N739AX

Part: NONE — NONE · airframe 100,457 hrs · 47,160 cycles

UPON APPROACH INTO DESTINATION KILN, EQUIPMENT OVERHEAT FOLLOWED BY CABIN ALTITUDE WARNING AT FL290. CREW DECLARED EMERGENCY DESCENT. LANDING UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. PACK TEMP CONTROLLER AND AIR SUPPLY MODULE BITE TEST IAW B767 FIM 21-51-803 AND FIM 36-20-804 SATISFACTORY. NO FAULTS NOTED. EQUIPMENT COOLING OPERATIONAL CHECK IAW B767 AMM 21-58-00 GOOD. NO FAULTS FOUND.

Part: WINDOW — NOISY · airframe 99,929 hrs · 46,873 cycles

AFTER TAKE OFF AND PRIOR TO V1 AT 120 KNOTS, CREW REPORTED AIR NOISE FROM R2 WINDOW. AIR TURN BACK TO DEPARTURE STATION KCLT. LANDING WAS UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONARY ACTIONS. ON ARRIVAL, AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. IN ACCORDANCE WITH B767 MAINTENANCE MANUAL 21-31-00, DIFFERENTIAL PRESSURIZATION CHECK SATISFACTORY. NO DEFECTS NOTED. SECURITY AND INTEGRITY OF SEAL, HARDWARE AND CONNECTIONS SATISFACTORY. NO FAULTS FOUND. OPERATIONAL CHECK IN ACCORDANCE WITH B767 MAINTENANCE MANUAL 21-31-00 GOOD. NO FAULTS FOUND. AIRCRAFT RELEASED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE · airframe 99,340 hrs · 46,571 cycles

POST FLIGHT, COCKPIT EMERGENCY FLASHLIGHT INOPERATIVE. SYSTEM DEFERRED IAW B767 MINIMUM EQUIPMENT LIST. ATI-25-63-04-01 MEL CAT C. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECK GOOD. DEFERRAL MAINTENANCE ITEM CLEAR.

Part: FLAP SYSTEM — WARNING MESSAGE · airframe 98,168 hrs · 45,992 cycles

ON CLIMB OUT, TRAILING EDGE FLAP ASYMMETRY CAUTION MESSAGE DISPLAYED CREW REPORTS AT TAKE OFF FLAPS FIVE UNITS, WHEN HANDLE WAS MOVED TO 1 UNIT MESSAGE DISPLAYED. AIR TURN BACK TO DEPARTURE STATION-KCVG. EMERGENCY DECLARATION RELAYED TO AIR TRAFFIC CONTROL. LANDING UNEVENTFUL WITH NO ADDITIONAL PRECAUTIONS NOTED. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. WORK IN PROGRESS

Part: INTERROGATOR — INOPERATIVE · airframe 91,427 hrs · 43,596 cycles

CREW REPORTED WHEN EXTERNAL POWER IS CONNECTED, SMOKE AND FUMES FILL THE COCKPIT. REMOVED AND REPLACED RIGHT DME IAW AMM 34-55-01. OPS CHECKED SATISFACTORY. E & E SYSTEM PURGED IAW CONDITIONAL INSPECTION AMM 05-51-56. AIRCRAFT RELEASED TO SERVICE.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 91,357 hrs · 43,570 cycles

CABIN ALTITUDE WARNING LIGHT WITH EICAS ON AT FLT390. DIVERTED WITH AN EMERGENCY DECLARATION. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE CABIN PRESSURE CONTROLLER. LEAK AND OPS CHECKED SATISFACTORY. COMPLIED WITH CONDITIONAL INSPECTION 05-51-24. FAULT NOT DUPLICATED. AIRCRAFT RELEASED TO SERVICE.

Part: ACM — INOPERATIVE (RIGHT) · airframe 90,820 hrs · 43,364 cycles

CREW REPORTED FA COMPARTMENT SMELLS OF OIL WITH PACKS ON, IN FLIGHT AND ON THE GROUND. THE AIRCRAFT WAS GROUNDED. OPERATING OF BOTH PACKS, A STRONG ODOR OF OIL WAS ISOLATED TO THE RIGHT PACK EXHAUST SYSTEM. CONDITIONAL INSPECTION OF SYSTEM IAW B767 AMM 21-00-21 COMPLIED WITH. NO CONTAMINATION WAS NOTED. REMOVED AND REPLACED RIGHT AIR CYCLE MACHINE. OPS CHECKED SATISFACTORY. AIRCRAFT RELEASED TO SERVICE.

Part: SEAT TRACK — CORRODED (BS 1480-1500) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SEAT TRACK AUXILIARY STRUCTURE AT RBL 77, R2 DOOR AREA IS CORRODED. BLENDED SEAT TRACK AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02 AND ENGINEERING DOCUMENT 47224FAB58, REV IR.

Part: DRAIN — CORRODED (BS 1601) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO STRUCTURE UNDER AFT FLOOR DRAIN IS CORRODED IN SEVERAL SPOTS FROM LBL 77 THROUGH RBL 77. REMOVED AND REPLACED FLOOR DRAIN SUPPORT IAW SRM 51-40-02 AND ENGINEERING DOCUMENTS 47224FAB79, AND 47224FAB67.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO STATION 1351 FLOOR UPPER CHORD IS CORRODED IN SEVERAL SPOTS FROM LEFT BUTT LINE 54 TO RIGHT BUTT LINE 54. REMOVED AND REPLACED AFT LOWER CARGO STATION 1351 UPPER CHORD ON FLOOR IN ACCORDANCE WITH SRM 51-40-02. FABRICATED IN ACCORDANCE WITH DRAWING 146T1213-22.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO STATION 1395 UPPER FLOORBEAM CAP CORRODED AROUND SEVERAL NUTPLATES LEFT BUTT LINE 54 THROUGH RIGHT BUTT LINE 54. REMOVED CORRODED FLOORBEAM CAP AND REPLACED WITH NEW FLOORBEAM CAP PER SRM 51-40-02.

Part: WEB — CRACKED (BS 1395) · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO BS 1395 WEB, 5 INCHES UNDER FLOORBEAM AT LBL 25 IS CRACKED. REPAIRED THE WEB IAW SRM 51-70-13.

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. CORROSION ON CLOSEOUT WEB STATION 1325 LEFT BUTT LINE 11. CLOSEOUT WEB IS EXFOLIATED COMPLETELY THROUGH AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-53. FABRICATED AND REPLACED IAW DRAWING 451T2504.

Part: ANGLE — CORRODED (DOOR SILL) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON THE LOWER SURFACE OF THE AFT LOWER CARGO DOOR LOWER SILL PLATE AT BS 1351. REMOVED, DRILLED AND INSTALLED A NEW DOOR SILL ANGLE IAW DRAWING 146T8510.

Part: STRINGER — CORRODED (BS 1558) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER 34R IS CORRODED AT BS 1558. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03, REPAIR 2, DETAIL II, AND DRAWINGS 146T3002 AND 146T1223.

Part: STRINGER — CORRODED (BS 1351) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER 35R, BS 1351 CORRODED. REPAIRED AREA IAW SRM 53-00-03 REPAIR 2, FIGURE 201.

Part: STRINGER CLIP — CORRODED (BS 1086) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION OF FORWARD SIDE OF STRINGER CLIP 37R AT BS 1086. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02, AND DRAWING 140T0833.

Part: STRINGER — CORRODED (BS 1197-1204) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO FLOOR, BS 1197 TO 1204, STRINGER 35L FOUND CORRODED IN 2 SPOTS. REMOVED DAMAGED SECTION AND REPAIRED IAW SRM 53-00-03, FIGURE 201, REPAIR 2.

Part: STRINGER — CRACKED (BS 676-696) · airframe 90,241 hrs · 43,067 cycles

STRINGER 1L IS CRACKED ON THE END AFT OF BS 676 AT SPLICE. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03, FIGURE 201.

Part: STRINGER — CRACKED (BS 676-696) · airframe 90,241 hrs · 43,067 cycles

STRINGER 11L CRACKED ON END AFT OF BS 676 AT SPLICE. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03, REPAIR 1, TYPE 1, REV 123.

Part: STRINGER — CORRODED (BS 1440-1470) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BULK CARGO BS 1462, STRINGER 34R CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03, REPAIR 2, DETAIL II, AND WO 669089-1095.

Part: STRINGER — CRACKED (BS 676) · airframe 90,241 hrs · 43,067 cycles

STRINGER 7L CRACKED ON END AFT OF BS 676 AT SPLICE. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03, FIGURE 201. STRINGER FABRICATED IAW SRM 53-00-03, REPAIR 1, TYPE 1, REV 123. COMPLIED WITH SERVICE BULLETIN 368-53-041.

Part: STRINGER — CORRODED (BS 1207-1219) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO BS 1219, STRINGER 33R IS CORRODED ON END. CUT OUT DAMAGED SECTION OF THE STRINGER AND INSTALLED IAW SRM 53-00-03, FIGURE 201, REPAIR 2.

Part: SHEAR TIE — CORRODED (BS 1395) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE CORRODED BS 1395 BETWEEN STRINGERS 35 - 36L. BLENDED THE SHEAR TIE, AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02 AND DRAWING 146T1215.

Part: STRINGER — CRACKED (BS 673-676) · airframe 90,241 hrs · 43,067 cycles

STRINGER 12L CRACKED ON END AFT OF BS 676 AT SPLICE. REMOVED AND REPLACED THE STRINGER IAW SERVICE BULLETIN 368-53-041, AND SRM 53-00-03, REPAIR 1, TYPE 1, REV 123.

Part: SLAT TRACK — CORRODED · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

NR 9 SLAT, INBOARD MAIN TRACK CORRODED ON LOWER SURFACE. REMOVED AND INSTALLED NEW INBOARD MAIN SLAT TRACK IAW 27-81-34.

Part: STRINGER — CRACKED (BS 672-676) · airframe 90,241 hrs · 43,067 cycles

STRINGER 8L CRACKED ON END AFT OF STATION 676 AT SPLICE. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03 FIGURE 201 AND COMPLIED WITH SERVICE BULLETIN 368-53-041.

Part: SLAT TRACK — CORRODED · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

NR 8 SLAT OUTBOARD MAIN SLAT TRACK CORRODED. REMOVED AND REPLACED THE SLAT TRACK IAW AMM 27-81-34, PARAGRAPH 3E.

Part: SKIN — CORRODED (BS 1197-1219) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO FUSELAGE SKIN CORRODED AT BS 1197 - 1219, STRINGER 33 - 35R. TWO AREAS BLENDED OUT OF LIMITS. CUT OUT DAMAGED AREAS, FABRICATED AND INSTALLED DOUBLER, TRIPLER, AND TWO FILLERS IAW SRM 53-00-01, FIGURE 201, REPAIR 14.

Part: FLOORBEAM — CORRODED (BS 303) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON FLOORBEAM UPPER HORIZONTAL FLANGE LOWER SURFACE BS 303, LBL 54 AROUND NUTPLATE. REMOVED DAMAGED ON FLOORBEAM UPPER FLANGE LOWER SURFACE. PERFORMED REPAIR IAW SRM 51-20-01.

