N21129

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 49,183 hrs · 32,045 cycles

MULTIPLE EXTERIOR AND INTERIOR EMERGENCY LIGHT INOPERATIVE. SUSPECT BAD BATTERY. REMOVED AND REPLACED EMERGENCY BATTERY 3. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 49,108 hrs · 31,968 cycles

INTERIOR EMERGENCY LIGHS ABOVE SEATS 18A AND 18CD INOPERATIVE. REMOVED AND REPLACED BOTH BULBS. OPS CHECK SAT.

Part: TRIM PANEL — UNSECURE (ZONE 800) · airframe 49,029 hrs · 31,888 cycles

SERVICE DOOR HARD TO OPEN OR CLOSE. FOUND DOOR TO BE BINDING ON TRIM. RESECURED TRIM. OPS CHECK GOOD.

Part: LOCK — OUT OF ADJUST (ZONE 800) · airframe 48,939 hrs · 31,798 cycles

MCD NOT SEALED FULLY WHILE SHOWING CLOSED. REMOVED THE SIDE HINGE MAIN DOOR LINING. SERVICED AND ADJUSTED ACTUATING AND LOCKING MECHANISM OF MCD. UPS/LEAK CHECK SAT. PERFORMED PRESSURIZATION CHECK. LEAK CHECK SAT. INSTALLED MCD LINING.

Part: MANIFOLD — LEAKING (HYD SYSTEM) · airframe 48,903 hrs · 31,765 cycles

HYD SYSTEM 1 FAIL WITH MFD HYD SYSTEM INDICATION ZERO. REMOVED AND REPLACED LH HYD MANIFOLD ASSEMBLY. OPS/LEAK CHECK SAT.

Part: SKIN — MECHANIC ERROR (RUDDER) · airframe 48,834 hrs · 31,701 cycles

2 MISDRILLED HOLES ON RUDDER II ABOVE ACCESS PANEL 327CL. REMOVED DAMAGE ON RUDDER 2 ABOVE ACCESS PANEL, FABRICATED REPAIR PARTS, LOCATED AND DRILLED HOLES. PREP, PRIMED DOUBLER AND FILLER. INSTALLED DOUBLER AND FILLER REPAIR PARTS ON RUDDER 2 ABOVE ACCESS PNL 327CL.

Part: SKIN — DAMAGED (ZONE 100) · airframe 48,834 hrs · 31,701 cycles

DAMAGE TO THE LH REAR FUSELAGE 1 AT FRAMES 70 TO 72 AND STRINGERS 16L-18L. PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION ON AND AROUND DAMAGED AREA OF LH REAR FUSELAGE I FROM FRAMES 70-72, STRINGERS 16L-18L. NO INDICATION OF CRACKS FOUND AT THIS TIME. REMOVED DAMAGE BY CUTOUT AT LH FR70 TO FR72 BTW STR 16L TO 18L. INSPECTED 2 CUTOUT AREAS. FABRICATED PARTS 1 DOUBLERS 2 FILLERS 2024T3 0.080" AND 2024T3 0.063. DEBURED AND COUNTERSINK HOLES AT DOUBLER. INSTALLED DOUBLER AND FILLERS 2EA AT LH SIDE FR70 TO FR72 BTW STGR 16L TO STGR 18L.

Part: DOUBLER — DAMAGED (RUDDER) · airframe 48,834 hrs · 31,701 cycles

FOUND DOUBLER ON RUDDER 1 FRON LH SIDE TO BE DAMAGED. REMOVED RUDDER 2. REMOVED RUDDER 1. REMOVED DOUBLER ON RUDDER 1. FABRICATED NEW DOUBLER W/ 2024-T3 0.040". TRANSFERRED HOLES TO NEW DOUBLER. INSTALLED DOUBLER ON RUDDER 1. APPLIED FILLET SEAL TO DOUBLER. INSTALLED RUDDERS. CONNECTED THE ENDS OF THE ACTUATOR TO RUDDER. PERFORMED CHECK ON VERTICAL STABILIZER SEAL.

Part: PANEL — DAMAGED (ZONE 300) · airframe 48,834 hrs · 31,701 cycles

DURING INSPECTION FOUND SURFACE CORROSION INSIDE PANEL 335GB ON LH ELEVATOR. REMOVED LH ELEVATOR. REPLACED LH ELEVATOR TIP. INSTALLED LH ELEVATOR. INSTALLED NEW HARDWARE TO ATTACH TORQUE TUBE TO STABILIZER STRUCTURE. BALANCED L ELEVATOR. INSTALLED ELEVATOR AND TAB. PERFORMED SERVO TAB DEFLECTION TEST ON LH ELEVATOR SERVO TAB DEFLECTION VALUE IS .46 DEGREES AVERAGE, DEFLECTION COMPLETED. PERFORMED RVDT/RVITS CALIBRATION PROCEDURE. CALIBRATION COMPLETE.

