Primary finding
Probable cause
The pilot’s failure to maintain airspeed in instrument meteorological conditions, which resulted in an aerodynamic stall.
Investigator assessment
Analysis narrative
The instrument-rated pilot was issued a clearance to descend to 4,000 feet for radar vectors to a nonprecision instrument approach in instrument meteorological conditions (IMC). The last 1 minute 23 seconds of radar data indicated the airplane leveled at 4,000 feet for about 35 seconds and then varied between 3,800 feet and 3,900 feet for the remainder of the flight for which data was available. During this timeframe, the airspeed decreased from 131 knots to 57 knots. Witnesses observed the airplane descending in a spin, and one reported hearing the engine running. Recorded engine data showed an increase in engine power near stall speed, which was likely the pilot's response to the low airspeed. The airplane damage was consistent with a low-speed impact with some rotation about the airplane's vertical axis. The pilot did not make any transmissions to air traffic control indicating any abnormalities or emergency. Postaccident examination of the airplane revealed no anomalies that would have precluded normal operation. During training on the accident airplane, the instructor recommended that the pilot get 25 to 50 hours of flight in visual meteorological conditions before flying in IMC in order to gain more familiarity with the radios, switches, and navigation equipment. The pilot only had 14 hours of flight time in the accident airplane before the accident flight, however it could not determined whether this played a role in the accident.
Source record
Factual narrative
HISTORY OF FLIGHT On May 2, 2010, about 2016 eastern daylight time (EDT), a JetProp DLX Piper PA-46-350P, N135CC, sustained substantial damage on impact with terrain near New Albany, Indiana. Instrument meteorological conditions prevailed at the time of the accident. The private pilot and passenger were fatally injured. The 14 CFR Part 91 personal flight was operating on an instrument rules (IFR) flight plan. The flight departed from Barkley Regional Airport (PAH), Paducah, Kentucky, about 1836 central daylight time (CDT) and was en route to Bowman Field Airport (LOU), Louisville, Kentucky. About 1800 CDT, an employee of a fixed base operator at PAH stated that he directed the parking of the airplane. The pilot requested 40 gallons of fuel per side. The employee did not see any leaks from the airplane, and the airplane looked to be in “real good shape.” About 1801-1805 CDT, the Washington Automated Flight Service Station, WS030 position, provided a weather briefing to a caller who had represented N135CC. The caller requested to be provided with “just a metar” at Louisville so he could see if he needed to go under visual flight rules (VFR) or IFR. When asked by the briefer if the caller was leaving soon, the caller said “yes.” The conversation continued and WS030 stated: “uh looks like you’ll have to go i f r *(louisville’s) callin it wind one seventy at five nine miles light rain ceiling nine hundred broken one thousand one hundred overcast temperature an dew point both twenty one… however at standiford they have six miles moderate rain an mist uh one thousand three hundred broken an one thousand nine hundred overcast” The caller then filed an IFR flight plan with a “filed off” time of “twenty minutes thirty minutes,” an altitude of “two one zero,” direct to “louisville bowman,” and a time en route of 45 minutes. The alternate airport was Louisville International Airport-Standiford Field (SDF), Louisville, Kentucky. WS030 stated, “an ya got the airmet sierra for i f r ceilings below a thousand visibilities below three precipitation an *(mist) an uh conditions are forecast to continue through o three hundred both for turbulence an the i f r” At 1826 CDT, N135CC requested an IFR clearance to LOU from PAH air traffic control. The clearance was, “cleared to bowman airport at filed maintain three thousand expect flight level two one zero within one zero minutes….” At 1833 CDT, N135CC was cleared for takeoff. A transcription of transmissions by N135CC and Louisville/Standiford Air Traffic Control Tower, Departure One Radar, at the following times, states, in part: 2002:30 EDT, N135CC, “louisville approach jet prop one three five charlie charlie with you one three thousand for one one thousand” 2002:36 EDT, DR1, “november one three five charlie charlie lousiville approach information romeo is current at bowman expect a v o r approach runway two four 2002:43 EDT, N135CC, “five charlie charlie has romeo now sir 2002:46 EDT, DR1, november five charlie charlie roger 2004:26 EDT, DR1, november five charlie charlie