N752CX

Part: CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,597 hrs · 21,968 cycles

CORROSION ON THE INSIDE OF THE U CHANNEL THAT SUPPORTS THE HYD ISOLATION VALVE, LOCATED ON THE BACK WALL IN THE LEFT WHEEL WELL STA 1180

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 68,597 hrs · 21,968 cycles

.CORROSION OF THE UPPER EXTERIOR SURFACE OFTHE RIGHT WING UPPER SKIN FWD OF THE AILERON

Part: SUPPORT CHANNEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,597 hrs · 21,968 cycles

RH AFT LOWER WING TO BODY FAIRING FRAME BS 1037 IS CORRODED

Part: FITTING — DEFORMED (ZONE 600) · airframe 68,597 hrs · 21,968 cycles

REMOVED FOR ACCESS THE RW SIDE LINK ATTACH FITTING "MICKEY MOUSE FITTING" FOR SIDE LOAD FITTING ALIGHNMENT. DURING REMOVAL FOUND DAMAGED FREEZE PLUG/BUSHING IN HOLE.

Part: RUB BLOCK — CRACKED (ZONE 600 FLAP) · airframe 68,597 hrs · 21,968 cycles

RIGHT WING INBD FLAP T/E FAIRING 671BB HAD A CRACKED RUB BLOCK AT FAIRING AFT ATTACH ARM.

Part: SUPPORT — CORRODED (ZONE 500) · corrosion level 2 · airframe 68,597 hrs · 21,968 cycles

LEFT WING UNDER PANEL 551 AT SEVERAL AREA AROUND NUTPLATES ARE CORRODED.

Part: BEAM — WORN (ZONE 800)

RIGHT MLG STRUT DOOR SUPPORT BEAM IS HEAVILY WORN ALONG THE EDGE JUST FWD OF DRAG STRUT.

Part: DOOR — GOUGED (ZONE 800)

LEFT MLG DOOR GOUGED.

Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,597 hrs · 21,968 cycles

RH AFT WING TO BODY FAIRING ATTACH FRAME AT STA 1220 IS CORRODED.

Part: SKIN — CORRODED (ZONE 100) · airframe 68,597 hrs · 21,968 cycles

FUSELAGE EXTERNAL SKIN IS CORRODED AT LAP SEAM S-20L BS 1718.

Part: SUPPORT BRACKET — CORRODED (ZONE 100)

LEFT LOWER WING - BODY FAIRING SUPPORT BRACKET STA 958 IS CORRODED.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 68,597 hrs · 21,968 cycles

RH AFT LOWER WING TO BODY FAIRING FRAME STA 1050 IS CORRODED.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 68,597 hrs · 21,968 cycles

RIGHT WING LOWER SURFACE (INSPAR) IS CORRODED AROUND FASTENER AND RUNS UNDER PYLON RIGHT AT I/B SIDE OF PYLON APROX 5 INCHES AFT OF FWD SPAR AT STRINGER 14.

Part: RESERVOIR — UNSERVICEABLE (ZONE 800) · airframe 68,079 hrs · 21,878 cycles

FOUND L1 DOOR ACTUATOR EMERGENCY RESERVIOIR UNSERVICABLE. REMOVED AND REPLACED L1 DOOR ACTUATOR EMERGENCY RESERVOIR IN ACCORDANCE WITH BOEING 757 AIRCRAFT MAINTENANCE MANUAL 52-11-30.

Part: DISPLAY — INOPERATIVE (ZONE 200) · airframe 65,852 hrs · 21,488 cycles

PRIOR TO ETOPS ENTRY POINT CREW REPORTED, BOTH FLIGHT MANAGEMENT COMPUTER DISPLAYS BLANK. ADDITIONALLY, AIR TRAFFIC CONTROL REPORTED NO ADS-B DATA RECEIVED. AIRCRAFT WAS IN IMC, ALTERNATIVELY, NO LIGHTING WAS SIGHTED. WITH COMPONENT FAULTS PRESENTING, FLIGHT COULD NOT CONTINUE AS SCHEDULED ETOPS ROUTE. AIR TURN BACK TO DEPARTURE STATION FJDG. CREW DECLARED AN EMERGENCY DESCENT. LANDING WAS UNEVENTFUL AND NO ADDITIONAL PRECAUTIONARY ACTIONS WERE NOTED. ON ARRIVAL, THE AIRCRAFT WAS GROUNDED FOR MAINTENANCE. SUBSEQUENT TO FLIGHT MANAGEMENT COMPUTER BUILT IN TEST EQUIPMENT CHECK AND ADDITIONAL TROUBLESHOOTING PER BOEING 757-200 (B757) FAULT ISOLATION MANUAL 34-61-FAULT TREE 802, 22-02-FAULT TREE 828, AND 34-61-FAULT TREE 818, LINE MAINTENANCE REPORTED LEFT CONTROL DISPLAY UNIT FAULTY. LEFT MULTI-PURPOSE DISPLAY UNIT REMOVED AND REPLACED IAW B757-200 AIRCRAFT MAINTENANCE MANUAL 34-61-02. OPERATIONAL CHECK GOOD. PER B757-200 FAULT ISOLATION MANUAL 34-45-FAULT TREE 810 AND AIRCRAFT MAINTENANCE MANUAL 34-45-00, TRAFFIC ALERT AND COLLISION/AIR DATA COMPUTING SYSTEM OPERATIONAL TEST SATISFACTORY. NO FAULTS FOUND. LIGHTNING STRIKE AND WATER INTRUSION IN E/E BAY CONDITIONAL INSPECTIONS IAW B757-200 AIRCRAFT MAINTENANCE MANUAL 05-51-19 AND 05-51-13 GOOD. NO EVIDENCE OF LIGHTNING STRIKE OR WATER INTRUSION IN E/E BAY. AIRCRAFT RETURNED TO SERVICE.

Part: SPLICE — CORRODED (LT WING) · airframe 65,536 hrs · 21,428 cycles

LH WING, WING SIDE OF BODY SPLICE, UPPER SPLICE EVIDENCE OF CORRION BS 900 TO BS 940.

