N917CK
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.
15 reports on file, 2013-08-14 – 2019-04-30.
Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 51,402 hrs · 62,857 cycles
FLOOR PANEL CORROSION
Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 51,402 hrs · 62,857 cycles
FLOOR PANEL CORRODED.
Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 51,402 hrs · 62,857 cycles
FLOOR PANEL CORROSION
Part: STRUCTURE — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 51,402 hrs · 62,857 cycles
R/W T/E FLAP, L/E TOP STA XFLS 127 TO XFLS 187
Part: SKIN — CRACKED (BS 972) · airframe 51,402 hrs · 62,857 cycles
R/H FUSELAGE SKIN CRACK STA 972 ABOVE R/H PYLON TRAILING EDGE FAIRING
Part: ANTENNA — FRACTURED (RADAR ALTIMETER) · airframe 51,321 hrs · 62,826 cycles
CLIMBING THROUGH FL240 PRESS WARNING LIGHT ILLUMINATED CABIN DIFF PRESSURE HIGHEST READING WAS 3PSI. AIRCRAFT RETURNED TO KYIP FOR UNSCHEDULED LANDING. UPON INSPECTION OF AIRCRAFT IT APPEARS THAT THE AIRCRAFT SUSTAINED A LIGHTING STRIKE AND THE FWD RADAR ALT ANTENNA WAS MISSING THUS RESULTING IN THE CABIN PRESSURIZATION BEING UNABLE TO MAINTAIN PRESSURE. CORRECTIVE ACTION: REPLACED DAMAGED DEACTIVATED #1 RAT ALT ANTENNA WITH BLANKING PLATE, AND PERFORMED LIGHTING STRIKE INSPECTION, NO DEFECTS NOTED.
Earlier reports · 2013–2017 · 9 reports
2017
Part: AILERON — CORRODED (LEFT) · corrosion level 2 · airframe 50,734 hrs · 62,490 cycles
LEFT OTBD AILERON HAS EVIDENCE OF CORROSION.
2014
Part: DOWNLOCK SWITCH — STUCK (RT MLG) · airframe 49,632 hrs · 61,799 cycles
RT GEAR, UNSAFE LIGHT ILLUMINATED DURING CRUISE, CLIMB. FOUND RT MLG DOWNLOCK SWITCH IN DOWNLOCK POSITION. R & R RT MLG DOWNLOCK SWITCH WITH SERVICEABLE UNIT IAW MM 32-60-1. NO DEFECTS NOTED.
Part: LATCH — OUT OF ADJUST (MLG) · airframe 49,359 hrs · 61,616 cycles
AFTER TAKEOFF, UNABLE TO RAISE LANDING GEAR. NO EMERGENCY PROCEDURES TAKEN, RETURNED DEPARTURE. ADJUSTED LANDING GEAR ANTI-RETRACTION LATCH RIG AND OP'S CHECKED GOOD IAW AMM 32-23-1. PERFORMED LANG GEAR SWING OP'S CHECKED GOOD IAW AMM 32-30-00.
2013
Part: SPAR — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 49,359 hrs · 61,615 cycles
CORROSION ON RT WING T/E FLAP REAR SPAR STA XRS 240.
Part: SPAR — CRACKED (RT ELEVATOR) · airframe 49,359 hrs · 61,615 cycles
RIGHT ELEVATOR HAS A CRACK INDICATION ON THE FRONT SPAR CHORD STA XE 92.
Part: SPAR — CRACKED (RT ELEVATOR) · airframe 49,359 hrs · 61,615 cycles
RIGHT ELEVATOR CRACK INDICATION ON FRONT SPAR CHORD STA XE 109.
Part: FRAME — CRACKED (ZONE 200) · airframe 49,359 hrs · 61,615 cycles
FRAME STRUCTURE HAS TWO CRACKS AT STA 83 + 10 FROM CENTER VIEWED THROUGH LT WIPER MOTOR HOLE. ONE CRACK IN FLANGE RADIOUS ABOUT .5" & 1 CRACK AT FASTENERS 1 INCH LONG.
Part: SKIN — CORRODED (RT ELEVATOR) · corrosion level 2 · airframe 49,359 hrs · 61,615 cycles
RT ELEVATOR TOP SIDE INBD SKIN DAMAGED, STA XE 15.
Part: SKIN — CORRODED (LT ELEVATOR) · corrosion level 2 · airframe 49,359 hrs · 61,615 cycles
EVIDENCE OF CORROSION ON UPPER OTBD END OF LT ELEVATOR, STA XE 209-233.