Part: STRAP — CORRODED (BS 1480) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BULK CARGO BS 1480, STRINGER 23L INTERCOSTAL INBOARD STRAP CORRODED. REMOVED AND REPLACED THE STRAP IAW SRM 51-40-02, AND ED 47221FAB88.

Part: SKIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT OTBD AILERON HAS AREAS OF CORROSION ON THE SKIN AROUND THE BALANCE WEIGHT. REMOVED AND REPLACED THE AILERON IAW AMM 27-11-02, PARAGRAPH 3G.

Part: FLOOR SUPPORT — CORRODED (BS 1483-1610) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO OUTER FLOOR SUPPORT CORRODED BS 1483-1610. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, AND ED 47224FAB08, AND 47224FAB51.

Part: WEB — CORRODED (DOOR SILL) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

R2 DOOR SILL CORRODED. BLENDED AREA IAW 53-00-15 DETAIL XII PAGE 113. FOUND TO BE OUT OF LIMITS. FABRICATED A NEW DOOR SILL WEB IAW DRAWING 146T8310,

Part: FLOORBEAM — CORRODED (BS 287) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON THE FLOORBEAM UPPER HORIZONTAL FLANGE LOWER SURFACE BS 287 LBL 45 - 54. REMOVED AND REPAIRED THE DAMAGED AREA IAW SRM 53-00-51, AND DRAWING 141T5111.

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT REAR SPAR SUPPORT IS CORRODED AT BOTH ENDS, LWS 853. REMOVED AND REPLACED THE SUPPORT STIFFENER IAW SRM 51-40-02. LEAK CHECKED IAW AMM 28-11-00. CHECKED GOOD.

Part: BEAR STRAP — CORRODED (BS 1260-1274) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

THE BEAR STRAP WAS CORRODED BS 1263-1274, BETWEEN STRINGERS 34 - 35R. THE BEAR STRAP WAS FOUND OUT OF LIMITS IAW SRM 51-10-02. FABRICATED AND INSTALLED A DOUBLER AND TRIPLE IAW SRM 53-00-01, AND ED 47224REA44.

Part: FLOORBEAM — CORRODED (BS 1220) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RBL 35 - 44, BS 1220 FLOORBEAM HAS CORROSION AROUND THE NUTPLATE. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-01, SECTION 9.

Part: STRINGER — CORRODED · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION OTBD OF RIB 2L, FORWARD LOWER EDGE OF LOWER STRINGER 8. CORROSION OUT OF LIMITS IAW SRM 55-10-02. PERFORM SPLICE REPAIR ON STRINGER 8 IAW SRM 55-16-02, REPAIR 1.

Part: FLOORBEAM — CORRODED (BS 1311) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO FLOORBEAM CORRODED BS 1311, RBL 5 - LBL 20. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1307-1329) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO FLOOR SUPPORT CORRODED AT LBL 12, BS 1307-1329. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1410) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BS 1410 UPPER FLOOR SUPPORT CORRODED AROUND ALL NUT PLATES LBL 54 THROUGH RBL 54. REMOVED SURFACE DAMAGE IAW SRM 53-00-51-1A-1. REMOVED AND REPLACED THE NUT PLATES IAW SRM 51-40-02.

Part: STRINGER — CORRODED · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION INBD OF RIB 2R LOWER STRINGER 5, VERTICAL LEG FORWARD AND AFT. CORROSION OUT OF LIMITS IAW SRM 55-10-02, FIGURE 101, DETAIL II. REMOVED AND REPLACED THE STRINGER IAW SRM 55-10-03, REPAIR 1, AND DRAWING 181T4000.

Part: FLOOR SUPPORT — CORRODED (BS 1395-1417) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO FLOOR SUPPORT CORRODED AT BS 1395-1415, LBL 24. FABRICATED A NEW FLOOR SUPPORT IAW DRAWING 452T3252. REMOVED & REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: FAILSAFE — CORRODED (BS 955) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION FOUND ON THE TERMINAL FITTING AT RBL 97 BS 955. REMOVED AND REPLACED THE FAILSAFE.

Part: STRAP — CORRODED (BS 1483) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOOR PLATE STRAP LBL 70 BS 1483 CORRODED. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIGURE 101, DETAIL II. FABRICATED A NEW STRAP IAW DRAWING 368-53-16-94372.

Part: ANGLE — CORRODED (BS 977) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

TWO ANGLES AT BS 977 CORRODED. REPAIRED IAW ED 47224REA51, AND 47224REA52.

Part: SHEAR TIE — CORRODED (BS 1480) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE CORRODED AT BS 1480 BETWEEN STRINGERS 38L-39R. BLENDED AND FOUND TO BE OUT OF LIMITS. REPLACED THE SHEAR TIE IAW DRAWINGS 146T1219, AND 146T3240.

Part: FLOORBEAM — CORRODED (BS 1153) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOORBEAM AT BS 1153 FROM LBL 36 - 48 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. REPLACED IAW SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1540-1562) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER 33L, BETWEEN BS 1540 - 1562 IS CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51-40-02 & DOCUMENT 146T8240.

Part: FORK — CORRODED (BS 955) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON THE UPPER FLANGE OF FORK AND ATTACH FITTING, IN THE UPPER FORWARD OUTBOARD CORNER OF THE LEFT WHEEL WELL. REMOVED AND REPLACED THE FORK AND SHEAR LINK.

Part: ANGLE — CORRODED (BS 1373) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BS 1373 LBL 54 FLOOR SUPPORT ANGLE CORRODED. BLENDED TO 100% MATERIAL LOSS. FABRICATED AND INSTALLED NEW ANGLE IAW DRAWING 453T1031.

Part: LINK — CORRODED (LT MLG WW) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT MLG WW, SHEAR LINK IS CORRODED. REMOVED AND REPLACED THE SHEAR LINK ASSEMBLY.

Part: FITTING — CORRODED (BS 955) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT MLG WW, FORWARD SHEAR LINK FITTING IS CORRODED. REMOVED AND REPLACED SHEAR LINK ASSEMBLY.

Part: SPAR CAP — CORRODED (RT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON RIGHT WING FRONT SPAR LOWER CAP UPPER SURFACE AT LEADING EDGE WS 1011. BLENDED OUT CORROSION TO 100% MATERIAL LOSS. CUT OUT DAMAGED SECTION, AND INSTALLED IAW ED 47224REA49.

Part: STRINGER — CORRODED (BS 676) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER 13L CRACKED ON END AFT OF BS 676. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03, FIGURE 201, REPAIR 1 AND SERVICE BULLETIN 368-53-041 REV 2.

Part: SUPPORT — CORRODED (BS 500-522) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD CARGO BAY LEFT UPPER OTBD CEILING SUPPORT IS CORRODED BETWEEN BS 500 - 522. REMOVED AND REPLACED SUPPORT IAW SRM 51-40-02, SECTION 9.

Part: SHEAR TIE — CORRODED (BS 1395) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE CORRODED AT BS 1395 BETWEEN STRINGERS 37 - 38L. FABRICATED AND INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02 AND DRAWING 140T2102.

Part: INTERCOSTAL — CORRODED (BS 1120) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1120 BETWEEN LBL 88 & RBL 88 DRAIN INTERCOSTALS CORRODED. REMOVED AND REPLACED THE DRAIN PAN INTERCOSTALS IAW DRAWING 368-53-13-90988.

Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT WING LEADING EDGE STRUT CORRODED AT WS 1030. REMOVED AND REPLACED RIB AND DOUBLER IAW SRM 57-41-09. CORROSION FOUND TO BE OUT OF LIMITS.

Part: FLOOR SUPPORT — CORRODED (BS 1417-1429) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD TIP OF BULK FLOOR SUPPORT AT LBL 29 IS CORRODED. BLENDED CORROSION. LOST 100% OF MATERIAL. FOUND TO BE OUT OF LIMITS. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02.

Part: STRUCTURE — CORRODED (BS 1050) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT WHEEL WELL OUTBOARD LONGERON CORRODED AFT END BS 1050 RIGHT BUTT LINE 90 UPPER SIDE OF HORIZONTAL WEB. UPON FURTHER INVESTIGATION LONGERON TO BE OUT OF LIMITS IAW SRM 53-50-05. REMOVED AND REPLACED LONGERON IAW SRM 51-40-02.

Part: STRINGER CLIP — CORRODED (BS 1678) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER CLIP 3R, BS 1678 BULKHEAD CRACKED. THE STRINGER CLIP WAS FABRICATED IAW DRAWING 148T2120, STRINGER CLIP AND HEAT TREATED IAW 5602 REVISION AF, 5946 REVISION AF. THE STRINGER CLIP WAS INSTALLED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1263) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOORBEAM BS 1263 LBS 33 - 40 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-07, REPLACED THE FLOORBEAM ANGLE.

Part: SKIN — CORRODED (BS 1241) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SKIN CORRODED BS 1241 JUST BELOW STRINGER 34R. CORROSION ON SKIN WAS FOUND TO BE OUT LIMITS. SKIN THICKNESS OF .210, REMAINING THICKNESS .100 IN ACCORDANCE WITH B767 SRM 51-00-01 TABLE I DETAIL II. REPAIRED PER AMES ENGINEERING DOCUMENT 47224REA44 REV A.

Part: SKIN — CORRODED (BS 1175-1197) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO BS 1175-1197 STRINGER 36R TO 37R SKIN CORRODED. REMOVED DAMAGE AREA AND REPAIRED IAW SRM 53-00-01-2R-12.

Part: ANGLE — CORRODED (BS 1461) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON STRINGER 23R AT BS 1461. REMOVED AND REPLACED IAW SRM 51-40-02 PAGE 4 PARAGRAPH 7 AND PAGE 2 PARAGRAPH 4.

Part: SKIN — CORRODED (BS 1170-1175) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SKIN BETWEEN STRINGERS 36 - 37R CORRODED AT BS 1170-1175. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-01-2R-12.

Part: SPLICE PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT WING LEADING EDGE SPLICE PLATE CORRODED WS 482. THE SPLICE PLATE WAS REPAIRED IAW ENGINEERING DOCUMENT 47224REA35.

Part: STIFFENER — CORRODED (BS 522) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

MAIN DECK FLOORBEAM HORIZONTAL STIFFENER IS CORRODED AT BS 522 RBL 42-55 . REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02 SECTION 9 AND ENGINEERING DOCUMENT 47224FAB76.

Part: STRINGER — CORRODED (BS 1131) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER 36R JUST AFT OF BS 1131 IS CORRODED ON OTBD SIDE. REMOVED AND REPLACED THE CORRODED STRINGER IAW SRM 53-00-03 AND SRM 51-40-02.

Part: FRAME — CORRODED (BS 676) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO INTERNAL FRAME AT BS 676, LBL 40 HAS CORROSION. REMOVED AND REPLACED IAW SRM 51-40-02.

Part: BEAR STRAP — CORRODED (BS 539) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFTER REMOVING THE FORWARD LOWER CORNER SEAL DEPRESSOR ON THE FORWARD LOWER CARGO DOOR, FOUND CORROSION ON THE BEAR STRAP COMMON TO THE SEAL DEPRESSOR. BLENDED CORROSION IAW SRM 53-00-15. BLEND WAS OUT OF LIMITS. REPAIRED IAW ENGINEERING DOCUMENT 47224REA12 REV IR.

