N17138

Part: ELEC CONNECTOR — FAULTED (FLAP SYS) · airframe 47,636 hrs · 30,712 cycles

FLAP FAIL, SPS ADVANCED EICAS MESSAGE DISPLAYED AFTER MOVING FLAP HANDLE DURING APPROACH. REMOVED AND REPLACED ELECTRICAL CONNECTOR PLUG P1104. FLAPS OPS CHECK GOOD. PERFORMED FLAP SCREWJACK ACTUATOR LUBRICATION ON ALL FLAP ACTUATORS. PERFORMED FLAP SCREWJACK ACTUATOR GEAR LUBRICATION ON ALL FLAP ACTUATORS OPS CHECK SAT, NO DEFECTS NOTED AT THIS TIME. PERFORMED INSPECTION OF FLAP SCREWJACK ACTUATORS SERVICING IAW. OPS AND LEAK CHECK SAT. NO DEFECTS NOTED AT THIS TIME.

Part: INVERTER — INOPERATIVE (ZONE 200) · airframe 47,594 hrs · 30,669 cycles

RIGHT EMERGENCY EXIT HATCH UPPER LIGHT PLACARD INOPERATIVE. REMOVED AND REPLACED INVERTER ASSEMBLY AT POSITION 5. OPS CHECK SAT.

Part: FLAP SYSTEM — FAILED · airframe 47,510 hrs · 30,592 cycles

FLAP FAIL WHILE MOVING FROM 9 TO 22. FLAP SURFACES AND FSL ARE SET TO 9 DEGREES. ALSO, CONNECTORS P3683 AND P3682 ARE DISCONNECTED AND SECURED FOR FLAPS 9 FERRY FLIGHT. STARTED ZERO RIGGING OF LH IB FLAP. COMPLETED ZERO RIGGING. OPS CHECK SAT. CONNECTORS P3683/P3682 RECONNECTED.

Part: PANEL — OUT OF POSITION (ZONE 800) · airframe 47,360 hrs · 30,454 cycles

MCD WONT CLOSE, TOP PANEL HAS GAP AND EXTERNAL HANDLE NOT FLUSH. PERFORMED MCD ADJUSTMENT/TEST AND PERFORMED CHECK WITH THE FORCE GAUGE. LOAD IS WITHIN LIMITS, FOUND RH UPPER ROLLER CAM TO BE LOOSE. RESECURED CAM. SERVICED/LUBRICATED MCD. MCD CYCLE OPEN/CLOSE. EXTERIOR HANDLE SITS FLUSH. OPS CHECK SAT, NO FURTHER DEFECTS NOTED AT THIS TIME. PERFORMED PRESSURIZATION CHECK. OPS CHECK FAIL. FOUND UPPER LH CORNER MCD FRAME SEAL TO BE LOOSE. RESECURED FRAME SEAL. PERFORMED ADJUSTMENT AND SERVICE EXTERIOR HANDLE SITS FLUSH OPS CHECK. NO DEFECTS FOUND AT THIS TIME. BUT PRESSURE CHECK FAIL, FOUND UPPER LH CORNER FRAME SEAL LOOSE. RE-SECURED SILL. PERFORMED PRESSURE/LEAK CHECK OF MCD. OPS CHECK SAT. NO OTHER DEFECTS NOTED. COMPLIED WITH SIDE HINGE MAIN DOOR ADJUSTMENT/TEST AND SERVICING. FOUND RH UPPER ROLLER CAM TO BE LOOSE. CAM RESECURED.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 47,345 hrs · 30,439 cycles

CENTER AISLE CEILING EMERGENCY LIGHT AT ROW 18 INOPERATIVE. REMOVED AND REPLACED ROW 18 CENTER AISLE CEILING EMERGENCY LIGHT. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 47,345 hrs · 30,439 cycles

MCD EXTERNAL EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EXTERNAL EMERGENCY LIGHT. OPS CHECK SAT.

Part: BOLT — LOOSE (ZONE 800) · airframe 47,247 hrs · 30,344 cycles

MAIN CABIN DOOR DIFFICULT TO CLOSE. FOUND INNER HANDLE BOX ATTACHMENT BOLTS TO BE LOOSE - TORQUED HANDLE BOX AND LUBRICATED DOOR. OPS CHECK SAT. NO FURTHER DEFECTS NOTED.

Part: HANDLE — FAULTED (ZONE 800) · airframe 47,230 hrs · 30,327 cycles

MCD EXTERIOR DOOR HANDLE NOT FULLY FLUSH. FA REPORTED LOUDER THAN NORMAL WHISTLING SOUNDS. RE-SEALED LOOSED FRAME SEAL. PERFORMED PRESSURIZATION CHECK. OPS CHECK, LEAK CHECK SAT. NO NOISES PRESENT. DOOR HANDLE SEATS FLUSH.

Part: DRIVE UNIT — FAILED (TE FLAPS) · airframe 47,021 hrs · 30,134 cycles

FLAP FAIL MESSAGE ON EICAS. NO FLAP CHANGE WHEN MOVING FLAP LEVER. REMOVED AND REPLACED FPDU. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 46,802 hrs · 29,926 cycles

MAIN CABIN DOOR UNLOCKING HANDLE LOWER ROLL PIN PULLED OUT RESECURED MAIN CABIN DOOR UNLOCKING HANDLE LOWER ROLL PIN.

Part: NONE — NONE · airframe 46,392 hrs · 29,554 cycles

PHOTO LUMINESCENT LIGHT STRIP LOOSE AT 3A. RESECURED EMERGENCY LIGHT STRIP AT 3A

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,137 hrs · 29,330 cycles

LH FWD WING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY CHARGER. OPS CHECK SAT.

Part: LAMP — INOPERATIVE · airframe 45,661 hrs · 28,905 cycles

MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED MCD EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT

Part: LIGHT — INOPERATIVE · airframe 45,452 hrs · 28,731 cycles

RH EXTERNAL LOWER EMERGENCY LIGHT RETAINER ASSY NOT FLUSH WITH FUSELAGE AND IS MISSING SEALANT. R&R EXTERNAL LOWER EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT.

Part: NONE — INOPERATIVE · airframe 45,264 hrs · 28,565 cycles

AC CABIN ALT RAPIDLY CLIMBED TO 8400 THEN 9000 FEET, CAB RATE CONTINUED TO -150. CAB ALT CONTINUED TO RISE. DID A RAPID DECENT AND EMERGENCY DECLARED. OPENED BOTH COCKPIT DV WINDOWS, INSPECTED SEALS, FOUND NO DEFECTS. THEN FULLY CLOSED BOTH WINDOWS. REMOVED AND REPLACED DIGITAL CONTROLLER. PERFORMED REACTIVATION OF THE OUTFLOW VALVES. PERFORMED PRESSURIZATION CONTROL SYSTEM FUNCTIONAL TEST. OPS CHECK SAT

Part: NONE — LEAKING · airframe 45,180 hrs · 28,489 cycles

BRAKE DEGRADED CAUTION MESSAGE ON FINAL APPROACH. ALL WHEEL SPEED SENSORS CHECKED AND FOUND SATISFACTORY. AIRCRAFT TAXIED OUT AND FOUND #2 BRAKES ON MFD HOTTER THAN ALL OTHER WHEELS. AIRCRAFT JACKED AND FOUND #2 BRAKES BINDING. REMOVED AND REPLACED #2 BRAKE ASSEMBLY. OPS CHECK SAT FOR THE TEMPERATURE ISSUE. DURING BLEEDING OF BRAKE IT WAS NOTED THAT THE BRAKE WAS GIVING FIRST BLEED AND THEN THE HYDRAULIC FLUID STOP FLOWING. SAME ON RIGHT SIDE. DFDR SHOWS NO PRESSURE ON THE #1 BRAKE. THIS WILL CAUSE THE BRAKE TEMPS TO RISE DURING BRAKING DUE TO THE #2 BRAKE PROVIDING ALL BRAKING POWER FOR THE LH GEAR. LEAK CHECK SAT

Part: LAMP — INOPERATIVE · airframe 45,176 hrs · 45,176 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT LAMP. OPS CHECK SAT.

