Double Eagle II Airport
Aircraft Accident/Incident Report

Albuquerque, New Mexico 87121
Saturday, March 10, 2007 15:58 MST

NTSB Narrative Summary Released at Completion of Accident

The company's chief pilot and student instructor had performed four successful touch-and-go landings. On the mishap landing, the student instructor started his flare at normal approach speed about 2 to 3 feet above the runway. As the airplane settled, the chief pilot raised the nose of the airplane slightly to prevent a bounced landing. The airplane subsequently ballooned. They elected to perform a go-around. The chief pilot advanced the power and "pitched the airplane to the landing attitude." The airplane settled to the runway in a slight left crab, touching down on the left main landing gear, which subsequently broke aft. The airplane came down on the runway and slid for 300 feet, departing the left side and flipping over onto its back. The airplane had been recently purchased by the company. Total airframe time was approximately 25 hours. An examination of the airplane showed the left main lower landing gear tube had fractured due to overstress at the landing gear wheel and brake attachment fitting. The overstress appeared consistent with a hard landing impact as a small compression buckle was observed at the top of the part and some tensile indications were seen at the bottom. There were also contact impressions on the inside of the tube most-likely made by the end of the main landing gear spring bar. The wheel and brake attachment fitting was identified as a steel with designation St37, according to the German DIN classification for steels. The St37 steel is specified to have a yield strength of at least 34 ksi (235 MPa) and tensile strength between 51 ksi and 70 ksi (350 MPa to 480 MPa). According to the ASM Metals Handbook, St37 is similar to SAE 1013 steel, which is a low-carbon steel. Hardness measurements on the fitting averaged 63.5 Rockwell B, with a standard deviation of 2 Rockwell B. For steel, a hardness of 65 Rockwell B corresponds to a tensile strength of 56 ksi, so the fitting appears to be within specification. This steel is at the lower end of the range of strength possible for steel. The ASM Metals Handbook indicates that fatigue resistance would also improve with increasing tensile strength. Information from the manufacturer indicates that the gear assembly was designed in accordance with ASTM F 2245, and successfully passed a drop test of 550 mm (21.7 inches) at a weight of 600 kg (1323 pounds). **This narrative was modified on August 13, 2007.**

NTSB Probable Cause Narrative

The total failure of the left main landing gear strut due to overload during the landing resulting in the loss of control and subsequent nose over. A factor contributing to the accident was the chief pilot 's inability to maintain directional control of the airplane after the landing gear failed. **This report was modified on August 13, 2007.**

Event Information

Type of Event Accident
Event Date 3/10/2007
Event Day of the Week Saturday
Time of Event 1558
Event Time Zone Mountain Standard Time
Event City Albuquerque
Event State NEW MEXICO
Event Country --
Zipcode of the event site 87121
Event Date Year 2007
Event Date Month 3
MidAir Collision Indicator No
On Ground Collision occurred ? No
Event Location Latitude 350843N
Event Location Longitude 1064743W
Event Location Airport Double Eagle II Airport
Event Location Nearest Airport ID AEG
Indicates whether the acc/inc occurred off or on an airport On Airport
Distance from airport in statute miles 0.5
Degrees magnetic from airport --
Airport Elevation 5837
Weather Briefing Completeness --
Investigator's weather source Weather Observation Facility
Time of the weather observation 1550 Mountain Standard Time
Direction of event from weather observation facility (degrees) 270
Weather Observation Facility ID AEG
Elevation of weather observation facility 5837
Distance of event from weather observation facility (units?) 1
Time Zone of the weather observation MST
Lighting Conditions Day
Lowest Ceiling Height --
Lowest Non-Ceiling Height 110
Sky/Lowest/Cloud Conditions Few
Sky Condition for Lowest Ceiling None
Visibility Runway Visual Range (Feet) --
Visibility Runway Visual Value (Statute Miles) --
Visibility (Statute Miles) 10
Air Temperature at event time (in degrees celsius) 17
Dew Point at event time (in degress fahrenheit) -8
Wind Direction (degrees magnetic) 0
Variable Wind Indicator Wind direction could be determined
Wind Speed (knots) --
Wind Velocity Indicator Calm
Wind Gust Indicator Not Gusting
Wind Gust (knots) --
Altimeter Setting at event time (in. Hg) 30.05
Density Altitude (feet) --
Intensity of Precipitation --
METAR weather report --
Event Highest Injury Minor
On Ground, Fatal Injuries --
On Ground, Minor Injuries --
On Ground, Serious Injuries --
Injury Total Fatal --
Injury Total Minor 2
Injury Total None --
Injury Total Serious --
Injury Total All 2
Investigating Agency NTSB
NTSB Docket Number (internal use) 21780
NTSB Notification Source FAA-Southwest Region
NTSB Notification Date Mar 10 2007 12:00AM
NTSB Notification Time --
Fiche Number and/or location -used to find docket information DMS
Date of most recent change to record Jul 25 2007 12:22PM
User who most recently changed record NTSB\lema
Basic weather conditions Visual Meteorological Cond
FAA District Office Albuquerque, NM FSDO