descend and maintain seven thousand 2004:30 EDT, N135CC, (unintelligible) thousand five charlie charlie 2009:20 EDT, DR1, november five charlie charlie descend and maintain four thousand 2009:23 EDT, N135CC, four thousand for five charlie charlie 2010:35 EDT, DR1, november five charlie charlie fly heading zero five zero it’ll be vectors north of Louisville international 2010:39 EDT, N135CC, zero five zero on the heading five charlie charlie 2014:17 EDT, DR1, novenber five charlie uh sierra is now current at bowman they just went i f r uh i believe the ceiling was eight hundred it’ll be coming out here shortly on my system you can go ahead and pick up uh sierra if you like 2014:30 EDT, N135CC, five charlie charlie getting sierra 2016:54 EDT, DR1, (unintelligible) five charlie charlie uh fly heading zero six zero descend and maintain three thousand There were no further recorded transmissions by N135CC. A witness reported that the airplane approached from the southeast with a “loud” engine sound. The airplane then went “upside down” and entered a “spiral nose-dive." The witness also reported that there was no smoke or fire from the airplane. PERSONNEL INFORMATION The pilot, age 59, held a private pilot certificate with airplane single-engine land, glider, and instrument airplane ratings. On November 13, 1986, he was issued a private pilot certificate with a glider rating. On January 28, 1994, he was issued an airplane single-engine land rating. On April 28, 1998, he was issued an instrument airplane rating. According to Federal Aviation Administration (FAA) records, on March 13, 2007, the pilot was involved in a runway incursion at Tucson International Airport, Tucson, Arizona. The pilot received an air traffic control clearance to taxi to runway 11L, which he read back correctly. The pilot stated that although he read the clearance as given, he taxied onto runway 11L expecting an immediate takeoff as he was aware of and saw air traffic on final approach for the same runway. The pilot was piloting a PA-46, N870FS, at the time of the runway incursion. On March 8, 2010, the pilot began JetProp Factory Training, which included 7 flights and 8.5 hours of flight time in the accident airplane. The president of JetProp stated that most of its customers received 5-10 hours of flight training, the amount of which depends on their ability. Most customers convert the airplane they have been flying so their panels are virtually the same. The pilot purchased an existing JetProp to train in, so the airplane and panel were new to him. The pilot was an average pilot with fairly good pilot skills, but he was always hunting around the panel for radios, switches, and navigation equipment. Because of this, it was recommended to the pilot that he should accumulate 25-50 hours under VFR before flying in instrument meteorological conditions without a safety pilot, to which the pilot agreed. The JetProp Factory Training endorsement in the pilot's logbook was dated March 11, 2010. From March 12 to April 25, 2010, there were 5 entries logging flights of the accident airplane, of which only three entries had an associated flight time, which totaled 5.6 hours. The pilot's total flight time, based upon logbook entries, was about 2,493.7 hours, which included entries for a Piper PA-46, N870FS. AIRCRAFT INFORMATION The airplane was manufactured in 1999 as a Piper PA-46-350P, serial number 4636192, and was modified by Rocket Engineering Corp. under supplemental type certificate (STC) ST00541SE at a total time and Hobbs time of 354.8 hours, dated January 21, 2002. Under STC ST00541SE, the design change was for the installation of a Pratt & Whitney PT6A-34. The airplane was equipped with a Hartzell HC-E4N-3M, 4-blade composite propeller. Piper Aircraft had not provided any PA-46-350P engineering and/or flight test data to Rocket Engineering Corp. for its STC ST00541SE. An Aircraft Registration Application by Deeems Holdings, LLC was signed by the pilot on March 8, 2010. The airplane received its last annual inspection, dated May 21, 2009, at a Hobbs and total time of 1,396 hours. The engine received its last annual inspection, dated May 21, 2009, at a Hobbs time of 1,396 hours and a total time of 1,041.2 hours. According to aircraft and engine logbook entries, dated March 8, 2010, the Hobbs time was 1,388 hours. A FlightSafety International JetProp DLX Pilot Training Manual recovered from the airplane states that the airspeed indicator green arc (normal operating range) is 68-172 knots indicated airspeed (KIAS) and the white arc (flaps down) is 57-117 KIAS. METEOROLOGICAL INFORMATION The LOU automated surface observing system (ASOS), located about 10.7 nautical mile (NM) and 80. 4 degrees from the acc