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Accidents · NTSB ERA11LA141 · Final report

Piper PA-31-350 accident near Baltimore, Maryland, February 11, 2011

On February 11, 2011 at about 1:27 am local time, a Piper PA-31-350, registered N31NW, was substantially damaged in an accident during enroute (cruise) near Baltimore, Maryland (Baltimore/Wash. Int. Airport). It was an executive or corporate flight under general aviation rules (Part 91). No one was hurt; 1 person was on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

An in-flight overload failure of the left elevator inboard balance weight rib for undetermined reasons.

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

What the record shows

Date
February 11, 2011 · about 1:27 am local time · cases in 2011
Place
Baltimore, Maryland · Baltimore/Wash. Int. Airport · cases near this airport · map
Type
Accident
Injuries
No one was hurt; 1 person was on board or involved.
Weather
visual conditions (good weather)
Aircraft
Piper PA-31-350 · all PA-31-350s on the register
Registration
N31NW · registry record · serial 318152139
Damage
Substantial damage
Flight
Executive or corporate flight · general aviation rules (Part 91)

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

While cruising at 7,000 feet with the autopilot activated, the pilot reported that the airplane's nose pitched down slightly, then up slightly, followed by another downward pitch that resulted in a 200-foot altitude deviation. The pilot disengaged the autopilot, re-leveled the airplane at 7,000 feet, and re-engaged the autopilot. Several minutes later, the pilot noticed a vibration in the control yoke, which he described as a "buzzing," and noticed that the airplane was flying in a right slight sideslip. The pilot trimmed the rudder and noted no further vibration. The remainder of the flight was uneventful. Upon landing and exiting the airplane, the pilot noted that the outer portion of the left elevator was bent downward, just outboard of the outermost hinge point and at an angle nearly perpendicular to its normal position. Detailed examination of the elevator showed that its forward spar had deformed but had not fractured. The inboard rib of the balance weight rib tip structure was deformed and fractured from its upper to lower chord aft of its leading edge. The fracture features of the rib were consistent with overload separation, and exhibited no evidence of a fatigue failure. No evidence of any preexisting damage was observed. The total number of flight hours the elevator had accumulated prior to being installed on the accident airplane could not be determined, although examination of the elevator and its sub-components confirmed that it complied with all relevant manufacturer's service bulletins and FAA airworthiness directives.

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. Aircraft structural failure during enroute (cruise) defining event

The NTSB's findings

  • cause Aircraft › Aircraft structures › Empennage structure › Spars/ribs (on elevator) › Failure other cases naming the airframe structure
  • cause Not determined › Not determined › (general) › (general) › Unknown/Not determined

Pilot

  • Certificate: airline transport pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane multi-engine; instructor: airplane single-engine; instructor: helicopter; instructor: instrument airplane; instrument: airplane; rotorcraft: helicopter
  • Flight time: 16,835 hours in all; 7,936 in this make and model; 202 in the last 90 days; 74 in the last 30 days; 13,053 as pilot in command; 895 on instruments
  • Last flight review: October 25, 2010
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: no injuries

The aircraft

  • Airframe total time: 11,338 hours
  • Last inspection: annual inspection, July 30, 2010
  • Maximum gross weight: 7,000 lb
  • Seats: 2
  • Landing gear: retractable
  • Engine 1: Lycoming TIO-540 (piston); 0 hours total
  • Engine 2: Lycoming TI0-540 SER (piston); 0 hours total
  • Operator: Laboratory CORP of America Holdings INC

The flight

  • Departed from: BUY Burlington NC at 11:50 pm
  • Destination: BWI Baltimore MD
  • Flight plan: IFR

Weather at the time

  • Light: night
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 21°F (-6°C), dew point 1°F (-17°C)
  • Altimeter: 30.15 inHg

Injuries

FatalSeriousMinorNone
Flight crew1

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

4 documents, released by the NTSB on May 16, 2012. 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/ERA11LA141.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.