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Accidents · NTSB WPR14LA253 · Final report

Mcdonnell Douglas Helicopter 500N accident near Santa Monica, California, April 18, 2014

On April 18, 2014 at about 8:40 pm local time, a 1993 Mcdonnell Douglas Helicopter 500N, registered N522GS, was substantially damaged in an accident during landing near Santa Monica, California (Santa Monica Muni airport). It was a personal flight under general aviation rules (Part 91). No one was hurt; 4 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The fracture of the right aft landing gear strut due to undetected fatigue cracking in an inboard rivet hole.

Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.

What the record shows

Date
April 18, 2014 · about 8:40 pm local time · cases in 2014
Place
Santa Monica, California · Santa Monica Muni · cases near this airport · map
Type
Accident
Injuries
No one was hurt; 4 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Mcdonnell Douglas Helicopter 500N, built 1993 · all 500Ns on the register
Registration
N522GS · registry record · serial LN056
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The private pilot/owner of the helicopter was conducting a local personal flight. The pilot reported that, upon landing, he slowly sat the helicopter down on a landing pad and then felt it "drastically" slip to the right. He then lifted the helicopter off the pad, at which time a passenger verified that the right aft landing gear strut was broken. A passenger reported that, upon touchdown, he heard a "loud pop." The Federal Aviation Administration (FAA) had previously issued an airworthiness directive (AD) applicable to the accident helicopter make and model to detect cracks that could result in the failure of the strut and subsequent loss of helicopter control during landing. The AD required modifications to the landing gear strut rivet holes and fairings and subsequent initial dye penetrant inspections followed by continuing 10x magnified visual inspections at intervals not to exceed every 100 hours time in service or during each annual inspection. According to the FAA, the AD was complied with at an airframe total time of 2,248.3 hours. At the time of the accident, the total airframe time was 2,274 hours. Examination of the right aft landing gear strut revealed that it had fractured due to undetected fatigue cracking in an inboard rivet hole. The fatigue cracks were very small, and given their size, they likely would not have been detectible by the existing required visual inspections. The cracks initiated after the rivet hole diameter was increased; therefore, they initiated after the initial penetrant inspection. Although it is possible that the fatigue cracks were the result of a degradation in material properties or, more likely, due to greater loads from a previous hard landing or normal landing on primarily the right skid, the investigation was not able to determine the origin of the fatigue cracks based on the available information.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Landing gear collapse during landing defining event

The NTSB's findings

Pilot

  • Certificate: private
  • Ratings: single-engine land; rotorcraft: helicopter
  • Flight time: 2,110 hours in all; 368.5 in this make and model; 32 in the last 90 days; 22 in the last 30 days
  • Last flight review: May 8, 2012
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 2,274 hours
  • Last inspection: 100-hour inspection, December 16, 2013
  • Maximum gross weight: 3,350 lb
  • Seats: 5
  • Landing gear: fixed
  • Engine: Rolls Royce 250C20RZ (turboshaft); 2,213 hours total
  • Operator: V & A Aviation LLC

The flight

  • Departed from: CMA Camarillo CA at 7:50 pm
  • Destination: SMO Santa Monica CA
  • Flight plan: none

Weather at the time

  • Light: daylight
  • Wind: from 240° at 8 knots
  • Visibility: 10 statute miles
  • Sky: a few clouds at 3,500 ft
  • Temperature: 68°F (20°C), dew point 54°F (12°C)
  • Altimeter: 29.92 inHg
  • Observation at 8:51 pm from KSMO

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers3

Documents from the investigation the NTSB's docket: the evidence folder behind the report

7 documents, released by the NTSB on June 29, 2016. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Connections how this case links to the rest of the register

Aircraft
Place

The whole map of how records connect · these connections as data: /graph/accident/WPR14LA253.json.

The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.