Part: BATTERY PACK — INOPERATIVE · airframe 45,176 hrs · 28,485 cycles

LH FWD WTF FAIRING EMERGENCY LIGHT INOPERATIVE. FOUND MULTIPLE EMERGENCY LIGHTS INOPERATIVE ON THE SAME CIRCUIT. REMOVED AND REPLACED #1 EMERGENCY LIGHT BATTERY. OPS CHECK SAT

Part: NONE — NONE · corrosion level 2 · airframe 44,768 hrs · 28,129 cycles

COPILOT SIDE SEAT TRACKS (INBD/OUTBD) FLOOR BEAMS SHOW SIGNS OF CORROSION. REMOVED CORROSION AND EVALUATED AREA FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR DOUBLER IND/OUT ISDE AT COPILOT SIDE SEAT TRACKS FLOOR BEAMS. INSTALL REPAIR DOUBLER. CORROSION LEVEL 2

Part: NONE — NONE · corrosion level 2 · airframe 44,768 hrs · 28,129 cycles

COCKPIT ENTRY FLOOR BEAM HAS SIGNS OF CORROSION, TOOLING MARKS AND INCORRECT NUT PLATE INSTALLED. REMOVED AND REPLACED DAMAGE PROFILE REINFORCEMENT AT COCKPIT ENTRY FLOOR BEAM. CORROSION LEVEL 2

Part: NONE — NONE · corrosion level 2 · airframe 44,768 hrs · 28,129 cycles

PILOT SIDE INBD AND OUTBD SEAT TRACK FLOOR BEAMS SHOW SIGNS OF CORROSION (FS9-FS10 4WD LBL12 AND LBL24). BLENDED AREA FOUND TO BE OUT OF LIMITS IN RIGHT SIDE INBD AND OUTBD SIDE TRACK PLACE BEAM. FABRICATED 2 REPAIR DOUBLER IN INBD AND OTBD SIDE. APPLIED ALODINE AND PRIMER, TOP COATED. CORROSION LEVEL 2

Part: NONE — NONE · corrosion level 2 · airframe 44,768 hrs · 28,129 cycles

AFT FUSELAGE, UNDER TOILET AREA, RH GUSSET BEAMS, FROM FR 61 TO 59, BOTH HAT BEAMS HAS SIGNS OF CORROSION AT BOLT HOLES 4 EACH. BLENDED OUT CORROSION AND EVALUATED AT RH GUSSET FROM FR 59 - FR 60 FOUND TO BE OUT OF LIMITS. REMOVE DAMAGE GUSSET, LOCATE AND DRILL NEW GUSSET AND INSTALL NEW GUSSET. APPLIED ALODINE, PRIMER AND TOPCOAT. CORROSION LEVEL 2

Part: NONE — NONE · airframe 44,768 hrs · 28,129 cycles

M/D CABIN RH SIDE, AT FRAME 53 - 34 FR SIGNS OF CORROSION ALONG FLOOR SILL. REMOVED AND REPLACED FLOOR SILL ON MID CABIN RH SIDE FR 56-41 AND FR 48-52. PERFORMED UTT BY NDT OF BLENDED AREA ON FR 41-48 MID RH CABIN FOUND TO BE WITHIN LIMITS

Part: NONE — NONE · corrosion level 2 · airframe 44,768 hrs · 28,129 cycles

HAT BEAM RH AFT OF FR 59 FOUND TO HAVE CORRODED AREA AT NUT PLATE AREA. CUTOUT DAMAGE AREA. FABRICATED REPAIR DOUBLER. APPLIED ALODINE, PRIMER, TOP COAT AND INSTALLED REPAIR DOUBLER. CORROSION LEVEL 2

Part: NONE — NONE · airframe 44,768 hrs · 28,129 cycles

LH FUSELAGE AT FR60 SILL AREA, SMALL PLATE FOR WATER SUPPLY HAS A CRACK AT NUT PLATE. INSTALLED EWIS PROTECTION ON LH FUSELAGE AT FR60 TO FR 59. REMOVED CABLE AND DUCT FAIRING FOR ACCESS. REMOVED DAMAGED SMALL PLATE, LOCATED AND DRILLED NEW PLATE. RE-INSTALLED CABLE AND DUCT FAIRING. REMOVED EWIS PROTECTION.

Part: NONE — NONE · corrosion level 2 · airframe 44,768 hrs · 28,129 cycles

RH FR19, Y=479 SUSPECT CORROSION ON HAT-BEAM. REMOVED AND REPLACED HAT BEAM AT Y=479 RH FR19 CORROSION LEVEL 2

Part: RIB — CORRODED (LT AILERON) · airframe 44,768 hrs · 28,129 cycles

LH AILERON INBD RIB SHOWS SIGNS OF CORROSION. FABRICATED AND REPLACED LH AILERON INBD RIB.

Part: PANEL — CORRODED (VERTICAL STAB) · airframe 44,768 hrs · 28,129 cycles

VERTICAL STAB INSIDE PANEL 325CL THE UPPER RUDDER ACTUATOR CONNECTING HARDWARE IS CORRODED. REMOVED & REPLACED UPPER RUDDER ACTUATOR BOLT & HARDWARE

Part: TARGET — OUT OF ADJUST (NLG) · airframe 44,748 hrs · 28,113 cycles

LG AIR/GROUND FAIL CAUTION MESSAGE RIGHT AFTER ROTATION FOLLOWED BY ENG 1-2 REV DISAGREE. ADJUSTED NLG DOWNLOCK PROX SWITCH TARGET. OPS CHECK SAT. PERFORMED OPERATIONAL CHECK OF #1 AND #2 T/R. OPS CHECK SAT. NO FAULTS FOUND AT THIS TIME. OPS CHECK SAT ON GEAR PINS

Part: NONE — NONE · airframe 44,545 hrs · 27,930 cycles

FUEL LEAK COMING FROM PANEL 651CB. REMOVED PANEL 651 CB. FOUND FUEL IN THE DRY BAY OUTSIDE OF RIB 20. AILERON PCA`S HAD FUEL ON THEM, THE HYDRAULIC LINE CLOTH COVERS WERE SOAKED IN FUEL WITH FUEL ON THE PANEL AND IN THE DRY BAY AREA. UNABLE TO CLASSIFY THE LEAK DUE TO THE FUEL COMING FROM THE  SURGE VENT TANK WHICH PER THE AMM VOL 1 28-11-00 PAGE 8 PARA 3 ONLY HAS FUEL IN IT DURING WING DOWN AND UNCOORDINATED MANEUVERS. LOOKING AT PRESSURE TESTING TO LOCATE THE SOURCE OF THE FUEL. REMOVED PANELS 651BB, 651AB TO FOM PERFORMED WING INTEGRAL FUEL TANK SEALING REPAIRS INSIDE PANEL 651AB BY FFC SERVICES. ALL PANELS INSTALLED NO OTHER DEFECT NOTED.

