N27152

Part: LAMP — UNSECURE (EMERGENCY LIGHT) · airframe 42,791 hrs · 26,240 cycles

CABIN DOOR EMERGENCY LIGHT INOPERATIVE. FOUND LAMP WASN'T FULLY SECURED. RE-SECURED LAMP, OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,603 hrs · 26,043 cycles

MAIN CABIN DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R MAIN CABIN DOOR EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,033 hrs · 24,604 cycles

MAIN DOOR EMERGENCY LIGHT INOPERATIVE. R&R MAIN DOOR EMERGENCY LIGHT. OPS CHECK SAT.

Part: LIGHT — UNSECURE (CABIN) · airframe 40,563 hrs · 24,179 cycles

EMERGENCY PATH LIGHTING PLASTIC COVER AND LIGHT BAR NEAR SEAT 1A BROKEN. SECURED EMERGENCY PATH LIGHT STRIP. NO OTHER DEFECTS NOTED AT THIS TIME.

Part: LIGHT — BURNED (CABIN) · airframe 40,234 hrs · 23,948 cycles

IAH - FLIGHT 4089 THE CREW REPORTED A STRONG ELECTRIC BURNING SMELL AROUND ROW 18. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A BURNT LIGHT SOCKET ON THE OVERHEAD LIGHT AT ROW 18. MAINTENANCE REMOVED THE AFFECTED SOCKET HARNESS AND PLACED THE OVERHEAD LIGHTING IN MEL 33-20-00/2 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THIS SDR FILED OPEN PENDING FINAL CORRECTIVE ACTION. SUPPLEMENTAL - ON 12/31/18 TYS MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSEMBLY, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. ***SDR CLOSED***

Part: YOKE — CRACKED (LT ENGINE) · airframe 39,636 hrs · 23,497 cycles

DURING A C-CHECK INSPECTION FOUND THE L/H ENGINE UPPER FORWARD ENGINE YOKE CRACKED. MAINTENANCE REMOVED AND REPLACED THE YOLK FITTING IAW EC/TC EA 145-2018-125. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.

Part: FLOOR SUPPORT — CORRODED (FRAME 59) · airframe 23,481 hrs · 39,611 cycles

CENTER LAVATORY FLOOR OMEGA BEAM CORRODED THROUGH NUT PLATE HOLE AT FRAME 59. CORRECTIVE ACTION: REPAIRED CENTER LAVATORY FLOOR OMEGA BEAM NUT PLATE AT FRAME 59 IAW SRM 53-24-10, REPAIR TYPE 3.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 39,611 hrs · 23,481 cycles

RIGHT WING INBOARD FLAP HAD AREAS OF DELAMINATION AT APPROXIMATELY 14 INCHES FROM INBOARD END. REPLACED THE CORE THROUGH THE BOTTOM SKIN.

Part: FRAME — CORRODED (FRM 59) · airframe 39,636 hrs · 23,497 cycles

ACFT IS IN FOR A C-CHECK WHEN INSPECTION FOUND SEVERAL AREAS CORRODED AT FRAME 59, STRINGERS 20R AND 21L. MAINTENANCE REMOVED THE DAMAGED AREA AND FABRICATED A REPAIR WITH L-ANGLES AND FRAME SECTION IAW SRM 53-00-04.

Part: YOKE — CRACKED (NACELLE) · airframe 39,611 hrs · 23,481 cycles

LEFT LOWER FORWARD YOKE CRACKED. REMOVED AND REPLACED YOKE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 39,162 hrs · 23,168 cycles

THE CREW REPORTED A STRONG BURNING ODOR IN THE COCKPIT, DURING FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE THE NR 1 PACK ON MEL 21-51-00-3 CAT C. THE AIRCRAFT WAS SUBSEQUENTLY APPROVED FOR RETURN TO SERVICE. OPEN

Part: ACM — INOPERATIVE (NR 1) · airframe 39,162 hrs · 23,168 cycles

ACM INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 ACM, OPS TESTED WITH NO DEFECTS NOTED. RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,950 hrs · 23,019 cycles

DURING ROUTINE INSPECTION, THE RT OVERWING EMERGENCY LIGHT WAS INOPERATIVE. MX REMOVED AND REPLACED THE BULB, OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,692 hrs · 22,123 cycles

THE CREW REPORTED FORWARD FACING ISLE OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY BATTERY CHARGER ASSEMBLY. OPS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 36,990 hrs · 21,634 cycles

FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY POWER SUPPLY NR 1. OPERATIONAL CHECKS WERE GOOD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,882 hrs · 22,977 cycles

DURING MAINTENANCE INSPECTION THE AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EMERGENCY LIGHT BATTERY CHARGER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — INOPERATIVE (NR 1) · airframe 36,171 hrs · 21,099 cycles

