N797AX

Part: SMOKE DETECTOR — DEFECTIVE (ZONE 100) · airframe 72,356 hrs · 49,257 cycles

DURING DESCENT THE FWD EQPT SMOKE EICAS MESSAGE AND EQUIPMENT COOLING SMOKE ANNUNCIATOR LIGHT ILLUMINATED. FOLLOWED QRH BOTH LIGHTS STAYED ILLUMINATED. CONTACTED ATC AND DECLARED AN EMERGENCY AND REQUESTED CLEARANCE DIRECT TO KCVG. WE WERE CLEARED DIRECT TO THE AIRPORT AND TO DESCEND TO 4,000. SUBSEQUENTLY REQUESTED TO LAND 36R. 36R ALLOWED US TO PROCEED DIRECTLY TO THE AIRPORT FOR A STRAIGHT IN APPROACH. AFTER ACCOMPLISHING ALL THE CHECKLIST ITEMS IN THE QRH, THE “FORWARD EQPT SMOKE” AND OVERHEAD “SMOKE” LIGHTS REMAINED ILLUMINATED. WE DID NOT HAVE SMOKE IN THE COCKPIT! WE FLEW A VISUAL APPROACH TO RUNWAY 36R. AFTER LANDING, WE TURNED OFF THE RUNWAY AT T6 AND STOPPED. BECAUSE BOTH SMOKE LIGHTS REMAINED ON, WE ELECTED TO POWER DOWN THE AIRCRAFT AND BEGIN EVACUATION. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCE TROUBLE SHOT SYSTEM. DURING T/S FOUND THAT EQUIP SMOKE LIGHT EXTINGUISHED AND MESSAGE CLEARED. FOUND THAT EQUP COOLING TEST SMOKE LIGHT & EICAS MSG. WOULD NOT SHOW. R/R EQUIPMENT SMOKE DETECTOR IAW AMM 21-58-19. SYS GROUND OPS CHECK NORMAL. PER MX CONTROL REQUEST R/R MISC TEST PNL IAW WDM 31-51-41. ALL TESTS OPS NOORMAL. NO DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: OVERHEAT — FALSE INDICATION · airframe 71,709 hrs · 48,982 cycles

AFTER BOTH ENGINE STARTS RECEIVED A FWD EQUIP OVERHEAT. AIRCRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE PERFORMED OPS TEST. EQ. COOLING MANUAL TEST PER AMM 21-58-00 NO EICAS MSG NOTED RAN THE SYSTEM FOR 15 MINUTES. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL PANEL — FAULTED (AUTOPILOT SYS) · airframe 71,287 hrs · 48,801 cycles

LEFT AND RIGHT AUTOPILOTS BECAME INOPERATIVE.CREW ELECTED TO TURN BACK TO CVG. AIRCRAFT LANDED WITHOUT FURTHER INCIDENCE. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE REMOVED AND REPLACED MCP IAW AMM 22-41-01, OPS GOOD, A/C RETURNED TO SERVICE.

Part: NONE — NONE · airframe 71,072 hrs · 48,716 cycles

AFTER FLAP RETRACTION ON TAKEOFF FLIGHT DECK TEMP BEGIN TO RISE UP TO 47'C WE TRIED TO GAIN CONTROL OF TEMP BY GOING TO STANDBY N, DID NOT WORK. ALSO TRIED OPERATING TRIM AIR VALVE IN MANUAL DID NOT WORK. ALSO TRIED TURNING THE TRIM AIR SWITCH OFF, DID NOT WORK. WE ALSO GOT A LEFT PACK TEMP EICAS MSG EVEN THOUGHT LEFT PACK WAS OFF AND DEFERRED. FLIGHT CREW ELECTED TO DIVERT INTO CVG. AIRCRAFT WAS GROUNDED BY MAINTENANCE. MAINTENANCE CONDUCTED OPERATIONAL TEST OF R/H PACK PER AMM 21-51-00. DURING R/H PACK OPERATION, L/H PACK OPERATING UNCOMMANDED. FOUND TRIM AIR SUPPLY CHECK VALVE INSTALLED IN REVERSE FLOW. REINSTALLED NAMED VALVE PER AMM 21-61-05. RESTARTED OPERATIONAL TEST OF R/H PACK PER AMM 21-51-00 OPS TEST NORMAL. SYSTEM TEST OF FLIGHT DECK/ CABIN TEMP CONTROL OK PER AMM 21-61-00. AIRCRAFT RETURNED TO SERVICE FOLLOWING A SUCCESSFUL MAINTENANCE EVALUATION FLIGHT.

Part: SPLICE PLATE — CORRODED (ZONE 500) · corrosion level 2 · airframe 70,825 hrs · 48,637 cycles

DURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), MAINTENANCE REPORTED CORROSION ON THE LEFT WING FIXED LEADING EDGE UPPER SPLICE PLATE(114T0223-19) FWD OF THE FRONT SPAR. CORROSION IS LOCATED AT APPROXIMATELY WS 450. CORROSION WAS REMOVED BY BLENDING AND MINIMUM REMAINING THICKNESS DOCUMENTED IN 0.50” X 0.50” GRID MAPPINGS. THE MINIMUM REMAINING THICKNESS(0.036”, NOMINAL 0.080”) WAS FOUND TO BE OUT OF ALLOWABLE LIMITS PER 767-200 SRM 57-41-01 ALLOWABLE DAMAGE 2. THIS REA PROVIDES PERMANENT REPAIR INSTRUCTIONS FOR THE ABOVE NOTED CONDITION, AS APPROVED BY FVCI 8110-3. REPAIR ACCOMPLISHED PER ABX-REA-5741-64372-00. VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DISCOVERED DURING AN FAA AUDIT OF VENDOR.

Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 70,825 hrs · 48,637 cycles

DURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), CORROSION WAS FOUND ON THE LH WING SKIN PANEL NO. 1(112T4102-1) AT THE REAR SPAR AND WS 440-450. THE CORROSION IS LOCATED ON THE UPPER SURFACE OF THE BOTTOM SKIN AND TRAVELS BETWEEN THE SKIN AND REAR SPAR, AND CLOSE TO THE AFT PITCH LOAD FITTING AND STRUT HYDRAULIC ATTACH BRACKETS. SEE FIGURE 1. BOEING WAS CONTACTED VIA SERVICE REQUEST #4-5408970356. THIS REA PROVIDES REPAIR INSTRUCTIONS FOR THE SUBJECT DAMAGE. REPAIRED LOWER WING SKIN IAW ABX-REA-5720-64374-00.

Part: NONE — CORRODED (ZONE 100) · airframe 70,825 hrs · 48,637 cycles

DURING AIRCRAFT CURRENT CHECK AT AIRBORNE (TAMPA), CORROSION WAS FOUND ON THE FORWARD CARGO DOOR LOWER SILL OUTER CHORD(143T8004-1). THE NOMINAL THICKNESS OF THE CHORD IN THE SUBJECT AREA IS 0.300 INCH. THE MINIMUM REMAINING THICKNESS IN THE AREA IS 0.226 INCH. CORROSION WAS REMOVED BY BLENDING PER 767-200 SRM 51-10-02 AND THE LOSS OF MATERIAL WAS FOUND TO BE OUT OF ALLOWABLE LIMITS PER 767-200 SRM 53-00-15. THIS REA PROVIDES PERMANENT REPAIR INSTRUCTIONS FOR THE NOTED CONDITION AS APPROVED BY FVCI 8110-3. REMOVED FASTENERS, REMOVED CORROSION, PERFORMED NDT THICKNESS EVAL FOUND IN LIMITS IAW ABX REA- 5330-64373-00, HFEC OPEN HOLE INSPECTION, FLAT PEENED AREA, ALODINED, PRIMED AND TOP COATED AREA IAW B767-200 SRM 51-20-01, 51-20-06, 51-20-00, 51-20-00, 51-40-02, AMM 51-21-00, SOPM 20-10-03 ABX-REA- 5330-64373-00, AND NTM PART 4+6 51-00-19

Part: VALVE — INTERMITTENT · airframe 70,379 hrs · 48,435 cycles

ANTISKID OFF EICAS MSG. AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. REPLACED PARKING BRAKE VALVE IAW AMM 32-44-04. PERFORMED OPS CHECK OF PARKING BRAKE SYSTEM IAW B767 AMM 32-44-00-730-801. ALL TEST PASS. NO LEAKS NOTED. AIRCRAFT RELEASED FOR FLIGHT .

Part: MECHANISM — DAMAGED (AILERONS) · airframe 70,312 hrs · 48,402 cycles

AILERON CONTROL CHECK AND CONTROL YOKE WILL NOT SPRING RETURN TO CENTER, AICRAFT BACK TO BLOCK AND GROUNDED BY MAINTENANCE. MAINTENANCE FOUND LEFT LATERAL CONTROL FEEL, CENTERING AND TRIM MECHANISM DAMAGED.REMOVED AND REPLACED IAW AMM 27-22-08. RII-27-03 COMPLIED WITH INSPECTION. SYSTEM OPS CHECKS NORMAL. AIRCRAFT RELEASEED FOR FLIGHT.