Part: SEAT FRAME — CRACKED (SEAT 22A) · airframe 44,332 hrs · 27,745 cycles

CRACKED AISLE SIDE FRAMES ON SEATS 4A, 10A, 19A, AND 22A. R&R SEATS 4A, 10A, 19A, AND 22A.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 43,996 hrs · 27,442 cycles

DURING OPERATIONS CHECKS OF EMERGENCY LIGHT FOUND SERVICE DOOR. EXIT IDENTIFIER, EXIT MARKER, EXIT LOCATOR ALL LOCATED IN GALLEY AREA INOPERATIVE. REMOVED AND INSTALLED NEW NR 2 BATTERY PACK AND CHARGER. EMERGENCY LIGHT OPERATION TEST GOOD.

Part: SEAT TRACK — CORRODED (LT CABIN) · corrosion level 2 · airframe 43,996 hrs · 27,442 cycles

LEFT AISLE UNDER SEAT TRACK NR 29 FLOOR BEAM HAS CORROSION. REMOVED AND REPLACED LEFT AISLE UNDER SEAT TRACK NR 29 FLOOR BEAM.

Part: STRINGER — DAMAGED (FRAME 17) · airframe 43,996 hrs · 27,442 cycles

STRINGER HAS GROOVE CUT IN THE BOTTOM SIDE, AT FR 17X+10.562 AND STGR 15R. REMOVED DAMAGED SECTION OF STRINGER 15R BETWEEN FRAMES 15 AND 16 ENDING AT FRAME 20 AND SPLICED IN NEW SECTION OF STRINGER.

Part: BUTTSTRAP — CORRODED (CABIN FLOOR) · corrosion level 2 · airframe 43,996 hrs · 27,442 cycles

LT FLOOR STRUCTURE UNDER SEAT 1A CORROSION ON BUTT STRAP IN 2 LOCATIONS. REMOVED AND REPLACED BUTT STRAP FLOOR STRUCTURE UNDER SEAT 1A.

Part: SEAT TRACK — CORRODED (LT CABIN) · corrosion level 2 · airframe 43,996 hrs · 27,442 cycles

LEFT AISLE, UNDER SEAT TRACK NR 30 FLOOR BEAM HAS CORROSION. REMOVED AND REPLACED LEFT AISLE UNDER SEAT TRACK NR 30 FLOOR BEAM.

Part: SEAT TRACK — CORRODED (LT CABIN) · corrosion level 2 · airframe 43,996 hrs · 27,442 cycles

LEFT AISLE, UNDER SEAT TRACK NR 31 FLOOR BEAM HAS CORROSION. REMOVED AND REPLACED LEFT AISLE UNDER SEAT TRACK NR 31 FLOOR BEAM.

Part: FRAME — CORRODED (RT NACELLE) · corrosion level 2 · airframe 43,996 hrs · 27,442 cycles

RIGHT ENGINE, FORWARD FRAME AFT FLANGE TO COMPOSITE OUTER BYPASS DUCT HAS MULTIPLE LOCATIONS OF CORROSION AROUND CIRCUMFERENCE APPROXIMATELY 60 PERCENT OF THE CIRCUMFERENCE. UPON FURTHER EVALUATION THE LOCATIONS OF CORROSION FOUND ON RIGHT ENGINE, FORWARD FRAME AFT FLANGE HAS MIGRATED INTO THE MATING SURFACE OF COMPOSITE OUTER BYPASS DUCT LOCATED AT THE FOLLOWING CIRCUMFERENCE LOCATIONS LOOKING FWD. AREA 1 IS LOCATED AT THE 12 O'CLOCK POSITION MEASURING 14" IN LENGTH. AREA 2 IS LOCATED AT THE 3 O'CLOCK POSITION MEASURING 18" IN LENGTH. AREA 3 EXTENDS FROM THE 5 O'CLOCK TO THE 10 O'CLOCK POSITION. PARTIALLY BLENDED AREA 2 CORROSION LOCATED AT THE 3 O'CLOCK POSITION USING HAND METHOD. BLEND MEASURES LENGTH 1" WIDTH 0.5" BLENDED ACTIVE CORROSION AT AFT FLANGE SPLIT LINE FROM 2 O'CLOCK POSITION. THE 2-3 O'CLOCK POSITION DAMAGE WAS NOT IN CONTACT WITH THE AFT SPLIT LINE, J-.013", H-10.1". THE 3-5 O'CLOCK POSITION DAMAGE IS IN CONTACT WITH THE AFT SPLIT LINE, BLEND 3-4 O'CLOCK POSITION J-N/A, H-6.1". BLEND 4-5 O'CLOCK POSITION J-0.019, H-7.7" DEPTH.

Part: FLAP SYSTEM — UNKNOWN · airframe 43,375 hrs · 26,915 cycles

FLAP FAIL ON APPROACH AT 0 DEGREE---PERFORMED GVI OF FLAP SYSTEM AND RAN OPS CHECKS OF FLAPS,OPS CHECK GOOD ACFT OK FOR SERVICE

Part: CONTROL UNIT — INOPERATIVE (ZONE 300) · airframe 42,933 hrs · 26,542 cycles

PITCH TRIM MAIN INOP FOLLOWED BY PITCH TRIM BACKUP INOP. RETURNED FROM FLIGHT AND DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. R&R HSCU AND MAIN PITCH TRIM CUTOUT SWITCH. OPS CHECK GOOD.

Part: FRAME — CORRODED (CARGO DOOR) · airframe 42,909 hrs · 26,520 cycles

LOWER FRAME ON CARGO DOOR HAS CORROSION AROUND NUTPLATE HOLES. R&R LOWER FR ON CARGO DOOR.

Part: GUSSET — CORRODED (FRAME 59) · airframe 42,909 hrs · 26,520 cycles

LH OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION AT FRAME 59. REMOVED & REPLACED LH OMEGA BEAM GUSSET, NUT PLATES STILL NEED TO BE INSTALLED. INSTALLED NUT PLATES.

Part: FRAME — CRACKED (FRM 10) · airframe 42,909 hrs · 26,520 cycles

COCKPIT FRAME 10 RH SIDE IS CRACKED AT UPPER END- R & R FR 10 RH.

Part: FRAME — CRACKED (FRM 10) · airframe 42,909 hrs · 26,520 cycles

COCKPIT FRAME 10 LH SIDE IS CRACKED AT UPPER END. R & R FRAME 10 LH.

Part: WEB — CRACKED (LT MLG WW) · airframe 42,909 hrs · 26,520 cycles

LT WW REAR WEB IS CRACKED AT LOWER O/B CORNER. R&R LT WW REAR WEB.

Part: FLOOR SUPPORT — CORRODED (FRAMES 54-55) · airframe 42,909 hrs · 26,520 cycles

LH FLOOR SILL HAS LIGHT CORROSION ON UPPER SURFACE BETWEEN FRAME 54 & 55 LH. REMOVED AND STARTED INSTALLING LH FLOOR SILL AT FR 54-55. FINISHED INSTALLING LH FLOOR SILL AT FR 54-55.

