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Accidents · NTSB NYC03MA183 · Final report

Beech 1900D accident near Yarmouth, Massachusetts, August 26, 2003

On August 26, 2003 at about 7:40 pm local time, a Beech 1900D, registered N240CJ, was destroyed in an accident near Yarmouth, Massachusetts (Barnstable Municipal Airport). It was a positioning 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 improper replacement of the forward elevator trim cable, and subsequent inadequate functional check of the maintenance performed, which resulted in a reversal of the elevator trim system and a loss of control in-flight. Factors were the flightcrew's failure to follow the checklist procedures, and the aircraft manufacturer's erroneous depiction of the elevator trim drum in the maintenance manual.

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

What the record shows

Date
August 26, 2003 · about 7:40 pm local time
Place
Yarmouth, Massachusetts · Barnstable Municipal Airport · map
Type
Accident
Injuries
2 people were killed.
Weather
visual conditions (good weather)
Aircraft
Beech 1900D · all 1900Ds on the register
Registration
N240CJ · no longer on the register · serial UE-40
Damage
Destroyed
Flight
Positioning flight · general aviation rules (Part 91)

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

The accident flight was the first flight after maintenance personnel replaced the forward elevator trim cable. When the flightcrew received the airplane, the captain did not address the recent cable change noted on his maintenance release. The captain also did not perform a first flight of the day checklist, which included an elevator trim check. Shortly after takeoff, the flightcrew reported a runway trim, and manually selected nose-up trim. However, the elevator trim then traveled to the full nose-down position. The control column forces subsequently increased to 250 pounds, and the flightcrew was unable to maintain control of the airplane. During the replacement of the cable, the maintenance personnel skipped a step in the manufacturer's airliner maintenance manual (AMM). They did not use a lead wire to assist with cable orientation. In addition, the AMM incorrectly depicted the elevator trim drum, and the depiction of the orientation of the cable around the drum was ambiguous. The maintenance personnel stated that they had completed an operational check of the airplane after maintenance. The Safety Board performed a mis-rigging demonstration on an exemplar airplane, which reversed the elevator trim system. An operational check on that airplane revealed that when the electric trim motor was activated in one direction, the elevator trim tabs moved in the correct direction, but the trim wheel moved opposite of the corresponding correct direction. When the manual trim wheel was moved in one direction, the elevator trim tabs moved opposite of the corresponding correct direction.

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; single-engine sea; instrument: airplane
  • Flight time: 2,891 hours in all; 1,364 in this make and model; 211 in the last 90 days; 76 in the last 30 days
  • Last flight review: June 5, 2003
  • Medical certificate: Class 1 (valid medical--w/ waivers/lim.)
  • Seat: frt
  • Injury: fatal

Pilot

  • Certificate: commercial pilot
  • Ratings: multi-engine land; single-engine land; instrument: airplane
  • Flight time: 2,489 hours in all; 689 in this make and model; 222 in the last 90 days; 52 in the last 30 days; 1,667 as pilot in command
  • Last flight review: November 3, 2002
  • Medical certificate: Class 1 (valid medical--w/ waivers/lim.)
  • Seat: rgt
  • Injury: fatal

The aircraft

  • Airframe total time: 16,503 hours
  • Last inspection: continuous airworthiness programme, August 26, 2003; 0 hours since
  • Maximum gross weight: 17,060 lb
  • Seats: 21
  • Landing gear: retractable
  • Engine 1: Pratt & Whitney PT6A-67D (turboprop); 0 hours total
  • Engine 2: Pratt & Whitney PT6A-67D (turboprop); 0 hours total
  • Operator: Colgan Air Inc.

The flight

  • Departed from: HYA Hyannis MA at 7:38 pm
  • Destination: ALB Albany NY
  • Flight plan: IFR
  • Runway 33, 5,252 ft by 150 ft
  • A second pilot was aboard

Weather at the time

  • Light: daylight
  • Wind: at 6 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 73°F (23°C), dew point 68°F (20°C)
  • Altimeter: 29.86 inHg
  • Observation at 7:56 pm from HYA, 4 miles away

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.