N674AN
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.
54 reports on file, 1999-08-06 – 2013-05-18.
Part: BALLAST — FAILED (GALLEY LIGHTS) · airframe 47,982 hrs · 16,528 cycles
F/A REPORTED ELECTRICAL ODOR NEAR AFT GALLEY. EMERGENCY DECLARED, AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND AFT OVERHEAD GALLEY LIGHT BALLAST WITH STRONG ELECTRICAL ODOR. REPLACED LIGHT CONTROL RELAY AND BALLAST ASSEMBLY FOR AFT GALLEY OVERHEAD LIGHT ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: STRAP — CRACKED (FUSELAGE) · airframe 47,152 hrs · 16,235 cycles
CENTER STRAP UNDER FRAME AT STATION 377 IS CRACKED. ACCOMPLISHED NESTED ANGLE REPAIR PER SRM 53-10-51-2R-1.
Earlier reports · 1999–2012 · 52 reports
2012
Part: TRANSMITTER — INOPERATIVE (TE FLAP) · airframe 44,262 hrs · 15,210 cycles
DEN - INFLIGHT JFK-EGE. CREW REPORTED FLAP SPLIT INDICATION. EMERGENCY DECLARED FLIGHT DIVERTED DEN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT AND RIGHT TRAILING EDGE FLAP POSITION TRANSMITTERS. SYSTEM GROUND CHECK NORMAL OPERATION.
2011
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
FLOORBEAM STATION 1640 HAS SEVERAL AREAS OF CORROSION TOP AND BOTTOM SIDE AROUND HOLES. CUT OUT DAMAGE AND INSTALLED T-CAP AND SPLICE STA 1640 PER BOEING LOR5L53005 REPAIR 5 AND EA B 757-53-019586.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
AFT DECK SEVERAL AREAS OF CORROSION STATIONS 1710 TO 1720 FROM STRINGERS 17 LEFT TO 17 RIGHT. REMOVED OLD MULTIPLE DOUBLER, AND INSTALLED ONE LARGER REPAIR DOUBLER IAW SRM 53-60-51-2R 2 AND EA B757-53-019472.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
CORROSION ON LAVATORY TIE DOWN AT STATION 1640 AT LC 25. REPLACED LAVATORY FLOOR FITTING PER SRM 51-10-02-0G.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
CABIN FLOOR SUPPORT HAT CHANNEL CORRODED. REPLACED CHANNEL IAW SRM 51-10-02-0G.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
AFT GALLEY DECK PLATE Z ANGLE STRUCTURE TOP OF DECK STATIONS 1680 TO 1720 LEFT SIDE CORRODED. Z-ANGLE INSTALLED PER AARD 51-10-05-1.
Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
CORROSION ON DOUBLER FORWARD OF RIGHT GALLEY MOUNT. INSTALLED NEW DOUBLER PER SRM 53-60-51-2R.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
RIGHT AFT GALLEY MOUNT IN AFT GALLEY AREA CORRODED. INSTALLED NEW MOUNT PER SRM 51-10-02-0G.
Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
CABIN, Z ANGLE STRUCTURE TOP OF DECK STATIONS 1680 TO 1720 ON RIGHT SIDE CORRODED. INSTALLED NEW Z ANGLE PER SRM 51-10-02-0G AND SRM 51-40-02-0G.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
HAT CHANNEL ON AFT DECK AT FRAME STATION 1680 TO 1710 CORRODED AROUND FASTENER HOLE. INSTALLED AFT CENTER HAT CHANNEL PER SRM 51-10-02-0G.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
RIGHT FORWARD GALLEY MOUNT IN AFT GALLEY AREA CORRODED. INSTALLED NEW MOUNT PER SRM 51-10-02-0G.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 43,125 hrs · 14,759 cycles
ACCIDENTAL IMPACT AT STATION 1844 STRINGER 2 LEFT. ACCOMPLISHED DOUBLER REPAIR PER AT STATION 1844 PER SRM 53-00-01-2R-3.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
G1B GALLEY, AFT OUTBOARD MOUNT IS CORRODED. INSTALLED A NEW G1B GALLEY MOUNT PER SRM 51-10-02-0G, PARAGRAPH 9.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 43,125 hrs · 14,759 cycles
CENTER INTERCOSTAL FLOORBOARD SUPPORT ANGLE CRACKED STATIONS 1520 TO 1540. REMOVED AND INSTALLED NEW SUPPORT ANGLE AT STATIONS 1520 TO 1540 PER SRM 51-10-02-0G.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
IN THE CABIN AT STATION 375 THE GALLEY MOUNT FORWARD END IS CORRODED, RIGHT BUTTLINE 11. INSTALLED NEW GALLEY MOUNT PER SRM 51-10-02-0G.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
MID LAVATORY MOUNT AFT OUTBOARD CORRODED. REPLACED MOUNT PER SRM 51-10-02-0G.
Part: MOUNT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 43,125 hrs · 14,759 cycles
MID LAVATORY MOUNT AFT INBOARD CORRODED. REPLACED MOUNT PER SRM 51-10-02-0G.
2010
Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,087 hrs · 13,680 cycles
PATHWAY EMERGENCY LIGHT AT SEAT 20D IS INOPERATIVE. REPLACED LAMP FOR PATHWAY EMERGENCY LIGHT AT SEAT 20D. OPS CHECKS NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,087 hrs · 13,680 cycles
EMERGENCY LIGHT ABOVE SEAT 13ABC IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ABOVE SEAT 13ABC. OPS CHECKS NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,087 hrs · 13,680 cycles
EMERGENCY LIGHT ON EXTERIOR SIDE OF RIGHT NUMBER DOOR 1 IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT ON EXTERIOR SIDE OF RIGHT NUMBER 1 DOOR. OPS CHECKS NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,645 hrs · 12,803 cycles
EXTERNAL EMERGENCY LIGHT AT LEFT FORWARD OVERWING INOPERATIVE. REPLACED LAMP.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 37,645 hrs · 12,803 cycles
EXTERNAL EMERGENCY LIGHT AT RIGHT AFT OVERWING INOPERATIVE. REPLACED LAMP.
2009
Part: LIGHT — BROKEN (ZONE 200) · airframe 40,764 hrs · 13,915 cycles
THE 20DEF EMERGENCY LIGHT IS BROKEN. REPLACED LIGHT ASSEMBLY FOR 20DEF EMERGENCY LIGHT. OPS CHECKS NORMAL.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 34,737 hrs
LAS - SEAT MOUNTED EMERGENCY LIGHTS FROM SEAT 9D TO 15D WILL NOT ILLUMINATE. REPLACED BATTERY PACK.
Part: MODULE — DEFECTIVE (EMERGENCY LIGHTS) · airframe 34,737 hrs
LAS - SEAT MOUNTED EMERGENCY PATH LIGHTS FROM SEATS 9D TO 15D WILL NOT ILLUMINATE. REPLACED DEFECTIVE MODULE.
