GLOBAL CROSSING AIRLINES, INC.

Operated by Global Crossing Airlines (per NTSB report)

CORROSION DISCOVERED DURING MAINT CHECK RESULTING IN MAJOR REPAIR: ACCOMPLISHED REPAIR OF RT WING TOP SURFACE JUST OUTBOARD OF OVER WING EXITS IN AREA 1, BETWEEN RIB 2 AND 3, STR 6-7, AND AREA 2, RIB 2-3, STR 11 IAW INSTRUCTIONS PROVIDED IN GLOBALX EO A320-57-251013 AND AIRBUS DOSSIER 81668019/009, 81668019/022; REPAIR INSTRUCTIONS R572-58616 ISSUE M.

PILOT REPORTED MAIN CARGO DOOR LOWER LEFT CORNER DOOR SEAL FRAME DAMAGED DURING LOADING OF CARGO. ACCOMPLISHED REPAIR AND FITTING REPLACEMENT AT LOWER FORWARD CORNER SEAL DEPRESSOR OF MAIN CARGO DOOR CUTOUT CAUSED BY GROUND EQUIPMENT DAMAGE, FWD JAMB INSTALLATION, APPROX STA 490, IAW AIRBUS A320 SRM AND PRECISION ENGINEERING EA 25-3012.

CORROSION ON REAR FUSELAGE SKIN AT AFT LAVATORY VENT OUTLET BETWEEN FR 69 TO FR 70, STG 30 TO STG 32. CLEANED CORROSION, FOUND OUT OF LIMITS CONDITION. PERFORMED HFEC SURFACE AND BOLT HOLE INSPECTIONS. FABRICATED AND APPLIED FILLER AND EXTERNAL DOUBLER REPAIR IAW A321 SRM 53-41-11-300-004, FIGURE 001, REPAIR CATEGORY A.

RIGHT RUDDER FAILS DURING FLIGHT CONTROL CHECK - FOUND BROKEN RUDDER CONTROL CABLE IN AFT SECTION OF TAIL FR71

DURING SCHEDULED MAINTERNANCE, INADVERTANT DEPLOYMENT OF LH OFFWING EVACULATION SLIDE OCCURRED. NO MECHANICAL DEFECTS NOTED AT THIS TIME.

DURING SCHEDULED MAINTERNANCE, FOUND RH OFFWING EVACULATION SLIDE WIRE CONTROL NUT DISCONNECTED. NO MECHANICAL DEFECTS NOTED AT THIS TIME.

INTERMITTENT VIBRATION AND NOISE FWD AIRCRAFT WITH BLOWER EXTRACT OVER RIDE AND BURN SMELL.

CARGO DOOR SEALS WERE INSTALLED INCORRECTLY RESULTING IN A FAILURE TO PRESSURIZE AIRCRAFT

R-1 DOOR CABIN PRESSURE SWITCH WARNING LIGHT CAME ON AND OFF ONCE MOMENTARILY

LOSS OF SYSTEM HYDRAULIC FLUID. REPLACED LEAKING HYDRAULIC HOSE ASSY.

L2 DOOR EMERGENCY EXIT LIGHT INOP

DOOR L1 SLIDE SEMI-DEPLOYED. DOOR OPENED WHILE ARMED.

FAP CIDS CAUTIOPN LIGHT ON "CHECK SLIDE PRESS EXIT L"

EMERGENCY AIR RETURN DUE TO HYD GREEN RSVR LOW LEVEL AFTER TAKE OFF.

DURING WEEKLY CHECK FOUND EPSU 10WL, 11WL, 13WL AT FAULT

DURING DAILY CHECK FOUND DOOR R1 EMERGENCY EXIT MARKING INOP. DURING REMOVAL OF EXIT MARKING FOUND ELECTRICAL CONNECTOR NOT CONNECTED, RECONNECTED AS PER ESPM 20-44-00 NOW WORKING SATIS.

MAIN CABIN FLOOR SUPPORT BEAM Y254 BETWEEN C16-C19 LBL10" HAS CORROSION BEYOND REPAIR LIMITS/ REPLACED

PASSENGER CABIN FWD EMERGENCY EXIT R/H SIDE COVER IS CRACKED

PASSENGER CABIN FWD EMERGENCY EXIT R/H SIDE COVER IS CRACKED

LEFT HAND AFT ASSENGER DOOR (L2) EMERGENCY OPERATION CYLINDER IS DISCHARGED/ PRESSURE ACCUMULATOR WAS SERVICED

MEGAPHONE DOES NOT WORK /REPLACED

MAIN CABIN FLOOR BETWEEN FR14-FR16 AT LBL 20" FOUND SUPPORT BEAM SURFACES SEVERAL AREAS OF CORROSION

MAIN CABIN FLOOR BETWEEN FR18-FR21 AT RBL 30" FOUND SUPPORT BEAM SEVERAL AREAS OF CORROSION

MAIN CABIN FLOOR BETWEEN FR17-FR19 AT RBL 50" FOUND SUPPORT BEAM SURFACES SEVERAL AREAS OF CORROSION

CORROSION AT LEFT WING UPPER SURFACE STA. 3758 BETWEEN RIB 12 TO RIB 13 AND STRINGER 10 TO STRINGER 11

LOSS OF YELLOW HYDRAULIC SYSTEM AT CRUISE. REPLACED HYDRAULIC LINE, UNION, AND PACKINGS.

DIRTY SOCKS SMELL DURING DECENT, PERFORMED TSM 49-00-81-810-874-A, FOUND APU OIL OVER SERVICED, DRAINED APU OIL TO CORRECT LEVEL AS PER AMM 49-90-00-600-007-A, RAN APU WIOTH BLEED AIR ON FOR 2 HOURS, NO SMELL NOTED AT THIS TIME A/C OK FOR SERVICE.

AFTER LANDING WITH THE APU ON THERE IS A STRONG SMELL OF DIRTY SOCKS IN THE COCK PIT AND CABIN. ACCOMPLISHED TSM 05-50-00-810-831-A FOUND APU GENERATOR LEAKING OIL REPLACED GENERATOR IAW AMM 24-23-51-04 OPS CHECKED GOOD NO FUME SMELL.

IN CRUISE AIRCRFAT EXPERIANCED AIRFRAM VIBRATION AT 320 KIAS CORRECTIVE ACTION -PERFORMED TSM 27-20-00-810 FOUND BLUE SYSTEM SERVO FREE PLAY CHECK OUT OF LIMITS, ALSO REPLACED YELLOW AND GREEN SYSTEM ACTUATORS IAW A320 AMM 24-24-00 NO FURTHER DEFECTS NOTED

CABIN PRESSURIZATION 1&2 INOP DURING CLIMB.