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 47,437 hrs · 30,402 cycles

FOUND RH FORWARD LOWER FAIRING EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED RH FORWARD LOWER FAIRING EXTERNAL EMERGENCY LIGHT. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE (UNKNOWN) · airframe 47,437 hrs · 30,402 cycles

FOUND FWD CENTER INTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY #4. OPS CHECK SAT. REMOVED AND REPLACED FWD CENTER INTERIOR EMERGENCY EXIT LIGHT. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 47,259 hrs · 30,231 cycles

OVERWING PASSENGER EXIT SIGN FALLING DOWN (CENTER). RESECURED EXIT SIGN. OPS CHECK SAT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 46,784 hrs · 145,703 cycles

ENTRANCE BEAM HAS CORROSION. REMOVED FLOOR SUPPORT BEAM AND REPLACED WITH NEW.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 46,784 hrs · 29,792 cycles

2 FLOOR DOUBLERS IN FRONT OF SERVICE DOOR CORRODED. INSTALLED DOUBLERS.

Part: SNAP RING — WORN (PAX DOOR) · airframe 46,073 hrs · 29,162 cycles

MAIN CABIN DOOR NOT OPENING FROM INSIDE. FOUND SNAP RING ON INTERMEDIATE TORQUE TUBE WORN AND OUT OF PLACE. REMOVED AND REPLACED SNAP RING. OPS CHECK SAT

Part: NONE — NONE · airframe 45,745 hrs · 28,871 cycles

LG AIR/GROUND FAIL, DID NOT RETRACT ON TAKEOFF AFTER 400FT. PLACED AIRCRAFT ON JACKS TO TROUBLESHOOT FAULT, WHILE AIRCRAFT IS OFF GROUND, AIRCRAFT GOES INTO ESSENTIAL MODE WITH "ELEC ESS ERF FAIL" MESSAGE ON EICAS. PERFORMED FIM, FAILURE ON ESSENTIAL BUS CONTACTOR #2. FOUND NO GROUND SIGNAL AT PIN E ON CONNECTOR J1150. TIGHTENED LOOSE CANNON PLUG ON P0775 OPS CHECK LANDING GEAR SWING SAT.

Part: BATTERY PACK — INOPERATIVE · airframe 44,734 hrs · 27,962 cycles

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED #3 EMERGENCY BATTERY. OPS CHECK GOOD.

Part: NONE — NONE · airframe 44,564 hrs · 27,805 cycles

RH AFT EMERGENCY LIGHT INOPERATIVE. R&R AFT EMERGENCY LIGHT BULB. OPS CHECK SAT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,333 hrs · 27,575 cycles

EMERGENCY LIGHT ABOVE PAX DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ABOVE PAX DOOR. OPS CHECK SAT

Part: GUSSET — CORRODED · airframe 44,165 hrs · 27,437 cycles

FF2 LH INBD FLOOR GUSSET FOUND CORRODED FR 8-13. DOUBLER CUT. FF2 LH INBD FLOOR GUSSET BTW FR 8-13 REPLACED WITH REPAIR DOUBLER.

Part: FLANGE — CRACKED · airframe 44,165 hrs · 27,437 cycles

RH PYLON YOKE UPPER FLANGE HOLE (X1) FOUND WITH CRACK. RH PYLON YOKE UPPER FLANGE HOLE REAMED. AFTER NDT INSPECTION, DAMAGE IS STILL PRESENT AT RH PYLON YOKE UPPER FLANGE. HOLE OVERSIZED AT SECOND PERMISSIBLE DIMENSION (0.421). 2 BUSHINGS LOCALLY FABRICATED. RH PYLON YOKE UPPER FLANGE REPAIRED WITH INSTALLATION OF REPAIR BUSHINGS

Part: SKIN — CORRODED (FRM 23 S16-17R) · airframe 44,165 hrs · 27,437 cycles

CF1 ON RH FUSE AT FR23 AT LEVEL JUNCTION STRINGER SPLICE STR 16R-17R-18R CORRODED. CORROSION ON STR 16R AND 17R AT FR 23 RH FUSE BLENDED AND FOUND WITHIN LIMIT. NO SIGNIFICANT LOSS OF MATERIAL. CORROSION ON STR 18R AT FR 23 BLENDED, FOUND OUT OF LIMITS. STR 18R, BTW FR 20-21 REPAIRED WITH SPLICE. NO FAULT FOUND

