BREEZE AVIATION GROUP INC

DURING LANDING ROLLOUT LANDING GEAR AURAL WARNING SOUNDED ACCOMPANIED BY UNSAFE INDICATION OF RIGHT MAIN GEAR, LG LEVER DISAG WARNING ANNUNCIATION, AND LG NO DISPATCH CAUTION ANNUNCIATION. PULLED CLEAR OF RUNWAY AND CALLED MECHANIC TO INSPECT GEAR BEFORE TAXIING FURTHER. MECHANIC INDICATED THAT LAND GEAR DOWN LOCK WAS SHEARED OFF FROM THE GEAR.

GREEN RUNNING MAN SIGN MISSING BY THE L1 DOOR, INSTALLED NEW EMERGENCY EXIT IDENTIFIER SIGN.

DURING DESCENT THE RIGHT OUTBOARD BRAKE INDICATED HIGH TEMP. IT CYCLED BETWEEN 0 AND 9 SEVERAL TIMES. AFTER IT DID THIS 3 TIMES RECEIVED BRAKE OVHT WARNING MESSAGE. EVALUATED IN REFERENCE TO THE FIM. NO FAULT MESSAGES POSTED. NO DISCREPANCIES OR DEFECTS FOUND.

DURING DESCENT THE RIGHT OUTBOARD BRAKE INDICATIED HIGH TEMP SEVERAL TIMES. REMOVED AND REPLACED TEMP SENSOR ON RH OUTBOARD BRAKE ASSEMBLY.

LEFT MIDDLE ELPU FAILED TO TEST. EMERGENCY LIGHTS ILLUMINATING WHEN THE AIRCRAFT IS POWERED DOWN AND EMERGENCY LIGHT SWITCH IS IN THE OFF POSITION. REPLACED THE LT MIDDLE ELPU IAW AMM.

FWD LT EMERGENCY LIGHT BATTERY FAILED TO TEST. EMERGENCY LIGHTS ILLUMINATING WHEN THE AIRCRAFT IS POWERED DOWN AND EMER LT SWITCH IS IN THE OFF POSITION. REPLACED THE LT FWD ELPU PER AMM.

INTERMITTENT ENGINE VIBRATION DECENDING THROUGH 10000 FEET. SECOND TIME WE HAD AN ENGINE FAULT INDICATION AS WELL. VIBRATION COULD BE FELT ON THE RUDDER PEDALS WITH ADDED THRUST ON THE LEFT ENGINE. PERFORMED VIBE ANALYSIS. VIBES REMAIN IN ALLOWABLE LIMITS DURING ENGINE RUNS. NO FUALTS PRESENT DURING ENGINE RUNS.

HEAVY CHECK, LOWER FUSELAGE MID RH EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY BATTERY.

FO WINDSHIELD SHATTERED DURING CLIMB. REMOVED AND REPLACED WINDSHIELD.

EMERGENCY LIGHT BATTERY FAULOT, RH CTR ELPU HARD FAULTED CAUSING SOME OF THE EMERGENCY LIGHTS TO TURN ON AND OFF UNCOMMANDED. REPLACED THE RH CTR ELPU.

HEAVY CHECK, UPPER FUSELAGE PAX CABIN EXIT MARKER LT & RT EMERGENCY LIGHT INOP. REPLACE ELPU NR 3.

DURING FLIGHT ENGINE OIL 2 PRESSURE DECREASED WENT TO APPROX 20 RED INDICATION, RAN QRH AND SHUT ENGINE DOWN. NO FURTHER INCIDENT.

EMERGENCY LIGHTS FLICKERING ON AND OFF IN ARMED PPOSITION. EMERGENCY LIGHTS ALSO TURNED ON AFRTER AIRCRAFT WAS POWERED DOWN WITH SWITCH IN OFF POSITION. ERMER LT BATT FAULT EICAS INTERMITTENT. REMOVED AND REPLACED EMERGENCY LIGHT POWER UNIT NR 4.

EMERGENCY LIGHT BATTERY FAULT. R & R LT FWD EMERGENCY LIGHT BATTERY.

