ERA18LA021

NTSB accident investigation · Socata TB200 · Annapolis, MD · November 10, 2017

Accident · No injuriesClass 2 · LimitedFinal report
Date
November 10, 2017, 15:20 local (20:20 UTC)
Place
Annapolis, MD
Injuries
3 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N207GTSocata TB200
Defining event
Maneuvering: Powerplant sys/comp malf/fail
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
Investigation class
Class 2
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20171110018449A
Case key
96314

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

A loss of engine power for undetermined reasons after the disconnection of the propeller governor control due to inadequate securenment during maintenance.

Findings · 2

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Not determinedNot determined › Not determined · Unknown/Not determinedSocata TB200: 1 caseAll aircraft: 2,247 casesProbable cause
Propeller system: propeller governorAircraft › Aircraft propeller/rotor · Not serviced/maintainedSocata TB200: 1 caseAll aircraft: 16 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The pilot stated that, about 45 minutes after departure, he felt a subtle vibration in the engine. A few minutes later, the propeller rpm increased uncommanded to 2,700 rpm and remained "pegged at the redline." The pilot was unable to control the rpm and the vibration increased, followed by smoke in the cabin and a loss of engine power; the pilot subsequently performed a forced landing, impacted a pole and guardrail, and the left wing and horizontal stabilator separated. Postaccident examination of the engine revealed that the propeller governor control arm had disconnected from the propeller governor. It is likely that during maintenance conducted 5 months before the accident, the linkage was not properly secured, and the bolt eventually backed out of the propeller control arm, which resulted in the separation; however this would not have directly resulted in the loss of engine power. The examination of the airframe and engine was otherwise unable to identify a definitive cause for the loss of engine power.

Factual narrative

On November 10, 2017, about 1520 eastern standard time, a Socata TB200, N207GT, operated by Tipton Tampico LLC, was substantially damaged during a forced landing near Annapolis, Maryland. The commercial pilot and the two passengers were not injured. The personal flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed, and no flight plan was filed for the flight that departed Tipton Airport (FME), Fort Meade, Maryland, about 1430. The pilot was conducting a sightseeing flight with his two children around the eastern shore of Maryland. About 45 minutes after departure, the airplane was at an altitude of 1,500 ft and about 25 miles southeast of FME, when the pilot felt a very light and subtle vibration from the engine. Shortly thereafter, the propeller rpm increased to 2,700 rpm uncommanded and remained "pegged at the redline." The pilot followed the emergency checklist and reduced engine power to remain below redline rpm, but it had little effect. The airplane was 11 miles southeast of FME when the engine vibration increased, and the cockpit started filling-up with smoke, so he diverted to Lee Airport (ANP) Annapolis, Maryland. The pilot reported that the engine gauges were all "indicating green" during this time, but once the situation started deteriorating rapidly, he focused on flying the airplane and did not recall reading the gauges again. Immediately after turning south towards ANP at around 1,400 feet, the engine experienced a total loss of power. The pilot realized that the airplane would not be able reach the airport and he made a forced landing on a road. The airplane struck a light pole, spun around, and impacted a guardrail before coming to rest. The impact sheared off the left wing and the horizontal stabilator. The engine remained attached to the fuselage but separated from the top engine mounts and came to rest in a vertical, nose down position. A postaccident examination of the engine revealed the propeller governor linkage was not connected to the propeller governor. The bolt and cotter key that is needed to secure the linkage to the propeller governor was missing. Further examination of the engine revealed that the fuel filter contained some debris, but it was not obstructed. No other mechanical deficiencies were found with the fuel system or engine that would have precluded normal operation of the engine. A review of the engine's maintenance logbook revealed that five months before the accident, on June 24, 2017, the propeller assembly was removed and reinstalled for a starter ring gear, alternator belt and crankshaft seal replacement. The engine's last annual inspection was conducted on October 24, 2017, at a total time of 1,496.53 hours. During that inspection, no anomalies were identified and logged. The airplane and engine then accrued about 13 hours since the annual inspection at the time of the accident. The pilot held a commercial pilotcertificate with ratings for airplane single-engine land instrument airplane and powered lift, instrument airplane. His most recent Federal Aviation Administration (FAA) second-class medical certificate was issued on June 13, 2017. The pilot reported 730 total hours of flight experience, with 13 hours in the accident airplane make and model. The weather conditions reported at FME, 12-miles northeast of the accident site, at 1524, included wind from 350° at 12 knots gusting to 17 knots, visibility 10 miles, clear skies, temperature 3° C, dew point -9° C, and an altimeter setting of 30.38 inches of mercury.

Aircraft

Registration
N207GT
Reported as
Socata TB200 (XL)
Category
Airplane
Serial number
2078
Built
2001
Airframe hours
1,510.03
Engine
Lycoming IO-360-A1B6D, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
1World Aero, LLC, doing business as 1World Aero, LLC
Registered owner
Tipton Tampico LLC
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 24, 2017 · 13 hours before
Departed
FME · Fort Meade, MD
Destination
FME · Fort Meade, MD
Airport
ANP · Lee
Equipment
ADS-B, Auto-pilot, Onboard weather, Stall warning system

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
32
Injuries
None
Certificates
Private, Commercial, Military
Airplane ratings
Single-engine land
Instrument ratings
Powered-lift, Airplane
Medical
Class 2, Without waivers/limitations
Last flight review
June 7, 2017
Seat
Left
Restraint
3-point
Flight hours
730 total · 13 in this make and model · 5 in the last 90 days · 0 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
350° at 12 knots, gusting 17
Visibility
10 statute miles
Lowest ceiling
None
Temperature
37 °F, dew point 16 °F
Altimeter
30.37 inHg
Observed at
FME, 5 nm away

Docket · 9

The files NTSB released with the investigation on October 17, 2020, on NTSB’s docket system: statements, records, photos and specialists’ reports. 15.0 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.