Wright-Patterson - Wright Patterson
Flight / Schedule
Wright-Patterson - Wright Patterson
Aircraft
Boeing KC-135 StratotankerRegistration
61-0328
MSN
18235/C13
Year of Manufacture
1961
Operator
United States Air Force - USAFDate
May 6, 1981 at 10:50 AM
Type
CRASHFlight Type
Training
Flight Phase
Flight
Crash Site
Plain, Valley
Crash Location
Walkersville Maryland
Region
North America • United States of America
Coordinates
39.4818°, -77.3508°
Crash Cause
Technical failure
Narrative Report
On May 6, 1981 at 10:50 AM, Wright-Patterson - Wright Patterson experienced a crash involving Boeing KC-135 Stratotanker, operated by United States Air Force - USAF, with the event recorded near Walkersville Maryland.
The flight was categorized as training and the reported phase was flight at a plain, valley crash site.
21 people were known to be on board, 21 fatalities were recorded, 0 survivors were identified or estimated. This corresponds to an estimated fatality rate of 100.0%.
Crew on board: 17, crew fatalities: 17, passengers on board: 4, passenger fatalities: 4, other fatalities: 0.
The listed crash cause is technical failure. On 6 May 1981, EC-135N, Serial Number 61-0328, call sign AGAR 23, departed Wright Patterson AFB, Ohio, at 1005 Eastern Daylight Savings Time (EDT) on a routine training mission. On board the aircraft were 17 crewmembers and four authorized passengers. The flight proceeded uneventfully as planned for approximately 45 minutes. Then in a few brief moments, a sequence of very rapid events resulted in a crash with the loss of all onboard. At 1049:48 EDT, The Federal Aviation Administration (FAA) lost radar contact with AGAR 23. The aircraft was cruising at Flight Level 290, at .78 Mach while performing a navigational training leg. The aircraft commander, Capt Emilio, occupied the right pilot seat and a passenger, Mrs. Emilio, occupied the left pilot seat. Also in the crew compartment were the 2 navigators, Lt Col Frederick and Capt Fonke, and 2 passengers, Mrs. Fonke and SSgt Brundige. For undetermined reasons, the aircraft pitch trim moved to the full nose-down position. The aircraft then a rapidly pitched over, most likely upon release of the autopilot, and induced sufficient negative "G" forces to cause the generators to trip off line, resulting in the loss of all AC electrical power. The pitch trim could not then be moved electrically. This condition, while unusual, can be controlled if prompt corrective action is taken; however, if corrective action is delayed approximately 8 seconds, the aircraft pitch angle will be greater than 30 degrees nose-down in the airspeed in excess of 350 knots indicated airspeed. Under these conditions, the aircraft cannot be controlled until the pitch trim is moved toward neutral. While it is evident that recovery was delayed, the reason for the delay is unknown. The aircraft became uncontrollable and entered a steep descent. During the rapid descent, an explosion occurred at approximately 1300 feet above ground level followed immediately by catastrophic failure, and complete break-up of the aircraft. The wreckage was found north of Walkersville and all 21 occupants were killed.
Aircraft reference details include registration 61-0328, MSN 18235/C13, year of manufacture 1961.
Geospatial coordinates for this crash are approximately 39.4818°, -77.3508°.
Fatalities
Total
21
Crew
17
Passengers
4
Other
0
Crash Summary
On 6 May 1981, EC-135N, Serial Number 61-0328, call sign AGAR 23, departed Wright Patterson AFB, Ohio, at 1005 Eastern Daylight Savings Time (EDT) on a routine training mission. On board the aircraft were 17 crewmembers and four authorized passengers. The flight proceeded uneventfully as planned for approximately 45 minutes. Then in a few brief moments, a sequence of very rapid events resulted in a crash with the loss of all onboard. At 1049:48 EDT, The Federal Aviation Administration (FAA) lost radar contact with AGAR 23. The aircraft was cruising at Flight Level 290, at .78 Mach while performing a navigational training leg. The aircraft commander, Capt Emilio, occupied the right pilot seat and a passenger, Mrs. Emilio, occupied the left pilot seat. Also in the crew compartment were the 2 navigators, Lt Col Frederick and Capt Fonke, and 2 passengers, Mrs. Fonke and SSgt Brundige. For undetermined reasons, the aircraft pitch trim moved to the full nose-down position. The aircraft then a rapidly pitched over, most likely upon release of the autopilot, and induced sufficient negative "G" forces to cause the generators to trip off line, resulting in the loss of all AC electrical power. The pitch trim could not then be moved electrically. This condition, while unusual, can be controlled if prompt corrective action is taken; however, if corrective action is delayed approximately 8 seconds, the aircraft pitch angle will be greater than 30 degrees nose-down in the airspeed in excess of 350 knots indicated airspeed. Under these conditions, the aircraft cannot be controlled until the pitch trim is moved toward neutral. While it is evident that recovery was delayed, the reason for the delay is unknown. The aircraft became uncontrollable and entered a steep descent. During the rapid descent, an explosion occurred at approximately 1300 feet above ground level followed immediately by catastrophic failure, and complete break-up of the aircraft. The wreckage was found north of Walkersville and all 21 occupants were killed.
Cause: Technical failure
Occupants & Outcome
Crew On Board
17
Passengers On Board
4
Estimated Survivors
0
Fatality Rate
100.0%
Known people on board: 21
Operational Details
Schedule / Flight
Wright-Patterson - Wright Patterson
Operator
United States Air Force - USAFFlight Type
Training
Flight Phase
Flight
Crash Site
Plain, Valley
Region / Country
North America • United States of America