Part: FLOOR SUPPORT — CORRODED (FRAMES 18-23) · airframe 42,909 hrs · 26,520 cycles

LH FLOOR SILL SHOW SIGNS OF CORROSION AT FR18 THRU 23. R&R FLOOR SILL AT FR 18-23.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 42,909 hrs · 26,520 cycles

RT SHEAR CLIP AT FR 80 BETWEEN STR 5&6 IS CRACKED. REMOVED CRACKED SHEAR CLIP AT FRAME 80 BETWEEN STRINGERS 5&6 AND INSTALLED NEW SHEAR CLIP.

Part: FLOOR SUPPORT — CORRODED (FRAMES 24-29) · airframe 42,909 hrs · 26,520 cycles

L/H FLOOR SILL SHOWS SIGNS OF CORROSION AT FR 24-29. REMOVED AND REPLACED LH FLOOR SILL.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 42,909 hrs · 26,520 cycles

LT SHEAR CLIP AT FR 80 BETWEEN STR 5&6 IS CRACKED. REMOVED LT SHEAR CLIP AT FRAME 80 RT BETWEEN STRINGERS 5 & 6 AND INSTALLED HI-LOKS INTO NEW PART, AIRCRAFT RIVETS NEED TO BE INSTALLED. FINISHED SHEAR CLIP INSTALLATION BY INSTALLING ALL RIVETS AND ANY OTHER REQUIRED FASTENERS.

Part: GUSSET — CORRODED (FRAME 59) · airframe 42,909 hrs · 26,520 cycles

AFT LAV CENTER OMEGA BEAM UPPER DIGITAL SUPPORT HAVE CORROSION AROUND NUTPLATE HOLE AT FRAME 59. REMOVED & REPLACED AFT LAV CENTER OMEGA BEAM GUSSET, NUTPLATES STILL REQUIRED TO BE INSTALLED. INSTALLED NUTPLATES.

Part: FLOOR SUPPORT — CORRODED (FRAME 61) · airframe 42,909 hrs · 26,520 cycles

AFT LAV RH FLOOR SUPPORT HAS CORROSION AROUND SCREW HOLE AT FRAME 61. REMOVED & REPLACED THE FLOOR SUPPORT,

Part: FLOOR SUPPORT — CORRODED (FRAMES 51-54) · airframe 42,909 hrs · 26,520 cycles

RH FLOOR SILL HAS LIGHT CORROSION FROM FRAME 54 THRU 51 ON UPPER SURFACE. REMOVED FLOOR SILL R/H SIDE FR 51. PICKED UP HOLES AND INSTALLED NEW RH FLOOR SILL AT FR 51 THRU 54.

Part: FLOOR SUPPORT — CORRODED (FRAMES 49-51) · airframe 42,909 hrs · 26,520 cycles

MAIN CABIN RH FLOOR SILL HAS CORROSION ON UPPER SURFACE FROM FRAME 49 THRU 51- REMOVED AND REPLACED MAIN CABIN RH FLOOR SILL BETWEEN FRAMES 49-51.

Part: PLATE — CORRODED (FRAME 16-18) · airframe 42,909 hrs · 26,520 cycles

LH DIGITAL PLATE AT PAX DOOR HAS SIGNS OF CORROSION AT FR 16 TO FR 18. REPAIRED LH DIGITAL PLATE AT PAX DOOR.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,909 hrs · 26,520 cycles

FWD 61 FWD SIDE SHOWS SIGNS OF CORROSION BETWEEN STR 18R AND STR20R. R&R FR 61 SHEAR CLIP BETWEEN STR 18R THRU 20R.

Part: SUPPORT BRACKET — CRACKED (FRAME 46) · airframe 42,909 hrs · 26,520 cycles

MAIN CABIN FRAME 46 RH LOWER SUPPORT BRACKET IS CRACKED BELOW FLOOR SILL- R/R THE CRACKED LOWER FRAME SUPPORT AT FR 46 R/H JUST BELOW THE FLOOR SILL.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 42,909 hrs · 26,520 cycles

SERVICE DOOR THRESHOLD IS CORRODED IN SEVERAL SPOTS. REMOVED AND STARTED INSTALLATION OF NEW SERVICE DOOR THRESHOLD. COMPLETED INSTALLATION OF SERVICE DOOR THRESHOLD.

Part: FLOOR SUPPORT — CORRODED (GALLEY) · airframe 42,909 hrs · 26,520 cycles

FWD GALLEY ANGLE REINFORCEMENT IS CORRODED RH SIDE. REMOVED AND REPLACED RH FWD GALLEY FLOOR SILL.

Part: TORSION BAR — CRACKED (AFT CARGO) · airframe 42,909 hrs · 26,520 cycles

AFT CARGO COMP, TORSION BAR AFT LOWER SUPPORT BRACKET WAS CRACKED. REMOVED AFT CARGO COMPT. TORSION BAR AFT LOWER SUPPORT BRACKET AND DRILLED NEW BRACKET. INSTALLED AFT CARGO COMP. TORSION BAR AFT LOWER SUPPORT BRACKET.

Part: SEAT TRACK — CORRODED (FRAME 41-50) · airframe 42,909 hrs · 26,520 cycles

MAIN CABIN SIDEWALL SEAT TRACK HAS LIGHT CORROSION FROM FRAME 41 THRU 50- R/R SEAT TRACKS WITH LIGHT CORROSION IN MAIN CABIN SIDEWALL FROM FRAME 41 THRU 50.

Part: FLOOR SUPPORT — CRACKED (FRAME 47) · airframe 42,909 hrs · 26,520 cycles

MAIN CABIN RH OMEGA BEAM I/B LOWER SUPPORT IS CRACKED AT FRAME 47- REMOVED FASTENERS ON THE RH OMEGA BEAM I/B LOWER SUPPORT ANGLE AT FR47. INSTALLED RH OMEGA BEAM I/B LOWER SUPPORT ANGLE AT FR47.

Part: FLOOR SUPPORT — CORRODED (FRAMES 22-55) · airframe 42,909 hrs · 26,520 cycles

RH FLOOR BEAM BETWEEN FR 22 & FR 55 SHOW SIGNS OF CORROSION- BLENDED AT DAMAGE ON RH FLOOR BEAM. INSPECTED DAMAGE AREA AFTER BLEND, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER AND REPAIRED AFECTED AREA ON FLOOR BEAM.INSTALLED DOUBLER AND PREPED AND PAINTED REPAIRED AREA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,909 hrs · 26,520 cycles

MAIN CABIN RT FLOOR SILL HAVE CORROSION ON UPPER SURFACE AT FR 47 RT. R&R MAIN CABIN RT FLOOR SILL AT FR 47 RT.

Part: FLOOR SUPPORT — CORRODED (FRAME 47) · airframe 42,909 hrs · 26,520 cycles

MAIN CABIN RH OMEGA BEAM O/B LOWER SUPPORT IS CRACKED AT FR47- REMOVED THE FASTENERS FROM THE R/H OMEGA BEAM O/B LOWER SUPPORT ANGLE. REMOVED THE RIVETS FROM THE RT OMEGA BEAM O/B LOWER SUPPORT ANGLE. INSTALLED RH O/B OMEGA BEAM LOWER SUPPORT LOWER SUPPORT ANGLE.