Part: BEAM — CORRODED · airframe 44,165 hrs · 27,437 cycles

CF1 ON LH FUSE OMEGA BEAM LH AND REPAIR ANGLE CORRODED. OMEGA BEAM REPLACED AND INSTALLED

Part: DOUBLER — CORRODED · airframe 44,165 hrs · 27,437 cycles

CF 1 ON RH FUSE BTW FR 19-20 SILL ASSEMBLY FWD AND DOUBLER SILL AFT CORRODED. CF1 ON RH FUSE BTW FR 19-20 SILL ASSY FWD CORROSION REMOVED WITHIN LIMITS AND REPROTECTED. LESS THAN .001" REMOVED. DVI INSP C/OUT WITH MAGN GLASS 30X NO FAULT FOUND. CF1 RH SILL AFT BTW FR 19-20 PREVIOUS REPAIR DOUBLER CORROSION REMOVED OUT OF LIMITS, NEW REPAIR DOUBLER FABRICATED. CF1 ON RH FUSE BTW FR 19-20 SILL ASSY FWD DOUBLER SILL AFT INSTALLED

Part: FLANGE — CORRODED · airframe 44,165 hrs · 27,437 cycles

FRAME 65 LOWER FLANGE AT STR 16L CORRODED. FRAME 65 LOWER FLANGE AT STR 16L BLENDED OUT OF LIMIT. CUT OUT ON FR65 LOWER FLANGE AT STR 16L REPAIRED.

Part: DOOR FRAME — CORRODED · airframe 44,165 hrs · 27,437 cycles

CORROSION FOUND ON CARGO DOOR FRAME 65 BTW STR 16 & 17. CARGO DOOR FR65 BTW STR 16L AND 17L CORROSION REMOVED OUT OF LIMITS. FR65 CUT AND SPLICE MFG BTW STR 14L-15L. CARGO DOOR FRAME 65 LH BTW STR 14-15 REPAIRED.

Part: TUBE — CRACKED (BLEED AIR DUCT) · airframe 44,020 hrs · 27,305 cycles

ON CLIMB OUT AT 6000 FEET E2 BLEED LEAK MESSAGE ON EICAS. FOUND LEAKING JOINT BLOWING HOT AIR ON SENSOR LOCATION #26. FOUND "T" TUBE BEFORE CROSSBLEED VALVE CRACKED. REMOVED RH BLEED VALVE, RH PACK VALVE, RH A/I VALVE, RH ATS VALVE AND ATTACHING DUCT TO FACILITATE BLEED LEAKAGE TEST. PERFORMED RH AIR BLEED SYSTEM LEAK TEST. LEAK TEST FAIL FOUND GROUND AIR START VALVE TO BE LEAKING. R&R GROUND CONNECTION VALVE. REPLACED LEAKING O-RINGS AT POSITION #26. REPLACED T DUCT AT CROSS BLEED VALVE. PERFORMED RH BLEED AIR SYSTEM LEAK TEST. OPS CHECK LEAK CHECK SAT.

Part: SKIN — DAMAGED (LT WING) · airframe 44,016 hrs · 27,301 cycles

LH WING L/E NO 3 REPAIR FOUND BTW RIB 22-23 ON NOSE SKIN. LH WING L/E #3 REPAIR REWORKED.

Part: SKIN — DENTED (RT WING) · airframe 44,016 hrs · 27,301 cycles

RIGHT WING L/E NR 1 DENT ON SKIN 4.0 FEET FROM INBOARD EDGE AND 7.5" FROM TOP EDGE. RT WING L/E NR 1 SKIN REPAIRED.

Part: SKIN — DENTED (ZONE 100) · airframe 44,016 hrs · 27,301 cycles

ON RH FUSE SKIN BTW FR 12-11 AND STR 20-21 2 DENTS FOUND. DENT #1 ON RH FUSE SKIN FROM 0650 FWD FR 11 AND 2100 ABOVE STR 21R DENT DRILLED 0185 AND INSTALLED RIVET PLUG. RH FUSE SKIN BTW FR 12-11 AND STR 20-21R DENT #2 IS AN EXISTING BLEND REMAINING 025 AND 032 BLEND IS OUT OF LIMITS AND REPAIRED.

