GULF AND CARIBBEAN CARGO, INC.

Operated by Gulf and Caribbean Cargo, Inc. (per NTSB report)

The flight crew failed to verify that the cargo was secured before takeoff.

Operated by GULF AND CARIBBEAN CARGO, INC. (per NTSB report)

Sanction: $4,500 · case closed 2023-11-03

Sanction: $4,538 · case closed 2018-10-24

Sanction: $40,000 · case closed 2015-05-21

Sanction: $6,000 · case closed 2015-07-21

Part: FLOOR PANEL — CRACKED (ZONE 100) · airframe 27,145 hrs · 25,186 cycles

CRACK IN FORWARD ELECTRONICS BAY FLOOR PANEL AT STA 193.00 LH SIDE.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R

Part: FRAME — DENTED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD DENTS AT BS 1130 BETWEEN STRINGER 24R AND 28R

Part: FRAME — DENTED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD DENT AT BS 1148 BETWEEN STRINGER 25R AND 28R

Part: FRAME — CRACKED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD CRACK AT BS 640 BETWEEN STRINGER 28L AND 27R

Part: FRAME — CRACKED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD CRACK AT BS 660 BETWEEN STRINGER 27L AND 27R

Part: FRAME — DENTED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD DENTED AT BS 1050 BETWEEN STRINGER 25L AND 28L

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 43,469 hrs · 25,021 cycles

FUSELAGE TRANSVERSE FLOOR BEAM UPPER FLANGE CORROSION DAMAGE AT BS 740 BETWEEN LBL 45 AND LBL 62

Part: BEAM — CORRODED (ZONE 300) · corrosion level 2 · airframe 43,469 hrs · 25,021 cycles

R/H SIDE H-STAB. TRAILING EDGE BEAM UPPER SURFACE CORROSION REPAIRED BY REPLACEMENT OF R/H TRAILING EDGE UPPER BEAM ENTIRE LENGTH BETWEEN ELEVATOR STATION 10 AND ELEVATOR STATION 209.90 I.A.W BOEING DRAWING 65-22987, SHEET 5, REVISION C.

Part: SKIN PANEL — DAMAGED (ZONE 300) · airframe 43,469 hrs · 25,021 cycles

R/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANEL 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R.

Part: FRAME — PUNCTURED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1070 BETWEEN STRINGER 26L AND 29L

Part: SKIN — DENTED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE SKIN GOUGE/DENT REPAIRED BELOW MCD BETWEEN BS 460 AND BS 620, AND BETWEEN STRINGER 15L-20L

Part: FRAME — PUNCTURED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1090 BETWEEN STRINGER 26L AND 28L

Part: FRAME — GOUGED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD GOUGED AT BS 1110 BETWEEN STRINGER 26L AND 28L

Part: FRAME — GOUGED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD GOUGED AT BS 1130 BETWEEN STRINGER 26L AND 28L

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FLOOR STABILIZER BEAM MULTIPLE SPOTS CORROSION AT BL 0 BETWEEN BS 449.94 AND BS 720+9.94

Part: FRAME — DENTED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD DENT AT BS 1050 BETWEEN STRINGER 26R AND 28R

Part: FRAME — DENTED (ZONE 100) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD DENT AT BS 1070 BETWEEN STRINGER 25R AND 29R

Part: FRAME — PUNCTURED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1090 BETWEEN STRINGER 26R AND 28R

Part: FRAME — PUNCTURED (ZONE 200) · airframe 43,469 hrs · 25,021 cycles

FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1110 BETWEEN STRINGER 25R AND 28R.

Part: SKIN PANEL — DAMAGED (ZONE 300) · airframe 43,469 hrs · 25,021 cycles

RIGHT HORIZONTAL STABILIZER UPPER T/E DAMAGED PANELS 65-20658-24 BETWEEN ELEV. STA. 99.79 AND 173.21 REPAIRED AND INSTALLED IAW. R24-02464-001, REVISION 6 ,DATE OCTOBER 03.2025.

Part: SKIN PANEL — DAMAGED (ZONE 300) · airframe 43,469 hrs · 25,021 cycles

R/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANELS 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21 REPAIRED AND INSTALLED I.A.W. V1 AEROSPACE DOC. NO. R24-02464-001, REVISION 6 ,DATE OCTOBER 03.2025

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

CENTER FUSELAGE SECTION RH DELTA BEAM LOWER CHORD CORRODED FROM BS720F-755 AND S-27L TO S-27R

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

AFT LOWER FUSELAGE SKIN PANEL CORROSION FROM BS1148-1166 AND S-18L TO S-20L.

