Accident Beechcraft C-45G Expeditor N3657G,
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ASN Wikibase Occurrence # 35929
 
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Date:Monday 7 September 1992
Time:13:40 LT
Type:Silhouette image of generic BE18 model; specific model in this crash may look slightly different    
Beechcraft C-45G Expeditor
Owner/operator:Exa, Incorporated
Registration: N3657G
MSN: AF461
Year of manufacture:1951
Total airframe hrs:7780 hours
Engine model:P&W R-985-AN-14B
Fatalities:Fatalities: 12 / Occupants: 12
Aircraft damage: Destroyed
Category:Accident
Location:Hinckley, IL -   United States of America
Phase: Initial climb
Nature:Parachuting
Departure airport:(OC2)
Destination airport:(OC2)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
AFTER TAKEOFF, THE AIRPLANE WAS SEEN AT LOW ALTITUDE TRAILING SMOKE FROM THE LEFT ENGINE. WITNESSES SAW THE WINGS 'TIPPING' BACK AND FORTH, THEN A WING DROPPED AND HIT THE GROUND. EXAMINATION REVEALED THAT A SUPERCHARGER BEARING HAD FAILED IN THE LEFT ENGINE. THE LEFT ENGINE HAD BEEN RECENTLY INSTALLED BY NON-CERTIFICATED PERSONNEL AFTER BEING INACTIVE FOR 18 YRS WITHOUT PRESERVATION. THE AIRPLANE HAD FLOWN ABOUT 184 HRS SINCE THE LAST ANNUAL INSPECTION; NO RECORD OF SUBSEQUENT 100-HR INSPECTION. THE LEFT PROP BLADES WERE FOUND IN AN INTERMEDIATE POSITION BETWEEN THE OPERATING RANGE AND THE FEATHERED POSITION. THE LEFT PROP WAS CHANGED SEVERAL WEEKS PRIOR TO THE ACCIDENT. THERE IS NO EVIDENCE THAT THE LEFT PROP HAD EVER BEEN SUCCESSFULLY CYCLED TO THE FULL FEATHER POSITION. THE OPERATOR AND PILOTS WERE NOT AWARE OF HAMILTON STANDARD SB 657 RECOMMENDING FULL-FEATHER CHECKS EVERY 30 DAYS. LEFT PROP FEATHERING MOTOR RELAYS NOT RECOVERED. ALL 11 PARACHUTISTS WERE FOUND IN CENTER PART OF FUSELAGE; NO EVIDENCE OF RESTRAINT USEAGE.

Probable Cause: INADEQUATE MAINTENANCE AND INSPECTION BY THE OPERATOR WHICH RESULTED IN AN ENGINE POWER LOSS DURING THE CRITICAL TAKEOFF PHASE OF FLIGHT. IN ADDITION, THE PILOT DID NOT, OR WAS UNABLE TO, ATTAIN A FULL-FEATHER POSITION ON THE LEFT ENGINE PROPELLER, WHICH WOULD HAVE MOST LIKELY ENABLED THE AIRPLANE TO SUSTAIN MINIMUM CONTROL AIRSPEED.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: DCA92MA048
Status: Investigation completed
Duration: 1 year and 2 months
Download report: Final report

Sources:

NTSB DCA92MA048

Location

Revision history:

Date/timeContributorUpdates
24-Oct-2008 10:30 ASN archive Added
08-Apr-2011 15:02 TB Updated [Time, Aircraft type, Cn, Operator, Phase, Nature, Source]
21-Dec-2016 19:22 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
10-Apr-2024 18:07 ASN Update Bot Updated [Time, Cn, Operator, Other fatalities, Source, Narrative, Category, Accident report]

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