Part: TEE FITTING — CORRODED (NLG) · corrosion level 2 · airframe 65,534 hrs · 21,427 cycles

CORROSION ON NOSE LANDING GEAR WHEEL WELL RIGHT HAND T-CHORD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,430 hrs · 21,381 cycles

MULTIPLE TIMES DURING FLIGHT, R EMER DOOR EICAS MESSAGE DISPLAYED. FLIGHT CONTINUED UNAFFECTED. NO ADDITIONAL FAULTS NOTED. IAW B757 FAULT ISOLATION MANUAL 52-71-FAULT TREE 805, CLEARED DEBRIS AND VERIFIED SECURITY AND INTEGRITY OF DOOR SILL AREA. DOOR FOUND TO BE FAIRED WITH THE FUSELAGE. RIGHT NO 3 EMERGENCY EXIT DOOR OPERATIONAL TEST GOOD PER B757 AIRCRAFT MAINTENANCE MANUAL 52-21-01. NO FAULTS FOUND.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 65,178 hrs · 21,348 cycles

POST FLIGHT LINE MAINTENANCE IDENTIFIED, L4 DOOR EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED L4 EMERGENCY FLASHLIGHT BATTERY PER B757 AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,093 hrs · 21,329 cycles

POST FLIGHT LINE MAINTENANCE REPORTED, R4 EMERGENCY FLASHLIGHT INOPERTIVE. REMOVED AND REPLACED EMERGENCY FLASH LIGHT BATTERY IAW 757 AMM 25-64-00. OPERATIONAL CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE · airframe 64,630 hrs · 21,231 cycles

DURING ROUTINE MAINTENANCE DISCOVERED L3 UPPER AND LOWER EMERGENCY LIGHTS, UPPER R3 DOOR LIGHTS AND LIGHTS AT ROW 4L INOPERATIVE. REMOVED AND REPLACED L3 DOOR EMERGENCY BATTERY PACK IAW B757 AMM 33-51-07. SYSTEM OPERATIONAL CHECK GOOD.

Part: STRUCTURE — CORRODED (RT WING TE FLAP) · airframe 64,113 hrs · 21,121 cycles

RIGHT OB LOWER MAIN AFT FLAP CORROSION ON LOWER SURFACE

Part: STRUCTURE — CORRODED (RT WING TE FLAP) · airframe 64,113 hrs · 21,121 cycles

RIGHT OB LOWER MAIN AFT FLAP CORROSION ON LOWER SURFACE.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING LOWER SURFACE TRAILING EDGE FROM WING TIP TO OUTBOARD FLAP HINGE NUMEROUS SPOTS OF CORROSION.

Part: CHANNEL — WORN (NR 2 NACELLE) · airframe 64,113 hrs · 21,121 cycles

# 2 PYLON ANGLE CHANNEL COVER WORN SEVERAL AREAS.

Part: FITTING — DAMAGED (NR 2 NACELLE) · airframe 64,113 hrs · 21,121 cycles

UPON REMOVAL OF # 2 PYLON INBOARD BATHTUB FITTING FOUND TO BE DAMAGED.

Part: DOUBLER — CORRODED (BS 1148) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WHEEL WELL FS 1148 UPPER PRESSURE DECK RBL 3 CORROSION ON DOUBLER AROUND HYDRAULIC FITTING.

Part: KEEPER — CORRODED (LT MLG WW) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WHEEL WELL FS 1060 10 INCHS OUTBOARD OF KEEL WEB TOP SIDE OF WHEEL WELL HYDRAULIC LINE ISOLATOR GROMMET KEEPER CORRODED HARDWARE AND CORROSION ON ANCHORING ANGLE.

Part: BRACKET — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING TRAILING EDGE SUPPORT BRACKET ATTACHING TO FUSELAGE FOR PANEL HAS CORROSION BL. 70.50 STATION 1158.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

CORROSION ON UPPER SURFACE LEFT WING ABOVE PYLON AREA 3 SPOTS.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

THREE AREAS OF CORROSION ON EXTERNAL LOWER SURFACE OF LEFT WING SKIN ON STRINGER L6 AT WS 150.50 TO 177.50.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING LOWER SURFACE CORROSION AROUND FUEL STICK 7 PANEL STATION 606.

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WHEEL WELL RBL 0 STATION 1096 HAS CORROSION ON INTER VERTICAL WEB AT MULTIPLE LOCATIONS.

Part: SKIN — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

NUMBER 2 PYLON THRU ACCESS PANEL 443AR INTERNAL SKIN LWR SECTION AROUND OPENING HAS CORROSION.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

#2 PYLON LEADING EDGE PANEL CORRODED SEVERAL SPOTS ON REPAIR RACK.

Part: STRINGER — CORRODED (BS 1412 S29L) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

AFT LOWER CARGO COMPARTMENT STA 1412 BELLY OF FRAME APPROX 29L STRINGER END HAS BAD CORROSION ON EAR OF STRINGER.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING SKIN LOWER SURFACE IS CORRODED AT WS 742.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

#2 PYLON ACCESS THRU PANEL 443HL LOWER FORWARD CORNER STRUCTURE INTERNALLY HAS CORROSION.

Part: NONE — NONE (ZONE 600) · airframe 64,113 hrs · 21,121 cycles

#7 SLAT HAS COMPOSITE DAMAGE MARKED LOWER TRAILING EDGE.

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

#2 PYLON THRU ACCESS PANEL 443CR INTERNAL SKIN HAS CORROSION FWD AND BELOW CUTOUT.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING SKIN LOWER SURFACE CORRODED AT WS 663 REAR SPAR.

Part: SLAT — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

# 7 SLAT HAS COMPOSITE DAMAGE MARKED LOWER TRAI;ING EDGE.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

PREVIOUS REPAIR ON LEFT WING UPPER SKIN AT WS 150.5 THRU WS 204.5 NEEDS REACCOMPLISHED PER AMES REA 47508REA41 AND FVCI ENGINEERING ORDER 22082-22 REV C.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

CORROSION ON EXTERNAL SIDE OFM LEFT WING LOWER SKIN AT WS 21.00 AND AFT FUEL PANEL 531CB CUTOUT.

Part: ACCESS PANEL — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

# 2 PYLON ACCESS THRU PANEL 433GL INTERNAL SKIN LOWER SECTION AROUND PANEL HAS CORROSION.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING TRAILING EDGE AROUND BBL. 70.50 BRACKET HAS CORROSION.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING UPPER TRAILING EDGE SKIN HAS CORROSION IN MULTIPLE AREAS ON BOTH SIDES (UPPER/LOWER) APPROXIMATELY AT WS. 188 TO WS. 216.

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING TRAILING EDGE AROUND WS. 177.50 AFT OF STABILIZING LINK( IN BETWEEN LANDING GEAR AND WHEEL WELL) BRACKET HAS CORROSION.

