N16178

Part: BRACKET — CORRODED (FUEL TANK) · corrosion level 2 · airframe 39,499 hrs · 27,776 cycles

CORROSION FOUND AROUND LOWER BRACKET ON VENTRAL FUEL TANK FACE CENTER. REMOVED AND REPLACED VENTRAL TANK. OPS AND LEAK CHECK SAT.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 38,807 hrs · 27,076 cycles

EMERGENCY LIGHT AT SEAT 18D OVERHEAD INOPERATIVE. REMOVED AND REPLACED LAMP AT 18D OVERHEAD. OPS CHECK SAT.

Part: CONTROL LEVER — INOPERATIVE (LANDING GEAR) · airframe 38,149 hrs · 26,414 cycles

LANDING GEAR WILL NOT RETRACT, WITH LANDING GEAR LEVER DISAGREE MESSAGE ON TAKEOFF. REMOVED AND REPLACED LH CONTROL LEVEL. OPS CHECK SAT. PERFORMED MLG EXTENSION AND RETRACTION OPS CHECK. OPS CHECK SAT. CLEANED LG WOW PROX SWITCHES. OPS CHECK SAT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,485 hrs · 25,800 cycles

MAIN ACCESS DOOR EXTERNAL EMERGENCY LIGHT IS OUT. REMOVED AND REPLACED MCD EXTERNAL EMERGENCY LIGHT ASSEMBLY. OPS CHECK SAT

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,485 hrs · 25,800 cycles

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

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 37,151 hrs · 25,486 cycles

MCD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY LIGHT BULB. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF4, LH FRAME 59 IN LAVATORY AREA BTW STR 15L-16L FOUND CRACKED. EXTENDED SPLICE REPAIR ON LH CENTER FUSE 4 FRAME 59, BTW STR 14L-16L

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF3, CRACKS (2X) FOUND ON LH OMEGA BEAM #4 FLOOR STRUCTURE BTW FR 35-39. AFTER NDT INSPECTION, CRACK FOUND AT FR 36 & 37. BEAM REPAIRED WITH 2 DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 37,030 hrs · 25,367 cycles

SURFACE CORROSION AROUND SCREW HOLES OF MAIN DOOR LOWER BEAM LINING ATTACHMENT. BEAM REPAIRED WITH 2 DOUBLERS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

NLG W/WELL, MISDRILLED DONE ON TOP SHELF ASSEMBLY DURING REPLACEMENT PROCESS. PLATE REPAIRED WITH 2 DOUBLERS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF1 EXT, DENT FOUND ON MAIN DOOR SKIN LOWER OF STR 15L AFT CORNER EDGE. DENT REDRESSED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

NLG W/WELL, CRACK FOUND ON NLG UP-LOCK AFT CROSS BEAM. NLG W/WELL ON NLG UP-LOCK REMOVED AND REPLACED AFT CROSS BEAM.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CRACKS SUSPECTED (13X) ON LH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. AFTER NDT INSPECTION, 11 CRACKS FOUND. SKIN REPAIRED WITH 11 BUSHINGS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF1, CRACKS (4X) FOUND ON LH OMEGA BEAM #1 FLOOR STRUCTURE BTW FR 18-24. AFTER NDT INSPECTION, 3 CRACKS AND 2 CORROSION SPOT FOUND. BEAM REPAIRED WITH 5 DOUBLERS

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

VERT STAB LH SKIN DENT BETWEEN SPAR 2 AND AUX SPAR 41% AND BETWEEN RIB ZV 915 AND RIB ZV 1169. SKIN REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

RF1, LH FR68 BOTTOM FRAME 68 SECTION FOUND CRACKED LOWER HOLDER BRACKET. Z FRAME REPAIRED WITH A SPLICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

RF1 EXT, CRACK FOUND BY NDT INSPECTION ON RH TOP SKIN AT FR 75 BTW STR 1R-3R. SKIN REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CRACKS SUSPECTED (8X) ON RH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3R-9R. SKIN REPAIRED WITH 16 BUSHINGS AND 1 REPAIR DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

RF1, CARGO DOOR SURROUND STRUCTURE AFT L-SHAPE AT FR 68 FOUND CORRODED. SHEAR CLIP REPAIRED WITH A SPLICE. CORROSION LEVEL 1.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

