Crash of a Boeing KC-135A-BN Stratotanker at Dyess AFB: 19 killed

Date & Time: Jan 31, 1989 at 1210 LT
Type of aircraft:
Operator:
Registration:
63-7990
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Dyess - Hickham
MSN:
18607
YOM:
1963
Location:
Crew on board:
7
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
19
Circumstances:
Shortly after liftoff from runway 16 at Dyess AFB, while climbing to a height of about 60-100 feet, the aircraft banked right, causing the right wing to struck the ground. Out of control, the aircraft crashed in a huge explosion and was totally destroyed by impact forces and a post crash fire. All 19 occupants were killed, among them army officer and family members including spouses and children.
Probable cause:
It is believed that vapor was coming out from an engine, maybe due to a technical problem on the water injection system.

Crash of a Boeing KC-135A-BN Stratotanker in Oscoda: 6 killed

Date & Time: Oct 11, 1988 at 1420 LT
Type of aircraft:
Operator:
Registration:
60-0317
Flight Type:
Survivors:
Yes
Schedule:
Oscoda - Oscoda
MSN:
18092
YOM:
1960
Crew on board:
6
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
Following a steep approach at Oscoda-Wurtsmith Airport in crosswind conditions, the four engine aircraft landed hard. Upon landing, it went out of control, veered off runway and came to rest, bursting into flames. Six crew members were killed while 10 others were injured. The aircraft was destroyed by a post crash fire.

Crash of a Boeing KC-135A-BN Stratotanker at Fairchild AFB: 7 killed

Date & Time: Mar 13, 1987 at 1320 LT
Type of aircraft:
Operator:
Registration:
60-0361
Flight Type:
Survivors:
No
Schedule:
Fairchild AFB - Fairchild AFB
MSN:
18136
YOM:
1961
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Aircraft flight hours:
10956
Circumstances:
At 1:20 p.m. on Friday, March 13, 1987, a B-52 Stratofortress and a KC-135 Stratotanker took off from Fairchild Air Force Base (AFB) to practice aerial maneuvers for a 15-minute air show scheduled on Sunday, May 17, Fairchild's annual Aerospace Day. The show was to be the debut of a new aerobatics team dubbed the Thunderhawks, the brainchild of General John T. Chain Jr., commander-in-chief of the Strategic Air Command (SAC). Its purpose was to demonstrate the capabilities of SAC’s large aircraft through a series exciting routines that included a low-level refueling simulation, high-bank turns, and flybys down the runway. Colonel Thomas J. Harris, commander of the 92nd Bombardment Wing at Fairchild AFB had been assigned the responsibility for the Thunderhawks’ creation and development in December 1986. The KC-135A-BN Stratotanker, No. 60-0361, had three instructor pilots aboard the aircraft: Lieutenant Colonel Michael W. Cornett, Captain Christopher Chapman, and Captain Frank B. Johnson. But no one on the ground at Fairchild knew who was actually in command of the aircraft when it took off. Also on board plane were two navigators, Captain James W. Litzinger and First Lieutenant Mark L. Meyers, and refueling-boom operator, Staff Sergeant Rodney S. Erks. The KC-135 had just taken off from runway 23, in tandem with the B-52, and was executing a steep left-hand turn when it suddenly rolled from an intended 45-degree bank to almost 90 degrees, stalling the two engines on the left wing. The crew managed to level the aircraft, but it was flying too low and slow to recover. The plane crashed landed in an open area north of the flightline, behind three large hangars, narrowly missing the base’s bombing and refueling squadron offices. It skidded through a security fence, across an access road, and killed Senior Master Sergeant Paul W. Hamilton, a member of the Thunderhawks on his day-off from flying, who was sitting in his car watching. The aircraft traveled for another 200 yards, then hit an unmanned weather radar tower and burst into flames. During the journey, the tail section separated from the fuselage as well as the wings, engines, and wheels. One wing, ripped off by the collision with the radar tower, landed 50 yards beyond the burning wreckage. Within minutes, Fairchild’s crash teams were on scene, fighting the fire caused by spilled jet fuel. Spokane International Airport, four miles east of the base, dispatched a crash truck and the Spokane Fire Department mobilized an entire engine company to assist in battling the blaze. Because of the toxic fumes and dangerous flare-ups, reporters and photographers were not permitted near the scene. It took firefighters more than three hours to extinguish the flames and hot-spots from the crash. Searchers found the bodies of five crewmen in the forward section of the blackened fuselage. The body of the sixth crew member was finally found late Friday night, tangled inside the cockpit wreckage. It wasn’t discovered immediately because the recovery teams were being careful to safeguard the crew compartment for the Air Force accident investigators.
Those killed were:
Cpt Christophe L. Chapman, pilot,
Lt Col Michael W. Cornett, pilot,
S/Sgt Rodney Scott Erks, refueling-boom operator,
SM/Sgt Paul W. Hamilton, refueling-boom operator,
Cpt Frank B. Johnson, pilot,
Cpt James W. Litzinger, navigator,
1st Lt Mark L. Myers, navigator.
Source: Daryl C. McClary via https://www.historylink.org/File/8871
Probable cause:
Loss of control caused by wake turbulences.

