Sunday, September 09, 2012

TL Ultralight SRO Stingsport TL-2000, N898N: Accident occurred September 01, 2012 in Longmont, Colorado

NTSB Identification: CEN12LA655
14 CFR Part 91: General Aviation
Accident occurred Saturday, September 01, 2012 in Longmont, CO
Probable Cause Approval Date: 04/10/2014
Aircraft: TL ULTRALIGHT SRO STINGSPORT, registration: N898N
Injuries: 2 Uninjured.

NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

While conducting maneuvers at 2,500 feet, the airplane began to vibrate violently. The pilot aborted the maneuver and retarded the throttle to idle; the engine experienced a total loss of power. The pilot executed a forced landing into a field. After the landing, the pilot and the designated pilot examiner noticed that two of the propeller blades had separated from the propeller hub. An examination of the fractured blades and blade sleeves revealed that blade A likely fractured due to progressive cracking at laminate bonds at the interface between the wood blade and the metal sleeve. The powdery wood observed in the slots and at the root end of the blade shank were indicative of rubbing wood as the cracks progressed. The blade B fracture was likely secondary and occurred due to the vibrations associated with the imbalance created by the blade A fracture and subsequent separation. The propeller log indicated that manufacturer-specified visual inspections and torque checks were not conducted at the specified interval of 150 hours but at intervals of about 203, 320, and 250 hours. The delayed visual inspections reduced the likelihood of detecting the cracks and the delayed torque checks might have contributed to crack growth in the blade.

The National Transportation Safety Board determines the probable cause(s) of this accident as follows:
The failure of the wood propeller blades in flight. Contributing to the accident was the owner/operator’s failure to complete required inspections on the propeller within the specified interval, which reduced the likelihood of detecting the cracks and may have contributed to the crack growth. 

HISTORY OF FLIGHT

On September 1, 2012, about 1130 mountain daylight time, a TL Ultralight SRO Stingsport airplane, N898N, conducted a forced landing after two of the propeller blades separated inflight near Longmont, Colorado. The airplane sustained substantial damage. The sport pilot and the designated pilot examiner (DPE) on board were not injured. The aircraft was registered to STING4FUN LLC and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as an instructional flight. Visual meteorological conditions prevailed for the flight, which operated without a flight plan. The flight originated from Erie Municipal Airport (KEIK), Erie, Colorado at 1100. 

The DPE stated that while the pilot was conducting a steep turn demonstration at 2,500 feet above the ground, the engine began vibrating violently. The pilot aborted the maneuver and retarded the throttle to idle when the engine experienced a total loss of power. The pilot made an emergency landing in a nearby field. After the landing, the pilot and DPE noticed that two of the three propeller blades had separated from the propeller hub. The airplane sustained substantial damage to the firewall and engine mount. 

PERSONNEL INFORMATION

The pilot, age 43, held a sport pilot certificate at the time of the accident. He received his private pilot certificate after the conclusion of the accident flight. 

AIRCRAFT INFORMATION

The airplane was a TL Ultralight SRO Stingsport, two-place, high wing, fixed gear, light sport airplane manufactured in 2006. An airworthiness certificate was issued for N889N on March 10, 2006. It was powered by a Bombardier Rotax engine and equipped with a 3 bladed WoodComp wooden propeller. 

Visual inspections of the propeller and propeller hub and bolt torques were checked per the TL Ultralight SRO and WoodComp instructions. The inspections were completed on: August 1, 2009 at a total time of 158.4; August 3, 2009 at a total time of 361.2; August 12, 2010 at a total time of 680.9; and September 1, 2011 at a total time of 924.8. 

According to WoodComp, the propeller inspections were required at 150 hour intervals. 

METEOROLOGICAL INFORMATION 

An automated weather report at Erie, Colorado, 14 miles north of the accident site, was issued at 1134 and reported: wind from 020 degrees and 3 knots, 10 miles visibility, sky clear, temperature 29 degrees Celsius (C), dewpoint 3 degrees C, and pressure 30.12 inches of mercury. 

WRECKAGE AND IMPACT INFORMATION

The airplane came to rest upright in a field. The engine mounts and firewall were bent during the forced landing. The rest of the airplane was otherwise unremarkable. 


TESTS AND RESEARCH

The remaining propeller blade and all three propeller sleeves were examined by the NTSB Materials Laboratory, Washington, DC. Each of the propeller blades and corresponding blades sleeves were labeled A, B, and C for identification purposes. 

Blade A consisted of an entire blade sleeve and a small amount of fractured wood inside the sleeve. A tan powdery substance was noted in the sleeve and in the slots of the sleeve. The substance was tested and matched that of the wood propeller. Progressive cracks were evident in blade A between the blade and the metal sleeve. 

Blade B consisted of an entire blade sleeve and a section of wood which remained attached to the sleeve and also extended out of the sleeve. The blade exhibited cracks in the wood that corresponded to the interface between the blade and the sleeve. 

Blade C consisted of an entire blade sleeve and an entire wood blade and exhibited kinked fibers in the composite layer and crack features at the blade root near the metal sleeve.


http://registry.faa.gov/N898N
 
NTSB Identification: CEN12LA655 
 Nonscheduled 14 CFR Part 91: General Aviation
Accident occurred Saturday, September 01, 2012 in Longmont, CO
Aircraft: TL ULTRALIGHT SRO STINGSPORT, registration: N898N
Injuries: 2 Uninjured.

This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed. NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.

On September 1, 2012, about 1746 mountain daylight time, a TL Ultralight SRO Stingsport TL-2000, N898N, was substantially damaged while maneuvering near Longmont, Colorado. The sport pilot and the designated pilot examiner (DPE) on board were not injured. The aircraft was registered to STING4FUN LLC and operated by the pilot under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, which was operated without a flight plan. The flight originated from Erie Municipal Airport (KEIK), Erie, Colorado at 1700.

The DPE stated that while the pilot was conducting a steep turn demonstration at 2,500 feet above ground level, the engine began vibrating violently. The pilot aborted the maneuver and pulled the throttle back to full idle whereupon the engine quit entirely. The pilot made an emergency landing in a nearby field without further incident. After landing, the pilot and DPE examined the airplane and found two of the three propellers were missing.

The remaining propeller and three propeller sleeves were retained for further examination.

 
IDENTIFICATION
  Regis#: 898N        Make/Model: LSA       Description: STINGSPORT
  Date: 09/01/2012     Time: 1746

  Event Type: Incident   Highest Injury: None     Mid Air: N    Missing: N
  Damage: Unknown

LOCATION
  City: LONGMONT   State: CO   Country: US

DESCRIPTION
  AIRCRAFT ON LANDING, PROP SEPARATED FROM HUB, LONGMONT, CO

INJURY DATA      Total Fatal:   0
                 # Crew:   1     Fat:   0     Ser:   0     Min:   0     Unk:    
                 # Pass:   1     Fat:   0     Ser:   0     Min:   0     Unk:    
                 # Grnd:         Fat:   0     Ser:   0     Min:   0     Unk:    

OTHER DATA
  Activity: Unknown      Phase: Landing      Operation: OTHER

  FAA FSDO: DENVER, CO  (NM03)                    Entry date: 09/04/2012


No comments:

Post a Comment