DCA82AA023

NTSB accident investigation · Beech D95A · Columbia, MD · May 28, 1982

Accident · FatalFinal report
Date
May 28, 1982, 10:58 local (14:58 UTC)
Place
Columbia, MD
Injuries
5 fatal
Damage
Destroyed
Phase of flight
Approach
Aircraft
N187QBeech D95A
Weather
Instrument (IMC) · Day
Status
Completed · report May 28, 1983
Report
Approved by Office Director
NTSB office
Major Investigations Division
FAA report
19820528019569A
Case key
70309

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

On this page

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 - in flightMissed approach (ifr)
Weather condition - low ceilingFactor
Weather condition - fogFactor
Weather condition - rainFactor
Missed approach - performedPilot in commandFactor
Aircraft weight and balance - exceededPilot in commandCause
Aircraft handling - improperPilot in commandCause
Excessive workload (task overload)Pilot in commandCause
Lack of recent instrument timePilot in commandCause
Spatial disorientationPilot in commandCause
In flight collision with objectDescent - uncontrolled
Object - residence

Analysis

The acft was vectored to intercept the localizer course for an ILS approach to rwy 10 at balt-wash-intl arpt. It was then observed to fly through & to the north of the localizer course. The acft was then directed to turn left to a heading of 360 for resequencing, however the acft was observed making a 360 to the right. The acft was tracked by the radar computer in a right turn, completing almost 360 deg of turn with a steady groundspeed decay accompanied by erraticaltitude excursions. This was followed by an abrupt course reversal, rapid groundspeed decay, & continued erratic altitude excursions. The acft crashed into a house in a residental section of Columbia in an inverted position. The acft's aft CG limit was exceeded. This would result in a deterioration of the acft's dynamic stability which would produce exaggerated acft reactions to otherwise normal control displacement inputs. The plt had not logged any instrument time or instrument approaches during the six months preceeding the accident.

Aircraft

Registration
N187Q
Reported as
Beech D95A
Category
Airplane
Serial number
TD609
Airframe hours
2,160
Engine
Lycoming IO-360-B1B, 180 horsepower, reciprocating
Damage
Destroyed
Flight
Public aircraft · Part 91
Operator
Angus Hines Jr.
Registered owner
Angus Hines Jr.
Departed
PVG · Portsmouth, VA
Destination
BW1 · Baltimore, MD
Flight plan
IFR

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
35
Certificates
Commercial, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--no waivers/lim.
Flight hours
2,134 total · 1,868 as pilot in command · 15 in the last 90 days

Weather

Conditions
Instrument (IMC) · Day
Wind
120° at 6 knots
Visibility
1 statute miles
Lowest ceiling
500 ft overcast
Temperature
151 °F
Altimeter
29.00 inHg
Observed at
BW1

FAA reports on this event · 1

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