Crash of a Boeing KC-135A-BN Stratotanker at Altus AFB

Date & Time: Feb 13, 1987
Type of aircraft:
Operator:
Registration:
60-0330
Flight Type:
Survivors:
Yes
Schedule:
Altus AFB - Altus AFB
MSN:
18105
YOM:
1961
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
10305
Circumstances:
The crew was performing a local training mission at Altus AFB. After landing, smoke spread in the cockpit and a fire erupted. The crew immediately stopped the aircraft and the runway and evacuated the cabin safely. There were no injuries while the aircraft was totally destroyed by fire.
Probable cause:
It was determined that UHF cables which runs near the aft wing root in the fuselage were melted due to an electrical fault. Fuel vapors in the area of the aft body tank ignited.

Crash of a Boeing KC-135A-BN at Howard AFB: 4 killed

Date & Time: Jun 17, 1986
Type of aircraft:
Operator:
Registration:
63-7983
Flight Type:
Survivors:
No
Schedule:
Grissom - Howard
MSN:
18600
YOM:
1963
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Aircraft flight hours:
8041
Circumstances:
For unknown reasons, the four engine aircraft landed hard and bounced. It became airborne again and went out of control before crashing onto a hill. All four crew members were killed.

Crash of a Boeing KC-135A-BN Stratotanker at Beale AFB: 7 killed

Date & Time: Aug 27, 1985
Type of aircraft:
Operator:
Registration:
59-1443
Flight Type:
Survivors:
No
Schedule:
Beale - Beale
MSN:
17931
YOM:
1960
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Aircraft flight hours:
9936
Circumstances:
The crew was dispatched at Beale AFB to follow a training program. Following several touch-and-go maneuvers, the crew started a new approach when the aircraft became unstable on final. The instructor allowed the pilot-in-command to continue the approach when the engine n°1 struck the runway surface, caught fire and exploded. Out of control, the airplane banked left and crashed, bursting into flames. All seven crew members were killed.

Crash of a Boeing RC-135T near Valdez: 3 killed

Date & Time: Feb 25, 1985
Type of aircraft:
Operator:
Registration:
55-3121
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Eielson - Valdez - Eielson
MSN:
17237
YOM:
1957
Flight number:
Mary 24
Location:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Aircraft flight hours:
15072
Circumstances:
The crew departed Eielson AFB southeast of Fairbanks on a training mission in the region of Valdez under callsign Mary 24. Following two successful approaches under MLS procedure, the crew started a third approach about four miles north of the prescribed MLS inbound course. While descending too low in poor visibility, the aircraft struck the slope of a mountain and crashed. SAR operations were initiated but eventually abandoned few days later as no trace of the aircraft nor the three occupants was found. The wreckage was recovered by walkers on August 2, 1985.
Probable cause:
It was reported that the crew had used an approach procedure certified for de Havilland Canada DHC-7, a STOL airplane. The glide slope and missed approach for this airplane are significantly steeper than those for an RC-135 jet.

Crash of a Boeing KC-135A-BN Stratotanker in Greenwood: 27 killed

Date & Time: Mar 19, 1982 at 2110 LT
Type of aircraft:
Operator:
Registration:
58-0031
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sawyer - Chicago
MSN:
17776/246
YOM:
1959
Crew on board:
4
Crew fatalities:
Pax on board:
23
Pax fatalities:
Other fatalities:
Total fatalities:
27
Aircraft flight hours:
9249
Circumstances:
The four engine airplane departed Kenneth Ingalls Sawyer AFB on a flight to Chicago-O'Hare Airport, carrying 23 passengers and a crew of four. After being cleared to descend from 22,000 feet to 8,000 feet, the crew reduced his speed when at an altitude of 13,700 feet, at a speed of 313 knots, the airplane suffered an in-flight explosion. Both wings detached, all four engines separated as well as the stabs and out of control, the airplane dove into the ground and crashed in an open field located in Greenwood, about 37 miles northwest of Chicago Airport. The aircraft was totally destroyed and all 27 occupants were killed.
Probable cause:
The exact cause of the accident could not be determined with certainty. Considered as 'most probable' was an over-pressurization under the cargo floor, an area that houses fuel and other potential sources of ignition. An explosion caused by the ignition of accumulated combustible vapors occurring in that area could, in fact, rapidly propagate to adjacent areas where fuel is present. There was also 'strong evidence' of explosive over-pressures in the forward, aft and upper fuel tank areas. Significantly, investigation showed that were the walls or fittings of the rubber bladder cells containing the volatile liquid to fail, fuel or vapor could be released into the tank cavity and in turn migrate to other part of the aircraft.