Part: SHUTOFF VALVE — INTERMITTENT (TRIM AIR) · airframe 68,785 hrs · 47,771 cycles

HOLDING NR 1, SUDDENLY GOT WARM IN COCKPIT. WINDOWS FOGGED, THEN EICAS COMPACTED. BOTH PILOT EADI/EHSI WENT FULL BRIGHT. THEN F/O'S EADI BLANKED. AIRCRAFT BACK TO BLOCK AND GROUNDED. CONDUCTED EQUIPMENT COOLING SYSTEM BIT, IAW B767 FIM 21-58 FT 873, NO FAULTS FOUND. CONDUCTED ZONE TEMP CONTROLLER BIT, IAW FIM 21-61 FT 872, NO FAULTS FOUND. REPLACED MANIFOLD INTERCONNECT VALVE, IAW AMM 21-58-01, OPERATIONS CHECK OK. CONDUCTED ENGINE RUN, IAW ABX ERU AND TAXI CHECKLIST, CPT AND F/O EADI AND HSI BLANKED, EICAS BLANKED. CONDUCTED PACK TEMP CONTROLLER BIT, IAW FIM 21-51 FT 803, NO FAULTS FOUND. INSPECTED RIGHT AND LEFT PACKS, FOUND TRIM AIR SHUT-OFF VALVE IN CLOSED POSITION AT ALL TIMES. REPLACED TRIM AIR SHUTOFF VALVE, IAW AMM 21-61-06, OPERATIONS CHECK OK. SEE LP 38047-11/3 FOR ENGINE RUN. UPON REPLACEMENT OF TRIM AIR SHUTOFF VALVE, REF L/P 35047-11/1. CONDUCTED ENGINE IDLE RUN W/PACKS FOR T/S, IAW ABX ERU AND TAXI CHECKLIST. CONDITIONS IN DISCREPANCY DID NOT RE-OCCUR AFTER 25 MINUTE ILDE RUN, COOLING SYSTEM OK.

Part: PUMP — FAILED (LT ENGINE) · airframe 68,307 hrs · 47,545 cycles

LEFT ENGINE HAD NO FUEL FLOW ON START. AIRCRAFT WAS GROUNDED.

Part: PANEL — CORRODED (LT WING) · airframe 67,509 hrs · 47,178 cycles

LH WING FUEKL TANK PANEL 533AB CORRODED. AIRCRAFT WAS GROUNDED.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 67,509 hrs · 47,178 cycles

LH WW AR STA 1021 ATTACH ANGLE CORRODED. AIRCRAFT WAS GROUNDED.

Part: ANGLE — CORRODED (LT MLG WW) · airframe 67,509 hrs · 47,178 cycles

LH MLG WW HAS LIGHT CORROSION AT STA 1021 JUST AFT OF CENTER SYSTEM HYD RETURN CONNECTION. AIRCRAFT WA GROUNDED.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 67,509 hrs · 47,178 cycles

BOTH HOLES ON AFT STRINGER SPLICES AT STA 676 S25L ARE CRACKED. AIRCRAFT WAS GROUNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 67,509 hrs · 47,178 cycles

LH WW KEEL BEAM WEB AREA AT APPROX. STA 1049 HAS CORROSION. AIRCRAFT WAS GROUNDED.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 67,509 hrs · 47,178 cycles

LH WW ATTACH ANGLE IB OF DOOR ACTUATOR HAS AREA OF CORROSION. AIRCRAFT WAS GROUNDED.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 67,509 hrs · 47,178 cycles

LH WW ATTACH ANGLE IB OF DOOR ACTUATOR HAS AREA OF CORROSION. AIRCRAFT WAS GROUNDED.

Part: LIGHT — UNKNOWN (CABIN) · airframe 67,231 hrs · 47,037 cycles

THE RIGHT FORWARD DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED) AND THE EMERGENCY LIGHTS WERE TROUBLESHOT IN ACCORDANCE WITH THE 767 FIM 33-51, FAULT TREE 803. THE M735 EMERGENCY LIGHTS POWER SUPPLY AND THE M736 EMERGENCY LIGHTS POWER SUPPLY WERE SWAPPED, THE M735 EMERGENCY LIGHTS POWER SUPPLY AND THE M734 EMERGENCY LIGHTS POWER SUPPLY WERE SWAPPED, M736 EMERGENCY LIGHTS POWER SUPPLY AND THE M737 EMERGENCY LIGHTS POWER SUPPLY WERE SWAPPED, THE M735 AND M736 BATTERIES WERE SWAPPED, AND ELECTRICAL CONNECTOR D9080P AND ELECTRICAL CONNECTOR D9084 WERE SWAPPED. REFERENCE THE ABX 797AX WIRING DIAGRAM MANUAL. THE CAUSE OF THE INOPERATIVE RIGHT FORWARD DOOR EMERGENCY LIGHT IS UNKNOWN.

Part: SPLICE — CORRODED (BS 1019) · airframe 65,912 hrs · 46,413 cycles

CORROSION IN THE TENSION BOLT HOLE OF SPLICE FITTING AT BODY STATION 1809.5, WATER LINE 214.76. THE SPLICE FITTING WAS REPLACED. THE AIRPLANE WAS GROUNDED.

Part: RING — CORRODED (BS 1582) · airframe 65,912 hrs · 46,413 cycles

CORROSION IN THE SECTION 48 PRESSURE RING (BODY STATION 1582) AT THREE BOLT LOCATIONS: S27R (UPPER/OUTBOARD), S33R (UPPER/OUTBOARD), AND S36L (LOWER/INBOARD). THE PRESSURE RING WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — CORRODED (HORIZTONTAL STAB) · airframe 65,912 hrs · 46,413 cycles

CORROSION ON THE UPPER RIGHT HORIZONTAL STABILIZER SKIN PANEL AT RIB STATION 12 AND STRINGER 3. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — DENTED (FUSELAGE) · airframe 65,527 hrs · 46,200 cycles

TWO DENTS ON THE FUSELAGE SKIN AT STATION 632. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: SKIN — DENTED (BS 632) · airframe 65,444 hrs · 46,166 cycles

THE FUSELAGE SKIN ADJACENT TO BS 632 FRAME, BETWEEN STRINGERS 24L AND 25L WAS DENTED. THE SKIN WAS REPAIRED. THE AIRPLANE WAS GROUNDED.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE LEFT WING LOWER TRAILING EDGE PANEL LOWER SURFACE BETWEEN WING STATIONS 903 AND 909. THE PANEL WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE RIGHT WING INBOARD SPOILER BEAM UPPER CHORD BETWEEN WS 282 AND 432. THE CHORD WAS REPLACED. THE ACFT WAS GROUNDED.

Part: SUPPORT BEAM — CORRODED (BS 1413) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE BULK CARGO BAY LOWER NET SUPPORT BEAM AT BS 1413. THE SUPPORT BEAM WAS REPLACED. THE ACFT WAS GROUNDED.

Part: SPLICE PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE RIGHT WING OUTBOARD FRONT SPAR LOWER PANEL ATTACH STRUCTURE (SPLICE PLATE) AT OUTBOARD FRONT SPAR STATION 925. THE SPLICE PLATE WAS REPAIRED. ACFT WAS GROUNDED.

Part: SPLICE PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE RIGHT WING INBOARD RIGHT MAIN LANDING GEAR SPLICE PLATE AT WS 255. THE SPLICE PLATE WAS REPLACED. AIRPLANE WAS GROUNDED.

Part: TEE FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE RIGHT WING TEE FITTING AT WS 255. THE TEE FITTING WAS REPLACED. THE ACFT WAS GROUNDED.

Part: STRINGER — CORRODED (BS 748) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON STRINGER 34L AT BS 748. THE STRINGER WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE LEFT WING NOSE BEAM BETWEEN OUTBOARD SPAR OSS 783 AND 791 AND BETWEEN OUTBOARD SPAR OSS 884 AND 909. THE NOSE BEAM SECTIONS WERE REPLACED. AIRPLANE WAS GROUNDED.

Part: BULKHEAD WEB — CORRODED (BS 955) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE MAIN LANDING GEAR WHEEL WELL PRESSURE BULKHEAD WEB AT BS 955. THE BULHEAD WEB WAS REPAIRED. ACFT WAS GROUNDED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE RIGHT WING UPPER SKIN LOWER SURFACE AT WING STATION 470. THE SKIN WAS REPAIRED. THE ACFT WAS GROUNDED.

Part: SKIN — CORRODED (BS 756) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE FUSELAGE SKIN AT BS 756 BETWEEN STRINGERS 34R AND 35R. THE SKIN WAS REPAIRED. AIRPLANE WAS GROUNDED.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE RIGHT WING AFT SPAR UPPER ANGLE AT WS 470. THE ANGLE WAS REPAIRED. THE ACFT WAS GROUNDED.

Part: SUPPORT — CORRODED (BS 1417) · corrosion level 2 · airframe 65,158 hrs · 46,037 cycles

CORROSION ON THE SUPPORT AT BS 1417. THE SUPPORT WAS REPLACED. THE ACFT WAS GROUNDED.

Part: CARABINER — MISSING (ESCAPE REEL) · airframe 64,560 hrs · 45,729 cycles

ONE EMERGENCY DESCENT SAFETY HARNESS CARABINER WAS MISSING FROM ITS STOWAGE POUCH. WHILE THE AIRPLANE WAS REMOVED FROM SERVICE (GROUNDED), A NEW SAFETY HARNESS CARABINER WAS INSTALLED INTO THE STOWAGE POUCH. THE CAUSE OF THE MISSING CARABINER IS UNKNOWN.

