N290AT
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.
19 reports on file, 2007-06-21 – 2014-02-23.
Part: RIB — CRACKED (RT HORIZ STAB) · airframe 26,173 hrs · 11,853 cycles
RT HORIZONTAL STABILIZER RIB A STAB STATION 166.30, RIB CRACKED AT 3RD VERTICAL STIFFENER. REPAIRED RIB IAW EA.
Part: SUPPORT — CRACKED (RT WING) · airframe 26,173 hrs · 11,853 cycles
RT WING TE PANEL SUPPORT BETWEEN NR 5 & NR 6 SPOILERS OTBD SUPPORT CRACKED. REPAIRED SUPPORT IAW SRM.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 26,173 hrs · 11,853 cycles
FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 887, RBL 21. R & R SUPPORT IAW SRM.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 26,173 hrs · 11,853 cycles
FLOOR SUPPORT CRACKED BETWEEN BS 277 TO BS 294, BL 0. R & R SUPPORT IAW SRM.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 26,173 hrs · 11,853 cycles
FLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R & R SUPPORT IAW SRM.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 26,173 hrs · 11,853 cycles
FLOOR SUPPORT CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R & R SUPPORT IAW SRM.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 26,173 hrs · 11,853 cycles
CABIN FLOOR SUPPORT CRACKED AT BS 344-360, BL 0, WL 208. R & R FLOOR SUPPORT IAW SRM.
Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 26,173 hrs · 11,853 cycles
MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 42. REPAIRED WEB IAW SRM & DRAWING.
Part: OIL FILTER — CONTAMINATED (NR 1 ENGINE) · airframe 26,113 hrs · 11,834 cycles
DIVERSION INFLIGHT SHUTDOWN ENG OIL FILTER BYPASS AMBER CAUTION MESSAGE. FOLLOWED QRH PROCEDURES REQUIRING ENG 1 SHUT DOWN. FOUND METAL IN NR 1 CHIP DETECTOR. R & R FILTER IAW MM.
Earlier reports · 2007–2013 · 10 reports
2013
Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 24,371 hrs · 11,105 cycles
R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT. REINSTALLED SLIDE IAW MM.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,252 hrs · 10,610 cycles
FWD GALLEY F/A FLASHLIGHT INOP. REMOVED AND REPLACED FWD GALLEY F/A FLASHLIGHT.
2012
Part: SLIDE — LOOSE (R1 DOOR) · airframe 21,369 hrs · 9,797 cycles
R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MM.
Part: LIGHT — BROKEN (CABIN) · airframe 21,151 hrs · 9,709 cycles
L2 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.
Part: COVER — DAMAGED (EXIT SIGN) · airframe 21,151 hrs · 9,709 cycles
L2 DOOR EMERGENCY EXIT SIGN COVER DAMAGED. REMOVED AND REPLACED COVER IAW MM.
2011
Part: COVER — OUT OF POSITION (CABIN)
GALLEY EXIT R1 SIGN FELL OFF (MX TEMP SECURED IN PLACE). RE-SECURED GALLEY EXIT LIGHT COVER AS REQUIRED.
Part: BATTERY PACK — FAILED (CABIN)
EMERGENCY LIGHT BATTERY PACK M1670 FAILED THE EMERGENCY BATTERY PACK CAPACITY FUNCTIONAL CHECK.
2010
Part: COVER — MISSING (CABIN)
EXIT LIGHT COVER MISSING NEXT TO 108, BESIDE R1 DOOR. REPLACED MISSING COVER.
2007
Part: FUSE — BLOWN (CABIN)
LEFT EMERGENCY EXIT WINDOW LIGHT INOP. RELAMPED AND REMOVED AND REPLACED FUSE REF AMM 33-21. OPS CHECK GOOD.
Part: PIN — INSTALLED (NLG)
NOSE GEAR WILL NOT RETRACT. FOUND NOSE GEAR LOCKOUT PIN INSTALLED. REMOVED NOSE GEAR LOCKOUT PIN, OK FOR SERVICE.