FLIGHT FINDINGSAVIATION OCCURRENCE MAP
Back to map

1991 Gulf War Boeing KC-135 accident

6 Feb 1991 · Near Jeddah, Saudi Arabia

United States Air Force Boeing KC-135E Stratotanker · Dual engine separation due to wake turbulence; subsequent emergency landing

From King Abdulaziz International Airport (JED) to King Abdulaziz International Airport (JED)

Report a problem

Event

Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
Event fatalities
0 · all aircraft and ground
Ground fatalities
Unknown
Occupants
4
Survivors
4
InjuriesFatal: death within 30 days. Serious: over 48 hours in hospital within a week, most broken bones, severe bleeding, nerve or organ damage, or serious burns. Minor: anything less. Glossary
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
Military

Boeing KC-135E Stratotanker

Aircraft type
Boeing KC-135
Category
Airplane · from aircraft type
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
58-0013
Onboard fatalities
0
Route
From King Abdulaziz International Airport (JED)To King Abdulaziz International Airport (JED)

Approximate · Estimated position: Jeddah, near the place the Wikipedia article names. Not the accident site.

From the Wikipedia article

On 6 February 1991, a Boeing KC-135 of the United States Air Force (USAF) operated by the 190th Air Refueling Wing took off from Prince Abdullah Air Base, Jeddah, Saudi Arabia, en route to a Gulf War refueling mission. The aircraft carried a crew of four. While in-flight, the aircraft lost engines one and two, both left-wing engines, while flying over the Saudi Arabian desert. To counteract the plane's descent, the pilots began dumping fuel. During the landing in Jeddah, due to the damage of the engine's hydraulic system, most of the descent was performed without autopilot. The aircraft landed safely at Jeddah.

Accident

WHALE 05 was scheduled for take off from Jeddah at 17:24 local time and climbed to 25,000 feet (7,600 m) to perform an aerial refueling. Another Boeing KC-135 took off at around the same time and was supposed to fly the same route. The co-pilot of the second aircraft ascended to the planned altitude of 25,000 feet (7,600 m). After reaching the target altitude, autopilot was engaged with the aircraft about one nautical mile behind the other KC-135.

Approximately 45 minutes after takeoff, WHALE 05 encountered forward wake turbulence and suddenly banked more than 110 degrees to the left, and within a few seconds it banked more than 110 degrees to the right. The captain activated the speed brakes and restored the aircraft to a near level attitude. During the sequence of events, both left wing engines detached from the aircraft. After recovery, fire alarms on the two left side engines activated. The captain ordered the boom operator to look at the engines, who reported that there was no fire but that the engines were physically gone. As the aircraft had only been airborne for a short time, it still held almost 31,000 gallons of fuel. In addition, the hydraulic reception, fuel pumps, and landing gear were damaged when the engines detached, and fuel was spilling from the left wing.

To maintain altitude and the speed of fuel discharge, the captain declared "Mayday" and decided to return to Jeddah. The aircraft returned to level flight at 16,000 feet (4,900 m). The aircraft arrived at Prince Abdullah Air Base an hour and fifteen minutes later. Since the hydraulic system had been damaged, the landing gear was deployed manually. The pilots requested to land on runway 34L because it was the longest runway and had an instrument landing system (ILS) approach. During the landing, the pilot deployed the thrust reverser on the number three engine, but immediately discontinued its use due to difficulty in directional control. Although several tires were damaged, the aircraft came to a stop at about 300 m (1,000 ft) from the end of the runway. The entire crew of WHALE 05 were awarded the Distinguished Flying Cross.

Text from the Wikipedia article “1991 Gulf War Boeing KC-135 accident” (revision 1370704206, retrieved 2026-09-18) by its authors, under CC BY-SA 4.0. Extracted as plain text: references, tables, images and some sections are left out. Read the article

Sources

Wikipedia article: 1991 Gulf War Boeing KC-135 accident
Article
1991 Gulf War Boeing KC-135 accident
Revision
1370704206 · 2026-08-22 · retrieved 2026-09-18
Wikidata
Q108056567
Licence
Text CC BY-SA 4.0, by the article's authors; Wikidata CC0; town positions GeoNames (CC BY 4.0)
Where each value comes from
Record
Wikipedia article "1991 Gulf War Boeing KC-135 accident" (page 78884904, revision 1370704206)
Date
Wikipedia infobox: date
Place and country
Wikipedia infobox: site
Map position
place the Wikipedia infobox site links (Wikidata coordinates)
Aircraft, operator and route
Wikipedia infobox: aircraft type, registration, operator, origin and destination; route airports from the linked airport articles' Wikidata codes (OurAirports)
Operation
operator named as an armed force or military unit in the infobox
Fatalities
Wikipedia infobox: aircraft fatalities
Ground fatalities
not stated in the Wikipedia infobox
Summary
Wikipedia infobox: summary
Source notes (1)
  • Wikipedia · Facts from the Wikipedia article's infobox and coordinates, not checked against an investigation report. Independent review pending.