Part: FAILSAFE — CRACKED (FUSELAGE) · airframe 62,648 hrs · 44,829 cycles

COMPLIED WITH TC S53-050·04-2. RT WHEEL WELL STA 955, RT FAIL-SAFE HAS HFEC DEFECT INDICATION AT LOWER HOLE COMMON TO FAIL-SAFE AND TEE FITTING. REF: SB 767-53A0100, FIG 2, SH 1. COMPLIED WITH FAIL SAFE TRIM OUT AT TC EA 53500014-003 AND DOCUMENT 47008 AND 04. CRACKED 1.8", PN: 145T2524, FAIL SAFE, FS/BS LOCATION: STA 955, STR/WS LOCATION, STR 22R. ACFT WAS GROUNDED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,648 hrs · 44,829 cycles

REMOVED CORROSION IAW SRM 57-51-02, FIG 101. INITIAL THICKNESS .094, REMAINING THICKNESS .061. BLENDED AREAS REQUIRED REPAIR AND WERE REPAIRED ON REA B657-62130. CORRODED LEVEL 2, PN 113T1621-58, SKIN, FS/BS LOCATION: FROM R/W T/E TO UPPER STR, WS LOCATION: RBL 97.42. ACFT WAS GROUNDED.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 62,648 hrs · 44,829 cycles

FOUND SKIN CORROSION COMMON TO THE TRIMMED OUT SECTION OF THE FAIL SAFE. CORROSION IS ISOLATED TO THE LOWER HOLE. COMPLIED WITH TASK CARD EA 53500014-004 AND DOCUMENT 470080RD10 CORROSION WAS REMOVED, WITHIN THE ALLOWABLE LIMITS. CORRODED, LEVEL 2, PN 145T3420, SKIN, FS/BS LOCATION: STA 955, STR/WS LOCATION: STR 22R. ACFT WAS GROUNDED.

Part: UNKNOWN — ODOR · airframe 62,648 hrs · 44,829 cycles

BOTH CREW MEMBERS SMELLED A STRONG ELECTRICAL ODOR. THE MAIN EQUIPMENT CENTER WAS INSPECTED. THERE WAS NO EVIDENCE OF BURNED WIRES OR EQUIPMENT. THE CAUSE OF THE ODOR WAS NOT FOUND.

Part: BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 61,866 hrs · 44,456 cycles

WING TE UPPER PANEL ATTACH BEAM RUNNING LENGTH WAYS, CORRODED ON FWD SIDE AT WS .273, INBD OF NR 6 SPOILER, AS SEEN THRU PANEL 551VB OPENING. REMOVED ATTACH BEAMS & INSTALLED SERVICEABLE ATTACH BEAMS, PN 113T1633-157 IAW SRM 51-40-02. CORRODED LEVEL 2, PN 113T1632-207 & 113T1635-157, PART NAME ATTACH BEAMS. ACFT WAS GNDED.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,866 hrs · 44,456 cycles

UPPER WING TE PANEL, ATTACH CHORD AT WING TO FUSELAGE JUNCTION, ABOVE UPLOCK CYLINDER, CORRODED AROUND NUTPLATES. REMOVED ATTACH CHORD & INSTALLED SERVICEABLE ATTACH CHORD, PN 113T1621-55 IAW SRM 51-40-2. CORRODED LEVEL 2, PN 113T1621-55, PART NAME ATTACH CORD. ACFT WAS GNDED.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,866 hrs · 44,456 cycles

STATION 859.5, RBL 89 INNER CHORD CRACKED .450" APPROX AT TRANSITION RADIUS, IAW ES02568 FIG 1 SH 2 ATTACHED TO NEA 53000045-001 FOR CRACK LOCATION. REPAIRED INNER CHAP AT STRINGER 859.5, RBL 89. IAW EA 53000048-101 & REA B653-61905-513. CORROSION LEVEL 2, PN 145T1380-4, PART NAME CHORD, SN NSN, LOCATION STATION 859.5, RBL 89. ACFT WAS GNDED.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 61,866 hrs · 44,456 cycles

UPPER CHORD CORRODED ON REAR SPAR TO WING TE BEAM, AT STATION 285, AT AFT END AS SEEN UNDER INBD END OF NR 6 SPOILER. REMOVED TE BEAM ASSEMBLY, R & R UPPER CHORD, PN 113T1623-141, WITH SERVICEABLE CHORD, INSTALLED TE BEAM ASSEMBLY IAW SRM 51-40-2. CORRODED LEVEL 2, PN 113T1623-141, PART NAME UPPER CHORD, EXACT FS & BS LOCATION ON ACFT & EXACT STRINGER & WS LOCATION ON ACFT, WS 285 - 285. ACFT WAS GNDED.

Part: BEAM — CORRODED (LT SPOILER) · corrosion level 2 · airframe 61,866 hrs · 44,456 cycles

WING TE AFT LOWER CHORD FOR PANEL 552HB AT TE WS 418 SPLIT ON EDGE. R & R CHORD AT STATION 418 IAW SRM 51-40-02. FABRICATED CHORD, PN 133T1407-1, IAW REA B657-61929MR. CORRODED LEVEL 2, PN 113T1407-1, SN NSN, PART NAME, SPOILER BEAM CHORD LOWER, EXACT FS & BS LOCATION ON ACFT FROM WBL 275, EXACT STATION & WS LOCATION ON ACFT, FROM 418. ACFT WAS GNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,866 hrs · 44,456 cycles

AFT BULK CARGO COMPARTMENT, BILGE AREA, STATION 1562, CORROSION. R & R REQUIRED PARTS & HARDWARE IAW SRM 51-40-02 PARA 4 & PARA 9. CORRODED LEVEL 2, PN 146T1223-23, PART NAME SHEAR TIE, EXACT FS & BS LOCATION ON ACFT 1562. EXACT STRINGER & WS LOCATION ON ACFT, STRINGER 38R - 38L. ACFT WAS GNDED.

Part: BULKHEAD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,866 hrs · 44,456 cycles

FORWARD SIDE OF APB, BETWEEN RS 18 & 21, OS TS1 HAS SEVERAL AREAS OF CORROSION. REPAIRED APB IAW SRM 53-80-08 REPAIR 2 DETAIL II FIG 201. CORRODED LEVEL 2, PN PO-06072803, PART NAME APB DOUBLER, FS & BS LOCATION RS 18 - 21, STRINGER & WS N/A TO N/A. ACFT WAS GNDED.

Part: SPLICE PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 61,866 hrs · 44,456 cycles

RIGHT WING CORRODED, BETWEEN NUTPLATE CHANNEL & WING LOWER SURFACE AT LE STATION 1070, FWD OF FRONT SPAR. R & R DAMAGED AREA IAW REA B657-61897 REV IR 01-06-2016. CORRODED LEVEL 2, PN 114T0222, SN N/A, PART NAME, LOWER SPLICE PLATE, EXACT FS & BS LOCATION ON ACFT FROM NA/ TO N/A, EXACT STRINGER & WS LOCATION ON ACFT FROM 1069 - 1139. ACFT WAS GNDED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,866 hrs · 44,456 cycles

CORRODED T CAP STATION 246, UNDER FWD LAVATORY AREA. REMOVED & FABRICATED NEW FLOORBEAM USING PO 0077887 7075-T6 .050, EXTRUSION IAW SRM 53-10-51 FIG 201. CORRODED, PN 141T5814-78, PART NAME CHORD, SN NSN, EXACT FS & BS LOCATION ON ACFT, FROM STATION 246, LBL 63 - LBL 81. ACFT WAS GNDED.

Part: FRAME — CORRODED (SLAT TRACK) · corrosion level 2 · airframe 61,866 hrs · 44,456 cycles

NUMBER 1 SLAT INBD IDLER TRACK, OTBD FRAME, CORROSION. REMOVED EXISTING FRAME, PN 114T2227-15 & INSTALLED SERVICEABLE FRAME IAW SRM 51-40-2. SDR INFO, CORRODED LEVEL 2, PN 114T2277-15, PART NAME: FRAME RIB STRUT, STRINGER & WS LOCATION. OSS1029 - OSS1029. ACFT WAS GNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,866 hrs · 44,456 cycles

CORRODED SHEAR TIE, AT STATION 1329, RBL 93. REMOVED SHEAR TIE, REPLACED WITH SERVICEABLE SHEAR TIE, PN 368-53-16 -94465-209 IAW SRM 51-40-2. CORRODED LEVEL 2, PN 368-53-16-94465-209, PART NAME CLIP, CARGO HEADING, EXACT FS & BS LOCATION ON ACFT, FROM STATION 1329 TO RBL 97. EXACT STRINGER & WS LOCATION. ACFT WAS GNDED.

Part: HYDRAULIC LINE — SPLIT (NLG) · airframe 61,514 hrs · 44,274 cycles

CENTER HYD SYS QTY DECREASED TO ZERO & SYS PRESS & QTY LIGHTS ILLUMINATED. EICAS MSG, C HYD SYS PRESS & C HYD QTY DISPLAYED. THE CAUSE OF THE DROP IN HYD PRESS & QTY WAS A SPLIT & LEAKING HYD HOSE CONNECTED TO THE NOSE GEAR RETRACT ACTUATOR. THE HYD HOSE WAS REPLACED IAW AMM 20-11-00 & 32-34-01.

Part: DETECTOR — OUT OF TRIM (LOW FLOW) · airframe 58,743 hrs · 42,915 cycles

EICAS MESSAGE FWD EQUIP OVERHEAT DISPLAYED & OVERHEAT LIGHT ILLUMINATED. LIGHT EXTINGUISHED AFTER SELECTOR WAS POSITIONED TO STAND-BY, ELEC OR BURNING ODOR. COMPLIED WITH FIM, NO FAULTS FOUND. TESTED EQUIP COOLING SWITCH ON P61 PANEL & OBSERVED AN OVERHEAT LIGHT BUT NO SMOKE LIGHT OR ASSOCIATED EICAS MESSAGES. REPLACED EQUIP COOLING SMOKE DETECTOR. OPS TESTED NORMAL. PRESSURIZED ACFT IN AIR MODE. NO OVERHEAT OR SMOKE LIGHTS OR ASSOCIATED EICAS MESSAGE. REPLACED FWD EQUIP LOW FLOW DETECTOR. SYS OPERATIONS CHECKED NORMAL. FWD EQUIP LOW FLOW DETECTOR WAS OUT OF TRIM.

