20130501006279A

Accident · Substantial damage

FAA accident report · Cessna 421A · Oakland, CA · May 1, 2013

Date
May 1, 2013 · 14:45 local
Place
Oakland, CA
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N216WA
NTSB investigation
NTSBWPR13LA214
Reported as
Cessna 421A
Reported engine
Continental GTSIO-520 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
5,700 total185 in this make and model52 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.

Cessna N216WA s/n 421A-0032.

PIC - privacy data omitted. The airman reported the intended flight was to maintain IFR currency. Aircraft owner privacy data omitted acting as safety pilot while under the hood. Several sucessful approaches were compelted until the final landing in oak rwy 27R. Both pilots confirmed 3 green gear annunciations during approach. Landing was normal and uneventful until rollout when left main gear collapsed causing the aircraft to skid to the left coming to a stop in the dirt at taxiway kilo.

There was no pre or post landing fire and no injuries.

Upon inspection of the aircraft the following damage was noted:

Multiple holes, scrapes and dents in the left wing, aileron and flaps.

Left wing leading edge spar was bent and broken from impact with a pole in the dirt at taxiway kilo.

The left bellcrank pivot bolt sheared.

Left strut bellcrank attach clevis fwd ear broken.

Bellcrank clevis casting at side brace lock link has one side broken off.

The last annual inspection was completed 1/23/2013.

The problem is a repeat discrepancy from 6/2006

SDR FAA report # 2006062700332

As the FAA filed it

CESSNA N216WA S/N 421A-0032.

PIC - ^PRIVACY DATA OMITTED^. THE AIRMAN REPORTED THE INTENDED FLIGHT WAS TO MAINTAIN IFR CURRENCY. AIRCRAFT OWNER ^PRIVACY DATA OMITTED^ ACTING AS SAFETY PILOT WHILE UNDER THE HOOD. SEVERAL SUCESSFUL APPROACHES WERE COMPELTED UNTIL THE FINAL LANDING IN OAK RWY 27R. BOTH PILOTS CONFIRMED 3 GREEN GEAR ANNUNCIATIONS DURING APPROACH. LANDING WAS NORMAL AND UNEVENTFUL UNTIL ROLLOUT WHEN LEFT MAIN GEAR COLLAPSED CAUSING THE AIRCRAFT TO SKID TO THE LEFT COMING TO A STOP IN THE DIRT AT TAXIWAY KILO.

THERE WAS NO PRE OR POST LANDING FIRE AND NO INJURIES.

UPON INSPECTION OF THE AIRCRAFT THE FOLLOWING DAMAGE WAS NOTED:

MULTIPLE HOLES, SCRAPES AND DENTS IN THE LEFT WING, AILERON AND FLAPS.

LEFT WING LEADING EDGE SPAR WAS BENT AND BROKEN FROM IMPACT WITH A POLE IN THE DIRT AT TAXIWAY KILO.

THE LEFT BELLCRANK PIVOT BOLT SHEARED.

LEFT STRUT BELLCRANK ATTACH CLEVIS FWD EAR BROKEN.

BELLCRANK CLEVIS CASTING AT SIDE BRACE LOCK LINK HAS ONE SIDE BROKEN OFF.

THE LAST ANNUAL INSPECTION WAS COMPLETED 1/23/2013.

THE PROBLEM IS A REPEAT DISCREPANCY FROM 6/2006

SDR FAA REPORT # 2006062700332

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 N216WA · 1

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