BREEZE AVIATION GROUP INC

Part: UNKNOWN — ODOR (CABIN) · airframe 3,936 hrs · 1,953 cycles

NO EMERGENCY DECLARED, ODOR, AFT GALLEY BURNING ODOR THEN HEATER DID NOT COME BACK ON. FLIGHT WAS NOT DIVERTED. NO MEDICAL ATTENTION REQUIRED. PERFORMED CB RESET IAW AMP BD500-A-J21-42-01-02AAA-421A-A DEFECT CLEARED. OPS CHECKED GOOD

Part: SEAT — OVERSERVICED (ZONE 200) · airframe 6,550 hrs · 3,065 cycles

CABIN ODOR, FA COMPLAINTS ABOUT STRONG ODOR COMING OUT OF THE VENTS (IN FLIGHT). ODOR DEEMED TO BE EXCESSIVE RESIDUAL KROIL FROM ADJUSTING THE FA3 JUMP SEAT. CLEANED UP RESIDUE. NO DEFECTS NOTED AT THIS TIME. NO PAX OR CABIN CREW NEEDED MEDICAL ATTENTION, AND NO EMERGENCY DECLARED.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,026 hrs · 5,090 cycles

ACFT IN HEAVY CHECK. CORROSION ON WASTE DOUBLER. REAR BARREL FR 75 WASTE DOUBLER INBOARD CORNER FOUND CORROSION. WASTE DOUBLER REPLACED C/O IAW REO-500-53-61-2718, & EC CATC-53-EA-02917.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,026 hrs · 5,090 cycles

HEAVY CHECK SUBMISSION - CORROSION - REAR BARREL BOTTOM SKIN FOUND CORRODED AT FR 76 STRG 35L. CORROSION REMOVED AS PER ASRP BD500-A-J51-21-06-01AAA-258A-A

Part: HYDRAULIC LINE — LEAKING (ZONE 100) · airframe 4,061 hrs · 2,072 cycles

HYD 3 LO PRESS IN FLIGHT AT FL310. ALL HYD QTY LOST. HYD SYSTEM 3 WAS SHUTOFF AS PER QRH. HYD QTY DRAINED TO 8% PRIOR TO QRH PROCEDURE AND COMPLETLY DRAINED TO 0% FOLLOWING QRH TO TURN ON HYD PUMP 3A AND 3B. REMOVED AND REPLACED HYD COIL LINE TO LOWER RUDDER PCU. SERVICED HYD SYSTEM. LEAK OP CHECKED GOOD.

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 43,106 hrs · 22,323 cycles

FLIGHT DECK EMERGENCY LIGHT DOES NOT COME ON WHEN THE EMERGENCY LIGHTS ARE SELECTED ON. REMOVED AND REPLACED THE FWD RH ELPU.

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,841 hrs · 5,121 cycles

HEAVY CHECK - FWD MID FUSELAGE SKIN BETWEEN FR 34/FR35, STGR 36L 36R, FOUND CORRODED. CORROSION REMOVED AND DAMAGE REPAIRED

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 11,841 hrs · 5,121 cycles

HEAVY CHECK, REAR BARREL WASTE DOUBLER FOUND CORRODED, WASTE DOUBLER REPAIRED.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 11,841 hrs · 5,121 cycles

HVY CHECK SUBMISSION - CORROSION FOUND AT FR 57/FR58 ON WTBF SUPPORT ANGLE UNDER FAIRING 195KB. ANGLE REPLACED.

Part: DOWNLOCK — SHEARED (ZONE 700) · airframe 4,253 hrs · 21,685 cycles

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.

Part: SIGN — MISSING (ZONE 200) · airframe 3,219 hrs · 1,689 cycles

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

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 700) · airframe 1,578 hrs · 934 cycles

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.

Part: SENSOR — FAULTED (BRAKE TEMP) · airframe 1,579 hrs · 935 cycles

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

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 42,997 hrs · 22,228 cycles

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.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 42,997 hrs · 22,228 cycles

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.

Part: ENGINE — VIBRATION · airframe 11,980 hrs · 5,003 cycles

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.

Part: BATTERY — FAILED (ZONE 200) · airframe 41,772 hrs · 21,312 cycles

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

Part: WINDSHIELD — FAILED (ZONE 200) · airframe 42,970 hrs · 22,211 cycles

FO WINDSHIELD SHATTERED DURING CLIMB. REMOVED AND REPLACED WINDSHIELD.

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 42,408 hrs · 21,607 cycles

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.

Part: BATTERY — FAILED (ZONE 200) · airframe 41,774 hrs · 21,313 cycles

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

Part: OIL SYSTEM — LOW PRESSURE (RN 2 ENGINE) · airframe 43,472 hrs · 22,229 cycles

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

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 42,054 hrs · 21,503 cycles

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.

Part: BATTERY — FAILED (ZONE 200) · airframe 42,041 hrs · 21,498 cycles

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

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 42,054 hrs · 21,503 cycles

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

Part: LIGHT SYS — MALFUNCTIONED (ZONE 200) · airframe 41,983 hrs · 21,462 cycles

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

Part: FAULT MESSAGE — FALSE ACTIVATION (ZONE 700) · airframe 1,971 hrs · 939 cycles

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.

Part: BATTERY PACK — FAULTED (ZONE 200) · airframe 41,975 hrs · 21,457 cycles

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

Part: LIGHT — NO DISCREPANCY (ZONE 200) · airframe 41,928 hrs · 21,425 cycles

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.

Part: FRAME — CORRODED (ZONE 200) · airframe 6,883 hrs · 3,879 cycles

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

Part: ELEC CONNECTOR — UNSECURE (ZONE 200) · airframe 41,898 hrs · 21,405 cycles

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

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 800) · airframe 6,848 hrs · 3,855 cycles

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.

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 6,947 hrs · 3,332 cycles

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

Part: HINGE — CORRODED (ZONE 500) · airframe 2,207 hrs · 1,735 cycles

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

Part: WARNING MESSAGE — FALSE INDICATION · airframe 2,923 hrs · 1,392 cycles

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.

Part: HEATER — ODOR (ZONE 200) · airframe 6,852 hrs · 3,288 cycles

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.

Part: CONTROL UNIT — FAILED (ZONE 700) · airframe 382 hrs · 222 cycles

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.

Part: NUT PLATE — BROKEN · airframe 10,545 hrs · 4,483 cycles

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.

Part: SHUTOFF VALVE — FAILED (NR 2 ENGINE) · airframe 8,595 hrs · 3,962 cycles

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.

Part: HEATER — FOD (ZONE 700) · airframe 8,209 hrs · 3,235 cycles

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.

Part: FUEL FILTER — CLOGGED (ZONE 100) · airframe 10,420 hrs · 4,416 cycles

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.

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles

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

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles

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

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles

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.

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles

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

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles

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

Part: POWER SUPPLY — FAILED (ZONE 200) · airframe 41,733 hrs · 21,299 cycles

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.

Part: SPINNER — LEAKING (RT ENGINE) · airframe 11,180 hrs · 4,589 cycles

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.

Part: UNKNOWN — ODOR (CABIN) · airframe 10,159 hrs · 4,466 cycles

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.

Part: THROTTLE — FAILED (ZONE 100) · airframe 4,645 hrs · 2,277 cycles

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.

Part: UNKNOWN — SMOKE (CABIN) · airframe 3,398 hrs · 1,675 cycles

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.