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

LEFT WING LE AT STATION 486 LOWER PANEL SUPPORT CORRODED UNDER NUTPLATES. REPLACED AIR LOAD STRUT & INSTALLED SLAT STOP IAW SRM 51-40-02 PN 114T2203-15AX. SDR INFO CORRODED, PN 114T2203-15AX, PART NAME AIR LOAD STRUT, SN N/A, FS & BS LOCATION 486 TO 486. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

STATION 1329 ABOVE STRINGER 33R, FLOORBEAM UPPER FLANGE CORRODED IN THE CORNER. REMOVED CORRODED INTERCOSTAL AT BS 1329 ABOVE STRINGER 33 RT, LOCATED & DRILLED FABRICATED IAW REA B653-60989 & INSTALLED INTERCOSTAL IAW B653- 60989 & SRM B767 51-40-02-0G, SB-106 5/1/14. SDR INFO CORRODED, PN 146T5000-38, PART NAME SUPPORT, SN NSN, FS & BS LOCATION 1329 - 1351, STRINGER & WS LOCATION STRINGER 35R. ACFT WAS GNDED.

Part: RIB — CORRODED (LT WING) · airframe 58,736 hrs · 42,909 cycles

LEFT WING LWR LE UPPER RIB AT STATION 486 FWD END CORRODED NEAR NR 5 SLAT OTBD AUXILIARY TRACK. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM 57-40-09. REPLACED RIB IAW REA B657-60930. PN 114T2204-15, SDR INFO CORRODED, PN 114T2204-15, PART NAME LE UPPER RIB, SN N/A, FS & BS LOCATION 486 TO 486. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

LEFT WING LWR AIR LOAD STRUT CORRODED NEAR NR 5 SLAT OTBD AUXILIARY TRACK. REPLACED AIR LOAD STRUT IAW REA B657-06930 PN 114T2203-13AX. SDR INFO CORRODED, PN 114T2203-13AX, PART NAME AIR LOAD STRUT, SN N/A, FS & BS LOCATION 490 TO 490. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,736 hrs · 42,909 cycles

FLC FUSELAGE STATION 676, STRINGER 24L LOWER FWD LOCK FASTENER IN SPLICE ON BACKSIDE HAS A CRACK RUNNING FROM IT THEN AFT. R & R DAMAGED STRINGER SECTION AT FS 670 TO 710 STRINGER 24L IAW B653-60933-MR REV IR DATED 04-01-2014. SDR INFO CRACKED 3 INCHES, PN 143T3001-32, PART NAME STRINGER, SN NSN, FS & BS LOC 676, STR & WS LOC STRINGER 24L. ACFT WAS GNDED.

Part: BEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

RIGHT OVER WING EXIT DOOR CUT OUT HAS SEVERAL SPOTS OF CORROSION. REMOVED CORROSION IAW SRM 53-00-01. REPAIRED IAW B653-60946-MA & LEAK CHECKED SATISFACTORY IAW AMM 05-51-24-2.

Part: ATTACH FITTING — CORRODED (RT WING) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

REAR SPAR TO WING TE PANEL ATTACH LOWER CHORD AT WS 1068 SPLIT ON EDGE. R & R TE LOWER CHORD AT WS 1068 IAW SRM 51-40-02.

Part: TEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

AFT LOWER CARGO STATION 1351 DOUBLER CORRODED BETWEEN STRINGERS 30L & 31L. R & R CORRODED TEAR STRAPS, DOUBLERS, IAW B653- 60974. SDR INFO PN 146T3232-2, NSN, CORRODED L2, PART NAME TEAR STRAP, FS LOC 1351, STRINGER LOC STRINGER 30L TO STRINGER 31L. ACFT WAS GNDED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

AFT LOWER CARGO STATION 1350 FRAME CORRODED BETWEEN STRINGERS 29L TO 31L. R & R ALC STATION 1350 FRAME BETWEEN STRINGER 29L & 33L IAW SRM 51-40-02 & B653-60974-MR. SDR INFO CORRODED LEVEL 2, PN 146T1213-15, SN NSN, PART NAME FRAME, EXACT FS & BS LOC ON ACFT FS 1351, EXACT STR & WS LOC ON ACFT STRINGER 25L TO STRINGER 33L. ACFT WAS GNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

STATION 1351 SHEAR TIE CORRODED BETWEEN STRINGER 30L & 31L. R & R SHEAR TIE AT STATION 1351 BETWEEN STRINGER 30L & 31L IAW SRM51-40-02 & B653-60974-MR. SDR INFO CORRODED LEVEL 2, PN 140T2103-757, SN NSN, PART NAME SHEAR TIE, CORRODED, EXACT FS & BS LOC ON ACFT FS 1351 TO FS 1351, EXACT STR & WS LOC ON ACFT STRINGER 30L TO STRINGER 31L. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

STATION 676 STRINGER 3L CRACKED 2 INCHES LONG. R & R CRACKED STRINGER 3L AT STATION 676 B653-60933- MR. SDR INFO CRACKED 2 INCHES, PN 143T3001-4, NSN, PART STRINGER, FS & BS LOC 676, STR & WS LOC STRINGER 3L. ACFT WAS GNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

AFT LOWER CARGO STATION 1351 SHEAR TIE CORRODED BETWEEN STRINGERS 33L & 34L. R & R REPAIRED SHEAR TIE AT ALC STATION 1351 BETWEEN STRINGER 33L & STRINGER 34L IAW SRM 51-40-02 & REA B653-60924-MR. SDR INFO CORRODED LEVEL 2, PN 140T2102U603, SN NSN, PART NAME SHEAR TIE, EXACT FS & BS LOC ON ACFT FS 1351 TO FS 1351, EXACT STR & WS LOC ON ACFT STRINGER 33L TO STRINGER 34L. ACFT WAS GNDED.

Part: TEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

STATION 1373 AT STRINGER 32L HAS A 2 - 3 INCH SECTION OF CORROSION. R & R TEAR STRAP IAW SRM 51-40-02 & REA B653-60974-MR. SDR INFO CORRODED LEVEL 2, PN 146T3232-3, NSN, CORRODED, NAME TEAR STRAP, LOCATION FS 1373, STRINGER 32L. ACFT WAS GNDED.

Part: WEB — CRACKED (FUSELAGE) · airframe 58,736 hrs · 42,909 cycles

FLC FUSELAGE STATION 470, BL0 UNDER DOUBLE WING LOCK SCREW HAS PUNCTURED THE SKIN OF U CHANNEL, DIRECTLY ABOVE EQUIPMENT COOLING OUTLET MOTOR. UPON INSPECTION PUNCTURE FOUND HAD CRACKS. R & R WEB IAW SRM 51-40-02. REINSTALLED WING LOCK SUPPORT IAW SRM 51-40-02. REINSTALLED CTR & AUX WING LOCKS IAW AMM 25-53-14-4. SDR INFO CRACKED 1/4 INCH, PN 452T2055Y4, PART NAME WEB, SN NSN, FS & BS LOCATION 470 TO 470, STRINGER & WS LOCATION LBL 10 TO RBL 20. ACFT WAS GNDED.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 58,736 hrs · 42,909 cycles

STATION 1043 FLOOR ATTACHMENT BRACKET BROKEN. R & R FLOOR ATTACHMENT BRACKET AT STATION 1043 UNDER FLOOR PANEL 241S IAW SRM 51-40-02. SDR INFO CRACKED 2 INCHES PN 368-53-95453-215AX, PART NAME ATTACH BRACKET, SN NSN, LBL 55, STA. 1043. ACFT WAS GNDED.

Part: STRUT — CORRODED (LE SLAT) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

LEFT WING LOWER LE AIR LOAD STRUT CORRODED AT WS 436 NEAR NR 5 SLAT INBD AUXILIARY TRACK. REPLACED AIR LOAD STRUT PN 114T2200-21AX IAW SRM 51-40-0. REFERENCE NR 1618 FOR PROX CLEARANCE & OPERATIONS CHECKS.

Part: SUPPORT ANGLE — CORRODED (LT WING) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

LEFT WING TE PANEL SUPPORT T ANGLE CORRODED UNDER NOSE PLATE AT PANEL 561QB. REMOVED CHORD & INSTALLED NEW CHORD PN 113T1683U43 IAW SRM CH 51-40-2. SDR INFO CORRODED LEVEL 2, PN 113T1683U43, PART NAME CHORD ASSEMBLY, SN NSN, EXACT STRINGER & WS LOCATION ON ACFT FROM WS 1105. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

STATION 676 CRACKED STRINGER 2L 3 INCHES LONG. R & R CRACKED STRINGER 2L AT STATION 676 IAW REA B653-60933-MR. SDR INFO CRACKED 3 INCHES, PN 143T3001-2, NSN, PART STRINGER, FS & BS LOC 676, STR & WS LOC STRINGER 2L. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,736 hrs · 42,909 cycles

STATION 676 STRINGER 7L CRACKED 4 INCHES LONG. R & R CRACKED STRINGER 7L AT STATION 676 IAW NR B653- 60933-MR. SDR INFO CRACKED 4 INCHES, PN 143T3001-6, NSN, PART STRINGER, FS & BS LOC 676, STRINGER & WS LOC STRINGER 7L. ACFT WAS GNDED.

