A-10s over Kosovo (illustrations removed)

Our two-ship was the third A-10 flight to launch that morning. We monitored the common VHF radio frequency and could hear the members of other flights describe the weather they were experiencing. Those descriptions became the best forecast of what lay ahead of us. The weather had become a real problem. Passing 6,000 feet, I noticed that ice had formed on the nose of the Maverick missiles, the rocket pods, and the leading edge of the wings. I told Buster, and he acknowledged having the same problem. We continued to climb in an attempt to find an altitude where the icing would stop, but it only seemed to get worse until we passed 17,000 feet. The A-10 flights ahead of us had also reported icing, and all aircraft were still in the weather when they leveled off at 25,000 feet, our final altitude for the track down south. Fortunately, a flight of two F-16s, which had taken off behind us and had climbed steeper and flown above us on departure, had just broken out at 30,000 feet and said that the weather above was clear. We decided to continue our climb to find clear weather and help the ice sublime. Unfortunately, our Hogs were loaded for combat with four Mk-82 bombs, two Maverick missiles, two rocket pods, an ALQ-131 jamming pod, and two AIM-9 missiles. That load made us extremely heavy, increased our drag, and precluded a quick climb.

We remained in the weather during our climb and flight down the Adriatic. After about 45 minutes, we finally reached 30,000 feet and could see sunlight above us. Leveling off approximately two miles in trail behind Buster, I was still in the weather and unable to see him. While doing an ops check to see how much fuel was remaining, I saw the master caution light begin to flash and looked to investigate. The right-generator caution light was illuminated, and the number-two (right) engine tachometer was wildly fluctuating between 30 and 90 percent. At this point, I was flying the aircraft about five degrees nose high to maintain level flight at 170 knots indicated airspeed (KIAS).

I immediately radioed Buster to let him know I had a problem and pulled the throttle back on number two in an attempt to recover the engine. When I moved the throttle, the engine immediately spooled back and flamed out. The right engine nacelle now generated drag rather than thrust. That and the combination of high altitude, low airspeed, and a dirty configuration caused the aircraft to yaw right and begin a descent. I immediately pushed the nose five to 10 degrees nose low, attempting to gain airspeed. As the aircraft yawed to the right, a chopped tone came over the headset indicating a stalled condition, which was immediately followed by a loud pop and buzzing sound as the number-one (left) engine compressor stalled. Things were getting serious in a hurry. I tried to stay calm and inform Buster what was happening.

While making the radio call, I saw the main attitude direction indicator (ADI) freeze in the centered position, both steering bars came into view, and all my caution-warning lights illuminated—and the bottom dropped out of my stomach. Those indications told me that I had lost all alternating current (AC) electrical power and that the aircraft had just reverted to direct current (DC) battery power. Not wanting to believe what I saw, I looked at the number-one engine as it rolled back below 30 percent, approximately 12 percent below what was needed for the generators to provide the much-needed AC electrical power. With virtually no thrust, the aircraft began to descend rapidly into the weather, and I soon lost what little sunlight I had been able to see through the clouds. I knew that the only way to clear a compressor stall was to completely shut down the engine, but the idea was still not one I wanted to entertain.

I then checked the DC-powered standby ADI, which showed the aircraft 15 degrees nose high and 20 degrees of right bank—the same attitude it indicated when I had leveled off. My confidence in this old piece of equipment was shot. With the main attitude indicator frozen, the standby attitude indicator unreliable, and no visual references due to the weather, I was forced to use the “needle and ball” of the turn-and-slip indicator to keep the aircraft in coordinated flight. My voice jumped about 10 octaves as I tried to tell Buster that I had just experienced a “double-engine flameout.”

This situation calls for a “boldface emergency procedure.” I had long ago been required to commit to memory the steps I now needed to take—but I had never dreamed of actually using them. My initial A-10 training instructor had even made jokes about this emergency, swearing it could never happen in the A-10 because the engines were too reliable. Some guys in the squadron even joked in our monthly emergency-procedures training that if it ever happened they would just jump out using the ejection procedure. With that in mind, I had to decide and act in a hurry.