Part: SUPPORT BRACKET — CRACKED (FRAME 66) · airframe 42,909 hrs · 26,520 cycles

AFT CARGO COMPT LOWER THRESHOLD 'T' PROFILE SUPPORT BRACKET IS CRACKED AT FRAME 66. REMOVED AND REPLACED "T" PROFILE SUPPORT BRACKET AT FRAME 66 IN AFT CARGO.

Part: SHEAR TIE — CRACKED (FRAME 67) · airframe 42,909 hrs · 26,520 cycles

AFT CARGO COMP FRAME 67 SHEAR CLIP IS CRACKED BETWEEN STR 6 & 7 LH. REMOVED AND STARTED INSTALLATION OF FR67 SHEAR CLIP. FINISHED INSTALLING SHEAR CLIP.

Part: SHEAR TIE — CRACKED (FRAME 72) · airframe 42,909 hrs · 26,520 cycles

AFT CARGO COMPT FRAME 72 SHEAR CLIP IS CRACKED BETWEEN STR 17 & 18 LH. REMOVED & REPLACED THE SHEAR CLIP.

Part: SEAT TRACK — CORRODED (FRAMES 42-51) · airframe 42,909 hrs · 26,520 cycles

LEFT OMEGA BEAM SEAT TRACKS HAVE LIGHT CORROSION FROM FRAME 42 THRU 51- R/R SEAT TRACK WITH LIGHT CORROSION ON LH OMEGA BEAM FROM 42 - 49 FRAMES. R/R LOWER SEAT TRACK AT LH AND RH STA 50 AND RH LOWER AT STA 51, SEAT TRACK ON STA 51 LH SIDE STILL NEEDS TO BE REPLACED. INSTALLED LH LOWER SEAT TRACK AT STA 51.

Part: GUSSET — CORRODED (FRAME 61) · airframe 42,909 hrs · 26,520 cycles

AFT LAV RH OMEGA BEAM UPPER DIGITAL SUPPORT HAS CORROSION ON UPPER SURFACE AT FRAME 61. REMOVED & REPLACED AFT LAV OMEGA BEAM GUSSET, NUTPLATES STILL REQUIRES TO BE INSTALLED. INSTALLED NUT PLATES.

Part: SHEAR TIE — CRACKED (FRAME 61) · airframe 42,909 hrs · 26,520 cycles

MAIN CABIN FRAME 61 LH SIDE SHEAR CLIP IS CRACKED BETWEEN STR 6 & 7 LH. REMOVED CABIN FRAME 61 LH SIDE SHEAR CLIP DUE TO CRACKING AND INSTALLED NEW SHEER CLIP.

Part: SHEAR TIE — CRACKED (FRAME 24) · airframe 42,909 hrs · 26,520 cycles

MAIN CABIN FRAME 24 LH SHEAR CLIP IS CRACKED AT STR 15 LH. REMOVED & INSTALLED NEW SHEAR CLIP AT FR L/H 24.

Part: FRAME — CRACKED (FRM 66) · airframe 42,909 hrs · 26,520 cycles

AFT CARGO COMPT FRAME 66 IS CRACKED AT STR 15 RH SIDE UNDER FLOOR SILL. CUT OUT DAMAGED FRAME 66 IN AFT CARGO COMPT AT STR 15 RH SIDE AND STARTED MAKING "L" ANGLE SPLICE PIECES. FABRICATED "L" ANGLES FOR THE REPAIR AND STARTED INSTALLING REPAIR ON AFT CARGO COMPT FR 66 AT STR 15 RH SIDE. FINISHED INSTALLING REPAIR FR 66.

Part: SHEAR TIE — CRACKED (FRAME 73) · airframe 42,909 hrs · 26,520 cycles

AFT CARGO COMPT FRAME 73 SHEAR CLIP IS CRACKED BETWEEN STR 8 & 9 LH SIDE. REMOVED & REPLACED THE SHEAR CLIP.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 42,909 hrs · 26,520 cycles

AFT CARGO COMPT FR 68 SHEAR CLIP IS CRACKED BETWEEN STR 6&7L. R&R AFT CARGGO SHEAR CLIP AT FR 68 AT STR 6&7L.

Part: SUPPORT BRACKET — CRACKED (FRAME 57) · airframe 42,909 hrs · 26,520 cycles

AFT FUSELAGE EXTERIOR @FRAME 57 LH SIDE BLEED AIR DUCT SUPPORT BRACKET IS CRACKED AFT OF VENTRAL TANK. R & R BLEED AIR DUCT BRACKET ON L/H SIDE OF FUSELAGE AT FR57 AFT OF THE VENTRAL TANK.

Part: SEAT TRACK — CORRODED (FRAMES 41-51) · airframe 42,909 hrs · 26,520 cycles

MAIN CABIN LH SIDE WALL SEAT TRACKS HAVE LIGHT CORROSION FROM FRAME 41 THRU 51- R/R SEAT TRACKS WITH LIGHT CORROSION IN MAIN CABIN LH SIDE WALL FROM FRAME 41 THRU 51.

Part: SHEAR TIE — CRACKED (FRAME 16) · airframe 42,909 hrs · 26,520 cycles

MAIN CABIN FRAME 16 RH SHEAR CLIP IS CRACKED AT STR 15 RH- REMOVED & REPLACED FR16 SHEAR CLIP AT STR 15R.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,909 hrs · 56,520 cycles

RT OVER WING BELLY FAIRING NUTPLATE ATTACH ANGLE ON SIDE OF FUSELAGE AT FR 49 IS CRACKED. R&R RT LATERAL FAIRING ATTACH ANGLE FROM FUSELAGE AT FR 49.

Part: DOOR FRAME — CORRODED (AFT CARGO) · airframe 42,909 hrs · 26,520 cycles

AFT CARGO DOOR LOWER FRAME HAS CORROSION AROUND NUTPLATE HOLES. R & R AFT CARGO DOOR LOWER FR.

Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 42,909 hrs · 26,520 cycles

RT WW AFT O/B CORNER BELLY FAIRING NUTPLATE 'L' SUPPORT ANGLE IS CRACKED. R/R THE RH W/W AFT O/B CORNER BELLY FAIRING "L" ANGLE.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,909 hrs · 56,520 cycles

RT OVER WING BELLY FAIRING NUTPLATE ATTACH ANGLE ON SIDE OF FUSELAGE AT FR 49 IS CRACKED. R&R RT LATERAL FAIRING ATTACH ANGLE FROM FUSELAGE AT FR 49.

Part: HINGE — CRACKED (FLAP SHROUD) · airframe 42,909 hrs · 56,520 cycles

LT O/B FLAP SHROUD FWD I/B HINGE HALF IS CRACKED AT I/B END. R&R THE LT O/B FLAP SHROUD I/B HINGE.

Part: FITTING — CRACKED (PYLON YOKE) · airframe 42,909 hrs · 26,520 cycles

RH FWD PYLON YOKE UPPER LINKAGE FITTING IS CRACKED. R&R RH FWD PYLON LOWER UPPER LINKAGE FITTING.