Part: SUPPORT FITTING — DAMAGED (RT WING) · airframe 58,736 hrs · 42,909 cycles

NR 7 FLAP FITTING REAR SPAR NR 3 HOLE AFT FITTING IS ELONGATED. REMOVED NR 7 FLAP SUPPORT FITTING, ROUTED TO MACHINE SHOP TO DETERMINE TRUE & ROUND HOLE SIZE. INFO PROVIDED TO ENGINEERING. ENGINEERING PROVIDED REA B657-60978-MR. NR 3 HOLE REPAIRED IAW REA B657-60978-MR. SDR INFO ELONGATED, PN 113T1324-4, PART NAME FLAP SUPPORT RIB, SN WS 608 TO WS 618. ACFT WAS GNDED.

Part: ANGLE — CRACKED (NR 1 COWLING) · airframe 58,736 hrs · 42,909 cycles

NR 1 ENG OTBD CORE COWL 3RD FRAME AFT T ANGLE CRACKED. REPLACED ANGLE IAW DWG 314T1210. SDR INFO CRACKED 1INCH, PN 314T1210, PART NAME INTERCOSTAL, ANGLE, SN NSN, FS & BS LOCATION NR 1 CORE COWL NAC 200 TO NAC 200, STRINGER WS LOCATION BL0. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,736 hrs · 42,909 cycles

STATION 676 STRINGER 10L CRACKED. REPAIRED STRINGER 10L STATION 676 IAW SRM 53-00-03 & REA - B653-60933-MR. SDR. CRACKED 1.0 INCHES , PN 143T3001-7, PART NAME STRINGER, NSN, FS & BS LOC FROM 676 TO 706, STRINGER & WS LOC STRINGER STRINGER 10L. ACFT WAS GNDED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

FLC FUSELAGE STATION 614, RBL 16 STRUCTURE CORRODED UNDER BILGE SUPPORT CHANNEL. REPLACED INTERCOSTAL AT STATION 614, LBL 16 IAW DWG 143T5000 SRM 53-00-04. SDR INFO CORRODED LEVEL 2, PN 143T5000, PART NAME INTERCOSTAL, SN NSN, FS & BS LOCATION 614 TO 624, STRINGER & WS LOCATION RBL 16 TO RBL 16. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,736 hrs · 42,909 cycles

STATION 676 STRINGER 12L CRACKED 1 INCH LONG. COMPLIED WITH REA B653-60933-MR ITEM`S 24, 25, 26 & 27. TO REPAIR STRINGER 12L AT STATION 676. CRACKED 1 INCH, PN 368-53-00-95387, PART NAME SN NSN, EXACT FS & BS LOC ON ACFT 676 TO 680, EXACT STR & WS LOC ON ACFT STRINGER 12L TO STRINGER 12L. ACFT WAS GNDED.

Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

CORROSION ON KEEL BEAM AT STATION 976 LBL 11. REMOVED CORROSION ON KEEL BEAM STATION 976 LBL 11 SRM 51-10-02 & REPAIRED IAW B653-60971-MR. SDR INFO CORRODED LEVEL 2, PN 145T8611-5, PART NAME KEEL BEAM, SN NSN, FS 974 TO FS 980. ACFT WAS GNDED.

Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

LEFT WING INBD UPPER TE FIXED PANEL CORRODED ON UNDERSIDE SUPPORT BEAM OTBD EDGE. R & R UPPER TE FIXED PANEL & T CAP ALODINE & PRIMED IAW SRM 51-20-01 & SRM FOR FASTENERS 51-40-02 SEAMED SEAL PANEL IAW SRM 51-20-05. SDR INFO CORRODED LEVEL 2, PN 113T16323-157, PART NAME UPPER CHORD, PANEL, SN NSN, WS LOC LT WING WS 281.615. ACFT WAS GNDED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

UPPER CARGO FLOOR PANEL SUPPORTS UNDER PANEL 251T HAS CORROSION AROUND NUMEROUS CLIP NUTS. R & R UPPER CARGO FLOOR PANELS SUPPORT SEAT TRACK PN 368-53-16-94344-201 UNDER PANEL 251T IAW SRM 51-40-02. SDR INFO CORRODED LEVEL 2, PN 368-53-16-94344-201, PART NAME SEAT TRACK, SN NSN, STATION 1405.45 TO 1502.0, LBL 77.50. ACFT WAS GNDED.

Part: STRUCTURE — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

LEFT HORIZONTAL STAB TIP LOWER FLANGE IS CORRODED, FORWARD END. BLENDED CORROSION IAW AMM 51-00-03. BLENDED AREA OUT OF LIMITS IAW SRM 55-10-09. REPLACED LWR CHORD IAW DWG 182T5800, PN 182T5800-41. SDR INFO CORRODED LEVEL 2, PN 182T5800-41, PART NAME CHORD, SN NSN, STRINGER & WS LOC HSBL 357.442 LE TO HSBL 357.442 LE ACFT WAS GNDED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

BILGE WEB PANEL SUPPORT INTERCOSTAL AT FS 1285 RBL 24 IS CORRODED. REMOVED CORRODED SUPPORT INTERCOSTAL AT FS 1285, RBL 24 & INSTALLED NEW SUPPORT IAW SRM 51-40-02. SDR INFO CORRODED LEVEL 2, PN 146T5000-8, PART NAME WEB, SN NSN, FS & BS LOCATION 1267 TO 1285 RBL 24. ACFT WAS GNDED.

Part: BEAR STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

FORWARD LOWER CARGO DOOR BEARSTRAP INSIDE HANDLING & LOADER CONTROL PANEL CUT OUT ARE CORRODED AT UPPER & LOWER LATCH LOCATIONS EXTENDING AROUND TO THE AFT LOWER CORNER. CUT OUT DAMAGED LOWER CARGO DOOR BEARSTRAP INSIDE HANDLING & LOADER CONTROL PANEL IAW 60945, FABRICATED ON REPAIR PARTS IAW 60945 & INSTALLED ALL REPAIR PARTS IAW 60945 SB 106 4-17-14. SDR INFO CORRODED LEVEL 2, PN 143T8521-1, PART NAME BEARS TRAP, SN NSN, FS & BS LOC 520 TO 539, STRINGER & WS LOC STRINGER 23R TO STRINGER 25R. ACFT WAS GNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,736 hrs · 42,909 cycles

STATION 676 STRINGER 13LT CRACKED 4 INCHES LONG. R & R CRACKED STRINGER 13 LT AT STATION 676 IAW SRM 53-00- 03 FOR B653-60933-MR. SDR INFO CRACKED 2 INCHES, PN 143T3001, SN NSN, PART NAME STRINGER, FS & BS LOC ON ACFT FROM STATION 676, STRINGER & WS LOC STRINGER 13L. ACFT WAS GNDED.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

CORROSION FOUND ON FLOORBEAM IN ALC, STATION 1285 APPROXIMATELY STRINGER 33 - 34R. LOCATED APPROXIMATELY 15 INCHES INSIDE OF ALC DOOR OPENING. REMOVED DAMAGED SECTION OF FLOORBEAM UPPER CHORD BS 1285 IAW SRM 53- 00-07, INSTALLED FABRICATED REPAIR IAW SRM 53-00-07 & SRM 51-40-02-0G. SDR INFO CORRODED LEVEL 2, PN 1506-3123 7075-T6511, PART NAME UPPER FRAME CHORD, SN NSN, FS & BS LOC 1285 TO 1285, STRINGER & WS LOC STRINGER 33R TO STRINGER 34R. ACFT WAS GNDED.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

FLC FUSELAGE STATION 676, LBL 21 - 28 UPPER CHORD UNDERNEATH CORRODED AT NUTPLATE LOCATIONS. R & R UPPER CHORD AT STATION 676 IN THE FLC IAW SRM 51-40- 02. PN 1506-3123, 7075-T6511, PO 0046081. SDR INFO CORRODED LEVEL 2, PN 1506-3123 7075-T6511, PART NAME UPPER CHORD, SN NSN. ACFT WAS GNDED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

ALC FRAME UPPER FLANGE CORRODED UNDER & AROUND NUTPLATES AT FS 1219 LBL 21 & LBL 35 - 40. REMOVED CORROSION FROM ALC FRAME UPPER FLANGE AROUND NUTPLATES AT FS 1219 LBL 21 & LB 35 - 40. NEW PART FABRICATED IAW SRM 53-00-07. SDR INFO CORRODED LEVEL 2, PN 146T1060-2, PART NAME UPPER CHORD, SN NSN, FS & BS LOCATION 1219 TO 1219, STRINGER & WS LOCATION LBL 19, 21, LBL 35 TO 40. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

LEFT WING TE PANEL SUPPORT HAS NUMEROUS RUSTED NUTPLATES INBD OF AUXILIARY TANK VENT AT PANEL 56NB. WORKED IAW B657-60943. REPLACED SUPPORT, PN 113T1683-31, PART NAME SUPPORT ASSEMBLY, CORRODED, EXACT STRINGER & WS LOC ON ACFT 1046.2 TO 1046.2. ACFT WAS GNDED.

