DCA84AA024

NTSB accident investigation · Lockheed L-188 · Chalkhill, PA · May 30, 1984

Accident · FatalFinal report
Date
May 30, 1984, 01:44 local (05:44 UTC)
Place
Chalkhill, PA
Injuries
4 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N5523Lockheed L-188
Weather
Night/dark
Status
Completed
Report
Approved by Office Director
NTSB office
Major Investigations Division
FAA report
19840530038939A
Case key
15808

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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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 flightCruise - normal
Light condition - dark nightFactor
Flight/nav instruments,attitude gyro - undeterminedCause
Flight/nav instruments,attitude indicator - false indication
Aircraft handling - not maintainedPilot in commandCause
Spatial disorientationPilot in commandCause
Airframe/component/system failure/malfunctionDescent - uncontrolled
Wing - overload
Design stress limits of aircraft - exceededPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

After departing the baltimore-washington arpt, the acft had climbed to FL 220. According to info on the cockpit voice recorder (vcr), the crew experienced gyro problems during the climb. They selected the #1 vertical gyro to drive both approach horizons (attitude indicators), since there was an indication of a malfunction in the #2 vertical gyro sys. About 7 min after leveling at FL 220, the flt was cleared to the dryer VOR. Shortly after that, there were indications of confusion in the cockpit which included the statements, 'what's happening here,' 'you got it?' & 'no.' the acft entered a right descending spiral; the indicated airspeed increased from aprx 205 to 317 KTS; then an in-flt breakup occurred. The wreckage was found scattered over an area aprx 2 mi long by 1 mi wide. An exam of the wreckage revealed that the in-flt structural failure had occurred due to overload, then a fire ignited in the right wing after it had failed. The acft was not equipped with an independent standby attitude indicator.

Aircraft

Registration
N5523
Reported as
Lockheed L-188
Category
Airplane
Serial number
1034
Airframe hours
35,668
Engine
Allison 501-D13, 3,750 horsepower, turbo prop
Damage
Destroyed
Fire
In-Flight
Flight
Part 121
Registered owner
Zantop Int'L Airlines, Inc.
Airworthiness certificate
Standard, Transport
Last inspection
Continuous airworthiness · May 13, 1984 · 0 hours before
Departed
Baltimore, MD
Destination
Ypsilanti, MI
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
37
Certificates
Commercial, Airline transport
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Toxicology
Performed
Flight hours
10,047 total · 7,173 in this make and model

Weather

Conditions
Night/dark
Wind
240° at 5 knots
Visibility
7 statute miles
Lowest ceiling
3,600 ft overcast
Temperature
45 °F, dew point 43 °F
Altimeter
30.00 inHg
Observed at
MGW

FAA reports on this event · 1

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