20190209010069A

Accident · Substantial damage

FAA accident report · Piper PA46-500TP · Vero Beach, FL · February 9, 2019

Date
February 9, 2019 · 12:10 local
Place
Vero Beach, FL
Airport
Vero Beach
Phase of flight
Other, Specify
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N403MM
Reported as
Piper PA46-500TP
Reported engine
Pratt & Whitney Canada PT6A-42A
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
10,800 total613 in this make and model44 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 February 9, 2019, at approximately 12.10 local time, the pilot of N403MM, a Piper 46-500TP single engine airplane, experienced an engine loss, followed by smoke and fire after aircraft testing. During the testflight the pilot of N403MM lost directional control while executing various developmental sideslips as assigned by engineers from the manufacturer and under the observation of a chase aircraft. The airplane entered an inverted spin, which required the pilot to deploy the spin chute to recover. Normal flight was resumed and while the airplane returned to the airport, the pilot observed low oil pressure and high oil temperature. The crew of the chase aircraft declared an emergency after communicating with the test pilot. While spiraling down overhead of Vero Beach, the pilot noticed unsual engine noise, followed by smoke, fire and complete engine loss. The pilot successfully landed the airplane without any further damage on runway 04 at the Vero Beach Airport, Florida, and was able to exit on taxiway c. the fire crew extinguished the engine fire. The engine and its components were destroyed due to the fire. The pilot experienced no injuries. Further examination of the airplane will reveal the extent of structural or any other damage, which may have been caused by negative g-forces the airplane was exposed to during the inverted spin. VMC conditions were reported at the time of the accident with the winds from 350 degrees at 10 knots and the visibility at least 10 statute miles.

As the FAA filed it

ON FEBRUARY 9, 2019, AT APPROXIMATELY 12.10 LOCAL TIME, THE PILOT OF N403MM, A PIPER 46-500TP SINGLE ENGINE AIRPLANE, EXPERIENCED AN ENGINE LOSS, FOLLOWED BY SMOKE AND FIRE AFTER AIRCRAFT TESTING. DURING THE TESTFLIGHT THE PILOT OF N403MM LOST DIRECTIONAL CONTROL WHILE EXECUTING VARIOUS DEVELOPMENTAL SIDESLIPS AS ASSIGNED BY ENGINEERS FROM THE MANUFACTURER AND UNDER THE OBSERVATION OF A CHASE AIRCRAFT. THE AIRPLANE ENTERED AN INVERTED SPIN, WHICH REQUIRED THE PILOT TO DEPLOY THE SPIN CHUTE TO RECOVER. NORMAL FLIGHT WAS RESUMED AND WHILE THE AIRPLANE RETURNED TO THE AIRPORT, THE PILOT OBSERVED LOW OIL PRESSURE AND HIGH OIL TEMPERATURE. THE CREW OF THE CHASE AIRCRAFT DECLARED AN EMERGENCY AFTER COMMUNICATING WITH THE TEST PILOT. WHILE SPIRALING DOWN OVERHEAD OF VERO BEACH, THE PILOT NOTICED UNSUAL ENGINE NOISE, FOLLOWED BY SMOKE, FIRE AND COMPLETE ENGINE LOSS. THE PILOT SUCCESSFULLY LANDED THE AIRPLANE WITHOUT ANY FURTHER DAMAGE ON RUNWAY 04 AT THE VERO BEACH AIRPORT, FLORIDA, AND WAS ABLE TO EXIT ON TAXIWAY C. THE FIRE CREW EXTINGUISHED THE ENGINE FIRE. THE ENGINE AND ITS COMPONENTS WERE DESTROYED DUE TO THE FIRE. THE PILOT EXPERIENCED NO INJURIES. FURTHER EXAMINATION OF THE AIRPLANE WILL REVEAL THE EXTENT OF STRUCTURAL OR ANY OTHER DAMAGE, WHICH MAY HAVE BEEN CAUSED BY NEGATIVE G-FORCES THE AIRPLANE WAS EXPOSED TO DURING THE INVERTED SPIN. VMC CONDITIONS WERE REPORTED AT THE TIME OF THE ACCIDENT WITH THE WINDS FROM 350 DEGREES AT 10 KNOTS AND THE VISIBILITY AT LEAST 10 STATUTE MILES.