Part: SUPPORT ANGLE — CORRODED (LT WING) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

LEFT WING TE PANEL SUPPORT T ANGLE PN 113T1683-33 IS CORRODED UNDER NOSE PLATE, OTBD OF AUXILIARY TANK VENT. R & R LT WING TE PANEL SUPPORT T ANGLE OTBD OF AUXILIARY TANK VENT IAW SRM 51-40-02 & B657-60935. SDR INFO CORRODED, PN 113T1683-33, PART NAME SUPPORT ASSEMBLY, EXACT STRINGER & WS LOC ON ACFT 1069.65 TO 1069.65. ACFT WAS GNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

CORROSION FOUND AT STA 1417 BETWEEN STRINGER 35R - 36R. R & R SHEAR TIE AT STA 1417 STRINGER 35 - 36R ALC IAW SRM 51-40-2. SDR INFO CORRODED, PN 140T2102-1906, PART NAME SHEAR TIE, SN NSN, EXACT FS & BS LOC ON ACFT 1417, EXACT STRINGER & WS LOC ON ACFT STRINGER 35R TO 36R. ACFT WAS GNDED.

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

WING REAR SPAR TO LOWER TE PANEL ATTACH BRACKET SPLIT ON OTBD EDGE AT WS 854. FABRICATED NEW SUPPORT RIB FROM & 10136-1700-7075-T6 PO G039188 IAW DWG 113T1673-21 & SAMPLE. INSTALLED NEW SUPPORT RIB IAW SRM 51-40-02. SDR INFO CORRODED, PN 113T16763-25, SN NA, PART NAME SUPPORT RIB, EXACT FS & BS LOCATION ON ACFT FROM WS 852.20 TO TE. ACFT WAS GNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

FORWARD LOWER CARGO FUSELAGE STATION 450, STRINGER 27L CORRODED & SPLIT AROUND RIVET. REPLACED STRINGER 27L IAW B653-60922-MR. SDR INFO CORRODED, PN 143T3001-41, PART NAME STRINGER, EXACT STRINGER & WS LOCATION ON ACFT FROM 450 TO 465, STRINGER 27L. ACFT WAS GNDED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

AFT LOWER CARGO FRAME UPPER FLANGE CORRODED UNDER NUTPLATE AT FS 1153 LBL 21. R & R AFT LOWER CARGO FLOOR SUPPORT UPPER FRAME CHORD IAW SRM 53- 00-51. SDR INFO CORRODED LEVEL 2, PN 146T1213-11, SN NSN, EXACT FS & BS, LOCATION ON ACFT FROM 1153 TO 1153. ACFT WAS GNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

AFT LOWER CARGO SHEAR TIE AT STATION 1329 CORRODED BETWEEN STRINGERS 29L & 30L. R & R SHEAR TIE AT FS 1329 STRINGER 29L - STRINGER 30L IAW SRM 51-40-02 PARA 4B & 7D. PN 140T2103-737, NSN, SHEAR TIE, CORRODED, FS 1329, STRINGER 29L - STRINGER 30L. ACFT WAS GNDED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

AFT LOWER CARGO STATION 1329 SHEAR TIE CORRODED BETWEEN STRINGERS 30L & 31L. R & R SHEAR TIE AT FS 1329, STRINGERS 30L & 31L IAW SRM 51-40-02 PARA 4B & 7D. SDR INFO CORRODED PN 140T2103-739, SN NSN, PART NAME SHEAR TIE, EXACT FS & BS LOCATION ON ACFT FROM FS 1329, EXACT STRINGER & WS LOCATION ON ACFT FROM 530L TO 531L. ACFT WAS GNDED.

Part: FITTING — CRACKED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

AFT LOWER CARGO LT SIDE STA 1087 OTBD LT ROLLER SUPPORT INTERCOSTAL TIE IS CRACKED AT BOTTOM RIVET. AFT LOWER CARGO LT SIDE STA 1087 OTBD LT ROLLER SUPPORT INTERCOSTAL, R & R CLIP. REINSTALLED INTERCOSTAL SRM 51-40-02. IAW DWG 451T 1302 & AMM 25-53-02. PN 451T2506-61, NSN, CLIP, CRACKED 1 1/2 INCHES, STA 1087, LBL 43. ACFT WAS GNDED.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

AFT LOWER CARGO STRINGER 36R CORRODED BETWEEN STATION 1395 & 1417. REPAIRED STRINGER 36R FROM FS 1384 TO 1406 IAW SRM 53-00-03 FIG 201 REPAIR 2. PN 146T3003-12, STRINGER, CORRODED, FS 1384 TO FS 1406, STRINGER 36R. ACFT WAS GNDED.

Part: STRUCTURE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

THE BULK CARGO DOOR, INTERIOR AREA, JUST AFT & ABOVE THE INNER HANDLE THERE IS CORROSION AT THE MISSING NUTPLATE. REMOVED 2 CORRODED CHORDS, REPLACED CHORDS WITH NEW FABRICATED CHORDS IAW SRM 51-40-02, DWG 146T6301 & SRM 52-30-01. PN 146T6342-1, 146T6319-5, NSN, CHORD, CORRODED, 1407 - 1461, CHORD 4 - CHORD 5. ACFT WAS GNDED.

Part: BRACKET — CRACKED (FUSELAGE) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

BELOW FLOOR PANEL 221A FOUND ANGLE BRACKET ON FLOOR BEAM CRACKED AT COCKPIT ENTRANCE. R & R ANGLE BRACKET IAW 141T5198 & SRM 51-40-02. SDR INFO CRACKED .4 INCHES, PN 141T5198-6, FS & BS LOC FROM STA 266.5 TO LBL 14. ACFT WAS GNDED.

Part: SKIN — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 58,736 hrs · 42,909 cycles

CORROSION FOUND BETWEEN RIBS 1R & 1L LOWER STRINGERS BETWEEN 4 & 5 ON HORZ STAB SKIN. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. .020 INCHES MATERIAL LOSS OUT OF .015 INCHES ALLOWABLE. CUT OUT DAMAGE & REPAIRED IAW SRM 55-10-01 FIG 201 REPAIR 2. SDR CORRODED 181.5 INCHES, PN 181T45200, SN NSN, PART NAME SKIN, EXACT FS & BS LOCATION ON ACFT FROM RIB 1L TO RIB 1R, EXACT STRINGER & WS LOCATION ON ACFT FROM STRINGER 4 TO STRINGER 5. ACFT WAS GNDED.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 57,546 hrs · 42,328 cycles

PASSING FL 260, LT FWD ENTRANCE DOOR MESSAGE ILLUMINATED. CHECKED IAW MM 52-11-00-6, OPS CHECKED NORMAL AND DOOR WARNING SYS OPS IAW 52-71-00-5. OPS CHECKED GOOD, ACFT WAS GROUNDED.

Part: ACTUATOR — FAILED (LE SLAT) · airframe 57,200 hrs · 42,169 cycles

27 81 05 00 EICAS MSG L/E SLAT ASYM DISPLAYED, LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. UPON WALK AROUND MAINTENANCE FOUND THE NUMBER 8 SLAT INBOARD PORTION EXTENDED AND OUTBOARD PORTION RETRACTED. FURTHER INVESTIGATION DETERMINED A FAILURE OF THE ROTARY ACTUATOR ASSEMBLY RESULTING IN DAMAGE TO THE FIXED LEADING EDGE AND BUCKLING THE SLAT ASSEMBLY. ACFT WAS GROUNDED.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 55,893 hrs · 41,567 cycles

LEFT OVERWING EXIT CUTOUT FRAME CORRODED ALONG THE AFT SIDE MIDWAY UP. CUT OUT CORRODED SECTION AND REPAIRED PER REA B653-59933-MR, ACFT WAS GROUNDED.

Part: SPAR — CORRODED (RT WING) · airframe 55,893 hrs · 41,567 cycles

CORROSION FOUND IN 2EA PLACES ON RIGHT WING UPPER SURFACE AT REAR SPAR UNDER T/E PANEL AT WS 261 AND WS 236. DEEP EXFOLIATION AT BOTH LOCATIONS. BLENDED AREAS ARE COMPLIED WITH ON REA B657-59956-MR, ACFT WAS GROUNDED.

Part: DOUBLER — CORRODED (RT WING) · airframe 55,893 hrs · 41,567 cycles

WING TRAILING EDGE PANEL FORWARD OF OUTBOARD AILERON HAS RAISED AREAS AT LEADING EDGE STA 927, 936, 981 APPROX ON UPPER SURFACE. REMOVED AND REPLACED DOUBLERS & FILLERS TO COMPLETE MAINTENANCE. INSTALLED ON REA B657-59950-MR, ACFT WAS GROUNDED.

Part: RIB — CRACKED (LE SLAT) · airframe 55,893 hrs · 41,567 cycles

NUMBER 5 SLAT OUTBOARD DRIVE ROD CUTOUT OUTBOARD NOSE RIB CRACKED. MANUFACTURED RIB IAW BOEING DWG 114T2511 REMOVED OLD RIB & REPLACED WITH NEW PART. WORKED IAW DWG 114T2511, B767 SRM 51-40-2 PAGE 7D, 51-20-01 METAL PO#0016868. HEAT TREAT IAW BAC 5602, BAC 5946, ACFT WAS GROUNDED.

Part: BEAM — CORRODED (LT WING) · airframe 55,893 hrs · 41,567 cycles

AREA OF CORROSION ON LOWER T-CAP OF UPPER PANEL ATTACH BEAM INBOARD OF GEAR AT WS 255, 23 INCHES FROM LEADING EDGE. BLENDED CORROSION SIZE:7.25 LONG X 1.00 WIDE LOCATION: WS 255, OUTBOARD HORZ FLANGE OF LWR CHORD. ON LOWER TEE CAP OF ATTACH BEAM AT WS 255. FOUND TO BE OUT OF LIMITS IAW B767 SRM CH 57-51-02. REPAIRED BLEND AREA IAW REA B657-59953MR, ACFT WAS GROUNDED.