RF1, CARGO DOOR SURROUND STRUCTURE FWD L-SHAPE AT FR 65 FOUND CORRODED. SHEAR CLIP REPAIRED WITH A SPLICE. CORROSION LEVEL 1

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF2, CRACKS (6X) FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BTW FR 23-30. REPLACED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 37,030 hrs · 25,367 cycles

AT CF4 EXT, CORROSION FOUND ON TOILET WASTE CUP BTW FR 60-61 AND BTW STR 18R-20R. WASTE DRAIN VALVE REMOVED. TOILET DRAIN CABLE REMOVED. RINSE NIPPLE REMOVED. TOILET WASTE CUP BTW FR60-61 STR 18R-20R BLENDED AND FOUND OUT OF LIMITS. AT CF4, TOILET WASTE CUP BTW FR 60-61 AND STR 18R-20R REMOVED. IN CF4, TOILET WASTE CIP ASSEMBLY BTW FR 60-61 STR 18R-20R REPLACED WITH NEW ONE. WASTE DRAIN VALVE INSTALLED. TOILET DRAIN CABLE INSTALLED. RINSE NIPPLE INSTALLED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 37,030 hrs · 25,367 cycles

RH MLG, FWD BEARING CAP TRACK CORRODED. REPAIRED RH MLG, FWD BEARING CAP TRACK

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 37,030 hrs · 25,367 cycles

LH MLG, FWD BEARING CAP TRACK CORRODED. REPAIRED LH MLG, FWD BEARING CAP TRACK

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 37,030 hrs · 25,367 cycles

CF4, LH OMEGA BEAM FOUND CORRODED ON FLOOR STRUCTURE AROUND NUTPLATE BTW FR 60-61. BEAM REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF3, RH CLOSING ANGLE BTW FRAME 46-50 FOUND CORRODED. BLENDS ARE TEMPORARILY ACCEPTED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 37,030 hrs · 25,367 cycles

CF3, LH CLOSING ANGLE BTW FRAME 46-50 FOUND CORRODED. BLENDS ARE TEMPORARILY ACCEPTED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

AT F.F. LH SKIN FOUND DAMAGED FWD OF FR 2 AND STR 15L. SKIN REPAIRED WITH A DOUBLER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

AT FF COCKPIT CRACK FOUND AT LH OVERHEAD HANDLE. RIB REPAIRED WITH A DOUBLER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF2, CRACK FOUND ON CENTER OMEGA BEAM #2 LH FLANGE AT FRAME 31 ON FLOOR STRUCTURE AREA. BEAM REPAIRED WITH A DOUBLER

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF2, CRACK FOUND ON CENTER OMEGA BEAM #2 LH FLANGE AT FRAME 33 ON FLOOR STRUCTURE AREA. BEAM REPAIRED WITH A DOUBLER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

AT RF1, FRAME 68, LH SIDE SHEAR CLIP BTW STR 6L-9L FOUND CRACKED. AR RF1, FRAME 68, LH SIDE SHEAR CLIP BTW STR 6L-9L REPLACED.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF2, CRACKS (4X) FOUND ON LH OMEGA BEAM #3 FLOOR STRUCTURE BTW FR 29-36. CF2, LH OMEGA BEAM #3 FLOOR STRUCTURE BTW FR 29-36 REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF2, FRAME 24, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. REPLACED SHEAR CLIP

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF2, FRAME 25, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. REPLACED SHEAR CLIP

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

RF1, FRAME 65, LH SHEAR CLIP U/FLOOR BTW STR 18L-19L CRACKED. AT RF1, FRAME 65, LH SIDE SHEAR CLIP BTW STR 18L-19L REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF2, FRAME 24, RH SHEAR CLIP FOUND CRACKED BTW STR 16R-17R. REPLACED SHEAR CLIP

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

CF2, FRAME 27, RH SHEAR CLIP FOUND CRACKED BTW STR 15R-16R. REPLACED SHEAR CLIP

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 37,030 hrs · 25,367 cycles

RF1 T-ANGLE AT FRAME 65 TO LOWER BEAM OF CARGO DOOR SURROUND STRUCTURE CORRODED. RF1, T-ANGLE AT FRAME 65 TO LOWER BEAM OF CARGO DOOR SURROUND STRUCTURE REPLACED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 37,030 hrs · 25,367 cycles

AT RF1, FRAME 72, LH SHEAR CLIP U/FLOOR BTW STR 17L-18L FOUND CRACKED. RF1, FRAME 72, LH SHEAR CLIP BTW STR 17L-16L REPLACED

Part: LAMP — INOPERATIVE (UNKNOWN) · airframe 36,868 hrs · 25,203 cycles

MCD EMERGENCY LIGHT OUT. REMOVED AND REPLACED MCD EMERGENCY LAMP. OPS CHECK SAT.