Part: SKIN — CORRODED (BS 1085) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON STRINGER 29R AND ON THE INTERIOR SKIN BS 1085. BLENDED THE CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-01, FIGURE 101. REMOVED AND REPLACED UPPER AND LOWER SHEAR TIE IAW SRM 51-40-02 SECTION 7.

Part: SKIN — CORRODED (RT MLG) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT MLG UPLOCK TORSION BOX, UPPER OTBD, AFT MOUNTING FLANGE SHIM HAS CORROSION AND A SUPPORT ANGLE IS BENT. REWORKED SUPPORT ANGLE, FABRICATED A SHIM IAW DRAWING 149T6972.

Part: PRESSURE DECK — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

PRESSURE DECK BETWEEN BS 1263 - 1285, LBL 10 IS CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-00, FIGURE 101. FABRICATED A NEW PRESSURE DECK AND INSTALLED.

Part: STRINGER — CORRODED (BS 1395-1417) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER 35L CORRODED BETWEEN BS 1395 - 1417. REPAIRED THE STRINGER IAW SRM 53-00-03, FIGURE 201, REPAIR 2.

Part: INTERCOSTAL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

INTERCOSTAL BS 1329-1351 LBL 26 FOUND TO BE CORRODED. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, FIGURE 1. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02 AND DRAWING 146T5000.

Part: INTERCOSTAL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

INTERCOSTAL AT BS 1329 - 1351, LBL 7 CORRODED. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, FIGURE 101. INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02, AND DRAWING 146T5000.

Part: INTERCOSTAL — CORRODED (BS 686) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 686, LBL 88 - RBL 88. STRUCTURE UNDER FLOOR DRAIN IS CORRODED. REMOVED AND REPLACED THE DRAIN PAN SUPPORT INTERCOSTALS IAW ENGINEERING DOCUMENT 47224FAB13, AND SRM 51-40-02, PARAGRAPH 7D.

Part: PRESSURE PANEL — CORRODED (BS 1153-1175) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

PRESSURE PLATE BS 1153 - 1175 CORRODED AROUND NUT PLATES. REMOVED CORROSION FROM THE PRESSURE PLATE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. R & R IAW DRAWING 146T5000.

Part: DRAIN — CORRODED (BS 686) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO DRAIN PAN AT BS 686, LBL 77 - 88 IS CORRODED. REMOVED AND REPLACED THE DRAIN PAN IAW SRM 51-40-02, PARAGRAPH 9B.

Part: INTERCOSTAL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BS 1329-1351 LBL 33 INTERCOSTAL CORRODED. BLENDED THE CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED THE INTERCOSTAL IAW DRAWING 146T5000 AND SRM 51-40-02.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LOWER AIR LOAD RIB AT WING STATION 470 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED THE RIB IAW DRAWING 114T2203 REVISION A AND SRM 51-40-02.

Part: SEAL — WORN (FUSELAGE) · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. WHILE INSTALLING THE RIGHT ELEVATOR CABLE THROUGH THE AFT PRESSURE BULKHEAD, FOUND CABLES TO BE RUBBING ON THE AIR SEAL PASS THROUGH. REMOVED AND REPLACED AIR SEAL IN ACCORDANCE WITH ENGINEERING DOCUMENT 47224REA46 FOR MAJOR REPAIRS OF SYSTEM.

Part: SEAL — WORN (FUSELAGE) · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. WHILE RIGGING RUDDER CABLES, FOUND CABLES TO BE RUBBING ON AIR SEAL. REMOVED AND REPLACED AIR SEAL IN ACCORDANCE WITH ENGINEERING DOCUMENT 47224REA46 FOR MAJOR REPAIRS OF SYSTEM.

Part: FLOOR SUPPORT — CORRODED (BS 1021) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO FLOOR SUPPORT CRACKED BS 1021, LBL 63. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO STRINGER 38R CORRODED BETWEEN STATION 1395-1417. REMOVED AND REPLACED DAMAGED STRINGER WITH REPAIRED STRINGER AND REPAIR STRINGER SPOILER IN ACCORDANCE WITH SRM 51-40-02 AND 53-00-03.

Part: BEAR STRAP — CORRODED (BS 1307) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO BS 1307 BEAR STRAP CORRODED BETWEEN STRINGERS 35 - 36R. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. FABRICATED A NEW BEAR STRAP IAW DRAWING 1460201 AND REPLACED IAW SRM 51-40-02.

Part: BEAR STRAP — CORRODED (BS 1350) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BEAR STRAP CORRODED BS 1350 BETWEEN STRINGERS 34 - 35R. REPAIRED IAW ED 47224REA43 AND SRM 53-00-51, FIGURE 201, REPAIR 14.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO SHEAR TIE CORRODED STATION 1373 JUST INBOARD OF STRINGER 35L. BLENDED AREAS. FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH SRM 51-10-02. ORIGINAL THICKNESS = .040", REMAINING THICKNESS = .030".

Part: STRINGER — CORRODED (BS 1562) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER 31L AND STRINGER CLIP CORRODED AT BS 1562. BLENDED CORROSION AND FOUND OUT OF LIMITSIAW SRM 51-60-03. FABRICATED A NEW STRINGER IAW SRM 53-00-03. INSTALLED NEW SECTION IN ACCORDANCE WITH B767 SRM 53-00-03 AND B767 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1120-1208) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1120-1208, LBL 88 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW DRAWING 368-53-16-94351, ENGINEERING DOCUMENT 47224FAB52, AND SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 999-1120) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 999-1230, LBL 88 SEAT TRACK CORRODED IN SEVERAL SPOTS. THE SEAT TRACK REPLACED IAW ENGINEERING DOCUMENT 47224FAB68, SRM 53-00-52 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1285-1307) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOOR SUPPORT BETWEEN BS 1285 - 1307 LBL 11 IS CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PARAGRAPH 7.

Part: FLOOR SUPPORT — CRACKED (BS 1285-1307) · airframe 90,241 hrs · 43,067 cycles

FLOOR SUPPORT BETWEEN BS 1285 - 1307, LBL 6 IS CRACKED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW ENGINEERING DOCUMENT 47224FAB34.

Part: STRUCTURE — CORRODED (BS 1294) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CLOSEOUT WEB BUILD UP BOX STRUCTURE BS 1295 BETWEEN LBL 11 AND 6 FOUND CORRODED. REMOVED AND REPLACED CORRODED STRUCTURE IAW SRM 51-40-02 PARAGRAPH 7.

Part: FLOORBEAM — CORRODED (BS 1329) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO, BS 1329 FLOORBEAM BETWEEN LBL 88 AND RBL 88 CORRODED IN SEVERAL SPOTS. THE FLOORBEAM WAS BLENDED. REPAIRED IAW ENGINEERING DOCUMENT 47224REA37.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO FOUND ON STRINGER 35L AT STATION 1329. CORROSION ON STRINGER 35L AT STATION 1329. 100% MATERIAL LOSS - OUT OF LIMITS IN ACCORDANCE WITH SRM 53-00-03. REMOVED AND REPLACED STRINGER 35L STATION 1329-1362 IN ACCORDANCE WITH SRM 53-00-03 REPAIR 2.

Part: FITTING — CORRODED (BS 1395-1460) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO STATION 1219-1582 LOADING SYSTEM BASES CORRODED BETWEEN LBL 54-77. REMOVED AND REPLACED TWO CLS FITTINGS. FABRICATED FITTINGS IAW ENGINEERING DOCUMENT 47224FAB63.

Part: SUPPORT — CORRODED (BS 1307) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION AT BS 1307, RBL 78 ON BOTTOM STRUCTURE OF MAIN DECK CARGO FLOOR AND HYDRAULIC LINE SUPPORT. REMOVED AND REPLACED IAW ENGINEERING DOCUMENT 47224FAB15 & DRAWING 146T5160.

Part: STRINGER — CORRODED (BS 1461-1518) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. BULK CARGO COMPARTMENT STRINGER 35R IS CORRODED FROM STATION 1461-1518. REMOVED STAMPED STRINGER AND REPLACED WITH REPAIR STRINGERS AND REPAIR SPLICES IAW SRM 53-60-03.

Part: FITTING — CORRODED (BS 1021) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1021 BETWEEN LBL 11 AND RBL 11 LOADING SYSTEM BASE CORRODED. REMOVED AND REPLACED THE BASE PLATE IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1395-1417) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1395 - 1417, LBL 88 FLOOR SUPPORT CORRODED. CORROSION OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 51-40-02 PAGE 9.

Part: SEAT TRACK — CORRODED (BS 1406-1483) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1406-1483 LBL 88 SEAT TRACK IS CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02, PAGE 7 PARAGRAPH 7D AND DRAWING 368-53-16-94405.

Part: SEAT TRACK — CORRODED (BS 576-610) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 610 - 576, RBL 11 SEAT TRACK IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02 PAGE 7 PARAGRAPH 7D AND DRAWING 368-53-16-94405.

Part: SKIN — CORRODED (BS 1228-1307) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SKIN CORRODED BS 1228 - 1307 BETWEEN STRINGERS 36L-36R. REPAIRED IAW SRM 51-40-02 AND 304858.14.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT WING LEADING EDGE SPAR HAS CORROSION AT BOTTOM APPROXIMATELY OSS 695. REMOVED CORROSION IAW SRM 57-20-10, FIGURE 101. REPAIRED IAW ENGINEERING DOCUMENT 47224REA30, TREATED AND PRIMED IAW AMM 51-21-00, AND 51-21-04.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION AROUND NUTPLATE ON LEADING EDGE OF RIGHT WING AUXILIARY TRACK LOWER ATTACH STRUT. BLENDED THE CORROSION IAW SRM 57-41-09, FIGURE 101, DETAIL IV. FOUND TO BE OUT OF SRM LIMITS. REMOVED AND REPLACED THE RIB IAW SRM 51-40-02, PAGE 9.

Part: SEAT TRACK — CORRODED (BS 610-654) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 610 - 654, LBL 11 SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02, PAGE 7, PARAGRAPH 7D, AND ENGINEERING DOCUMENTS 47224FAB66 AND 47224FAB37.

Part: SEAT TRACK — CORRODED (BS 1210-1406) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO, BS 1210 - 1406 LBL 77 SEAT TRACK CORRODED IN SEVERAL SPOTS. SEAT TRACK HAS BEEN FABRICATED IAW DRAWING 368-53-16-94405 AND ENGINEERING DOCUMENT 47224FAB04.AND INSTALLED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 788-889) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO STATION 788 - 889 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW 368-53-13-91031 AND SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. INTERCOSTAL IS CORRODED AT STATION 1285-1305 AT RIGHT BUTT LINE 4. REMOVED INTERCOSTAL AND REMOVED CORRODED SECTION .015 MATERIAL LOSS. FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH SRM 53-00-04. INSTALLED NEW INTERCOSTAL IN ACCORDANCE WITH SRM 51-40-02 PARAGRAPH 7.

Part: STRINGER — CORRODED (BS 1417) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BULK CARGO BAY STRINGER 36R IS CORRODED AFT OF BS 1417 FRAME ON INBOARD VERTICAL LEG. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03, REPAIR 2, AND SRM 53-60-03, DETAIL 1.

Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT WING LEADING EDGE BOTH UPPER AND LOWER AIRLOAD RIBS CORRODED RWS 638. FOUND TO BE OUT OF LIMITS IAW SRM 57-41-09, FIGURE 101. REMOVED AND REPLACED RIBS IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1461) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO, BS 1461 FLOORBEAM BETWEEN LBL 88 AND RBL 88 CORRODED IN SEVERAL SPOTS. THE FLOORBEAM WAS REPAIRED IAW 47224REA37.

Part: SEAT TRACK — CORRODED (BS 672) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 672 RBL 54 SEAT TRACK CORRODED. REMOVED AND REPLACED IAW SRM 51-40-02 PAGE 7 PARAGRAPH 7D.

Part: SEAT TRACK — CORRODED (BS 685-810) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 685 - 810, LBL 77 SEAT TRACK CORRODED IN SEVERAL SPOTS. BLENDED CORRODED IAW SRM 53-00-52 - BLENDS WITHIN LIMITS. AREA NOT WITHIN LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINEERING DOCUMENT 47224FAB16 REVISION IR.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. OUTBOARD STRINGER-TIE AT STATION 698 STRINGER 38R IS CORRODED. REPLACED STRINGER TIE AT STATION 698 STRINGER 38R IN ACCORDANCE WITH ENGINEERING DOCUMENT 47224FAB49 REV 1R. INSTALLED IN ACCORDANCE WITH SRM 51-40-02.

Part: SKIN — CORRODED (BS 1080) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. CORROSION FOUND ON SKIN BS 1080 BETWEEN STRINGERS 34-35R. REPAIRED THE SKIN CORROSION IAW ENGINEERING DOCUMENT 47224REA41 AS A CAT B REPAIR.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

WHILE REMOVING THE RIGHT LEADING EDGE STRUCTURE, FOUND CORROSION ON THE LOWER FRONT SPAR AT WS 810. REMOVED CORROSION, BLENDED AREA WITHIN LIMITS IAW SRM 57-20-01, FIGURE 101, DETAIL III. REPAIRED IAW ED 47224REA30. TREATED PRIMED AREA IAW AMM 51-21-04 AND 51-21-00.

Part: STRINGER — CORRODED (BS 1351) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER 34R, BS 1351 CORRODED. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03. REPAIRED THE STRINGER IAW SRM 53-00-03 AND ED 47224REA43.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT WING LEADING EDGE LOWER SPAR CORRODED RWS 641. REMOVED CORROSION, BLENDED AREA. FOUND AREA TO BE OUT OF LIMITS. REPAIRED IAW ENGINEERING DOCUMENT 47722REA30.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT WING LEADING EDGE SPAR CORRODED RWS 540. REMOVED CORROSION, BLENDED AREA WITHIN LIMITS IAW SRM 57-20-10 FIGURE 101 DETAIL III. TREATED AND PRIMED AREAS IAW AMM 51-21-04, 51-21-00.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. INTERCOSTAL IS CORRODED BETWEEN STATION 1263-1285 AT LEFT BUTT LINE 20. REMOVED AND REPLACED INTERCOSTAL AT STATION 1263-1285 LEFT BUTT LINE 12 OF AFT LOWER CARGO IN ACCORDANCE WITH SRM 51-40-02 AND DRAWING 146T5000.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. INTERCOSTAL LABELED "INTERCOSTAL SEC 46 STATION 1395-1417 CRACKED THRU FASTENER HOLE. REMOVED AND REPLACED INTERCOSTAL AT STATION 1395-1417 RIGHT BUTT LINE 54 IN ACCORDANCE WITH SRM 51-40-02 AND DRAWING 452T3279.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO INTERCOSTAL IS CORRODED AT LOWER SURFACE BETWEEN STATION 1263-1286 LEFT BUTT LINE 22. INTERCOSTAL BETWEEN STATION 1263-1285 AT LEFT BUTT LINE 22 WAS FOUND TO BE OUT OF LIMITS. INSTALLED NEW INTERCOSTAL IN ACCORDANCE WITH SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO INTERCOSTAL IS CORRODED LOWER SURFACE BETWEEN STATION 1263-1285 RIGHT BUTT LINE 22. INTERCOSTAL BETWEEN STATION 1263-1285 AT RIGHT BUTT LINE 22 FOUND TO BE OUT OF LIMITS. INSTALLED NEW INTERCOSTAL IN ACCORDANCE WITH SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. CORROSION ON INTERCOSTALS AT STATION 1263-1285, STRINGER 34L-35L. INTERCOSTALS FOUND TO BE OUT OF LIMITS BETWEEN 1263-1285 STRINGER 34L-35L. INSTALLED NEW INTERCOSTALS IN ACCORDANCE WITH SRM 51-40-02.

Part: DOOR FRAME — CORRODED (BS 1417) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CARGO DOOR FORWARD ENCLOSURE CORRODED 21 TO 34 INCHES FROM FLOOR LEVEL. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW AMM 51-00-53. FABRICATED NEW WEB.

Part: SPLICE PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT WING LEADING EDGE LOWER SPLICE PLATE UPPER SURFACE CORRODED IN MULTIPLE SPOTS FROM RWS 420 TO 718. REMOVED AND REPLACED LOWER SPLICE IAW ENGINEERING DOCUMENT 47224REA21.

Part: DOOR SILL — CORRODED (BS 1417-1461) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BULK CARGO DOOR CUTOUT LOWER SILL HAS CORROSION ON FORWARD INBOARD CORNER. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-40-02 PARAGRAPH 4-7.

Part: INTERCOSTAL — CORRODED (BS 1263-1351) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON INTERCOSTALS AT RBL 80 ABOVE AFT LOWER CARGO DOOR. BLENDED CORROSION ON INTERCOSTALS IAW SRM 53-00-16. 100% MATERIAL LOSS. MATERIAL FOUND TO BE OUT OF LIMITS. FABRICATED NEW INTERCOSTALS AND REPLACED IAW DRAWING 453T1539 51-40-02.

Part: SKIN — CORRODED (BS 1086) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION FOUND ON THE SKIN BS 1086 JUST ABOVE STRINGER 34R. REPAIRED IAW REA 47224REA41.

Part: SKIN — CORRODED (BS 1080-1094) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON THE FUSELAGE INTERIOR SKIN FROM STRINGER 33 TO 35R. BS 1085. REPAIRED IAW ENGINEERING DOCUMENT 4722REA41.

Part: FLOORBEAM — CORRODED (BS 1285) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOORBEAM BS 1285 LBL 10 - 33 CORRODED. FOUND TO BE OUT LIMITS. INSTALLED A NEW FLOORBEAM IAW SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1170) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER 37R, BS 1170 IS CORRODED. REMOVED AND REINSTALLED THE STRINGER IAW SRM 53-00-01.

Part: STRINGER CLIP — CORRODED (BS 1086) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON FORWARD SIDE OF STRINGER CLIP AT STRINGER 33R BS 1086. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 PAGE 7 PARAGRAPH 7D.

Part: FAILSAFE — CORRODED (BS 1219-1395) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FAILSAFE UNDER RBL 88 SEAT TRACK BETWEEN BS 1263 - 1317 IS CORRODED, REMOVED AND REPLACED FAILSAFE IAW SRM 51-40-02 AND ENGINEERING DOCUMENT 47224FAB44.

Part: STRINGER — CORRODED (BS 1562) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON STRINGER 27R AT BS 1562. FOUND TO BEOUT OF LIMITS IAW SRM 53-00-03. INSTALLED A NEW STRINGER IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. STRINGER TIE CRACKED AT STATION 390 STRINGER 32L. REMOVED AND REPLACED STRINGER TIE AT STATION 390 STRINGER 32L IN ACCORDANCE WITH SRM 51-40-02 PARAGRAPH 7.

Part: STRINGER — CORRODED (BS 390-472) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

A CORRODED STRINGER AT BS 434-456, STRINGER 32L. INSTALLED REPAIRS IAW SRM 53-00-03 REPAIR 2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. INTERCOSTAL IS CORRODED OUT OF LIMITS AT STATION 1263-1285 RIGHT BUTT LINE 15. MATCH DRILLED NEW INTERCOSTAL IN ACCORDANCE WITH SRM 51-40-05. INTERCOSTAL TO BE INSTALLED ON NR 69086-000-2749.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. INTERCOSTAL IS CORRODED OUT OF LIMITS AT STATION 1285-1307 AT LEFT BUTT LINE 36. RECEIVED AND MATCH DRILLED NEW INTERCOSTAL IN ACCORDANCE WITH SRM 51-40-05. INTERCOSTAL WILL BE INSTALLED ON NR 2749.

Part: ATTACH BRACKET — CRACKED (BS 1043) · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1043 BETWEEN LBL 11 AND RBL 11 INTERCOSTAL ATTACH BRACKET IS CRACKED. INSTALLED REPLACEMENT INTERCOSTAL ATTACH BRACKET IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. UPPER CARGO SEAT TRACK LEFT BUTT LINE 54 STATION 668-788 HAS CORROSION THAT IS OUT OF LIMITS IN SEVERAL AREAS. REMOVED AND REPLACED SEAT TRACK LEFT BUTT LINE 54 STATION 668-788 IN ACCORDANCE WITH SRM 51-40-02 PAGE 7 PARAGRAPH 7D AND IN ACCORDANCE WITH DRAWING 368-53-16-94405. PRIMED AND PAINTED IN ACCORDANCE WITH SRM 51-20-00 PAGE 1 PARAGRAPH 1C.

Part: STRINGER — CORRODED (BS 1086-1098) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION UNDER STRINGER CLIP AT STRINGER 39L, BS 1086. STRINGER CLIP AREA OF STRINGER 39L HAS PIECE MISSING, FOUND TO BE OUT LIMITS IAW SRM 51-00-03. REPAIRED THE STRINGER IAW SRM 51-00-03.

Part: FLOORBEAM — CORRODED (BS 1197) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO, BS 1197 LBL 88 - RBL 88 FLOORBEAM IS CORRODED IN SEVERAL SPOTS. REPAIRED THE FLOORBEAM IAW SRM 53-0051, ENGINEERING DOCUMENTS 47224REA31 AND 47224REA32.

Part: STRINGER — CORRODED (BS 390-434) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BS 412 - 434 STRINGER 35R, CORROSION AROUND STRINGER FASTENERS COMMON TO THE FUSELAGE SKIN. REPAIRED DAMAGED SECTION OF THE STRINGER IAW SRM 53-00-03, FIGURE 201, AND ENGINEERING DOCUMENT 47224REA38.

Part: STRINGER CLIP — CORRODED (BS 434) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER CLIP AT BS 434, STRINGER 29L IS CORRODED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1470) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1470 AT LBL 65-11 FLOORBEAM CORRODED IN SEVERAL SPOTS. FABRICATED A CHANNEL IAW SRM 51-30-01 AND DOC 452T3259.

Part: WEB — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BULK CARGO DOOR AFT ENCLOSURE WEB CORRODED FROM FLOOR LEVEL UP 34 INCHES. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-0015. FABRICATED A NEW WEB IAW DRAWING 146T1281-4.

Part: SHEAR TIE — CORRODED (BS 434) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO SHEAR TIE AT BS 434 BETWEEN STRINGERS 32 - 33L IS CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-40-02 PARAGRAPH 4E AND 4D.