EMERGENCY BATT FAULT ON EICAS, FWD RH ELPU FAILED. R/R FWD RH ELPU PER AMM. OPS CHECK GOOD. - LATE SUBMISSION

FWD EMERGENCY LIGHTS FLICKERING. PERFORMED AIRCRAFT POWER RESET. PERFORMED OPS CHECK OF THE EMERGENCY LIGHTS PER AMM. OP CHECKED PASSED.

LANDING GEAR ADVISORY GEAR FAULT AND LANDING GEAR ADVIVSORY BRAKE FAULT AFTER. PREVIOUS CREW HAD GEAR FAULT AND BRAKE FAULT AFTER GEAR DOWN ON FINAL. PREVIOUS CREW HAD GEAR FAULT AND BRAKE FAULT AFTER GEAR DOWN ON FINAL. PERFORMED AIRCRAFT POWER RESET AND NORMAL START UP ON GROUND POWER AFTER 15 MINUTES. PERFORMED FIM PROCEDURE. RESET AND OPS CHECKS COMPLIED WITH. ALL FAULTS CLEARED AND OPS CHECKS PASSED.

FWD EMERGENCY LIGHT BATTERY FAULT. EMERGENCY LIGHTS CAME ON UNCOMMANDED IN THE FWD GALLEY. CYCLED POWER. ITEM CLEARED.

EMER LT BATT FAULT. EMERGENCY LIGHTS CAME ON AND STAYED ON IN THE ARMED POSITION. CHARGED EMERGENCY LIGHTS. PERFORMED OPS CHECK WITH ENGINES RUNNING. OPS CHECKED GOOD.

HVY CHECK SUBMISSION - REAR BARREL WAS DOUIBLER AT FRAME 75 FOUND CORROSION, TEMP REPAIR CARRIED OUT AS PER BREEZE EA.

FA REPORTS EMERGENCY LIGHTS FLICKERING AT OVERWING EXIT. RESECURED ELECTRICAL CONNECTOR, OPS CHECK GOOD.

DOOR ARMED MESSAGE WHEN L1 DOOR OPEN BY GATE AGENT. DEFECT TYPE: INFO, NOTED BY MOC. CREW PERFORMED NORMAL DOOR CLOSURE AND ARMING AND DISARM AND OPEN AND MESSSAGE CLEARED.

HVY CHECK SUBMISSION - CORROSION FOUND ON WASTE DOUBLER CUTOUT AT REAR BARREL FRAME 75-76. REPAIRED IAW AIRBUS REO.

LH WING TE PANEL SUKPPORT STRUTURE BETWEEN RIB 22-23 HAS CORROSION. REMOVED AND REPLACED HINGE AT RIB

DUAL BLEED FAILURE - 36 R BLEED FAIL - R HPV FAIL CLSD - 36 L BLEED FAIL - L PRESS REG SOV INOP- PERFORMED FAUL RESET. PERFORMED POWER RESET OF AIRCRAFT. RAN ENGINES WITH CREW, AND PERFORMED BAS IBIT TEST ON IASC 1A, IASC 2A, IASC 1B, AND IASC 2B. NO DEFECTS NOTED AND ALL TESTS PASSED.

WHEN HEATER TURNED ON THERE WAS A BURNING SMELL. REMOVED AND INSTALL GALLEY HEATER. OPS CHECK GOOD. THIS CLEARS MEL. NO MEDICAL ATTENTION WAS NEEDED FOR CREW OR PAX AND NO EMERGENCY DECLARED.

ENROUTE KHVN, RECEIVED A "BRAKE ON" CAUTION. PERFORMED ASSOCIATED CHECKLIST; CAUT REMAINED. CYCLED PARKING BRAKE TO SEE IF ISSUE WOULD CLEAR WITHOUT SUCCESS. AFTER CYCLING PARKING BRAK, "PARKING BRAKE FAIL" ANNUNCIATED. COMPLETED ASSOCIATED CHECKLIST. BOTH CAUTIONS REMINAED ON. REMOVED AND REPLACED #4 ELECTROMECHANICAL CONTROLLER UNIT. OPS CHECKED GOOD.