THE CREW REPORTED SMOKE IN THE FLIGHT DECK DURING INITIAL CLIMB THAT SMELLED LIKE ELECTRICAL. THE SMOKE CLEARED & THEN RETURNED DURING LANDING PHASE AND THE FLIGHT DECK WAS HOT. THE AIRCAFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE NR 1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, ANDTHE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 35,898 hrs · 20,897 cycles

CREW REPORTED UPON ENTERING ICING CONDITIONS THE COCKPIT FILLED WITH SMOKE AND ACFT PERFORMED AIR RETURN BACK TO EWR. MX INSPECTED AND RAN A/C SYSTEMS NOTED NR 1 PACK ACM SEIZED. REMOVED AND REPLACED NR 1 ACM AND HEAT EXCHANGER WITH OPERATIONAL CHECKS GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — FROZEN (AC BAY) · airframe 35,855 hrs · 20,860 cycles

CREW REPORTED A SMELL IN THE CABIN A/C AIR RETURNED TO ORF AFTER T/O SAFELY. CONTRACT MX CW SMOKE IN THE CABIN FIM, FOUND THAT PACK 1 FROZE UP, MOVED TO DMIL OPERATE PER MEL 21-51-00-3 CAT C, EXPIRATION DATE 11/11/1. MX REMOVED AND REPLACED NR 1 PACK AND AIR CYCLE MACHINE. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: ACM — SEIZED (NR 1) · airframe 35,853 hrs · 20,858 cycles

THE CREW REPORTED A STRONG SMOKE ODOR AT THE END OF TAKEOFF ROLL AND IN FLIGHT. THE AIRCRAFT RETURNED TO DEPARTURE AND LANDED WITHOUT INDCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 1 ACM FROZEN.

Part: ENGINE — LEAKING (NR 1) · airframe 35,446 hrs · 20,560 cycles

NR 1 ENGINE SMOKES ON SHUTDOWN AND PUDDLES OF OIL IN RTBS. REMOVED AND REPLACED THE ENGINE, OPS AND LEAK CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: ACM — FROZEN (NR 1) · airframe 34,420 hrs · 19,815 cycles

THE CREW REPORTED SMOKE IN THE COCKPIT AND BACK OF THE CABIN. THE ACFT RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THAT ACFT AND PLACED THE NR 1 PACK ON MEL, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE. ON MAINTENANCE R & R THE NR 1 ACM, OPERATIONALLY TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 34,260 hrs · 19,702 cycles

DURING C-CHECK, TOILET WASTE VALVE SUPPORT CORRODED. R & R TOILET WASTE VALVE SUPPORT IAW AMM 38-20-04. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 34,260 hrs · 19,702 cycles

DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — ODOR (CABIN) · airframe 33,573 hrs · 19,222 cycles

THE CREW REPORTED BURNING ODOR IN CABIN WITH PACKS OPERATING ON APU BLEED. MAINTENANCE INSPECTED AND FOUND ODOR COMING FROM PASSENGER-CABIN SIDEWALL LIGHT FIXTURE BRACKET. THEY REPLACED THE PASSENGER CABIN LIGHT IAW 145 33-21-06. OPS CHECKS WERE GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,688 hrs · 16,645 cycles

DURING MAINTENANCE INSPECTION, THE COCKPIT FLOOD EMERGENCY LIGHT, FIRST AISLE PATH CEILING EMERGENCY LIGHT AND LT FORWARD FUSELAGE EXTERNAL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENENCE R & R THE NR 1 EMERGENCY LIGHT POWER SUPPLY, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 29,688 hrs · 16,645 cycles

DURING MAINTENANCE INSPECTION, THE AFT OVERWING EMERGENCY EXIT LOCATOR SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE NR 4 EMERGENCY LIGHT INVERTER. OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 28,647 hrs · 15,995 cycles

CARGO DOOR LOWER FWD STRUCTURE CORRODED BEYOND LIMITS AROUND NUT PLATE HOLES. CUT OUT DAMAGE AND REPAIRED WITH A SHIM, FILLER AND "L" SHAPED DOUBLER IAW EC5230-01312.

Part: FLOOR SUPPORT — CORRODED · airframe 28,647 hrs · 15,995 cycles

LEFT OMEGA BEAM CORRODED BEYOND LIMITS AFTER BLEND OUT. CUT OUT DAMAGE, FABRICATED AND INSTALLED REINFORCEMENT ANGLE IAW EC5320-01859.