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT WING LEADING EDGE LOWER SPLICE PLATE IS CORRODED AT LWS 435. REMOVED AND REPLACED THE SPLICE IAW AMES 47224REA17.

Part: STRINGER — CORRODED (BS 1303) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SKIN BULGED AROUND FASTENERS BS 1303, STRINGER 31L. THE STRINGER WAS FOUND TO BE 100% OUT OF LIMITS IAW SRM 53-00-03, FIGURE 101. FABRICATED AND INSTALLED A NEW STRINGER IAW DRAWING 146T3001 AND SRM 53-00-03 REPAIR 2.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION FOUND AT LEFT WING LOWER SKIN INBOARD OF THE OUTBOARD SKATE ANGLE. BLENDED AND REMOVED CORROSION IAW ENGINEERING DOCUMENT 47224REA39.

Part: SEAT TRACK — CORRODED (BS 1406-1502) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO LBL 77, BS 1406-1502 SEAT TRACK IS CORRODED IN SEVERAL SPOTS. CORROSION REMOVED IAW SRM 51-40-02, 53-10-52, 53-00-51, AND ENGINEERING DOCUMENT 47224FAB16, STEP 5 0-3.

Part: SHEAR TIE — CORRODED (BS 434) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO SHEAR TIE CORRODED AT BS 434, STRINGERS 33 - 34L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-40-02 PARAGRAPH 4C AND 4D.

Part: SEAT TRACK — CORRODED (BS 620) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 620, LBL 33 SEAT TRACK CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-52 FIGURE 101. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINEERING DOCUMENT 47224FAB04.

Part: FLOORBEAM — CORRODED (BS 1502) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO FLOORBEAM , BS 1502 BETWEEN RBL 11 AND 33 CORRODED IN SEVERAL SPOTS. REPAIRED THE FLOORBEAM IAW ENGINEERING DOCUMENT 47224REA34 AND DOCUMENT NUMBER CS-22216-011.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO STRINGER 36L IS CORRODED AT LOWER SURFACE BETWEEN STATION 1263-1285. REMOVED CORRODED SECTION OF STRINGER 36L AT STATION 1250-1300 AND REPLACED WITH FILLER STRINGER AND SPLICE IN ACCORDANCE WITH SRM 53-00-03.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. STRINGER SPLICE AT STATION 434 STRINGER 32R IS CORRODED. REMOVED AND REPLACED STRINGER SPLICE AT STATION 434 STRINGER 32R IN ACCORDANCE WITH SRM 53-30-03 REPAIR 1 DETAIL IV.

Part: BEAM — CRACKED (NR 2 PYLON) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

NUMBER 2 PYLON LOWER BEAM UNDER RIGHT HYDRAULIC BAY DOOR CHAFED AND CRACKED AT FORWARD END. REMOVED AND REPLACED THE BEAM IAW SRM 51-40-02 AND DRAWING 313T1380.

Part: STRINGER — CORRODED (BS 1241-1263) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON STRINGER AND SPLICE 39R AT BS 1241 - 1263. REMOVED CORRODED, DAMAGED SECTION OF THE STRINGER AND REPLACED WITH FILLER SECTION SPLICES IAW SRM 53-00-02.

Part: STRINGER — CORRODED (BS 1351-1373) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER 35L STATION 1351-1373 CORRODED. STRINGER 35L FOUND TO BE OUT OF LIMITS STRINGER SPLICE WAS INSTALLED ON NR 2786.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO DOOR CUTOUT FORWARD LOWER CORNER HAS CORROSION AROUND FASTENERS. REMOVED CORROSION, AND FOUND TO BE OUT OF LIMITS. REPAIRED IAW REA 47224REA12.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO INTERCOSTAL IS CORRODED AT LOWER SURFACE BETWEEN STATION 1285 - 1307 RIGHT BUTT LINE 12. REMOVED AND REPAIRED INTERCOSTAL AT STATION 1285 RIGHT BUTT LINE 12 IN ACCORDANCE WITH SRM 51-40-02 SECTION 7D.

Part: FRAME — CORRODED (BS 1320) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SUB-FRAME CORRODED THROUGH AT BS 1320, RBL 85. REMOVED AND REPLACED THE SUB-FRAME IAW DRAWING 146T5160 AND ENGINEERING DOCUMENT 47224FAB09.

Part: STRINGER — CORRODED (BS 390-434) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO STRINGER 28L BETWEEN BS 412-434 IS CORRODED. REMOVED THE STRINGER AND REPAIRED IAW SRM 53-00-03 AND ENGINEERING DOCUMENT 47224REA20. AIRCRAFT GROUNDED.

Part: SEAT TRACK — CORRODED (BS 922-1021) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 922-1021 LBL 74.75 SEAT TRACK CORRODED IN SEVERAL SPOTS. BLENDED AND FOUND TO BE WITHIN LIMITS IAW SRM 53-00-52 FIGURE 101. REMOVED AND REPLACED SEAT TRACK AT STATION 999-1065 LEFT BUTT LINE 74.75 IN ACCORDANCE WITH AMES ENGINEERING DOCUMENT 47224FAB42 AND B767 SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1120-1208) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1120-1208, LBL 77 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINEERING DOCUMENT 47224FAB16 AND SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1070-1208) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO, BS 1120-1208 RBL 11 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINEERING DOCUMENT 47224FAB16 AND SRM 51-40-02.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. STRINGER-TIE CORRODED AT STATION 434 STRINGER 27L. FABRICATED NEW STRINGER CLIP IN ACCORDANCE WITH ENGINEERING DOCUMENT 47224FAB50. INSTALLED NEW PART IN ACCORDANCE WITH SRM 51-40-02.

Part: STRINGER — CORRODED (BS 412-134) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO STRINGER 27L BETWEEN BS 412-434 IS CORRODED. REMOVED THE STRINGER AND REPAIRED IAW SRM 53-00-03 AND ENGINEERING DOCUMENT 47224REA20. ACFT GROUNDED.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. STRINGER-TIE CORRODED AT STATION 434 STRINGER 28L. FABRICATED NEW STRINGER CLIP IN ACCORDANCE WITH ENGINEERING DOCUMENT 47224FAB50. INSTALLED NEW PART IN ACCORDANCE WITH SRM 51-40-02.

Part: INTERCOSTAL — CORRODED (BS 1324-1351) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RBL 16, BS 1324 - 1351, INTERCOSTAL HAS AREAS OF CORROSION. REMOVED NUT PLATES AND BLENDED AREAS OF CORROSION ON INTERCOSTAL. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04 FIGURE 101 DETAIL 2. REPLACED THE INTERCOSTAL.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO STRINGER 35L IS CORRODED AT STATION 1351. STRINGER 35L AT STATION 1351 FOUND TO BE OUT OF LIMITS. STRINGER SPLICE REPAIR INSTALLED IN ACCORDANCE WITH SRM 53-00-03.

Part: DOOR SILL — CORRODED (BS 522-544) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

ANGLE UNDER FORWARD LOWER CARGO DOOR CUT OUT MAIN SILL AT BS 544 IS CORRODED ON THE FLANGE THAT ATTACHES TO THE CLOSE OUT WEB. REMOVED CORRODED SILL CLIP, FABRICATED NEW SILL CLIP FROM 7075-0, NEW CLIP WAS HEAT TREATED 7075-76, CLIP WAS TREATED, PRIMED, PAINTED, AND INSTALLED IN ACCORDANCE WITH B767 SRM 51-40-02 AND BOEING DRAWING 143T5003.

Part: SHEAR TIE — CORRODED (BS 434) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE CORRODED AT BS 434 STRINGER 33 - 34R. REMOVED AND REPLACED THE SHEAR TIE IAW DRAWING 140T2102.

Part: STRINGER SPLICE — CORRODED (BS 1285) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER SPLICE 39R CORRODED BS 1285. REPLACED IAW SRM 53-40-02.

Part: FLOORBEAM — CORRODED (BS 620) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION FOUND ON FLOORBEAM AT BS 620. REPAIRED IAW SRM 51-40-02, PARAGRAPH 4B, AND PARAGRAPH 7D.

Part: STRINGER — CORRODED (BS 390-466) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BS 412 - 434, STRINGER 33R, CORROSION AROUND FASTENERS IN STRINGER COMMON TO THE SKIN. REMOVED AND REPLACED THE STRINGER IAW SRM 53-00-03, FIGURE 201, AND ENGINEERING DOCUMENT 47224REA38, STEPS 15-22.

Part: WEB — CORRODED (BS 544-610) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION FOUND ON WEB AT BS 544 - 566, LBL 24 - 42. REMOVED, FABRICATED, AND INSTALLED A NEW WEB IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 632) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION FOUND OF CHORD OF FRAME FLOORBEAM BS 632. REPLACED THE CHORD LBL 44 TO RBL 44 IAW SRM 51-40-02, PARAGRAPH 4 AND 7.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. FOUND SKIN CORRODED AT STATION 412-434 STRINGER 35R. REPAIRED DAMAGED AREA IN ACCORDANCE WITH SRM 53-00-01 AND ENGINEERING DOCUMENT 47224REA40.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO STRINGER 37L IS CRACKED AT STATION 1300 INBOARD LOWER SURFACE. REMOVED AND REPLACED STRINGER 37L AT STATION 1298-1268.5 IN ACCORDANCE WITH SRM 53-00-03 REPAIR 2.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO STRINGER 39L IS CORRODED BETWEEN STATION 1250-1307. CORROSION FOUND TO BE OUT LIMITS IN ACCORDANCE WITH SRM 53-00-03 FIGURE 101. INSTALLED FABRICATED STRINGER SECTION 39L STATION 1250-1274 AND 1274-1307 IN ACCORDANCE WITH SRM 53-00-03.

Part: STRINGER CLIP — CORRODED (BS 1086) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON FORWARD SIDE OF STRINGER CLIP AND STRINGER 39L AT BS 1086. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1021-1120) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1021-1120, LBL 54 SEAT TRACK IS CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINEERING DOCUMENT 47224FAB42.

Part: STRINGER — CORRODED (BS 1350-1373) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BS 1350-1373 STRINGER 37R CORRODED. CUTOUT AND SPLICED IN NEW SECTION OF STRINGER IAWSRM 53-00-03.

Part: INTERCOSTAL — CORRODED (BS 1241-1261) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

TOP OF INTERCOSTAL BETWEEN BS 1241 AND 1261, STRINGERS 29 AND 30R IS CORRODED BETWEEN THE CAP ANGLES. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02 SECTION 7 PARAGRAPH D.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFTER REMOVING PANEL 566JT, FOUND CORROSION ON THE AFT SPAR OF THE LEFT WING OTBD FLAP AT OTEF 92.75. REPLACED TRAILING EDGE FLAP.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFTER REMOVING SEALANT, FOUND CORROSION AROUND EDGES OF REPAIR ON THE RT HORIZONTAL STAB AT FRONT SPAR HSS 171. REMOVED AND REPLACED THE SKIN PANEL IAW SRM 51-40-02.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. STRINGER CORRODED AT STATION 434-456 STRINGER 37L. REMOVED AND REPLACED DAMAGED SECTION STRINGER 37L STATION 390-478 IN ACCORDANCE WITH ENGINEERING DOCUMENT 47224REA38 AND SRM 53-00-03.

