# NTSB WPR10LA121: American Champion 8KCAB, N101BY, Fallon, NV, January 27, 2010

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Limited investigation · Final report
- Date: January 26, 2010, 16:30 local (Jan 27, 2010, 00:30 UTC)
- Place: Fallon, NV
- Coordinates: 39.498889, -118.748611 (estimated)
- Nearby events: https://openairdocs.org/map.md?lat=39.4989&lon=-118.7486&mi=10
- Phase of flight: [Landing](https://openairdocs.org/ntsb-phases/550) (OpenAirDocs' grouping)
- Defining event: [Landing-landing roll: Sys/Comp malf/fail (non-power)](https://openairdocs.org/ntsb-events/330)
- Highest injury: No injuries
- Injuries: 2 uninjured
- Status: Completed, report May 3, 2012
- Report: Approved by Office Director
- NTSB office: Western Pacific Region
- Parties: Federal Aviation Administration
- SAIBs cited in the narratives: [SAIB CE-10-39](https://openairdocs.org/saib/CE-10-39) (OpenAirDocs)
- NTSB case key (mKey): 75319
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=WPR10LA121
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/75319/pdf
- NTSB docket: https://data.ntsb.gov/Docket?ProjectID=75319
- Page: https://openairdocs.org/ntsb/WPR10LA121

## Probable cause

Interference between the front seat lap belt and the rear seat rudder/brake pedal assembly that prevented normal operation of the rudder/brake system, which resulted in the pilots’ inability to maintain directional control.

## Findings

NTSB's coded findings; those marked are part of the probable cause.

- [Fuselage: seat/cargo attach fitting](https://openairdocs.org/ntsb-findings/01035347): Aircraft › Aircraft structures · Design (probable cause); cases with it: [American Champion 8KCAB, 1 case](https://openairdocs.org/ntsb-findings/01035347/cases.md?model=2121000), [All aircraft, 27 cases](https://openairdocs.org/ntsb-findings/01035347/cases.md)
- [Flight control system: rudder control system](https://openairdocs.org/ntsb-findings/01022720): Aircraft › Aircraft systems · Unintentional use/operation (probable cause); cases with it: [American Champion 8KCAB, 1 case](https://openairdocs.org/ntsb-findings/01022720/cases.md?model=2121000), [All aircraft, 93 cases](https://openairdocs.org/ntsb-findings/01022720/cases.md)
- [Performance/control parameters: directional control](https://openairdocs.org/ntsb-findings/01062020): Aircraft › Aircraft oper/perf/capability · Attain/maintain not possible (probable cause); cases with it: [American Champion 8KCAB, 6 cases](https://openairdocs.org/ntsb-findings/01062020/cases.md?model=2121000), [All aircraft, 3,958 cases](https://openairdocs.org/ntsb-findings/01062020/cases.md)

## Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event best describes what happened.

- [Landing-landing roll: Sys/Comp malf/fail (non-power)](https://openairdocs.org/ntsb-events/330) (defining event); cases with it: [American Champion 8KCAB, 1 case](https://openairdocs.org/ntsb-events/330/sequence.md?model=2121000), [All aircraft, 994 cases](https://openairdocs.org/ntsb-events/330/sequence.md)
- [Landing-landing roll: Loss of control on ground](https://openairdocs.org/ntsb-events/230); cases with it: [American Champion 8KCAB, 7 cases](https://openairdocs.org/ntsb-events/230/sequence.md?model=2121000), [All aircraft, 4,585 cases](https://openairdocs.org/ntsb-events/230/sequence.md)
- [Landing-landing roll: Nose over/nose down](https://openairdocs.org/ntsb-events/096); cases with it: [American Champion 8KCAB, 6 cases](https://openairdocs.org/ntsb-events/096/sequence.md?model=2121000), [All aircraft, 2,287 cases](https://openairdocs.org/ntsb-events/096/sequence.md)

## Analysis

The certified flight instructor (CFI), seated in the front seat, reported that the airplane started to drift to the right during the landing roll. The student pilot, seated in the rear seat, applied left rudder to counteract the drift, but the airplane continued to the right. The CFI took control of the airplane and applied full left rudder and full power; however, the airplane continued to the right until the left main landing gear collapsed and the airplane nosed over. The airplane was equipped with dual lap belt aerobatic harnesses. Postaccident examination revealed that, when full left rudder was applied, the front seat pilot's upper lap belt caught on the rear seat right rudder/brake pedal assembly and activated the right brake. As a result of this finding, the manufacturer issued an Airplane Flight Manual Supplement (AFMS) that provided guidance for pilots to examine the front seat lap belts for proper tension and clearance from the rear seat rudder pedals during their prestart and preflight checks. In addition, the Federal Aviation Administration issued a Special Airworthiness Information Bulletin (SAIB CE-10-39) that addressed proper installation of the dual lap belt system and informed pilots of the issuance of the AFMS pertaining to the lap belts.

