20040616012579A

Accident · Minor damage

FAA accident report · Cessna 421B · Bend, OR · June 16, 2004

Date
June 16, 2004 · 09:30 local
Place
Bend, OR
Airport
Bend Municipal Airport
Phase of flight
To Aborted (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N332CC
NTSB investigation
NTSBSEA04LA108
Reported as
Cessna 421B
People aboard
3
Fatal injuries
0
Pilot’s flight hours
14,800 total25 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) Aircraft commenced take-off roll at take-off power. As pilot released brakes, aircraft veered right, immediately power was reduced to flight idle and the rudder and brakes applied. According to the pilot, braking was unresponsive, even with 2nd pilot assisting in braking. Aircraft rolled off right side of runway, the nose gear collapsed. Damage to the aircraft included the left tunnel structure at the nose gear trunnion attach point and propeller damage as well. Investigation of the left wheel brake system revealed that the two outer (out of the four) brake pads were missing or had fallen out. These missing pads could not be located.

As the FAA filed it

(-23) AIRCRAFT COMMENCED TAKE-OFF ROLL AT TAKE-OFF POWER. AS PILOT RELEASED BRAKES, AIRCRAFT VEERED RIGHT, IMMEDIATELY POWER WAS REDUCED TO FLIGHT IDLE AND THE RUDDER AND BRAKES APPLIED. ACCORDING TO THE PILOT, BRAKING WAS UNRESPONSIVE, EVEN WITH 2ND PILOT ASSISTING IN BRAKING. AIRCRAFT ROLLED OFF RIGHT SIDE OF RUNWAY, THE NOSE GEAR COLLAPSED. DAMAGE TO THE AIRCRAFT INCLUDED THE LEFT TUNNEL STRUCTURE AT THE NOSE GEAR TRUNNION ATTACH POINT AND PROPELLER DAMAGE AS WELL. INVESTIGATION OF THE LEFT WHEEL BRAKE SYSTEM REVEALED THAT THE TWO OUTER (OUT OF THE FOUR) BRAKE PADS WERE MISSING OR HAD FALLEN OUT. THESE MISSING PADS COULD NOT BE LOCATED.

NTSB investigation

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