N727NK
Registered owner: ANTARES AVIATION LLC, FL (owner ≠ operator)
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
INTERCOSTAL CORRODED AT STA 1060 STRINGER 20 LEFT.
LEFT BUTTLINE 56, STA 344 SEAT TRACK CORRODED.
NR 2 ENGINE, UPPER FORWARD MOUNT ASSY CORRODED.
LEFT BUTTLINE 55 SEAT TRACK HAS SEVERAL AREAS OF CORROSION BETWEEN STA 991 TO 1030.
SEAT TRACK CORRODED BETWEEN STA 800 TO 815, LEFT BUTTLINE 25.
INTERCOSTAL AT STA 1060, LEFT BUTTLINE 26 AREA OF CORROSION.
CORROSION AROUND EDGE OF WALL AND FLOOR WEB AT STA 1148, RIGHT BUTTLINE 63.
CORROSION AROUND PINS IN FLOOR WEB AT STA 1146 BETWEEN RIGHT BUTTLINE 54 AND 58.
SEAT TRACK SUPPORT CORRODED AT LEFT BUTTLINE 45.5, STA 1090 TO 1110.
TOP CORD OF FLOORBEAM CORRODED ON FLOORBEAM AT STA 1110, LEFT BUTTLINE 24 TO 52.
RIGHT WING AFT BOTTLE PIN CUP HAS EVIDENCE OF CORROSION UNDER PIN CUP.
EVIDENCE OF CORROSION BETWEEN STA 950E AND 950E, STRINGER 15L.
FRAME DAMAGED AT STA 1130 BETWEEN STR 27 AND 28 RIGHT.
CORROSION ON RIGHT SIDE OF UPPER RUDDER TRAILING EDGE AT RS 175.
CORROSION ON LEFT SIDE OF UPPER RUDDER TRAILING EDGE BETWEEN RS 220 AND 242.
FLOOR TO SKIN WEB CRACKED, .25' AT EDGE OF LIGHTENING HOLE AT STA 490, RIGHT BUTTLINE 72.
FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE AT STA 1110 LEFT BUTTLINE 1 TO RIGHT BUTTLINE 12.
SHEAR TIE CORRODED AT STA 1130 BETWEEN STR 29 AND 30 LEFT.
SHEAR TIE CORRODED AT STA 1110, BETWEEN STR 28 AND 29 LEFT.
SUPPORT WEB CRACKED LEFT BUTTLINE 25 FROM STA 1130 TO 1110.
CORROSION ON LEFT SIDE OF UPPER RUDDER BETWEEN STA 212 AND 220.
FLOORBEAM CORRODED STA 1110 LEFT BUTTLINE 12 TO LEFT BUTTLINE 24 TOP AND BOTTTOM.
UPPER RUDDER SKIN CORRODED RIGHT SIDE TRAILING EDGE BETWEEN STA 220-247.
SKIN DAMAGED ON LOWER RUDDER LEFT SIDE BETWEEN STA 113-118.
SHEAR TIE CORRODED AT STA 1130 BETWEEN STR 27 AND 28 RIGHT.
CRACK ON TOP OF NR 1 PYLON OUTBD FASTENER HOLE"P" OF S/B 727-54A0010R6, FROM HOLE TO OTBD EDGE OF LOWER ANGLE.
LEFT UPPER RUDDER PANEL BETWEEN STA 212 AND 220 HAS ONE AREA OF DELAMINATION.
FRAME AT STA 1148 CORRODED AT STR 26R.
SHEAR TIE CORRODED AT STATION 1130 BETWEEN STR 27 AND 28 LEFT.
SHEAR TIE CORRODED STA 1166 BETWEEN STR 29 AND 30 LEFT.
OTBD STRUCTURE AT DOOR FRAME, BS 950E DAMAGED AT STR 27R.
FRAME DOUBLER CORRODED AT BS 1166, BETWEEN STR 25L AND 25R.
WEB AT BS 990 CORRODED FROM RBL 27 TO RBL 29.
CORROSION ON BOTTOM CORD OF FLOORBEAM AT STA 1130, LBL 28.
STRINGER 29L, CORRODED BETWEEN STA 950F AND 960F.
FRAME AT BS 950B CORRODED ABOVE STR 28L.
FLOOR SUPPORT, CORRODED BETWEEN STA 950E AND 960E AT STR 27R.
STRINGER 29R CRACKED AT BS 985.
FRAME AT BS 990, RBL 22 AREA OF CORROSION.
SHEAR TIE CORRODED ON AFT SIDE STA 1148 BETWEEN STR 28R AND 29R.