Part: WEB — CRACKED (RT MLG WW) · airframe 42,909 hrs · 26,520 cycles

RT W/W REAR WEB IS CRACKED AT LOWER O/B CORNER. R&R RH W/W REAR WEB.

Part: TRAY — CRACKED (HF COMMS) · airframe 42,909 hrs · 26,520 cycles

AFT AVIONICS COMP RH RADIO ALTMETER SUPPORT TRAY LOWER BRACKED IS CRACKED- R&R AFT AVIONICS COMP RH RADIO ALTIMETER SUPPORT TRAY LOWER BRACKET.

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 42,909 hrs · 56,520 cycles

LT WW AFT O/B CORNER BELLY FAIRING NUTPLATE L SUPPORT ANGLE IS CRACKED. R&R LT WW AFT O/B CORNER BELLY FAIRING NUTPLATE L SUPPORT ANGLE.

Part: SHEAR TIE — CORRODED (FRAME 68) · airframe 42,909 hrs · 26,520 cycles

AFT CARGO DOOR FRAME HAS CORROSION ON SHEAR CLIP AT FR68 NEAR STR 15L- REMOVED ERROSION ON SHEAR CLIP ON FR68 NEAR STR 15L, REMOVED .002", WITHIN LIMITS.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,834 hrs · 26,450 cycles

FWD RAD ALT ANTENNA SUPPORT IS CORRODED, REMOVED AND REPLACED FWD RAD ALT ANT SUPPORT

Part: LOCALIZER — MALFUNCTIONED (COCKPIT) · airframe 41,406 hrs · 25,317 cycles

LOCALIZER NR 1 AND NR 2 UNRELIABLE AT LAN. LOC NEEDLE WOULD DEFLECT FULL LEFT TO RIGHT INTERMITTENTLY WITHIN 10 MILES TO FIELD. PERFORMED TRPUBLESHOOTING. INSPECTED AND CHECKED ELECTRICAL BONDING OF VOR/LOC ANTENNA, AND COAX CONNECTIONS FROM INU TO VOR/LOC ANTENNA. NO DEFECTS FOUND. PREFORMED VOR/ILS, DME, AND DME OPS CHECK. OPS CHECK NORMAL.

Part: ANGLE — CORRODED (NOT REPORTED) · airframe 41,171 hrs · 25,120 cycles

AFT CARGO LOWER THRESHOLD Z ANGLE HAS CORROSION AROUND FASTNER HOLES....REMOVED & REPLACED AFT CARGO DOOR LOWER THRESHOLD Z ANGLE.

Part: SHEAR TIE — CRACKED (FRAME 71) · airframe 41,171 hrs · 25,120 cycles

AFT CARGO FRAME 71 SHEER CLIP IS CRACKED BETWEEN STR 8-10 R/H SIDE....REMOVED & REPLACED AFT CARGO FR 71 SHEER CLIP BETWEEN STR 8-10 R/H SIDE.

Part: SHEAR TIE — CRACKED (FRAME 77) · airframe 41,171 hrs · 25,120 cycles

AFT FUSELAGE INSIDE ACCESS 312AR FRAME 77 SHEAR CLIP IS CRACKED AT STR 3 R/H ABOVE ICU....REMOVED AND REPLACED SHEAR CLIP AT AFT FUSELAGE FRAME 77.

Part: CONTROL UNIT — FAULTED (HORIZONTAL STAB) · airframe 40,605 hrs · 24,659 cycles

MAIN PITCH TRIM INOPERATIVE. REMOVED AND REPLACED HSCU. OPS CHECKED GOOD.

Part: PITCH CONTROL — MALFUNCTIONED (MAIN)

MAIN PITCH TRIM FAILED, R2 PRIMARY PITCH TRIM CUTOUT SWITCH PUSHBUTTON POPS, CHECKED GOOD.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 40,554 hrs · 24,619 cycles

CABIN DEPRESSURIZATION DURING CRUISE LESS THAN 1000 FPM. MASK DID NOT DROP. NORMAL LANDING, DECLARED EMERGENCY. PERFORMED AN OPS CHECK OF MANUAL PRESSURIZATION SYSTEM, OPS CHECKED GOOD.

Part: CONNECTOR — LOOSE (HCSU) · airframe 40,510 hrs · 24,582 cycles

PITCH TRIM MAIN INOP. INSPECTED HSCU, FOUND CONNECTOR J2 LOOSE. SECURED CONNECTOR, RESET SYSTEM, OPS CHECK GOOD AT THIS TIME.

Part: CLAMP — UNSECURE (BLEED AIR SYS) · airframe 40,501 hrs · 24,574 cycles

BLEED 2 LEAK ON CLIMB OUT.. RESECURED V CLAMPS ON RT ENGINE BLEED VALVE OPS CHECK GOOD NO LEAKS OR FAULTS FOUND.

Part: TRANSDUCER — FAULTY (MLG WHEEL)

BANGING NOISE FROM RIGHT SIDE OF AIRCRAFT WITH SPOILERS OPENING AND CLOSING UNCOMMANDED. R&R NR 4 WHEEL SPEED TRANSDUCER. PERFORMED OPS CHECK OF SYSTEM. CHECKS GOOD AT THIS TIME.

Part: WARNING LIGHT — FALSE ACTIVATION (BLEED OVERTEMP) · airframe 39,494 hrs · 23,734 cycles

NR 1 AND 2 BLEED OVERTEMP ILLUMINATED IN FLT. PERFORMED A BLEED TEST WITH CREW. NO DEFECTS NOTED.

Part: INDICATION SYS — MALFUNCTIONED (ANTI ICE SYSTEM) · airframe 39,494 hrs · 23,734 cycles

AFTER TAKEOFF, ENCOUNTERED ICING AND ECS BLEED TEMP CARROT NR 1 WENT INTO THE RED BAND. RECEIVED A BLEED 1 OVERTEMP MESSAGE. IAW QRH ISOLATED THAT SIDE AND CONTINUED AT FL 240 OUT OF ICING CONDITIONS. ENCOUNTERED ICING AGAIN AND RECEIVED A BLEED 2 OVERTEMP. BEFORE RUNNING QRH, RECEIVED A W/G A/ICE FAIL AND THEN AN ICE CONDA/I INOP MESSAGE. BEFORE CLOSING BLEED 2, LOST CABIN PRESSURIZATION AND THE PRESSURE CLIMBED ABOVE 10,000. DESCENDED QUICKLY TO PREVENT MASKS DROPPING. RAN AIR BLEED SYSTEM TEST AND ANTI ICE TEST. FOUND THE NR 1 BLEED CARROT TO MOVE MULTIPLE TIMES OVER FROM GREEN TO RED BACK TO GREEN. FAIL NEVER RECORDED OR SHOWN ON EICAS. AFTER USING FIM AND CONFERING WITH PREVIOUS HISTORY, INSPECTED THERMOSTATS IN THE CARGO BAY, FOUND THE THERMOSTATS TO BE IN GOOD CONDITION. PULLED PYLON PANELS FOR L & R, NO DEFECTS NOTED. CHANGED THE FAN AIR VALVE DUE TO FIM ON LOG PAGE 358705. PERFORMED AN OPS TEST OF AIR BLEED SYSTEM AND FOUND THE BLEED 1 CARROT STAYED IN GREEN. DURING TESTING SECTION. BLEED 1 & 2 OPS TEST AND LEAK TESTED GOOD FROM CARGO BAY TO PYLON PANELS.

