BFO90FA002

NTSB accident investigation · Beech 58P · Nokesville, VA · October 26, 1989

Accident · FatalField investigationFinal report
Date
October 25, 1989, 20:40 local (Oct 26, 1989, 00:40 UTC)
Place
Nokesville, VA
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Other
Aircraft
N86MCBeech 58P
Weather
Visual (VMC) · Night/bright
Status
Completed · report September 5, 1991
Report
Approved by Office Director
FAA report
19891025042789A
Case key
11536

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

Improper installation of the elevator trim actuators, and subsequent jamming of the elevator trim in a nose down trim position.

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/malfunctionOther
Flt control syst,elevator trim/tab control - improperCause
Maintenance,installation - improperOther maintenance personnelCause
Flt control syst,elevator trim/tab control - jammedCause
Loss of control - in flightApproach - vfr pattern - downwind
Aircraft control - not possiblePilot in command
In flight collision with terrain/waterDescent - uncontrolled

Analysis

After taking off at ngt on rwy 34L, the acft was mnvrd to a left dnwnd (same rwy). According to witnesses, the eng(s) went to a hi pwr setting on dnwnd, but the acft speed rmnd slow. Apchg (abeam) midfield, the acft turned left, then wentinto a dscnt & crashed west of the arpt. Impact was on an ese hdg, in a 15 to 17 deg dscnt. The left fuel slctr was fnd in the 'off' psn, but the actuating cable had pulled thru the housing (presumably drg impact). The rgt fuel slctr was on. Both props sepd fm the crankshaft with evidence of torsional failure. There was a history of elevator trim (e/t) problems. Just bfr this flt, maint had been performed on the e/t. e/t actuators were fnd reversed, which reversed the drctn of trim. Both e/t tabs were fnd byd the full nose dwn trim psn. Calculated force to override at the full nose dwn psn was: 121 to 136 lbs at 100 KTS, 197 to 203 lbs at 150 KTS, 200 to 305 lbs at 200 KTS. Also, e/t chain was fnd off ofthe sprocket & jammed btn the brg plate & a bracket; 1 of 2 bolts was missing fm brg plate; otr bolt was finger tight.

Aircraft

Registration
N86MC
Reported as
Beech 58P
Category
Airplane
Serial number
TJ-406
Airframe hours
1,182
Engine
Continental TSIO-520-WB, 325 horsepower, reciprocating
Damage
Destroyed
Fire
On-Ground
Flight
Personal · Part 91
Registered owner
West Springfield Aviation Svcs
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 22, 1989 · 36 hours before
Airport
W10 · Manassas Muni, runway 34, 3,700 × 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
51
Certificate
Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Toxicology
Performed
Flight hours
1,284 total · 50 in this make and model

Weather

Conditions
Visual (VMC) · Night/bright
Wind
360° at 3 knots
Visibility
20 statute miles
Lowest ceiling
25,000 ft broken
Temperature
72 °F, dew point 41 °F
Altimeter
30.00 inHg
Observed at
IAD, 14 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.