N686AA
Registered owner: BANK OF UTAH TRUSTEE, UT (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.
40 reports on file, 1995-02-01 – 2012-10-30.
Part: HYDRAULIC LINE — RUPTURED (HYDRAULIC SYS) · airframe 62,727 hrs · 21,879 cycles
MCO - CREW REPORTED AFTER GEAR DOWN AND FLAPS 20 DEGREE, LEFT HYDRAULIC SYSTEM PRESSURE EICAS MESSAGE. EMERGENCY DECLARED FLIGHT LANDED MCO WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT DOWNLOCK ACTUATOR LINES THAT WERE RUPTURED. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SKIN — PUNCTURED (FUSELAGE) · airframe 61,611 hrs · 21,480 cycles
A 1.5 INCH PUNCTURE ON THE LEFT SIDE 21 INCH FORWARD AND 8.5 INCHES BELOW THE LEFT NUMBER 1 DOOR. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-00-01-2R-3.
Earlier reports · 1995–2011 · 38 reports
2011
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,940 hrs · 20,828 cycles
CORROSION ON LOWER PORTION OF THE WEB AT STATIONS 1400 TO 1420 BUTTLINE 5 LEFT. INSTALLED NEW WEB PER SRM 51-70-00-0G.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,940 hrs · 20,828 cycles
CORROSION ON THE LOWER PORTION OF THE WEB AT STATIONS 1400 TO 1420 BUTTLINE 5 RIGHT. REPLACED DAMAGED WEB PER SRM 51-70-00-0G.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 59,878 hrs · 20,807 cycles
MIA - CREW REPORTED FIRST OFFICER WINDSHIELD SHATTERED AFTER WINDOW HEAT ARCING. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FIRST OFFICERS WINDSHIELD. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: ASPIRATOR — SEPARATED (EVAC SLIDE) · airframe 59,322 hrs · 20,606 cycles
DURING OVERHAUL MAINTENANCE OF EMERGENCY LIFE RAFT, ONE CHAMBER OF THE RAFT DID NOT INFLATE. UPON INVESTIGATION, IT WAS FOUND THAT THE ASPIRATOR, THE DIFFUSER/MIXING TUBE, HAD SEPARATED FROM THE INLET HOUSING. REMOVED ASPIRATOR AND INSTALLED A SERVICEABLE ONE.
Part: TRANSMITTER — TRIPPED (TE FLAP) · airframe 59,171 hrs · 20,553 cycles
DFW - CREW REPORTED ON APPROACH SELECTED FLAPS TO 25 DEGREES BUT FLAPS STUCK AT 20 DEGREES WITH A CORROSPONDING TRAILING EDGE FLAP DISAGREE LIGHT AND EICAS MESSAGE. FLIGHT LANDED DFW WITHOUT INCIDENT. RESET RIGHT OUTBOARD FLAP TRANSMITTER OVERLOAD INDICATOR THAT HAD TRIPPED. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 59,032 hrs · 20,506 cycles
MIA - CREW REPORTED PRESSURIZATION PROBLEM DUE TO LEFT PACK AND BLEED FAIL. FLIGHT ATTENDANT STATED, HEARD A LOUD POP BY THE RIGHT NUMBER 1 DOOR FOLLOWED BY A LOUD SQUEAL. THE O2 MASKS WERE DEPLOYED. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT CONTROLLER. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,481 hrs · 20,305 cycles
EMERGENCY PATH LIGHTING FROM ROWS 9 TO 16 WORKING, BUT VERY DIM. REPLACED ASSOCIATED POWER SUPPLY AND BATTERY PACK. OPS CHECK NORMAL.
Part: CHECK VALVE — DEFECTIVE (CABIN PRESSURE) · airframe 58,292 hrs · 20,233 cycles
JFK - INFLIGHT BOS-STT. CREW REPORTED UNABLE TO MAINTAIN CABIN PRESSURE WITH RIGHT PACK AND LEFT PACK ON MEL. EMERGENCY DECLARED FLIGHT DIVERTED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT CABIN SUPPLY CHECK VALVE THAT WAS DEFECTIVE AND AFT CARGO DOOR SEAL. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,705 hrs · 20,027 cycles
EMERGENCY LIGHT IN BULLNOSE ABOVE SEAT 25C IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN BULLNOSE ABOVE SEAT 25C. OPS CHECKS NORMAL.
Part: LIGHT — DEFECTIVE (CABIN) · airframe 57,705 hrs · 20,027 cycles
EMERGENCY PATHWAY LIGHT AT SEAT 4E IS VERY DIM. REPLACED LAMP FOR EMERGENCY PATHWAY LIGHT AT SEAT 4E. OPS CHECKS NORMAL.
2010
Part: CIRCUIT CARD — FAULTY (AIRSPEED) · airframe 56,201 hrs · 19,496 cycles
TUL - CREW REPORTED AIRSPEED INDICATION SPLIT. EMERGENCY DECLARED RETURNED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED SPEED CARD. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SKIN — WORN (TE FLAP) · airframe 56,200 hrs · 19,495 cycles
RIGHT OUTBOARD MAIN FLAP LEADING SKIN HAS WORN AREA 15 INCHES LONG FROM INBOARD END. REMOVED LEADING EDGE SKIN, CUT OUT WORN AREA, FORMED DOUBLER AND DRILLED, PRIMED AND INSTALLED DOUBLER PER SRM 57-53-01-2R.
