N331CK
Registered owner: KALITTA CHARTERS II LLC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| KALITTA CHARTERS II LLC (K11A) | Operator | 2018-07-03 – 2018-07-03 | Operator named in NTSB report |
| Kalitta Charters Ii Llc | Operator | 2018-07-03 – 2018-07-03 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 344 AND STA 360 LBL 44" HAS EVIDENCE OF CORROSION UNDERNEATH FLANGE ( APPROX 4" IN LENGTH).
FLOOR BEAM @ STA 344 LBL 44" (APPROX 6" IN LENGTH) HAS EVIDENCE OF CORROSION UNDERNEATH FLANGE AND ATTACHMENT HOLES.
FUSELAGE FLOOR STRUCTURE - FRAME @ STA 727 A CRACKED JUST ABOVE STRINGER 17L
FUSELAGE FLOOR STRUCTURE - INTERCOASTAL @ STA 344 LBL 11" HAS EVIDENCE OF CORROSION
BS 908, STR 4L CRACKED AT 2EA FASTNER HOLES COMMON TO BUT SPLICE STRAP.
FUSELAGE FLOOR STRUCTURE - FLOOR BEAM @ STA 294 FROM LBL 8" TO RBL 12" (FROM 0L R/H TO L/H) ON TOP AND UNDERNEATH ATTACHMENT HOLES.
FUSELAGE FLOOR STRUCTURE - FLOOR BEAM @ STA 302 RBL 45" HAS EVIDENCE OF CORROSION
FUSELAGE FLOOR STRUCTURE - FLOOR BEAM AT STA 328 OBL OUT TO LBL 60" AND RBL 60" EVIDENCE OF CORROSION ON TOP AND UNDERNEATH ATTACHMENT HOLES.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK AT STA 420 RBL 26" (APPROX) HAS EVIDENCE OF CORROSION.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 767 AND STA 807 LBL 60" (APPROX 30" IN LENGTH) HAS EVIDENCE OF CORROSION.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 727E AND STA 767 0BL (APPROX 24" IN LENGTH) HAS EVIDENCE OF CORROSION.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK AT STA 500C RBL 26" HAS EVIDENCE OF CORROSION.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 807 & STA 827 RBL 60" HAS EVIDENCE OF CORROSION.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 767 & STA 787 RBL 60" HAS EVIDENCE OF CORROSION.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 767 AND STA 727E LBL 60" ( APPROX 35" IN LENGTH) HAS EVIDENCE OF CORROSION.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 767 AND STA 747 RBK 60" (APPROX 5" IN LENGTH) HAS EVIDENCE OF CORROSION.
FUSELAGE FLOOR STRUCTURE - FLOOR SUPPORT @ STA 907 LBL 62" HAS EVIDENCE OF CORROSION
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 827 AND STA 847 RBL 44" HAS EVIDENCE OF CORROSION.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 807 AND STA 827 RBL 46" (APPROX 19" IN LENGTH) HAS EVIDENCE OF CORROSION.
EVIDENCE OF CORROSION ON SEAT TRACK AT STA 5D-480 46 INCHES LEFT OF 0-BL.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 847 & STA 867 RBL 27" EVIDENCE OF CORROSION.
EVIDENCE OF CORROSION ON SEAT TRACK AT STA 500 60 INCHES RIGHT OF 0-BL.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK @ STA 827 RBL 60" HAS EVIDENCE OF CORROSION.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 867 AND STA 847 LBL 25" HAS EVIDENCE OF CORROSION.
FUSELAGE FLOOR STRUCTURE - SEAT TRACK BETWEEN STA 887 AND STA 867 LBL 58" HAS EVIDENCE OF CORROSION.
L1 WINDOW HEAT CAUSED DELAMINATION RESULTING IN CRACKS. R&R L1 WINDOW IAW B737 AMM 56-11-11 NO DEFECTS NOTED. PER COMPANY REQUEST R&R L1 WINDOW HEAT CONTROLLER IAW B737 AMM 30-41-11 OPS CHECK GOOD
CRACK ON LT AFT BELLY JUST AFT OF WING TO BODY FAIRING BETWEEN STA 767-787 ABOVE STR L 25.
TWO CRACKS ON LT AFT BELLY JUST AFT OF WING TO BODY FAIRING.
L/H MLG AFT SUPPORT FITTING CRACKED
LEFT WING SKIN CORROSION WBL 15
L/H REAR SPAR HAS CRACK IN 1EA FASTENER HOLE AT RSS 224
CRACK NOTED ON UPPER SKIN T/E FASTENER HOLE @ RSS 270 ON R/H WING
R/H REAR SPAR UPPER CHORD CRACKED, R&R REAR CHORD BETWEEN RSS 1.5.24 TO RSS 285
R/H MLG SUPPORT FITTING CRACKED
ON TAKEOFF ROLL NR 1 GENERATOR WENT OFF LINE, REJECTED TAKEOFF. R&R THE NR 1 GENERATOR, NR 1 CSD, IAW AMM 24-21-11, AND 24-11-11. OPS AND LEAK CHECK GOOD IAW AMM 24-11-11 AND AMM 71-00.