Crash of a Boeing KC-135A-BN Stratotanker near Luke AFB: 4 killed

Date & Time: Mar 13, 1982 at 1050 LT
Type of aircraft:
Operator:
Registration:
57-1489
Flight Type:
Survivors:
No
Schedule:
Phoenix - Luke AFB
MSN:
17560/169
YOM:
1958
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
3604
Captain / Total hours on type:
370.00
Aircraft flight hours:
10650
Circumstances:
The KC-135A aircraft departed Phoenix-Sky Harbor International Airport at 0755 MST for a scheduled 3-hour and 30-minute flight. After completing the navigation leg, the aircraft descended into the Phoenix area for transition at Luke AFB. After completing one TACAN approach at Luke AFB, the KC-135A aircraft was vectored to Phoenix-Sky Harbor International Airport for an ILS touch-and-go landing. The aircraft was then vectored back to the final approach course for a TACAN runway 03 left approach at Luke AFB. The KC-135A aircraft was cleared for the approach to Luke AFB, and after the final approach fix radio call, a midair collision occurred with a Grumman American Yankee civilian aircraft. The empennage of the KC-135A separated, rendering the aircraft incapable of flight and it was destroyed upon ground impact. The Grumman American Yankee aircraft was destroyed during the midair collision. The four crew members in the KC-135A and the two civilians in the Grumman American Yankee were fatalities.
Crew:
LT Col James N. Floor,
Lt Col Ted L. Beam,
Maj Truman R. Young Jr.,
T/Sgt Donald J. Plough.
Probable cause:
The USAF KC-135 was on an IFR flight plan and executing a TACAN 03L approach to Luke AFB. The AA-1 had departed Sky Harbour Airport and had been released by phoenix TRSA. The AA-1 was heading westerly in airspace designated as a special traffic area and was required to have been at or below 2,000 ft msl. A pilot of another aircraft who was trailing the AA-1 stated that a low broken cloud cover was encountered and he had to descend to about 2,000 ft to remain 500 ft below the bases. He stated the pilot of the AA-1 did not descend but appeared to be skimming along in and out of the bases of the clouds. He noticed the KC-135 descending through the cloud deck followed immediately by the collision. The collision occurred about 5 mi south of Luke AFB at an altitude of 2,500 ft msl. The logbook of the AA-1 pilot indicated this was his first trip to the phoenix area. Luke AFB was depicted on the north side of the sectional chart only. VOR airway #16 was split along an e-w line with the northern and southern halves being depicted on each side of the chart.

Occurrence #1: midair collision
Phase of operation: cruise - normal
Findings
1. En route charts - inadequate
2. (c) vfr procedures - improper - pilot in command AA-1
3. (f) lack of familiarity with geographic area - pilot in command AA-1
Final Report:

Crash of a Boeing EC-135N in Walkersville: 21 killed

Date & Time: May 6, 1981 at 1050 LT
Type of aircraft:
Operator:
Registration:
61-0328
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Wright-Patterson - Wright Patterson
MSN:
18235/C13
YOM:
1961
Flight number:
AGAR23
Crew on board:
17
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
21
Aircraft flight hours:
13471
Circumstances:
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.
Probable cause:
At 1049:48 EDT, FAA lost radar contact with the aircraft. The aircraft was cruising at flight level 290 at .78 Mach and was performing a navigational training leg. Navigational legs are normally flown on autopilot, and FAA altitude readouts showed the aircraft was within 100 feet of assigned altitude, characteristic of autopilot flight. The aircraft commander, Capt Joseph Emilio, occupied the right pilot seat and a passenger, Mrs. Peggy Emilio, occupied the left pilot seat. Also in the crew compartment were the 2 navigators, Lt Col Benjamin B. Frederick and Capt Donald V. Fonke, and 2 passengers, Mrs. Linda Fonke and SSgt Joseph T. Brundige. This phase of flight, the navigational leg, was the least demanding on the pilot and was the logical time for the passengers to come forward to view the cockpit area. There is no evidence that the presence of the passengers in the crew compartment contributed to, or caused, the accident. For undetermined reasons, the aircraft pitch trim moved to the full nose-down position. The autopilot can overcome the trim until near full nose-down. The aircraft then rapidly pitched over, most likely upon release of the autopilot, and induced sufficient negative "G" forces to cause the generators to trip off line and loss of all AC electrical power. The pitch trim could not then be moved electrically. This condition, while unusual, can be easily 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° nose-down in the airspeed in excess of 350 KIAS. Under these conditions, the aircraft cannot be controlled until the pitch trim is moved toward neutral. While it is clear that recovery was delayed, the reason for the delay is unknown. The aircraft became uncontrollable and entered a steep descent. The aircraft emerged from the clouds at 2,000 feet above ground level (AGL) and was intact. Airspeed was in excess of 400 KTAS and die to angle was 20 to 30 degrees. Engine power was above 2.0 engine pressure ratio (EPR). At approximately 1,500 feet mean sea level (MSL) an explosion occurred inside the pressurized compartment of the fuselage and weakened the aircraft structure to the extent that catastrophic failure of the aircraft followed immediately. Cause of this explosion is undetermined; however, the aircraft was in an unrecoverable condition at the time of the explosion and a crash was already inevitable.