N14162

Part: FLAP SYSTEM — DAMAGED · airframe 45,419 hrs · 30,860 cycles

FLAP FAIL, ON EICAS DURING CLIMB. RESET AND PERFORMED OPS CHECK OF FLAPS, FLAPS JAMMING AT 9 DEGREES, SUSPECTED BAD RH INBOARD ACTUATOR. INSPECTED AND FOUND RH INBOARD FLAP, RH FLAP SHROUD, AND RH ROLLER TO BE DAMAGED. REMOVED RH INBOARD FLAP AND SHROUD. REMOVED PANELS 197AB, 197BB, AND 197CL, FLAP 1 AND 2 C/BS PULLED, HYD 1 AND 2 CB PULLED. GSE 066 INSTALLED ON RH SPOILERS. REMOVED AND REPLACED RH INBOARD ROLLER. REINSTALLED RH INBOARD FLAP AND REATTACHED GIMBLES. OUTBOARD FLAP SHROUD DRIVER NEEDS REINSTALLED. PERFORMED ZERO DEGREE RIGGING. PANELS 197AB, 197BB, AND 197CL INSTALLED. INSTALLED FLAP SHROUD AND SHROUD DRIVER. PUSHED CB FLAPS 1 AND 2 AND HYD 1 AND 2. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (MULTIPLE) · airframe 44,060 hrs · 29,558 cycles

ICU PILOT FA COMMUNICATION INOPERATIVE. CABIN AND CABIN EMERGENCY LIGHT WILL NOT EXTINGUISH. RESET SYSTEM POWER. SYSTEM OPS CHECKED NORMAL. EMERGENCY LIGHTS OP CHECK NORMAL. NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,694 hrs · 29,233 cycles

FUEL IMBALANCE RIGHT WING FUEL SHOWS 0 IN FLIGHT. FUEL IMBALANCE WAS CREW INDUCED WHEN FOLLOWING QRH DUE TO THE RH WING SHOWING 0. REMOVED AND REPLACED FUEL RELAY BOX. OPS CHECK SAT. NO PRESENT REPEATER CODES. CHECKED POWER TO WING FCU, POWER PRESENT, CHECKED HARNESS AROUND FCU AND SHOOK. OPS CHECK SAT. INSPECT THE PRESSURE REFUEL PANEL AND CONNECTORS. CHECK THE FINGER OF THE FUELING CONTROL PANEL AND PRESSURE REFUELING ADAPTER COMPARTMENT ACCESS DOOR FOR MALADJUSTMENT. INSPECT THE SELECT SWITCH FOR DAMAGE. INSPECTED PRESSURE REFUEL PANEL, CONNECTORS, FINDER OF THE FUELING CONTROL PANEL AND THE POWER SELECT SWITCH. NO DEFECTS NOTED.

Part: CONTROL PANEL — UNKNOWN (UNKNOWN) · airframe 43,304 hrs · 28,860 cycles

FWD FA INTERPHONE EMERGENCY LIGHT SLIGHTLY ILLUMINATED. SLAVED IN NEW ATTENDANT HANDSET. NO FIX. REINSTALLED ORIGINAL HANDSET BACK. SWAPPED FORWARD AND AFT HANDSETS, NO FIX. SLAVED IN AN ICU PANEL, NO FIX. ORIGINAL PLACED BACK IN. SLAVED IN A PA AMPLIFIER, NO FIX. ORIGINAL PLACED BACK IN. SLAVED IN APU GCU, NO FIX. ORIGINAL PLACED BACK IN. REMOVED AND REPLACED THE LAVATORY ATTENDANT CALL SWITCH PC BOARD, NO FIX. THIS ONLY OCCURS WHEN SHED BUS 1 AND 2 ARE OFF (AUTO MODE) EICAS MESSAGE IS PRESENT WITH BATTERIES OR APU GENERATOR. DOES NOT OCCUR WITH GPU SELECTED OR SHED BUS IS IN OVERRIDE.REMOVED ATTENDANT CALL PANEL ASSEMBLY. INSTALLED AFT ATTENDANT CALL PANEL ASSEMBLY. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,261 hrs · 28,823 cycles

MAIN CABIN DOOR HARD TO OPEN. LUBED MAIN DOOR. OPS CHECK SAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,210 hrs · 28,780 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. PERFORMED MAIN DOOR TEST. OPS CHECK SAT

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 43,189 hrs · 28,758 cycles

EMERGENCY LIGHT STRIP FWD OF 1A MISSING AND ALSO ALONG GALLEY. FOUND MISSING STRIPS AND RESECURED WITH ADHESIVE TAPE. NO DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 42,705 hrs · 28,302 cycles

SMOKE ODOR FROM APU BLEED DURING TAKE OFF. PERFORMED OPERATIONAL CHECK OF APU. COULD NOT DUPLICATE. SUSPECT SMELL WAS ENGINE EXHAUST IN BLEED.