Part: SKIN — CORRODED (ZONE 600) · airframe 64,113 hrs · 21,121 cycles

RIGHT WING UPPER TRAILING EDGE SKIN HAS CORROSION IN MULTIPLE AREAS ON BOTH SIDES (UPPER/LOWER) APPROXIMATELY AT W.S. 188 TO W.S. 216.

Part: BRACKET — CORRODED (ZONE 600) · airframe 64,113 hrs · 21,121 cycles

RIGHT WING TRAILING EDGE UPPER SUPPORT BRACKET FOR WIRING HAS CORROSION AT WS 168 - WS 181.

Part: BRACKET — CORRODED (ZONE 600) · airframe 64,113 hrs · 21,121 cycles

RIGHT WING TRAILING EDGE AROUND BBL 70.50 HAS CORROSION.

Part: SUPPORT BEAM — CORRODED (ZONE 600) · airframe 64,113 hrs · 21,121 cycles

RIGHT WING TRAILING EDGE AROUND W.S.177.50 AFT OF STABILIZING LINK 9IN-BETWEEN LANDING GEAR AND WHEEL WELL.SUPPORT BEAM

Part: SKIN PANEL — CORRODED (ZONE 600) · airframe 64,113 hrs · 21,121 cycles

RIGHT WING LOWER SKIN (PANEL #1) WS 663 HAS CORROSION.

Part: SUPPORT BEAM — CORRODED (ZONE 200) · airframe 64,113 hrs · 21,121 cycles

LOWER CHORD HAS CORROSION AT STA 1180 - 1242.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING SKIN LOWER SURFACE IS CORRODED AT W.S. 736 REAR SPAR.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING LOWER T/E EXTERNAL SKIN HAS CORROSION AT W.S.708.

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

NUMBER 1 PYLON INBOARD SIDE FORWARD EXTERNAL SKIN REQUIRES REMOVAL FOR CORROSION.

Part: ROLLER TRAY — DAMAGED (UPPER CARGO) · airframe 64,113 hrs · 21,121 cycles

UPPER CARGO ROLLER AT RBL 30.0 IS CUT.

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

# 1 PYLON INBOARD SIDE INTERNAL SKIN AROUND PANEL 433LR HAS CORROSION IN MULTIPLE AREAS.

Part: SKIN PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING LOWER T/E EXTERNAL SKIN HAS CORROSION AT W.S. 656.

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

# 1 PYLON OUTBOARD SIDE SKIN AROUND 433BL HAS CORROSION INTERNALLY IN MULTIPLE AREAS.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

CORROSION ON UPPER SURFACE LEFT WING 48" FROM FUSELAGE 50" FROM LEADING EDGE.

Part: PRESSURE DECK — CORRODED (RT MLG WW) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WHEEL WELL PRESSURE DECK WEB CORRODED AT STA 1139.819, BL 0 - RBL 8.20

Part: PRESSURE DECK — CORRODED (RT MLG WW) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WHEEL WEEL PRESSURE DECK WEB CORRODED AT STA 1159, RBL 4 AND STA 1153, RBL 6.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

CORROSION ON UPPER SURFACE LEFT WING 48" FROM FUSELAGE 50" FROM LEADING EDGE.

Part: SKIN — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

CORROSION BETWEEN SKIN AND PYLON STRUCTURE IN TWO PLACES FWD AND AFT SIDE INSIDE #1 PYLON OUTBOARD PANEL 433AL.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING SKIN LOWER SURFACE IS CORRODED AT W.S. 698 REAR SPAR.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING SKIN LOWER SURFACE IS CORRODED AT W.S. 761 REAR SPAR.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING TRAILING EDGE WS 832 OUTBOARD OF THE AILERON AREAS OF CORROSION AROUND NUT-PLATES.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING INBD MAIN FLAP HAS 3 DAMAGED AREAS ON THE UPPER SKIN PANEL.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING SKIN LOWER SURFACE IS CORRODED AT W.S. 751 REAR SPAR.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING UPPER SURFACE PANEL ABOVE LANDING GEAR ACTUATOR OUTBOARD BOLT CORROSION UNDER NUMEROUS NUT-PLATES.

Part: SUPPORT BEAM — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING T/E PANEL SUPPORT BEAM HAS CORROSION ON TOP APPROX W.S. 216.

Part: SHIM — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING CLECO POINT ATTACHMENT CORRODED APPROX WING STATION 223.

Part: WEB — CORRODED (LT MLG WW) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

KEEL WEB IN LEFT WHEEL WELL SHOWS SIGNS OF CORROSION AT STA 1146.

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

ANGLE IN THE LEFT WHEEL WELL SHOWS SIGNS OF CORROSION FOR THE PRESSURE SENSITIVE FLOW LIMITER ABOVE THE TRANSFER CYLINDER ACCUMALATOR ON THE KEEL WEB.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING CORROSION ON LOWER SURFACE OF SKIN AT FSS 580 10'' AFT OF L/E.

Part: SKIN — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

# 2 PYLON ACCESS THRU PANEL 443HL LOWER FORWARD CORNER STRUCTURE INTERNALLY HAS CORROSION.

Part: FITTING — CORRODED (BS 1140) · airframe 64,113 hrs · 21,121 cycles

LOWER KEEL FITTING STA 1140 RIGHT WHEEL WELL REMOVED FOR REPLACEMENT BECAUSE REA REPAIR SHIFTING HOLE ATTACH POINTS.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING LOWER SURFACE IS CORRODED AT W.S. 646, REAR SPAR.

Part: CHANNEL — CORRODED (ZONE 400) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

THE HEAT SHIELD ON THE AFT STRUT FAIRING HAS BULGED AREA ON THE INBOARD SIDE.

Part: SHIM — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING UPPER T/E BONDED PANEL, BONDED SHIM STACK IS CORRODED

Part: SKIN — CORRODED (NR 2 NACELLE) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

#2 PYLON THRU ACCESS PANEL 443CR, INTERNAL SKIN HAS CORROSION FWD, AFT AND BELOW CUTOUT.

Part: STIFFENER — CORRODED (ZONE 100) · airframe 64,113 hrs · 21,121 cycles

BRACKET IN THE RIGHT WHEEL WELL AT STA 1086 RBL4 HAS CORROSION.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 64,113 hrs · 21,121 cycles

RIGHT WHEEL WELL 1040 HOT EXHAUST FRAME INBD ANGLE CORROSION UNDER NUT PLATES.

