LAX04LA276

NTSB accident investigation · Beech 95-B55 · Minden, NV · July 24, 2004

Accident · No injuriesLimited investigationFinal report
Date
July 23, 2004, 17:45 local (Jul 24, 2004, 00:45 UTC)
Place
Minden, NV
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N88CSBeech 95-B55
Weather
Visual (VMC) · Day
Status
Completed · report June 8, 2005
Report
Approved by Office Director
Parties
Federal Aviation Administration
FAA report
20040723017159A
Case key
59753

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 lower the landing gear during landing approach, which resulted in his inadvertent gear up landing. A factor was his distraction due to a component malfunction.

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.

Airframe/component/system failure/malfunctionApproach - vfr pattern - downwind
Electrical system,electric relay - shortedFactor
Wheels up landingLanding - flare/touchdown
Gear extension - not performedPilot in commandCause
Diverted attentionPilot in commandFactor

Analysis

During the approach, the pilot failed to extend the landing gear, and the airplane touched down on the runway with retracted landing gear. The pilot was an airplane mechanic, and he was in the process of preparing the airplane for export. The accident occurred during the first flight following his replacement of both engines' propeller assemblies. On departure, while concentrating on synchronizing the engine's speed, the pilot detected "a slight smell of electrical burning" in the cockpit. The odor increased on the downwind leg, and the pilot "expedited" the base leg and believed that he had extended the landing gear. During the landing flare the stall warning horn sounded and the propeller blades contacted the runway. Subsequently, the Federal Aviation Administration coordinator conducted an examination of the airplane. The airplane was placed on jacks and the landing gear system was tested. The landing gear was completely cycled three times with positive indications of the gear being up and then in the down position. This was noted by the gear up and down indicator lights, and also by the gear mechanical indicator. The starter vibrator was found discolored and charred indicating the presence of an overheated condition.

Factual narrative

On July 23, 2004, about 1745 Pacific daylight time, a Beech 95-B55, N88CS, landed with its landing gear retracted at the Minden-Tahoe Airport, Minden, Nevada. The airplane was substantially damaged during the landing and subsequent ground fire. The private pilot, who was the sole occupant, was not injured. GFA Aircraft Sales, Minden, operated the airplane. Visual meteorological conditions prevailed, and no flight plan had been filed for the local area personal flight. The flight was performed under the provisions of 14 CFR Part 91, and it originated from Minden about 1735.

The pilot verbally reported to the National Transportation Safety Board investigator that he had performed the last annual inspection on the airplane, and thereafter, he had replaced both engines' propellers. The accident occurred during the first landing on the first flight following the propeller installations. The pilot stated that he was preparing the airplane for export.

In the pilot's completed "Aircraft Accident Report," he reported that after takeoff, while on the crosswind leg, he detected "a slight smell of electrical burning" in the cockpit. The odor increased on the downwind leg, and he "expedited" the base leg and "selected landing gear down." On final approach no landing gear warning horn was heard, and the green gear down light illuminated. During the landing flare the stall warning horn sounded, and the propeller blades contacted the runway.

A Minden airport employee inspected the runway. He reported to the Safety Board investigator that he observed propeller score marks in the runway's surface near the 1,500-foot runway distance marker. The airplane came to rest near the 2,500-foot runway distance marker. All of the airplane's wheels appeared stowed in the gear wells.

The pilot subsequently completed a Federal Aviation Administration (FAA) "Malfunction or Defect Report." In the report, the pilot indicated that the airplane examination disclosed that the ignition vibrator had started a fire in the pilot's lower panel. A gear up landing resulted from the electrical burn, which had incapacitated the gear warning horn.

According to the FAA coordinator, between July 26 and 28, 2004, the airplane was examined. The examination revealed damage to both propeller assembles and abrasive damage to the underside of the airplane. The airplane's interior was found fire damaged in the instrument panel and pilot's floor area. The airplane was placed on jacks and the landing gear was tested. The landing gear was completely cycled three times with positive indications of the gear being up and then in the down position. This was noted by the gear up and down indicator lights, and also by the gear mechanical indicator. The starter vibrator was discolored and charred, indicating a possible overheated condition. Application of electrical power to the airplane showed that the starter vibrator immediately started to spark. After removal of electrical power from the starter vibrator the rest of the airplane systems that were tested operated normally.

The FAA coordinator opined to the Safety Board investigator that during the accident flight the pilot had likely become distracted. The pilot had indicated that he had been concentrating on his newly performed propeller installation and engine/propeller synchronization, when he noticed an unusual odor in the airplane.

Aircraft

Registration
N88CS
Reported as
Beech 95-B55
Category
Airplane
Serial number
TC-723
Airframe hours
4,704
Engine
Continental IO-470, 260 horsepower, reciprocating
Damage
Substantial damage
Fire
On-Ground
Flight
Personal · Part 91
Operator
GFA Aircraft Sales
Registered owner
Veng B Ung
Airworthiness certificate
Standard, Normal
Last inspection
Annual · July 2, 2004 · 1 hours before
Departed
MEV · Minden, NV
Destination
MEV
Airport
MEV · Minden-Tahoe, runway 34, 7,400 × 100 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
54
Injuries
None
Certificate
Private
Airplane ratings
Single-engine sea, Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, Valid Medical--w/ waivers/lim
Last flight review
December 17, 2003
Seat
Left
Flight hours
4,150 total · 745 in this make and model · 60 in the last 90 days · 18 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
280° at 11 knots
Visibility
10 statute miles
Lowest ceiling
18,000 ft broken
Temperature
93 °F, dew point 52 °F
Altimeter
29.94 inHg
Observed at
RNO, 30 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.