20000426022339I

Incident · Minor damage

FAA incident report · Cessna 140 · Greenville, MI · April 26, 2000

Date
April 26, 2000 · 18:00 local
Place
Greenville, MI
Airport
Greenville Municipal Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N2255V
Reported as
Cessna 140
People aboard
2
Fatal injuries
0
Pilot’s flight hours
220 total30 in this make and model60 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)Pilot was practicing landings at (6D6), on third pilot claimed he encountered a wind gust during flare and then nosed into the runway hitting the prop and the main gear. The pilot stated his indicated approach speed was approx. 60. The aircraft bounced and then settled to the runway. Damage was only to the prop, and internal engine inspection requirements - AD for prop strike. Left main wheel brake rotor also contaced the pavement when the gear flexed on initial impact (minor scraping on rotor edge noted). No internal gear support structure damage was found during inspection. The aircraft was inspected by an A&P, a serviceable prop was installed, and on 4-27-00 the aircraft was ferried to lowell (24C) for repairs.

As the FAA filed it

(-23)PILOT WAS PRACTICING LANDINGS AT (6D6), ON THIRD PILOT CLAIMED HE ENCOUNTERED A WIND GUST DURING FLARE AND THEN NOSED INTO THE RUNWAY HITTING THE PROP AND THE MAIN GEAR. THE PILOT STATED HIS INDICATED APPROACH SPEED WAS APPROX. 60. THE AIRCRAFT BOUNCED AND THEN SETTLED TO THE RUNWAY. DAMAGE WAS ONLY TO THE PROP, AND INTERNAL ENGINE INSPECTION REQUIREMENTS - AD FOR PROP STRIKE. LEFT MAIN WHEEL BRAKE ROTOR ALSO CONTACED THE PAVEMENT WHEN THE GEAR FLEXED ON INITIAL IMPACT (MINOR SCRAPING ON ROTOR EDGE NOTED). NO INTERNAL GEAR SUPPORT STRUCTURE DAMAGE WAS FOUND DURING INSPECTION. THE AIRCRAFT WAS INSPECTED BY AN A&P, A SERVICEABLE PROP WAS INSTALLED, AND ON 4-27-00 THE AIRCRAFT WAS FERRIED TO LOWELL (24C) FOR REPAIRS.

Other reports on N2255V · 1

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