Part: ATTACH ANGLE — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING T/E UPPER SUPPORT BEAM FWD ATTACH LINKS CORRODED APPROX W.S. 216 OR WBL 130.

Part: PRESSURE DECK — CORRODED (ZONE 100) · airframe 64,113 hrs · 21,121 cycles

RIGHT WHEEL WELL PRESSURE DECK WEB STA 1139.819, BL 0, RBL- 8.20 CORRODED.

Part: SKIN — CRACKED (LT MLG DOOR) · airframe 64,113 hrs · 21,121 cycles

LEFT MLG BODY DOOR EXTENSION TRAILING EDGE IS CRACKED/DIS-BONDED.

Part: PRESSURE DECK — CORRODED (ZONE 100) · airframe 64,113 hrs · 21,121 cycles

RIGHT WHEEL WELL PRESSURE DECK WEB STA1160, RBL 8.20 - 16.50 CORRODED.

Part: PRESSURE DECK — CORRODED (RT MLG WW) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RT WHEEL WELL PRESSURE DECK SHOWS SIGNS OF CORROSION STA 1130 - 1154 RBL 0-12.

Part: PRESSURE DECK — CORRODED (ZONE 100) · airframe 64,113 hrs · 21,121 cycles

RIGHT WHEEL WELL PRESSURE DECK WEB STA 1159, RBL 4 AND STA 1153, RBL 6 CORRODED.

Part: WEB — CORRODED (BS 1100) · airframe 64,113 hrs · 21,121 cycles

CORROSION ON WEB STA. 1100.

Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RW SKIN LOWER SURFACE CORRODED, RT WING STATION 676.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 64,113 hrs · 510,202 cycles

FWD ATTACH ANGLE AT PANEL 198JR IS CRACKED(RT FILLET AREA) REF AMES N/R 147534-0100-0281

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

BRACKET CORRODED

Part: PRESSURE WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RWW PRESSURE DECK CORRODED

Part: SLAT — DAMAGED (ZONE 600) · airframe 6,411,321 hrs · 21,121 cycles

#7 SLAT COMPOSITE DAMAGE

Part: TIE CLIP — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LWW SUPPORT ANGLE CORRODED

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING LOWER SKIN PANEL CORRODED.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

CORROSION UPPER SURFACE LW

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RWW UPPER PRESSURE DECK STIFFENER CORRODED

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RWW STIFFENER CORRODED

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LMLG DOOR FORWARD LOWER ANGLE CORRODED

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LW LOWER SURFACE IS CORRODED

Part: PRESSURE DECK — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WHEEL WELL PRESSURE DECK CORRODED

Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

PANEL 117BL CORRODED

Part: SKIN SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

ANGLE CORRODED LWW

Part: SKIN SPLICE — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LWW ANGLE CORRODED

Part: PRESSURE WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WHEEL WELL PRESSURE PANEL CORRODED

Part: BRACKET — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RIGHT WING TRAILING EDGE SUPPORT BRACKET CORRODED.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LW L/E RIB LWR STRAP AT WS 285.65 CORRODED

Part: SUPPORT PLATE — CORRODED (ZONE 500) · corrosion level 2

LT WING PANEL 551CT CORRODED

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING LOWER WING PNL STA. 822-829 IS CORRODED AT FUEL PNL

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LWW UPPER WEB STIFFENER AT STA 1144 LBL 16.5 CORRODED

Part: BRACKET — CORRODED (ZONE 100) · airframe 64,113 hrs · 21,121 cycles

REF AMES NR 147534-0100-0150 LWW FS1180 35" OTBD KEEL CENTER WEB AT CEILING ISOLATION VALVE STAND OFF MOUNTING WEB CORROSION ON AFT SIDE.

Part: FLAP SYSTEM — CRACKED (ZONE 600) · airframe 64,113 hrs · 21,121 cycles

FOUND CRACK IN THE RIGHT O/B AFT FLAP T/E LOWER SURFACE BY THE O/B SUPPORT FITTING

Part: SKIN PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING TE EXTERNAL SKIN CORRODED AT WS 717.5 TO 775.5

Part: SKIN PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING UPPER SURFACE L/E CORRODED

Part: WEB — CORRODED (BS 1175) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

KEEL WEB IN LEFT WHEEL WELL AT STA 1175 SHOWS SIGNS CORROSION AROUND HYDRAULIC LINES

Part: STIFFENER — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LONGITUDINAL STIFFENER IN LEFT WHEEL WELL AT LWS 38 FROM STA 1100-1110 CORRODED

Part: SKIN PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING LOWER SKIN CORRODED FROM WS 150-177.5 AT AFT SPAR

Part: WEB — CORRODED (BS 900) · airframe 64,113 hrs · 21,121 cycles

REF AMES NR 147534-0100-0077 AFT SIDE OF STA 900 WEB IS CORRODED AROUND PNEUMATIC DUCT AND HYDRAULIC LINE RBL 12

Part: PRESSURE DECK — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LT WHEEL WELL PRESSURE DECK CORRODED

Part: SKIN — CORRODED (LT WING) · airframe 64,113 hrs · 21,121 cycles

CORROSION ON UPPER SURFACE LWING 60" FROM FUSELAGE 18" FROM L/E. REF AMES NR 147534-0500-0030

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RT WHEEL WELL PRESSUER DECK CORRODED STA 100 RBL 49

Part: PRESSURE DECK — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LT WHEEL WELL PRESSURE DECK CORRODED

Part: FLOORBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LOWER FLANGE OF ANGLE IN THE KEEL AREA AT STA 1168 CORRODED

Part: DOOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RT WHEEL WELL PRESSURE DECK CORRDED STA 1094 RBL 47

Part: PRESSURE DECK — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RT WHEEL WELL PRESSURE DECK CORRODED

Part: DOOR — CORRODED (ZONE 100) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

RT WEHEEL WELL PRESSURE DECK CORRODED STA 1100 RBL 64-58

Part: SKIN PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

UPPER SURFACE LEFT WING ABOVE PYLON AREA CORRODED

Part: SKIN — CORRODED (WS 74.5 S8L) · airframe 64,113 hrs · 21,121 cycles

CORROSION ON EXTERNAL SURFACE OF LEFT WING LOWER SKIN AT WS 74.5 AND APPROXIMATELY SIX INCHES AFT OF STRINGER L8 REF AMES NR 147534-0500-0018

Part: SKIN PANEL — CORRODED (ZONE 600) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

