19970605013519I

Incident · Minor damage

FAA incident report · Beech A36 · Charlottesville, VA · June 5, 1997

Date
June 5, 1997 · 15:30 local
Place
Charlottesville, VA
Airport
Charlottesville-Albemarle
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N2050N
Reported as
Beech A36
People aboard
1
Fatal injuries
0
Pilot’s flight hours
4,500 total50 in this make and model14 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.

Narrative: on June 5, 1997, upon landing at Charlottesville, albermarle airport, Virginia, a noise was heard by the pilot in command. The pilot made a go-around, reported that he cycled the landing gear, and made a successful landing. Inspection of the aircraft revealed damage to all three propeller blades, inboard portion of the flaps, passenger step, and antennas. The investigation revealed a defective nose landing gear door extension/retraction linkage. Further tests of the landing gear warning system, extension and retraction system were satisfactory. The landing gear warning horn was checked for proper operation, and no defects were found. privacy data omitted Mr. Oswald has passed a reexamination flight test. Incident closed.

As the FAA filed it

NARRATIVE: ON JUNE 5, 1997, UPON LANDING AT CHARLOTTESVILLE, ALBERMARLE AIRPORT, VIRGINIA, A NOISE WAS HEARD BY THE PILOT IN COMMAND. THE PILOT MADE A GO-AROUND, REPORTED THAT HE CYCLED THE LANDING GEAR, AND MADE A SUCCESSFUL LANDING. INSPECTION OF THE AIRCRAFT REVEALED DAMAGE TO ALL THREE PROPELLER BLADES, INBOARD PORTION OF THE FLAPS, PASSENGER STEP, AND ANTENNAS. THE INVESTIGATION REVEALED A DEFECTIVE NOSE LANDING GEAR DOOR EXTENSION/RETRACTION LINKAGE. FURTHER TESTS OF THE LANDING GEAR WARNING SYSTEM, EXTENSION AND RETRACTION SYSTEM WERE SATISFACTORY. THE LANDING GEAR WARNING HORN WAS CHECKED FOR PROPER OPERATION, AND NO DEFECTS WERE FOUND. ^PRIVACY DATA OMITTED^ MR. OSWALD HAS PASSED A REEXAMINATION FLIGHT TEST. INCIDENT CLOSED.