Part: FLAP TRACK — CRACKED (ZONE 500) · airframe 44,542 hrs · 25,488 cycles

CRACK FOUND ON LEFT WING OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP TRACK. CRACK WAS IN UPPER FLANGE INBOARD FLANGE.

Part: SPAR — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

WING CENTER BOX FRONT SPAR CORRODED IN MULTIPLE PLACES ON VERTICAL AND HORIZONTAL CHORD FLANGES AT BS740 FROM LBL70.5 TO RBL70.5

Part: SHEAR WEB — CRACKED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles

AFT UPPER FUSELAGE FLOOR SHEAR WEB CRACK NEAR BS1166-1176.9 AND RBL8 TO RBL17.87

Part: SKIN PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

AFT LOWER FUSELAGE SKIN CORROSION FROM BS990-1010 AT S-26L

Part: FRAME — CRACKED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles

FORWARD LOWER FUSELAGE FRAME UPPER CHORD CRACKED AT BS700 FROM S-28L TO S-28R

Part: FRAME — CRACKED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles

FT LOWER FUSELAGE FRAME CRACKED AT BS1070 FROM S-26R TO S-28R

Part: FRAME — PUNCTURED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles

AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1130 FROM S-25L TO S-29L.

Part: FRAME — PUNCTURED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles

FRAME INNER CHORD PUNCTURE AT BS 1090 BETWEEN S26R AND S28R.

Part: FRAME — PUNCTURED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles

AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1090 FROM S-24L TO S-28L

Part: FRAME — DENTED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles

AFT LOWER FUSELAGE FRAME INNER CHORD DENTED AT BS1110 FROM S-24L TO S-28L

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

CORROSION ON FUSELAGE SKIN AT BS1028 TO 1055 AND S-29L TO S-29R

Part: SPAR — CORRODED (ZONE 300) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

CORROSION ON RH HORIZONTAL STAB REAR SPAR UPPER CHORD AT STAB STATION 104.25 THRU 123.25 AND 141.5 THRU 160.5

Part: NONE — NONE (NONE) · airframe 44,542 hrs · 25,488 cycles

BMS3-27 IS NO LONGER PROCURABLE. BOEING SR KFC-GUC-24-0105-09B APPROVED THE USE OF BMS3-38 AS AN ALTERNATE.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

AFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORROSION AT BS1148 FROM LBL45 TO LBL55

Part: STRUCTURE — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

CORROSION AT MULTIPLE LOCATIONS AT A-NUT ATTACHMENTS. FORWARD LOWER FUSELAGE LONGITUDINAL STABILIZER LOWER CHORD REPAIRED AT BL0 FROM BS450-660

Part: WINDOW FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

AFT UPPER FUSELAGE WINDOW FRAMES CORROSION FROM BS950A-950C AND S-10R TO S-14R

Part: FRAME — PUNCTURED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles

AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1148 FROM S-25R TO S-28R.

Part: VERTICAL BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

VERTICAL BEAM CORRODED AT LOWER END. REPAIRED AT BL 0 BS 1183.

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

AFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORRODED AT BS1030 FROM LBL10 TO LBL20.

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 44,542 hrs · 25,488 cycles

NON-PRODUCTION FASTENERS INSTALLED .AFT LOWER FUSELAGE FRAME REPAIRED AT BS1050 FROM S-25L TO S-28L

Part: BEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

RIGHT OTBD END OF THE SIDELOAD BEAM CORRODED. CENTER FUSELAGE BULKHEAD SIDELOAD BEAM CORRODED AT BS740 FROM LBL30 TO RBL30

Part: BEAR STRAP — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

CORROSION ON BEAR STRAP, DOUBLER, AND FUSLAGE EXTERNAL SKIN AT AFT CONER OF AFT CARGO DOOR FROM FS965 TO FS1010 AND STR S-21R TO S-29L

Part: SKIN — CRACKED (ZONE 600) · airframe 44,542 hrs · 25,488 cycles

CRACKED AT THE SLAT HOOK CUT-OUT IN THE AFT CORNER. AT WS 519 ON THE RIGHT WING

Part: SPAR WEB — ELONGATED (ZONE 500) · airframe 44,542 hrs · 25,488 cycles

ELONGATED HOLE ON VERTICAL STIFFENER WEB IN CENTER FUEL TANK FRONT SPAR AT LBL40

Part: KEELBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 44,542 hrs · 25,488 cycles

KEEL BEAM BREATHER WEB CORRODED AT SEVERAL LOCATIONS ON THE UPPER SURFACE FROM BS740 TO 795 AND LBL13 TO RBL13