SKIN CORRODED UNDER EDGE OF DOUBLER AT STA 950E, STR 27R.
EVIDENCE OF CORROSION AT LOWER AFT CORNER CUTOUT STA 990, STR27R.
DOOR FRAME AT BS 950F HAS AREA OF CORROSION ABOVE STR 27R ON WEB.
INTERCOSTAL CORRODED AT STR 28R BETWEEN STA 950F AND 970.
LT RAM AIR INLET LOWER FUSELAGE SKIN BULGED STA 720A. CORROSION FOUND AT STRINGER AT KEELBEAM.
EXIT LIGHT INOP ABOVE L2 DOOR.
STRINGER 30R CCORRODED ON LOWER SIDE AT BS 1013.
SHEAR TIE CORRODED AT STA 420 BETWEEN STR 28L AND 28R.
CENTER CABIN EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK.
STA. 680, STR 23R TO 24R, FRAME DENTED
LBL 44, SEAT TRACK CROWN CORRODED FROM STA 760 TO 848.
1/2 INCH CRACK IN FRAME AT STA 580 ABOVE FWD SERVICE DOOR.
UPPER FLOORBEAM CORRODED FS 1070, LBL 56.
RBL 16, STA 350, BILGE AREA, LOWER CHORD CORRODED.
SHEAR TIE CORRODED STA 350 FROM RBL 19 TO RBL 24.
STA 340, RBL 19 TO RBL24, FRAME CORRODED
STA 660, STRINGER 24R, FRAME DENTED.
FRAME AT STA 26 LEFT DENTED.
STA 1130, RBL 51, FLOORBEAM CHORD CORRODED.
FRAME AT STATION 950 DENTED.
TOP OF ELEVATOR HINGE CHORD CORRODED FROM STA 70 THRU 170.
FRAME AT STATION 950 DENTED.
'T' CHORD AT STA 350 CORRODED.
FLOOR BEAM UPPER CHORD CORRODED AT NUTPLATE.
VERTICAL ANGLE CORRODED.
WEB CORRODED AT BS 1213 WL 177 RBL 5.
TRANSVERSE BEAM AT TAIL SKID CORRODED.
HAT CHANNEL CORRODED
TAIL SKID TRANSVERSE BEAM FWD ATTACH ANGLE CORRODED.
FLOOR SUPPORT CORRODED.
SUB FLOOR CORRODED
LOWER BEAM CORRODED.
UNDER FLOOR WEB CORRODED.
SUBFLOOR WEB CORRODED AFT LAV.
FLOOR SUPPORT EXTRUSION CORRODED.
SEAT TRACK CORRODED.
SEAT TRACK CORRODED.
VERTICAL WEB CRACK AT LIGHTNING HOLE.
SEAT TRACK FLANGE CORRODED.
SEAT TRACK CORRODED BS 1130.
SEAT TRACK FLANGE CORRODED.
SEAT TRACK CORRODED.
ELEVATOR UPPER HINGE CORD CORRODED.
FLOORBEAM WEB DAMAGED BELOW UPPER CHORD, STA 460, RBL-25.
DENT IN SKIN STA 328 ABOVE FWD ENTRY DOOR
SEAT TRACK CROWN AND FLANGE CORRODED
SEAT TRACK CROWN CORRODED.
SEAT TRACK CORRODED.
SEAT TRACK CROWN CORRODED.
LEFT WING REAR SPAR VERTICAL STIFFENER CORRODED AT LOWER END W.S. 200
DURING FLIGHT, ALL 8 RT READING STATION CB`S POPPED SIMULTANEOUSLY. PA INOPERATIVE ALL STATIONS. NO SMOKING CB POPPED, PASSENGER AND CREW CALL CB POPPED. ATTEMPTED TO RESET CB`S IAW AOM PROCEDURES. CB`S IMMEDIATELY POPPED. DID NOT ATTEMPT TO RESET, AGAIN. ON POST FLIGHT INSPECTION FOUND 28V DC BATTERY CHARGER CB POPPED. REPLACED APPROXIMATELY 80 BURNED WIRE SEGMENTS BEHIND FWD GALLEY BY DOUBLE SPLICING IAW SWP 20-30-12 AND REPAIRS IAW SWP 20-10-13. ALL SYSTEMS OPS CHECKED GOOD IAW MM. (K)
DURING PREFLIGHT TRANSIT FOUND WHITE EMERGENCY DOOR LIGHTS AT L-2 AFT DOOR VERY WEAK. REMOVED AND REPLACED POWER SUPPLY BATTERY CHARGER ASSY. OPS CHECK OK IAW MM 33-50-02. (SDR040010)