FAA incident reports · 4
FAA accident and incident reports matched to this aircraft by N915DN and the event date: up to this one’s cancellation.
Incident 20070320003559IGround Taxi, Other Airplane · Boise, ID(-23) After a normal landing, taxi, and arrival at gate B22 at the Boise airport (boi), delta airlines flight 1240 was in the process of deplaning passengers while the first officer was conducting a post-flight termination walk around. At that time, he…Incident 20060407006629INormal Cruise · Boise, ID(-23) Delta flight 1234, enroute from slc to sea diverted to Boise. Pilot noted a vibration while at FL320. He checked the engine instruments and saw the left engine epr had rolled back and EGT was flashing approximately 634 degrees. He retarded the throttle…Incident 20040421014949INormal Cruise · Salt Lake City, UT(-23) Flight crew of of aircraft thought aircraft right hydraulic system became disabled because the hydraulic pressure and quantity indicators (EFIS) read "----". Flight crew shut down right hydraulic system and declared an emergency landing to destination…Incident 20001208024379ILevel Off Touchdown · Santa Ana, CA(-23) Attached narrative
Service difficulty reports · 110
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DALA2019120607128Unknown · fumesDURING TAXI IN AFTER LANDING CLE, AFT FLT ATTENDANT REPORTED A HAZE/ SMOKE IN CABIN FROM ABOUT MIDWAY TO THE AFT OF CABIN. ONE FLIGHT ATTENDANT SAID IT HAD AN ACID/ACRID SMELL. THE HAZE DISAPATED BY THE TIME WE ARRIVED AT GATE. THERE WERE NO PASSENGER COMPLAINSDR DALA2019030501446Strut · damagedSHIP 9215-- DIV-- BOS. NOSE GEAR WOULD NOT RETRACT AFTER TAKE OFF. CORRECTIVE ACTION: PROPERLY SERVICED NOSE GEAR STRUT. CYCLED GEAR AND FOUND CHUNK OF CHROME MISSING FROM LOWER STRUT FWD SIDE WHEN FULLY EXTENDED. REMOVED AND REPLACED PISTON AXLE ASSEMBLY AND SDR DALA2019021901030Access Panel · crackedFOUND 2 CRACKS ON INTERNAL WEB AT ACCESS PANEL ON LH SIDE OF RAM AIR INLET. REMOVED FASTENERS, VERIFIED CRACK TERMINATION AND CONTAINMENT. DAMAGE CONTAINED BY INSTALLATION OF REPAIR DOUBLERS. FABRICATED AND DRILLED 2 INTERNAL DOUBLERS (FROM .063 T6) PER SRM 55
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