Part: NONE — NONE · airframe 36,263 hrs · 24,667 cycles

MCD DIFFICULT TO OPEN. CLEANED AND LUBBED MAIN CABIN DOOR ROLLERS. OPS CHECK SAT.

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 36,135 hrs · 24,548 cycles

MAIN CABIN DOOR WONT OPEN. FOUND HANDLE TO NOT BE IN THE FULL OPEN POSITION, FULLY OPERATED HANDLE TO OPEN, DOOR OPERATES AS INTENDED OPENED AND CLOSED DOOR 10 TIMES WITH NO FAULTS.

Part: LIGHT — DETACHED (SEAT 1A) · airframe 36,046 hrs · 24,466 cycles

EMERGENCY FLOOR LIGHTING STRIP CAME OFF SEAT 1A. RESECURED EMERGENCY FLOOR LIGHTING STRIP

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 35,945 hrs · 24,374 cycles

MCD DIFFICULT TO OPEN FROM INSIDE. ADJUSTED THE DOOR HANDLE.

Part: DOOR — BINDING (MAIN) · airframe 35,944 hrs · 24,374 cycles

MCD DIFFICULT TO OPEN FROM INSIDE.

Part: LIGHT — MISSING (CABIN) · airframe 35,887 hrs · 24,325 cycles

FOUR EMERGENCY LIGHTS MISSING ON FLOOR. INSTALLED THE FLOOR EMERGENCY LIGHTS.

Part: LATCH — STICKING · airframe 35,506 hrs · 23,992 cycles

MCD LATCH STUCK. OPENED AND CLOSED DOOR 15 TIMES AS REQUIRED. NO DEFECTS NOTED AT THIS TIME

Part: FRAME — DAMAGED (FRM 69 S7R) · airframe 34,879 hrs · 23,426 cycles

FRM 69 HAS DAMAGED NUT PLATE AND ELONGATED HOLE AT STGR 7R. REMOVED DAMAGE HOLE FINAL SIZE D=0.252" AT FRAME 69 STR 7R. FOUND TO BE IN LIMITS.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 34,879 hrs · 23,426 cycles

LAV UNDER FLOOR SUPPORT AT FR 59-61 BUT LINE O CORROSION. REMOVED AND REPLACED LAV FLOOR SUPPORT CENTER GUSSET AT FR 59-61

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 34,879 hrs · 23,426 cycles

UNDER BAGGAGE COMP UNDER RADIO ALT 2 CORROSION. REMOVED AND REPLACED UNDER BAGGAGE COMP RADIO ALT #2 ANTENNA SUPPORT.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 34,879 hrs · 23,426 cycles

ALL SEAT TRACKS GOUGED / POSSIBLE CORROSION. BLENDED CORROSION / GOUGES ON ALL SEAT TRACKS LH UPPER, CENTER FLOOR FRAMES 19-59 AND RH UPPER, CENTER FLOOR FROM FRAME 23-59. ALL SEAT TRACKS WITHIN LIMITS. REMOVED AND REPLACED 2 SEAT TRACKS AT FRAME 26-28 LH FLOOR. TREATED ALL SEAT TRACKS LH RH SIDE UPPER AND LOWER FRAME.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 34,879 hrs · 23,426 cycles

LAV UNDER FLOOR SUPPORT AT FR 59-61 STR 17L HAS CORROSION. REMOVED AND REPLACED LAV UNDERFLOOR, FLOOR SUPPORT AT FR 59-61 STR 17L

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 34,879 hrs · 23,426 cycles

UNDER BAGGAGE COMP UNDER RADIO REC #2 CORROSION. PERFORMED PERMANENT REPAIR UNDER BAGGAGE COMPARTMENT UNDER RADIO REC #2 SKIN.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 34,788 hrs · 23,426 cycles

