20130228003979A

Accident · Substantial damage

FAA accident report · Piper PA-32-300 · Sanford, NC · February 28, 2013

Date
February 28, 2013 · 15:56 local
Place
Sanford, NC
Airport
Lee County Regional
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N1953H
Reported as
Piper PA-32-300
Reported engine
Lycoming TI0-540 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
400 total228 in this make and model13 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 02-28-2013, privacy data omitted of pittsboro, NC was in command of Piper cherokee pa 32-300 registration # N1953H, s/n 32-740044, which departed from siler city (5W8) in route to Sanford raleigh exec (tta).

At approx. 15:50 hrs. On final to taa the aircraft landed off the airport, no injuries, two people on board. Inspector wayne vohs assisted inspector tim mcquain and traveled to Sanford (tta) to investigate.

Interviewed pilot privacy data omitted and FBO personnel cheri swanson.

Pilot reported loss of throttle lever response and called tta UNICOM to declare an emergency landing. Pilot flew beyond the runway under power lines, struck a berm for a road and a fence post, causing left main landing gear to depart the aircraft and major left wing damage. Aircraft then landed across road in a field coming to a rest approximately 200 yards past road, resulting in substantial damage to the aircraft.

Inspectors vohs and mcquain inspected the aircraft and verified that throttle lever movement did not consistently move the fuel injection servo lever verifying the statement of the pilot that throttle was unresponsive.

This condition would cause loss of engine power setting control that attributed to the accident.

Aircraft sustained substantial damage.

NTSB arranged for aircraft to be relocated to atlanta air salvage and requested additional disassembly into throttle pedestal area.

Found clevis pin disconnected from throttle/cable end.

More disassembly discovered clevis pin, washer and cotter pin from throttle connection on floor below assembly.

Cotter pin had missing tang and appeared to be improper size.

As the FAA filed it

ON 02-28-2013, ^PRIVACY DATA OMITTED^ OF PITTSBORO, NC WAS IN COMMAND OF PIPER CHEROKEE PA 32-300 REGISTRATION # N1953H, S/N 32-740044, WHICH DEPARTED FROM SILER CITY (5W8) IN ROUTE TO SANFORD RALEIGH EXEC (TTA).

AT APPROX. 15:50 HRS. ON FINAL TO TAA THE AIRCRAFT LANDED OFF THE AIRPORT, NO INJURIES, TWO PEOPLE ON BOARD. INSPECTOR WAYNE VOHS ASSISTED INSPECTOR TIM MCQUAIN AND TRAVELED TO SANFORD (TTA) TO INVESTIGATE.

INTERVIEWED PILOT ^PRIVACY DATA OMITTED^ AND FBO PERSONNEL CHERI SWANSON.

PILOT REPORTED LOSS OF THROTTLE LEVER RESPONSE AND CALLED TTA UNICOM TO DECLARE AN EMERGENCY LANDING. PILOT FLEW BEYOND THE RUNWAY UNDER POWER LINES, STRUCK A BERM FOR A ROAD AND A FENCE POST, CAUSING LEFT MAIN LANDING GEAR TO DEPART THE AIRCRAFT AND MAJOR LEFT WING DAMAGE. AIRCRAFT THEN LANDED ACROSS ROAD IN A FIELD COMING TO A REST APPROXIMATELY 200 YARDS PAST ROAD, RESULTING IN SUBSTANTIAL DAMAGE TO THE AIRCRAFT.

INSPECTORS VOHS AND MCQUAIN INSPECTED THE AIRCRAFT AND VERIFIED THAT THROTTLE LEVER MOVEMENT DID NOT CONSISTENTLY MOVE THE FUEL INJECTION SERVO LEVER VERIFYING THE STATEMENT OF THE PILOT THAT THROTTLE WAS UNRESPONSIVE.

THIS CONDITION WOULD CAUSE LOSS OF ENGINE POWER SETTING CONTROL THAT ATTRIBUTED TO THE ACCIDENT.

AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE.

NTSB ARRANGED FOR AIRCRAFT TO BE RELOCATED TO ATLANTA AIR SALVAGE AND REQUESTED ADDITIONAL DISASSEMBLY INTO THROTTLE PEDESTAL AREA.

FOUND CLEVIS PIN DISCONNECTED FROM THROTTLE/CABLE END.

MORE DISASSEMBLY DISCOVERED CLEVIS PIN, WASHER AND COTTER PIN FROM THROTTLE CONNECTION ON FLOOR BELOW ASSEMBLY.

COTTER PIN HAD MISSING TANG AND APPEARED TO BE IMPROPER SIZE.