CORROSION ON EXTERNAL SIDE OF RIGHT WING REAR SPAR LOWER CHORD IN RIGHT WHEEL WELL WHERE SPAR ATTACHES TO CENTER WING BOX

Part: SKIN PANEL — CORRODED (ZONE 500) · corrosion level 2 · airframe 64,113 hrs · 21,121 cycles

LEFT WING EXTERNAL LOWER SURFACE SKIN STR L6 AT WS 150.5 TO 177.5 CORRODED

Part: ROLLER TRAY — CUT (ZONE 200) · airframe 64,113 hrs · 21,121 cycles

UPPER CARGO ROLLER TRAY AT RBL 30.0 IS CUT REF AMES N/R 147534-0200-0042

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,860 hrs · 20,781 cycles

AIRCRAFT GROUNDED FOR UNSCHEDULED POWER PLANT MAINTENANCE, IDENTIFIED R1 DOOR EMERGENCY EXIT DOORS LIGHT INOPERATIVE. REMOVED AND REPLACED REMOVED AND REPLACED R1 EMERGENCY EXIT LIGHTS POWER SUPPLY IAW AMM 33-51-07. OPERATIONAL CHECK SATISFACTORY. NO FURTHER DEFECTS NOTED.

Part: SWITCH — FAULTY (EMERGENCY LIGHT) · airframe 62,593 hrs · 20,672 cycles

DURING EMERGENCY LIGHT OPS CHECKS MULTIPLE LIGHTS FAILED TO COME ON. REMOVED AND REPLACED TWO BATTERY PACKS AT M736 AND M737 IAW AMM 33-51-07. REMOVED AND REPLACED 5 AMP FUSE IAW AMM 33-51-07. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. OPS CHECK GOOD. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH IAW SWPM 20-83-11 OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 62,593 hrs · 20,672 cycles

DURING EMERGENCY LIGHT OPS CHECKS MULTIPLE LIGHTS FAILED TO COME ON. REMOVED AND REPLACED TWO BATTERY PACKS AT M736 AND M737 IAW AMM 33-51-07. REMOVED AND REPLACED 5 AMP FUSE IAW AMM 33-51-07. PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW 33-51-00 OPS CHECK GOOD. REMOVED AND REPLACED EMERGENCY LIGHT SWITCH IAW B757-SWPM 20-83-11 OPS CHECK GOOD.

Part: STRINGER — CORRODED (RT WING) · airframe 62,593 hrs · 20,672 cycles

RIGHT WING STA 718 STRINGER U12 WAS CORRODED. REMOVED AND ELVAUATED CORROSION, ORIGNAL MATERIAL .100 IN., MATERIAL LOSS .068 IN., MATERIAL REMAINING .022., MATERIAL LOSS ALLOWABLE 10%. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND PERFORMED STRINGER REPAIR IAW SRM. 57-00-03 DET.III., REPAIR 1 FIGURE 201, 53-20-03 AND ER RES 15213.

Part: DOUBLER — CORRODED (NR 2 NACELLE) · airframe 62,593 hrs · 20,672 cycles

NR 2 NACELLE STRUT DOOR (443LL) HAS CORROSION ON FWD BOTTOM CORNER ON DOOR LANDING. ACCOMPLISHED REPAIR IAW ENGINEERING ORDER CONTROL 20191, TITLED REPAIR-DOUBLER, INBOARD NACELLE SIDE SKIN PANEL ASSEMBLY NR 2 ENG, PPS 176.25.

Part: SUPPORT BEAM — CORRODED (ZONE 100) · airframe 52,028 hrs · 18,242 cycles

NON-ROUTINE 2832N248 DISCREPANCY. LMWW, CORROSION ON FWD LOWER FLANGE OF LT MAIN GEAR DOOR ACTUATOR SUPPORT BEAM STA 1120. CORRECTIVE ACTION, LT WHEEL WELL MAIN GEAR DOOR ACTUATOR SUPPORT REPAIRED IAW FVCI EO CONTROL 20184.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 62,593 hrs · 20,672 cycles

AIRBORNE/PEMCO NON-ROUTINE 2832N241 DISCREPANCY: CORROSION ON KEEL BEAM LOWER SURFACE NLEFT CHORD AT STA 1170 CORRECTIVE ACTION: REPAIRED PER FVCI E.O. #20174

Part: FLOOR SUPPORT — CORRODED (BS 324-345) · airframe 62,593 hrs · 20,672 cycles

FWD WET AREA, FLOOR SUPPORT BETWEEN BS 324 AND 345 CORRODED AT RBL 40. ACCOMPLISHED EO 20215, REPAIR OF SEC. 41 WITHOUT ANY DEVIATIONS.

Part: DOUBLER — CORRODED (NR 2 NACELLE) · airframe 62,593 hrs · 20,672 cycles

NR 2 NACELLE STRUT DOOR (443LL) HAS CORROSION ON FWD BOTTOM CORNER ON DOOR LANDING. ACCOMPLISHED REPAIR IAW ENGINEERING ORDER CONTROL 20191, TITLED REPAIR-DOUBLER, INBOARD NACELLE SIDE SKIN PANEL ASSEMBLY NR 2 ENG, PPS. 176.25.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 62,593 hrs · 20,672 cycles

NON-ROUTINE 2832N271 DISCREPANCY, NWW, STA 263 BLKHD AFT FACE, LOWER CHORD HAS CORROSION FROM STR 26L TO STR 26R. CORRECTIVE ACTION: REPAIRED NWW STA 263 BULKHEAD LOWR CHORD PER EO CONTROL 20172 + 20181.

Part: PANEL — CORRODED (NR 1 PYLON) · airframe 62,593 hrs · 20,672 cycles

NON-ROUTINE 2832N283, NR 1 ENG ZONE 433 NACELLE STRUT MID STRUCTURE O/B PANEL, LWR AFT CORNER; FOUND EXCESSIVE CORROSION. REPAIRED NR 1 ENGINE NACELLE STRUT MID STRUCTURE O/B PANEL, ACCOMPLISHED REPAIR ON ENGINEERING ORDER 20192, WITHOUT ANY DEVIATIONS.

