N680AN
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.
46 reports on file, 1999-07-09 – 2017-09-26.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 49,145 hrs · 17,129 cycles
UPON FURTHER EVALUATION RT OVERWING PORT IS CORRODED OUT OF LIMITS IAW SRM 53-20-01 A1 REV 121 DATED MAY 20/2017.
Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,145 hrs · 17,129 cycles
MAIN CABIN FLOOR AFT SHEAR WEB PANEL HAS SEVERAL AREAS OF CORROSION ON UPPER SURFACE STA 1681 TO 1720 RBL 60 TO LBL 60.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 49,145 hrs · 17,129 cycles
MAIN CABIN INTERCOSTAL BETWEEN STA 540-560 AT LBL 45 IS CRACKED ON THE UPPER FLANGE.
Part: FRAME — CRACKED (FUSELAGE) · airframe 49,145 hrs · 17,129 cycles
CRACK IN AFT FACE OF FRAME AT STA 1540 BETWEEN 7R-6R.
Earlier reports · 1999–2015 · 42 reports
2015
Part: BEARING — LACK OF LUBE (TE FLAP) · airframe 49,117 hrs · 17,115 cycles
EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH WHEN FLAP SELECTED TO 1 CREW RECEIVED AN EICAS TE FLAP DISAGREE INDICATION. EXTENDED FLAPS TO 20 DEGS USING QRH PROCEDURES. ACCOMPLISHED FIM 27-51-00-815-808 & FSEU BITE CHECK WITH NO FAULTS FOUND. INSPECTED FLAP TRANSMISSIONS, NO OVERLOAD INDICATED. LUBED TE FLAP TRACK BEARINGS & OPERATED FLAPS. SYS CHECKED NORMAL.
2014
Part: TRANSMISSION — MALFUNCTIONED (TE FLAP) · airframe 48,204 hrs · 16,774 cycles
TRAILING EDGE FLAP DISAGREE INDICATION DURING FINAL APPROACH. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RT INBD FLAP TRANSMISSION. SYS GND CHECKED NORMAL OPERATION CLOSED.
Part: SKIN — CRACKED (LE SLAT) · airframe 47,742 hrs · 16,603 cycles
CRACK IN NR 2 SLAT COVE SKIN AT FASTENER HOLES AT INBD DRIVE TRACK. INSTALLED DOUBLER IAW AARD 57-43-00-4.
Part: SKIN — GOUGED (FUSELAGE) · airframe 47,742 hrs · 16,603 cycles
GOUGE IN CROWN SKIN AT STATION 600. INSTALLED PLUG FASTENER IAW EA B757-53-035743.
Part: PANEL — CRACKED (LE SLAT) · airframe 47,742 hrs · 16,603 cycles
TWO CRACKS ON UNDERSIDE OF COVE PANEL NR 9 SLAT. INSTALLED DOUBLER REPAIR IAW AARD 57-43-00-4 REPAIR 4.
Part: ACTUATOR — INOPERATIVE (LE SLAT) · airframe 46,950 hrs · 16,318 cycles
MIA CREW REPORTED LE SLAT DISAGREE. EMERGENCY DECLARED FLIGHT MIA LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED NR 13 ROTARY ACTUATOR & RESET TORQUE LIMITER. SYS GND CHECKED NORMAL, OPERATION CLOSED.
2013
Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 43,678 hrs · 15,142 cycles
MIA - CREW REPORTED DURING DESCENT MID LAVATORY SMOKE DETECTOR BEGAN RINGING WITH NO EVIDENCE OF SMOKE OR FIRE. FLIGHT LANDED MIA WITHOUT INCIDENT. REPLACED MID LAVATORY SMOKE DETECTOR. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SKIN — GOUGED (FUSELAGE) · airframe 43,678 hrs · 15,142 cycles
DENTED AND GOUGED AREA IN FUSELAGE SKIN BODY STATION 511, STRINGERS 29 TO 28 LEFT. INSTALLED PERMANENT DOUBLER REPAIR PER SRM 53-00-01-2R-3.
2012
Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 43,358 hrs · 15,017 cycles
MIA - CREW REPORTED RIGHT GENERATOR CONTROL SWITCH FAILED. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED GENERATOR CONTROL PANEL. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 42,963 hrs · 14,875 cycles
EMERGENCY LIGHTS AT ROW 16DEF INOPERATIVE. RECONNECTED WIRE PLUG CONNECTION BEHIND SIDE WALL AT 16DEF. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,886 hrs · 14,849 cycles
LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT OVERWING EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,886 hrs · 14,849 cycles
RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: COVER — CRACKED (CABIN) · airframe 42,886 hrs · 14,849 cycles
LEFT NUMBER FOUR DOOR EMERGENCY EXIT SIGN COVER CRACKED. REPLACED LEFT NUMBER FOUR DOOR EMERGENCY EXIT LIGHT ASSEMBLY. OPS CHECK NORMAL.
Part: CONTACT — DEFECTIVE (EMERGENCY LIGHTS) · airframe 42,459 hrs · 14,692 cycles
AISLE AND EXIT ROW EMERGENCY LIGHTS OUT AT ROW 16D. REPLACED CONTACT THAT WAS PUSHED IN, OPS CHECK NORMAL.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,482 hrs · 13,977 cycles
SEAT 18F EMERGENCY EXIT SPOT LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY SPOT LIGHT AT SEAT 18F. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 39,580 hrs · 13,648 cycles
LEFT NUMBER 1 DOOR EXTERIOR MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP AT LEFT NUMBER 1 DOOR FOR EXTERIOR MOUNTED EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: CHARGER — FAILED (MAIN BATTERY) · airframe 37,493 hrs · 12,890 cycles
KIN - INFLIGHT MIA-AUA. CREW REPORTED MAIN BATTERY DISCHARGE LIGHT ILLUMINATED IN FLIGHT. FLIGHT DIVERTED KIN LANDED WITHOUT INCIDENT. AUXILIARY POWER UNIT BATTERY AND CHARGER RELOCATED TO THE MAIN SHIPS BATTERY POSITION. APU BATTERY AND CHARGER PLACARD PER MEL. REPLACED APU BATTERY (MPN 018550000) AND CHARGER ON 01/18/2011 AT TUL. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,197 hrs · 12,029 cycles
SEAT 27D SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 27D SEAT MOUNTED EMERGENCY LIGHT. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,979 hrs · 11,949 cycles
EXTERNAL EMERGENCY LIGHT ON AFT CARGO DOOR INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT ON AFT CARGO DOOR. OPS CHECKED NORMAL.
