FAA incident reports · 2
FAA accident and incident reports matched to this aircraft by N806CK and the event date: after August 18, 1989, when the previous aircraft’s registration ended, through this one’s cancellation.
Incident 19900711033579IForced/Precautionary Landing · San Antonio, TXHydraulic quantity in auxiliary reservoir depleted after takeoff. Returned, NR3 engine hydraulic pump had failed.Incident 19900711033569IForced/Precautionary Landing · San Antonio, TXHydraulic system failure for second time that day. Returned. NR2 engine hydraulic pump had failed.
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CKSA98349Plug · mislocatedON CLIMBOUT, BURNING SMELL NOTED IN COCKPIT. FO'S AUDIO PANEL CB POPPED. AFTER 5 MIN COOL DOWN, CB RESET AN IMMEDIATELY POPPED AGAIN. BURNING SMELL DISIPATED. FOUND FO'S MIC JACK SHORTING OUT DUE TO LOCATION OF MOUNTING BRACKET. RELOCATED AS REQUIRED. SYSDR CKSA98001Wire · brokenNR 2 OIL LIGHT LOW PRESS CAME ON, T/R AND T/R DOOR LIGHT CAME ON, GEN FAIL LIGHT CAME ON, OIL PRESS THEN DROPPED AS DID OIL QUANTITY. COMPLETED NR 2 ENGINE SHUTDOWN. LATER AT TOD NR 2 ENGINE FIRE WARNING LIGHT (1/2 SYSTEM) CAME ON, FIRED BOTTLE. REPAIRED WISDR CKSA96191Lockout Cylinder · reqd serviceWHEN 35 DEGREES FLAPS WERE SELECTED, FLAPS CAME DOWN TO 25 DEGREES, MISSED APPROACH. SELECTED FLAPS 35 DEGREES, FLAPS CAME DOWN TO 25 DEGREES UNTIL AIRCRAFT SLOWED TO 145 KIAS, THEN FLAPS LOWERED TO 35 DEGREES. BLED AND SERVICED FLAP LOCKOUT CYLINDER PER MM SDR CKSA96188Skin · puncturedON WALKAROUND, FOUND HOLE IN SIDE OF AIRCRAFT AT STATION 480 JUST AFT OF A-PIT. AIRCRAFT REPAIRED PER SRM 53-4-0, 53-2-1 WITH A CLASS TWO REPAIR, REFERENCE EA 96-296. REINSPECT WITHIN 12,000 CYCLES, REPETITIVE INSPECT AT 4,000 CYCLES THEREAFTER.SDR CKSA95139Link Assy · failedKCVG - FLT 68278 - UPON GEAR RETRACTION DURING CLIMB, NOSE GEAR DOOR DID NOT FULLY CLOSE. THIS CAUSED A VIBRATION IN NOSE GEAR DOOR WELL. FLEW ACFT AT 230KIAS/M.65. (UPLATCH FAIL CHECK SPEED). WITH GEAR DOWN, NO VIBRATION NOTED. ALL OTHER GEAR INDICATIONSSDR CKSA95064Floor Beam · corrosionKOSC - DURING C-CHECK INSPECTION, FOUND CORROSION ON FLOOR BEAM WEB AT LIGHTING HOLE AT RIGHT END STATION 440 'A' PIT. REMOVED CORROSION IAW SRM 51-1-6 FABRICATED AND INSTALLED PART IAW ENGINEERING SKA95118-1. COMPLIED WITH AIA EA95-176. (M)SDR CKSA95063Angle · corrosionKOSC - DURING C-CHECK INSPECTION, FOUND INBOARD LOWER AFT ANGLE IN WHEELWELL DOGHOUSE AREA SURFACE CORRODED. REMOVED ANGLE, REMOVED CORROSION IN CENTER WING UPPER SKIN PANEL. CORROSION REMOVAL OUT OF SRM LIMITS. REPAIRED SKIN PER ENGINEERING SKETCH SKA95118
Other aircraft with N806CK · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. No aircraft carries N806CK now.