Part: RUDDER — CHAFED · airframe 44,016 hrs · 27,301 cycles

RUDDER 1, LT SKIN CHAFFED 8 INCH FROM LOWER EDGE, 12 INCH LONG. CHAFFED LT SKIN OF RUDDER 1 AT LOWER EDGE REPAIRED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 44,016 hrs · 27,301 cycles

REAR FUSELAGE II, LT SIDE, AT FR 77-78-79, BTW STR 3-8 MULTIPLES REPAIR BUSHING. REAR FUSE II AT FR 77 BTW STR 3-4L SKIN REPAIRED AT THE 2 CONSECUTIVE REPAIR BUSHING LOCATIONS.

Part: SKIN — DENTED (ZONE 200) · airframe 44,016 hrs · 27,301 cycles

RH FUSE BTW FR 2-3 AND BTW STR 11-13, SKIN DENTED. RH FUSE SKIN BTW FR 2-3 STR 11-13 REPAIRED

Part: SKIN — DENTED (ZONE) · airframe 44,016 hrs · 27,301 cycles

ON RH FUSE DENT FOUND BTW FR26 AND FR25 AND BTW STR 13R AND 14R. DENT IS OUT OF LIMITS. DENT DIMENTION L 0.800 W 0.600 H 0.020. RH FUSE SKIN BTW FR26 & FR25 BTW STR 13R & 14R REPAIRED.

Part: SKIN — DAMAGED (ZONE 200) · airframe 44,016 hrs · 27,301 cycles

SUSPICIOUS BLEND ON RH FUSELAGE SKIN AT FR 68 BTW STR 18-19. DOUBLER REPAIR ON RH LOWER REAR FUS-1, AT FRAME 68, BTW STR 18R-19R REPAIRED

Part: SKIN — NOT REPORTED (FRAMES 26-27) · airframe 44,016 hrs · 27,301 cycles

REPAIR DOUBLER ON RH CENTER FUSE 2, BTW FR 26-27 AND BTW STR 16R-18R. REPAIR DOUBLER ON RH FUSELAGE 2, BTW FR 26-27, AND STR 16R-18R REWORKED

Part: VALVE — INOPERATIVE (CARGO BAY) · airframe 43,913 hrs · 27,219 cycles

BLEED 2 OVERHEAT. REMOVED CARGO FLOOR TO INSPECT REFERENCE LINES. REMOVED AND REPLACED #2 FAN AIR VALVE. FOUND NO DEFECTS. OPS CHECK GOOD. AIRCRAFT GOOD FOR SERVICE. MORE INFORMATION AVAILIBLE LATER.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 43,838 hrs · 27,157 cycles

SMOKE IN COCKPIT WITH ASSOCIATED BURNING SMELL. PERFORMED INSPECTION AND OPS CHECK OF CAPT'S AND F/O'S CHART HOLDER LAMPS. NO SMOKE OR BURN SIGNS. INSPECTED RELAY BOX AND RELAY WITH POWER ON AIRCRAFT. NO SIGN OR SMOKE NOTED. INSPECTED L/H AND R/H SIDE WINDSHIELD HEATING SENSORS AND TEMP CONTROLLERS. NO BURN SIGN OR SMOKE NOTED. INSPECTED COCKPIT EMERGENCY FLASH LIGHTS. NO BURN SIGNS OR SMOKE NOTED. REMOVED CAPT'S SIDE SPEAKER LINING AND PERFORMED INSPECTION. NO BURN OR SMOKE NOTED. COULD NOT DUPLICATE SMOKE ISSUE. AIRCRAFT RETURNED TO SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 42,858 hrs · 26,322 cycles

ABORTED TAKE OFF AT 60KTS. PITCH TRIM T/O CONFIG WARNING. PITCH TRIM INDICATOR NEEDLE MOVING, BUT SETTING STAYS AT 8. RERACKED AURAL WARNING UNIT, CLEANED HSCU CONNECTORS, HORIZ (STAB) ACTUATOR POTS. PERFORMED T/O CONFIG TEST, CHECKS GOOD. VERIFIED HORIZ STAB MARKINGS MATCH INDICATION IN COCKPIT.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 42,609 hrs · 26,114 cycles

FLAP FAIL ON EXTENSION DURING APPROACH UPON FLAPS 9 EXTENSION, PERFORMED GVI OF FLAPS, RESET FLAP SYSTEM. OPS CHECK GOOD. AC OK FOR SERVICE

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 42,092 hrs · 25,732 cycles

CARGO DOOR Z ANGLE HAS CORROSION. REMOVED AND REPLACED CARGO DOOR Z ANGLE.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 42,092 hrs · 25,732 cycles

STOP SIGN ON RT SIDE AT FRAME 20 HAS CORROSION. REMOVED AND REPLACED STOP SIGN ON RT SIDE AT FRAME 20.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 42,092 hrs · 25,732 cycles

STOP SIGN ON RT SIDE AT FRAME 22 HAS CORROSION. REMOVE AND REPLACED STOP SIGN AT FRAME 22.

