19970126000839A

Accident · Destroyed

FAA accident report · Piper PA-28RT-201 · Chehalis, WA · January 26, 1997

Date
January 26, 1997 · 12:00 local
Place
Chehalis, WA
Airport
Chehalis-Centralia
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N344LC
NTSB investigation
NTSBSEA97LA052
Reported as
Piper PA28RT201
Reported engine
Lycoming IO360E1A
Fatal injuries
0
Pilot’s flight hours
113 total111 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.

Crashed during takeoff. (.4) the first pilot (PIC) and his father, the second pilot, shared the duties of a preflight inspection on the airplane in preparation to perform some touch-and-go landings. The second pilot visually checked both fuel tanks and noted that the left tank was low. He stated that he had mentioned this to the first pilot, and the first pilot did not 'carefully note.' The first pilot selected the left tank for the flight because the left fuel quantity gauge was erroneously indicating a full tank. During the third touch-and-go takeoff, the engine was starved of fuel and suddenly lost all power about 300 feet above the ground. The second pilot, who was also a CFI, immediately took the controls, banked the airplane to the right to avoid trees, and force landed the airplane into an open corn field. The right wing struck the ground during the landing and the airplane nosed over. No preimpact mechanical deficiencies were found with the engine. An examination of the left cockpit fuel quantity gauge revealed that the needle was captured between a deformed face plate and a sticky substance found beneath the glass. The source of the deformation and substance could not be determined.

As the FAA filed it

CRASHED DURING TAKEOFF. (.4) THE FIRST PILOT (PIC) AND HIS FATHER, THE SECOND PILOT, SHARED THE DUTIES OF A PREFLIGHT INSPECTION ON THE AIRPLANE IN PREPARATION TO PERFORM SOME TOUCH-AND-GO LANDINGS. THE SECOND PILOT VISUALLY CHECKED BOTH FUEL TANKS AND NOTED THAT THE LEFT TANK WAS LOW. HE STATED THAT HE HAD MENTIONED THIS TO THE FIRST PILOT, AND THE FIRST PILOT DID NOT 'CAREFULLY NOTE.' THE FIRST PILOT SELECTED THE LEFT TANK FOR THE FLIGHT BECAUSE THE LEFT FUEL QUANTITY GAUGE WAS ERRONEOUSLY INDICATING A FULL TANK. DURING THE THIRD TOUCH-AND-GO TAKEOFF, THE ENGINE WAS STARVED OF FUEL AND SUDDENLY LOST ALL POWER ABOUT 300 FEET ABOVE THE GROUND. THE SECOND PILOT, WHO WAS ALSO A CFI, IMMEDIATELY TOOK THE CONTROLS, BANKED THE AIRPLANE TO THE RIGHT TO AVOID TREES, AND FORCE LANDED THE AIRPLANE INTO AN OPEN CORN FIELD. THE RIGHT WING STRUCK THE GROUND DURING THE LANDING AND THE AIRPLANE NOSED OVER. NO PREIMPACT MECHANICAL DEFICIENCIES WERE FOUND WITH THE ENGINE. AN EXAMINATION OF THE LEFT COCKPIT FUEL QUANTITY GAUGE REVEALED THAT THE NEEDLE WAS CAPTURED BETWEEN A DEFORMED FACE PLATE AND A STICKY SUBSTANCE FOUND BENEATH THE GLASS. THE SOURCE OF THE DEFORMATION AND SUBSTANCE COULD NOT BE DETERMINED.

NTSB investigation

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