SERV DOOR SILL AND UNDER DOOR SILL AC SKIN CORROSION. REMOVED AND REPLACED DOOR SILL AT SERVICE DOOR

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 34,879 hrs · 23,426 cycles

UNDER LAV FLOOR SUPPORT CORROSION BEAM FR 60 STR 17L. REPAIRED UNDER LAY FLOOR SUPPORT FLOOR BEAM FR 60 STR 17L

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 34,879 hrs · 23,426 cycles

LATERAL FLOOR SUPPORT STR 15R FRAMES 52-57, 45-47, 23-41 CORROSION. LATERAL FLOOR SILL SUPPORT STR 15R FRAMES 52-57, 45-47, 23-41. REMOVED CORROSION AND REMOVED AND REPLACED SILL SUPPORT.

Part: NOT REPORTED — NOT REPORTED · corrosion level 2 · airframe 34,879 hrs · 23,426 cycles

RH HAT BEAM AT Y + 479.0 FOUND TO HAVE SIGNS OF CORROSION AFTER REMOVAL OF GUSSET FROM FRM 59-61. FAB 2 REPAIR DOUBLER AND INSTALLED ON RH BEAM FR 49-61.

Part: NONE — NONE · corrosion level 2 · airframe 34,879 hrs · 23,426 cycles

FWD WET AREA FLOOR SUPPORT AT FR 23+2 STR 15R CORROSION. REMOVED AND REPLACED 2EA ANGLES.

Part: NONE — NONE · airframe 34,788 hrs · 23,426 cycles

CORROSION AT FR61 BETWEEN STRG 14R AND STR 15R ON PARTITION PANEL. REMOVED AND REPLACED PARTITION SECTION AT FRAME 61 STRINGER 15R-14R

Part: NONE — NONE · corrosion level 2 · airframe 34,879 hrs · 23,426 cycles

UNDER PASSENGER DOOR SIL AIRCRAFT SKIN CORROSION. REMOVED AND REPLACED PAX DOOR SILL.

Part: INVERTER — INOPERATIVE · airframe 34,854 hrs · 23,407 cycles

FWD SIDE OF EMERGENCY EXIT SIGN OVER ROW 18 NOT ILLUMINATED. R&R #5 EMERGENCY LIGHT INVERTER. OPS CHECK GOOD AT FWD SIDE EMERGENCY ROW 18

Part: LIGHT — MISINSTALLED (LT OVERWING) · airframe 34,412 hrs · 23,005 cycles

LH OVER WING EXTERNAL EMERGENCY LIGHT INSTALLED UPSIDE DOWN. PAINT MARKS ARE NOT PRESENT. REPOSITIONED LH OVERWING EXTERNAL EMERGENCY LIGHT.

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 33,857 hrs · 22,518 cycles

EXTERNAL LT FWD OVERWING EMERGENCY LIGHT LAMP OUT. REMOVED AND REPLACED LT EXTERNAL FWD OVERWING EMERGENCY LIGHT LAMP. OPERATIONS CHECK SATISFACTORY, NO FURTHER DEFECTS NOTED.

Part: SKIN — CRACKED (LT WING) · airframe 33,523 hrs · 22,227 cycles

RT OUTBOARD LEADING EDGE III IS CRACKED AT BOTH OUTER VORTILLONS. R & R LEADING EDGE III RT. OPS CHECK SAT.

Part: SEAL — STUCK (GALLEY DOOR) · airframe 32,252 hrs · 21,047 cycles

WHISTLING SOUND COMING FROM GALLEY DOOR IN FLIGHT. FOUND PIECE OF SECURITY SEAL STRUCK TO THE GALLEY SERVICE DOOR. REMOVED AND COMPLIED WITH PRESSURIZATION CHECK. OPS AND LEAK CHECK SAT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,814 hrs · 20,651 cycles

SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LIGHT BULB. OPS CHECK SAT.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,810 hrs · 20,649 cycles

IAH - DURING MAINTENANCE INSPECTION A DENT IN THE SKIN WAS DISCOVERED AT FRAME 63 STRINGER 21R-20R ON A RIVET LINE. MAINTENANCE CUT OUT THE DAMAGED SKIN AND PERFORMED A FILLER / DOUBLER REPAIR. OPERATIONAL/ PRESSURIZATION CHECKSWERE PERFORMED WITHOUT DEFECT AND THE AIRCRATF WAS APPROVED FOR RETURN TO SERVICE.

