# NTSB WPR11LA265: Aerovodochody L-29 Delfin, N37KF, Reno, NV, June 18, 2011

- Type: NTSB accident investigation
- Classification: Accident · No injuries · Limited investigation · Final report
- Date: June 18, 2011, 14:50 local (21:50 UTC)
- Place: Reno, NV
- Coordinates: 39.667221, -119.876113
- Nearby events: https://openairdocs.org/map.md?lat=39.6672&lon=-119.8761&mi=10
- Phase of flight: [Maneuvering](https://openairdocs.org/ntsb-phases/450) (OpenAirDocs' grouping)
- Defining event: [Maneuvering: Sys/Comp malf/fail (non-power)](https://openairdocs.org/ntsb-events/330)
- Highest injury: No injuries
- Injuries: 1 uninjured
- Status: Completed, report November 7, 2012
- Report: Approved by Office Director
- NTSB office: Western Pacific Region
- Parties: Reno FSDO
- NTSB case key (mKey): 80812
- NTSB case page: https://web.ntsb.gov/investigations/?ntsbnumber=WPR11LA265
- NTSB report (PDF, downloads): https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/80812/pdf
- NTSB docket: https://data.ntsb.gov/Docket?ProjectID=80812
- Page: https://openairdocs.org/ntsb/WPR11LA265

## Probable cause

The failure of a modified engine mount to keep the engine properly aligned, which resulted in partial failure of the rudder support structure due to the deflection of the jet engine exhaust.

## Findings

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

- [Power plant: mounts](https://openairdocs.org/ntsb-findings/01057120): Aircraft › Aircraft power plant · Capability exceeded (probable cause); cases with it: [Aerovodochody L-29 DELFIN, 1 case](https://openairdocs.org/ntsb-findings/01057120/cases.md?model=0564310), [All aircraft, 5 cases](https://openairdocs.org/ntsb-findings/01057120/cases.md)
- [Empennage structure: rudder misc structure](https://openairdocs.org/ntsb-findings/01035544): Aircraft › Aircraft structures · Failure (probable cause); cases with it: [Aerovodochody L-29 DELFIN, 1 case](https://openairdocs.org/ntsb-findings/01035544/cases.md?model=0564310), [All aircraft, 3 cases](https://openairdocs.org/ntsb-findings/01035544/cases.md)

## Sequence of events

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

- [Maneuvering: Sys/Comp malf/fail (non-power)](https://openairdocs.org/ntsb-events/330) (defining event); cases with it: [Aerovodochody L-29 DELFIN, 1 case](https://openairdocs.org/ntsb-events/330/sequence.md?model=0564310), [All aircraft, 994 cases](https://openairdocs.org/ntsb-events/330/sequence.md)
- [Maneuvering: Aircraft structural failure](https://openairdocs.org/ntsb-events/337); cases with it: [Aerovodochody L-29 DELFIN, 1 case](https://openairdocs.org/ntsb-events/337/sequence.md?model=0564310), [All aircraft, 290 cases](https://openairdocs.org/ntsb-events/337/sequence.md)

## Analysis

While being flown on an air race qualification/training flight, the experimental jet’s engine support mount, which had been recently installed to accommodate an increased-thrust engine modification, failed to keep the engine properly aligned. The resultant misalignment resulted in jet blast being directed onto and melting a portion of the rudder support structure. Although there was no indication of the problem in flight, during the landing roll, the pilot discovered that the rudder did not function properly, and directional control had to be maintained by alternate means. During the investigation, it was determined that five other racing airplanes of the same make and model had been modified in a similar manner and that there were slight structural variations and areas of poor welding associated with some of the mounts. As a result of this accident, the manufacturer of the engine modification instituted a program to obtain an independent professional engineering analysis of the engine mount design. Later, in response to another accident, the National Transportation Safety Board (NTSB) issued Safety Recommendation A-12-13, which asked the Reno Air Race Association (RARA) to require aircraft owners to provide an engineering evaluation for aircraft with any major modification. On August 27, 2012, pending receipt of further information showing that the process proposed by RARA specifically requires an owner of an aircraft with a major modification to provide an engineering evaluation that includes flight demonstrations and analysis within the anticipated flight envelope, the NTSB classified the recommendation Open-Acceptable Response.

