N610AA
Registered owner: ANDURIL INDUSTRIES INC, CA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
24 reports on file, 1995-08-06 – 2012-04-06.
Part: GOVERNOR — INOPERATIVE (FUEL FLOW) · airframe 71,184 hrs · 25,599 cycles
CREW REPORTED DURING DESCENT RIGHT ENGINE SHUTDOWN (SINGLE ENGINE TIME 10 MINS). CREW ABLE TO RESTART ENGINE AT APPROXIMATELY 10000 FEET. EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FUEL FLOW GOVERNOR AND HIGH PRESSURE FUEL PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — CRACKED (CABIN) · airframe 71,182 hrs · 25,598 cycles
CREW REPORTED RIGHT NUMBER 4 DOOR EMERGENCY LIGHT LENS MISSING. FOUND ASSEMBLY CRACKED. REPLACED LIGHT ASSEMBLY. OPS CHECK NORMAL.
Part: ACTUATOR — TRIPPED (SLATS) · airframe 70,789 hrs · 25,446 cycles
CREW REPORTED LEADING EDGE SLAT DISAGREE EICAS MESSAGE. ACCOMPLISHED QRH. FLIGHT RETURNED DEN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 8 SLAT OUTBOARD ACTUATOR INDICATOR POPPED. REPLACED NUMBER 8 SLAT OUTBOARD ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Earlier reports · 1995–2011 · 21 reports
2011
Part: ENGINE — LEAKING (RIGHT) · airframe 67,888 hrs · 24,362 cycles
STL - CREW REPORTED ON DESCENT RIGHT ENGINE EICAS MESSAGE - OIL QUANTITY AND OIL PRESSURE LOW. ACCOMPLISHED PRECAUTIONARY ENGINE SHUTDOWN (SINGLE ENGINE TIME 28 MINS). EMERGENCY DECLARED FLIGHT LANDED STL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT STL ON 02/08/2011. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SLIDE — MALFUNCTIONED (R1 DOOR) · airframe 67,685 hrs · 24,288 cycles
RIGHT NUMBER 1 DOOR WAS OPENED ON THE INSIDE WHILE STILL ARMED. SLIDE DEPLOYMENT WAS UNSUCCESSFUL. REPLACED SLIDE AND BOTTLE FOR RIGHT NUMBER 1 DOOR. OPS CHECK NORMAL.
2010
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 67,418 hrs · 24,201 cycles
CORROSION ON FUSELAGE SKIN, STATION 536 BETWEEN STRINGERS 29 RIGHT AND 29 LEFT. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 53-00-01.
2009
Part: SOCKET — BROKEN (CABIN) · airframe 64,168 hrs · 23,046 cycles
SEAT MOUNTED EMERGENCY LIGHTS AT SEAT 18D INOPERATIVE. REPLACED BROKEN SOCKET AT SEAT 18DEF.
Part: LENS — MISSING (CABIN) · airframe 64,168 hrs · 23,046 cycles
EMERGENCY LIGHT AT LEFT NUMBER FOUR DOOR FORWARD SIDEWALL MISSING LENS. REPLACED LENS AT LEFT NUMBER FOUR DOOR.
Part: ROTARY ACTUATOR — MALFUNCTIONED (LE SLAT) · airframe 62,746 hrs · 22,525 cycles
SFO - UPON RETRACTING FLAPS FROM 1 DEGREE TO 0 DEGREES LEADING EDGE LIGHT AND LEADING EDGE SLAT DISAGREE MESSAGE ILLUMINATED. EMERGENCY DECLARED RETURNED SFO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 AND 20 ROTARY DRIVE ACTUATORS. REMOVED AND REPLACED FLAT SLAT ELECTRICAL UNIT. SYSTEM GROUND CHECK NORMAL OPERATION.
