DEN04LA065

NTSB accident investigation · Mooney M20C · Clovis, NM · March 13, 2004

Accident · No injuriesLimited investigationFinal report
Date
March 12, 2004, 21:20 local (Mar 13, 2004, 04:20 UTC)
Place
Clovis, NM
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N6958VMooney M20C
Weather
Instrument (IMC) · Night/dark
Status
Completed · report September 29, 2004
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20040312003339A
Case key
59086

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 improper in-flight planning and decision making during an instrument approach resulting in the pilot's intentional descent below approach minimums, and the pilot's failure to maintain obstacle clearance resulting in the in-flight collision with an object. Contributing factors include the dark night light conditions, and the wires.

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.

In flight collision with objectApproach
In-flight planning/decision - improperPilot in commandCause
Decision height - continued belowPilot in commandFactor
Altitude/clearance - not maintainedPilot in commandCause
Missed approach - initiatedPilot in command
Object - wire,transmissionFactor
Light condition - dark nightFactor
Weather condition - low ceiling

Analysis

According to the pilot, at 11,000 feet msl, while on a cross-country IMC flight, he encountered rime icing conditions. He requested, and was given, clearance to descend to 8,000 feet msl. He stated that he received the local weather conditions and decided to divert to a nearby airport. He stated that the airport weather conditions were reported as: ceiling, 100 feet; visibility, 4 miles; and wind, 165 degrees at 6 knots. After contacting the local approach control, he requested and received vectors for runway 04. He stated that, at approximately 4,400 feet msl, while established on the glide slope and localizer, he struck something, and all radio communication was lost. The pilot immediately initiated a missed approach. Approximately 1 hour later, he reestablished radio contact with the local approach control. Approach control gave him vectors to runway 22 at another nearby airport. He stated that he "broke out" of the clouds at approximately 200 to 300 feet agl, on a "45 degree" to runway 22. At 2230, he landed at without further incident. An examination of the airplane revealed several scratches along the bottom of the aft fuselage and empennage. These "braided" scratches were similar to scratches associated with contacting a power transmission line. Several areas on the bottom of the airplane exhibited burns and "arcing." The airplane received substantial damage to the aft fuselage bulkhead and lower tail cone assembly.

Factual narrative

On March 12, 2004, at approximately 2120 mountain standard time, a Mooney M20C, N6958V, was substantially damaged when it struck a power transmission line during final approach to Clovis Municipal Airport (CVN), Clovis, New Mexico. The private pilot, the sole occupant on board, was not injured. Instrument meteorological conditions prevailed. An instrument flight rules (IFR) flight plan was filed for this personal flight being conducted under the provisions of Title 14 CFR Part 91. The flight originated at Winslow, Arizona, at approximately 1800, and was en route to Ardmore, Oklahoma.

According to the pilot, at 11,000 feet msl, at a point just west of Clovis, he encountered rime icing conditions. At approximately 2110, he requested, and was given, clearance to descend to 8,000 feet msl. He stated that after he received the local weather conditions, he decided to divert to CVN. He stated that the weather conditions at CVN were reported as, ceiling, 100 feet; visibility, 4 miles; and wind, 165 degrees at 6 knots. At approximately 2115, the pilot contacted Cannon Approach Control and requested vectors to CVN. He was given vectors for runway 04. The pilot stated that, at approximately 4,400 feet msl, while established on the glide slope and localizer, he struck something, and all radio communication was lost. At 2120, the pilot initiated a missed approach.

The pilot stated that he flew around for 1 hour. At approximately 2220, Cannon Approach "came back on," however, radio communication was intermittent. At that time, while on a heading of 240 degrees, Cannon Approach gave him vectors to Cannon Air Force Base (CVS), which was 270 degrees from his position. After responding to Cannon Approach, by transponder indent, he was directed to runway 22 at CVS. He stated that he "broke out" of the clouds at approximately 200 to 300 feet agl, on a "45 degree" to runway 22. At 2230, he landed at CVS without further incident.

An FAA inspector, who examined the airplane, stated that several scratches were located along the bottom of the aft fuselage and empennage. These "braided" scratches were similar to scratches associated with power transmission line contact. Several areas exhibited burns and "arcing." The wire strike resulted in substantial damage to the aft fuselage bulkhead and lower tail cone assembly.

According to a member services representative from Farmers' Electric Cooperative, Inc., of New Mexico (FEC), on the evening of March 12, 2004, a customer, who lived near the Clovis Municipal Airport, called in to report a power outage that had occurred at approximately 2130 mst. An FEC lineman surveyed the area and located a blown line fuse. The line fuse was "refused" and power was restored at 2223. On March 15, 2004, after receiving reports that a low flying airplane had struck wires in the vicinity of the airport, another FEC lineman conducting a follow-up inspection, located a set of damaged power lines approximately 1/4 of a mile to the right of the runway centerline and approximately 1/4 of a mile south of the approach for runway 04.

The lineman stated that it appeared the low flying airplane had struck the top phase, 14,000 volt, #2 ACSR conductor wire. The impact stretched the conductor wire, breaking the smaller stranded (braided) wires, but leaving the conductor wire intact. Although the conductor wire remained intact, the power outage was the result of a "direct short," caused by the top phase conductor wire's contact with another phase wire. At the point where the damage occurred, the top phase wire was approximately 27 feet, 3 inches, above the ground.

Aircraft

Registration
N6958V
Reported as
Mooney M20C
Category
Airplane
Serial number
21-1191
Airframe hours
7,000
Engine
Lycoming, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
George W. Carlson
Airworthiness certificate
Standard, Normal
Last inspection
Annual · September 30, 2003 · 50 hours before
Departed
INW · Windslow, AZ
Destination
1F0 · Ardmore, OK
Flight plan
IFR
Airport
CVN · Clovis Municipal

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
67
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--no waivers/lim.
Last flight review
August 4, 2002
Seat
Left
Flight hours
1,750 total · 1,400 in this make and model

Weather

Conditions
Instrument (IMC) · Night/dark
Wind
165° at 6 knots
Visibility
4 statute miles
Lowest ceiling
100 ft overcast
Temperature
46 °F, dew point 46 °F
Altimeter
30.02 inHg

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 N6958V · 1

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