GLOBAL CROSSING AIRLINES, INC.

Operated by Global Crossing Airlines (per NTSB report)

Sanction: $17,000 · case closed 2023-07-06

Part: SKIN — CORRODED (ZONE 600) · airframe 65,233 hrs · 20,539 cycles

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.

Part: SEAL DEPRESSOR — DAMAGED (ZONE 800) · airframe 51,371 hrs · 25,185 cycles

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.

Part: SKIN — CORRODED (ZONE 100) · airframe 45,782 hrs · 22,362 cycles

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.

Part: CONTROL CABLE — BROKEN (ZONE 300) · airframe 50,372 hrs · 22,048 cycles

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

Part: SLIDE — UNWANTED DEPLOY (ZONE 800) · airframe 48,402 hrs · 19,160 cycles

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

Part: NUT — DISCONNECTED (ZONE 800) · airframe 48,402 hrs · 19,160 cycles

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

Part: COOLING FAN — VIBRATION (ZONE 100) · airframe 48,212 hrs · 19,071 cycles

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

Part: SEAL — MISINSTALLED (CARGO DOOR) · airframe 48,776 hrs · 15,759 cycles

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

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,876 hrs · 20,916 cycles

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

Part: HOSE — LEAKING (ZONE 400) · airframe 38,784 hrs · 12,982 cycles

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

Part: EPSU — INOPERATIVE (ZONE 200) · airframe 47,496 hrs · 15,292 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOP

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 25,232 hrs · 9,374 cycles

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

Part: RESERVOIR — LOW PRESSURE (SLIDE) · airframe 37,587 hrs · 25,309 cycles

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

Part: FLEX HOSE — CUT (ZONE 700) · airframe 42,252 hrs · 20,527 cycles

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

Part: EPSU — DISCHARGED (ZONE 100) · airframe 47,946 hrs · 29,338 cycles

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

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 47,929 hrs · 30,002 cycles

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.

Part: FLOORBEAM — CORRODED

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

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,837 hrs · 29,945 cycles

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

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,837 hrs · 29,945 cycles

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

Part: UNKNOWN — LOW PRESSURE (ZONE 800) · airframe 47,837 hrs · 29,945 cycles

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

Part: UNKNOWN — UNKNOWN (UNKNOWN)

MEGAPHONE DOES NOT WORK /REPLACED

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 47,837 hrs · 29,945 cycles

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

Part: FLOORBEAM — CORRODED (MAIN CABIN) · airframe 47,837 hrs · 29,945 cycles

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

Part: FLOORBEAM — CORRODED (MAIN CABIN) · airframe 47,837 hrs · 29,945 cycles

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

Part: SKIN — CORRODED (LT WING) · airframe 47,837 hrs · 29,945 cycles

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

Part: HYDRAULIC LINE — LEAKING (YELLOW SYS) · airframe 46,576 hrs · 14,760 cycles

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

Part: APU — ODOR · airframe 41,555 hrs · 20,188 cycles

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.

Part: GENERATOR — ODOR (APU) · airframe 41,546 hrs · 20,180 cycles

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.

Part: SERVO — WORN (ZONE 300) · airframe 60,106 hrs · 17,901 cycles

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

Part: CABIN PRESSURE — UNKNOWN · airframe 46,062 hrs · 29,024 cycles

CABIN PRESSURIZATION 1&2 INOP DURING CLIMB.