Part: LINE — LOOSE (NR 2 ENGINE) · airframe 41,662 hrs · 25,400 cycles

ENGINE 2 SHUTDOWN IN FLIGHT STARTING DESCENT DUE TO E2 LOW OIL PRESSURE EICAS MSG. R&R NR 2 ENG AFT TUBE OIL LINE TO OUTER BYPASS, OPS AND LEAK CHECK GOOD.

Part: COFFEEMAKER — SHORTED (GALLEY) · airframe 40,975 hrs · 24,836 cycles

SMOKE IN GALLEY COMIMG FROM COFFEE MAKER AREA. F/A DISCHARGED FIRE EXTINGUISHER. A/C LANDED IN ROC AND WAS FARRIED TO ORD FOR MX. R&R COFFEE MAKER AND PORTABLE FIRE EXTINGUISHER. ALSO R&R COFFEE MAKER RAIL AND FUSE. ALL OPS CHECKS GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 39,718 hrs · 23,801 cycles

STEERING INOP MESSAGE ON EICAS. PERFORMED MIP1.91, MIP SUCCESSFUL. NO FURTHER ACTION REQ.

Part: ACM — ODOR (LEFT) · airframe 39,118 hrs · 23,315 cycles

ACRID BURNING ODOR AFTER THE NR 2 ENGINE WAS STARTED, HAZE FILLED THE FLIGHT DECK. SMELLED LIKE ELECTRICAL AND RUBBER. R & R THE NR 1 PACK ACM. OPS CHECKED GOOD.

Part: ACM — ODOR (LEFT) · airframe 39,118 hrs · 23,315 cycles

ACRID BURNING ODOR AFTER THE NR 2 ENGINE WAS STARTED, HAZE FILLED THE FLIGHT DECK. SMELLED LIKE ELECTRICAL AND RUBBER. R & R THE NR 1 PACK ACM. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,421 hrs · 21,835 cycles

LT EMERGENCY DOOR FLOOD LIGHT NR 21 INOP. R&R LT EMERGENCY DOOR FLOOD LIGHT NR 21 BULB, OPS CHECK GOOD.

Part: SHEAR TIE — CORRODED (FRAME 68) · corrosion level 2 · airframe 35,156 hrs · 20,169 cycles

DURING C-CHECK, THE SHEAR CLIP AT FRAME 68 WAS FOUND TO BE CORRODED BETWEEN STRINGERS 16L-17L. MAINTENANCE PERFORMED A SPLICE REPAIR IAW EC5330-03067. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAME 61) · corrosion level 2 · airframe 35,156 hrs · 20,169 cycles

DURING C-CHECK, THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 61. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW SRM 53-24-10. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FRAMES 65-68) · corrosion level 2 · airframe 35,156 hrs · 20,169 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: ENGINE — ODOR (NR 1) · airframe 33,599 hrs · 19,099 cycles

THE CREW REPORTED AN ACRID ODOR COMING FROM 1 OR BOTH PACKS. DESELECTING PACK NR 1 MITIGATES THE ODOR. MAINTENANCE REPLACED THE NR 1 ENGINE. OPS CHECKS WERE GOOD.

Part: ACM — CONTAMINATED · airframe 33,566 hrs · 19,076 cycles

THE CREW REPORTED THAT PACK 1 AND PACK 2 SMELLED LIKE BURNING OIL WHEN ON, ENGINE BLEEDS IN FLIGHT. THE ACFT LANDED WITHOUT INCIDENT, WHERE MAINTENANCE INSPECTED THE ACFT AND FOUND EVIDENCE OF APU INGESTION OF ANTI-ICE FLUID, OPERATIONALLY TESTED BOTH PACKS USING ENGINE BLEEDS WITH NO SMELL NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — SHORTED (LT OVERWING) · airframe 30,272 hrs · 16,978 cycles

THE LT OVERWING EMERGENCY LIGHT WAS DISCOVERED INOPERATIVE WITH ASSOCIATED LT AND RT EXIT IDENTIFIERS. MAINTENANCE TROUBLESHOT AND FOUND THE LT EXTERIOR LIGHT ASSY INTERNALLY SHORTED. MAINTENANCE R & R THE LT OVERWING EXTERIOR EMERGENCY LIGHT ASSY WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (ZONE 600) · airframe 29,914 hrs · 16,766 cycles

