posted on Jan, 19 2023 @ 10:31 PM
The aircraft (85-0089) was undergoing routine maintenance for a problem with the variable exhaust nozzle on the #1 engine. The engine run required a
run to maximum augmenter to verify the nozzle positioning. During the run, the #1 engine catastrophically failed, resulted in severed fuel lines,
resulting in a fire in the #1 engine, that resulted in $15M in damage to the engine, fuselage, and wing area.
The aircraft flew on 20 April, 2022 as SLAM1, completing an approximately 3 hour sortie. They used the augmenter for takeoff, and flew the mission at
approximately 0.75 mach, with a 25 degree wing sweep. Upon landing, they turned the aircraft over to another crew for a hot refuel, and another
sortie, flying as HAWK81. The incoming crew shut down engines #3 and 4, and left #1 and #2 at idle for the refueling. The new crew noticed that the
#1 variable exhaust nozzle indication showed closed, when it should have been in the full open position at idle. Engine specialists checked that the
exhaust nozzle indications in the cockpit were operational, and matched the physical position of the nozzle. The crew was asked to advance the power
on the engine, which resulted in the nozzle moving to the correct position, and returning to the correct position at idle.
As the engine crew was leaving the aircraft, the engine went back to indicating closed. The crew was called back out, and the decision was made to
switch to another aircraft. Upon troubleshooting the aircraft, without the engine running, with a diagnosis of hydraulic filter, and hydraulic pump
servo filter being the cause of the nozzle failure. After installation of the new filters, the T.O. required an augmenter run to ensure the hydraulic
pump operated properly, and didn't leak fluid. The engine crew started engines, following all T.O. procedures, and initiated the augmenter check.
Both ground observers, and cockpit personnel observed the engine nozzle operating correctly, and moving to the proper positions for the power
settings. The augmenter was run for 10 seconds, as instructed by the T.O. before being moved to the idle position.
The maintenance crew performed a second augmenter run, as required, and during this run, as the augmenter lit, there was a fuel flow augmenter flame
detection light, immediately followed by a fireball near the fan section of the engine, that expanded fifty feet out along the wing, and 200 feet into
the air. Pieces of engine and cowling were found as far as 1,000 feet away from the aircraft. The engine run supervisor ordered the other member in
the cockpit, and the ground personnel to evacuate the area, while he shut down the engine, notified the tower, and activated the on board firefighting
equipment. Fire crews arrived on scene and had the fire out within ten minutes.
An examination of the engine maintenance history showed that it had been removed from an aircraft at Ellsworth for a #4 bearing leak, and sent to the
Dyess Centralized Repair Facility in 2021. In January 2022, the engine was installed on the Mishap Aircraft. According to the Digital Engine
Computer, the engine had 320 Total Accumulated Cycles since its last overhaul in 2017. A TAC is the number of times the engine is accelerated and
decelerated. The engine had 3,680 TACs remaining before its next overhaul.
The history of the 2nd Stage Fan Disk was examined back to 1998 when it was first installed into an engine. It underwent all required modifications
and updates as scheduled. In May 2014, the disk was damaged in a FOD ingestion incident. It was repaired according to T.O. requirements and placed
into storage as a spare asset. It underwent a SLEP in 2017 before being installed into the Mishap Engine later that year, as part of the engine SLEP.
The ME served as a spare engine, until it was installed in an aircraft in 2019. The ME had 7448.7 total hours, and 12.2 hours since its last Hourly
Postflight Inspection.
The 2nd Stage Fan Disk was found in three large pieces, and many smaller pieces, with most of the blades damaged. The #1 engine nacelle suffered
extensive fire damage, in addition to the damage caused by the disk exiting the side of the nacelle. The disk was found 564 feet from the aircraft.
The left wing suffered extensive fire damage, with physical buckling near the wing root, above the nacelle.