ERA14CA463

NTSB accident investigation · Beech D55 · Hazleton, PA · September 27, 2014

Accident · No injuriesData collectionFinal report
Date
September 27, 2014, 13:45 local (17:45 UTC)
Place
Hazleton, PA
Injuries
4 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N222JJBeech D55
Defining event
Landing-landing roll: Miscellaneous/other
Weather
Visual (VMC) · Day
Status
Completed · report January 12, 2015
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20140927019669A
Case key
90183

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

The brake application for unknown reasons resulting in rupture of the left main landing gear tire and tube, and subsequent loss of directional control.

Findings · 3

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.

Landing gear system: brakeAircraft › Aircraft systems · Not specifiedBeech D55: 1 caseAll aircraft: 297 casesProbable cause
Landing gear system: tire casingAircraft › Aircraft systems · Damaged/degradedBeech D55: 2 casesAll aircraft: 36 cases
Landing gear system: tubeAircraft › Aircraft systems · Damaged/degradedBeech D55: 2 casesAll aircraft: 19 cases

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

After an uneventful 30 minute flight the pilot returned to the airport and entered the traffic pattern for a full stop landing on runway 28; the wind at the time was variable at 3 knots. He reported the touchdown was normal, but about 5 to 10 seconds after touchdown, "the plane started rumbling and pulling hard to the left"; he confirmed he was not on the airplane's brakes at that time. He reported the nose steering was not effective, and when the left main landing gear wheel was in the grass, he advanced the left throttle in an attempt to overcome the left turning tendency. The airplane then contacted a temporary rock road and both main landing gears collapsed. All occupants exited the airplane uninjured, and when he deemed it safe, he reentered the airplane and secured the fuel selectors. Postaccident inspection of the airplane by several FAA inspectors revealed the left tire was deflated and a hole was completely worn through the casing on an area of the tread, and also through the tube. Postaccident operational testing of the airplane's brake system revealed no evidence of preimpact failure or malfunction. The brakes released with release of pressure on the brake pedals; no sticking was noted. Damage to a portion of the left wing at the leading edge and main spar was noted. Damage was also noted the main spar of the left aileron, and to structure on the lower fuselage aft of the wing trailing edge.

Factual narrative

After an uneventful 30 minute flight the pilot returned to the airport and entered the traffic pattern for a full stop landing on runway 28; the wind at the time was variable at 3 knots. He reported the touchdown was normal, but about 5 to 10 seconds after touchdown, "the plane started rumbling and pulling hard to the left"; he confirmed he was not on the airplane's brakes at that time. He reported the nose steering was not effective, and when the left main landing gear wheel was in the grass, he advanced the left throttle in an attempt to overcome the left turning tendency. The airplane then contacted a temporary rock road and both main landing gears collapsed. All occupants exited the airplane uninjured, and when he deemed it safe, he reentered the airplane and secured the fuel selectors. Postaccident inspection of the airplane by several FAA inspectors revealed the left tire was deflated and a hole was completely worn through the casing on an area of the tread, and also through the tube. Postaccident operational testing of the airplane's brake system revealed no evidence of preimpact failure or malfunction. The brakes released with release of pressure on the brake pedals; no sticking was noted. Damage to a portion of the left wing at the leading edge and main spar was noted. Damage was also noted the main spar of the left aileron, and to structure on the lower fuselage aft of the wing trailing edge.

Aircraft

Registration
N222JJ
Reported as
Beech D55
Category
Airplane
Serial number
TE-639
Built
1968
Airframe hours
3,463
Engines
Cont Motor IO-520-CB, 250 horsepower, reciprocatingCont Motor IO 520 SERIES, 285 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
Jld Conyngham Ltd
Registered owner
Jld Conyngham Ltd
Airworthiness certificate
Standard, Normal
Last inspection
Annual · July 1, 2014 · 11 hours before
Departed
HZL · Hazelton, PA
Destination
HZL · Hazelton, PA
Airport
HZL · Hazelton Municipal Airport, runway 28, 4,898 × 100 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
53
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 3, With waivers/limitations
Last flight review
May 20, 2013
Seat
Left
Restraint
Lap only
Flight hours
612 total · 203 in this make and model · 435 as pilot in command · 12 in the last 90 days · 2 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 3 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
81 °F, dew point 54 °F
Altimeter
30.23 inHg
Observed at
AVP, 24 nm away

Docket · 11

The files NTSB released with the investigation on December 23, 2014, on NTSB’s docket system: statements, records, photos and specialists’ reports. 15.4 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.