Loss of control Accident Curtiss C-46F Commando N9904F,
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ASN Wikibase Occurrence # 334778
 
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Date:Saturday 17 December 1955
Time:20:40
Type:Silhouette image of generic C46 model; specific model in this crash may look slightly different    
Curtiss C-46F Commando
Owner/operator:Riddle Airlines
Registration: N9904F
MSN: 30262
Year of manufacture:1944
Engine model:Pratt & Whitney R-2800-75
Fatalities:Fatalities: 2 / Occupants: 2
Aircraft damage: Destroyed, written off
Category:Accident
Location:near Hollywood, SC -   United States of America
Phase: En route
Nature:Cargo
Departure airport:Wilmington-New Hanover County Airport, NC (ILM/KILM)
Destination airport:Jacksonville-Thomas Cole Imeson Municipal Airport, FL
Investigating agency: CAB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The aircraft was engaged on a scheduled cargo flight from New York to Miami, Florida, with scheduled stops at Wilmington, North Carolina and Jacksonville, Florida. Flying on a VFR flight plan the aircraft landed at Wilmington at 18:57 and departed again at 19:36, estimating Jacksonville at 21:56. At approximately 20:40, at a point near Hollywood, South Carolina, engines were heard by witnesses and lights were seen descending on an erratic path as the aircraft fell in several pieces to the ground.

The aircraft was manufactured for and operated by the U.S. Air Force as a C-46A, and was decommissioned and stored in the Egyptian desert. Subsequently an Italian firm bought the aircraft, and the Curtiss-Wright company authorised this firm to convert C.46A's to C-46E's, and provided them with an incomplete set of drawings relative to this conversion, which is identical to that for the C-46F insofar as the tail surfaces arc concerned. Where specified material was not available the nearest available material was used. In every case the strength of the material in the new part exceeded the strength of the material specified. Many of the newly installed parts were heavier than the original parts.
A comparison of the rudder elevators, their tabs and their control mechanisms on the accident aircraft with applicable Curtiss-Wright drawings disclosed many nonconformities.

PROBABLE CAUSE: "An in-flight structural failure resulting from a violent pitch-down induced by the erratic action of nonconforming elevator tab controls."

Accident investigation:
cover
  
Investigating agency: CAB
Report number: final report
Status: Investigation completed
Duration:
Download report: Final report

Sources:


Images:


photo (c) DCA, Accident Investigation and Analysis Branch; Hollywood, SC; 17 December 1955

Revision history:

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