Part: SKIN — CRACKED (LE SLAT) · airframe 56,200 hrs · 19,495 cycles
RIGHT WING: THERE ARE TWO CRACKS IN THE COVE SKIN OF THE NUMBER 9 SLAT AT THE INBOARD DRIVE TRACK. INSTALLED REPAIR DOUBLER ON SLAT 9 COVE SKIN IAW AARD 57-43-00-4.
Part: SKIN — CRACKED (LE SLAT) · airframe 56,200 hrs · 19,495 cycles
CRACK IN THE NUMBER 10 SLAT COVE SKIN OUTBOARD DRIVE TRACK. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER AARD 57-43-00-4.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,019 hrs · 19,426 cycles
EMERGENCY LIGHT ON SEAT 11D INOPERATIVE. RELAMPED EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,019 hrs · 19,426 cycles
RIGHT AFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP.
2009
Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,125 hrs · 18,744 cycles
EMERGENCY LIGHT AT SEAT 26D INOPERATIVE. REPLACED LAMP AT SEAT 26D.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,125 hrs · 18,744 cycles
EMERGENCY LIGHT AT SEAT 21D INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 21D.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 54,189 hrs · 18,768 cycles
EMERGENCY LIGHT AT SEAT 30D INOPERATIVE. REPLACED LAMP AT SEAT 30D.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,189 hrs · 18,768 cycles
EMERGENCY LIGHT AT SEAT 28D INOPERATIVE. REPLACED LAMP AT SEAT 28D.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,473 hrs · 18,518 cycles
ESCAPE PATH LIGHTING AT SEAT 21D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT 21D ESCAPE PATH LIGHTING.
2008
Part: SKIN — CRACKED (LE SLAT) · airframe 51,188 hrs · 17,713 cycles
NR 10 SLAT ASSY SKIN CRACKED. REPAIR DOUBLER INSTALLED IAW AARD 57-43-00-04
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 51,188 hrs · 18,813 cycles
NR 10 SLAT ASSY SKIN CORRODED. REPAIR DOUBLER INSTALLED IAW ECO B757-57-004757 DATED 10/16/2008.
Part: SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,188 hrs · 17,713 cycles
SILL TIE DOWN SUPPORT CORRODED. REPLACED SUPPORT IAW SRM 51-10-02.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHTS AT OVERHEAD WING EXIT INOPRATIVE. REPLACED BATTERY PACK AT SEAT ROW 25 RIGHT FOR EMERGENCY LIGHTS AT OVERHEAD WING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)
DFW - EMERGENCY EXIT LIGHT AT SEAT ROW 27 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 48,793 hrs
TPA - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: LIGHT — INOPERATIVE (CABIN)
JFK - EMERGENCY EXIT LIGHT AT FORWARD MID LEVEL LEFT NR 3 DOOR INOPERATIVE. REPLACED LEFT NER 3 DOOR FORWARD MID LEVEL EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: HEATER — MALFUNCTIONED (WINDOW)
ATL - INFLIGHT T2279 SMOKE IN COCKPIT AND CABIN. LANDED WITHOUT INCIDENT IN ATL. FOUND FIRST OFFICERS WINDSHIELD HEAT HIGH VOLTAGE TAP BAD. RAN ENGINES AT HIGH POWER SETTING. NO SMOKE OR ODOR NOTED. REPLACED R1 WINDOW. 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, ONE GIRT BAR SPRING OUT OF ADJUSTMENT. ADJUSTED ONE GIRT BAR SPRING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: CONNECTOR — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 5E INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3E INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: MODULE — INOPERATIVE (CABIN)
AUS - DURING OVERNIGHT MAINTENANCE, CABIN EMERGENCY EXIT ESCAPE PATH LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT MODULE AND BATTERY PACKS. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: CLAMP — BROKEN (A/C BAY)
DFW - FLT 2155 - EN ROUTE LGA-DFW, SHORTLY AFTER TAKEOFF DETECTED ALT WARNING IN COCKPIT. UPON DESCENT HEARD A SQUEALING NOISE IN COCKPIT. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE PACK SUPPLY DUCT CLAMP. LEAK CHECKS GOOD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — BROKEN (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT LEFT SIDE OVERWING EXIT DOOR BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT OVERWING EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: CONNECTOR — DEFECTIVE (PAX DOOR)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN AT R2 DOOR INOPERATIVE. REPAIRED EMERGENCY EXIT SIGN CONNECTOR AT R2 DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1999
Part: LIGHTS — TRIPPED (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AND FORWARD PART OF AIRCRAFT STAYS ILLUMINATED IN ARMED POSITION. RESET EMERGENCY EXIT FLOOR PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: EEL WIRE — FAILED (CABIN)
DFW - DURING OVERNIGHT, MAINTENANCE FOUND EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT FIRST CLASS COFFEE BAR INOPERATIVE. REPAIRED WIRING ON EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKS NORMAL OPERATION. (X)