Part: BRAKE ASSY — LEAKING (NR 1 & 4) · airframe 31,124 hrs · 19,466 cycles

HYD SYS 1 LOW QUANTITY WITH HYD SYS 1 FAIL. REMOVED AND REPLACED THE NR 1 & 4 BRAKE ASSEMBLIES. OPS AND LEAK CHECKED GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (FRAMES 15-18) · airframe 30,103 hrs · 19,451 cycles

DURING A C CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT SPLICE, FRAMES 15 - 18. MAINTENANCE INSTALLED A DOUBLER AND FILLER ON FLOOR SUPPORT SPLICE IAW SRM 53-21-10.

Part: FLOORBEAM — CORRODED (FRAME 20) · airframe 30,103 hrs · 19,451 cycles

DURING A C CHECK, CORROSION FOUND ON THE FLOORBEAM, FRAME 20. MAINTENANCE REPLACED THE FLOORBEAM IAW SRM 53-23-10.

Part: DOOR SILL — CORRODED (FRAMES 19-20) · airframe 30,103 hrs · 19,451 cycles

DURING A C CHECK, FOUND CORROSION ON SERVICE DOOR SILL, FORWARD SECTION, BETWEEN FRAMES 19 AND 20, STRINGER 15R-17R. MAINTENANCE REPAIRED SERVICE DOOR SILL IAW SRM 53-21-10

Part: SPLICE — CORRODED (FRAMES 23-24) · airframe 30,103 hrs · 19,451 cycles

DURING A C CHECK, FOUND CORROSION ON TH EBAND SPLICE, FRAMES 23 - 24, STRINGERS 18R-19R. MAINTNENACE INSTALLED A NEW SPLICE IAW SRM 51-40-02.

Part: SUPPORT — CORRODED (WASTE VALE) · airframe 30,103 hrs · 19,451 cycles

DURING A C CHECK, FOUND THE TOILET WASTE VALVE SUPPORT CORRODED FROM 8 OCLOCK TO 2 OCLOCK POSTIONS. MAINTENANCE REPLACED THE SUPPORT.

Part: SHEAR TIE — CORRODED (FRAME 62A) · airframe 30,103 hrs · 19,451 cycles

DURING A C CHECK, FOUND THE SHEAR TIE, FRAME 62A BETWEEN STRINGERS 20R & 19R WAS FOUND CORRODED. MAINTENANCE REPLACED THE SHEAR TIE.

Part: DOOR SILL — CORRODED (CARGO BAY) · airframe 30,103 hrs · 19,451 cycles

DURING A C CHECK, THE CARGO DOOR SILL WAS CORRODED AROUND FASTNERS TO STRUCTURE AT FRAMES 66 - 67. MAINTENANCE REPLACED THE LOWER FRAME DOOR BEAM IAW SRM 51-40-02./

Part: SHEAR TIE — CORRODED (FRAME 62A) · airframe 30,103 hrs · 19,451 cycles

DURING A C CHECK, FOUND THE SHEAR TIE, FRAME 62A, BETWEEN STRINGERS 21R & 20R TO BE CORRODED. MAINTENANCE REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (FRAME 62) · airframe 30,103 hrs · 19,451 cycles

DURING A C CHECK, FOUND THE SHEAR TIE AT FRAME 62, BETWEEN STRINGERS 21R & 20R TO BE CORRODED. MAINTENANCE REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (CARGO DOOR AREA) · airframe 30,103 hrs · 19,451 cycles

DURING A C CHECK, FOUND THE CARGO DOOR LATERAL SHAPE WAS CORRODED AT THE FORWARD LOWER CORNER, NEAR FASTNERS. MAINTENANCE REPLACED CARGO DOOR LATERAL SHAPE SHEAR TIE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,806 hrs · 16,430 cycles

DURING POST FLIGHT THE CREW REPORTED THAT THE EMERGENCY LIGHTS AT THE BASE OF THE RT OVERWING EMERGENCY EXIT DOOR WERE INOPERATIVE. THE ACFT WAS FERRIED, WHERE MAINTENANCE R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 24,777 hrs · 15,654 cycles

DURING ROUTINE MAINTENANCE THE AFT CENTER AISLE EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT INVERTER. OPERATIONAL CHECKS WERE GOOD.