Part: LIGHT — UNSECURE (CABIN) · airframe 42,223 hrs · 27,880 cycles

EMERGENCY LIGHT STRIP AT 1A NEEDS RESECURED. RESECURED EMERGENCY LIGHT STRIP AT 1A.

Part: NONE — NONE · airframe 42,013 hrs · 27,679 cycles

FLOOR PROXIMITY LIGHT STRIP MISSING ALONGSIDE SEAT 5A. ADJUSTED FLOOR PROX LIGHT STRIP ALONGSIDE SEAT 5A. OPS CHECK SAT

Part: FRAME ANGLE — CRACKED · airframe 41,950 hrs · 27,627 cycles

FRAME #66 AT CARGO DOOR CUT-OUT MAIN FRAME HAS 1/2 CRACKED AT UPPER FLANGE BETWEEN RIVETS. REPAIRED FR66 UPPER FLANGE AT CARGO DOOR CUT-OUT

Part: PANEL SUPPORT — CORRODED · corrosion level 2 · airframe 41,950 hrs · 27,627 cycles

1R SERVICE DOOR ALUMINUM STRUCTURE S/S THRESHOLD PANEL IS CORRODED. REMOVED AND REPLACED SERVICE DOOR SILL UNDER S/S THRESHOLD PANEL.

Part: SKIN PANEL — CORRODED · corrosion level 2 · airframe 41,950 hrs · 27,627 cycles

REAR FUSELAGE I SKIN HAS CORROSION UNDER RAR #2. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER AT RAR #2 ANTENNA LOCATION

Part: NONE — WORN · airframe 41,658 hrs · 27,368 cycles

RIGHT HAND EXTERIOR OVERWING "EXIT" PLACARD ILLEGIBLE. REMOVED AND REPLACED EXTERIOR OVERWING EXIT PLACARD. NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,807 hrs · 26,617 cycles

EMERGENCY LIGHT BY 3C INOPERATIVE. REMOVED AND REPLACED POWER SUPPLY #2. OPS CHECK SAT.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,767 hrs · 26,583 cycles

RH FWD WTF FAIRING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED #2 EMERGENCY LIGHT BATTERY CHASSIS. OPS CHECK SAT, ALSO R&R RH FWD EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK SAT

Part: BATTERY PACK — UNSECURE (EMERGENCY LIGHT) · airframe 40,682 hrs · 26,508 cycles

RH EMERGENCY EXIT HATCH LIGHT INOP AT SEAT 18 C/D. SECURED #3 EMER LIGHT BATTERY, OPS CHECKS GOOD

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 40,577 hrs · 26,417 cycles

RH TOP EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R RH TOP EXTERNAL EMERGENCY LIGHT. OPS CHECK SAT. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,510 hrs · 25,460 cycles

RH FWD EXTERNAL EMERGENCY LIGHT INOPERATIVE. R&R RH FWD EMERGENCY LAMP. OPS CHECK FAILED. R&R #2 BATTERY. OPS CHECK SAT.

Part: FIRE DETECTOR — INOPERATIVE (NR 2 ENGINE) · airframe 39,492 hrs · 25,445 cycles

EICAS MESSAGE E2 FIRE DETECTION FAIL. R&R FIRE DETECTOR LOOP (ENGINE #2). OPS CHECK CARRIED OUT. FOUND SATISFACTORY. NO OTHER DEFECTS NOTED.

Part: PLACARD — INCORRECT (EMERGENCY EXIT) · airframe 37,654 hrs · 23,724 cycles

EMERGENCY HATCH LH SIDE WRONG PLACARD. R&R LEFT EMERGENCY EXIT PLACARD. NO OTHER DEFECTS NOTED AT THIS TIME

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,298 hrs · 23,383 cycles

CORROSION FOUND ON THE OMEGA BEAM FR 59/60 AFTER OMEGA BEAM GUSSET REMOVAL. REPAIRED CENTER OMEGA BEAM FR 59-60, JUST FWD OF FRAME 60.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,298 hrs · 23,383 cycles

BAGGAGE DOOR FWD LATERAL L-SHAPE BRACKET HAS CORROSION AT FR 65 STR 15L-16L. FABRICATED, LOCATED AND DRILLED BAGGAGE DOOR DOUBLER AT FRAME 65 BETWEEN STR 17L AND 18L.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 37,298 hrs · 23,383 cycles

CORROSION - RT OMEGA BEAM UNDERNEATH GUSSET FR 59-60. REPAIRED RT OMEGA BEAM UNDERNEATH GUSSET FR 59-60. 59.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 35,859 hrs · 22,064 cycles

PITCH TRIM MAIN INOPERATIVE IN FLIGHT. R&R HSCU. OPS CHECK SAT.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 34,931 hrs · 21,137 cycles

LAV SMOKE DETECTOR WENT OFF INFLIGHT. R&R LAV SMOKE DETECTOR IAW AMM 26-14-01. OPS CHECK SAT.