DURING C-CHECK THE RT AILERON PCA ATTACH FITTING BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MAINTENANCE R & R THE BRACKET IAW EC5750-01177, REV C. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 29,914 hrs · 16,766 cycles

DURING C-CHECK, FRAME 75 TO VERTICAL STABILIZER FITTING WAS FOUND CORRODED. MAINTENANCE REMOVED THE CORROSION AND REPAIRED THE FITTING IAW EC 5310-01317. ACFT APPROVED FOR RETURN TO SERVICE.

Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 29,914 hrs · 16,766 cycles

DURING C-CHECK, THE HORIZONTAL STABILIZER LEFT HINGE PIN FITTING WAS FOUND TO HAVE CORROSION. MAINTENANCE R & R THE HINGE FITTING IAW EC5510-01240. AIRCRAFT APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — WORN (ZONE 500) · airframe 29,914 hrs · 16,766 cycles

DURING C-CHECK, THE LEFT SPOILER INBD ATTACHMENT BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MX R & R THE BRACKET IAW AMM 57-51-02. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 29,914 hrs · 16,766 cycles

DURING C-CHECK, THE LT HORIZONTAL STABILIZER L/E WAS FOUND TO BE CORRODED AROUND RIVET HEADS ON THE UPPER SURFACE. MAINTENANCE REMOVED THE CORROSION AND REPAIRED THE L/E IAW EC5510-01214, REV B. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,914 hrs · 16,766 cycles

DURING C-CHECK, SHEAR TIE AT FRAME 65 BETWEEN STRINGERS 15-16L FOUND TO BE CORRODED. MX REMOVED CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5320-01494. ACFT APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (ZONE 200) · airframe 29,914 hrs · 16,766 cycles

DURING C-CHECK, LEFT AFT SKIN WAS FOUND TO BE CRACKED AROUND SEVEN FASTENERS BETWEEN FRAMES 77-79 AND STRINGERS 4L-5L. REAMED AND PERFORMED A BUSHING REPAIR IAW EC5330-02022. ACFT APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 29,914 hrs · 16,766 cycles

DURING C-CHECK THE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59-60. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01473. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — OUT OF ADJUST (RT MLG) · airframe 23,667 hrs · 12,800 cycles

SDF FLT 2010 THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE UPON EXTENDING LANDING GEAR. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR NR 2 PROXIMITY SWITCH. ADJUSTED THE GAP ON THE RIGHT GEAR NR 1 PROXIMITY SWITCH AND SERVICED BOTH LEFT AND RIGHT GEARS. OPERATIONAL CHECKS WERE GOOD.

Part: ELECTRONIC UNIT — FAULTY (COCKPIT) · airframe 23,616 hrs · 12,759 cycles

ORD FLT 6134 THE CREW REPORTED A AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: ACM — MALFUNCTIONED (NR 2) · airframe 22,506 hrs · 12,054 cycles

FLIGHT 2400 - EWR - FLIGHT CREW REPORTED PACK NR 2 LOUD NOISE AND SMOKE IN CABIN. EWR MX REMOVED AND REPLACED NR 2 ACM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 20,378 hrs · 10,877 cycles

FLIGHT 3099 - EWR - FLIGHT CREW REPORTED NR 1 SMELLED BURNING OIL AND HAD A SMALL AMOUNT OF SMOKE EMITTING FROM THE COWLING OBSERVED DURING POST-FLIGHT INSPECTION. EWR MX RAN ENGINE FOR SEVERAL MINUTES AND PERFORMED INSPECTION FOR LEAK AND SMOKE. NO LEAK NOR SMOKE DETECTED. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 19,691 hrs · 10,511 cycles

FLIGHT 2381 - AVL - FLIGHT CREW REPORTED AUTO PILOT FAIL IN FLIGHT. CREW DIVERTED FLIGHT AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT (HSCU) AND HORIZONTAL STABILIZER ACTUATOR (HSA) AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR NR C2XA10RI049 FOR THE HSCU AND SDR NR C2XA10RI050 FOR HSA.