Part: ACM — SEIZED (AC BAY) · airframe 392,025 hrs · 23,333 cycles

SMOKE IN AFT CABIN AND COCKPIT 20 MINUTES AFTER PACK 2 OVERHEAT, STRONG ODOR AND FLIGHT ATTENDANT FIRST SAW SMOKE BY SERVICE DOOR. INSPECTED AND FOUND PACK 1 SEIZED UP. R&R NR 1 ACM OPS CHECK GOOD.

Part: STRUCTURE — CORRODED (RT) · airframe 38,966 hrs · 23,284 cycles

RIGHT OTBD SILL BETWEEN FRAMES 24 AND 29 HAS CORROSION. R & R THE SILL.

Part: GLOWSTRIP — UNSECURE (CABIN) · airframe 36,356 hrs · 21,121 cycles

EMERGENCY PHOTOLUMINECENT STRIP AT EMERGENCY EXIT ROW NOT ATTACHED TO FLOOR. RESECURED EMERGENCY EXIT FLOOR STRIP IAW AMM 33-51-01.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,219 hrs · 20,999 cycles

EMERGENCY LIGHT MAIN CABIN DOOR LIGHT DOES NOT WORK. REMOVED AND REPLACED MAIN CABIN DOOR EMERGENCY LIGHT BULB. OPS CHECK GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 29,670 hrs · 16,730 cycles

PILOT REPORTED A BURNING ELECTRICAL ODOR. MX INSPECTED ACFT AND NO FAULTS WERE FOUND. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED · airframe 29,247 hrs · 16,455 cycles

LEFT FORWARD FLOOR SUPPORT CORRODED BEYOND LIMITS IN VARIOUS AREAS. R & R LT FORWARD FLOOR SILL.

Part: DOOR FRAME — CORRODED (CARGO DOORWAY) · airframe 29,247 hrs · 16,455 cycles

CARGO DOOR FRAME LOWER AREA CORRODED AROUND FASTENER HOLES, CORRODED BEYOND LIMITS. CUTOUT AND REPAIRED WITH FILLER AND INTERNAL DOUBLER IAW EC5230-01306

Part: FITTING — CORRODED (ZONE 300) · airframe 29,247 hrs · 16,457 cycles

DURING C-CHECK, WHEN INSPECTION FOUND CORROSION ON THE LT AND RT SIDE OF THE HORIZONTAL STAB FITTINGS. MX REAM FITTINGS TO THE FIRST OVERSIZE BUSHION IAW SRM 55-30-02. PERFORM THE DIHEDRAL AND INCIDENCE ALLIGNMENTS AND EVERYTHING PASSED AND ACFT WILL BE RELEASED AT THE END OF THE C-CHECK.

Part: MUFFLER — DISCONNECTED (RECIRC FAN) · airframe 23,877 hrs · 12,902 cycles

MSP - FLIGHT 2470, THE CREW REPORTED WHITE CABIN SMOKE AT 2000FT. THE AIRCRAFT RETURNED TO MSP WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE RE-ATTACHED THE MUFFLER TO THE RT RECIRC FAN, OPERATIONALLY TESTED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SWITCH — INOPERATIVE (COCKPIT) · airframe 23,755 hrs · 12,827 cycles

IAH - FLIGHT 2344, THE CREW REPORTED A BLEED 2 FAIL IN FLIGHT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO BLEED PUSH BUTTON SWITCH, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROLLER — OVERHEATED (AUTOPILOT SYS) · airframe 21,667 hrs · 11,619 cycles

IAH - FLIGHT 3026, DURING PREFLIGHT INSPECTION THE CREW REPORTED A BURNING SMELL COMING IN THE COCKPIT. MAINTENANCE INSPECTED THE COCKPIT, REMOVED AND REPLACED THE GUIDANCE CONTROLLER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 19,211 hrs · 10,287 cycles

EXIT SIGN ON 3BC SEAT PARTITION IS INOP. REMOVED AND REPLACED INVERTER IAW EMB 33-15-02. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 19,067 hrs · 10,212 cycles

IAH - FLIGHT 3044, THE CREW REPORTED A LAV SMOKE WARNING HORN IN THE GALLEY WENT OFF DURING DESCENT WITH NO EICAS MESSAGE OR EVIDENCE OF SMOKE, AND LASTED ABOUT 10 MINUTES. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,612 hrs · 9,962 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,612 hrs · 9,962 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 38. REPAIRED CENTER OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SUPPORT — CORRODED (LAV WASTE) · airframe 18,612 hrs · 9,962 cycles

SHV - DURING C-CHECK, LAV WASTE DRAIN VALVE SUPPORT CORRODED. REMOVED AND REPLACED LAV WASTE DRAIN VALVE SUPPORT IAW EMB 145 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,612 hrs · 9,962 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 29. REPAIRED CENTER OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,612 hrs · 9,962 cycles

SHV - DURING C-CHECK, LT OMEGA BEAM HAS CORROSION BETWEEN FR 33-34. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FRAME — CORRODED (FUSELAGE) · airframe 18,612 hrs · 9,962 cycles

SHV - DURING C-CHECK, FR 65 HAS CORROSION BETWEEN STR 16L-17L. REPAIRED FR 65 IAW EC 5320-01501. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,612 hrs · 9,962 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 25. REPAIRED OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,612 hrs · 9,962 cycles

SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION BETWEEN 33-34. REPAIRED CENTER OMEGA BEAM IAW EMB 145 SRM 53-00-10. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 18,612 hrs · 9,962 cycles

SHV - DURING C-CHECK, CRACKS AROUND RIVETS AT FR 77,78 AND 79 ON LT SIDE. REPAIRED CRACKS IAW EC 5330-02013. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 18,612 hrs · 9,962 cycles

SHV - DURING C-CHECK, CRACKS AROUND RIVETS AT FR 78 AND 79 ON RT SIDE. REPAIRED CRACKS IAW EC 5330-2013. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PROXIMITY SENSOR — INOPERATIVE (SPOILER) · airframe 18,097 hrs · 9,679 cycles

DFW - FLIGHT 2658, DURING TAXI THE CREW REPORTED THAT THE SPOILERS WERE DEPLOYING UNCOMMANDED DURING TAXI AND WHEN STATIONARY. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT WITH NO HELP, AND THEN REMOVED AND REPLACED THE SPOILER PROXIMITY SENSORS, OPERATIONALLY TESTED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 17,383 hrs · 9,283 cycles

IAH - FLIGHT 2174 - DURING POST FLIGHT INSPECTION THE CREW REPORTED AN EMERGENCY LIGHT TO BE INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 17,319 hrs · 9,248 cycles

TYS - AIRCRAFT IN FOR A A-CHECK WHEN INSPECTION FOUND SEAT 12 BC UPPER WALL EMERGENCY LIGHT INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT INVERTER AND OPS CHECK GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 16,585 hrs · 8,864 cycles

IAH - FLIGHT 2126 DURING PREFLIGHT INSPECTION THE CREW REPORTED EXIT ROW RT SIDE " EXIT " LIGHT INOP. MX INSPECTED THE ACFT, RESET THE EMERGENCY LIGHT SYSTEM, OPS TESTED THE EMERGENCY LIGHTS WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE

Part: INVERTER — INOPERATIVE (CABIN) · airframe 16,378 hrs · 8,751 cycles

EMERGENCY EXIT LIGHT AT FWD SERVICE DOOR FRAME INOP. R&R INVERTER IAW EMB 145 AMM 33-50-11. OPS CK GOOD. ACFT RELEASED AND RETURNED TO SERVICE.

