IAD04LA019

NTSB accident investigation · Krotje VM-1 Esqual · Cambridge, OH · May 1, 2004

Accident · Minor injuriesLimited investigationFinal report
Date
May 1, 2004, 11:30 local (15:30 UTC)
Place
Cambridge, OH
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N626EAKrotje VM-1 Esqual
Weather
Visual (VMC) · Day
Status
Completed · report December 3, 2004
Report
Approved by Office Director
Parties
FAA/FSDO
FAA report
20040501008759A
Case key
59166

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The pilot's failure to maintain directional control. A factor was the inadequate brake system installed on the airplane.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - on ground/waterTakeoff - roll/run
Directional control - not maintainedPilot in commandCause
Landing gear,normal brake system - inadequateFactor
On ground/water collision with objectTakeoff - roll/run
Object - runway light
Terrain condition - water

Analysis

The pilot attempted a takeoff in the homebuilt airplane. During the takeoff roll, the airplane veered off the left side of the runway, struck runway lights, and went into a creek. A post-accident examination of the airplane revealed that it was equipped with a free-castoring nose wheel and motorcycle brakes. It was found that the left brake dragged due to a lack of clearance between the brake pad and brake rotor. The lack of clearance was attributable to the design of the brakes and their adaptation from a motorcycle to an airplane.

Factual narrative

On May 1, 2004, about 1130 eastern daylight time, a homebuilt VM-1 Esqual, N626EA, was substantially damaged during an attempted takeoff from Cambridge Municipal Airport (CDI), Cambridge, Ohio. The certificated private pilot received minor injuries. Visual meteorological conditions prevailed, and no flight plan had been filed for the local personal flight, conducted under 14 CFR Part 91.

According to the pilot, he attempted to take off from runway 22. After he set the throttle to takeoff power, the airplane "started pulling abruptly to the left." The pilot applied "strong right rudder," in an effort to counteract the turning, but to no avail. The airplane then veered off the left side of the runway, struck runway lights, and went into a creek.

A Federal Aviation Administration (FAA) inspector examined the airplane after the accident and submitted a Service Difficulty Report (SDR). According to the report, the airplane was equipped with a free-castoring nose landing gear and was configured to use motorcycle brakes on the main landing gear. A post-accident examination of the brakes revealed that the right brake operated normally; however, the left brake dragged due to a lack of clearance between the brake pad and the brake rotor. The lack of clearance was attributable to the design of the brakes and their adaptation from a motorcycle to an airplane.

Aircraft

Registration
N626EA
Reported as
Krotje VM-1 Esqual
Category
Airplane, amateur-built
Serial number
E180032
Airframe hours
138.4
Engine
Jabiru 3300, 120 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · March 13, 2004 · 14.6 hours before
Departed
CDI · Cambridge, OH
Destination
PHD · New Philadelphi, OH
Airport
CDI · Cambridge Municipal Airport, runway 22, 4,298 × 75 ft, asphalt

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
68
Injuries
Minor
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--w/ waivers/lim
Last flight review
April 27, 2003
Seat
Left
Flight hours
519 total · 9 in this make and model · 519 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
200° at 7 knots
Visibility
9 statute miles
Lowest ceiling
3,100 ft broken
Temperature
70 °F, dew point 61 °F
Altimeter
30.00 inHg
Observed at
ZZV, 15 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.