## Factual narrative

On January 26, 2010, about 1630 Pacific standard time, an American Champion Aircraft 8KCAB, N101BY, departed runway 3 on landing and came to rest inverted at Fallon Municipal Airport (FLX), Fallon, Nevada. The airplane sustained structural damage to the collapsed left main landing gear and tail section of the airplane. The certified flight instructor (CFI) and the owner/pilot were not injured. The flight had departed FLX about 1530 for the local area flight, and no flight plan had been filed. According to the CFI, the flight was to familiarize the owner/pilot with a conventional landing-gear airplane. The owner was seated in the rear seat, and the CFI was seated in the front seat. The CFI demonstrated one landing prior to the flight departing the pattern for the local practice area in order to familiarize the pilot with the flight controls. They performed several turns, descents and climbs, and then returned to the airport for landing. The pilot performed two uneventful landings, and on the third landing just after touchdown, the CFI noted a moderate drift to the right. The CFI stated that the pilot had applied left rudder to counteract the drift, but the airplane continued to the right. At that point, the CFI took the flight controls and applied full left rudder and full power. The airplane continued to the right until the left main landing gear collapsed and the airplane nosed over. In the RECOMMENDATION section of the National Transportation Safety Board (NTSB) accident reporting form, the CFI reported that the front seat 5-point Hooker Aerobatic harness had a tendency to drape itself over the right rear cockpit rudder/brake pedal assembly. He stated that this could have caused the right brake to be inadvertently activated when full left rudder was applied. The airplane and seat belt mechanism were inspected by an airworthiness inspector from the Federal Aviation Administration (FAA). The FAA inspector confirmed the CFI's observation that with the application of full left rudder, the front pilot's seatbelt could catch on the right rudder/brake pedal assembly as it was moving aft due to left rudder input. This action inadvertently allowed the application of the right brake. The NTSB docket for this accident contains a video that demonstrates this interaction. The FAA inspector also examined the dual lap belt installation. According to the airplane manufacturer, American Champion, the only dual lap belt installation they use is the Hooker Aerobatic harness. That harness consisted of two lap belts sewn in parallel with one another on top of a large pad that is worn across the lap of the pilot. The FAA inspector reported that the two lap belts were connected to a single point, the outer lug on the floor. According to a drawing from American Champion, the dual lap belt should attach to two separate locations instead of just the outer floor lug. FAA inspectors from the Chicago Aircraft Certification Office visited both American Champion inRochester, Wisconsin, and Gauntlet Warbirds, in Aurora, Illinois, to review possible rudder interference by the lap belt installation on the 8KCAB model airplane. They found that the lap belts typically cleared the rudder pedals by less than 1 inch. Factors that affected the clearance included seat cushion padding, physical size of the pilot, centering of the belt cushion on the pilot, and tightness of the lap belt when secured. As a result of that review, an Airplane Flight Manual Supplement (AFMS) was issued by American Champion, and approved by the FAA. It called for both a pre start and pre flight check of the lap belts for proper tension and clearance from the aft seat rudder pedals. The FAA also issued a Special Airworthiness Information Bulletin (SAIB CE-10-39, dated July 23, 2010. The SAIB notified pilots of the AFMS issuance. It also recommended that airplanes equipped with the Hooker Aerobatic dual lap belts use floor mounted attach lugs. The upper or secondary lap belt should be moved from the outside of the outer attach lug to the inside of the outer attach lug per a service bulletin in order to provide additional clearance between the belt and pedal assembly.

## Aircraft

- Registration: [N101BY](https://openairdocs.org/aircraft/N101BY), registered now, S/N 9492004, built 2004 (OpenAirDocs)
- Reported make and model: American Champion Aircraft 8KCAB
- Registry model: [American Champion 8KCAB](https://openairdocs.org/model/american-champion-8kcab) (registry code 2121000) (OpenAirDocs)
- Registry engine: [Lycoming AEIO-360 series](https://openairdocs.org/engine/lycoming-aeio-360-series) (registry code 41522, reciprocating) (OpenAirDocs)
- Category: Airplane
- Serial number: 949-2004
- Airframe hours: 440
- Engines: Textron Lycoming AEIO-360-H1B 180 horsepower reciprocating
- Damage: Substantial damage
- Flight: Instructional, Part 91
- Operator: Donald H. Sefton
- Registered owner: Donald H. Sefton
- Airworthiness certificate: Standard, Aerobatic; Standard, Normal
- Last inspection: Annual, April 23, 2009, 2 hours before
- Departed: FLX, Fallon, NV
- Destination: FLX, Fallon, NV
- Airport: FLX, Fallon Municipal Airport, runway 03, 5,703 × 75 ft, asphalt

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Flight instructor; age 73; injuries: none; commercial, flight instructor; airplane ratings: single-engine land, multi-engine land; instrument ratings: airplane; medical: class 2, with waivers/limitations; last flight review April 21, 2009; seat: front; flight hours: 9,138 total, 33 in this make and model, 8,111 as pilot in command, 27 in the last 90 days, 12 in the last 30 days
- Pilot; age 57; injuries: none; commercial; airplane ratings: single-engine land, multi-engine land; instrument ratings: airplane; medical: class 2, with waivers/limitations; last flight review June 14, 2009; seat: rear; flight hours: 791 total, 7 in this make and model

## Weather

- Conditions: Visual (VMC), Day
- Wind: 350° at 5 knots
- Visibility: 10 statute miles
- Lowest ceiling: 3,500 ft broken
- Temperature: 122 °F
- Altimeter: 29.95 inHg
- Observed at: FLX

## FAA reports on this event (1)

The FAA's own accident and incident reports, matched to the aircraft by N-number and date (OpenAirDocs).

- [Accident 20100126004979A](https://openairdocs.org/incident/20100126004979A), Jan 26, 2010: American Ch 8KCAB, Fallon, NV, Substantial damage. While performing touch and go practice, immediately after touchdown, aircraft began uncontrollable swerve to the right, exited right side of runway and…

## Docket (2 files)

The files NTSB released with the investigation on March 29, 2012, on NTSB's docket system: https://data.ntsb.gov/Docket?ProjectID=75319. 1.5 MB in all.

- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1 (item 1, .PDF, 521 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40364800&FileExtension=.PDF&FileName=Pilot%2FOperator%20Aircraft%20Accident%20Report,%20NTSB%20Form%206120.1-Redacted.PDF
- Video File (item 2, AVI, 965 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40364806&FileExtension=avi&FileName=Video%20File-Master

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

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