19971218039159A

Accident · Destroyed

FAA accident report · Piper PA-28R-200 · Skidmore, WV · December 18, 1997

Date
December 18, 1997 · 20:20 local
Place
Skidmore, WV
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N9418N
NTSB investigation
NTSBNYC98LA045
Reported as
Piper PA28R200
Reported engine
Continental IO360*
Fatal injuries
0
Pilot’s flight hours
880 total14 in this make and model30 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.

(-23) Engine failed in flight. Pilot attempted restart with no success. A/c substantially damaged upon landing. (.4)the airplane was in cruise flight at 7,500 feet with the engine producing satisfactory power. The pilot said the engine slowly and smoothly lost power over a 10-15 second duration. The engine completely lost power over an unlighted rural area and the pilot struck trees and collided with terrain during the subsequent forced landing. Examination of aircraft records revealed the engine and the fuel control were overhauled by their respective manufacturers and the engine was installed 2 weeks prior to the accident. The engine had accumulated 14.6 hours since overhaul. Examination of the engine revealed no mechanical deficiencies. Examination of the fuel control servo revealed that a lock nut was no longer installed. The initial flow tests revealed a flow rate equivalent to idle cut off. When a test nut was installed, the unit flowed 'perfectly.' When questioned about the performance of the fuel servo and the engine with the outer nut no longer installed in the servo, the inspector stated, 'basically, what it does is it shuts off the fuel when that nut backs off. It's just like pulling it to idle cut off.'

As the FAA filed it

(-23) ENGINE FAILED IN FLIGHT. PILOT ATTEMPTED RESTART WITH NO SUCCESS. A/C SUBSTANTIALLY DAMAGED UPON LANDING. (.4)THE AIRPLANE WAS IN CRUISE FLIGHT AT 7,500 FEET WITH THE ENGINE PRODUCING SATISFACTORY POWER. THE PILOT SAID THE ENGINE SLOWLY AND SMOOTHLY LOST POWER OVER A 10-15 SECOND DURATION. THE ENGINE COMPLETELY LOST POWER OVER AN UNLIGHTED RURAL AREA AND THE PILOT STRUCK TREES AND COLLIDED WITH TERRAIN DURING THE SUBSEQUENT FORCED LANDING. EXAMINATION OF AIRCRAFT RECORDS REVEALED THE ENGINE AND THE FUEL CONTROL WERE OVERHAULED BY THEIR RESPECTIVE MANUFACTURERS AND THE ENGINE WAS INSTALLED 2 WEEKS PRIOR TO THE ACCIDENT. THE ENGINE HAD ACCUMULATED 14.6 HOURS SINCE OVERHAUL. EXAMINATION OF THE ENGINE REVEALED NO MECHANICAL DEFICIENCIES. EXAMINATION OF THE FUEL CONTROL SERVO REVEALED THAT A LOCK NUT WAS NO LONGER INSTALLED. THE INITIAL FLOW TESTS REVEALED A FLOW RATE EQUIVALENT TO IDLE CUT OFF. WHEN A TEST NUT WAS INSTALLED, THE UNIT FLOWED 'PERFECTLY.' WHEN QUESTIONED ABOUT THE PERFORMANCE OF THE FUEL SERVO AND THE ENGINE WITH THE OUTER NUT NO LONGER INSTALLED IN THE SERVO, THE INSPECTOR STATED, 'BASICALLY, WHAT IT DOES IS IT SHUTS OFF THE FUEL WHEN THAT NUT BACKS OFF. IT'S JUST LIKE PULLING IT TO IDLE CUT OFF.'

NTSB investigation

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