Part: BEAM — CORRODED (RT WING) · airframe 55,893 hrs · 41,567 cycles

WING STA 819 EXFOLIATION CORROSION FOUND ON LOWER SURFACE OF RIGHT WING T/E PANEL SUPPORT BEAM AT WS 257, 22 INCHES AFT OF AFT WING SPAR UNDERNEATH "I" BEAM SUPPORT. BLENDED CORROSION IAW REA B657-59954-MR, ACFT WAS GROUNDED.

Part: RIB — CORRODED (LE SLAT) · airframe 55,893 hrs · 41,567 cycles

NUMBER 8 SLAT INBOARD AUX TRACK ATTACH FITTING OUTBOARD LOWER RIB HAS CORROSION AROUND NUT PLATES. LOWER RIB REPLACED UNDER NR 8 SLAT INBOARD AUX TRACK ATTACH FITTING OUTBOARD & NEW NUT PLATES INSTALLED IAW B767 SRM 57-41-09, ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,893 hrs · 41,567 cycles

STRINGER 9L HAS A 5 INCH CRACK AT THE UPPER RADIUS AND LOWER RADIUS LOCATED AT THE AFT SPLICE PLATE STA 676. REPLACED STRINGER CLIP AND REPAIRED STRINGER IAW REA B653-59940-MR SRM 51-40-02.SB-44/350771, ACFT WAS GROUNDED.

Part: SKIN — CORRODED (RT WING) · airframe 55,893 hrs · 41,567 cycles

RIGHT WING LEADING EDGE OF WING TRAILING EDGE UPPER PANEL AT STA 819 APPROX HAS RAISED SPOT. REMOVED PANEL, FOUND CORROSION, BLENDED OUT OF LIMITS PER SRM 57-20-01. COMPLIED WITH B657-59951-MR, ACFT WAS GROUNDED.

Part: SKIN — CORRODED (LT WING) · airframe 55,983 hrs · 41,567 cycles

LEFT WING UPPER T/E WING SKIN AT STA 466, 505, AND 532 ARE CORRODED. REMOVED CORROSION FROM UPPER T/E WING SKIN IAW B767 SRM 57-20-01. REPAIRED UPPER T/E WING SKIN AT WS 505, 532 IAW AMES REA B657-55943-MR. TREATED & PRIMED AREAS IAW B767 SRM 51-20-01, ACFT WAS GROUNDED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,893 hrs · 41,567 cycles

STRINGER 8L HAS A 4 INCH CRACK AT THE UPPER RADIUS LOCATED AT THE AFT SPLICE PLATE STA 676. REPAIRED STRINGER 8 IAW REA 653-59940-MR, ACFT WAS GROUNDED.

Part: COWLING — WORN (LEFT) · airframe 55,893 hrs · 41,567 cycles

NR 1 ENGINE INBOARD CORE COWL TRAILING EDGE WORN TO SHARP EDGE IN SEVERAL PLACES. REPLACED NR 1 INBOARD CORE COWL T/E STRAP IAW 767 SRM 51-40-02 AND CMM 71-11-45. SEE PWA & PWS #30 FOR DETAILS. CORE COWL RE-INSTALLED ON NR 0676, ACFT WAS GROUNDED.

Part: RIB — CRACKED (LE SLAT) · airframe 55,893 hrs · 41,567 cycles

NUMBER 4 SLAT OUTBOARD DRIVE ROD CUTOUT INBOARD NOSE RIB CRACKED. REMOVED AND REPLACED NR 4 SLAT I/B DRIVE ROD CUTOUT I/B NOSE RIB IAW B767 SRM 51-40-02 REF DRAWING 114T2512, ACFT WAS GROUNDED.

Part: INERTIA REEL — OUT OF POSITION (CABIN) · airframe 52,884 hrs · 40,309 cycles

SAFETY INERTIAL REEL FELL OUT ON APPROACH. SUPERNUMERARY COMPARTMENT. STOWED DESCENT DEVICE IAW B767 AMM 25-61-03.

Part: BEAM — CORRODED (RT MLG) · airframe 52,201 hrs · 39,997 cycles

CORROSION ON BEAM, AFT OF RT MLG AFT TRUNNION - BEAM RUNS INBOARD TO OUTBOARD VIEWED FROM 652 AB LOOKING UP. REMOVED AND REPLACED IAW 767 SRM 51-40-2.

Part: SUPPORT — CORRODED (AILERON) · airframe 52,201 hrs · 39,997 cycles

LEFT, I/B AILERON, I/B AILERON HINGE SUPPORT RIB UPPER NUT PLATE CHANNEL IS CORRODED ON BOTH SIDES OF SUPPORT AND RIB AS MARKED. REMOVED AND REPLACED TEE P/N 113T1510-33AX IAW AMM 51-40-2. LEAK CHECK GOOD IAW B767 AMM 28-11-00.

Part: SUPPORT BEAM — CORRODED (LT MLG) · airframe 52,201 hrs · 39,997 cycles

CORROSION ON BEAM AFT OF LEFT MLG AFT TRUNNION. PANEL SUPPORT BEAM RUNS INBOARD TO OUTBOARD VIEWED FROM 552AB LOOKING UP. OPEN PANEL FOM REMOVED AND REINSTALLED SUPPORT RIB. RE-INSTALLED PANEL IAW BOEING 767 SRM 51-40-2.

Part: SUPPORT FITTING — CORRODED (LT WING) · airframe 52,201 hrs · 39,997 cycles

AREA OF CORROSION AT APPROX WS 450 WHERE LT AILERON DROOP MECHANISM - TO AFT SPAR ATTACH ANGLE. REMOVED AND REPLACED VERTICAL SUPPORT FITTING IAW B767 AMM 51-40-02. LEAK CHECK GOOD IAW B767 AMM 28-11-00.

Part: SUPPORT BEAM — CRACKED (LT PYLON) · airframe 52,201 hrs · 39,997 cycles

LEFT ENG PYLON HYD ACCESS BAY OUTBOARD SUPPORT BEAM IS CRACKED THRU NUT PLATE, COMMON TO PANEL 437ELX. INSTALLED NEW LEFT WING ENG PYLON HYD ACCESS BAY SUPPORT BEAM IAW B767 SRM 51-40-2.

Part: RIB — CORRODED (ZONE 600) · airframe 52,201 hrs · 39,997 cycles

NR 9 SLAT I/B AUX TRACK ATTACH FITTING I/B RIB HAS CORROSION UNDER PANEL ATTACH NUT PLATES. REMOVED AND REPLACED RIB ON NR 9 SLAT I/B AUX TRACK ATTACH FITTING IAW B767 SRM 57-40-02.

Part: RIB — CORRODED (LE SLAT) · airframe 52,201 hrs · 39,997 cycles

NR 2 SLAT I/B AUX TRACK FITTING O/B RIB CORRODED AROUND PANEL ATTACH NUT PLATES AND SHIM PACK FOR FITTING. REMOVED NR 2 SLAT I/B AUX TRACK I/B AND O/B LOWER RIBS. INSTALLED NEW RIBS IAW 767 SRM 51-40-02.

Part: RIB — CORRODED (LE SLAT) · airframe 52,201 hrs · 39,997 cycles

WING L/E PANEL ATTACH NUT PLATE HAS CORROSION UNDER IT AT NR 10 SLAT BETWEEN O/B AUX AND MAIN TRACK. REMOVED AND REPLACED DAMAGED RIB AND CLOSE OUT NOSE BEAM WEB ON LT WING SLAT O/B AUX TRACK O/RIB IAW B767-200 SRM 51-40-02.

Part: RIB — CORRODED (LE SLAT) · airframe 52,201 hrs · 39,997 cycles

CORROSION AROUND PANEL ATTACH NUT PLATES ON NR 3 SLAT I/B AUX TRACK I/B AND O/B RIBS. REMOVED AND REPLACED RIB IAW 767-200 SRM 51-40-02.

Part: RIB — CORRODED (RT WING) · airframe 52,201 hrs · 39,997 cycles

NR 9 SLAT STRUT RIB IS CORRODED (LOCATED I/B OF THE O/B AUX TRACK). REMOVED AND REPLACED NR 9 SLAT STRUT RIB I/B OF THE O/B AUX TRACK IAW B767 SRM 51-40-02.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 52,201 hrs · 39,997 cycles

PANEL ATTACH ANGLE AT STA 958 BETWEEN LT AND RT KEEL BEAM IS CORRODED. REMOVED AND REPLACED IAW BOEING 767 SRM 51-40-2.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 522,001 hrs · 39,997 cycles

PANEL ATTACH ANGLE AT STA 913 BETWEEN LT AND RT KEEL BEAM IS CORRODED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-02.

Part: PANEL — CRACKED (LT WING) · airframe 52,201 hrs · 39,997 cycles

NR 4 SLAT I/B DRIVE ROD CUTOUT I/B NOSE RIB CLOSING PANEL CRACKED. REMOVED, FABRICATED NR 4 SLAT I/B DRIVE ROD CUTOUT I/B NOSE RIB CLOSING PANEL IAW DWG 114T25-12. INSTALLED RIB IAW B767 SRM 51-40-02 REMOVED AND REPLACED SLAT TRACK CURTAIN FOR NR 4 SLAT I/B TRACK IAW B767 SRM 51-40-02.