Part: TRANSDUCER — SHORTED (BRAKE SYS) · airframe 31,305 hrs · 18,546 cycles

PILOT REPORTED AFTER LANDING AND EXITING ON HIGH SPEED TAXIWAY THEY EXPERIENCED A COMPLETE BRAKE FAILURE AND COULD NOT STOP THE ACFT. EMERGENCY BRAKE WAS PULLED TO STOP ACFT SAFELY. MAINTENANCE R & R THE PILOT LT BRAKE PEDAL POSITION TRANSDUCER WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — FAULTY (PITCH TRIM) · airframe 27,752 hrs · 16,118 cycles

THE CREW REPORTED PITCH TRIM INOPERATIVE MESSAGE IN FLIGHT FOR BOTH MAIN AND BACKUP. THE ACFT RETURNED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BOTH MAIN AND BACKUP PITCH TRIM SWITCHES. OPS CHECKS WERE GOOD.

Part: STRUCTURE — GOUGED (ZONE 100) · airframe 27,558 hrs · 15,989 cycles

VENTRAL FUEL TANK HAS .045 GOUGE ON LOWER SURFACE UNDER FUSELAGE SKID AFT FAIRING. BLENDED GOUGE TO SMOOTH CONTOUR. INSTALLED DOUBLER AND REWORKED AFT FAIRING UPPER SURFACE EDGE TO OBTAIN CLEARENCE. ACCOMPLISHED REPAIR IAW ETD2014-145-054344 AND EC 2810-01075, DATED 2 JUL 2014, WO 80235; WC 1221.

Part: ATTACH ANGLE — CRACKED (WG-BDY FAIRING) · airframe 27,558 hrs · 15,989 cycles

LT LOWER WING TO FUSELAGE LATERAL FAIRING ATACH ANGLES ARE CRACKED. REMOVED AND REPLACED THE ATTACH ANGLES IAW SRM 51-40-02, 51-20-03, 51-40-06, 51-20-01, CPM 51-21-04.

Part: FLOORBEAM — CORRODED (FRAME 53) · airframe 27,558 hrs · 15,989 cycles

CORROSION ON RT FLOORBEAM ANGLE AT FRAME 53. R & R RT FLOORBEAM ANGLE IAW SRM 51-40-02. ON WO 80235, WC 1216.

Part: GUSSET — CORRODED (BS 479) · airframe 27,558 hrs · 15,989 cycles

FLOOR SUPPORT GUSSET AT BS 479 CORRODED. R & R GUSSET IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FRAME 60) · airframe 27,558 hrs · 15,989 cycles

LEFT FLOOR SUPPORT FRAME 60 CORRODED. R & R FLOOR SUPPORT IAW SRM 51-20-03, 51-40-02 AND SWP 20-21-00.

Part: FLOOR SUPPORT — CORRODED (FRAME 62) · airframe 27,558 hrs · 15,989 cycles

LEFT FLOOR SUPPORT AT FRAME 62 CORRRODED. R & R LT FLOOR SUPPORT IAW SRM 51-40-02, 5140-04, 51-40-06, SWPM 20-21-00.

Part: ATTACH ANGLE — CRACKED (WG-BDY FAIRING) · airframe 27,558 hrs · 15,989 cycles

RIGHT UPPER WING TO FUSELAGE LATERAL FAIRING ATTACH ANGLE CRACKED. R & R ATTACHMENT ANGLE IAW SRM 51-40-02, 51-20-03, 51-40-09, CPM 51-21-06.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 27,558 hrs · 159,989 cycles

AVIONICS RACK SUPPORT ANGLE AT FRAME 75 IS CRACKED. R & R SUPPORT ANGLE IAW SRM 51-40-20.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,536 hrs · 15,988 cycles

PILOT REPORTED THE OVERHEAD EMERGENCY EXIT SIGN NOT ILLUMINATING PROPERLY. MX R & R INVERTER AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 27,481 hrs · 15,954 cycles

