IAD03LA066

NTSB accident investigation · Cessna T210N · Hampton Bays, NY · July 21, 2003

Accident · Minor injuriesLimited investigationFinal report
Date
July 20, 2003, 21:10 local (Jul 21, 2003, 01:10 UTC)
Place
Hampton Bays, NY
Injuries
5 minor
Damage
Destroyed
Phase of flight
Enroute
Aircraft
N155RRCessna T210N
Weather
Visual (VMC) · Night
Status
Completed · report November 25, 2003
Report
Approved by Office Director
Parties
Teledyne Continental Motors, FAA/FSDO
FAA report
20030720030349A
Case key
57514

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

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Probable cause

A loss of engine power for undetermined reasons. A factor was the lack of suitable terrain for the forced landing.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of engine powerCruise
Reason for occurrence undeterminedCause
Forced landingEmergency descent/landing
On ground/water encounter with terrain/waterEmergency landing
Terrain condition - water
Terrain condition - none suitableFactor

Analysis

The airplane had just leveled off at 2,000 feet msl, on a night, over-water, non-scheduled passenger flight, when the engine began to lose power. The pilot immediately turned the auxiliary fuel pump on, switched fuel tanks, and turned towards land. The engine continued to lose power, and the pilot prepared the airplane and the four passengers for a water landing. The pilot pushed the mixture control level full forward, and completed the emergency checklist items; however, the engine continued to lose power and could not be restarted. The airplane came to rest in approximately 8 feet of water, about 150 yards off shore. Examination of the airplane revealed approximately 50 gallons of fuel onboard, and no anomalies were noted with the fuel system. The engine was test run on the airframe, after the oil and spark plugs (electrodes were wet) were removed and replaced. After several attempts, the engine started and ran at various power settings without interruption. The ignition switch was also tested and no abnormalities were found.

Factual narrative

On July 20, 2003, at 2110 eastern daylight time, a Cessna T210N, N155RR, was substantially damaged during a forced landing into Peconic Bay, near Hampton Bays, Long Island, New York. The certificated commercial pilot and the four passengers sustained minor injuries. A dog was fatally injured. Night visual meteorological conditions prevailed for the flight that originated at East Hampton Airport (HTO), East Hampton, New York, about 2100, destined for LaGuardia Airport (LGA), New York, New York. No flight plan was filed for the non-scheduled passenger flight conducted under 14 CFR Part 135.

In a written statement, the pilot reported that after departing runway 28, he turned to a heading of 290 degrees, and climbed to an altitude of 2,000 feet mean sea level (msl). Shortly thereafter, the autopilot disengaged, and the engine began to lose power. The pilot immediately turned the auxiliary fuel pump on, switched fuel tanks, and turned toward Francis S. Gabreski Airport (FOK), Westhampton Beach, New York. The engine continued to lose power, and the pilot prepared the airplane and the passengers for a water landing.

The pilot pushed the mixture control level full forward, and completed the emergency checklist items. However, the engine continued to lose power. As a last resort, the pilot pushed in and held the emergency fuel pump on, and tried to restart the engine; however, the engine would not start.

The airplane came to rest in approximately 8 feet of water, about 150 yards off shore.

On July 21, 2003, the airplane was recovered from the water under the supervision of a Federal Aviation Administration (FAA) inspector. The inspector stated that the airplane was relatively intact, and the engine was securely attached to the airframe. The propeller blades exhibited minimal damage.

Both wings were removed from the fuselage, and approximately 50 gallons of light blue fuel were drained from both wing fuel tanks. The firewall fuel filter screen was found full of fuel, and absent of debris. Both of the wing fuel finger screens were also absent of debris.

On July 22-23, 2003, the FAA inspector witnessed the preparation and test run of the engine. Mechanics prepared the engine by replacing the oil, spark plugs (electrodes were wet), and installed two separate fuel tanks to replace the wing fuel tanks. After several attempts, the engine started and ran at various power settings without interruption.

The ignition switch was removed and tested, and no mechanical deficiencies were noted.

The pilot reported a total of 2,500 flight hours, of which, 400 hours were in make and model.

Weather at the time of the accident at Gabreski Airport, about 6 nautical miles away, at 2053, was reported as wind from 200 degrees at 5 knots, visibility 7 statute miles, clear skies, temperature 70 degrees F, and dewpoint 66 degrees F, and a barometric pressure of 30.01 inches HG.

Aircraft

Registration
N155RR
Reported as
Cessna T210N
Category
Airplane
Serial number
21063286
Airframe hours
3,264.2
Engine
Continental TSIO-520-R, 310 horsepower, reciprocating
Damage
Destroyed
Flight
Part 135
Registered owner
Air Hamptons
Airworthiness certificate
Standard, Normal
Last inspection
Annual · May 23, 2003 · 61.4 hours before
Departed
HTO · East Hampton, NY
Destination
LGA · La Guardia, NY

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
25
Injuries
Minor
Certificates
Flight instructor, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Last flight review
July 2, 2003
Seat
Left
Flight hours
2,500 total · 400 in this make and model · 2,260 as pilot in command · 120 in the last 90 days

Weather

Conditions
Visual (VMC) · Night
Wind
200° at 5 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
70 °F, dew point 66 °F
Altimeter
30.01 inHg
Observed at
KFOK, 6 nm away

FAA reports on this event · 1

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