ERA09CA374

NTSB accident investigation · Boeing A75N1(PT17) · Quinton, VA · June 29, 2009

Accident · No injuriesData collectionFinal report
Date
June 29, 2009, 17:30 local (21:30 UTC)
Place
Quinton, VA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N38978Boeing A75N1(PT17)
Defining event
Landing-landing roll: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed · report December 15, 2009
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
Case key
74174

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 directional control on landing for undetermined reasons.

Findings · 1

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 determinedBoeing A75N1(PT17): 8 casesAll aircraft: 2,247 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

During the landing rollout on runway 28 with a light and variable wind, the pilot applied the brakes to stop the airplane. The right brake “grabbed and would not release,” and he applied “hard left brake and full left rudder” to maintain control of the airplane. The tail of the airplane began to rise and he then released the left brake. The airplane subsequently nosed over and came to rest inverted, incurring substantial damage to the right wing, the wing spar, and the vertical stabilizer. Post-accident inspection by a Federal Aviation Administration (FAA) inspector found that the Hayes Industries expanding drum brakes appeared to be operating normally. The nearest weather reporting station reported at 1754, or approximately 24 minutes after the accident, that the wind was from 250 degrees at 8 knots. The weather reporting airport is located approximately 9 nautical miles west-northwest of the accident airport.

Factual narrative

According to the pilot, during the landing rollout on runway 28 with a light and variable wind, he applied the brakes to stop the airplane. The right brake “grabbed and would not release,” and he applied “hard left brake and full left rudder” to maintain control of the airplane. The tail of the airplane began to rise and he then released the left brake. The airplane subsequently nosed over and came to rest inverted, incurring substantial damage to the right wing, the wing spar, and the vertical stabilizer. Post-accident inspection by a Federal Aviation Administration (FAA) inspector found that the Hayes Industries expanding tube brakes appeared to be operating normally. The nearest weather reporting station reported at 1754, or approximately 24 minutes after the accident, that the wind was from 250 degrees at 8 knots. The weather reporting airport is located approximately 9 nautical miles west-northwest of the accident airport.

Aircraft

Registration
N38978
Reported as
Boeing A75N1(PT17)
Category
Airplane
Serial number
75-3756
Airframe hours
2,703
Engine
Lycoming R680-13, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Parker Joseph M
Registered owner
Parker Joseph M
Airworthiness certificate
Standard, Normal
Last inspection
Annual · June 23, 2009
Departed
W96 · Quinton, VA
Destination
W96 · Quinton, VA
Airport
W96 · New Kent County Airport, runway 28, 3,600 × 75 ft, asphalt

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
64
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, With waivers/limitations
Last flight review
August 22, 2006
Flight hours
1,261 total · 244 in this make and model · 1,261 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
250° at 8 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
88 °F, dew point 54 °F
Altimeter
29.54 inHg
Observed at
KRIC, 9 nm away

Docket · 4

The files NTSB released with the investigation on August 24, 2009, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.0 MB in all.