N68159
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
15 reports on file, 2006-08-20 – 2012-10-03.
Part: SOCKET — LOOSE (EMERGENCY LIGHT) · airframe 50,793 hrs · 7,357 cycles
RT EXIT EMERGENCY LIGHT AFT OF CARGO DOOR INOPERATIVE. FOUND LIGHT SOCKET LOOSE IN REFLECTOR, REPLACED SOCKET AND REFLECTOR, OPS CK NORMAL.
Part: MEGAPHONE — NO TEST (AFT CABIN) · airframe 49,705 hrs · 7,212 cycles
AFT MEGAPHONE INTERMITENT. REPLACED AFT MEGAPHONE, CHECKED OK.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,300 hrs · 7,028 cycles
EMERGENCY LIGHTS AT ROWS 3, 4, 5 INOP. REPLACED BATTERY PACK AT ROW 19R, OPS CK NORMAL.
Earlier reports · 2006–2011 · 12 reports
2011
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 46,107 hrs · 6,751 cycles
UNSCHEDULED STAB TRIM EICAS LIGHT ILLUMINATED ON T/O ROLL APPROX 40 KTS ABORTED, LIGHT WENT OUT AS WE TAXIED OFF R/WAY PERFORMED UNSCHEDULED STAB TRIM TEST PER FIM 27-09-00 PG 167 STEPS 1 & 2 FAULT BALLS RESET, RAN TEST NO FAULTS NOTED. ACFT READY FOR SERVICE.
Part: FRAME — CRACKED (NR 2 PYLON) · airframe 45,401 hrs · 6,659 cycles
SUPPORT TASK - NR 2 PYLON NAC STA 285 I/B FRAME CHORD AND UPPER CLIP FOUND CRACKED. NR 2 PYLON NAC STA 285 I/B FRAME CRACKED CHORD AND UPPER CRACKED CLIP. REPLACED AS PER SRM 51-10-02 AND NEW FRAME CHORD AND NEW CLIP INSTALLED AS PER SRM 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,401 hrs · 6,659 cycles
CABIN LT STA 303 LBL 25-50 FLOORBEAM UPPER SURFACE FOUND CORROSION. CABIN LT STA 303 LBL 20 - LBL 68 FLOORBEAM UPPER FLANGE REPAIRED AS PER SRM 53-00-51 FIG 201 REPAIR 1 AND HFEC NIL CRACK FOUND.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 45,401 hrs · 6,659 cycles
CABIN LT STA 325 LBL 22 TO 50 FLOORBEAM UPPER SURFACE FOUND CORROSION. CABIN LT STA 325 LBL 12 TO LBL 68 FLOORBEAM UPPER FLANGE REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201 AND HFEC NIL CRACK FOUND.
Part: FITTING — CRACKED (NR 2 PYLON) · airframe 45,401 hrs · 6,659 cycles
SUPPORT TASK NR 2 PYLON NAC STA 285 TO STA 295 HORI TEE CHORD CRACKED. NR 2 PYLON NAC STA 285 TO STA 295 HORI TEE CHORD REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02.
2009
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,963 hrs · 5,541 cycles
R1 DOOR FLT ATTENDANT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED BATTERY, OPS CHECKS GOOD.
2008
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 33,818 hrs · 5,108 cycles
FWD CARGO STA 412 CABIN FLOORBEAM ATT SEAT TRACK CRACK LBL 20. CABIN STA 380 - 412 LBL 20 SEAT TRACK REPLACED PER SRM 51-10-02 AND FASTENER INSTALLED PER SRM 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,818 hrs · 5,108 cycles
CABIN - STA 325 LBL 25 - LBL 54 FLOOR SUPPORT FOUND CORRODED. CABIN STA 325 LBL 18 - LBL 59 FLOOR SUPPORT BEAM REPAIRED PER SRM 53-00-51, FIG 201, REPAIR 1 AND HFEC NO CRACK FOUND.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,818 hrs · 5,108 cycles
CABIN - FLOOR SUPPORT FOUND CORRODED AT BS 303 BETWEEN LBL 20-35. CABIN FLOOR SUPPORT BEAM STA 303 LBL 20 TO LBL 60 REPAIRED PER SRM 53-00-51 REPAIR 1 FIG 201 AND HFEC NO CRACK FOUND.
2006
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,129 hrs · 3,647 cycles
INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 30-58. THE FLOORBEAM WAS REPLACED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 23,129 hrs · 3,647 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303-325, LBL 35. THE CORROSION WAS REMOVED AND THE FLOOR SUPPORT WAS REPLACED IAW SRM 53-00-51, FIGURE 101 AND SRM 51-40-02.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,129 hrs · 3,647 cycles
INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 30-60. THE CORROSION WAS REMOVED AND THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 101 AND SRM 53-00-51, FIGURE 201, REPAIR 1.