Part: PLATE — CORRODED (CARGO DOOR) · airframe 52,201 hrs · 39,997 cycles

FWD INBOARD CORNER OF BULK CARGO DOOR LOWER SILL UPPER SURFACE CORRODED. FOUND CORROSION BEYOND LIMITS. REPLACED BULK CARGO DOOR LOWER SILL FLOOR PLATE AND RE-SEALED IAW BOEING 767 DWG 146T8211 AND SRM 51-40-02.

Part: SKIN — DAMAGED (HORIZ STAB) · airframe 52,201 hrs · 39,997 cycles

FOUND FWD SKIN AT LT STAB HORSE COLLAR DAMAGED. REMOVED DAMAGED SKIN FROM AIRCRAFT MANUFACTURED NEW SKIN IAW 767 SRM 53-80 SECTION 48 PAGE 1 DETAIL 1 PO 407827176. INSTALLED NEW SKIN IAW 767 SRM 51-40-2. RE-INSTALLED I/B LOWER SEAL PANEL IAW SRM 51-40-2.

Part: STIFFENER — GOUGED (NR 1 PYLON) · airframe 52,201 hrs · 39,997 cycles

NR 1 PYLON AFT FAIRING (STRINGER) 437DB INNER STIFFENER OUTBOARD SIDE IS GOUGED. FABRICATED NEW INNER STIFFENER FOR NR 1 PYLON AFT FAIRING AND INSTALLED FABRICATED STIFFENER IAW B767-200 SRM 54-51-71.

Part: SKIN — CHAFED (FUSELAGE) · airframe 52,201 hrs · 39,997 cycles

SKIN CHAFED THRU ON LEFT SIDE FUSELAGE WHOLE LOWER HORSE COLLAR OPERATES. REPAIRED AREA IAW 767 SRM 53-80-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 51,872 hrs · 39,836 cycles

LEFT FWD ENTRY DOOR LIGHT ILLUMINATED INFLIGHT DOOR HANDLE RAISED OUT OF POSITION. INSPECTED BOTH OUTER AND INNER DOOR HANDLES FOR OPERATION PER MM 52-11-2-5-5 BOTH WERE GOOD. COMPARED TO L1 AND R1 DOOR HANDLES AND OPERATION BOTH WERE THE SAME. CHECKED RIG OF L1 DOOR SW19 AND R1 DOOR SW193 BOTH WERE IN LIMITS.

Part: HANDLE — POPPED (ENTRY DOOR) · airframe 51,505 hrs · 39,659 cycles

EICAS MSG FWD ENTRY DOOR ILLUMINATED INFLIGHT 3 TIMES DOOR HANDLE POPPED SLIGHTLY OPEN EACH TIME, BUT WOULD NOT REMAIN IN FULL LOCKED POSITION. INSPECTED DOOR HANDLE & MECHANISM FOR WEAR. ALL WAS GOOD. INSPECTED DOOR PROX SW 194 & 195. BOTH WERE 52-11-25-5, ALL CHECKS WERE GOOD.

Part: FITTING — CRACKED (HORIZ STAB) · airframe 49,291 hrs · 38,619 cycles

DURING C-CHECK AT ILN, MAINTENANCE FOUND A CRACK INDICATION DURING AFTER MODIFICATION INSPECTION OF THE RIGHT FORWARD OUTER CHORD AND TENSION FITTING PER A/B 767-53A0078, AS MANDATED BY AD 2005-11-02. THREE DISCREPANT FASTENER HOLE LOCATIONS WERE OVERSIZED TO REMOVE DISCREPANCIES AND THE LOWER TENSION FITTING WAS REPLACED AS THE ANOMALY WAS TOO LARGE TO REMOVE BY HOLE ENLARGEMENT. RESULTING IN 3 HOLE LOCATIONS WITH HOLES LARGER THAN ALLOWED IN THE BULLETIN. BOEING INSTRUCTED ABX TO INSTALL OVERSIZED FASTENERS IN THE 3 LOCATIONS THROUGH THE ENTIRE STACK UP, TO INCLUDE THE CHORD, FITTINGS AND FUSELAGE SKIN. REPAIRED IAW REA B657-58095-MR.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,291 hrs · 38,619 cycles

DURING C-CHECK INSPECTION, FOUND LWW BULKHEAD STA 1065 HAD BULGE AT LOWER HYDRAULIC FITTING LBL 70. FOUND CRACK ON STRUCTURE UNDER FITTING. BULKHEAD REPAIRED IAW B767 SRM 51-70-13 FIG 1. CRACK REQUIRED CUTOUT AND DOUBLER. CUT OUT CRACK AND FABRICATED DOUBLER FROM 2024-T3 .040. CORROSION FOUND AND EVALUATED WAS ON SECONDARY STRUCTURE. NOT LEVEL 2 OR 3.

Part: WIRE — DETACHED (CABIN) · airframe 45,927 hrs · 37,499 cycles

R1 EMERGENCY EXIT LIGHT DID NOT ILLUMINATE WHEN EMERGENCY TEST SWITCH WAS DEPRESSED. FOUND WIRES TO EXIT LIGHT NOT ATTACHED. CHECKED AND ATTACHED WIRES, OPS CHECKED GOOD IAW BOEING MM.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 45,927 hrs · 37,499 cycles

EMERGENCY 02 TEST LIGHT WOULD NOT PRESS TO TEST (INOPERATIVE) SUPERNUMERARY AREA. REPOSITIONED WIRING AT DEPRESS LIGHT L9003 IAW WDM 33-24-11. OPS CHECKED GOOD IAW BOEING MM.

Part: SKIN — DEBONDED (LT ELEVATOR) · airframe 45,894 hrs · 37,486 cycles

LEFT ELEVATOR OUTBOARD HAD INTERPLY DISBOND AT EACH ACTUATOR FITTING AREA ON LOWER LEADING EDGE. REPLACED LEFT ELEVATOR ON NON ROUTINE 0395 IAW BOEING SRM.

Part: RIB — CORRODED (RT WING) · airframe 45,894 hrs · 37,486 cycles

CORROSION WS 564, RIGHT WING LEADING EDGE PANEL SUPPORT/RIB. REPLACED STRUT RIB IAW B767 SRM 51-40-02.

Part: RIB — CORRODED (RT WING) · airframe 45,894 hrs · 37,486 cycles

CORROSION WS 720, RIGHT WING LEADING EDGE LOWER PANEL SUPPORT/RIB. REPLACED STRUT RIB IAW B767 SRM 51-40-02.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 45,894 hrs · 37,486 cycles

L1 DOOR CUTOUT LOWER CORNER INTERNAL DOUBLER AFT CORNER HAD CRACK INDICATION. TWO CRACKS, ONE .275 INCH AND ONE .210 INCH. REPAIRED AREA IAW REA B653-55867-MR.

Part: PIN — CORRODED (RT HORIZ STAB) · airframe 45,894 hrs · 37,486 cycles

RIGHT HORIZONTAL STABILIZER PIVOT PIN HAD CORRODED PITTING IN THREADS. REPLACED PIVOT PIN IAW JOB CARD 7302001.

Part: PIN — CRACKED (LT HORIZ STAB) · airframe 45,894 hrs · 37,486 cycles

LEFT OUTER HORIZONTAL STABILIZER PIVOT PIN CRACKED. REPLACED PIVET PIN AND OUTBOARD PIVOT SPACER IAW B767 JOB CARD 7302001.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 45,894 hrs · 37,486 cycles

CRACKED STIFFENER COCKPIT FLOORBEAM STA 266.5 APPROXIMATELY LEFT BUTT LINE 10.50. REMOVED, FABRICATED AND INSTALLED STIFFENER ON FLOORBEAM STA 266.5, LEFT BUTT LINE 10.50 IAW BOEING SRM.

Part: CYLINDER — CRACKED (RT MLG) · airframe 45,894 hrs · 37,486 cycles

RIGHT MAIN LANDING GEAR HAD A LARGE CRACK AT CASTING ON UPPER CENTER AFT END. REPLACED RIGHT MAIN LANDING GEAR ON JOB CARD 32-045-01-2 IAW BOEING SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 45,894 hrs · 37,486 cycles

R1 DOOR CUTOUT HAD DEFECT EXTENDING FROM RIVET AND LOWER AFT CORNER. REPAIRED AREA IAW REA B653-55851-MR.

Part: WIRE — CHAFED (CONTROL PANEL) · airframe 43,973 hrs · 36,911 cycles

CIRCUIT BREAKER P15 ON P11 PANEL FOR AUTO 1 CABIN ALTITUDE CONTROL TRIPPED, WOULD NOT RESET. FOUND BURNED WIRING ADJACENT TO OUT FLOW VALVE A/C MOTOR. REMOVED, REPAIRED AND/OR REPLACED DEFECTIVE WIRING AS NECESSARY PER ABX 767 WDM 21-31-31, 21-31-21, 21-31-11 AND BOEING STANDARD WIRING PRACTICES 20-10-11 CABIN PRESS SYS NR 1 CHECK GOOD ON GROUND PER ABX 767 AMM 21-31-00-5.

Part: WARNING LIGHT — INTERMITTENT (EMERGENCY DOOR) · airframe 41,927 hrs · 36,074 cycles

EMERGENCY DOOR LIGHT FLASHED INTERMITTENTLY IN TURBULENCE. FOUND EMERGENCY DOOR LIGHT FLICKERING ON GROUND. NO EICAS MESSAGE. CODE 007 ON PSEU. RESEATED CARD 3 AND 4 IN PSEU. RETESTED PSEU IAW B767 MM 32-09-04. NO FAULTS NOTED. DOOR LIGHT EXTINGUISHED.