N620AA
Registered owner: KINSER TODD, SD (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.
35 reports on file, 1995-06-05 – 2012-06-12.
Part: SKIN — CORRODED (LE SLAT) · corrosion level 2 · airframe 68,561 hrs · 24,357 cycles
CORROSION ON INBOARD LEADING EDGE NOSE SKIN. REMOVED CORRODED AREA AT SKIN AND INSTALLED DOUBLER PER AARD 57-43-00-1.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 68,172 hrs · 24,213 cycles
SEAT MOUNTED EMERGENCY LIGHT AT 27D INOPERATIVE. SECURED LOOSE CONNECTOR AT WALL FOR SEAT 27D EMERGENCY LIGHT. OPS CHECKED NORMAL.
Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 68,172 hrs · 24,213 cycles
BULLNOSE EMERGENCY LIGHT AT SEAT 29D INOPERATIVE. REPLACED LAMP FOR BULLNOSE EMERGENCY LIGHT AT SEAT 29D. OPS CHECK NORMAL.
Earlier reports · 1995–2011 · 32 reports
2011
Part: SIGN — OUT OF POSITION (CABIN) · airframe 67,647 hrs · 24,025 cycles
EMERGENCY EXIT LIGHT AT SEAT 17F FELL OFF. RE-INSTALLED EXIT SIGN. OPS CHECK NORMAL.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 65,844 hrs · 23,384 cycles
CORROSION ON STRINGER 29 RIGHT AT STATION 1460. SPLICED IN NEW SECTION OF STRINGER PER SRM 53-60-03-2R AND EA 757-53-017171.
Part: DOOR — CRACKED (L4) · airframe 65,844 hrs · 23,384 cycles
LEFT NUMBER 4 DOOR IS CRACKED IN CUT-OUT UPPER HINGE. REPAIRED PER EA B757-52-017045.
Part: WEB — CRACKED (RT MLG WW) · airframe 65,844 hrs · 23,384 cycles
RIGHT WHEELWELL CRACKED AT HYDRAULIC LINE ABOVE KEELBEAM STATION 1110. INSTALLED DOUBLER PER AARD 53-40-12-01.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,935 hrs · 22,358 cycles
LEFT AFT OVERWING EXIT FLOOD LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT AFT OVERWING EXIT FLOOD LIGHT. OPS CHECKED NORMAL.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 62,935 hrs · 22,358 cycles
SEAT 23D EMERGENCY LIGHT INOPERATIVE. RE-SECURED CONNECTOR FOR SEAT 23D EMERGENCY LIGHT. OPS CHECKED NORMAL.
Part: LIGHT — DAMAGED (CABIN) · airframe 62,935 hrs · 22,358 cycles
RIGHT FORWARD OVERWING EXIT MARKER DAMAGED. REPLACED EXIT MARKER FOR RIGHT FORWARD OVERWING EXIT. OPS CHECKED NORMAL.
2009
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 61,280 hrs · 21,741 cycles
FLOORBEAM AT STATION 700 IS CRACKED. REPAIRED UNDER SRM 53-00-51-2R3.
Part: SKIN — CORRODED (NR 7 SLAT) · corrosion level 2 · airframe 61,280 hrs · 21,741 cycles
CORROSION ON LEADING EDGE SLAT NUMBER 7 ABOUT 38 INCHES FROM INBOARD END OF SLAT. REMOVED CORRODED AREA, INSTALLED FLUSH DOUBLER REPAIR PER AARD 57-43-00-1.
Part: SLAT — CORRODED (LT WING) · corrosion level 2 · airframe 61,280 hrs · 21,741 cycles
NUMBER TWO SLAT LEADING EDGE LEFT WING AT STATION 623.50 SHOWS CORROSION. REMOVED CORROSION AND INSTALLED FLUSH DOUBLER PER ESO 90249 AND SRM 57-43-00-01.
Part: SKIN — CORRODED (NR 7 SLAT) · corrosion level 2 · airframe 61,280 hrs · 21,741 cycles
NUMBER 7 SLAT HAS AREA OF CORROSION APPROXIMATELY 30 INCHES FROM OUTBOARD END. REMOVED DAMAGED SKIN AND INSTALLED FLUSH DOUBLER REPAIR PER AARD57-43-00-1.