PILOT REPORTED DURING DESCENT AROUND 14,000 FT THE ODOR OF SMOKE AND FUMES IN COCKPIT FOR ABOUT ONE MINUTE. ALL THREE CREW DONNED O2 MASKS NEVER SAW SMOKE JUST SMELLED IT AND IRRITATED EYES. MX PERFORMED A GVI OF BOTH ENGINES INLETS AND EXHAUSTS FOR OIL LEAKS NO FAULTS FOUND. PERFORMED ENGINE RUNS AND COULD NOT DUPLICATE ODOR OR SIGNS OF SMOKE. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 27,416 hrs · 15,911 cycles

DURING MX INSPECTION, DISCOVERED THE EMERGENCY EXIT SIGN AT SEAT 3C WOULD NOT ILLUMINATE. MX R & R NR 2 EMERGENCY LIGHT INVERTER, OPS CHECKED GOOD. ACFT APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — CONTAMINATED · airframe 26,657 hrs · 15,424 cycles

CREW REPORTED SMOKE IN COCKPIT IMMEDIATELY AFTER TAKEOFF AND PERFORMED AIR TURN BACK. MAINTENANCE INSPECTED ACFT AND DETERMINED THE ACFT WAS DE-ICED PRIOR TO TAKEOFF AND FOUND DE-ICE FLUID IN BOTH ENGINE INLETS. MAINTENANCE REMOVED FLUID AND RAN ENGINES AND PACKS WITH NO SMOKE NOTED. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — GOUGED (FRAMES 21-22) · airframe 26,422 hrs · 15,290 cycles

DURING MAINTENANCE INSPECTION, THE LT FUSELAGE SKIN AFT OF THE PAX DOOR BETWEEN STRINGERS 13 & 14L AND FRAMES 21-22 FOUND TO BE GOUGED BEYOND LIMITS. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A FILLER-DOUBLER REPAIR IAW SRM 53-21-01, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: COFFEEMAKER — SMOKE (GALLEY) · airframe 25,954 hrs · 15,003 cycles

DURING GROUND OPERATIONS, THE CREW NOTED A SMOKE ODOR IN CABIN AND ELECTED TO RETURN TO THE GATE. MAINTENANCE DETERMINED THE SOURCE OF THE SMOKE TO BE THE RT COFFEE BREWER. THE BREWER WAS REPLACED, OPS CHECKS PERFORMED AND THE DISCREPANCY CLEARED.

Part: RIB — CRACKED (WHEELWELL) · airframe 25,020 hrs · 14,416 cycles

DURING 2A INSPECTION, THE RT WHEELWELL AFT RIB WAS FOUND TO HAVE MULTIPLE CRACKS. MX REMOVED THE CRACKED SECTION OF RIB AND PERFORMED A FILLER & DOUBLER REPAIR IAW EC5320-01974 AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 25,020 hrs · 14,416 cycles

DURING 2A INSPECTION, FUSELAGE SKIN WAS FOUND TO BE CRACKED FR 42 BELOW S2R. MX REMOVED THE DAMAGE AND PERFORMED EC5330-02353, AND ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,550 hrs · 13,509 cycles

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE RT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MX R & R THE NR 4 EMERGENCY LIGHT POWER SUPPLY, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,548 hrs · 13,508 cycles

AFT OVERWING EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 BATTERY POWER SUPPLY. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,845 hrs · 12,398 cycles

ON SCHEDULED MX INSPECTION, THE OVERHEAD EMERGENCY EXIT LIGHT IN THE GALLEY WAS FOUND INOPERATIVE. MX R & R THE LAMP WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 16,945 hrs · 9,305 cycles

SHV - DURING C-CHECK, SKIN CRACKED AROUND RIVETS FR 79 STR 3R-5R. REPAIRED SKIN IAW EC5330-02248. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 16,945 hrs · 9,305 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM CORRODED AT FR 24. REPAIRED AT FR 24 IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,945 hrs · 9,305 cycles

SHV - DURING C-CHECK CARGO DOOR LOWER CUTOUT CORRODED. REMOVED AND REPLACED CARGO DOOR LOWER CUTOUT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 16,945 hrs · 9,305 cycles

SHV - DURING C-CHECK - LT OMEGA BEAM CORRODED AT FR 19-23. REPAIRED LT OMEGA BEAM IAW EC5320-01229. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 15,795 hrs · 8,665 cycles

EXIT SIGN ABOVE FWD F/A SEAT INOP. REMOVED AND REPLACED NR 1 E/L INVERTER IAW EMB 145 AMM 33-50-11, OPS CHECK GOOD.

