KALITTA AIR LLC

Operated by KALITTA AIR LLC (per NTSB report)

The fatigue failure of multiple hinge ribs associated with the right outboard aileron, which resulted in abnormal aileron movement and airframe vibration. Contributing to the failure was the mis-rigged condition of the right outboard aileron, which increased operational loads on the hinge fittings during cruise flight.

Operated by KALITTA AIR LLC (per NTSB report)

Operated by KALITTA AIR LLC (per NTSB report)

Incorrect lubrication of the foreflap fitting assembly.

Operated by Kalitta Air (per NTSB report)

An unavoidable collision with a garbage dumpster that had blown into the path of the airplane during the takeoff roll.

Operated by KALITTA AIR (per NTSB report)

Operated by KALITTA AIR LLC (per NTSB report)

An engine fire in the No. 3 engine due to the failure of, and subsequent flammable fluid leak from, one of three fuel or hydraulic lines located in the engine's accessory raceway that ignited when the fluid came in contact with the hot engine cases. Contributing to the incident were the lack of adequate inspection and test requirements and appropriate life limit or inspection interval requirements by the manufacturer.

Operated by Kalitta Air (per NTSB report)

The pilot's failure to verify the extension of the landing gear prior to landing, and his failure to perform the emergency landing gear extension procedure. The popped circuit breaker was a factor.

Sanction: $9,075 · case closed 2018-06-18

Sanction: $24,000 · case closed 2013-08-05

Sanction: $8,000 · case closed 2012-09-24

Sanction: $6,000 · case closed 2008-12-15

Sanction: $32,500 · case closed 2009-08-28

Sanction: $5,000 · case closed 2008-02-12

Sanction: $12,000 · case closed 2006-05-16

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 91,962 hrs · 15,814 cycles

MAIN ENTRY L1 DOOR FWD EMERGENCY LIGHT INOPERATIVE.

Part: SEAL — LEAKING (FO WINDOW) · airframe 70,414 hrs · 12,782 cycles

FO WINDOW SEAL NOISY. CLEANED AND INSPECTED R2 WINDOW SEAL IAW BOEING SOPM 20-30-03 AND B777-200/300 AMM 56-11-13. ALL CHECKS GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

UPPER DECK SEAT TRACK APPROX RBL 40 STA 450 HAS EVIDENCE OF CORROSION

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

POSSIBLE CORROSION ON STRINGER 49L IN AFT CARGO AT BS 1860 - 1880.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

POSSIBLE CORROSION ON STRINGER 48L IN AFT CARGO AT BS 1920-1940.

Part: SPLICE PLATE — CORRODED (ZONE 600) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

EVIDENCE OF CORROSION ON RT WING IN L/E CAVITY APPROX WS 1454 TWO INCHES FWD OF FRONT SPAR

Part: STRINGER — CRACKED (ZONE 200) · airframe 110,074 hrs · 18,726 cycles

UPPER DECK R/H SIDE STRINGER 8R UPPER SURFACE HAS POSSIBLE CRACK BY HILOK FASTENER JUST FWD OF BODY FRAME 460

Part: PANEL — CRACKED (ZONE 200) · airframe 110,074 hrs · 18,726 cycles

L/H CANTED PRESSURE DECK COMPOSITE PANEL STA 1240 LBL 70-80 DAMAGED

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

FLIGHT DECK FLOORBEAM UPPER SURFACE CORRODED AT WEB SEAM BS 330 LBL 41 TO RBL 41.

Part: TENSION TIE — CRACKED · airframe 110,074 hrs · 18,726 cycles

2 EACH CRACK INDICATIONS IN FASTENER HOLES IN THE FRAME COMMON TO THE TENSION TIE AT STA 1160 R/H SIDE

Part: TENSION TIE — CRACKED (ZONE 100) · airframe 110,074 hrs · 18,726 cycles

INNER FRAME DOUBLER CRACKED AT STA 1160 R/H

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

UPPER DECK SEAT TRACK FOUND TO BE CORRODED AT STA 720-780 LBL 30

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

UPPER DECK SEAT TRACK CORRODED AT STA 720 LBL 24

Part: STIFFENER — CORRODED (ZONE 600) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

EVIDENCE OF CORROSION ON R/H WING IN L/E CAVITY ON FWD SPAR STIFFENER APPROX WS 1513

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

UNDER SIDE OF PANEL SUPPORT HAS CORROSION IN AFT BULK CARGO COMPARTMENT APPROX STA 2160 RBL 38-48

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

UNDERSIDE OF FLOOR PANEL SUPPORT HAS CORROSION IN AFT BULK CARGO COMPARTMENT APPROX STA 2160 LBL 5-12

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

UNDER SIDE OF PANEL SUPPORT HAS CORROSION IN AFT BULK CARGO COMPARTMENT APPROX STA 2160 RBL 12

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

POSSIBLE CORROSION ON S-49L IN AFT CARGO AT STA 1860-1880.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

POSSIBLE CORROSION ON S-48L IN AFT CARGO AT BS 1920-1940

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

CORROSION FOUND AT BS 1965 ON STRINGER 51R.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 110,074 hrs · 18,726 cycles