Part: SERVICE PANEL — CORRODED (ZONE 100) · airframe 62,593 hrs · 20,672 cycles

FWD LAV SVC PANEL INSIDE ALL FASTENER ARE CORRODED AND 2EA COVER PLATES HAVE CORROSION. REMOVED AND REPLACED FASTENERS AND FABRICATED 2EA COVER PLATES ON 2832N1011, ACCOMPLISHED EO 20195 ON N/R 2832N245 WITHOUT ANY DEVIATIONS.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 62,593 hrs · 20,672 cycles

NWW LOWER CHORD HAS CORROSION BETWEEN RT AFT GEAR DOOR AND HINGE FITTINGS. REMOVED CORROSION ON NWW LWR CHORD RT AFT AREA IAW-B757-200-SRM-53-10-14. GRID MAP LWR CHORD AREA 2 EA AREA ON LWR CHORD, IAW- PRELIMINARY-E.O. CONTROL 20613. HFEC ACCOMPLISHED IAW-NTM-PT6-51-00-19 AND ROTO PROBE ACCOMPLISHED, IAW-NTM-PT6-51-00-16. ACCOMPLISHED EO CONTROL 20163.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 62,593 hrs · 20,672 cycles

NON-ROUTINE 2832N258 DISCREPANCY. RMWW, CORROSION ON KEEL BEAM RIGHT CHORD UPPER SURFACE IN RADIUS OF TAB THAT ATTACHES TO STA 1120 GEAR DOOR ACTUATOR SUPPORT BEAM. CORROSION RUNS UNDER SUPPORT BEAM. CORRECTIVE ACTION. REMOVED CORROSION ON RT KEEL BEAM CHORD UPPER SURFACE AT STA 1120, RBL 7.5, MINIMUM REMAINING THICKNESS 0.187", REMOVED 0.063", ORIGINAL THICKNESS 0.250". REWORK SUBSTANTIATED AND REPAIRED IAW ENGINEERING ORDER CONTROL NR 20178.

Part: SPAR CAP — CORRODED (LT WING) · corrosion level 2 · airframe 60,327 hrs · 20,135 cycles

CORRODED UPPER AFT SPAR CAP AT LEFT WS 180. REPAIRED THE SPAR CAP IAW 47313REA05.

Part: SUPPORT BEAM — CORRODED (BS 1040-1060) · corrosion level 2 · airframe 60,327 hrs · 20,135 cycles

PANEL SUPPORT BEAM INBD OF PANEL 197BL IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04. REMOVED AND REPLACED IAW DWG 149N7550, AND SRM 51-40-02, PARA 7. AIRCRAFT GROUNDED

Part: TUBE — CRACKED (NR 1 NACELLE) · airframe 60,327 hrs · 20,135 cycles

NR 1 PYLON AFT MOUNT BARREL NUT FWD GUIDE TUBE IS CRACKED, LANYARDS ARE NOT SECURE. REPAIRED THE MOUNT BARREL NUT FWD GUIDE TUBE IAW AMES 47313REA01 AND SECURED THE LANYARDS IAW AMM 71-21-03.

Part: STIFFENER — CORRODED (BS 1040) · corrosion level 2 · airframe 60,327 hrs · 20,135 cycles

RIGHT MLG WW BS 1040 BULKHEAD ABOVE ECS DUCT,STIFFENER IS CORRODED AT FASTENER. REMOVED & REPLACED THE CHANNEL STIFFENER IAW SRM 51-40-02 & 58-757-35-0024.

Part: SKIN — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 60,327 hrs · 20,135 cycles

RT OTBD FORE FLAP LOWER SURFACE HAS 2 SMALL AREAS OF CORROSION OTBD OF THE OTBD SUPPORT MECHANISM. REPAIRED THE AREAS OF CORROSION ON THE RT WING OTBD FORE FLAP LOWER SURFACE IAW SRM 57-53-01, REPAIR 5, FIG 201. AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE.

Part: WEB — CORRODED (BS 1105-1110) · corrosion level 2 · airframe 60,327 hrs · 20,135 cycles

LWR KEEL WEB HAS AREA OF CORROSION AROUND HYD LINE BULKHEAD FITTING JUST FWD AND ABOVE LANDING GEAR DOOR ACTUATOR. REPAIRED THE VERTICAL LWR KEEL WEB IAW REA47313 REA 03.REINSTALLED ABOVE THE GEAR DOOR ACTUATOR. LEAK CHECKED IAW IAW AMM 29-11-00. ACFT GROUNDED.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 59,491 hrs · 19,953 cycles

L4 INBOUND FLASHLIGHT BATTERY DEAD. REMOVED AND REPLACED THE BATTERY IAW AMM 25-60-00.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 59,342 hrs · 19,927 cycles

CAPTAIN'S EMERGENCY FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERIES IAW AMM 25-64-00. OPS CHECKED SATISFACTORY. AIRCRAFT RELEASED TO SERVICE.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 58,333 hrs · 19,739 cycles

IN FLIGHT EMERGENCY DECLARATION. AIR TURN BACK. 5 COMPRESSOR STALLS/SURGES WITH ENGINE EXCEEDANCE VALUES RECORDED. INDICATIONS RETURNED TO NORMAL THEREAFTER AND PRIOR TO LANDING. AIRCRAFT GROUNDED FOR BORESCOPE INSPECTION AND FURTHER ANALYSIS. WORK IN PROGRESS. REMOVED AND REPLACED VALVE ASSY. REMOVED AND REPLACED RIGHT ENGINE. OPERATIONAL CHECKS SATISFACTORY. ENGINE RUNS SATISFACTORY. FAULT NOT DUPLICATED. NO FURTHER DEFECTS NOTED. AIRCRAFT RELEASED TO SERVICE ETOPS 180.

Part: SKIN — DENTED (BS 1701-1720) · airframe 58,291 hrs · 19,725 cycles

SKIN DENTED BETWEEN BS 1701 AND 1720, STRINGER 11 TO 16L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIGURE 101. REPAIRED THE AREA IAW ENGINEERING DOCUMENT 47255REA01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,862 hrs · 19,457 cycles

L3 AND R3 EMERGENCY EXIT DOOR LIGHTS INOPERATIVE. R & R BATTERY POWER PACK AT MID/AFT IAW AMM 33-51-07. OPS CHECK SATISFACTORY. ADDITIONAL FAULTS NOT NOTED. ACFT RELEASED TO SERVICE.

Part: LINER — DEFECTIVE (R4 DOOR) · airframe 56,717 hrs · 19,431 cycles

R4 DOOR WILL NOT DISARM. RETRACTABLE DOOR MECHANISM STICKING DUE TO EXCESSIVE CONTACT WITH DOOR LINERS. TRIMMED DOOR LINER ON L4 DOOR. OPERATIONAL CHECKED SATISFACTORY IAW AMM 52-11-20. ACFT RELEASED TO SERVICE.

