N422BN
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
Maintenance disclosures
STRINGER 24L HAS CORROSION AT BS 735.
STRINGER 29R AT BS 1000 UPPER FLANGE CRACKED.
HORIZONTAL WEB INBD ATTACH ANGLE AT BS 299, LBL 16 CORRODED.
SHEAR TIE CORRODED AT BS 985 STUB FRAME BETWEEN STRINGER 28-29R.
STRINGER 29L HAS CORROSION BETWEEN BS 950D AND 950E.
STRINGER 29R HAS CORROSION BETWEEN BS 950D AND 950E.
STRINGER 30L HAS AREAS OF CORROSION BETWEEN BS 950A AND 950C.
HORIZONTAL WEB INBD ATTACH ANGLE CORRODED AT BS 300, RBL16.
MAIN DECK FLOOR SUPPORT AT BS 1177, RBL 3, HAS AREA OF CORROSION.
STRINGER 29L HAS AREAS OF CORROSION BETWEEN BS 970 AND 990.
EVIDENCE OF CORROSION AT SKIN DOUBLER AT STRINGER 26L BETWEEN BS 1160 AND 1180.
STRINGER 29L HAS AREAS OF CORROSION BETWEEN BS 950E AND 950F.
STRINGER 29R CORRODED AT BS 1000.
NR 2 ENGINE S-DUCT HAS CORROSION ON INTERNAL SKIN BETWEEN RIB 16-17 AT 6 O'CLOCK POSITION.
AT PRODUCTION BREAK SPLICE IN S-DUCT AT BS 1243 BOTTOM SIDE BETWEEN RIB 16 AND 17 SPLICE REPAIR DAMAGED.
SHEAR TIE CORRODED AT BS 1010 BETWEEN STRINGERS 29-30L.
NR 2 ENGINE S-DUCT INTERNAL SKIN BULGING AT RIB 22 AT 6 O'CLOCK POSITION.
HORIZONTAL WEB INBD ATTACH ANGLE CORRODED AT BS 348, RBL16.
INTERCOSTAL AT STRINGER 20R HAS CORROSION HAS CORROSION AT BS 360 - 380.
RBL 46, SEAT TRACK CORRODED AT STA 1080-1090.
RBL 46, SEAT TRACK HAS AREAS OF CORROSION BETWEEN STA 1090 TO 1130.
RBL 24, STA 1110 SEAT TRACK CORRODED.
LBL 24, STA 1135, SEAT TRACK CORRODED.
BS 1070, LBL 26, FLOORBEAM UPPER CAP CORRODED.
BS 1070, LBL 12, FLOORBEAM UPPER CAP CORRODED.
LEFT FLOOR WEB, STA 1157, LBL 48 HAS AREAS OF CORROSION.
RIGHT FLOOR WEB, BS 1170, HAS AREAS OF CORROSION.
BS 1130 RBL 21, UPPER FLOORBEAM CAP CORRODED UNDER WEB.
INTERNAL SKIN, CORRODED AT STA 796, STRINGER 4L.
BS 1030 TO 1110, RBL 24, SEAT TRACK HAS AREAS OF CORROSION.
BATTERY PACK FAILED FUNCTION TEST, STA 760.
FUSELAGE SKIN, EXTERNAL, HAS A BULGE AND PULLING FASTENERS AT STA 1148, BETWEEN STRINGER 24R AND 27R.
CORROSION ON FUSELAGE SKIN AFT OF BS 540, INBD OF STRINGER 27R
CORROSION FOUND AROUND FASTENERS ON RT WING L/E WING STATION 277.
CORROSION FOUND AROUND FASTENERS ON RT WING, L/E AT WING STA 320.
CORROSION ON SKIN OTBD OF STRINGER 27R FWD OF BS 720C.
FUSELAGE SKIN OIL CANNING STA 660-680 BETWEEN STRINGER 21R AND 22R.
CTR WING SKIN CORRODED AT STRINGER 3C, LBL 17 INSIDE LT RAM AIR DUCT.
LOWER CTR WING SKIN CORRODED AT STRINGER 6C, LBL 30 INSIDE LT RAM AIR DUCT.
CORROSION ON SKIN UNDER STRINGER 27R FROM 720A TO 720B+10".
STRINGER CLIP CORRODED AT STRINGER 30, BS 950A.
R1 DOOR CREASED BS 385-410 BETWEEN STR 14R AND 16R.
STRINGER 25R SPLICE CORRODED BETWEEN BS 660 AND 680.
STRINGER 24L DAMAGED AT STA 430.
FUSELAGE FRAME CRACKED 1.5", BEYOND REPAIR, CUTOUT ABOVE STRINGER 27R AT BS1090.
EMERGENCY PATH LIGHTING INOP FROM ROW 14 TO ROW 23.
L2 DOOR EMERGENCY EXIT LIGHT INOP.