N106JG

Destroyed
Fatal

Piper PA-32R-301TS/N: 32R-8229059

Accident Details

Date
Tuesday, September 24, 2002
NTSB Number
MIA02FA173
Location
Yeehaw Junction, FL
Event ID
20020930X05244
Coordinates
27.666666, -80.916664
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
2
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
2

Probable Cause and Findings

the pilot's continued flight into known severe weather, resulting in an in-flight separation of the right wing, vertical stabilizer and the stabilator. Factors in this accident were heavy thunderstorm, and failure of the FAA controllers to provide the pilot information on observed weather areas, and the specialist at the AFSS to provide the pilot with forecasted adverse weather conditions.

Aircraft Information

Registration
N106JG
Make
PIPER
Serial Number
32R-8229059
Engine Type
Reciprocating
Year Built
1982
Model / ICAO
PA-32R-301TP32R
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
D A DECISION LLC
Address
1239 E LAKE COLONY DR
Status
Deregistered
City
MAITLAND
State / Zip Code
FL 32751-6129
Country
United States

Analysis

HISTORY OF FLIGHT

On September 24, 2002, about 1410 eastern daylight time, a Piper PA-32R-301T, N106JG, registered to and operated by D.A. Decision LLC, had a separation of the right wing, outboard left wing, vertical stabilizer, the stabilator, and impacted the ground near Yeehaw Junction, Florida, while maneuvering through thunderstorms. Instrument meteorological conditions prevailed at the time and an instrument flight rules (IFR) flight plan was filed for the 14 CFR Part 91 personal flight. The airplane was destroyed. The private-rated pilot and one passenger were fatally injured. The flight had originated from Lantana, Florida, at 1330, en route to Orlando, Florida.

At 1257:00, the pilot of N106JG contacted the Saint Petersburg Automated Flight Service Station (AFSS), and requested to file an IFR flight plan from Palm Beach County Airport (LNA), Lantana, Florida direct to Executive Airport (ORL), Orlando, Florida and return. The pilot advised his estimated time of departure was 1400 with time en route of 1 hour 10 minutes. In addition, the pilot requested weather along the route of flight. The specialist reported low levels of precipitation between LNA and ORL with the majority of the weather east of Melbourne, Florida up to and including Daytona Beach, Florida. Thunderstorm activity was reported north of Orlando, Florida.

At 1350:30, the pilot of N106JG contacted the Miami Air Route Traffic Control Center (ZMA) Sector 3 Vero Beach Terminal Radar (R3) controller, and reported level at 7,000 feet. Radar data indicated the airplane's target was approximately 30 miles northwest of LNA. The R3 controller acknowledged the transmission and advised, "Vero Beach altimeter is 29.95" (inches of mercury).

At 1350:50, the pilot requested a 10-degree turn to the left for weather. The R3 controller approved the turn and advised the pilot to "proceed direct BAIRN intersection when able." The pilot acknowledged the transmission. Radar data indicated N106JG's radar track turned 10 degrees to the left. Mode C (transponder) was 7,000 feet.

At 1353:52, radar data indicated N106JG's radar target turned to the right and tracked a course heading of 330 degrees consistent with a heading to the BAIRN intersection. Mode C was 6,900 feet.

At 1358:10, the R3 controller announced on the frequency that Convective SIGMET (Significant Meteorological Advisory) 55E, 56E and 57E were in effect until 1555 and further information could be obtained through Flight Watch, HIWAS (Hazardous In-flight Weather Advisory Service), and Flight Service.

At 1408:44, the pilot of N106JG advised he was in "IMC 7" (instrument metrological conditions at 7,000 feet), and requested a descent, which the R3 controller approved to 5,000 feet. Radar data indicated N106JG's Mode C was 7,100 feet. Thirteen seconds later at 1408:57, the pilot responded, "one oh six juliet gulf the gyro is out." The R3 controller asked the pilot to say again and the pilot responded, "Gyro's out one oh six juliet gulf." The R3 controller instructed the pilot to "descend and maintain 5,000 feet." There was no response from the pilot. Radar data indicated the airplane's Mode C was 7,500 feet and then the radar track began a tight right descending turn. The R3 controller made several more attempts to contact the pilot. No further communications were received. The last radar return was received at 1409:40. Mode C was 900 feet. The supervisor initiated Search and Rescue notification.

Radar data showed that between 1408:44 and 1408:57, the airplane ascended 400 feet. Between 1409:04 and 1409:33 the aircraft descended 4,100 feet, and the last radar return at 1409:40, the airplane had descended 1,300 feet.

PERSONNEL INFORMATION

The pilot, held an FAA private pilot certificate, with airplane single engine land, and airplane instrument, last issued on May 5, 2002, when the airplane instrument rating was added. The pilot held an FAA class 3 medical certificate issued on June 24, 2000, with the limitations the "Holder shall wear corrective lenses." The pilot received a biennial flight review, as required by 14 CFR Part 61, on May 9, 2002.

As per the entries in the pilot's personal flight logbook, he had accumulated a total of 397 total flight hours, 377 total single engine flight hours, and 97 hours in this make and model aircraft. In addition, the logbooks showed that he had 24 total night flight hours, 83 simulated instrument flight hours, and 39 actual instrument flight hours.

