N675AN
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.
37 reports on file, 1999-08-10 – 2018-02-13.
Part: SUPPORT — CORRODED (BS 1480-1500) · corrosion level 2 · airframe 56,632 hrs · 18,308 cycles
STRINGER 17L BETWEEN BS 1480 TO 1500 CREASE BEAM SUPPORT HAS CORROSION IN SEVERAL AREAS.
Earlier reports · 1999–2014 · 36 reports
2014
Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 49,845 hrs · 17,301 cycles
RIGHT NR 2 DOOR UPPER HINGE CUT OUT IS CRACKED. INSTALLED DOUBLER IAW SRM 52-10-02-2R-1.
Part: SWITCH — FAILED (APU) · airframe 48,780 hrs · 16,918 cycles
MIA CREW REPORTED AUXILIARY POWER UNIT FAILED WITH RT INTEGRATED DRIVE GENERATOR ON PLACARD. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED APU LOW OIL TEMPERATURE SWITCH & RT INTEGRATED DRIVE GENERATOR, MPN 727792N. SYS GND CHECKED NORMAL, OPERATION CLOSED.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 48,070 hrs · 16,660 cycles
ROW 21D WHITE EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR SEAT 21D EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.
Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 45,620 hrs · 15,774 cycles
CCS - CREW REPORTED BIRD STRIKE TO RIGHT ENGINE FOLLOWED BY ENGINE FAILURE (SINGLE ENGINE TIME 4 MINUTES). EMERGENCY DECLARED FLIGHT RETURNED CCS LANDED WITHOUT INCIDENT. UPON LANDING CREW DISCHARGED FIRE BOTTLE. AIRCRAFT REMOVED FROM SERVICE. FOUND FIVE ENGINE FAN BLADES AND ATRITION LINER DAMAGED. REPLACED BLADES AND FIRE BOTTLE. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 45,361 hrs · 15,676 cycles
COCKPIT FLOORBEAM AREA INTERCOSTAL CRACKED AT BODY STATION 300, LEFT BUTTLINE 9, THRU ACCESS PANEL 117AL. REPLACED INTERCOSTAL PER SRM 51-40-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 45,361 hrs · 15,676 cycles
INTERCOSTAL WEB CRACKED AT RIGHT BUTTLINE 24 AND BODY STATION 325. REMOVED AND REPLACED WEB INTERCOSTAL PER SRM 51-40-02.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,361 hrs · 15,676 cycles
MAIN CABIN FLOORBEAM SUPPORT UPPER SURFACE CORRODED AT BODY STATION 347, RIGHT BUTTLINE 23. INSTALLED NEW T-CAP SUPPORT PER SRM 51-40-05 AND BOEING DRAWING 141N5150.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,361 hrs · 15,676 cycles
MAIN CABIN FLOORBEAM SUPPORT UPPER SURFACE CORRODED FROM BODY STATIONS 395 TO 405, RIGHT BUTTLINE 62. INSTALLED SUPPORT AND ASSEMBLY PER SRM 51-40-02.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,361 hrs · 15,676 cycles
MAIN CABIN FLOOR SUPPORT LOWER ATTACH ANGLE CORRODED BODY STATION 335, RIGHT BUTTLINE 27. REPLACED ANGLE PER SRM 51-40-02.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,361 hrs · 15,676 cycles
MAIN CABIN FLOORBEAM SUPPORT UPPER SURFACE CORRODED AT BODY STATION 403, RIGHT BUTTLINES 12 TO 23. REPLACED SUPPORT PER SRM 51-40-02.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,361 hrs · 15,676 cycles
MAIN CABIN FLOORBEAM SUPPORT UPPER SURFACE CORRODD BODY STATION 403, RIGHT BUTTLINES 47 TO 58. REPLACED SUPPORT AND ASSEMBLY SRM 51-40-02.
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,361 hrs · 15,676 cycles
MAIN CABIN FLOORBEAM SUPPORT UPPER SURFACE CORRODED FROM BODY STATIONS 395 TO 405, RIGHT BUTTLINE 11. INSTALLED NEW SUPPORT PER SRM 51-40-02.
2012
Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,361 hrs · 15,676 cycles
MAIN FLOORBEAM SUPPORT UPPER SURFACE CORRODED BODY STATION 365, RIGHT BUTTLINES 44 TO 47. REMOVED DAMAGE AND REPAIRED SUPPORT PER EA B757-53-027701.
2011
Part: CONNECTOR — LOOSE (CABIN) · airframe 40,102 hrs · 13,701 cycles
EMERGENCY LIGHT AT SEAT 11E FAILED TO TEST. FOUND LOOSE CONNECTOR TO WALL CONNECTION. RESEATED CONNECTOR. OPS CHECK NORMAL.
