20211115020529A

Accident · Substantial damage

FAA accident report · Piper PA-22-160 · West Union, OH · November 15, 2021

Date
November 15, 2021 · 17:30 local
Place
West Union, OH
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3463Z
NTSB investigation
NTSBCEN22LA038
Reported as
Piper PA-22-160
Reported engine
Lycoming 0-320 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Student
Pilot’s flight hours
51 total43 in this make and model19 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.

On Monday, November 15, 2021, at approximately 1818 EDT, a Piper PA-22 aircraft, registration n-number N3463Z, was involved in an accident when it exited the runway and crashed into a fence in West Union, Ohio, at the adams county airport (kamt). The aircraft departed the lawrenceburg county airport (2M2) at approximately 1630 EDT.

The pilot reported that he was on a solo cross-country flight in furtherance of his private pilot certificate when the accident occurred. The pilot stated that after a descent from 5,500 ft to 2,500FT, the airplane began to roll left unless he continuously held about 3/4 right aileron input. The use of rudder did not null the left roll tendency. Due to the left roll and lower cloud bases ahead, he elected to divert to alexander salamon airport (kamt). After an initial attempt to land on runway 5, he entered left traffic for runway 23.during the landing flare, the airplane continued the left roll and touched down hard a little past the 1, 000 ft runway touchdown markers the airplane bounced and touched back down before departing the left side of the runway where it impacted a ditch and nosed over, sustaining substantial damage to the fuselage and engine mount.

FAA airworthiness inspectors assisted by local aircraft mechanics inspected the accident aircraft?s primary flight control linkages, control surfaces, and secondary flight control linkages and surfaces. During this post-accident examination, control cable continuity and routing was verified from rudder pedals to the rudder and full rudder travel was observed. The aileron system was inspected, control cable continuity and routing was verified from the control column to each aileron. Full travel of each aileron was observed. The aileron/rudder interconnect was also verified and found to be operational with no restrictions. The aileron control yoke was found to be improperly rigged so that when the ailerons were even with the wingtips the yoke was approximately 20 degrees offset to the left, which when placed in a neutral position would correspond to a turn to the right.

As the FAA filed it

ON MONDAY, NOVEMBER 15, 2021, AT APPROXIMATELY 1818 EDT, A PIPER PA-22 AIRCRAFT, REGISTRATION N-NUMBER N3463Z, WAS INVOLVED IN AN ACCIDENT WHEN IT EXITED THE RUNWAY AND CRASHED INTO A FENCE IN WEST UNION, OHIO, AT THE ADAMS COUNTY AIRPORT (KAMT). THE AIRCRAFT DEPARTED THE LAWRENCEBURG COUNTY AIRPORT (2M2) AT APPROXIMATELY 1630 EDT.

THE PILOT REPORTED THAT HE WAS ON A SOLO CROSS-COUNTRY FLIGHT IN FURTHERANCE OF HIS PRIVATE PILOT CERTIFICATE WHEN THE ACCIDENT OCCURRED. THE PILOT STATED THAT AFTER A DESCENT FROM 5,500 FT TO 2,500FT, THE AIRPLANE BEGAN TO ROLL LEFT UNLESS HE CONTINUOUSLY HELD ABOUT 3/4 RIGHT AILERON INPUT. THE USE OF RUDDER DID NOT NULL THE LEFT ROLL TENDENCY. DUE TO THE LEFT ROLL AND LOWER CLOUD BASES AHEAD, HE ELECTED TO DIVERT TO ALEXANDER SALAMON AIRPORT (KAMT). AFTER AN INITIAL ATTEMPT TO LAND ON RUNWAY 5, HE ENTERED LEFT TRAFFIC FOR RUNWAY 23.DURING THE LANDING FLARE, THE AIRPLANE CONTINUED THE LEFT ROLL AND TOUCHED DOWN HARD A LITTLE PAST THE 1, 000 FT RUNWAY TOUCHDOWN MARKERS THE AIRPLANE BOUNCED AND TOUCHED BACK DOWN BEFORE DEPARTING THE LEFT SIDE OF THE RUNWAY WHERE IT IMPACTED A DITCH AND NOSED OVER, SUSTAINING SUBSTANTIAL DAMAGE TO THE FUSELAGE AND ENGINE MOUNT.

FAA AIRWORTHINESS INSPECTORS ASSISTED BY LOCAL AIRCRAFT MECHANICS INSPECTED THE ACCIDENT AIRCRAFT?S PRIMARY FLIGHT CONTROL LINKAGES, CONTROL SURFACES, AND SECONDARY FLIGHT CONTROL LINKAGES AND SURFACES. DURING THIS POST-ACCIDENT EXAMINATION, CONTROL CABLE CONTINUITY AND ROUTING WAS VERIFIED FROM RUDDER PEDALS TO THE RUDDER AND FULL RUDDER TRAVEL WAS OBSERVED. THE AILERON SYSTEM WAS INSPECTED, CONTROL CABLE CONTINUITY AND ROUTING WAS VERIFIED FROM THE CONTROL COLUMN TO EACH AILERON. FULL TRAVEL OF EACH AILERON WAS OBSERVED. THE AILERON/RUDDER INTERCONNECT WAS ALSO VERIFIED AND FOUND TO BE OPERATIONAL WITH NO RESTRICTIONS. THE AILERON CONTROL YOKE WAS FOUND TO BE IMPROPERLY RIGGED SO THAT WHEN THE AILERONS WERE EVEN WITH THE WINGTIPS THE YOKE WAS APPROXIMATELY 20 DEGREES OFFSET TO THE LEFT, WHICH WHEN PLACED IN A NEUTRAL POSITION WOULD CORRESPOND TO A TURN TO THE RIGHT.

NTSB investigation

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