AIRCRAFT INFORMATION

The airplane was a Piper Aircraft Inc., model PA32R-301T, serial number 32R-8229059, manufactured in 1982. At the time of the accident the airplane and engine had accumulated 2,813.9 total flight hours. The airplane and engine received an annual inspection on March 21, 2002, 38.2 hours before the accident. The airplane was equipped with one Lycoming model TIO-540-S1AD engine, serial number L-8183-61A, six cylinder, air cooled, direct drive, horizontally opposed, turbocharged, fuel injected, internal combustion engine rated at 300 horsepower at 2700 rpm, and had 953.8 hours since field overhaul. The propeller was manufactured by Hartzell, and was a model HC-E3YR-1RF. According to the maintenance records the last static pressure/instrument check was completed on March 21, 2002. The airplane was equipped with a attitude indicator, horizontal situation indicator (HIS), and a lightning detector (Stormscope).

METEOROLOGICAL INFORMATION

The NTSB Meteorological Factual Report revealed that at the time of the radio transmission to ATC that, "the gyro is out," N106JG was penetrating intense to extreme weather echoes VIP 5 to VIP 6 (Video Integrator Processor ...weather intensity); containing thunderstorms. The thunderstorms contained heavy rain, IMC (instrument metrological conditions), up and downdrafts, horizontal gusts, and turbulence of at least moderate intensity. From about 10 minutes before the accident to the accident time, thunderstorms increased in coverage and intensity, moving into the accident area from the south.

Thunderstorms were noted in Convective SIGMET (Significant Meteorological Advisory) 57E and Miami Center Weather Advisory 201. Both advisories were in effect for the time and area of the accident. The Area Forecast issued at 1345 also forecast thunderstorms for an area that included the accident location. The upper air data from Tampa, Florida, located about 77 nautical miles west of the location of the last radar contact, showed that the freezing level was near 16,000 feet.

Lightning data revealed there were 124 cloud to ground lightning strikes recorded in a 15 statute miles radius of the location of the last radar point of N106JG for the time period 1400 to 1415. The closest cloud to ground strikes to the last radar contact occurred at 1409:15.690. The strike was at 154.8 degrees at 3.6 statute miles. A strike at 148.7 degrees at 3.8 statute miles from the last radar contact occurred at 1409:15.629.

The following are sources of weather information that were valid at the time of the accident:

The 0857 Terminal Forecast 9 for Orlando, Florida: wind 110 degrees at 9 knots; visibility greater than 6 statue miles; rain showers; cloud ceiling 2,500 feet scattered, 8,000 feet broken; 1100-1500 expect visibility 3 statute miles; moderate rain showers; cloud ceiling 2,000 feet broken.

The 0857 Area Forecast 10 for Florida: cloud ceiling 3,000 feet scattered to broken, 10,000 feet broken, cloud tops 25,000 feet; scattered to widely scattered thunderstorms, moderate rain showers, thunderstorm tops to 45,000 feet.

Convective SIGMET 55E valid until 1555: Florida and surrounding coastal waters; from 80 miles southeast of Crestview, Florida; 40 miles west of Cross City, Florida; 100 miles southwest of Cross City, Florida; 130 miles southeast of Crestview, Florida; 80 miles southeast of Crestview, Florida an area of embedded thunderstorms moving from 140 degrees at 25 knots; cloud tops reported above 45,000 feet.

Convective SIGMET 56E valid until 1555: Florida, Georgia and surrounding coastal waters; from 10 miles east northeast of Alma, Georgia; 70 miles east northeast of Jacksonville, Florida; 50 miles east northeast of Ormond Beach, Florida; 50 miles west of Jacksonville, Florida; 10 miles east northeast of Alma, Georgia an area of thunderstorms moving from 160 degrees at 15 knots; cloud tops to 42,000 feet.

Convective SIGMET 57E valid until 1555: Florida and coastal waters; from 30 miles east of Orlando, Florida; 10 miles east of Vero Beach, Florida; 50 miles south southeast of Fort Myers, Florida; 30 miles east of Orlando, Florida an area of developing thunderstorms moving from 140 degrees at 25 knots; cloud tops to 44,000 feet.

WRECKAGE AND IMPACT INFORMATION

The aircraft impacted in an open swamp area, south of Yeehaw Junction, Florida, about 2 miles west of state road 441, and the highway 60 intersection. The aircraft came to rest in a stream, on a heading of 215 degrees. A postimpact fire ensued which destroyed the cockpit and cabin area. The accident occurred during the hours of daylight about 27 degrees, 40.606 minutes north, and 080 degrees, 55.950 minutes west.

The engine and airframe were examined at the site of the accident. The main wreckage was destroyed by fire. The complete right wing, tail section and outboard section of the left wing were found distributed along a debris path on a 150 degrees magnetic heading.

The left wing was found separated at the wing root and was located at the accident site, next to the fuselage. An additional separation of the left wing was observed 87 inches outboard of the wing root. The post impact fire had consumed the inboard section of the left wing. The aft spar attachment was found pulled from the fuselage. The nut and bolt remained attached to the attachment bracket. The forward spar attachment remained attached to the fuselage. The flap was separated from the wi...

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA02FA173