Part: FLOOR SUPPORT — CORRODED (BS 522-544) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON FLOOR SUPPORT RBL 16.5, BS 522 - 544. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 PART 7A AND ENGINEERING DOCUMENT 47224FAB43. AIRCRAFT GROUNDED.

Part: INTERCOSTAL — CORRODED (BS 1219-1241) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON POWER ROLLER INTERCOSTALS RBL 33 BS 1219 TO 1241. CORROSION ON POWER DISTRIBUTION UNIT INTERCOSTALS. BLENDED CORROSION LOST .047 FROM .075 AND LOST .032 FROM .075.

Part: SHEAR TIE — CORRODED (BS 1263) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

ALL SHEAR TIE CORRODED AT BS 1263 STRINGER 35L-35R. CORROSION BLENDED OUT OF LIMITS. REPLACED SHEAR TIE IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1120-1208) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1120 - 1208, LBL 33 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINEERING DOCUMENT 47224FAB04, AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 610-632) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOOR SUPPORT BETWEEN BS 610 - 632 RBL 16.4 IS CORRODED. FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED A REPLACEMENT FLOOR SUPPORT IAW SRM 51-40-02 AND SRM 51-40-05.

Part: FLOORBEAM — CORRODED (BS 1307) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO FLOORBEAM, BOTTOM FLANGE, AT BS 1307, RBL 52 FOUND CORRODED. REPAIRED THE FLOORBEAM IAW ENGINEERING DOCUMENT 47224REA33.

Part: STRINGER — CORRODED (BS 390-488) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO STRINGER 38L BETWEEN BS 412-434 IS CORRODED. THE STRINGER WAS REPLACED IW SRM 53-00-03 FIGURE 201 AND ENGINEERING DOCUMENT 47224REA20 STEPS 15-21. AIRCRAFT GROUNDED

Part: SIDEWALL SUPPORT — CORRODED (BS 1395-1417) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SIDEWALL SUPPORT AT BS 1395 - 1417 STRINGER 30R FOUND CORRODED. REMOVED AND REPLACED SIDEWALL SUPPORT IAW SRM 51-40-02, SECTION 4, PARAGRAPH 4B, AND SECTION 7 PARAGRAPH D.

Part: FLOOR SUPPORT — CORRODED (BS 1241-1263) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOOR SUPPORT FROM BS 1241 - 1263 LBL 33 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-43-01.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO STRINGER 37R IS CORRODED AT STATION 1263 LOWER OUTBOARD. REMOVED AND REPLACED CORRODED SECTION OF STRINGER 37R AT STATION 1252-1275 IN ACCORDANCE WITH SRM 53-00-03 REPAIR 2.

Part: FRAME — CORRODED (BS 1131) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON THE LOWER SURFACE OF THE FRAME BS 1131, UNDER ROLLER TRAY ASSEMBLY IN CLOSE PROXIMITY TO STRINGER 33L. CORROSION FOUND TO BE OUT OF LIMITS IAW 53-00-07 FIGURE 101. REMOVED AND REPLACED IAW DRAWING 451T1203.

Part: SEAT TRACK — CORRODED (BS 1410-1518) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO SEAT TRACK RBL 77 BS 1500 CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINEERING DOCUMENT 47224FAB16 & SRM 51-40-02.

Part: FRAME — CORRODED (BS 1175) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO FRAME AT BS 1175 STRINGER 24L BELOW ROLLER TRAY CORRODED AT NUT PLATE. FOUND TO BE OUT OF LIMITS. REPLACED THE FRAME IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1208-1406) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO, BS 1208-1406 RIBL 77 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINEERING DOCUMENT 47224FAB04 AND SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1210-1406) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO, BS 1210 - 1406 LBL 33 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINGEERING DOCUMENT 47224FAB04 AND SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1241-1263) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOOR SUPPORT FROM BS 1241-1263 CORRODED RBL 33. BLENDED AND IS OUT OF LIMITS IAW SRM 53-00-51. INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOOR SUPPORT CORRODED BS 1263-1285. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-43-01.

Part: STRINGER — CORRODED (BS 1303-1306) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SKIN BULGED AROUND FASTENERS BS 1303, STRINGER 30L. REMOVED AND REPLACED CORRODED SKIN IAW SRM 51-40-02 PAGE 4-B AND PAGE 9.

Part: PRESSURE PANEL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LBL 4 THROUGH RBL 16, BS 1329 - 1351 PRESSURE PLATE ASSEMBLY HAS AREAS OF CORROSION. FABRICATED PRESSURE PLATE FROM DRAWING 452T2002.

Part: MOUNT — CORRODED (BS 1175) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOOR MOUNT BS 1175 STRINGER 37 - 39L CORRODED. REMOVED AND REPLACED THE MOUNT.

Part: STRINGER SPLICE — CORRODED (BS 434) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT SIDE OF STRINGER SPLICE 38R CORRODED AT BS 434. REMOVED AND REPLACED THE STRINGER SPLICE IAW DRAWING 140T0115.

Part: SEAT TRACK — CORRODED (BS 1120-1208) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1120-1208 RBL 54 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINEERING DOCUMENT 47224FAB04 AND SRM 51-40-02. AIRCRAFT GROUNDED.

Part: LINE — CORRODED (PNEUMATIC SYS) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

PNEUMATIC LINE FUSELAGE BS 1396 CORRODED ON SURFACE. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS IAW 20-10-09, SECTION 4.2D, TABLE FIGURE 804.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO SHEAR TIE IS CORRODED AT STATION 1285 BETWEEN STRINGER 39R AND STRINGER 38R. REMOVED SHEAR TIE. BLENDED OUT CORROSION. FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH SRM 53-00-03 AND INSTALLED SHEAR IN ACCORDANCE WITH SRM 53-00-03 AND SRM 51-70-40.

Part: SEAT TRACK — CORRODED (BS 1208-1406) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1208-1406 RBL 54 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINEERING DOCUMENT 47224FAB03.

Part: SEAT TRACK — CORRODED (BS 1560-1600) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO SEAT TRACK RBL 11 BS 1560-1600 CORRODED. AIRCRAFT GROUNDED. REMOVED AND REPLACED SEAT TRACK IAW ED 47224FAB03.

Part: SEAT TRACK — CORRODED (BS 1208-1406) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1208-1406 RBL 11 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW ENGINEERING DOCUMENT 47224 AND SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 698) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE IS CORRODED AT STRINGER 38L AND BS 698. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02 AND REA 47224FAB07.

Part: STRINGER — CORRODED (BS 434-456) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORRODED STRINGER 30L AT BS 434-456. REMOVED DAMAGED SECTION OF STRINGER 30L AND INSTALLED A REPAIR IAW SRM 53-00-03 REPAIR 2.

Part: STRINGER — CORRODED (BS 434-456) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SURFACE CORROSION AND PAINT MISSING AT BS 434-456, STRINGER 39L ON THE UPPER SURFACE OF A STRINGER. REMOVED & REPLACED THE STRINGER IAW SRM 53-00-03 FIG 201 REPAIR 2. REA 47224REA20 STEPS 22-29. AIRCRAFT GROUNDED.

Part: SKIN — CORRODED (BS 654-698) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON LOWER SKIN ADJACENT TO THE MARKER BEACON ANTENNA AT BS 660-678. CORROSION FOUND TO BE OUT OF LIMITS, REMOVED TWO AREAS THAT WERE OUT OF LIMITS AND REPAIRED SKIN IAW SRM 53-00-01 REPAIR 14 AND REA 47224REA27. AIRCRAFT GROUNDED.

Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO SHEAR TIE AT BS 1285 IS CORRODED BETWEEN STRINGERS 39 - 38L. REMOVED AND REPLACED THE SHEAR TIE IAW 53-00-03.

Part: STRINGER — CORRODED (BS 434) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO STRINGER 39L, BS 434. REMOVED AND REPLACED STRINGER IAW SRM 53-00-03, FIGURE 201 REPAIR 2. REA 47224REA20 STEPS 22-29.

Part: RETAINER — CORRODED (BS 742) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FRAME FITTING AT FORWARD SIDE OF BS 742 COMMON TO THE SEAT TRACK AT RBL 33 HAS CORROSION. REMOVED CLIP AND FABRICATED NEW CLIP. INSTALLED NEW CLIP IAW SRM 51-20-02 PARAGRAPH 7D AND REA 47224FAB22 REVISION IR.

Part: INTERCOSTAL — CORRODED (BS 522-544) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION FOUND ON INTERCOSTAL AT BS 522 - 544 AT LBL 7. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 434) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE CORRODED FUSELAGE BS 434 STRINGERS 37R-38R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4B.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. INTERCOSTAL BETWEEN STATION 610-632 AT LEFT BUTT LINE 7 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED INTERCOSTAL AT STATION 610-632 AT LEFT BUTT LINE 7 IN ACCORDANCE WITH SRM 51-40-02.

Part: SKIN — CORRODED (BS 1518) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO BS 1518 STRINGER 24R. SKIN CORRODED. PERFORMED DAMAGED SKIN REPAIR IAW REA 47224REA23.

Part: STRINGER CLIP — CORRODED (BS 1502) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO BS 1502 STRINGER 26L IS CORRODED. STRINGER REPLACED IAW SRM 53-00-03.

Part: SHEAR TIE — CORRODED (BS 1373) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE BS 1373 RBL 14 IS CORRODED. REPLACED IAW SRM 51-40-02, AND DRAWING 146T1214 REVISION D.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. INTERCOSTAL STATION 588-610 RIGHT BUTT LINE 33 HAS CORROSION AROUND NUT PLATE. REMOVED AND REPLACED CORRODED INTERCOSTAL STATION 588-610 RIGHT BUTT LINE 33 IN ACCORDANCE WITH SRM 51-40-02 PARAGRAPH 7.

Part: FLOOR SUPPORT — CORRODED (BS 544-566) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON FLOOR SUPPORT BETWEEN BS 544-566, RBL 33.15. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 PARAGRAPH 7.

Part: INTERCOSTAL — CORRODED (BS 610-632) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

INTERCOSTAL BETWEEN BS 610-632 AT LBL 33.8 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-40-02 SECTION 7.

Part: FAILSAFE — CORRODED (BS 1370) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FAIL SAFE STRAP CORRODED AT STATION 1263 AT INTERSECTION OF AFT LOWER CARGO DOOR SILL AND EXTENDING 6 INCHES UPWARD. REMOVED CORROSION. CORROSION FOUND TO BE OUT OF LIMITS. REPLACED FAIL SAFE STRAP ALL IN ACCORDANCE WITH B767 SRM 53-00-15.

Part: SHEAR TIE — CORRODED (BS 1285) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO SHEAR TIE IS CORRODED AT BS 1285 BETWEEN STRINGERS 39L - 39R. REMOVED THE SHEAR TIE. BLENDED SURFACE CORROSION REMOVED. FOUND TO BE WITHIN LIMITS. INSTALLED THE SHEAR TIE IAW SRM 58-00-03.

Part: FITTING — CHAFED (BS 1055) · airframe 90,241 hrs · 43,067 cycles

LEFT MLG WHEEL WELL SIDE STRUT SWIVEL FITTING CHAFED. REPAIRED IAW ENGINEERING DOCUMENT REA 47224REA28.

