19971107032639A

Accident · Substantial damage

FAA accident report · Cessna 421A · Tomahawk, WI · November 7, 1997

Date
November 7, 1997 · 17:15 local
Place
Tomahawk, WI
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2957Q
NTSB investigation
NTSBCHI98LA032
Reported as
Cessna 421A
People aboard
1
Fatal injuries
0
Pilot’s flight hours
28,000 total300 in this make and model40 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.

(Tty) acft auto dis on climb out, upon landing the right ele was found severely damaged. Merrill, WI. (.4)on climb out at 11,000 feet at 700 feet per minute rate of climb on autopilot, the pilot heard a loud bang and felt a 'rapid vibration in the control yoke.' The pilot reported pitch trim was not available and said he checked the engines for proper operations. The flight landed without further incident. Examination of the aircraft revealed substantial damage to the right elevator and trim tab. The rear trim tab linkage bolt was missing and there was little damage to the yoke or trim tab bushing. Paint transfer marks were found on the trim tab from the elevator. An undersized cotter pin was found in the forward linkage bolt. (-23) see narrative #CHI98LA032

As the FAA filed it

(TTY) ACFT AUTO DIS ON CLIMB OUT, UPON LANDING THE RIGHT ELE WAS FOUND SEVERELY DAMAGED. MERRILL, WI. (.4)ON CLIMB OUT AT 11,000 FEET AT 700 FEET PER MINUTE RATE OF CLIMB ON AUTOPILOT, THE PILOT HEARD A LOUD BANG AND FELT A 'RAPID VIBRATION IN THE CONTROL YOKE.' THE PILOT REPORTED PITCH TRIM WAS NOT AVAILABLE AND SAID HE CHECKED THE ENGINES FOR PROPER OPERATIONS. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. EXAMINATION OF THE AIRCRAFT REVEALED SUBSTANTIAL DAMAGE TO THE RIGHT ELEVATOR AND TRIM TAB. THE REAR TRIM TAB LINKAGE BOLT WAS MISSING AND THERE WAS LITTLE DAMAGE TO THE YOKE OR TRIM TAB BUSHING. PAINT TRANSFER MARKS WERE FOUND ON THE TRIM TAB FROM THE ELEVATOR. AN UNDERSIZED COTTER PIN WAS FOUND IN THE FORWARD LINKAGE BOLT. (-23) SEE NARRATIVE #CHI98LA032

NTSB investigation

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