19970417014839I

Incident · Minor damage

FAA incident report · Cessna 310 · Denver, CO · April 17, 1997

Date
April 17, 1997 · 19:40 local
Place
Denver, CO
Airport
Centennial Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N5232A
Reported as
Cessna 310
Reported engine
Continental O470L
People aboard
2
Fatal injuries
0
Pilot’s flight hours
1,531 total1,268 in this make and model137 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: Mr. Rhodes experienced an unsafe gear indication after departing apa enroute to cys, he attempted an emergency gear extension then executed a flyby and apa atlt advised him that the nose gear appeared only partially extended. Mr. Rhodes landed the C-310 on runway 35R and the nose gear collapsed on rollout. An inspection revealed the cause of the malfunction to be failure of the landing gear actuator mechanism intermediate gear drive tube assembly. M or d report submitted, damage to the aircraft was minor and the pilot and aircraft were found to be in compliance. No further action.

As the FAA filed it

NARRATIVE: MR. RHODES EXPERIENCED AN UNSAFE GEAR INDICATION AFTER DEPARTING APA ENROUTE TO CYS, HE ATTEMPTED AN EMERGENCY GEAR EXTENSION THEN EXECUTED A FLYBY AND APA ATLT ADVISED HIM THAT THE NOSE GEAR APPEARED ONLY PARTIALLY EXTENDED. MR. RHODES LANDED THE C-310 ON RUNWAY 35R AND THE NOSE GEAR COLLAPSED ON ROLLOUT. AN INSPECTION REVEALED THE CAUSE OF THE MALFUNCTION TO BE FAILURE OF THE LANDING GEAR ACTUATOR MECHANISM INTERMEDIATE GEAR DRIVE TUBE ASSEMBLY. M OR D REPORT SUBMITTED, DAMAGE TO THE AIRCRAFT WAS MINOR AND THE PILOT AND AIRCRAFT WERE FOUND TO BE IN COMPLIANCE. NO FURTHER ACTION.