Technical Case Study: In-Flight Reduction Gear Box (RGB) Failure and Metal Contamination

Powerplant Featured Case Medium Level Published Jun 12, 2026
Technical Case Visual

Case Description

During a routine flight, the crew observed a sudden drop in the Reduction Gear Assembly (RGB) oil pressure, indicated by the "G" needle on the cockpit's dual pressure indicator
. The pilot performed an emergency engine shutdown and feathered the propeller to prevent the airflow from windmilling the engine, which could have led to a catastrophic mechanical breakup
. Upon landing, technicians performed a resistance check on the RGB magnetic plugs (magplugs) located in the front case and found a significant drop in resistance, indicating the presence of conductive debris
. A subsequent visual inspection of the magplugs revealed large pieces of metal, confirming a severe internal failure of the RGA gear train or bearings (such as the pinion, main drive, or planetary gears) [126, 127, 128, Conversation History]. Due to the high risk of cross-contamination through the common return oil lines, the decision was made to perform a Quick Engine Change (QEC) and send the power plant to the shop for a major teardown and RGA replacemen
Required Tools

Ohmmeter: Required to perform the initial electrical resistance check on the magnetic plugs before removal
.
Standard Mechanic’s Hand Tools: For the removal of access panels and magplug units.
QEC Hoist and Engine Stand: Necessary for the removal of the contaminated engine and installation of the serviceable unit
.
Oil System Flushing Rig: Used to clean the 20-gallon oil tank, oil cooler, and nacelle lines to ensure no residual metal remains in the system
.
Torque Wrench: Required for the precision re-rigging of throttle and condition lever linkages

Safety Protocol

Propeller Feathering: Ensure the propeller is fully feathered during shutdown to eliminate the rotational forces that generate further internal heat and debris
.
Burn Hazards: Use caution when removing magplugs or draining oil immediately after flight, as the scavenge oil can reach temperatures up to 82°C
.
Hazardous Materials: Handle metal-contaminated oil as a hazardous material; avoid skin contact with the oil (MIL-L-23699) and metal "chips" which may be sharp
.
Safetying: All turnbuckles and critical fluid connections must be properly safetied with clips or wire during the QEC installation to prevent loosening due to vibration
.
System Isolation: Ensure the fire shutoff valves are closed during engine removal to prevent accidental fuel or oil spills

Lessons Learned

Indication Monitoring: The ability to differentiate between Gearbox (G) and Engine (E) oil pressure is critical; an RGA failure requires an immediate shutdown, whereas a power section fluctuation might follow different emergency procedures
.
Early Detection Value: The magplug's ability to provide a resistance check allows for a "no-disassembly" diagnosis of internal failure, saving time and preventing further engine runs that would increase contamination
.
Contamination Control: In a dry-sump system where oil returns to a common tank, a failure in one section (RGA) can potentially contaminate the other (Power Section)
.
Total System Hygiene: Replacing the gearbox alone is insufficient after a major metal-generating event; the entire oil system (lines, tank, and cooler) must be flushed to protect the new components from secondary damage
Case Overview
Estimated Time 80.5
Views 31
Author Fayez ALmutairi