- 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.
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.