Part: STIFFENER — CORRODED (BS 588-610) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOOR SUPPORT AT BS 588-610 LBL 37 HAS CORROSION AROUND NUTPLATE. REMOVED AND FABRICATED A REPLACEMENT IAW SRM 51-40-02 PARAGRAPH 4.

Part: SHEAR TIE — CORRODED (BS 698) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. SHEAR TIE CORRODED AT STRINGER 37R - 38R AND BS 698. INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4B.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. STRINGER CORRODED UNDER SPLICE PLATE BETWEEN STATION 1285 AND 1307 STRINGER 34L. BLENDED MATERIAL WITH 100% MATERIAL LOSS AND IS OUT LIMITS IN ACCORDANCE WITH SRM 53-00-03 DETAIL II. REPLACED CORRODED SECTION AND REPAIRED IN ACCORDANCE WITH SRM 53-00-03.

Part: SHEAR TIE — CORRODED (BS 654) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO INTERNAL GUSSET AT BS 654 BETWEEN STRINGERS 37L AND 38L HAS CORROSION. INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4B.

Part: INTERCOSTAL — CORRODED (BS 1021) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1021 BETWEEN RBL 54 - 77 INTERCOSTAL CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW DRAWING 368-53-00-95455. AIRCRAFT GROUNDED.

Part: SPAR — CORRODED (BS 1015) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT WING LEADING EDGE BS 1015 LOWER END OF LEADING EDGE SPAR WEB CORRODED. REMOVED CORROSION AREA FOUND TO BE OUT OF LIMITS. REPAIRED IAW ENGINEERING DOCUMENT 47224 REA 29.

Part: SKIN — CORRODED (BS 632-654) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO INTERNAL SKIN AT BS 632-654 STRINGER 34 - 35L HAS CORROSION. FOUND CORROSION TO BE OUT OF LIMITS, CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-00-01 REPAIR 12 FIGURE 201.

Part: INTERCOSTAL — CORRODED (BS 610-632) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

INTERCOSTAL BETWEEN BS 610-632 AT RBL 31.5 IS CORRODED OUT OF LIMITS. REMOVED AND INSTALLED A NEW INTERCOSTAL IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 566-588) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON FLOOR SUPPORT RBL 26 AT BS 566 - 588. REMOVED AND REPLACED THE THE FLOOR SUPPORT AND FOUND IT TO BE OUT OF LIMITS IAW SRM 51-40-02 PARAGRAPH 407, SRM 51-40-05.

Part: SKIN — CORRODED (BS 434-460) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SKIN FOUND TO BE CORRODED. REMOVED DAMAGED PORTION OF SKIN AND INSTALLED REPAIR IAW SRM 53-00-01 FIGURE 201 REPAIR 3.

Part: SHEAR TIE — CORRODED (BS 676) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON SHEAR TIE LOCATED BETWEEN STRINGERS 39L AND 39R, BS 676. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-50-02 SECTION 7.

Part: SHEAR TIE — CORRODED (BS 1307) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO BS 1307, SHEAR TIE BETWEEN 36-37R CORRODED. REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 742 SHEAR TIE BETWEEN 38 - 39L CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED A NEW SHEAR TIE IAW DRAWING 140T2102.

Part: STRINGER — CORRODED (BS 434-456) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORRODED STRINGER 29L BS 434-456. REMOVED DAMAGED SECTION OF THE STRINGER AND INSTALLED REPAIR IAW SRM 53-00-03 REPAIR 2.

Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 742 SHEAR TIE BETWEEN STRINGER 36 - 37R CORRODED. BLENDED THE CORRODED AREA AND FOUND TO BE OUT OF LIMITS. FABRICATED A NEW SHEAR TIE. HEAT TREATED IAW DRAWING 14T2102 AND 5602 REVISION AF.

Part: STRINGER CLIP — CORRODED (BS 456) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER CLIP AT BS 456, STRINGER 29L IS CORRODED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 AND DRAWING 140T2101-3001.

Part: STRINGER — CORRODED (BS 720-742) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION AT STRINGER 35R AND BS 720-742. REMOVED CORRODED SECTION OF STRINGER AND INSTALLED A NEW STRINGER FILLER AND SPLICES IAW SRM 53-00-03 FIGURE 201 REPAIR 2 AND ENGINEERING DOCUMENT 4722REA14.

Part: FLOOR SUPPORT — CORRODED (BS 610-632) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOOR SUPPORT AT BS 620-632, RBL 26 HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION IAW DRAWING 143T209REV AND FABRICATED A REPLACEMENT NUT PLATE SHIM IAW SRM 51-20-12 PARAGRAPH 8.

Part: FLOOR SUPPORT — CORRODED (BS 522-544) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION FOUND THE FLOOR SUPPORT RBL 33 AT BS 522-544. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 SECTION 7.

Part: SKIN — CORRODED (BS 544-610) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SKIN CORRODED AROUND ANTENNA AT STRINGER 37 - 38L AND BS 566 - 588. BLENDED AREAS FOUND TO BE OUT OF LIMITS REPAIRED IAW REA47224REA19 AND SRM 53-00-01 REPAIR 14 FIGURE 201.

Part: SEAT TRACK — CORRODED (BS 1208-1339) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO, BS 1208-1339, RBL 33 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1339-1406) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1339-1406 RBL 33 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE FOR SEAT TRACK IAW SRM 51-40-02. AIRCRAFT GROUNDED.

Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 742 SHEAR TIE BETWEEN STRINGER 37 - 38L CORRODED. FABRICATED A NEW SHEAR TIE IAW DRAWING 14T02102. INSTALLED THE SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4B-7D.

Part: SKATE ANGLE — CORRODED (NR 1 PYLON) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

NR 1 PYLON OUTBOARD SKATE ANGLE INBOARD SURFACE HAS SEVERAL BROKEN AND RUSTED NUTPLATES AND SURFACE CORROSION ALONG THE ENTIRE LENGTH. REMOVED CORROSION ALONG THE LENGTH OF OUTBOARD SKATE ANGLE. STARTING MATERIAL .125. BLENDED .077. MATERIAL LEFT .118. WITHIN LIMITS IAW SRM 54-51-71. REMOVED 20" OF SKATE FITTING PER 47224REA22. REINSTALLED NUTPLATES IAW SRM 51-40-02. LEAK CHECK WILL BE PERFORMED ON NONROUTINE 2748.

Part: FRAME — CRACKED (BS 1153) · airframe 90,241 hrs · 43,067 cycles

AFTER REMOVING THE UPPER J CHORD FROM FRAME AT BS 1153 IN THE AFT LOWER CARGO, FOUND THE FRAME WEB CRACKED AT LBL 21. REPAIRED IAW SRM 51-20-13,

Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. FORWARD LOWER CARGO BS 742 SHEAR TIE AND WEB AFT SIDE BETWEEN STRINGER 36L AND 37L CORRODED. FABRICATED NEW SHEAR TIE IAW DRAWING 14T2102, FROM 7075-0, PO# 0082134 .O63. INSTALLED NEW SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4B.

Part: SEAT TRACK — CORRODED (BS 1208-1339) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1208-1339 RBL 33 SEAT TRACK CORRODED IN SEVERAL SPOTS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02.

Part: FAILSAFE — CORRODED (BS 544) · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFTER REMOVING WEB FOR REPAIR ON NONROUTINE 0759, FOUND CORROSION ON THE FAIL SAFE STRAP AT BS 544 BETWEEN STRINGERS 34 AND 35R. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS. REPAIRED BLENDED AREA BY REINFORCEMENT IN ACCORDANCE WITH REA 47224REA24.

Part: STRINGER — CORRODED (BS 687-710) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER CORRODED UNDER THE DOME NUT SPACER AT BS 699, STRINGER 32L. REMOVED DAMAGED SECTION OF THE STRINGER AND INSTALLED REPAIR TO STRINGER IAW SRM 53-00-03 REPAIR 2.

Part: WEB — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BS 1263-1285 CENTER TOP PLATE TORQUE BOX PLATE HAS SEVERAL AREAS OF CORROSION. BLEND THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07. DRILLED NEW WEB IAW SRM 51-40-05.

Part: FLOOR SUPPORT — CORRODED (BS 1540) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FLOOR SUPPORT AT BS 1540 LBL 15 IS CRACKED AND CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DRAWING 146T5004.

Part: SHEAR TIE — CORRODED (BS 1562) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE AT BS 1562 BETWEEN STRINGERS 29 AND 30L IS CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02 AND DRAWING 146T2104-661.

Part: STRINGER — CORRODED (BS 782) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO, BS 782 STRINGER 39R CORRODED. INSTALLED A NEW STRINGER IAW SRM 51-40-02 PARAGRAPH 4D. AIRCRAFT GROUNDED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. LOWER FLOORBEAM WEB CRACKED AT STATION 1373 BETWEEN STRINGER 35R AND 36R. CUTOUT AND REMOVED DAMAGED PART OF WEB. FABRICATED AND INSTALLED FILLER AND DOUBLER IN ACCORDANCE WITH SRM 51-70-13 FIGURE 1 TYPICAL WEB REPAIR.

Part: STRINGER — CORRODED (BS 753) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BS 764 - 783 STRINGER 37R CORRODED. AIRCRAFT GROUNDED. REPAIRED THE STRINGER IAW REA14 AND SRM 53-00-03 FIGURE 201 REPAIR 2.

Part: SHEAR TIE — CORRODED (BS 764) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 764 SHEAR TIE CORRODED BETWEEN STRINGERS 37 AND 38L. INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4B AND 7D. AIRCRAFT GROUNDED.

Part: STRINGER — CORRODED (BS 765) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 765 STRINGER 37L CORRODED. REPAIRED THE STRINGER IAW 47225REA14 AND SRM 53-00-03. AIRCRAFT GROUNDED.

Part: BRACKET — CRACKED (BS 249) · airframe 90,241 hrs · 43,067 cycles

LOWER ATTACH BRACKET FOR PANEL 432CL CRACKED AT FORWARD END. REMOVED AND REPLACED LOWER ATTACH BRACKET FOR PANEL 432CL IN ACCORDANCE WITH B767 SRM 51-40-02 PARAGRAPH 7.

Part: STRINGER — CORRODED (BS 764-785) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 764 - 785 STRINGER 37L CORRODED. CUT OUT CORRODED AREA OF STRINGER AND INSTALLED A REPAIR FILLER AND SPLICE IAW SRM 53-00-03 REPAIR 2 AND REA 47224REA14. AIRCRAFT GROUNDED.

Part: STRINGER — CORRODED (BS 782) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 782 STRINGER 34R CORRODED. REPAIRED THE STRINGER IAW SRM 53-00-03 REPAIR 2 AND 47224REA14.

Part: BEAM — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT WING LEADING EDGE LWS 414 HAS CORROSION ON LOWER LEADING EDGE. REMOVED, FABRICATED AND REPLACED NOSE BEAM WEB IAW SRM 51-40-02 AND DRAWING 114T2300.

Part: SKIN — CORRODED (BS 742-785) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 765-770 APPROXIMATELY, CORRODED INBOARD SIDE OF STRINGER 37L. REPAIRED AREA IAW 47223REA 18 AND SRM 53-00-01 FIGURE 201. AIRCRAFT GROUNDED.