EMERGENCY LIGHT POWER SUPPLY AT APPROX STA 830 BEHIND GALLEY FAILS OPS CHECKED

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 110,074 hrs · 18,726 cycles

L/H SIDE UPPER DECK DOOR BATTERY HAS LOW VOLTAGE

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

LEFT WING FUEL TANK ACCESS CUTOUT 553BB HAS CORROSION

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

LEFT WING FUEL TANK ACCESS CUTOUT 553EB HAS CORROSION

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

LEFT WING FUEL TANK ACCESS CUTOUT 545BB HAS CORROSION

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

LEFT WING FUEL TANK ACCESS CUTOUT 546AB HAS CORROSION

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

LEFT WING FUEL TANK ACCESS CUTOUT 546BB HAS CORROSION

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

LEFT WING FUEL TANK ACCESS CUTOUT 552EB HAS CORROSION

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

LEFT WING FUEL TANK ACCESS CUTOUT 553GB HAS CORROSION

Part: ACCESS PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

LEFT WING FUEL TANK ACCESS CUTOUT 545AB HAS CORROSION

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

UPPER DECK SEAT TRACK APPROX RBL 40 STA 450 HAS EVIDENCE OF CORROSION

Part: BEAM — CRACKED (FUEL CELL) · airframe 110,074 hrs · 18,726 cycles

CENTER WING TANK INTERIOR NR 2 SPANWISE BEAM WEB HAS POSSIBLE CRACK AT APPROX LBL 90

Part: ANGLE — CRACKED (ZONE 400) · airframe 110,074 hrs · 18,726 cycles

CRACKED ANGLE AT NAC 354 IN LOWER AFT TORQUE BOX # 2 PYLON

Part: TENSION TIE — CRACKED · airframe 110,074 hrs · 18,726 cycles

VISIBLE CRACK APPROX 2 INCHES LONG FOUND IN LT SIDE OF TENSION TIE AT STA 1160

Part: STIFFENER — CORRODED (ZONE 600) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

EVIDENCE OF CORROSION ON RT WING IN L/E CAVITY ON FWD SPAR STIFFENER APPROX WS 1513

Part: TENSION TIE — CRACKED · airframe 110,074 hrs · 18,726 cycles

TENSION TIE AT STA 1120 FOUND TO HAVE CRACK INDICATION AT I/B FASTENER HOLE COMMON WITH L/H SIDE FRAME

Part: STRINGER CLIP — CRACKED · airframe 110,074 hrs · 18,726 cycles

O/B FASTENER HOLE WITH POSSIBLE CRACK INDICATION FOUND AT STA 1120 COMMON WITH FRAME, STRINGER CLIP AND TENSION TIE

Part: TENSION TIE — CRACKED · airframe 110,074 hrs · 18,726 cycles

FOUND 2EA CRACK INDICATIONS IN FASTENER HOLES AS MARKED AT STA 1160 TENSION TIE TO FRAME ATTACHMENT LOCATIONS L/H

Part: TENSION TIE — DAMAGED · airframe 110,074 hrs · 18,726 cycles

TENSION TIE AT STA 1120 RT SIDE HAS DAMAGED FASTENER HOLE

Part: TENSION TIE — CRACKED (ZONE 200) · airframe 110,074 hrs · 18,726 cycles

CRACK INDICATIONS FOUND ON FRAME DOUBLER AT STA 1160 L/H, S-10L

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 110,074 hrs · 18,726 cycles

CRACK FOUND AT INTERCOSTAL BL 0 L/H OUTER FLANGE STA 306

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 110,074 hrs · 18,726 cycles

CRACK FOUND AT INTERCOSTAL BL 0 RT OUTER FLANGE STA 339

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 110,074 hrs · 18,726 cycles

CRACK FOUND AT INTERCOSTAL BL 0 R/H OUTER FLANGE STA 310.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 110,074 hrs · 18,726 cycles

CRACK FOUND AT INTERCOSTAL BL 0 LT OUTER FLANGE BS 326.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 110,074 hrs · 18,726 cycles

CRACK FOUND AT INTERCOSTAL BL 0 L/H OUTER FLANGE STA 310

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 110,074 hrs · 18,726 cycles

CRACK FOUND AT INTERCOSTAL BL 0 L/H OUTER FLANGE STA 323

Part: INTERCOSTAL — CRACKED · airframe 110,074 hrs · 18,726 cycles

CRACK FOUND AT INTERCOSTAL BL 0 RT INNER FLANGE BS 337

Part: WEB — CRACKED (ZONE 100) · airframe 110,074 hrs · 18,726 cycles

CRACKED WEB BELOW BULK PIT FLOOR AT STA 2060 RBL 25

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

MAIN DECK STA 2220-2240 RBL 90 EVIDENCE OF CORROSION. ( SEAT TRACK)

Part: FITTING — CORRODED (BULKHEAD) · corrosion level 2 · airframe 110,074 hrs · 18,726 cycles

POSSIBLE CRACK INDICATION IN BOLT HOLE COMMON WITH OUTER CHORD OF RT SIDE BS 2598 BULKHEAD AT WL 321 FOUND DURING OPEN HOLE HFEC INSPECTION.