N190AJ
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.
6 reports on file, 2000-05-16 – 2001-11-27.
Part: DETECTOR — GROUNDED (#3 ENGINE) · airframe 73,871 hrs · 46,186 cycles
DISCREPANCY: Fire detection light on #3 engine came on in flight. (ground fault).CORRECTIVE ACTION: Replaced #3 engine fire detector.
Part: STRINGER CLIP — CRACKED (FUSELAGE) · corrosion level 2 · airframe 72,882 hrs
BS 680 STRINGER 17L CRACK AT FUSELAGE TO FRAME CLIPS FORWARD AND AFT. REPLACED (2) SHEAR TIES, MADE FROM 7075-T6, .040. PER SRM 53-10-4 FIG 11, 12 AND 13.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,882 hrs
FLOORBEAM AT BS 1090, LBL 62.5 CORRODED. REMOVED CORRODED AREA, FABBED AND INSTALLED REPAIR PARTS PER SRM 53-10-8 FIG 8.
Part: POSITION SWITCH — INACCURATE (LE FLAPS) · airframe 72,351 hrs · 44,597 cycles
AT 22,000 FEET, LEADING EDGE FLAP NR 5 AMBER LIGHT CAME ON. DESCENDED TO 20,000 FEET AND CYCLED FLAPS AND LEADING EDGE FLAPS, NR 2, 4 AND 5 AMBER LIGHTS REMAINED ON. RETURNED TO ANCHORAGE. REPLACED LEADING EDGE FLAP POSITION SWITCHES FOR NR 2, 4 AND 5 POSITIONS.
Part: PIN — DISLODGED (NLG TORQUE LINK) · airframe 72,220 hrs
AIRCRAFT LANDING AT OTZ. AT NOSE GEAR TOUCH DOWN A SEVERE SHIMMY AND VIBRATION WAS FELT WITH NO NOSE STEERING AVAILABLE. MAINTENANCE, UPON ARRIVAL FOUND THE TORQUE LINK APPEX PIN HAD COME OUT AND DISCONNECTED THE TORQUE LINKS DUE TO BEING INSTALLED INCORRECTLY. REPLACED BOTH NOSE WHEELS AND FERRIED TO BASE WITH NOSE GEAR DOWN AND PINNED. AT BASE MAINTENANCE REPLACED THE UPPER AND LOWER TORQUE LINKS, THE CONTROL ROD AND THE APPEX PIN.
Part: PIN — MISINSTALLED (NLG TORQUE LINK)
OTZ - AICRAFT LANDING, AT NOSE GEAR TOUCH DOWN, A SEVERE SHIMMY AND VIBRATION WAS FELT WITH NO NOSE STEERING AVAILABLE. MAINTENANCE, UPON ARRIVAL, FOUND THE TORQUE LINK APPEX PIN HAD COME OUT AND DISCONNECTED THE TORQUE LINKS DUE TO BEING INSTALLED PREVIOUSLY INCORRECTLY. REPLACED BOTH NOSE WHEELS AND FERRIED TO BASE WITH NOSE GEAR DOWN AND PINNED. AT BASE, MAINTENANCE REPLACED THE UPPER AND LOWER TORQUE LINKS, THE CONTROL ROD AND THE APEX PIN. (X)