2008
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,626 hrs
DFW - EMERGENCY LIGHT EXIT SIGN AT OVERHEAD RT NR ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGN AT OVERHEAD RT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,626 hrs
DFW - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,626 hrs
DFW - EXTERIOR EMERGENCY LIGHT AT LT NR ONE DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT LT NR ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LIGHT — DIRTY (EXTERIOR) · airframe 32,626 hrs
DFW - EXTERIOR EMERGENCY LIGHT AT RT NR FOUR DOOR INOPERATIVE. CLEANED AND SECURED LIGHT ASSEMBLY FOR EXTERIOR EMERGENCY LIGHT AT RT NR FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,626 hrs
DFW - EMERGENCY LIGHT EXIT SIGN AT OVERHEAD MID LAVATORY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGN AT OVERHEAD MID LAVATORY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,455 hrs
MIA EMERGENCY LIGHT AT RT NUMBER THREE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT RT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,455 hrs
MIA EMERGENCY LIGHT AT SEAT ROW 26 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 26. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED) (A)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DFW - EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: INDICATOR — TRIPPED (TE FLAPS) · airframe 31,563 hrs
JFK INFLIGHT T1876/09FEB MIA TO LGA - CREW REPORTED FLAP FAULT DURING DEPLOYMENT. TRAILING EDGE DISAGREE INDICATION. EXTENDED FLAPS WITH ALTERNATE SYSTEM. LANDED JFK WITHOUT INCIDENT. FOUND LEFT TRANSMISSION NUMBER ONE OVERLOAD INDICATOR TRIPPED. RESET INDICATOR AND SERVICED TRANSMISSION. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: BULB — BROKEN (EMERGENCY LIGHTS)
MIA - EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR BROKEN. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER THREE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS)
MIA - EMERGENCY LIGHT AT SEAT 5E INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 5E. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT SEAT ROW 26 INOPERATIVE. REPLACED LEFT BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 26. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT SEAT 36D INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 36D. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: GOVERNOR — INOPERATIVE (RT ENGINE)
FLL INFLIGHT T2369/12MAR RIGHT HAND ENGINE PARAMETER FLUCTUATIONS. RETURNED TO FLL AND LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE FUEL FLOW GOVERNOR AND THE HIGH PRESSURE FUEL PUMP. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: SKIN — DAMAGED (FUSELAGE)
TUL - REPAIR OF TEMPORARY REPAIR OF FUSELAGE SKIN AT STRINGER 26L TO 27L AT STATION 500. CUT OUT AREA WAS 4.5 INCHES BY 6.25 INCHES. REPAIRED TEMPORARY REPAIR PER ESO 09309 AND SRM 53-30-01.
2003
Part: CONNECTOR — LOOSE (CARGO BAY)
MIA AFT CARGO DOOR EMERGENCY LIGHT INOPERATIVE. FOUND CONNECTOR DISCONNECTED AT BATTERY PACK. REPOSITIONED AND SECURED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (CABIN)
MIA - OVERNIGHT MAINTENANCE OBSERVED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT SEAT 20D. REINSTALLED LOOSE CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGTHS AT SEAT 1E INOPERATIVE. REPLACED EMEREGNCY EXIT SEAT LIGHT AT 1E. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT FLOOR PATH STRIP. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, MAIN CABIN FLOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT STRIP AT MAIN CABIN FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING FROM ROW 15 TO 17, AND 34 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — DAMAGED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE FLOOR PATH LIGHTS IN FIRST CLASS INOPERATIVE. REPAIRED WIRING. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: CONNECTOR — DAMAGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE FLOOR PATH LIGHTS INFORWARD COACH AREA INOPERATIVE. REPLACED EMERGENCY EXIT ESCAPE FLOOR PATH LIGHTS IN FORWARD COACH AREA CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (SEAT 26-34)
MIA - DURING OVERNIGHT MAINTENANCE EMERGENCY EXIT LIGHT FLOOR PATH LIGHTS AT SEAT 26D AND 34D INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT 26D TO 34D. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: WIRE — LOOSE (ROWS 9D-17D)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTING STRIPS FROM SEAT 9D TO SEAT 17D INOPERATIVE. RE-SECURED WIRE TO EMERGENCY EXIT FLOOR PATH LIGHTING STRIPS BETWEEN SEATS 9D AND 17D. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: BOTTLE — FAILED TEST (LT EMERG EXIT)
MEX - DURING OVERNIGHT MAINTENANCE, EMERGENCY OVERWING SLIDE BOTTLE WOULD NOT TEST FROM CABIN. PLACARDED LEFT OVERWING BOTTLE 'TEST INOP' PER MEL. REPLACED EMERGENCY OVERWING SLIDE BOTTLE. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)