DCA84AA002

NTSB accident investigation · Hawker Siddeley HS-748-2A · Pinckneyville, IL · October 12, 1983

Accident · FatalFinal report
Date
October 11, 1983, 20:53 local (Oct 12, 1983, 01:53 UTC)
Place
Pinckneyville, IL
Injuries
10 fatal
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N748LLHawker Siddeley HS-748-2A
Weather
Instrument (IMC) · Night/dark
Status
Completed
Report
Approved by Office Director
NTSB office
Major Investigations Division
FAA report
19831011076029A
Case key
15796

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.

Airframe/component/system failure/malfunctionClimb - to cruise
Electrical system,generator - failure,partialFactor
Electrical system,generator - switched offFactor
Electrical system,generator - failure,totalFactor
In-flight planning/decision - improperPilot in commandCause
Self-induced pressurePilot in commandFactor
Inadequate recurrent trainingCompany/operator managementFactor
Inadequate surveillance of operationFaa(organization)Factor
Not performedPilot in command
Electrical system,battery - exhaustion
Electrical system - inoperative
Flight/nav instruments - inoperative
Loss of control - in flightCruise
Aircraft handling - not possiblePilot in command
Spatial disorientationPilot in commandCause
In flight collision with terrain/waterDescent - uncontrolled

Analysis

About 1.5 min after departing springfield, IL, the fltcrew reported a slight electrical problem, but they continued on course. About 33 min later & a few min before the acft should have reached its destination, the acft crashed. Impact occurred while the acft was descending in a right wing low attitude. Before crashing, the plane's heading had changed about 180 deg. A CVR transcript revealed the l generator (gen) had failed after takeoff & the 1st officer had mistakenlyisolated the r gen. Attempts to restore the r gen were unsuccessful. The captain elected to continue to the destination rather than return to the nearby dept arpt. The cld bases were at 2000' MSL, but ATC could not provide an IFR clnc BELOW3000 ft. just before crashing, the crew indicated a total loss of electrical power. The l gen drive shaft had sheared. The reason for the r gen not to reset was not determined. There was evidence that recurrent fltcrew training did not prepare the crew to understand & cope with the elec problem & that FAA surveillance did not detect the trng deficiency.

Aircraft

Registration
N748LL
Reported as
Hawker Siddeley HS-748-2A
Category
Airplane
Serial number
1716
Airframe hours
21,182
Engine
Rolls-Royce RDA-7,MK535-2, 2,238 horsepower, turbo prop
Damage
Destroyed
Flight
Part 121
Operator
Air Illinois, Inc
Departed
SPI · Springfield, IL
Destination
MDH · Carbondale, IL
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
32
Certificates
Commercial, Airline transport, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Flight hours
5,891 total · 3,170 in this make and model · 261 in the last 90 days · 81 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Instrument (IMC) · Night/dark
Wind
180° at 10 knots, gusting 8
Visibility
1 statute miles
Lowest ceiling
2,000 ft overcast
Temperature
63 °F, dew point 61 °F
Altimeter
29.00 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 N748LL · 1

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