N636TM

Substantial
Minor

RAYTHEON AIRCRAFT COMPANY G36S/N: E-3746

Summary

On August 20, 2014, a Raytheon Aircraft Company G36 (N636TM) was involved in an accident near Milton, FL. The accident resulted in 2 minor injuries, with 3 people uninjured out of 5 aboard. The aircraft sustained substantial damage.

The National Transportation Safety Board determined the probable cause of this accident to be: The pilot's inadequate preflight planning, which resulted in an attempted takeoff over the airplane's maximum gross weight and beyond its aft center of gravity limit. Contributing to the accident was the pilot's lack of total flight experience in the aircraft make and model.

The pilot attempted the takeoff with the airplane loaded 238 pounds over the maximum gross weight of 3,833 pounds, with the center of gravity (cg) 3.3 inches aft of the aft cg limit. During the takeoff roll, the nose of the airplane lifted 10 knots prior to the recommended rotation speed for a no-flap takeoff, and witnesses described the airplane in an unstable "pitch-up" attitude before it settled back on the runway and overran the departure end, struck a ditch, and came to rest with substantial damage to the left wing and horizontal stabilizer. The pilot reported he had 1.8 hours of flight experience in the accident airplane make and model, and that there were no mechanical malfunctions with the airplane that would have precluded normal operation.

This accident is documented in NTSB report ERA14CA397. AviatorDB cross-references NTSB investigation data with FAA registry records to provide comprehensive safety information for aircraft N636TM.

Accident Details

Date
Wednesday, August 20, 2014
NTSB Number
ERA14CA397
Location
Milton, FL
Event ID
20140820X02638
Coordinates
30.635833, -86.989440
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
2
Uninjured
3
Total Aboard
5

Probable Cause and Findings

The pilot's inadequate preflight planning, which resulted in an attempted takeoff over the airplane's maximum gross weight and beyond its aft center of gravity limit. Contributing to the accident was the pilot's lack of total flight experience in the aircraft make and model.

Aircraft Information

Registration
Make
RAYTHEON AIRCRAFT COMPANY
Serial Number
E-3746
Engine Type
Reciprocating
Model / ICAO
G36M360
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
2ND PACKAGING DR
Status
Deregistered
City
WEYERS CAVE
State / Zip Code
VA 24486
Country
United States

Analysis

The pilot attempted the takeoff with the airplane loaded 238 pounds over the maximum gross weight of 3,833 pounds, with the center of gravity (cg) 3.3 inches aft of the aft cg limit. During the takeoff roll, the nose of the airplane lifted 10 knots prior to the recommended rotation speed for a no-flap takeoff, and witnesses described the airplane in an unstable "pitch-up" attitude before it settled back on the runway and overran the departure end, struck a ditch, and came to rest with substantial damage to the left wing and horizontal stabilizer. The pilot reported he had 1.8 hours of flight experience in the accident airplane make and model, and that there were no mechanical malfunctions with the airplane that would have precluded normal operation.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA14CA397