FTW98LA222

NTSB accident investigation · Mooney M20E · Watkins, CO · May 18, 1998

Accident · Minor injuriesLimited investigationFinal report
Date
May 17, 1998, 21:30 local (May 18, 1998, 03:30 UTC)
Place
Watkins, CO
Injuries
1 minor, 2 uninjured
Damage
Substantial damage
Phase of flight
Taxi
Aircraft
N1306WMooney M20E
Weather
Visual (VMC) · Night/dark
Status
Completed · report February 15, 2001
Report
Approved by Office Director
FAA report
19980517019699A
Case key
20608

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 visual contact with the taxiway. Factors were the pilot's disabling the electrical system by turning off the master switch, a dark night, and excessive taxi speed.

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.

On ground/water encounter with terrain/waterTaxi - from landing
Electrical system - closedFactor
Taxispeed - excessivePilot in commandFactor
Light condition - dark nightFactor
Visual lookout - not maintainedPilot in commandCause

Analysis

The pilot said that he experienced a total electrical failure while on a night cross-country flight. He landed without incident but while taxiing along the unlit taxiway, he lost sight of the centerline stripe. The airplane went off the taxiway and down an embankment. The airport night manager said the pilot told him he would 'turn on the navigation lights, if necessary,' to warn other airplanes. Postaccident inspection disclosed that when the master switch was turned on, all electrical components functioned normally. A specific gravity check indicated the battery was fully charged. According to the operator's records, the Hobbs meter and tachometer registered 65.9 and 3903.3, respectively, when the pilot checked the airplane out. At the accident site, the Hobbs meter and tachometer registered 67.6 and 3905.1, respectively, a Hobbs meter difference of 1.7 hours and a tachometer difference of 1.8 hours. The operator said he believed the pilot had turned off the master switch in an attempt to save on rental charges. He had also received reports from other renter pilots who said the pilot had bragged about saving money by turning off the master switch. An FAA inspector said that, based on the point where the aircraft departed the taxiway and its point of impact, taxi speed was excessive.

Factual narrative

On May 17, 1998, approximately 2130 mountain daylight time, a Mooney M20E, N1306W, operated by Flight Training, Inc., was substantially damaged when collided with terrain while taxiing from landing at Watkins, Colorado. The private pilot and one passenger were not injured, but another passenger sustained a minor injury. Visual meteorological conditions prevailed, and a VFR flight plan had been filed. The flight was conducted under Title 14 CFR Part 91, and had originated at Akron, Colorado, approximately 2030.

According to the pilot's accident report, while en route to the Front Range Airport, the cockpit "lights dimmed [electrical charging system failure]." He shut down all electrical devices with the exception of the navigation lights and rotating beacon. He said that as he got closer to his destination, he "did not have enough [electrical] power to communicate or turn on the runway lighting system." Front Range Airport's approach lights came on and he flew towards the airport. He then noticed two airplanes in the traffic pattern. He landed on runway 17.

Although runway 17 is equipped with pilot-controlled high intensity runway lights, the parallel taxiway is not illuminated0. The pilot said that after he turned off the runway, he tracked the taxiway centerline. He said he "was blind. . .The battery was exhausted. . .The visibility was near zero. I was fixated on the center line of the taxiway and negotiated some turns. I lost the center line and went off the taxi way, where I pulled back on the elevator control for soft field procedure. There was a sensation of falling. The aircraft had gone off a sharp embankment."

According to the airport's night manager, he was driving to the fuel farm when he encountered the pilot walking along the taxiway. The pilot told him what had happened, then expressed concern that the airplane might be a hazard to other traffic and offered to "turn on the navigation lights, if necessary." The night manager said he thought the remark was odd if the airplane had had a total electrical failure.

An FAA inspector later examined the airplane. When the master switch was closed, all electrical components functioned normally. Additionally, the inspector said that, based on the point where the aircraft departed the taxiway and its point of impact, taxi speed was excessive.

The airplane operator asked a mechanic to examine the airplane. In his written statement, the mechanic said he "checked all lights [internal and external] and found them operational except for the landing light, which had been broken during the off-pavement excursion. Closer inspection of the landing light showed that when it was broken, it was not illuminated. A specific gravity check. . .found the battery to be fully charged. Inspection of the battery relays and primary power bus also showed no defects."

The airplane owner contacted this investigator and said that according to the operator's records, the Hobbs meter and tachometer registered 65.9 and 3903.3, respectively, when the pilot checked the airplane out. At the accident site, the Hobbs meter and tachometer registered 67.6 and 3905.1, respectively, a Hobbs meter difference of 1.7 hours and a tachometer difference of 1.8 hours. The Hobbs meter is electrically driven and begins operating when the master switch is turned on. The tachometer is driven by engine oil pressure and begins operating when the engine is started and oil pressure is sensed. It is also affected by engine speed; the higher the rpm, the faster the clock operates. Airplane renters have historically billed customers based on the Hobbs meter reading because it registers approximately .1 to .2 hours greater than the tachometer. The airplane owner and operator said they became suspicious when they discovered the tachometer registered .1 greater than the Hobbs meter, and expressed the belief that the pilot had turned off the master switch in an attempt to save on rental charges.

This investigator, accompanied by the airplane operator, went to the accident site on June 25, 1998. Faint tire marks, identified by the operator as having been made by N1306W, were noted on the tarmac. These marks were approximately 75 feet long and terminated at an embankment dropoff. At the bottom of the dropoff, approximately 140 feet from the edge of the tarmac, were ground scars identified by the operator as having been made by the airplane's landing gear. There were no ground scars between the tarmac and the point of impact.

This investigator also examined the airplane in its hangar. According to the operator, the only disturbance to the airplane was the removal of the right portion of the engine cowling. All electrical components came on line when the master switch was turned on.

The airplane operator said he had also received reports from other renter pilots who said they had heard the pilot brag about being able to save money by turning off the master switch.

Aircraft

Registration
N1306W
Reported as
Mooney M20E
Category
Airplane
Serial number
194
Airframe hours
3,905
Engine
Lycoming IO-360-A1A, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Flight Training, Inc.
Registered owner
Martin W. Brink
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · May 7, 1998 · 17 hours before
Departed
AKO · Akron, CO
Destination
FTG
Flight plan
VFR
Airport
FTG · Front Range

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
38
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
131 total · 23 in this make and model · 68 as pilot in command · 21 in the last 90 days · 7 in the last 30 days · 1 in the last 24 hours

Weather

Conditions
Visual (VMC) · Night/dark
Wind
170° at 13 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
59 °F, dew point 34 °F
Altimeter
29.00 inHg
Observed at
DEN, 10 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.

Other investigations on N1306W · 2

Matched to the same aircraft by N-number and date.