BS 639 LBL 45.5 WL 204 FLOORBEAM WEB CRACKED @ 1 LOWER FASTENER
AT FL 350 THE CABIN ALTITUDE HORN SOUNDED, THE CABIN CLIMBED ABOVE 10,000 FT AND CONTINUED TO CLIMB WITH THE OUTFLOW VALVE CLOSED. FOUND DEBRIS IN FORWARD CARGO PIT DOOR, REMOVED DEBRIS, PERFORMED PRESSURIZATION CONTROL SYSTEM, OP'S CHECK GOOD IAW AMM 21-31-00. NO DEFECTS NOTED.
CRACKED FRAME, BS 312 LT ABOVE THE L1 DOOR.
CRACKED FRAME, BS 312 LT ABOVE THE L1 DOOR
R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE.
SHEAR TIE BS 986, 27L & 27R HAS DAMAGED FASTENER HOLES
CORROSION UNDERSIDE OF SEAT TRACK FLANGE AT BS 727+6, LBL 45.5
SHEAR TIE STA 927 RBL 9 SHOWS CORROSION
CORROSION ON THE SEAT TRACK FROM BS 727+6 - 727B, RBL 25.
CORROSION ON THE FLOOR SUPPORT AT BS 727+6 - 727B, RBL 25.
CORROSION ON THE OTBD FLANGE OF THE SEAT TRACK AT BS 717, LBL 60.
CORROSION ON THE OTBD FLANGE OF THE SEAT TRACK AT BS 790, LBL 60.
AFT CARGO DOOR CUTOUT LOWER FWD CORNER BS 800, STRINGER 24R HAS SKIN CRACKED.
UPPER SIDE OF LOWER TEE OF THE MAIN DECK FLOORBEAM HAS CORROSION AT BS 827, RBL 55.
UPPER SIDE OF LOWER TEE OF MAIN DECK FLOORBEAM HAS CORROSION AT BS 807, RBL 55.
LEFT WING LOWER SURFACE WS 453 HAS CORROSION BEHIND THE NR 2 SLAT OTBD TRACK.
BS 867, LBL 32 TO RBL 60 ON LOWER FLOORBEAM IN THE AFT CARGO BAY CORROSION
RIGHT NACELLE AT NS 222 ACCESS PANEL IS CRACKED
AFT CARGO DOOR LOWER SILL, CORRODED BENEATH LOWER SILL ON WEB & FASTENERS
CORROSION ON UPPER SILL PLATE ANGLE OF AFT CARGO DOOR SURROUND.
BARE METAL ON LOWER SIDE OF AFT CARGO FLOOR SUPPORT BS 750, LBL 8.
CORROSION ON SPLICE PLATE ABOVE AFT CEILING PANEL, BS 917, BL 0.
LOWER AFT SIDE OF FLOORBEAM, BS 727E, LBL 60 UPPER TEE CORRODED.
AFT CARGO BS 727E, RBL 30, FLOOR SUPPORT CORRODED.
CRACK IN CIRCUMFERENTIAL FRAME IN AFT PIT JUST UNDER FLOOR SUPPORT BS 727, BL 0.
CORROSION ON FLOOR SUPPORT BS 720 - 727 + 10, LBL 45.5.
CORROSION ON INSIDE OF SKIN BS 970. STRINGER 27R
LOWER SIDE OF MAIN DECK FRAME IN MULTIPLE SPOTS, BS 727B LBL 55 TO RBL 55 CORRODED.
CORROSION ON LOWER SIDE OF SEAT TRACK BS 727A, RBL 45
CORROSION ON LOWER SIDE OF SEAT TRACK.
LOWER BEARSTRAP UNDER AFT CARGO FLOORBOARD BS 727, STRINGERS 27L TO 23L CORRODED
INTERCOSTAL STA 727 IN AFT PIT LBL 20, 24" ABOVE FLOOR BOARD 2" CRACK.
AFT PIT STA 727E LBL 1 CORROSION AROUND NUT PLATE.
CRACK ABOVE LAP JOINT ON EXTERIOR SKIN AT STA 747 STR 25R.
SPLICE ANGLE UNDER MAIN DECK FLOOR BOARD STA 1000 RBL 42.
CRACK NEAR LAP JOINT AT STA 520 LT SIDE ABOVE WINDOW PLUG.
MAIN DECK UNDER FLOOR BOARD HAS SUPPORT STRAP AT 1006 - 1016 RBL 27.
MAIN DECK UNDER FLOOR BOARD HAS SUPPORT FRAME AT STA 1016 RBL 36.
SEAT TRACK SECTION ON MAIN DECK SEAT TRACK LINK AT STA 520-540 LBL 24.75.
R & R FUSELAGE SKIN FROM STA 907 - 1016 STR 25L -25R.
CORROSION ON WEB, BS 947.5, STRINGER 26R.
STRING 27R HAS CORROSION AT STA 975.
R1 DOOR EXTERIOR SKIN AT LOWER AFT HINGE CUTOUT CRACKED.