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Accidents · NTSB ERA21LA287 · Final report

Piper PA46-500TP accident near Manteo, North Carolina, July 6, 2021

On July 6, 2021 at about 7:07 pm local time, a 2005 Piper PA46-500TP, registered N31062, was substantially damaged in an accident during initial climb near Manteo, North Carolina (Dare County Rgnl airport). It was a personal flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The improperly secured pneumatic compressor discharge air (P3) line coupling nut on the engine, which ultimately allowed the nut to back off resulting in a partial loss of engine power.

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

What the record shows

Date
July 6, 2021 · about 7:07 pm local time
Place
Manteo, North Carolina · Dare County Rgnl · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Piper PA46-500TP, built 2005 · all PA46-500TPs on the register
Registration
N31062 · registry record · serial 4697208
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

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

After takeoff, the pilot retracted the landing gear and the turbopropeller-powered single-engine airplane’s engine lost partial power. The pilot attempted to regain engine power using a manual override but was unsuccessful. A forced landing was made at the departure airport, during which the airplane touched down at intersecting runways and traveled through the grass before coming to a stop, resulting in substantial damage to the fuselage. with the nose gear sheared off. Examination of the airplane after the accident revealed substantial damage to the fuselage. Examination of the engine revealed that the front of the compressor discharge air (P3) pneumatic line was secured to the gas generator case. The P3 line’s rear coupling nut was lockwired to the adjacent bolt. The lockwire was removed and the coupling nut was loosely fitted (no torque) with the adjacent nipple. The exterior surface of the nut exhibited fretting wear from contact with the twists of the lockwire. The fretting wear was observed on the conical surface of the nipple from contact with the mating surface of the tube. Examination at higher magnification of the oval-shaped fretting wear along the outer surface of the “B”-nut mating with the nipple showed the fretting damage occurred due to the nut being in contact with the lockwire while the nut was attempting to move in the counterclockwise direction (in the direction loosening the nut). Since the nut would not move significantly once the lockwire was in place, it suggested that the torque at installation was low, which would have allowed the nut to loosen, thus compromising the seal of the connection. Subsequently, when the pneumatic line seal became loose, it likely resulted in the loss of P3 air pressure and the subsequent partial loss of engine power like what the pilot described. A review of the maintenance records could not determine when the P3 pneumatic line was most recently secured.

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. Loss of engine power (partial) during initial climb defining event
  2. Runway excursion during landing

The NTSB's findings

  • Aircraft › Aircraft power plant › Engine (turbine/turboprop) › Compressor section › Incorrect service/maintenance
  • Aircraft › Aircraft power plant › Engine bleed air system › (general) › Incorrect service/maintenance
  • Personnel issues › Task performance › Maintenance › (general) › Maintenance personnel

Pilot

  • Certificate: airline transport pilot, flight instructor
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 2,659 hours in all; 277 in this make and model; 20 in the last 90 days; 9 in the last 30 days; 2,543 as pilot in command; 137 on instruments
  • Last flight review: November 21, 2020
  • Medical certificate: Class 3 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

Passenger

  • Seat: rgt
  • Injury: no injuries

The aircraft

  • Airframe total time: 1,513 hours
  • Last inspection: annual inspection, July 7, 2020; 123 hours since
  • Maximum gross weight: 5,092 lb
  • Seats: 6
  • Landing gear: retractable
  • Engine: Pratt & Whitney PT6-42A (turboprop); 1,513 hours total

The flight

  • Destination: HEF Manassas VA
  • Flight plan: IFR

Weather at the time

  • Light: daylight
  • Wind: from 190° at 13 knots
  • Visibility: 10 statute miles
  • Sky: broken clouds at 4,800 ft
  • Temperature: 84°F (29°C), dew point 68°F (20°C)
  • Altimeter: 30.13 inHg
  • Observation at 2:55 pm from MQI

Weather report (METAR): METAR KMQI 061855Z AUTO 19013KT 10SM BKN048 29/20 A3013 RMK AO2 T02880202=

Injuries

FatalSeriousMinorNone
Flight crew1
Passengers1

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

11 documents, released by the NTSB on September 14, 2023. 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.

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.