Part: SEAL — LOOSE (SERVICE DOOR) · airframe 16,067 hrs · 8,581 cycles

CLE FLIGHT 2505 - THE CREW REPORTED A LOUD BANGING NOISE AT THE SERVICE DOOR ON CLIMBOUT FROM CLE. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE SERVICE DOOR SEAL LOOSE AND HANGING OUT AT THE BOTTOM. RESECURED THE SERVICE DOOR SEAL AND OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (CABIN)

FLIGHT 2129 -EWR- FLIGHT CREW REPORTED THAT PASSENGER NOTICED BURNING ODOR FROM AIR VENTS ABOUT HALFWAY THROUGH FLIGHT, THEN ODOR WENT AWAY. EWR MAINTENANCE PERFORMED OPERATIONAL CHECK OF PACK 1 AND 2 SYSTEM AND NO ODOR WAS DETECTED. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)

Part: RADIO — INOPERATIVE (COMM 1)

IAH FLIGHT 2187. THE CREW REPORTED, WERE UNABLE TO TRANSMIT ON COMM 1. THE ACFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 COMM UNIT. OPERATIONAL CHECKS WERE GOOD. (S)

Part: FITTING — WORN (RT AILERON) · airframe 13,763 hrs · 7,351 cycles

SHV - DURING C-CHECK IT WAS FOUND THAT THE RT AILERON PCA ACTUATOR ATTACHMENT FITTING ON THE AILERON SPAR HAD MIGRATED HAT BUSHINGS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW CONTINENTAL EXPRESS EC5750-01177. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 13,644 hrs · 7,287 cycles

ORF - FLIGHT 2113, THE CREW REPORTED A STRONG ODOR POSSIBLY ELEC IN FLIGHT. THE AIRCRAFT LANDED AT ORF WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, VERIFIED NO EICAS MESSAGES OR OTHER DISCREPANCIES. OPERATIONALLY CHECK ELECTRICAL SYSTEMS WITH NO DEFECTS NOTED, AND THE AIRCTRAFT WAS APPROVED TO RETURN TO SERVICE.

Part: FUSE — FAILED (POWER SUPPLY) · airframe 12,980 hrs · 6,948 cycles

EMERGENCY LIGHTS OVERWING INOP. REMOVED AND REPLACED FUSES IN NR 4 POWER SUPPLY IAW EMB 145 VCMM 33-21-70. OPS CHECKED GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: LIGHT — MISSING (GALLEY) · airframe 12,676 hrs · 6,780 cycles

CLE FLIGHT 2219. THE CREW REPORTED THE EMERGENCY LIGHT STRIP WAS MISSING NEAR THE GALLEY. MAINTENANCE INSPECTED AND INSTALLED MISSING LIGHT STRIP NEAR THE GALLEY. OPERATIONAL CHECKS WERE GOOD.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 12,299 hrs · 6,581 cycles

EWR - MX - BAG SMOKE LIGHT REMAINS ON IN EICAS. MX REMOVED AND REPLACED NR 2 BAGG SMOKE DETECTOR IAW EMB145 AMM AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: FIRE WARNING — MALFUNCTIONED (CARGO BAY) · airframe 12,014 hrs · 6,437 cycles

FLT 2557 - EWR - CREW REPORTED BAGG FIRE LIGHT CAME ON IN FLIGHT WITH NO WARNING SOUND. EWR MX RESET ELECTRICAL POWER AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 11,876 hrs · 6,367 cycles

DURING ROUTINE INSPECTION, MX DISCOVERED FWD BAGGAGE SMOKE DETECTOR TO NOT TEST PROPERLY. MAINTENANCE REMOVED AND REPLACED FWD BAGGAGE SMOKE DETECTOR. OPERATIONAL CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 11,830 hrs · 6,343 cycles

IAH - FLIGHT 3089 - THE CREW REPORTED THAT ON ARRIVAL TO IAH HAD A BAGGAGE SMOKE WARNING IN EICAS, AND A BAGGAGE WARNING LIGHT ON. THE CREW DISCHARGED THE CARGO FIRE BOTTLES AS A PRECAUTION, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE FORWARD CARGO COMPARTMENT SMOKE DETECTOR & FIRE BOTTLES, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 11,830 hrs · 6,343 cycles

IAH - FLIGHT 3089 - THE CREW REPORTED THAT ON ARRIVAL TO IAH HAD A BAGGAGE SMOKE WARNING IN EICAS, AND A BAGGAGE WARNING LIGHT ON. THE CREW DISCHARGED THE CARGO FIRE BOTTLES AS A PRECAUTION, AND THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED THE AFT CARGO COMPARTMENT SMOKE DETECTOR & FIRE BOTTLES, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FADEC — MALFUNCTIONED · airframe 11,305 hrs · 6,068 cycles

IAH - FLIGHT 2326, THE CREW REPORTED THAT THE AIRCRAFT WOULD NOT COME OUT OF TAKEOFF MODE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE THE FADEC 2A, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 11,144 hrs · 5,980 cycles

IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE AISLE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE INSPECTED THE AIRCRAFT AND RESECURED THE LIGHT STRIP BY THE GALLEY, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: MANIFOLD — SEPARATED (RT ENGINE) · airframe 8,986 hrs · 4,807 cycles

SHORTLY AFTER T/O THE CREW REPORTED THAT THE NR 2 ENGINE ITT SPIKED. POWER WAS REDUCED AND E2 ANTI-ICE FAIL MESSAGE APPEARED ON EICAS. THE CREW RETURNED WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BRACKET — GOUGED (ZONE 500) · airframe 8,837 hrs · 4,717 cycles

TYS - DURING A SCHEDULE 2C INSPECTION THE LEFT PCA BRACKET WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE BRACKET IAW EMB135/145 SRM 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETION OF ALL WORK.

Part: WINDSHIELD — BURNED (COCKPIT) · airframe 5,004 hrs · 2,662 cycles

IAH - FLIGHT 3229, THE CREW REPORTED THE NUMBER TWO PACK CAUSED A BURNING SMELL DURING DESCENT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE NUMBER TWO PACK TO BE OPERATING NORMALLY, FURTHER INSPECTION REVEALED THE CAPTAINS WINDSHIELD TERMINAL BLOCK WAS BURNT. THE CAPTAINS WINDSHIELD WAS REMOVED AND REPLACED, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: VALVE — FAULTY (NR 1 A/C PACK) · airframe 4,975 hrs · 2,645 cycles

CREW REPORTED, PACK NR 1 PRODUCED STRONG RUBBER/PLASTIC SMELL DURING LAST 10-15 MINUTES OF FLIGHT; SMELL ASSOCIATED WITH AUTO MODE [OF PACK] ONLY, A/C. RELEASED IAW MEL 21-60-04 CATEGORY-C CONTROL NUMBER 050284. MAINTENANCE REMOVED AND REPLACED FORWARD AIR DISTRIBUTION VALVE IAW EMB145 MM 21-22-01, OPS CHECKED GOOD.