Part: CONTROL UNIT — INOPERATIVE (HORIZ STAB) · airframe 19,691 hrs · 10,511 cycles

FLIGHT 2381 - AVL - FLIGHT CREW REPORTED AUTO PILOT FAIL IN FLIGHT. CREW DIVERTED FLIGHT AND LANDED UNEVENTFULLY. EWR MX REMOVED AND REPLACED HORIZONTAL STABILIZER CONTROL UNIT (HSCU) AND HORIZONTAL STABILIZER ACTUATOR (HSA) AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. SDR NUMBER C2XA10RI049 FOR THE HSCU AND SDR NUMBER C2XA10RI050 FOR HSA.

Part: COMPUTER — FAULTY (COCKPIT) · airframe 19,666 hrs · 10,500 cycles

IAH FLT 2836 THE CREW REPORTED THE PITCH TRIM INDICATIONS WOULD BLANK OUT IN FLIGHT CAUSING THE AUTO-PILOT TO FAIL. THE PRIMARY AND STANDBY TRIM STILL WORKED CORRECTLY. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 IC600 COMPUTER. OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — UNKNOWN · airframe 19,216 hrs · 10,234 cycles

FLIGHT 2055, THE CREW REPORTED A BLEED TWO LEAK. THE AIRCRAFT RETURNED WHERE IT LANDED WITHOUT INCIDENT. MX INSPECTED THE AIRCRAFT AND PERFORMED HIGH POWER RUNS WITH NO LEAKS OR DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 19,155 hrs · 10,200 cycles

SHV - DURING C-CHECK RT OMEGA BEAM DOUBLER AT FRAME 20 HAS CORROSION (LEVEL 2 LOCAL). MAINTENANCE REPAIRED RT OMEGA BEAM DOUBLER AT FRAME 20 IAW EMB-145 CPM 51-20-00. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ELECTRONIC UNIT — MALFUNCTIONED (COCKPIT) · airframe 18,482 hrs · 9,832 cycles

CLE - FLT 2332 - THE CREW REPORTED A LANDING GEAR AIR/GROUND FAIL MESSAGE ON THE EICAS IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE LGEU AND RELAYS KO824, KO025, KO352, KO453.

Part: FAN — INOPERATIVE (E&E BAY) · airframe 17,104 hrs · 9,094 cycles

FLIGHT 2997 - MSP - FLIGHT CREW REPORTED STRONG SMELL IN COCKPIT AND FWD CABIN. MX FOUND RT AVIONICS EXHAUST FAN INOPERATIVE. MX REMOVED AND REPLACED FAN AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: BALLAST — BURNED (CABIN) · airframe 16,903 hrs · 8,996 cycles

FLIGHT 2291 - EWR - FLIGHT CREW REPORTED ELECTRICAL BURNING SMELL IN CABIN AROUND SEAT 1A. EWR MX REMOVED AND REPLACED SEAT 1A BALLAST AND PERFORMED OPERATIONAL SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: BRACKET — WORN (RT AILERON) · airframe 14,222 hrs · 7,580 cycles

SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA BRACKET WAS WORN AND WOULD NOT CONTAIN THE HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — GOUGED (AILERON) · airframe 14,222 hrs · 7,580 cycles

SHV - DURING C-CHECK IT WAS FOUND THAT THE LT PCA BRACKET ON THE AILERON WAS GOUGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BRACKET IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 14,222 hrs · 7,580 cycles

SHV - DURING C-CHECK IT WAS FOUND THAT THE CARGO DOOR INNER SKIN HAD CORROSION AROUND SEVERAL SCREW HOLES. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5230-01173. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SWITCH — INOPERATIVE (LT MLG) · airframe 13,820 hrs · 7,381 cycles

IAH - FLIGHT 2185, THE CREW REPORTED THAT THE LEFT MAIN LANDING GEAR DISAGREE LIGHT WHEN THE GEAR WAS EXTENDED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN GEAR DOWNLOCK PROXIMITY SWITCH, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL LEVER — INOPERATIVE (MLG) · airframe 13,811 hrs · 7,377 cycles

IAH - FLIGHT 2365, THE CREW REPORTED A LANDING GEAR LEVER DISAGREE WARNING ILLUMINATED INFLIGHT WHILE THE LANDING GEAR WAS IN UP AND LOCKED POSITION. NORMAL INDICATIONS ACHIEVED WHEN GEAR WAS LOWERED. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR LEVER, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: HANDLE — LOOSE (CABIN DOOR) · airframe 13,572 hrs · 7,252 cycles

IAH - FLIGHT 2785, THE CREW REPORTED THAT THE MAIN CABIN DOOR COULD NOT BE OPENED FROM THE INSIDE. MAINTENANCE TIGHTENED THE INTERNAL HANDLE ON THE MAIN DOOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 13,407 hrs · 7,169 cycles