Part: SIGN — DISCONNECTED (EMERGENCY LIGHT) · airframe 22,194 hrs · 13,867 cycles

DURING 1A INSPECTION, THE AFT ENERGENCY EXIT SIGN IN THE CEILING WAS FOUND TO BE INOPERATIVE. MAINTENANCE INSPECTED THE LIGHT, RESECURRED THE ELECTRICAL CONNECTORS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 22,179 hrs · 13,858 cycles

DURING MX INSPECTION THE EXTERNAL SERVICE DOOR EXIT LIGHT WAS FOUND INOPERATIVE. MX REPAIRED BROKEN WIRE IN THE SERVICE DOOR WIRE HARNESS WITH OPS CHECK GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ANGLE — CORRODED (RAMP) · corrosion level 2 · airframe 18,877 hrs · 11,722 cycles

FORWARD CARGO RAMP SUPPORT ANGLE HAS CORROSION BEYOND LIMITS AROUND NUT-PLATE HOLES. REMOVED AND REPLACED SUPPORT ANGLE

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 18,877 hrs · 11,722 cycles

LEFT FLOOR SUPPORT HAS CORROSION BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 18,877 hrs · 11,722 cycles

RIGHT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 18,877 hrs · 11,722 cycles

RIGHT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 18,877 hrs · 11,722 cycles

CENTER OMEGA BEAM GUSSET HAS CORROSION BEYOND LIMITS AT FORWARD SCREW HOLES. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 18,877 hrs · 11,722 cycles

RIGHT OMEGA BEAM GUSSET HAS CORROSION BEYOND LIMITS FORWARD AND AFT OF SCREW HOLES. R & R GUSSET.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 18,877 hrs · 11,722 cycles

RIGHT FLOOR SUPPORT CORRODED BEYOND LIMITS. R & R FLOOR SUPPORT.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 18,877 hrs · 11,722 cycles

LEFT FLOOR SUPPORT HAS CORROSION AT SCREW HOLES. R & R FLOOR SUPPORT.

Part: GUSSET — CORRODED (FLOOR SUPPORT) · corrosion level 2 · airframe 18,877 hrs · 11,722 cycles

LEFT OMEGA BEAM GUSSET HAS CORROSION BEYOND LIMITS AT FORWARD SCREW HOLES. REMOVED AND REPLACED GUSSET.

Part: INVERTER — FAULTY (EMERGENCY LIGHTS) · airframe 18,219 hrs · 11,283 cycles

DURING ROUTINE MX THE FWD CABIN CEILING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX REPLACED THE NR 6 EMERGENCY LIGHT INVERTER. OPS CHECKS WERE GOOD.

Part: CONTROL UNIT — FAULTY (HORIZONTAL STAB) · airframe 14,207 hrs · 8,677 cycles

ON CLIMB CREW REPORTED CAPTAIN PITCH TRIM AND MAIN PITCH TRIM INOP. CREW PERFORMED AIR RETURN WITHOUT INCIDENT. MX R & R HORIZ STABILZER CONTROL UNIT AND THE CAPTAIN'S YOKE PITCH TRIM SWITCH WITH OPS CHECKS SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: CONTROL UNIT — INTERMITTENT (COCKPIT) · airframe 11,682 hrs · 6,871 cycles

ABE FLT 6041 THE CREW REPORTED A MAIN PITCH TRIM INOP MESSAGE ON THE EICAS. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE HORIZONTAL STAB CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD.

Part: LINE — DAMAGED (BLEED AIR SYS) · airframe 10,854 hrs · 6,178 cycles

THE "BLEED 2 OVER TEMP" MESSAGE DISPLAYED ON EICAS. REMOVED AND REPLACED DAMAGE SERVO LINE CONNECTED TO NR 2 FAN AIR VALVE IAW EMB 145 AMM 36-11-11-400-801-A, OPS CHECK GOOD. AIRCRAFT RELEASED TO SERVICE.

Part: LINE — DAMAGED (BLEED AIR SYS) · airframe 10,846 hrs · 6,169 cycles

MCI FLT 232 THE CREW REPORTED A BLEED 2 OVERTEMP MESSAGE IN FLT. THE AIRCRAFT RETURNED TO MCI AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED A DAMAGED SERVO LINE AT THE NR 2 FAN AIR VALVE. OPERATIONAL CHECKS WERE GOOD.

