GULF AND CARIBBEAN CARGO, INC.
Also recorded as: GULF AND CARIBBEAN AIR, GULF AND CARIBBEAN CARGO, INC., IFL GROUP
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
No NTSB accidents or incidents linked to this operator.
FAA enforcement actions
FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal.
217 reports on file — showing most recent 50.
CRACK IN FORWARD ELECTRONICS BAY FLOOR PANEL AT STA 193.00 LH SIDE.
FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R
FUSELAGE FRAME INNER CHORD DENTS AT BS 1130 BETWEEN STRINGER 24R AND 28R
FUSELAGE FRAME INNER CHORD DENT AT BS 1148 BETWEEN STRINGER 25R AND 28R
FUSELAGE FRAME INNER CHORD CRACK AT BS 640 BETWEEN STRINGER 28L AND 27R
FUSELAGE FRAME INNER CHORD CRACK AT BS 660 BETWEEN STRINGER 27L AND 27R
FUSELAGE FRAME INNER CHORD DENTED AT BS 1050 BETWEEN STRINGER 25L AND 28L
FUSELAGE TRANSVERSE FLOOR BEAM UPPER FLANGE CORROSION DAMAGE AT BS 740 BETWEEN LBL 45 AND LBL 62
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.
R/H HORIZONTAL STABILIZER UPPER T/E DAMAGED PANEL 65-20659-24 BETWEEN ELEV. STA. 99.79 AND 173.21
FUSELAGE FRAME BOTTOM CHORD CORROSION DAMAGE AT BS 970 BETWEEN STRINGER 28R AND 29R.
FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1070 BETWEEN STRINGER 26L AND 29L
FUSELAGE SKIN GOUGE/DENT REPAIRED BELOW MCD BETWEEN BS 460 AND BS 620, AND BETWEEN STRINGER 15L-20L
FUSELAGE FRAME INNER CHORD PUNCTURED AT BS 1090 BETWEEN STRINGER 26L AND 28L
FUSELAGE FRAME INNER CHORD GOUGED AT BS 1110 BETWEEN STRINGER 26L AND 28L
FUSELAGE FRAME INNER CHORD GOUGED AT BS 1130 BETWEEN STRINGER 26L AND 28L
FUSELAGE FLOOR STABILIZER BEAM MULTIPLE SPOTS CORROSION AT BL 0 BETWEEN BS 449.94 AND BS 720+9.94
FUSELAGE FRAME INNER CHORD DENT AT BS 1050 BETWEEN STRINGER 26R AND 28R
FUSELAGE FRAME INNER CHORD DENT AT BS 1070 BETWEEN STRINGER 25R AND 29R
FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1090 BETWEEN STRINGER 26R AND 28R
FUSELAGE FRAME INNER CHORD SCREW DAMAGE AT BS 1110 BETWEEN STRINGER 25R AND 28R.
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.
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
CENTER FUSELAGE SECTION RH DELTA BEAM LOWER CHORD CORRODED FROM BS720F-755 AND S-27L TO S-27R
AFT LOWER FUSELAGE SKIN PANEL CORROSION FROM BS1148-1166 AND S-18L TO S-20L.
CRACK FOUND ON LEFT WING OUTBOARD TRAILING EDGE FLAP, OUTBOARD FLAP TRACK. CRACK WAS IN UPPER FLANGE INBOARD FLANGE.
WING CENTER BOX FRONT SPAR CORRODED IN MULTIPLE PLACES ON VERTICAL AND HORIZONTAL CHORD FLANGES AT BS740 FROM LBL70.5 TO RBL70.5
AFT UPPER FUSELAGE FLOOR SHEAR WEB CRACK NEAR BS1166-1176.9 AND RBL8 TO RBL17.87
AFT LOWER FUSELAGE SKIN CORROSION FROM BS990-1010 AT S-26L
FORWARD LOWER FUSELAGE FRAME UPPER CHORD CRACKED AT BS700 FROM S-28L TO S-28R
FT LOWER FUSELAGE FRAME CRACKED AT BS1070 FROM S-26R TO S-28R
AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1130 FROM S-25L TO S-29L.
FRAME INNER CHORD PUNCTURE AT BS 1090 BETWEEN S26R AND S28R.
AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1090 FROM S-24L TO S-28L
AFT LOWER FUSELAGE FRAME INNER CHORD DENTED AT BS1110 FROM S-24L TO S-28L
CORROSION ON FUSELAGE SKIN AT BS1028 TO 1055 AND S-29L TO S-29R
CORROSION ON RH HORIZONTAL STAB REAR SPAR UPPER CHORD AT STAB STATION 104.25 THRU 123.25 AND 141.5 THRU 160.5
BMS3-27 IS NO LONGER PROCURABLE. BOEING SR KFC-GUC-24-0105-09B APPROVED THE USE OF BMS3-38 AS AN ALTERNATE.
AFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORROSION AT BS1148 FROM LBL45 TO LBL55
CORROSION AT MULTIPLE LOCATIONS AT A-NUT ATTACHMENTS. FORWARD LOWER FUSELAGE LONGITUDINAL STABILIZER LOWER CHORD REPAIRED AT BL0 FROM BS450-660
AFT UPPER FUSELAGE WINDOW FRAMES CORROSION FROM BS950A-950C AND S-10R TO S-14R
AFT LOWER FUSELAGE FRAME INNER CHORD PUNCTURE AT BS1148 FROM S-25R TO S-28R.
VERTICAL BEAM CORRODED AT LOWER END. REPAIRED AT BL 0 BS 1183.
AFT UPPER FUSELAGE TRANSVERSE FLOOR BEAM UPPER CHORD CORRODED AT BS1030 FROM LBL10 TO LBL20.
NON-PRODUCTION FASTENERS INSTALLED .AFT LOWER FUSELAGE FRAME REPAIRED AT BS1050 FROM S-25L TO S-28L
RIGHT OTBD END OF THE SIDELOAD BEAM CORRODED. CENTER FUSELAGE BULKHEAD SIDELOAD BEAM CORRODED AT BS740 FROM LBL30 TO RBL30
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
CRACKED AT THE SLAT HOOK CUT-OUT IN THE AFT CORNER. AT WS 519 ON THE RIGHT WING
ELONGATED HOLE ON VERTICAL STIFFENER WEB IN CENTER FUEL TANK FRONT SPAR AT LBL40
KEEL BEAM BREATHER WEB CORRODED AT SEVERAL LOCATIONS ON THE UPPER SURFACE FROM BS740 TO 795 AND LBL13 TO RBL13
Linked aircraft
No aircraft currently linked.