20050310005799I

Incident · Minor damage

FAA incident report · Cirrus SR20 · Jacksonville, FL · March 10, 2005

Date
March 10, 2005 · 19:47 local
Place
Jacksonville, FL
Airport
Craig Municipal Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N8160C
NTSB investigation
NTSBMIA05IA087
Reported as
Cirrus SR20
Reported engine
Continental IO360*
People aboard
2
Fatal injuries
0
Pilot’s flight hours
148 total77 in this make and model40 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) During landing on runway 05 at Craig Municipal Airport, Jacksonville, Florida, pilot allowed Cirrus SR-20, N8160C, to experience a moderate bounce. Although such bounce did not result in a significant impact with the runway surface, the nose wheel assembly broke away from the nose gear strut at a welded connection joining the two components. A post incident inspection of such welded joint revealed a separation between approximately one third of the circumference of the weld and the hollow nose gear strut. This separation of the welded joint was rusty and pitted, indicating a pre-incident condition, and appeared to be caused by an inadequate welding procedure during the manufacturing process of the assembly. The assembly described herein was sent to the NTSB lab for further analysis, and associated follow-up with the aircraft manufacturer.

As the FAA filed it

(-23) DURING LANDING ON RUNWAY 05 AT CRAIG MUNICIPAL AIRPORT, JACKSONVILLE, FLORIDA, PILOT ALLOWED CIRRUS SR-20, N8160C, TO EXPERIENCE A MODERATE BOUNCE. ALTHOUGH SUCH BOUNCE DID NOT RESULT IN A SIGNIFICANT IMPACT WITH THE RUNWAY SURFACE, THE NOSE WHEEL ASSEMBLY BROKE AWAY FROM THE NOSE GEAR STRUT AT A WELDED CONNECTION JOINING THE TWO COMPONENTS. A POST INCIDENT INSPECTION OF SUCH WELDED JOINT REVEALED A SEPARATION BETWEEN APPROXIMATELY ONE THIRD OF THE CIRCUMFERENCE OF THE WELD AND THE HOLLOW NOSE GEAR STRUT. THIS SEPARATION OF THE WELDED JOINT WAS RUSTY AND PITTED, INDICATING A PRE-INCIDENT CONDITION, AND APPEARED TO BE CAUSED BY AN INADEQUATE WELDING PROCEDURE DURING THE MANUFACTURING PROCESS OF THE ASSEMBLY. THE ASSEMBLY DESCRIBED HEREIN WAS SENT TO THE NTSB LAB FOR FURTHER ANALYSIS, AND ASSOCIATED FOLLOW-UP WITH THE AIRCRAFT MANUFACTURER.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N8160C · 1

Matched to the same aircraft by N-number and date.