Aircraft Involved

Aircraft #1

Aircraft Registration Number N102RK
NTSB Number DEN07FA068
Missing Aircraft Indicator --
Federal Aviation Reg. Part Part 91: General Aviation
Type of Flight Plan filed None
Flight plan Was Activated? --
Damage Substantial
Aircraft Fire None
Aircraft Explosion None
Aircraft Manufacturer's Full Name Flight Design USA
Aircraft Model CT-SW
Aircraft Series Identifier --
Aircraft Serial Number 06-11-15
Certified Max Gross Weight 1320
Aircraft Category Airplane
Aircraft Registration Class --
Aircraft is a homebuilt? No
Flight Crew Seats --
Cabin Crew Seats --
Passenger Seats --
Total number of seats on the aircraft 2
Number of Engines 1
Fixed gear or retractable gear Fixed
Aircraft, Type of Last Inspection Annual
Date of Last Inspection Feb 1 2007 12:00AM
Airframe hours since last inspection 1
Airframe Hours 25
ELT Installed Yes
ELT Activated Yes
ELT Aided Location of Event Site No
ELT Type --
Aircraft Owner Name RK Aviation, Inc.
Aircraft Owner Street Address --
Aircraft Owner City Albuquerque
Aircraft Owner State NM
Aircraft Owner Country USA
Aircraft Owner Zipcode 87121
Operator is an individual? No
Operator Name Bode Aviation, Inc.
Operator Same as Owner? No
Operator Is Doing Business As --
Operator Address Same as Owner? No
Operator Street Address 7401 Paseo del Volcan, NW
Operator City Albuquerque
Operator State NM
Operator Country USA
Operator Zip code 87121
Operator Code --
Owner has at least one certificate None
Other Operator of large aircraft? --
Certified for Part 133 or 137 Operation --
Operator Certificate Number --
Indicates whether an air carrier operation was scheduled or not --
Indicates Domestic or International Flight --
Operator carrying Pax/Cargo/Mail --
Type of Flying (Per_Bus / Primary) Instructional
Second Pilot on Board Yes
Departure Point Same as Event Yes
Departure Airport Code AEG
Departure City Albuquerque
Departure State NM
Departure Country USA
Departure Time 1500
Departure Time Zone MST
Destination Same as Local Flt dest & departure same, accident can occur anywhere
Destination Airport Code --
Destination City --
Destination State --
Destination Country --
Specific Phase of Flight Landing - aborted
Report sent to ICAO? --
Evacuation occurred --
Date of most recent change to record Jun 19 2007 11:19AM
User who most recently changed record BOWL
Since inspection or accident Time of Accident
Event Location Runway Number and Location 22
Runway Length 7400
Runway Width 100
Sight Seeing flight No
Air Medical Flight No
Medical Flight --