Part: SKIN — DENTED (FUSELAGE) · airframe 28,647 hrs · 15,995 cycles

DENT IN FUSELAGE SKIN, FRAME 80 STRINGER 5R. CUTOUT DAMAGED AREA, FABRICATED FILLER, DOUBLER AND INSTALLED.

Part: BUSHING — WORN (ZONE 300) · airframe 28,647 hrs · 15,995 cycles

DURING C-CHECK INSPECTION, FOUND THE LT AND RT SIDE HORIZONTAL STAB HINGE BUSHING MIGRATED, MAINTENANCE REWORKED HOUSING AND INSTALLED THE 1ST OVERSIZED BUSHIONS IAW SRM 55-10-02.

Part: INTAKE DUCT — CONTAMINATED · airframe 27,034 hrs · 14,951 cycles

THE CREW REPORTED AT APPROX 500FT AGL STRONG ODOR OF SMOKE AND VISUAL SMOKE COMING INTO COCKPIT THROUGH PACK DUCTWORK. IMMEDIATELY TURNED OFF PACKS AND RECIRCULATING FAN. SMOKE SUBSIDED AND THE CREW PERFORMED EMERGENCY AIR RETURN AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND EVIDENCE OF DEICING FLUID IN APU AIR INTAKE DUCT. CLEANED AIR INTAKE DUCT RAN ENGINES WITH PACKS AND BLEEDS ON AT VARIOUS SETTINGS NO SMOKE WAS NOTED. THE ACFT WAS RELEASED FOR SERVICE.

Part: BLEED AIR SYS — CONTAMINATED · airframe 27,006 hrs · 14,935 cycles

THE CREW REPORTED SMOKE IN COCKPIT AND CABIN. MX INSPECTED AND FOUND TO BE CAUSED BY DEICE FLUID IN BLEED DUCTS. RAN APU AND ENGINES WITH BLEEDS ON. CLEARED DEICE FLUID FROM BLEED DUCTS AND OPS CHECKS WERE GOOD.

Part: ENGINE — FAILED (LEFT) · airframe 24,195 hrs · 13,804 cycles

SUPPLEMENTAL: ON FINAL APPROACH, APPROXIMATELY 1800FT CREW EXPERIENCED ENGINE 2 VIBE FOLLOWED BY ENGINE 2 LOW PRESSURE EICAS MESSAGE FOLLOWED BY SMOKE IN THE CABIN AND EMERGENCY LANDING. THE ACFT LANDED WHERE MX R & R THE NR 2 ENGINE, OPS TESTED WITH NO DEFECTS AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BULB — FAILED (EMERGENCY LIGHT) · airframe 23,393 hrs · 12,641 cycles

DURING ROUTING SCHEDULED MX, THE AFT LEFT WING EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MX R & R THE AFT LT WING EMERGENCY LIGHT BULB IAW AMM 33-50-10, OPS CHECKED SUCCESSFULLY. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 22,705 hrs · 145,759 cycles

UNCOMMANDED STEERING ON TOUCHDOWN AIRCRAFT DEPARTED RUNWAY. AIRCRAFT SUSTAINED DAMAGE ON LOWER FUSELAGE IN SEVERAL AREAS. AIRCRAFT REPAIRED WITH THE FOLLOWING EC5300-01023, ETD2011-145-104349 AND ETD2011-145-104407. AIRCRAFT WAS RELEASED TO SERVICE 9/12/11.

Part: STEERING SYS — UNCONTROLLABLE (NLG) · airframe 22,703 hrs · 12,179 cycles

MLI - FLT 5821 THE CREW REPORTED UNCOMMANDED NOSE WHEEL STEERING ON TOUCHDOWN. THE AIRCRAFT DEPARTED THE RUNAWAY. SUPPLEMENT TO FOLLOW:

Part: PROXIMITY SWITCH — OUT OF ADJUST (LT MLG) · airframe 22,486 hrs · 12,029 cycles

TYS - A/C WAS DEPARTING CAE WHEN THE CREW GOT A MESSAGE ON THE EICAS OF LANDING GEAR AIR/GND FAILURE ON T/O. A/C RETURNED TO CAE AND WAS FERRIED TO TYS WITH RESTRICTIONS. UPON A SAFE ARRIVAL IN TYS, MAINTENANCE FOUND THE LEFT MLG REAR WOW PROX SWITCH OUT OF LIMITS. ADJUSTED THE GAP IAW EMB 145XR AMM 32-63-05; COMPLIED WITH THE GEAR EXTENSIONS AND RETRACTIONS TEST IAW EMB 145XR AMM 32-30-00. NO DISCREPANCIES NOTED AND WAS RELEASED FOR A TEST FLIGHT TO FURTHER EVALUATE. TEST FLIGHT WAS CANCELED DUE TO WEATHER SO THEREFORE A/C WAS REPO TO RIC TO VERIFY ANY ISSUES. NONE NOTED AND WAS RELEASED TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (LANDING GEAR) · airframe 22,457 hrs · 12,011 cycles

