ANC12IA085

NTSB incident investigation · Bellanca 8KCAB · Homer, AK · July 29, 2012

Incident · No injuriesIncident investigationFinal report
Date
July 29, 2012, 14:00 local (22:00 UTC)
Place
Homer, AK
Injuries
1 uninjured
Damage
Minor damage
Phase of flight
Landing
Aircraft
N5026BBellanca 8KCAB
Defining event
Landing-flare/touchdown: Sys/Comp malf/fail (non-power)
Weather
Visual (VMC) · Day
Status
Completed · report June 12, 2013
Report
Approved by Office Director
NTSB office
Alaska Regional Office
Parties
FAA Anchorage FSDO
Case key
84611

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

On this page

Probable cause

The failure of the left main landing gear leg due to fatigue. Contributing to the incident was maintenance personnel's failure to completely remove all corrosion before repainting the gear leg.

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.

Maintenance: repairPersonnel issues › Task performance · Maintenance personnelBellanca 8KCAB: 1 caseAll aircraft: 99 casesProbable cause
Landing gear system: main landing gearAircraft › Aircraft systems · Fatigue/wear/corrosionBellanca 8KCAB: 1 caseAll aircraft: 241 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 was landing the tailwheel-equipped airplane on a dry paved runway. He stated that just after touchdown, he heard a noise and felt the airplane pull to the left. He tried to abort the landing, but noted that the left main landing gear had separated from the fuselage, so he landed the airplane in the grassy area adjacent to the runway. During the landing the airplane sustained minor damage. The spring steel left main landing gear assembly was fractured about 5 inches from the fuselage attach point. Postaccident metallurgical examination revealed that the landing gear leg fractured due to fatigue that initiated from pits on the lower surface of the leg. The pits were filled with brown paint that was covered with white paint. Therefore, it is likely that the pits were formed by corrosion that was not completely removed before the gear leg was repainted.

Factual narrative

On July 29, 2012, about 1400 Alaska daylight time, a Bellanca 8KCAB airplane, N5026B, sustained minor damage during landing at the Homer Airport, Homer, Alaska. The solo airline transport rated pilot was not injured. The airplane was being operated as a 14 Code of Federal Regulations Part 91 personal flight when the incident occurred. Visual meteorological conditions prevailed, and no flight plan was filed. In an interview with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) on August 8, the pilot stated that just after touchdown on the dry paved runway, he heard a noise and felt the airplane pull to the left. He lifted the airplane off the runway, and noticed that the left main landing gear had separated from the fuselage. He elected to immediately land the airplane in the grass safety area adjacent to the runway. The spring steel left main landing gear assembly was fractured approximately 5 inches from the fuselage attach point. An examination of the landing gear assembly was performed by the NTSB Materials Laboratory, and revealed the gear leg fractured due to fatigue that initiated from pits on the lower surface of the leg. The pits were filled with brown paint, and the brown paint was covered with white paint. A complete copy of the NTSB's materials laboratory factual report is included in the public docket for this accident. The pilot did not complete a NTSB Accident/Incident Reporting Form 6120.1.

Aircraft

Registration
N5026B
Reported as
Bellanca 8KCAB
Category
Airplane
Serial number
442-78
Airframe hours
2,314
Engine
Lycoming AEIO-360 SER, 180 horsepower, reciprocating
Damage
Minor damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · January 1, 2012
Departed
Anchorage, AK
Destination
Homer, AK
Flight plan
Unknown
Airport
PAHO · Homer Airport, runway 21, 6,701 × 150 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
57
Injuries
None
Certificate
Airline transport
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1
Seat
Front

Weather

Conditions
Visual (VMC) · Day
Wind
150° at 10 knots, gusting 19
Visibility
10 statute miles
Lowest ceiling
7,000 ft broken
Temperature
55 °F, dew point 45 °F
Altimeter
29.92 inHg
Observed at
PAHO

Docket · 2

The files NTSB released with the investigation on April 18, 2013, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.6 MB in all.