| Los Angeles Airways Flight 417 | |
| Date: | August 14, 1968 |
| Type: | Mechanical failure |
| Occurrence Type: | Accident |
| Site: | Compton, California, United States |
| Coordinates: | 33.9°N -130°W |
| Fatalities: | 21 |
| Injuries: | 0 |
| Aircraft Type: | Sikorsky 61L |
| Operator: | Los Angeles Airways |
| Tail Number: | N300Y |
| Passengers: | 18 |
| Crew: | 3 |
| Survivors: | 0 |
| Origin: | Los Angeles International Airport |
| Destination: | Disneyland Heliport |
Los Angeles Airways Flight 417 was a Sikorsky S-61 helicopter that crashed on August 14, 1968 in the city of Compton, California. All eighteen passengers and three crew members were killed. The aircraft was destroyed by impact and fire. According to the National Transportation Safety Board the probable cause of the accident was fatigue failure. The accident happened when the (arbitrarily designated) yellow blade, one of five main rotor blades, separated from the spindle that attached the blade to the rotor head. Following failure, the helicopter was uncontrollable and it fell to the ground. The fatigue crack originated in an area of substandard hardness and inadequate shot peening.[1]
Los Angeles Airways (LAA) Flight 417, piloted by Captain Kenneth Lee Waggoner, former USMC helicopter pilot, was a regularly scheduled passenger flight from Los Angeles International Airport to the Disneyland Heliport in Anaheim, California. The aircraft and crew had completed three round trips to various destinations in the Greater Los Angeles Metropolitan Area beginning at 0607 PDT and departed the ramp at Los Angeles for Flight 417 at 1026. The flight, operating under Visual Flight Rules was cleared by Air traffic control to take off and proceed eastbound at 10:28:15. At 10:29:30 the flight reported to Hawthorne Tower that it was departing Los Angeles eastbound along Imperial Highway at 1200feet. At 10:32:55 Air Traffic Control advised, "L.A. four seventeen, seven miles east, radar service terminated". The flight acknowledged, "Four seventeen thank you". This was the last known radio contact with the flight.
Statements were obtained from 91 witnesses. A consensus of their observations indicates that the helicopter was proceeding along a normal flightpath when a loud noise or unusual sound was heard. A main rotor blade was either observed to separate or was seen separated in the vicinity of the main rotor disc. As the helicopter fell in variously described gyrations, the tail cone either folded or separated. In order to establish an approximate altitude for the flight, several comparative flights were conducted in a similar helicopter. Most witnesses indicated the flights at 1200feet to 1500feet appeared to be most accurate.
The aircraft crashed in Lueders Park in Compton, a recreational park located in a residential area bordering Rosecrans Avenue. The entire fuselage, both engines, main rotor head assembly, four main rotor blades, and the pylon assembly were located in the main impact area. The fifth main rotor blade (yellow)[2] including the sleeve and part of spindle, was located approximately 0.25disp=flipNaNdisp=flip north-west of the main wreckage site. Minor parts associated with this rotor blade were scattered over a three-block area northwest of the park. Examination of the yellow blade spindle (S/N AJ19) revealed a fatigue fracture in the shank of the spindle adjacent to the shoulder in the inboard end of the shank.
a Sikorsky S-61L helicopter, serial number 61031 was the prototype for the S-61L, and had accumulated 11,863.64 total flying hours prior to the day of the accident. It is estimated that approximately 3.17 hours were flown on August 14, 1968. The aircraft was equipped with two General Electric CT58-140-1 turboshaft engines.
The aircraft was serviced with 1000lb of JP-4 fuel and had a takeoff gross weight of 17185lb, which was below the maximum allowable takeoff weight of 19000lb. The computed centre of gravity at the time of the accident was 260.111inches from datum, which is 267.4inches forward of the main rotor hub centerline. The allowable limits are from 256to for a gross weight of 17000lb. The estimated gross weight at the time of the accident was 17118lb.
In the course of the investigation by the National Transportation Safety Board (NTSB) they made the following findings:
Following the initial evidence of a metal fatigue type failure, the National Transportation Safety Board recommended on August 16, 1968 to the Federal Aviation Administration:
On the same date the FAA issued Emergency Airworthiness Directive 68-19-07. The directive has since been amended twice and now requires the following action:[3]