2009
Part: SKIN — DAMAGED (NR 2 PYLON) · airframe 34,010 hrs · 11,599 cycles
NUMBER TWO ENGINE PYLON INBOARD SKIN DAMAGED AT STATION 133. INSTALLED DOUBLER PER ENGINEERING AUTHORITY B757-54-008266,
Part: STRUCTURE — CORRODED (TE FLAP) · corrosion level 2 · airframe 34,010 hrs · 11,599 cycles
CORROSION ON TOP OF RIGHT INBOARD FLAP SPAR AREA IN SEVERAL PLACES. INSTALLED TWO DOUBLERS PER ENGINEERING AUTHORIZATION COMP 57-008337.
Part: SLAT — DAMAGED (LT WING) · airframe 34,010 hrs · 11,599 cycles
LEFT WING NUMBER 3 SLAT TRAILING EDGE BOTTOM AT STATION 465 WORN. DAMAGED AREA IS 2 INCHES BY 25 INCHES. REMOVED DAMAGED AREA AND INSTALLED 310 DEGREE HOT BOND PERMANENT REPAIR PER SRM 51-70-10-2R 4 FIG 202.
Part: PAN — GOUGED (L1 DOOR) · airframe 34,010 hrs · 11,599 cycles
LEFT NUMBER ONE PASSENGER DOOR HANDLE PAN IS GOUGED. REMOVED DAMAGED PAN AND REPLACED WITH NEW PAN.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 33,562 hrs · 11,441 cycles
LEFT OVERWING EXIT SIGN INOPERATIVE. RELAMPED SIGN AND INSTALLED SERVICEABLE BATTERY PACK, OPS OK.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,040 hrs · 11,248 cycles
TUL - CORROSION ON SCREW HOLES (CABIN FLOOR). INSTALLED REPAIR UNDER SRM 53-00-51-2R3.
Part: FLOOR SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,040 hrs · 11,248 cycles
TUL - CORROSION ON FLOOR SKIN FROM LEFT BUTTLINE 0 TO LEFT BUTTLINE 54. INSTALLED REPAIR UNDER SRM 53-60-51-2R ALT 11.
2008
Part: SIGN — DISLODGED (EMERGENCY LIGHT) · airframe 31,024 hrs
DFW - EMERGENCY EXIT SIGN OVER SEAT 17F FELL OFF. SECURED EMERGENCY EXIT SIGN OVER SEAT 17F. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT SEAT 16DEF INOPERATIVE. SECURED LOOSE CONNECTOR FOR EMERGENCY LIGHT AT SEAT 16DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT SEAT 9DEF INOPERATIVE. INSTALLED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 9DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT SEAT ROW 10DEF INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 10DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT SEAT 17DEF INOPERATIVE. INSTALLED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 17DEF. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY WALL MOUNTED FLOOD LIGHT AT MID LAVATORY INOPERATIVE. REPLACED EMERGENCY WALL MOUNTED FLOOD LIGHT ASSEMBLY AT MID LAVATORY WALL. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — BROKEN (CABIN)
MIA - EMERGENCY LIGHT AT SEAT 9D BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 9D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WINDSHIELD — CRACKED (COCKPIT)
EWR INFIGHT T596/12MAR AT 290 KNOTS AT FLIGHT LEVEL 280 CAPTAINS WINDSHIELD SHATTERED. LANDED EWR WITHOUT INCIDENT. REPLACED WINDSHIELD PER MAINTENANCE MANUAL 56 11 01 04. REPLACED HEAT CONTROLLER AS PRECAUTIONARY. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
2005
Part: MODULE — INOPERATIVE (EMERGENCY LIGHT)
LGA - EMERGENCY LIGHT AT RIGHT FOUR DOOR INOPERATIVE. REPLACED BATTERY AND CHARGER M736 FOR EMERGENCY LIGHT AT RIGHT FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (CABIN)
DFW - EMERGENCY EXIT SIGN LIGHT AT THE L764 CLASS DIVIDER AT STATION 647 INOPERATIVE. REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY M731 FOR EMERGENCY EXIT SIGN LIGHT AT THE L764 DIVIDER. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT)
JFK - SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT AT ROW 27D INOPERATIVE. SECURED CONNECTOR AT SEAT 27D FOR SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHTS AT SEAT ROWS 27 THROUGH 36 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS FOR SEAT ROWS 27 THROUGH 36. SYSTEM GROUND CHECKED NORMAL OPERATION.
1999
Part: CONNECTOR — FAILED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EEMRGENCY EXIT FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR IN FIRST CLASS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, AFT SECTION IN FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPAIRED WIRING TO THE AFT SECTION IN FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: WIRE — BROKEN (ROW 5EF)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING AT SEAT 5EF INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING WIRE AT SEAT 5EF. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: LIGHT — DEFECTIVE (CABIN)
DFW - DURING OVENRIGHT MAINTENANCE, LEFT AND RIGHT MAINTENANCE LEFT AND RIGHT EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)