2009
Part: BELTFRAME — DENTED (FUSELAGE) · airframe 36,002 hrs · 12,210 cycles
BELTFRAME DENTED AT STATION 1420, STRINGER 25 LEFT TO 26 LEFT. INSTALLED REPAIR PER SRM 53-00-07-2R AND EA B757-53-008265.
Part: PAN — GOUGED (L4 DOOR HANDLE) · airframe 36,002 hrs · 12,210 cycles
LEFT NUMBER 4 PASSENGER DOOR BUTTERFLY HANDLE TRAY HAS 3 INCH GOUGE. REMOVED AND REPLACED HANDLE PAN PER ESO 90108.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS)
DFW - OVERHEAD EMERGENCY PATH LIGHTING AT ROW 2E INOPERATIVE. REPLACED LAMP AT OVERHEAD EMERGENCY PATH LIGHTING AT ROW 2E.
2008
Part: LIGHT — DAMAGED (CABIN)
DFW - EMERGENCY LIGHT AT RIGHT AFT LAVATORY DAMAGED. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT RIGHT AFT LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: ACTUATOR — LEAKING (SPOILERS)
MIA INFLIGHT T688/22AUG DFW TO SJU, LOST CENTER HYDRAULIC FLUID DURING FLIGHT. DIVERTED TO MIA AND LANDED WITHOUT INCIDENT. FOUND NUMBER ONE SPOILER ACTUATOR LEAKING. REPLACED NUMBER ONE SPOILER ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
JFK - EMERGENCY LIGHT AFT OF LEFT NUMBER THREE DOOR INOPERATIVE. RELAMPED EMERGENCY LIGHT AFT OF LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS)
BOS - EMERGENCY LIGHTS AT LEFT ROW 27 INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT LEFT ROW 27. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS)
BOS - EMERGENCY LIGHTS AT RIGHT ROW 29 INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT RIGHT ROW 29. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS)
BOS - EMERGENCY LIGHTS AT LEFT ROW 20 INOPERATIVE. RELAMPED EMERGENCY LIGHTS AT LEFT ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHT)
SEA - EMERGENCY LIGHT AT LEFT OVERWING EXIT HAS MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT OVERWING EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: LIGHT — INOPERATIVE (CABIN)
MIA - EMERGENCY LIGHTS AT SEATS 12D AND 13D INOPERATIVE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHTS AT SEATS 12D AND 13D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: O-RING — LEAKING (ZONE 500)
LEFT ENGINE BEGAN TO USE FUEL AT INCREASED RATE. LANDED JAX WITHOUT INCIDENT. FOUND LEFT HAND FUEL LEAKING FROM FUEL CONTROL SUPPLY LINE. REPLACED O-RING ON FUEL CONTROL SUPPLY LINE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2002
Part: STRIP — LOOSE (CABIN)
ALT - DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHTING STRIP LOOSE AT ROW 14. REATTACHED STRIP AT ROW 14. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
JFK - FOUND FLOOR PATH LIGHT IN FIRST CLASS INOPERATIVE. SECURED CONNECTOR IN FIRST CLASS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: TIRE — SEPARATED (LANDING GEAR)
MIA - FLT 2111 - EN ROUTE MIA-LIM, DURING TAKEOFF, NR 7 TIRE CAP SEPARATED. RETURNED TO MIA WITHOUT INCIDENT. FOUND DAMAGE TO THE RIGHT WING, TRAILING EDGE FLAP AND NR 2 ENGINE COWL. COMPLETED REPAIRS TO TRAILING EDGE FLAP, A WING PANEL, AND ENGINE COWLING. REPLACED THE NR 7 TIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: ECU — FAILED (E/E BAY)
MIA - FLT 1736 - EN ROUTE SJU-MIA - INBOUND TO MIA, TRAILING EDGE FLAPS STUCK AT 20 DEGREES. LANDED AT MIA WITHOUT INCIDENT. REPLACED NR 1 FLAT/SLAT ELECTRONIC UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT SECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE FLOOR PATH LIGHT AT MID GALLEY HAS ONE BULB INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT MID GALLEY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT DOORS 2L AND 2R INOPERATIVE. REPAIRED BROKEN WIRE AT AFT END OF GALLEY NUMBER 2. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: WIRE — FAILED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS CABIN INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHTING IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: SOCKET — CORRODED (RT EMRG EXIT)
ORD - DURING OVERNIGHT MAINTENANCE, RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATE. CLEANED CORRODED LIGHT SOCKET. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: WIRE — SHORTED (CABIN)
BOS - DURING OVERNIGHT INSPECTION, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPAIRED EMERGENCY EXIT FLOOR PATH LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)