Part: THERMOSTAT — INOPERATIVE (BLEED AIR SYS) · airframe 10,846 hrs · 6,169 cycles

MCI - REPO-FLIGHT 232, THE CREW REPORTED A BLEED TWO OVERTEMP. THE AIRCRAFT DIVERTED TO MCI WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE PLACED THE NUMBER TWO BLEED AIR ON MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. IAH MAINTENANCE SUBSEQUENTLY REMOVED AND REPLACED THE E2 FAN AIR THERMOSTAT, OPERATIONALLY TESTED WITH NO DEFECTS. REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: THERMOSTAT — FAULTY (BLEED AIR SYS) · airframe 10,845 hrs · 6,168 cycles

OAK FLT 230 THE CREW REPORTED A BLEED 2 OVERTEMP MESSAGE. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 FAN AIR THERMOSTAT. OPERATIONAL CHECKS WERE GOOD.

Part: ENGINE — ODOR (NR 2) · airframe 9,866 hrs · 5,302 cycles

DURING ENGINE MX RUNS A OIL ODOR IN THE CABIN WAS NOTED COMING FROM THE NR 2 ENGINE. MX REPLACED THE NR 2 ENGINE AND OPS CHECKS WERE GOOD.

Part: SUMP — LEAKING (ENGINE) · airframe 9,866 hrs · 5,302 cycles

AIR RETURN FOR LAV SMOKE INDICATION. MAINTENANCE COMPLIED WITH A VISUAL CHECK, BOROSCOPE BOTH ENGINES AND TEST FLEW TO CLE AND NO FURTHER ISSUES WERE NOTED. TEST FLIGHT GOOD. RELEASED BACK TO SERVICE. RESULTS OF THE ENGINE TEARDOWN REVEALED LEAKAGE FROM THE COOL FRONT SUMP.

Part: SUMP — LEAKING (NR 1 ENGINE) · airframe 9,865 hrs · 5,300 cycles

FLT 113 LAV SMOKE ON DEPARTURE. ACFT RETURNED TO TYS. NR 1 ENG CHANGE IN PROCESS. THE RESULT OF THE INVESTIGATION AT THE SHOP SHOWED THAT LEAKAGE WAS FOUND FROM THE COOL FRONT SUMP.

Part: HOUSING — DETERIORATED (EMERGENCY LIGHT) · airframe 9,831 hrs · 5,270 cycles

RIC - DURING ROUTINE INSPECTION, RIC MX FOUND LT FORWARD OVERWING EMERGENCY LIGHT INOPERATIVE. MX R&R LT FORWARD OVERWING EMERGENCY LIGHT HOUSING AND PERFORMED OPS CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SKIN — PUNCTURED (FUSELAGE)

EWR/TYS-ACFT WAS STRUCK IN EWR BY A BELTLOADER AND PUNCTURED THE SKIN UNDER THE CARGO BAY. THE ACFT WAS FERRY FLOWN TO TYS. TYS MAINTENANCE INSTALLED A DOUBLER, FILLER, AND SHIMS ON FUSELAGE SKIN BETWEEN FRAMES 64-65 AND STRINGERS 19L-21L IAW EC 5330-01830. THE PRESSURE CHECK WAS GOOD AND THE ACFT WAS RELEASED TO SERVICE. (S)

Part: INLET — CORRODED (NR 2 ENGINE)

TYS - DURING A 2C INSPECTION CORROSION WAS FOUND IN THE NR 2 ENG AIR INLET ATTACH POINT HOLES. MAINTENANCE REWORKED THE ATTACH POINT HOLES IAW EC 5420-01136 AND WILL BE RELEASED AT THE END OF THE C-CHECK. (S)

Part: FUEL CELL — LEAKING (LT WING) · airframe 4,380 hrs · 2,378 cycles

TYS FLIGHT 2205 MADE A UNSCHEDULED LANDING DUE TO SOME FUEL LEAKING FRON THE LEFT WING. MAINTENANCE REMOVED SEALANT FROM THE EFFECTED AREA AND RESEALED IAW EMB 145XR 51-20-01. LEAK CHECKS WERE GOOD AND A/C WAS RELEASED BACK INTO SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 964 hrs · 552 cycles

COCKPIT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED EMERGENCY FLASHLIGHT OPS CHECK GOOD AIRCRAFT RELEASED AND RETURNED TO SERVICE.