20020809022999A

Accident · Substantial damage

FAA accident report · Cessna 310N · Grand Junction, CO · August 9, 2002

Date
August 9, 2002 · 14:58 local
Place
Grand Junction, CO
Airport
Walker Field
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N111KC
NTSB investigation
NTSBDEN02LA093
Reported as
Cessna 310N

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) Mr. Quisenberry was providing multiengine dual instruction to Mr. Houghton in the aircraft. They had departed glenwood springs airport around 0930 hrs the day of the accident. After completing several legs of a cross country flight they arrived back at glenwood springs around 1400 hrs and were going to perform a short field landing. Mr. Houghton was flying the aircraft. On short final to runway 32 the aircraft developed a high sink rate. Full power was added but the aircraft contacted the runway hard. It became airborne again as a result of the power application. The gear was not raised as Mr. Quisenberry thought it might be damaged. The right main gear was observed trailing behind the right wing. The aircraft diverted to rifle, CO. But once there, the decision was made to go to Grand Junction because of better crash rescue facilities. The right main gear fell off near rifle. Once at Grand Junction, the gear was raised for a gear up landing rather than land with one main gear missing. On final engine and props were secured and aircraft was landed gear up.

As the FAA filed it

(-23) MR. QUISENBERRY WAS PROVIDING MULTIENGINE DUAL INSTRUCTION TO MR. HOUGHTON IN THE AIRCRAFT. THEY HAD DEPARTED GLENWOOD SPRINGS AIRPORT AROUND 0930 HRS THE DAY OF THE ACCIDENT. AFTER COMPLETING SEVERAL LEGS OF A CROSS COUNTRY FLIGHT THEY ARRIVED BACK AT GLENWOOD SPRINGS AROUND 1400 HRS AND WERE GOING TO PERFORM A SHORT FIELD LANDING. MR. HOUGHTON WAS FLYING THE AIRCRAFT. ON SHORT FINAL TO RUNWAY 32 THE AIRCRAFT DEVELOPED A HIGH SINK RATE. FULL POWER WAS ADDED BUT THE AIRCRAFT CONTACTED THE RUNWAY HARD. IT BECAME AIRBORNE AGAIN AS A RESULT OF THE POWER APPLICATION. THE GEAR WAS NOT RAISED AS MR. QUISENBERRY THOUGHT IT MIGHT BE DAMAGED. THE RIGHT MAIN GEAR WAS OBSERVED TRAILING BEHIND THE RIGHT WING. THE AIRCRAFT DIVERTED TO RIFLE, CO. BUT ONCE THERE, THE DECISION WAS MADE TO GO TO GRAND JUNCTION BECAUSE OF BETTER CRASH RESCUE FACILITIES. THE RIGHT MAIN GEAR FELL OFF NEAR RIFLE. ONCE AT GRAND JUNCTION, THE GEAR WAS RAISED FOR A GEAR UP LANDING RATHER THAN LAND WITH ONE MAIN GEAR MISSING. ON FINAL ENGINE AND PROPS WERE SECURED AND AIRCRAFT WAS LANDED GEAR UP.

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 N111KC · 1

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