## Factual narrative

On June 18, 2011, about 1450 Pacific daylight time, an experimental Aerovodochody L-29 Delfin, N37KF, experienced the partial failure of the primary airframe structure supporting the airplane's rudder while in the air race pattern at Reno-Stead Airport, Reno, Nevada. The commercial pilot, who was the sole occupant, was not injured, but the airplane, which was owned and operated by Raju Mann Ward, sustained substantial damage. The local 14 Code of Federal Regulations Part 91 air race qualification/training flight, which took off from the same airport about 20 minutes prior to the accident, was being operated in visual meteorological conditions. No flight plan had been filed. According to the Federal Aviation Administration (FAA) inspector who responded to the scene, while the airplane was in flight, part of the engine support structure that had been installed as part of a modification to install a higher thrust engine, had failed to hold the new engine in proper alignment. That failure allowed jet blast from the engine to be deflected onto a portion of the primary airframe structure. The melting of that structure affected the support and movement of the airplane's rudder. Although the failure occurred in flight, it was not detected until the pilot was operating the rudder pedals during the landing roll. Although the pilot was able to keep the airplane on the runway, she had to apply alternative/non-standard control inputs in order to do so. During the investigation it was determined that at least five other L-29 airplanes had the same type of mounts, which were all designed, welded/manufactured by the same entity. According to the FAA inspector who looked at these mounts, the welding was poor on some of them, and there was some degree of structural variation between a number of the mounts.

## Aircraft

- Registration: [N37KF](https://openairdocs.org/deregistered/N37KF-2018-03-13), registration cancelled 2018-03-13, S/N 993233, built 1969 (OpenAirDocs)
- Reported make and model: AEROVODOCHODY L-29 DELFIN
- Registry model: [Aerovodochody L-29 DELFIN](https://openairdocs.org/model/aerovodochody-l-29-delfin) (registry code 0564310) (OpenAirDocs)
- Registry engine: [Motorlet M-701C](https://openairdocs.org/engine/motorlet-m-701c) (registry code 46000, turbo-jet) (OpenAirDocs)
- Category: Airplane
- Serial number: 993233
- Engines: Rolls Royce 601 Viper 3750 lbs thrust turbo jet
- Damage: Substantial damage
- Flight: Air race/show, Part 91
- Operator: Ward Raju Mann
- Registered owner: Ward Raju Mann
- Last inspection: Condition, June 10, 2011
- Departed: 4SD, Reno, NV
- Destination: 4SD, Reno, NV
- Airport: 4SD, Reno-Stead, runway 26, 7,600 × 150 ft, asphalt

## Flight crew

As NTSB recorded them. NTSB leaves out names.

- Pilot; age 36; injuries: none; commercial; airplane ratings: single-engine land, multi-engine land; instrument ratings: airplane; medical: class 2, without waivers/limitations; last flight review September 30, 2010; seat: front; flight hours: 2,000 total, 1,700 as pilot in command, 20 in the last 90 days, 10 in the last 30 days, 2 in the last 24 hours

## Weather

- Conditions: Visual (VMC), Day
- Wind: 240° at 14 knots, gusting 26
- Visibility: 10 statute miles
- Lowest ceiling: 19,000 ft broken
- Temperature: 82 °F, dew point 34 °F
- Altimeter: 29.90 inHg

## 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 20110618012739A](https://openairdocs.org/incident/20110618012739A), Jun 18, 2011: Aerovodochody L-29 DELFIN, Reno, NV, Substantial damage. Aircraft was participating in pylon racing seminar race training. Aircraft has been modified by the installation of a larger engine. (Rolls royce viper 540)

## Docket (2 files)

The files NTSB released with the investigation on September 4, 2012, on NTSB's docket system: https://data.ntsb.gov/Docket?ProjectID=80812. 435 KB in all.

- Pilot/Operator Aircraft Accident Report, NTSB Form 6120.1 (item 1, .PDF, 299 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40374577&FileExtension=.PDF&FileName=Pilot%2FOperator%20Aircraft%20Accident%20Report,%20NTSB%20Form%206120.1-Redacted.PDF
- Record of Conversation (item 2, .PDF, 136 KB): https://data.ntsb.gov/Docket/Document/docBLOB?ID=40374578&FileExtension=.PDF&FileName=Record%20of%20Conversation-Master.PDF

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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