FACILITY FOR REPAIR - (HVY) - HD LO QTY - WHILE PERFORMING MX FOR HYD LEAK, FOUND LWR VS TE PANEL BOTTOM NUT PLATE BRACKET BROKEN OFF. VS TE LOWER CLOSURE RIB PN C01953501-005 AND VS TE HINGE #1 ASSY REPLACED PER CATA-55EA-02533.

RIGHT NEACELLE OVERHEAT CAUTION MESSAGE IN FLIGHT. CLEARED AFTER RUNNING CHECKLIST. GOT MESSAGE AGAIN AFTER GOING BACK TO CLIMB POWER. RETURNED TO FIELD. REMOVED AND REPLACED BUFFER SHUT OFF VALVE. OPS AND LEAK CHECKS GOOD.

AFT GALLEY HEATER ODOR WHEN TURNED ON THAT DID NOT DISSIPATE. SMELLED LIKE A WOMANS HAIR DRYER. FOUND LINT ON GALLEY SCREEN, LINT REMOVED. PLACED ON MEL. REMOVED AND REINSTALLED THE AFT GALLEY HEATER TO FURTHER IINSPECT THE COMPONENT, FOUND DUST AND OTHER FOD. REMOVED ALL FOD. CLEARED MEL.

LT AND RT FUEL FILTER CAUTION MESSAGE APPEARED SHORTLY AFTER TAKEOFF WHEN PASSING THROUGH 7000 FEET. BEGAN RUNNING QRH AND MESSAGED DIESAPPEARED. FUEL FLOW AND SYNOPTIC PAGE LOOKED NORMAL AND MESSAGE DID NOT ILLUMINATE AGAIN. DECLARED EMERGENCY FOR PRIORITY SPACING AND LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED FUEL FILTER ON LH AND RH ENGINES. LEAK CHECKED GOOD. OPERATIONAL CHECKS GOOD. SMALL AMOUNTS OF CONTAMINATES SEND OUT FOR EXAMINATION.

RH FWD ELPU FUALTY. ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. REPLACED FWD RH ELPU

ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. REPLACED FWD LH ELPU.

ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. REPLACED THE RH CENTER ELPU.

ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. LH MIDDLE ELPU REPLACED

RH AFT ELPU FAULTY. ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. REPLACED THE RH AFT ELPU

LH AFT ELPU FAULTY. ELPU'S FAULTING CAUSING THE EMERGENCY LIGHTS TO FLICKER AND TURN ON UNCOMANDED WITH THE LIGHTS IN THE ARMED POSITION. REPLACED LH AFT ELPU.

CABIN ODOR - RIGHT ENGINE SPINNER COVERED IN OIL, OIL SPLATTER IN COWLING. OIL SMELL IN FLIGHT DECK AND CABIN ON DESCENT AROUND 10K FEET. COMPLIED WITH FIM TASKS IN REFERENCE TO A220 AMM 71-00-00. FOUND NO OIL LEAK, FLUID FOUND TO BE DE-ICING FLUID. NO SMELL OF OIL IN CABIN NOR FLIGHT DECK DURING ENGINE RUN. AIRCRAFT GOOD FOR CONTINUED SERVICE. NO EMERGENCY DECLARED.

DURING SERVICE FAS REPORTED WEIRD SMELL IN CABIN. TECH INSPECTED VENTS AND ONLY FOUND MINOR DUST. PERFORMED INSPECTION OF AREA WITH NO DEFECTS NOTED. PERFORMED AIR CONDITIONING SYSTEM OPERATION TEST. NO SMELLS OR DEFECTS NOTED. NO EMERGENCY DECLARED, AND NO MEDICAL ATTENTION NEEDED FOR PAX OR CREW.

AT CRUISE, FL 360, RECEIVED RT THROTTLE FAILED CAUTION MESSAGE. RAN QRH AND DIVERTED TO MEM. REMOVED AND REPLACED THROTTLE QUADRANT. OPS CHKD WAS GOOD. PERFORMED OPS CHECK OF BRAKE SYSTEM, OPS CHKD GOOD.

