Approximately 208 civil helicopter wire strike accidents for a ten year period 1970 to 1979 are analyzed. It is found that 83% of the wire strikes occurred during bright clear weather. Analysis of the accidents is organized under pilot, environment, and machine factors. Methods to reduce the wire strike accident rate are discussed, including detection/warning devices, identification of wire locations prior to flight, wire cutting devices, and implementation of training programs. The benefits to be gained by implementing accident avoidance methods are estimated to be fully justified by reduction in injury and death and reduction of aircraft damage and loss
The discovery of tremendous amounts of energy from the Atomic Explosion (ex: first Atomic Bomb on Hi...
The scope of a critical in-flight event (CIFE) with emphasis on pilot management of available resour...
A 0.165-scale isolated inlet model was tested in the NASA Lewis Research Center 8-ft by 6-ft Superso...
The scope of this study considered the first 15 years of accumulated space station concepts for Init...
A model scale hover test was conducted in the Sikorsky Aircraft Model Rotor hover Facility to identi...
The performance and maturity of a preprototype, three-person capacity, automatically controlled and ...
The High Energy Astronomy Observatory Program is briefly described to introduce guest observers to t...
Tests were conducted, during April and May 1973, on an 0.030-scale replica of the Space Shuttle Vehi...
The theory of Limit Design is the application of the theory of Plasticity to the estimation of the a...
The merits of an advanced helicopter and a tilt rotor aircraft for light utility, scout, and attack ...
Tests were performed to determine low cycle fatigue and crack growth rate properties of one iron-bas...
All tractors tested at the Nebraska Tractor Test Laboratory were certified by their manufacturers as...
Digital simulation models of enhanced TCAS 2/CDTI traffic sensors are developed, based on actual or ...
The purpose of this ATM is to document the Parts Application Analysis (PAA) for the S-Band transmitt...
Master copies of the Lunar Module (LM) Malfunction procedures; pre-print diagrams + hand written not...
The discovery of tremendous amounts of energy from the Atomic Explosion (ex: first Atomic Bomb on Hi...
The scope of a critical in-flight event (CIFE) with emphasis on pilot management of available resour...
A 0.165-scale isolated inlet model was tested in the NASA Lewis Research Center 8-ft by 6-ft Superso...
The scope of this study considered the first 15 years of accumulated space station concepts for Init...
A model scale hover test was conducted in the Sikorsky Aircraft Model Rotor hover Facility to identi...
The performance and maturity of a preprototype, three-person capacity, automatically controlled and ...
The High Energy Astronomy Observatory Program is briefly described to introduce guest observers to t...
Tests were conducted, during April and May 1973, on an 0.030-scale replica of the Space Shuttle Vehi...
The theory of Limit Design is the application of the theory of Plasticity to the estimation of the a...
The merits of an advanced helicopter and a tilt rotor aircraft for light utility, scout, and attack ...
Tests were performed to determine low cycle fatigue and crack growth rate properties of one iron-bas...
All tractors tested at the Nebraska Tractor Test Laboratory were certified by their manufacturers as...
Digital simulation models of enhanced TCAS 2/CDTI traffic sensors are developed, based on actual or ...
The purpose of this ATM is to document the Parts Application Analysis (PAA) for the S-Band transmitt...
Master copies of the Lunar Module (LM) Malfunction procedures; pre-print diagrams + hand written not...
The discovery of tremendous amounts of energy from the Atomic Explosion (ex: first Atomic Bomb on Hi...
The scope of a critical in-flight event (CIFE) with emphasis on pilot management of available resour...
A 0.165-scale isolated inlet model was tested in the NASA Lewis Research Center 8-ft by 6-ft Superso...