20130501005929A

Accident · Substantial damage

FAA accident report · Adolphson Tim E CCK-1865 · Bellingham, WA · May 1, 2013

Date
May 1, 2013 · 18:32 local
Place
Bellingham, WA
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N88XC
NTSB investigation
NTSBWPR13CA220
Reported as
Adolphson Tim E CCK-1865
Reported engine
Amateur-built UNKNOWN ENG
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
30,000 total13 in this make and model

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 5/1/2013 , at approximately 1832 PDT, an amateur built exp. Make: Adolphson Tim E, model: CCK-1865 aircraft, sustained substancial damage while performing a touch and go at the Bellingham airport. Directional control was lost after landing rollout resulting in ground loop of aircraft the son of the PIC {pilot in command)was at the controls during the landing and subsequent ground loop to provide input on aircraft performance .the son remarked right after landing and just pror to the ground loop that the aircraft was skittish. The PIC took controll of aircraft immediatley after the ground loop. PIC contacted a fixed base operator on the field to assist in removal of aircraft from runway,

Investigation confirmed minor damage to right wing tip, right wing strut separation at main landing gear attach bracket, right wheel fracture, right caliper bracket bent and caliper torn off. Right aileron sustained substancial damage at control rod attach point with major deformation to structure of the aileron . Pilot and passenger were not injured

As the FAA filed it

ON 5/1/2013 , AT APPROXIMATELY 1832 PDT, AN AMATEUR BUILT EXP. MAKE: ADOLPHSON TIM E, MODEL: CCK-1865 AIRCRAFT, SUSTAINED SUBSTANCIAL DAMAGE WHILE PERFORMING A TOUCH AND GO AT THE BELLINGHAM AIRPORT. DIRECTIONAL CONTROL WAS LOST AFTER LANDING ROLLOUT RESULTING IN GROUND LOOP OF AIRCRAFT THE SON OF THE PIC {PILOT IN COMMAND)WAS AT THE CONTROLS DURING THE LANDING AND SUBSEQUENT GROUND LOOP TO PROVIDE INPUT ON AIRCRAFT PERFORMANCE .THE SON REMARKED RIGHT AFTER LANDING AND JUST PROR TO THE GROUND LOOP THAT THE AIRCRAFT WAS SKITTISH. THE PIC TOOK CONTROLL OF AIRCRAFT IMMEDIATLEY AFTER THE GROUND LOOP. PIC CONTACTED A FIXED BASE OPERATOR ON THE FIELD TO ASSIST IN REMOVAL OF AIRCRAFT FROM RUNWAY,

INVESTIGATION CONFIRMED MINOR DAMAGE TO RIGHT WING TIP, RIGHT WING STRUT SEPARATION AT MAIN LANDING GEAR ATTACH BRACKET, RIGHT WHEEL FRACTURE, RIGHT CALIPER BRACKET BENT AND CALIPER TORN OFF. RIGHT AILERON SUSTAINED SUBSTANCIAL DAMAGE AT CONTROL ROD ATTACH POINT WITH MAJOR DEFORMATION TO STRUCTURE OF THE AILERON . PILOT AND PASSENGER WERE NOT INJURED

NTSB investigation

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