Part: VALVE — INOPERATIVE (ENGINE ANTI ICE) · airframe 59,230 hrs · 21,041 cycles
ORD CREW REPORTED LT ENGINE ANTI-ICE FAILED. EMERGENCY DECLARED LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT HAND ENGINE ANTI-ICE VALVE. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)
Part: SLAT — MALFUNCTIONED (WING) · airframe 59,071 hrs · 20,993 cycles
LAS - ON APPROACH CAPTAIN REPORTED RECEIVING SLAT LEADING EDGE ASYMMETRY WARNING LIGHT. ABORTED APPROACH AND DID GO AROUND. EMERGENCY DECLARED, LANDED LAS WITH SLATS AT 20 WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. NO FAULTS FOUND. CYCLED SLATS SEVERAL TIMES. SYSTEM GROUND CHECK NORMAL OPERATION.
2008
Part: FSEU — FAILED (TE FLAPS) · airframe 58,469 hrs
MIA INFLIGHT - ON FINAL APPROACH BOTH LEADING EDGE AND TRAILING EDGE FLAP DISAGREE INDICATIONS. REPLACED NUMBER ONE FLAP SLAT ELECTRONICS UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 58,371 hrs
TPA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 11D INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 11D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,229 hrs
LGA EMERGENCY LIGHT AT OVERHEAD SEAT 16C INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 16C. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
2007
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
JFK - EMERGENCY LIGHT AT AFT DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT AFT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: ACTUATOR — INOPERATIVE (SLATS)
MIA - DURING DESCENT, LEADING EDGE SLAT DISAGREE OCCURRED DURING FLAP EXTENSION FROM ONE DEGREE TO FIVE DEGREES. FOUND NUMBER NINE AND TEN LEADING EDGE ROTARY ACTUATORS TRIPPED. REPLACED NUMBER NINE AND TEN LEADING EDGE ROTARY ACTUATORS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHTS AT SEATS 16D THROUGH 25D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEATS 16D THROUGH 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT ON ROWS 16D TO 26D INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON ROWS 16D TO 26D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
FIRST CLASS EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK FOR FIRST CLASS EMERGENCY LIGHTS. SYSTEM GROUND CHECKED. NORMAL OPERATION.
2003
Part: WIRE — MISINSTALLED (EMERGENCY LIGHT)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT 16D TO 23D INOPERATIVE. FOUND WIRE CROSSED AT SEAT 16D. RESPLICED PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
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)
2001
Part: HYDRAULIC LINE — LEAKING (NR 1 ENGINE)
DFW - FLT 1086 - EN ROUTE DFW-BOS, LEFT HYDRAULIC PRESSURE DECREASED TO ZERO. RETURNED DFW AND LANDED WITHOUT FURTHER INCIDENT. REPLACED LEFT SIDE RETURN LINE. NO LEAKS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (CABIN)
TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT SEAT 3E DIM. REPLACED EMERGENCY EXIT LAMP AT SEAT 3E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT ON SEAT 27D INOPERATIVE. SECURED LOOSE CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1998
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, FORWARD LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. ATTACHED LEADS TO FORWARD LEFT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: MODULE — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, R2 DOOR EMERGENCY EXIT LIGHT JUST AFT OF DOOR INOPERATIVE, REPLACED EMERGENCY EXIT AISLE PATH LIGHTING CONTROL MODULE AND BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, FORWARD EMERGENCY EXIT FLOOR PATH LIGHTS WERE INOPERATIVE. REPAIRED EMERGENCY FLOOR PATH WIRE AT FORWARD CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: CONNECTOR — LOOSE (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 6 THROUGH 17 INOPERATIVE. REINSTALLED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 6. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: EEL CONDUCTOR — BROKEN (CABIN)
DFW - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FORWARD PART OF FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL STRIP — DEFECTIVE (CABIN)
ORD - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 3E-5E LENS WILL NOT STAY IN PLACE. REPLACED EMERGENCY EXIT FLOOR LIGHT STRIP AT 3E-5E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)