Part: SLEEVE — BURNED (NR 2 PACK) · airframe 15,013 hrs · 8,251 cycles

IAH - FLIGHT 2857 THE CREW REPORTED A BURNING SMELL AFTER TAKE OFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED A BURNT SLEEVE ON THE NUMBER TWO PACK DUAL TORQUE MOTOR, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 15,012 hrs · 8,250 cycles

IAH - ON DESCENT THE CREW REPORTED HEARING A LOUD GRINDING NOISE SEEMING TO COME FROM THE FWD AVIONICS COMPARTMENT (BEHIND THE CAPTS LEFT FOOT PEDAL) ASSOCIATED WITH A BURNING SMELL. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AVIONICS COMPARTMENT WITH NO DEFECTS OR SMELL NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 13,846 hrs · 7,602 cycles

FLIGHT 2142 - MKE - FLIGHT CREW REPORTED BURNING RUBBER SMELL IN THE COCKPIT, EICAS SCREEN WENT DARK AND C/B POPPED. MX REMOVED AND REPLACED EICAS DISPLAY UNIT, RESET THE C/B AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: STRUCTURE — CORRODED (DOOR FRAME) · airframe 12,118 hrs · 6,694 cycles

SHV-DURING C-CHECK CARGO DOOR CUTOUT INTERNAL LWR FWD AREA IS CORRODED. MX REPAIRED CARGO DOOR CUTOUT INTERNAL LWR FWD AREA IAW EC5330-01458. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · airframe 12,118 hrs · 6,694 cycles

SHV-DURING C-CHECK CARGO DOOR SHEAR CLIP AT FRM 65 HAS SIGNS OF CORROSION (MARKED) AT CUT OUT. MX REPAIRED CARGO DOOR SHEAR CLIP AT FRM 65 IAW EC 5330-01458. THE ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (CARGO BAY)

FLT 0023 - OKC - FLIGHT CREW REPORTED BAGGAGE SMOKE INDICATION ON EICAS. SYSTEM WAS RESET AS PER MAINTENANCE CONTROL INSTRUCTIONS. OPERATIONALLY CHECKED SATISFACTORY AND ACFT WAS RELEASED TO RETURN FOR SERVICE. (S)

Part: ACTUATOR — INOPERATIVE (HORIZ STAB) · airframe 10,982 hrs · 6,005 cycles

FLT 223 - SAT - FLIGHT CREW REPORTED MAIN PITCH TRIM FAIL INFLIGHT. MX PERSONNEL REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR OPERATIONALLY CHECKED SATISFACTORY, AIRCRAFT WAS RELEASED TO RETURN FOR SERVICE.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 9,156 hrs · 4,956 cycles

FLT 9 - COS TO ONT - FLIGHT CREW REPORTED BAG SMOKE INDICATION IN-FLIGHT. CONTRACT MX PERSONEL INSPECTED CARGO COMPARTMENT AND NO ABNORMALITIES WERE NOTED. AIRCRAFT WAS RELEASE IN ACCORDANCE WITH MEL 26-15-00 CAT -C- CONTROL 126970. WHEN AIRCRAFT ARRIVED TO ONT, EXPRESSJET MX PERSONEL REMOVED THE FWD AND THE AFT BAGGAGE COMPARTMENT SMOKE DETECTORS (FWD: P/N 473597-13, S/N 1777 TSN 14842 CSN 11464 TSO 14842. AFT:P/N 47359-13, S/N 2935 TSN 10975 CSN 8517 TSO 10975) AND REPLACED THEM. OPERATIONALLY CHECK WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 8,762 hrs · 4,739 cycles

SCHEDULE MX - SVC/RTN - ONT - DURING OVERNIGHT INSPECTION MX PERSONAL FOUND LEFT AND RIGHT HANDS EXTERIOR OVERWING EMERGENCY LIGHTS INOPERATIVE. MX PERSONAL REMOVED AND REPLACED NR 4 BATTERY CHARGER ASSY MAS PER EMB 145 AMM 33-50-04, OPS CHECKS GOOD. A/C WAS APPROVED TO RETURN TO SERVICE.

Part: INDICATION SYS — MALFUNCTIONED (CARGO DOOR) · airframe 8,395 hrs · 4,541 cycles

FL 22 - ONT TO TUL - AIR RETURN DUE TO BAGGAGE DOOR OPEN ON EICAS. CREW RETURNED TO ONT. MX INSPECTED BAGGAGE DOOR AND FOUND NO EVIDENCE OF BAGGAGE DOOR BEING OPEN IN FLIGHT. MX FOUND AN INDICATION PROBLEM. A/C WAS RELEASE IAW MEL 52-70-00/2 CAT-C CONTROL 121022. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.