IAH - FLIGHT 2390, THE CREW REPORTED AN AIR/GROUND FAIL AFTER T/O. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ELECTRONIC CONTROL UNIT, (LGEU), OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG) · airframe 27,161 hrs · 11,632 cycles

IAH - FLIGHT 2435, DURING TAKEOFF THE CREW REPORTED AN AIR GROUND FAIL MESSAGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE NLG WEIGHT ON WHEELS PROXIMITY SENSOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — INOPERATIVE (COCKPIT) · airframe 21,050 hrs · 11,243 cycles

FLIGHT 2610 - EWR - FLIGHT CREW REPORTED ELECTRICAL PROBLEM WITH NUMEROUS MESSAGES ON EICAS (LG AIR. GRND FAIL, SPS ADV, SPS1 INOP, SPOILER FAIL). EWR MX REMOVED AND REPLACED LGEU AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,773 hrs · 9,950 cycles

IAH - DURING AIRCRAFT MOVE TWO DENTS ON THE LEFT FUSELAGE 1 CTR SKIN WAS REPORTED BETWEEN FRAMES 19 & 20, STRINGERS 11L AND 12L. MAINTENANCE PERFORMED A DOUBLER REPAIR ON THE AFFECTED SKIN, LEAK CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 17,135 hrs · 9,086 cycles

ABQ - FLIGHT 2728 - DURING PREFLIGHT INSPECTION THE CREW REPORTED THE RIGHT SIDE EMERGENCY EXIT HATCH EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. THE AIRCRAFT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND REPLACED THE AFFECTED INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 17,081 hrs · 9,059 cycles

SHV - EMERGENCY LIGHT INVERTER NR 6 IS INOP. REMOVED AND REPLACED NR 6 INVERTER IAW EMB 145XR AMM 33-50-11. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 16,425 hrs · 8,712 cycles

TYS FOR IAH - THE NOSE WHEEL DEFLECTED MOMENTARILY DURING ROLLOUT UNCOMMANDED. MAINTENANCE PERFORMED FUNCTIONAL TEST OF THE STEERING MANIFOLD IAW EMB 145XR AMM 32-50-04. FUNCTIONAL TEST GOOD. PERFORMED AN ADJUSTMENT TEST OF THE LOAD POTENTIOMETER IAW EMB 145XR AMM 32-50-05. TESTED WITHIN LIMITS, NO OTHER FAULTS FOUND AND WAS REL TO SERVICE.

Part: FAN — STUCK (E/E BAY) · airframe 16,559 hrs · 12,746 cycles

TYS FOR IAH - THE RECIRCULATING FAN IN FWD AVIONICS BAY BECAME INOP. AIRCRAFT RETURN BACK TO IAH. MAINTENANCE RELEASED A/C IAW EL 21-24-01/2 CAT (C).

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 15,113 hrs · 8,016 cycles

FLIGHT CREW REPORTED LAV SMOKE WARNING ON EICAS DURING CLIMBOUT WITH ASSOCIATED GALLEY WARNING BELL. MX REMOVED AND REPLACED ENGINE NR1 AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SILL — CORRODED (FUSELAGE) · airframe 13,882 hrs · 7,335 cycles

SHV - DURING C-CHECK LOWER INTERNAL PORTION OF BAG DOOR CUTOUT HAS VARIOUS AREAS OF CORROSION FROM FR 65 TO FR 68. MX REMOVED AND REPLACED CARGO DOOR CUTOUT LOWER SILL FROM FR 6T TO FR 68 IAW EMB 145 XR SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN FOR SERVICE. (S)

Part: SILL — CORRODED (FUSELAGE) · airframe 13,882 hrs · 7,335 cycles

SHV - DURING C-CHECK CORROSION UNDER THRESHOLD AT SERVICE DOOR. MX REMOVED AND REPLACED SERVICE DOOR CENTER SILL IAW EMB 145 XR SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE. (S)

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 7,639 hrs · 4,035 cycles

GSO - FLIGHT 2420, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE FLOOR EMERGENCY LIGHTS WERE INOPERATIVE. THE FLOOR LIGHTS WERE CHARGED, AND OPERATIONAL CHECKS WERE GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ODOR — DETECTED (COFFEEMAKER)

CLE FLIGHT 3320 THE CREW REPORTED SMOKE AND BURNING RUBBER SMELL EMITTING FROM COFFEE POTS. MAINTENANCE INSPECTED AND RELEASED AIRCRAFT IAW MEL 25-60-02/3.