20100831044889A

Accident · Substantial damage

FAA accident report · Piper PA-28-140 · Anderson, IN · August 31, 2010

Date
August 31, 2010 · 19:00 local
Place
Anderson, IN
Airport
Anderson Municipal-Darlington Fld
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N3969K
NTSB investigation
NTSBCEN10CA518
Reported as
Piper PA-28-140
Reported engine
Lycoming 0-320 series
People aboard
3
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
9,230 total416 in this make and model26 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.

A CFI was the PIC of a discovery flight with two passengers departing from kaid runway 18 on the evening of 31 August 2010. Winds were reported at 240 at 4 knots; OAT of 29 c. the pilot did not make a weight and balance calculation prior to flight. Based on the pilot's estimate of passenger weights, the aircraft was operated at a very high gross weight. (The operator was unable provide a passenger manifest or to provide an accurate record of passsenger weights). The pilot stated that the aircraft's performance with takeoff power set appeared to be normal. The pilot stated that he rotated at approximately 60 mph, however, he also stated that he may have pulled the aircraft off the runway instead of letting the aircraft fly itself off the runway (as specified in the manufacturer's owner's handbook). Shortly after lift off, the pilot stated the aircraft rolled left. As the pilot made control inputs to correct the roll, he felt that the aircraft was not climbing normally and noted that the aircraft then began sinking. The aircraft touched down in a grassy area to the immediate east of runway 18 with takeoff power set. As the aircraft touched down in a nose high attitude, the lower portion of the aft fuselage contacted a frangible runway marker and several runway lights. The pilot then selected idle power and turned on to the adjacent crossing runway (12/30) and taxied back to the kaid ramp. Post flight inspection revealed the aircraft experienced damage to the left stabilator, and the lower surface of the aft fuselage former had significant impact damage.

As the FAA filed it

A CFI WAS THE PIC OF A DISCOVERY FLIGHT WITH TWO PASSENGERS DEPARTING FROM KAID RUNWAY 18 ON THE EVENING OF 31 AUGUST 2010. WINDS WERE REPORTED AT 240 AT 4 KNOTS; OAT OF 29 C. THE PILOT DID NOT MAKE A WEIGHT AND BALANCE CALCULATION PRIOR TO FLIGHT. BASED ON THE PILOT'S ESTIMATE OF PASSENGER WEIGHTS, THE AIRCRAFT WAS OPERATED AT A VERY HIGH GROSS WEIGHT. (THE OPERATOR WAS UNABLE PROVIDE A PASSENGER MANIFEST OR TO PROVIDE AN ACCURATE RECORD OF PASSSENGER WEIGHTS). THE PILOT STATED THAT THE AIRCRAFT'S PERFORMANCE WITH TAKEOFF POWER SET APPEARED TO BE NORMAL. THE PILOT STATED THAT HE ROTATED AT APPROXIMATELY 60 MPH, HOWEVER, HE ALSO STATED THAT HE MAY HAVE PULLED THE AIRCRAFT OFF THE RUNWAY INSTEAD OF LETTING THE AIRCRAFT FLY ITSELF OFF THE RUNWAY (AS SPECIFIED IN THE MANUFACTURER'S OWNER'S HANDBOOK). SHORTLY AFTER LIFT OFF, THE PILOT STATED THE AIRCRAFT ROLLED LEFT. AS THE PILOT MADE CONTROL INPUTS TO CORRECT THE ROLL, HE FELT THAT THE AIRCRAFT WAS NOT CLIMBING NORMALLY AND NOTED THAT THE AIRCRAFT THEN BEGAN SINKING. THE AIRCRAFT TOUCHED DOWN IN A GRASSY AREA TO THE IMMEDIATE EAST OF RUNWAY 18 WITH TAKEOFF POWER SET. AS THE AIRCRAFT TOUCHED DOWN IN A NOSE HIGH ATTITUDE, THE LOWER PORTION OF THE AFT FUSELAGE CONTACTED A FRANGIBLE RUNWAY MARKER AND SEVERAL RUNWAY LIGHTS. THE PILOT THEN SELECTED IDLE POWER AND TURNED ON TO THE ADJACENT CROSSING RUNWAY (12/30) AND TAXIED BACK TO THE KAID RAMP. POST FLIGHT INSPECTION REVEALED THE AIRCRAFT EXPERIENCED DAMAGE TO THE LEFT STABILATOR, AND THE LOWER SURFACE OF THE AFT FUSELAGE FORMER HAD SIGNIFICANT IMPACT DAMAGE.

NTSB investigation

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