Part: LINER — DEFECTIVE (L4 DOOR) · airframe 56,717 hrs · 19,431 cycles

L4 DOOR WILL NOT DISARM. UPON TROUBLESHOOTING FOUND RETRACTABLE DOOR MECHANISM STICKING DUE TO EXCESSIVE CONTACT WITH DOOR LINERS. TRIMMED DOOR LINER ON L4 DOOR. OPERATIONAL CHECK SATISFACTORY. ACFT RELEASED TO SERVICE ETOPS 180.

Part: SLEEVE — WORN (L4 DOOR) · airframe 56,652 hrs · 19,413 cycles

L4 EXTERIOR DOOR HANDLE DOES NOT OPERATE PROPERLY. R & R WORN BEARING SLEEVE ON L4 DOOR EXTERIOR HANDLE & ADJUSTED IAW AMM 52-11-25. OPERATIONAL CHECKED SATISFACTORY IAW AMM 52-11-00. ACFT RELEASED TO SERVICE.

Part: GUIDE ARM — WORN (L4 DOOR) · airframe 56,652 hrs · 19,413 cycles

L4 DOOR HARD TO CLOSE. DOOR SEAL WILL NOT REMAIN SECURE IN SEAL RETAINER. REMOVED L4 DOOR. R & R L4 DOOR GUIDE ARM ASSEMBLY IAW AMM 52-11-04. ADJUSTED LATCH ROLLER IAW AMM 52-11-00 2G STEP 2. OPERATIONAL CHECKED SATISFACTORY. PRESS LEAK CHECKED IAW AMM 05-51-24 SATISFACTORY. FAULT NOT DUPLICATED. NO ADDITIONAL FAULTS NOTED. ACFT RELEASED TO SERVICE.

Part: MECHANISM — LACK OF LUBE (R4 DOOR) · airframe 56,601 hrs · 19,398 cycles

R4 PAX & CREW DOOR HARD TO CLOSE. DETAILED VISUAL INSPECTION, NOTED NO FAULTS ATTRIBUTING TO REPORTED DIFFICULTY. LUBRICATED R4 DOOR LATCH CRANK ROLLERS MECHANISM IAW AMM 12-21-18. OPERATIONAL CHECK VERIFIED INTEGRITY OF R4 DOOR. ACFT RELEASED TO SERVICE.

Part: DOOR SEAL — OUT OF POSITION (L4 DOOR) · airframe 56,601 hrs · 19,398 cycles

L4 DOOR DIFFICULT TO CLOSE FROM INSIDE. DOOR SEAL WILL NOT STAY IN TRACK. RE-INSTALLED SEAL IN RETAINER TRACK IAW AMM 52-09-01. VERIFIED INTEGRITY OF SEAL WITH OPERATIONAL CHECK. NO ADDITIONAL FAULTS NOTED. SEAL REMAINED IN TRACK. ACFT RELEASED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 56,586 hrs · 19,393 cycles

R1 EXTERIOR EMER LIGHT INOPERATIVE. DOES NOT ILLUMINATE. UPON TROUBLESHOOTING NOTED THE POWER SUPPLY HAS NO POWER. R & R THE BATTERY EMER POWER SUPPLY IAW AMM 33-51-07. OPERATIONAL CHECKED SATISFACTORY. NO FURTHER DEFAULTS NOTED. ACFT RELEASED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 56,586 hrs · 19,393 cycles

L1 INTERIOR EMER SIGN INOPERATIVE, DOES NOT ILLUMINATE. REPAIRED WIRE 23532-0011-22 AT CONNECTOR D4532 IAW SWPM 20-10-13. OPERATIONAL CHECK SATISFACTORY IAW AMM 33-51-01. NO ADDITIONAL FAULTS NOTED. ACFT RELEASED TO SERVICE.

Part: SLIDE — DEPLOYED (L1 DOOR) · airframe 56,585 hrs · 19,392 cycles

ENGINE RUN, AFTER ENG SHUTDOWN L1 DOOR SLIDE DEPLOYED. R & R L1 SLIDE & L1 DOOR ASSIST RESERVOIR IAW AMM 25-66-01 & 52-11-30 RESPECTIVELY. DOOR ASSIST PRESS CHECKS SATISFACTORY IAW DOOR ASSIST. L2 DOOR OPERATIONAL CHECKED SATISFACTORY, NO FAULTS NOTED. ACFT RELEASED TO SERVICE.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 55,291 hrs · 19,142 cycles

ROW 2 RT OVERHEAD BIN, PAX CABIN MEGA PHONE INOPERATIVE. DEFERRED IAW MEL 25-63-01-01. CAT D, NO FLY DATE 09 11 2015. PART REQUISITIONED, WORK IN PROGRESS.

Part: GLOWSTRIP — DETACHED (CABIN) · airframe 55,268 hrs · 19,137 cycles

ROW 6 LT SIDE LIGHT STRIP MISSING RED DOT. ROW 2 REPOSITIONED, PHOTO LUMINESCENT STRIP AT ROW 2 LT SIDE TO REVEAL RED EXIT LOCATOR SQUARE IAW AMM 33-51-00. ACFT RELEASED TO SERVICE.

Part: DIODE — LOOSE (INDICATION SYS) · airframe 55,220 hrs · 19,125 cycles

NOSE LANDING GEAR INDICATOR INOPERATIVE DURING APPROACH & LANDING. AFTER 2ND CYCLE OF LG LIGHT WITH 1/2 ILLUMINATION OCCURRED. EMER DECLARED AT DESTINATION STATION. NO ISSUES WITH LANDING. GND PERSONNEL ADVISED OF ALL THREE LG DOWN INDICATION. NO EICAS MX MSGS WERE NOTED. PERFORMED PSEU TEST IAW MM 32-09-04. NO INFLIGHT MSGS PRESENT. FOUND DIODE CARD IN NLG POSITION INDICATOR LOOSE. RESEATED INTO SOCKET & RELAMPED IAW MM 33-13-00. LG POSITION INDICATION SYS TESTED SATISFACTORY IAW AMM 32-61-00. ACFT RELEASED TO SERVICE.

