviation Administration) found that the valve stem to the tire inner tube had completely sheared off and was located inside the tire. No other damage to the inner tube was noted, and no other anomalies were observed within the assembly. The operator’s director of maintenance reported no preimpact mechanical malfunctions or failures that would have precluded normal operation. A video recording of the accident landing (taken by a passenger in the first row of passenger seats) indicated that, based on the sound recorded, the left main landing gear tire became flat immediately after main gear touchdown. The left flat tire would have increased the drag between the tire and the runway surface, resulting in a left-turning tendency and a loss of directional control. In addition, a photograph taken during the on-scene investigation showed a double track on the runway starting near the location where the left main tire touched down. The double track was likely caused by the rubber in the left and right sidewalls of the tire contacting the runway after the center of the tire deflated. The left main landing gear tire was installed on the airplane 3 days before the accident. The tire could have become flat if it had been improperly installed or had a material defect. It is also possible that the tire became flat because it hit something not heard or seen on the video of the landing. In addition, another photograph taken during the on-scene investigation showed that the valve stem of the tire inner tube was sheared, indicating that the tire could have become flat because the valve (within the valve stem) had failed. The failure mode for the left main landing gear tire could not be determined based on the available evidence. Nevertheless, the evidence was sufficient to show that the reason for the airplane’s loss of lateral directional control was the flat left main tire.
Aircraft
- Registration
- N186GC
- Reported as
- Cessna 208 (B)
- Category
- Airplane
- Serial number
- 208B2161
- Built
- 2009
- Airframe hours
- 8,044.3
- Engine
- Pratt & Whitney Canada PT6A-114A, 675 horsepower, turbo prop
- Damage
- Substantial damage
- Flight
- Other work use · Part 135
- Operator
- Grand Canyon Airlines
- Registered owner
- Zuni Llc
- Airworthiness certificate
- Standard, Normal
- Last inspection
- AAIP · August 22, 2020 · 35.8 hours before
- Departed
- KBVU · Boulder City, NV
- Destination
- Same as departure
- Airport
- 1Z1 · Grand Canyon Bar Ten Airstrip, runway 34, 4,600 × 40 ft, asphalt
- Equipment
- Electronic primary flight display, Angle of attack indicator, Onboard weather, ADS-B, Stall warning system
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
- 57
- Injuries
- None
- Certificate
- Commercial
- Airplane ratings
- Multi-engine land, Single-engine land
- Instrument ratings
- Airplane
- Medical
- Class 1, With waivers/limitations
- Last flight review
- August 25, 2020
- Seat
- Left
- Restraint
- 5-point
- Flight hours
- 1,460 total · 600 in this make and model · 1,210 as pilot in command · 216 in the last 90 days · 70 in the last 30 days · 3 in the last 24 hours
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 350° at 6 knots, gusting 14
- Visibility
- 10 statute miles
- Lowest ceiling
- None
- Temperature
- 102 °F, dew point 32 °F
- Altimeter
- 30.02 inHg
- Observed at
- KAZC, 43 nm away
Docket · 10
The files NTSB released with the investigation on July 12, 2021, on NTSB’s docket system: statements, records, photos and specialists’ reports. 12.5 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.