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Accidents · NTSB NYC06MA131 · Final report

Eurocopter EC-135P1 accident near Washington, District of Columbia, May 30, 2006

On May 30, 2006 at about 8:45 pm local time, a Eurocopter EC-135P1 (helicopter), registered N601FH, was destroyed in an accident near Washington, District of Columbia (Whc airport). It was flown under charter and air-taxi rules (Part 135). 1 person was killed and 3 people were seriously injured. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The operator's inadequate training program and the pilot's failure to maintain control of the helicopter following his inadvertent disabling of the No. 1 and then the No. 2 engine full authority digital engine control system.

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

What the record shows

Date
May 30, 2006 · about 8:45 pm local time
Place
Washington, District of Columbia · Whc · map
Type
Accident
Injuries
1 person was killed and 3 people were seriously injured.
Weather
visual conditions (good weather)
Aircraft
Eurocopter EC-135P1 · all EC-135P1s on the register
Registration
N601FH · registry record · serial 0069
Damage
Destroyed
Flight
Flight · charter and air-taxi rules (Part 135)

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

The pilot reported that, during his first approach to the hospital helipad, the helicopter "shuffled," and the No. 1 engine rpm increased. The pilot stated that he increased collective pitch, reduced the throttle on the No. 1 engine, and aborted the landing. He noted that the No. 1 engine was no longer controlled by the full authority digital engine control (FADEC) system and that he had to control it manually. The pilot twice overflew the helipad, and, while maneuvering for another approach, he lost control of the helicopter, and it descended and struck a tree and the ground. Examination of the throttles, throttle linkages, engines, control systems, cockpit display system (CDS), and FADEC units revealed no evidence of any preimpact mechanical anomalies. Postaccident testing of the engines and analysis of data retrieved from the CDS and FADEC units revealed that the accident pilot had inadvertently moved the No. 1 throttle out of its neutral detent, placing the engine in manual mode and out of FADEC control. Although the pilot recognized that the No. 1 engine was no longer controlled by the FADEC, he responded with further manual throttle adjustments and did not perform the published procedure to restore FADEC control to the engine. The data showed that, as the pilot continued to manually control the No. 1 engine, he subsequently moved the No. 2 throttle out of its detent, placing that engine also in manual mode and out of FADEC control. With neither engine under FADEC control, the pilot attempted control of the rotor rpm while controlling both engines manually. This configuration resulted in a high-workload scenario in which it would be particularly challenging for the pilot to control the helicopter during the maneuvering and approach-to-land phases of flight. The accident helicopter was the only EC-135P1 CDS variant in the operator's fleet. Its engines, its displays, and its procedure for restoring FADEC control differed from the EC-135 variant in which the accident pilot was trained. According to the manufacturer's training guidelines, differences training is recommended before a pilot who is trained on another variant flies the EC-135P1 CDS. However, the investigation revealed that the operator provided the accident pilot only about an hour of formal differences training in the EC-135P1 CDS, and there was no evidence that the training adequately covered that variant's FADEC-restore procedures and other issues pertinent to flight safety. The pilot had accumulated about 914 hours of flight experience in EC-135s, with about 45 hours in the EC-135P1 CDS variant. The accident was not the first indication to the operator that pilots who were trained in another variant experienced difficulties with the accident helicopter. According to one other pilot and the accident pilot, they each previously experienced events involving loss of FADEC control in the accident helicopter (in November 2005 and March 2006, respectively) but completed successful landings. The operator determined no mechanical explanation for the events and did not report, and was not required to report, them to its Federal Aviation Administration (FAA) principal operations and maintenance inspectors. The other pilot reported that, at the time of his November 2005 event, he was untrained in the EC-135P1 CDS and was completely unfamiliar with the procedure required to restore FADEC control. That pilot reported that, during his event, he oversped the helicopter's engines and the main rotor, and, as a result, the operator removed the helicopter from service, conducted inspections of the engines and main rotor system, and determined that differences training was needed for the EC-135P1 CDS; however, the operator failed to adequately provide such training. Because the FAA had no knowledge of the previous events with the accident helicopter, it had no indication to suspect that the differences training implemented by the operator was deficient.

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: airline transport pilot, commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane; instrument: helicopter; rotorcraft: helicopter
  • Flight time: 15,613 hours in all; 914 in this make and model; 65 in the last 90 days; 22 in the last 30 days
  • Last flight review: December 1, 2005
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: rgt
  • Injury: serious injuries

The aircraft

  • Airframe total time: 2,995 hours
  • Last inspection: approved inspection programme, May 1, 2006
  • Maximum gross weight: 6,250 lb
  • Seats: 4
  • Landing gear: fixed
  • Engine 1: Pratt & Whitney Canada PW206B (turboshaft); 0 hours total
  • Engine 2: Pratt & Whitney Canada PW206B (turboshaft); 0 hours total

The flight

  • Departed from: Washington DC at 8:38 pm
  • Destination: DC08 Washington DC

Weather at the time

  • Light: daylight
  • Wind: from 120° at 9 knots
  • Visibility: 7 statute miles
  • Sky: broken clouds at 6,000 ft
  • Temperature: 90°F (32°C), dew point 68°F (20°C)
  • Altimeter: 30.03 inHg
  • Observation at 4:52 pm from DCA, 5 miles away

Injuries

FatalSeriousMinorNone
Crew3
Passengers1

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.