FLT 2596 - EWR - CREW REPORTED EICAS LAV SMOKE MESSAGE, NO CABIN FIRE OR SMOKE NOTICED. EWR MX PERFORMED OPERATIONAL CHECK IAW EMB 145 AMM SUCCESSFULLY AND COULD NOT DUPLICATE THE PROBLEM. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — INTERMITTENT (LAVATORY) · airframe 12,258 hrs · 6,593 cycles

FLT 2994 - EWR - CREW REPORTED FALSE LAV SMOKE ALARM IN FLIGHT. EWR MX REMOVED AND REPLACED LAV SMOKE SENSOR IAW EMB145 AMM 26-14-01 AND PERFORMED OPERATIONAL TEST SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SEAL — FAULTY (MAIN DOOR) · airframe 10,575 hrs · 5,723 cycles

CLE FLIGHT 2451 THE CREW REPORTED UPON ARRIVAL IN MKE THE F/A WAS UNABLE TO OPEN THE MAIN CABIN DOOR. MAINTENANCE INSPECTED AND REPLACED THE MAIN CABIN DOOR SEAL. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,331 hrs · 5,044 cycles

TYS DURING A CURRENT 2C INSPECTION THE LEFT LAV OMEGA BEAM TOP CAP WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE CORRODED AREA IAW EMB 145XR SRM 51-40-02 AND 51-20-02-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 2C INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,331 hrs · 5,044 cycles

TYS DURING A CURRENT 2C INSPECTION THE CENTER LAV OMEGA BEAM TOP CAP WAS FOUND CORRODED. MAINTENANCE REMOVED AND REPLACED THE THE CORRODED AREA IAW EMB 145XR SRM 51-40-02 AND 51-20-02-06. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF THE 2C INSPECTION.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 9,331 hrs · 5,044 cycles

TYS DURING A 2C INSPECTION BOTH GUSSETS ON THE RIGHT OMEGA BEAM IN THE GALLEY HAD SISNS OF CORROSION. MAINTENANCE REMOVED AND REPLACED THE RIGHT OMEGA BEAM AND BOTH GUSSETS IAW 145XR SRM 51-40-02 AND 51-20-03. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED WHEN THE C-CHECK INSPECTION IS COMPLIED WITH.

Part: ODOR — DETECTED (CABIN/COCKPIT) · airframe 5,843 hrs · 3,163 cycles

CREW REPORTED, "STRONG ODOR OF SMOKE IN CABIN AND COCKPIT". MX PERFORMED GENERAL VISUAL INSP OF BLEED SYSTEM DUCTS NR 1 AND NR 2 IAW EMB145XR AMM NR 36-11-09, NO DEFECTS NOTED. RAN BOTH ENGINES ON 2 DIFFERENT OCCASIONS IAW EMB145XR AMM NR 71-00-01 AT LOW AND HIGH POWER SETTINGS, CHECKED BOTH AIRBLEED SYSTEMS IAW EMB145XR AMM NR 36-00-00-700-803-A. NO SMOKE ODOR FOUND IN CABIN OR COCKPIT, SYSTEMS OPS CHECKED GOOD.

Part: FITTING — DAMAGED (RT AILERON) · airframe 4,842 hrs · 2,605 cycles

TYS, DURING A SCHEDULED INSPECTION THE RIGHT AILERON TO PCA ATTACH FITTING HOUSING WAS GOUGED AND ELONGATED. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW EMB-145XR-AMM 27-11-00 AND EC5750-01177.

Part: ENGINE — FAILED (RIGHT)

THE CREW REPORTED THAT ON DESCENT INTO IAH THE NUMBER TWO ENGINE FAILED (UNCOMMANDED SHUT DOWN). THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONAL CHECKED GOOD, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — FLAMED OUT (NR 2)

DURING CLIMBOUT THROUGH 27,000 FT THE NR 2 ENGINE FAILED. ATTEMPTS WERE MADE TO RESTART THE ENGINE WITHOUT SUCCESS. THE AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT INCIDENT WHERE THE AFFECTED ENGINE WAS REPLACED.

Part: SMOKE — DETECTED (CABIN)

IAH- FLIGHT 2719, THE CREW NOTED SMOKE IN THE CABIN DURING CLIMB, DID AN AIR RETURN, AND, LANDED WITHOUT INCIDENT. IAH- MAINTENANCE INSPECTED THE AIRCRAFT, AND, PERFORMED A OPERATIONAL CHECK OF THE AIR CONDITIONING SYSTEM, NO DEFECTS NOTED, AND, THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.