Part: WIRE — DAMAGED (CABIN) · airframe 55,054 hrs · 19,087 cycles

RIGHT FWD EMER EXIT AISLE LIGHT INOPERATIVE. COMPLIED WITH FIM 33-51 FT 802. REPAIRED WIRING AT RT FWD AISLE LIGHT SOCKET IAW SWPM 20-10-11 & RELAMPED IAW AMM 33-51-05. SYSTEMS OPERATIONAL CHECKED SATISFACTORY IAW AMM 33-51-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 54,858 hrs · 19,043 cycles

L3 DOOR, R3 DOOR & LT FWD AISLE EMER EXIT LIGHTS INOPERATIVE. COMPLIED WITH FIM 33-51 FT 802. R & R L3 DOOR EMER EXIT LIGHTS BATTERY POWER SUPPLY ASSEMBLY IAW AMM 33-51-07. SYS OPERATIONS CHECKED NORMAL IAW AMM 33-51-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 54,838 hrs · 19,039 cycles

R4 DOOR EMER EXIT LIGHTED SIGNS INOPERATIVE. R & R R4 DOOR EMER LIGHTS POWER SUPPLY BATTERY PACK IAW AMM 33-51-07. SYSTEMS OPERATIONAL CHECKED SATISFACTORY IAW AMM 33-51-00.

Part: BATTERY — NOT SEATED (CABIN) · airframe 54,809 hrs · 19,033 cycles

R4 DOOR EMER EXIT SIGN INOPERATIVE. RESEATED R4 DOOR EMER EXIT LIGHTS POWER PACK BATTERY IAW AMM 33-51-07. OPERATIONS CHECKED NORMAL IAW AMM 33-51-00.

Part: DIAPHRAGM — CRACKED (L1 DOOR) · airframe 54,403 hrs · 18,936 cycles

L1 DOOR RESERVOIR DEPLOYED. FAULT ISOLATED TO DOOR ASSIST BOTTLE DIAPHRAGM. REMOVED, REPAIRED, SERVICED & INSTALLED L1 RESERVOIR IAW AMM 52-61-3 & AMM 12-15-10. LEAK & OPERATION CHECK SATISFACTORY.

Part: COVER — DETACHED (L4 DOOR) · airframe 54,346 hrs · 18,925 cycles

L4 AFT GIRT BAR COVERS NOT ATTACHED. AFT GIRT BAR COVERS REMOVED. DMI 45243 INITIATED. CAT A NO CONDITIONS NFD 10/15/2014.

Part: COVER — DETACHED (L4 DOOR) · airframe 54,346 hrs · 18,925 cycles

L4 DOOR FWD GIRT BAR COVERS NOT ATTACHED. FWD AFT COVERS REMOVED. DMI 45243 INITIATED IAW MEL 25-20-01-01. CAT A NO SPECIAL CONDITIONS NO FLY DATE 10/15/2014.

Part: RAM AIR DOOR — WORN (AC BAY) · airframe 54,288 hrs · 18,910 cycles

LEFT RAM AIR DOOR WORN BEYOND LIMITS IAW AMM 21-53-01. R & R LT RAM AIR DOOR. OPERATIONAL CHECK SATIS IAW AMM 21-53-01.

Part: SENSOR — OUT OF ADJUST (DOOR) · airframe 54,288 hrs · 18,910 cycles

EICAS MSG DISPLAYED LT EMER ADJUSTED LT EMER INDICATION SENSOR IAW AMM 52-71-00. OPERATIONAL CHECK SATISFACTORY.

Part: CONNECTOR — LOOSE (FLAP SYSTEM) · airframe 53,850 hrs · 18,792 cycles

EICAS MESSAGE TE FLAP DISAGREE DISPLAYED. FLAPS 30 SELECTED & FAILED TO POSITION WITH AIR, AIR SPEED LESS THAN 165. CYCLED FLAPS 3 TIMES & INSPECTED SLATS. CHECKED FSGU & DVI OF FLAP PDU XMT FOUND LOOSE CONNECTOR. CLEANED & SECURED CONNECTOR. RECYCLED FLAPS AGAIN, NO DEFECTS NOTED. IAW BSWPM 20-60-06 SECURITY & CONDITION OF TE FLAP PDU DISCONNECT D01806 WERE INSPECTED. NO DEFECTS WERE NOTED WITH PINS OR WIRING IAW BWDM 27-51-11. NO MSG ON FSEU. ACFT VERIFIED ETOPS 180.

Part: WIRE — DAMAGED (CABIN) · airframe 52,677 hrs · 18,465 cycles

FORWARD CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPAIRED WIRE ON L1 DOOR OVERHEAD LIGHT IAW B767 AMM 33-51-00, SWPM 20-30. OPERATIONS CHECKED GOOD, ACFT WAS GNDED.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,283 hrs · 18,353 cycles

PASSENGER COMPARTMENT, LT SIDE POSITION NR 4 EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED LEFT POWER SUPPLY. OPS CHECKED GOOD IAW AMM 33-51-07.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 52,282 hrs · 18,352 cycles

PASSENGER COMPARTMENT, RT SIDE EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHTING BATTERY PACK IAW AMM 33-51-07. OPS CHECKED GOOD IAW AMM 33-51-00.

Part: PROXIMITY SENSOR — INOPERATIVE (GIRT BAR) · airframe 52,180 hrs · 18,320 cycles

L1 DOOR ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOPERATIVE. DURING TROUBLESHOOTING, EMERGENCY DOOR ASSIST BOTTLE WAS USED AND ESCAPE SLIDE FELL OFF L1 DOOR. SLIDE DID NOT DEPLOY. R & R L1 DOOR EMERGENCY POWER ASSIST RESERVOIR BOTTLE IAW AMM 52-11-30. INSPECTED L1 ESCAPE SLIDE ASSY IAW AMM 25-66-01. NO DEFECTS NOTED. REINSTALLED SLIDE ASSY TO L1 DOOR IAW AMM 25-66-01. REINSTALLED SLIDE COVER ASSY IAW AMM 52-11-02. L1 DOOR OPS CHECKED GOOD. R & R THE FWD GIRT BAR PROXIMITY SENSOR IAW AMM 25-66-11. L1 DOOR GIRT BAR ENGAGEMENT LIGHT, OPS CHECKED GOOD.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 52,046 hrs · 18,263 cycles

CAPTAIN'S OXYGEN MASK HARNESS IS LEAKING. R & R CAPTAINS OXYGEN MASK IAW AMM 35-11-51. OPS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (EMERGENCY EQUIP) · airframe 52,043 hrs · 18,262 cycles

DURING DITCHING EXERCISE, FOUND 2 FLASHLIGHTS FROM SURVIVAL KIT INOPERATIVE. R & R SURVIVAL KIT IAW AMM 25-64-00.