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Accidents · NTSB DEN07FA079 · Final report

Robinson R44 II accident near Ponte Vedra Bch, Florida, March 27, 2007

On March 27, 2007 at about 2:30 pm local time, a Robinson R44 II (helicopter), registered N744SH, was destroyed in an accident near Ponte Vedra Bch, Florida. It was an instructional flight under general aviation rules (Part 91). 2 people were killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

the mechanic's improper installation of the attachment hardware for the servo to swashplate push-pull tube joint which resulted in a disconnection, subsequent loss of control, and impact with terrain. Contributing factors were the company management's inadequate surveillance and enforcement of maintenance procedures, the excessive maintenance workload due to inadequate staffing of maintenance personnel, and the insufficient management of maintenance tasks.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
March 27, 2007 · about 2:30 pm local time
Place
Ponte Vedra Bch, Florida · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Robinson R44 II · all R44 IIs on the register
Registration
N744SH · no longer on the register · serial 10830
Damage
Destroyed
Flight
Instructional flight · general aviation rules (Part 91)

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

The local instructional flight was scheduled for a east departure from the airport and a flight south along the coastline. Several witnesses observed the helicopter approximately 200-500 feet above ground level (agl) in cruise flight along the coastline on a south heading. One witness, a former pilot and mechanic, reported he observed the helicopter in straight and level flight, then heard a change in "rotor noise, followed by a bang/pop/twang sound." The helicopter then "snap-rolled" to the left and descended into the terrain in a nose low attitude. Examination of the helicopter's flight control system revealed that the right forward servo to swashplate push-pull tube joint was disconnected and the attach hardware (bolt, lock nut, two washers, pal nut) was missing. The left forward servo to swashplate push-pull joint was connected; however, the nut was found partially engaged on the bolt threads, and the torque was "finger tight"; no pal nut was noted. Material analysis of the components revealed that only one of the two nuts for the left and right connections were installed, and then only finger tight. The nut on right servo connection rotated off during flight which allowed the bolt to extract itself and disconnect the servo from the push-pull tube. Prior to the accident flight, an inspection, which required the push-pull tubes to servo connections to be disassembled, was performed on the helicopter, and a 0.5-hour maintenance test flight. The mechanic who preformed the inspection, stated he forgot to properly secure the hardware for the left and right servo connections. The mechanic stated the reasons for the error were the following: 1. He was pulled," in all directions" by company personnel since his arrival at that facility; 2. The "reassembly was not opposite of the disassembly," which was a personal maintenance practice he used to eliminate errors; 3. Two nights prior to the completion of the inspection and the maintenance test flight, the apprentice providing assistance, wanted to stay late to finish with the mechanic a certain section of the inspection. As a result, the mechanic forgot to go back and secure the hardware connecting the two push-pull tube to servo joints; 4. The company was understaffed with maintenance personnel. According to the company's maintenance quality control program, any maintenance completed on a helicopter was to be inspected by another mechanic. A review of the program revealed that the mechanics were not following the program, and the company was not providing oversight and enforcing the program.

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

Pilot

  • Certificate: flight instructor, commercial pilot
  • Ratings: instructor: helicopter; rotorcraft: helicopter
  • Flight time: 462 hours in all; 29 in this make and model; 113 in the last 90 days; 47 in the last 30 days; 334 as pilot in command; 174 on instruments
  • Last flight review: March 1, 2007
  • Medical certificate: Class 2 (without waivers/limitations)
  • Seat: left
  • Injury: fatal

Dual student

  • Certificate: student
  • Flight time: 10 hours in all
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 861.6 hours
  • Last inspection: 100-hour inspection, March 1, 2007; 1 hours since
  • Maximum gross weight: 2,500 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine: Lycoming IO-540-AEIA5 (piston); 0 hours total
  • Fire on the ground

The flight

  • Departed from: CRG Jacksonville FL at 2:10 pm
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: from 360° at 10 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 75°F (24°C), dew point 0°F (-18°C)

Injuries

FatalSeriousMinorNone
Crew2

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

The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), has not been read from the NTSB for this case yet; the list appears here once it has. Open the docket at the NTSB.

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 never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.