UPON LANDING AND FLIGHT REVERSER DEPOLYMENT, FLIGHT ATTENDANTS REPORTED CABIN FILLED WITH WHITE SMOKE. ALL CREW NOTED A STRONG ODOR RESEMBLING EXCESSIVE HEAT, CONSISTENT WITH A POSSIBLE OVERHEATING CONDITION. NO EMERGENCY DECLARED, AND NO ONBOARD MEDICAL ATTENTION NEEDED FOR CREW OR PAX. EVALUATED DISCREPANCY REFERENCING FIM. DISCREPANCY COULD NOT BE DUPLICATED AT THIS TIME. NO FURTHER DEFECTS NOTED.

LEFT ENGINE FIRE MESSAGE. ENG SHTDOWN IN FLIGHT. A/C RETURNED TO FIELD. LEFT ENG FIRE INDICATION ON CLIMBOUT "L ENG BTL LO". REMOVED AP12, INSTALLED SEALS, AND REINSTALLED AP12 LINE.

CORROSION FOUND AT WASTE DOUBLER ACCESS AT REAR BARREL. REPAIRED PER AIRBUS REO.

HVY CHECK - CORROSION FOUND ON AFT MID FUSELAGE BOTTOM SKIN AT STRG 36R BETWEEN FR 57. REPAIRED PER REO.

L2 DOOR EMERGENCY SLIDE DEPLOYED INADVERTENTLY, REMOVED AND REPLACED L2 DOOR EMERGENCY SLIDE.

EMERGENCY BATTERY FAULT MESSAGE, LT MID ELPU FAILED. REMOVED AND REPLACED LT MID ELPU.

MOMENTRY SMELL OF SMOKE FROM AFT GALLEY COFFEE POT. FA REPORTED SMELL WENT AWAY AFTER COFFEE MAKER 2 IN AFT GALLEY WAS SHUT OFF AT THE CMS. REMOVED COFFEE MAKER. FOUND NO EVIDENCE OF BURNS. REINSTALLED COFFEE MAKER. NO EMERGENCY DECLARED, AND NO PAX OR CREW REQUIRED MEDICAL ATTENTION.

AFT GALLEY HEATER WHEN TURNED ON GAVE STRONG ELECTRICAL BURNING SMELL. WHEN TURNED OFF, SMELL DISAPATED AND DID NOT RETURN. HEATER LEFT OFF FOR DURATION OF FLIGHT. NO ONBOARD MEDICAL ATTENTION NEEDED FOR CREW OR PAX. NO EMERGENCY DECLARED. AFT GALLEY HEATER PLACED ON MEL.

BURNING ODOR IN CABIN DURING FLIGHT, CREW RAN FIRE/SMOKE/FUMES QRH. ODOR DISSIPATED AFTER THE QRH. PERFORMED FAULT ISOLATION PROCEDURE FOR FUES OR SMOKE EVENTS IN CABIN BY PERFOMING ENGINE RUNS AND PERFOMING A VISUAL INSPECTION OF THE ENGINES TO CHECK FOR ANY FLUID LEAKS IAW BD500-A-J21-22-00-04AAA-423A-A. NO EICAS WARNINGS OR FAULT MSG PRESENT ON OMS. PERFORMED GENERAL VISUAL INSPECTION OF THE FWD AVIONICS BAY WHICH IS BELOW THE FWD GALLEY, NO SMOKE ODOR OR BURN MARKS NOTED. INSPECTED THE AREA WHERE THE SMOKE ODOR CAME FROM AND FOUND THE EMERGENCY ACCESS LATCH TO THE COCKPIT DOOR VERY WARM. DEACTIVATED LATCH AND PLACED ON MEL. NO ONBOARD MEDICAL NEEDED, AND NO EMERGENCY DECLARED.

AFTER LANDING, AS CLEARING THE RUNWAY R ENG FIRE WARNING MSG. RAN THE R ENG FIRE CHECKLIST. ENGINE REMOVE AND REPLACE.