2008
Part: LENS — MISSING (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT SEAT ROW 31ABC MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 31ABC. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT SEAT ROW 12ABC MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT ROW 12ABC. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,445 hrs
BOS - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT ROW 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SLIDE — FAILED (L1 DOOR)
SNA LEFT NUMBER ONE DOOR SLIDE FAILED TO DEPLOY WHEN DOOR OPENED IN ARMED POSITION. REPLACED SLIDE AND POWER RESERVOIR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 58,517 hrs
JFK - EMERGENCY LIGHT AT SEAT 32D INOPERATIVE. SECURED CONNECTOR ON HARNESS FOR EMERGENCY LIGHT AT SEAT 32D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — LOOSE (EMERGENCY LIGHTS)
MIA - EMERGENCY EXTERIOR LIGHT AT LEFT NUMBER THREE DOOR INOPERATIVE. FOUND LIGHT BULB LOOSE. ADJUSTED LIGHT BULB FOR EMERGENCY EXTERIOR LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPINNED HARNESS CONNECTOR FOR EMERGENCY LIGHT AT SEAT ROW 26DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: SLIDE — DISLODGED (L1 DOOR)
MIA - L1 SLIDE PARTIAL UNSUCCESSFUL DEPLOYMENT. SLIDE FELL OUT ON JETBRIDGE. DOOR ASSIST BOTTLE DISCHARGED UPON ARRIVE AT GATE WHEN DOOR WAS BEING OPENED BY GROUND CREW. FOUND GIRT BAR ENGAGED DURING INSPECTION. REPLACED SLIDE AND DOOR ASSIST BOTTLE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: SPRING — OUT OF ADJUST (GIRT BAR)
DURING ACCOMPLISHMENT OF ENGINEERING REQUEST TO CHECK GIRT BAR SPRINGS AT EACH PASSENGER DOOR POSITION, EIGHT GIRT BAR SPRINGS OUT OF ADJUSTMENT. ADJUSTED EIGHT GIRT BAR SPRINGS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: LIGHT — BROKEN (L2 DOOR)
SFO - FLT 485 - AIRCRAFT ARRIVED SFO WITH L2 DOOR EMERGENCY EXIT LIGHT BROKEN. REPLACED L2 DOOR EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLOORBEAM — CORRODED (BS 365)
AFW - FORWARD CABIN FLOORBEAM STATION 365 LBL 60 HAD CORROSION BLENDED BEYOND SRM LIMITS. ALODINED, FABRICATED REPAIR STRAP FROM STAINLESS STEEL PRIMED, FILLED BLEND AREA, INSTALLED STRAP WET PER MRB 757-1120. (M)
Part: FLOORBEAM — CORRODED (BS 1640)
AFW - AFT CABIN FLOORBEAM STATION 1640 HAD CORROSION BEYOND SRM LIMITS. ALODINED BLEND AREAS, FABRICATED REPAIR STRAP FROM STAINLESS STEEL. PRIMED, FILLED BLENDED AREAS, INSTALLED STRAPS WET WITH SEALANT. (M)
Part: FLOORBEAM — CORRODED (BS 377)
AFW - FORWARD CABIN FLOORBEAM STATION 377 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDED BOTH AREAS LBL 31 AND LBL 56, ALODINED AND PRIMED, FILLED BLENDS, SATISFACTORY FOR CONTINUED SERVICE PER MRB 757-1119. (M)
Part: FLOORBEAM — CORRODED (BS 1640)
AFW - FOUND CORROSION REMOVED FROM CABIN FLOORBEAM STATION 1640 BEYOND SRM LIMITS. BLENDED CORRODED AREAS, ALODINED, FABRICATED REPAIR STRAP FROM STAINLESS STEEL. PRIMED STRAP AND FLOORBEAM, FILLED BLEND AREA, INSTALLED REPAIR STRAP. (M)
1995
Part: EEL CONDUCTOR — BROKEN (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT MID GALLEY INOPERATIVE. REPLACED FLAT CONDUCTOR AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)