N14667
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.
6 reports on file, 2000-04-06 – 2007-01-27.
Part: SKIN — CRACKED (R-1 DOOR) · airframe 22,004 hrs · 11,784 cycles
INSPECTION FOUND A 2 INCH CRACK AT LIGHTENING HOLE OF LOWER ROW 2ND FROM AFT IN R-1 DOOR SKIN. THE DOOR SKIN WAS REPAIRED IAW ECRA 5241-01017.
Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 22,004 hrs · 11,784 cycles
INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT TOP ANGLE BETWEEN STA 344 AND 360, BL 0. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02.
Part: BATTERY PACK — UNKNOWN (EMERGENCY LIGHT) · airframe 21,250 hrs · 11,377 cycles
EMERGENCY EXIT LIGHTS CAME ON IN FLIGHT. REPLACED BATTERY PACK IN FWD GALLEY CEILING.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 15,502 hrs · 8,390 cycles
INSPECTION FOUND A DEEP CREASE IN FUSELAGE SKIN AT STA 986.5, S26L TO S26R. A REPAIR WAS INSTALLED IAW ECRA 5331-01131. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR ON OR BEFORE JULY 14, 2006 OR THE ACCUMULATION OF 14,390 TOTAL FLIGHT CYCLES.
Part: BULKHEAD — CANNING (FUSELAGE) · airframe 13,668 hrs · 7,425 cycles
INSPECTION FOUND SKIN WEB OIL CANNED AT AFT PRESSURE BULKHEAD FORWARD SIDE RT LOWER SECTION BETWEEN S23R AND Z-CHANNEL. THE DAMAGED SECTION OF SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED IAW SRM 53-80-08, FIGURE 201.
Part: BATTERY PACK — INOPERATIVE (ROWS 10 - 17) · airframe 4,675 hrs · 2,496 cycles
INSPECTION FOUND EMERGENCY EXIT LIGHT AT ROWS 10 - 17 INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-51.