2009-11 · NASA ASRS report 862382
A Line Mechanic reports about the missing max N2 engine speed starter re-engagement information on their Quick Reference Checklists. Mechanics use the data for engine run emergencies on their A320's. The information is crucial in order to re-engage the starter after an engine shutdown; to blow out tail-pipe fires.
After a stable start on an A320; (Auto-Start with Auto Protection box no longer displayed on ECAM); #2 engine had what appeared to be an idle speed compressor stall with roll back. Engine was shut down and as N2 speed decreased; EGT climbed; indicating tail pipe fire; (fire was also indicated by Ground Crew). Starter was engaged at 10% N2; to blow fire out. Issue is that our Quick Reference Checklists card Mechanics use for emergencies; does not give the N2 max speed for when the starter can be re-engaged. It appears; the thinking is that tail-pipe fires only happen during starts and that the Auto-Start/Protection will take over and re-engage the starter at the correct time. The tail pipe fire on the aircraft we had in November was at normal stable idle and Auto-protection was no longer armed. It was possible; if we did not know the correct max N2 speed in which a starter could be re-engaged; the starter (shaft) could have been sheared off. Then the ability to blow the fire out would have been lost. Not all of our aircraft have the same max N2 re-engage speed for blowing a fire out; which is why each engine information should be listed on all the Quick Reference Checklists that Mechanics use for emergencies. This fire could have gotten out of control and damaged more than the engine. Even though we had the Engine Run-up Handbook with us; it is not set up for quick references during an emergency as the Quick Reference Checklists are obviously designed to be.
Reporter stated his awareness about the lack of Max N2 Speed information on their Quick Reference Checklists stating when a starter re-engagement can be attempted; began on the first day after their A320 had been pushed out of the hangar following a Maintenance Check. During an idle speed engine run; the #2 engine had an idle speed compressor stall with a roll back. Although the engine was shut down and N2 speed was decreasing; he noticed the EGT was climbing indicating a tail-pipe fire. At that moment he referred to his Quick Reference Checklists; but could not find the re-engagement N2 speed reference. Reporter stated he wanted to re-emphasize that after a stable engine start; if an engine fire occurs like the one he had experienced on the A320; the Auto Protection feature; or Phase; does not take over to protect the engine. Reporter stated the cause of the A320 engine fire was due to a loose pneumatic line 'B'-nut connection and wrong bleed solenoids being installed on the right side of the fan case at the bleed solenoid support bracket. The 7th and 10th stage bleed valves were affected. Mechanics have to look at the numbers inscribed on the solenoid casting by a vibrating tool to verify they have the correct solenoid.
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Source: NASA Aviation Safety Reporting System (public domain). Reports are voluntary submissions and are not verified by NASA.
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