Part: WEB — CORRODED (BS 1263-1285) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFTER REMOVAL OF WEB AT BS 1263-1285, STRINGER 34L FROM THE AFT LOWER CARGO, FOUND WEB TO BE CORRODED. WEB AND STIFFENERS CORRODED 100%. OUT OF LIMITS IAW SRM 53-00-04, FIGURE 101. FABRICATED A NEW WEB AND STIFFENERS IAW DRAWING 146T5000 AND INSTALLED.

Part: SHEAR TIE — CORRODED (BS 360) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION AT BS 390, STRINGER 37 - 39R. REMOVED SHEAR TIE. CLEANED CORROSION. FABRICATED SHEAR TIE IAW 51-40-02, PARAGRAPH 4 AND PARAGRAPH 7. AIRCRAFT GROUNDED.

Part: PAN — CORRODED (BS 785) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 785 BULKHEAD OUTBOARD SIDE STRINGER 38R CORRODED. REMOVED AND REPLACED IAW SRM 51-40-02. AIRCRAFT GROUNDED.

Part: SHEAR TIE — CORRODED (BS 764) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 764 SHEAR TIE BETWEEN STRINGER 35R & 36R CORRODED. INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4D.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO AT STATION 1518 STRINGER 34R CORRODED. REMOVED AND EXFOLIATED STRINGER SECTION AND REPLACED IN ACCORDANCE WITH SRM 53-00-03.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. FORWARD LOWER CARGO STATION 764 SHEAR TIE (FORMER) CORRODED BETWEEN STRINGER 38L AND 39L. FABRICATED NEW PORT IN ACCORDANCE WITH REA DOCUMENT 47224FAB08. INSTALLED NEW SHEAR TIE IN ACCORDANCE WITH SRM 51-40-02 PARAGRAPH 7D AND 4B.

Part: STRINGER CLIP — CRACKED (BS 1702) · airframe 90,241 hrs · 43,067 cycles

STRINGER CLIP 2L AT BULKHEAD BS 1702 FOUND CRACKED. REPLACED THE STRINGER CLIP IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 767) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 764 SHEAR TIE CORRODED BETWEEN STRINGERS 36 AND 37L. INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4B. AIRCRAFT GROUNDED.

Part: SHEAR TIE — CORRODED (BS 1373) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE AT BS 1373 STRINGER 36 - 37R, HAS BARE METAL. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02 PARAGRAPH VII.

Part: STRINGER — CORRODED (BS 643-665) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER CORRODED UNDER DOME NUT SPACER AT BS 658 STRINGER 29L. REMOVED & REPLACED THE STRINGER IAW SRM 53-00-03 AND 47224REA25.

Part: BEAM — CORRODED (LT MLG WW) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION IN LEFT WHEEL WELL, WING BUTT LINE 159 UPPER PANEL SUPPORT BEAM HAS SEVERAL AREAS OF CORROSION FORWARD & AFT, INBOARD SIDE, TO INCLUDE SUPPORT LINK. CORROSION OUT OF LIMITS. REMOVED AND REPLACED PANEL SUPPORT BEAM IAW SRM 51-40-02 PARAGRAPH 4, PARAGRAPH 7, PARAGRAPH 10.

Part: RIB — CORRODED (RT WING) · airframe 90,241 hrs · 43,067 cycles

RIGHT WING LEADING EDGE WS 400-446 NOSE RIB CRACKED. ACFT GROUNDED. INSTALLED A NEW NOSE RIB IAW DRAWING 114T2230 AND SRM 51-40-02 PAGE 7 PARAGRAPH 717.

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT WING LEADING EDGE WS 1102 IS BULGING ON THE UPPER SURFACE. INSTALLED A NEW LEADING EDGE SPLICE PLATE IAW SRM 57-40-02 AND REA 4722HREA13 . AIRCRAFT GROUNDED

Part: TORQUE BOX — CORRODED (BS 1268-1285) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON THE LEFT TORQUE BOX PLATE, BS 1268 - 1285. THE PANEL WAS BLENDED OUT OF LIMITS IAW SRM 51-10-00. FABRICATED A NEW PANEL IAW DRAWING 146T5000.

Part: ATTACH FITTING — CORRODED (LT WING LE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT WING LEADING EDGE LOWER AIRLOAD RIB AT WS 635 IS CORRODED ON PANEL ATTACH FLANGE. REMOVED AND REPLACED LOWER AIRLOAD RIB IAW SRM 51-40-02. AIRCRAFT GROUNDED.

Part: SPLICE — CORRODED (BS 1065-1100) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON THE SPLICE FITTING THAT IS LOCATED BETWEEN STRINGER 23L AND 24L AND EXTENDS FROM BS 1065 TO 1100. REMOVED AND REPLACED THE LONGERON CHORD, WEBB, AND BRACKET AT STATION 1065 TO 1100 BETWEEN STRINGER 23L AND 24L IN ACCORDANCE WITH B767 SRM 51-40-02.

Part: FRAME — CORRODED (BS 1109) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON THE LOWER SURFACE OF THE FRAME BS 1109 UNDER ROLLER TRAY ASSEMBLY STRINGER 33L. BLENDED OUT OF LIMITS IAW 53-00-07. REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 588) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. FORWARD LOWER CARGO SHEAR TIE CORRODED AT FUSELAGE STATION 588 STRINGER 37L THRU 38L. FABRICATED NEW SHEAR TIE FOR STATION 588 STRINGER 37L THRU 38L IN ACCORDANCE BOEING DRAWING 140T8102.

Part: SHEAR TIE — CORRODED (BS 544) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BAY SHEAR TIE CORRODED AT BS 544 STRINGER 37-38L. FABRICATED A NEW SHEAR TIE IAW DRAWING 140T8102.

Part: CARGO TRACK — CORRODED (BS 1407-1605) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CARGO TRACK RBL 54 BS 1600 IS CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 53-00-52 & ENGINEERING DOCUMENT 47224RFAB03 STEPS 17-24.

Part: WEB — CRACKED (BS 1263) · airframe 90,241 hrs · 43,067 cycles

BS 1263 WEB HAS CRACKED AREAS AROUND ATTACH HOLES. FABRICATED WEB IAW DRAWING 453T1936-5, AND AMM 51-24-04.

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT WING, TRAILING EDGE, RWS 255.4 TO 375.8, UPPER SPOILER SUPPORT BEAM AFT EDGE CORROSION. BLENDED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-51-02 FIG 101. REMOVED AND INSTALLED NEW SUPPORT BEAM IAW DRAWING 654T0391.

Part: STRINGER CLIP — CORRODED (BS 456) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER CLIP CORRODED AT BS 456, STRINGER 32L. FABRICATED A NEW STRINGER CLIP IAW BOEING DRAWING 140T2101.

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT WING LEADING EDGE UPPER SPLICE PLATE IS CORRODED AT LWS 500. REMOVED SECTION OF UPPER WING SPLICE FROM LWS 412.2 TO 512.3. INSTALLED SPLICE SECTION IAW AMES ENGINEERING DOCUMENT REA 47224REA15.

Part: STRINGER CLIP — CORRODED (BS 434) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER CLIP AT BS 434, STRINGER 32L HAS ELONGATED HOLES. FABRICATED NEW STRINGER CLIP IAW DRAWING 140T2101.

Part: CARGO TRACK — CORRODED (BS 1580-1600) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CARGO TRACK LBL 54 BS 1580-1600 CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 53-00-52 AND ENGINEERING DOCUMENT 47224FABO3.

Part: CARGO TRACK — CORRODED (BS 1595-1575) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CARGO TRACK LBL 11 BS 1595 - 1575 IS CORRODED. REMOVED AND REPLACED THE CARGO TRACK AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. R & R THE CARGO TRACK IAW CEA 47234FAB03.

Part: STRINGER — CORRODED (BS 1562) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO BS 1562, STRINGER 26L IS CORRODED. REMOVED CORRODED SECTION OF STRINGER AND REPLACE WITH SPLICE IAW SRM 53-00-03. AIRCRAFT GROUNDED.

Part: ATTACH BRACKET — CRACKED (NR 7 SLAT) · airframe 90,241 hrs · 43,067 cycles

NR 7 SLAT LOWER TRAILING EDGE TO COVE ATTACH ANGLES CRACKED 27, 50, 61, AND 72 INCHES FROM OUTBOARD END. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 57-40-02 PARARGRAPH 7D, 4B, AND DRAWING 114T3166. AIRCRAFT GROUNDED.

Part: ATTACH FITTING — CORRODED (BS 1395) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION AROUND CARGO WING ATTACH PLATE BS 1395 LBL 54 - 66. REPLACED AND REINSTALLED WING ATTACH PLATE IAW SRM 51-40-02. AIRCRAFT GROUNDED.

Part: CARGO TRACK — CORRODED (BS 1560-1600) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CARGO TRACK LBL 33 BS 1560-1600 CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 53-00-52 & ENGINEERING DOCUMENT 47224FAB03.

Part: CARGO TRACK — CORRODED (BS 1475-1600) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CARGO TRACK RBL 33 BS 1475 - 1600 CORRODED. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 53-00-52 & ENGINEERING DOCUMENT 47224FAB03.

Part: STRINGER — CORRODED (BS 1513) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO BS 1513 STRINGER 28L IS CORRODED. REMOVED CORRODED SECTION OF STRINGER AND REPLACED IAW SRM 53-00-03. AIRCRAFT GROUNDED

Part: STRINGER — CORRODED (BS 434-463) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

A CORRODED STRINGER AT BS 434-456, STRINGER 31L. REMOVED DAMAGED SECTION OF STRINGER AND INSTALLED A REPAIR TO THE STRINGER IAW SRM 53-00-03 REPAIR 2. ACFT GROUNDED.

Part: STRINGER SPLICE — CORRODED (BS 785) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

ON REMOVAL OF STRINGER 37R, FOUND STRINGER TIE TO BE CORRODED AT BS 785 BULKHEAD. STRINGER SPLICE FITTING WAS LOCATED AND DRILLED IAW SRM 51-40-05.

Part: STRINGER — CORRODED (BS 1461) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO BS 1461 STRINGER 32L END FITTING IS CORRODED. CUT OUT CORRODED SECTION AND REPLACED IAW SRM 53-60-03.

Part: CLOSEOUT PANEL — CORRODED (BS 522-544) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO CLOSE OUT PANEL WEB BS 522-544 RBL 33-42 IS CORRODED ON EDGE AROUND THREE FASTENERS. FABRICATED A NEW CLOSE OUT PANEL WEB.

Part: INTERCOSTAL — CORRODED (BS 588) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON CEILING INTERCOSTAL JUST FORWARD OF BS 588 AT FORWARD CARGO DOOR CUTOUT UPPER FORWARD CORNER. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-40-02 AND SRM 51-30-02 SECTION 2 DETAIL VII.

Part: CEILING PANEL — CORRODED (BS 544-588) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SEVERAL AREAS OF CORROSION ON CARGO CEILING SUPPORT CLIP NUTS AT CARGO DOOR CUTOUT AREA. REMOVED, FABRICATED AND INSTALLED 8 CEILING PANELS DUE TO CORROSION BEING OUT OF LIMITS IN ACCORDANCE WITH B767 SRM 51-30-01 SECTION 7 AND SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE CORRODED AT BS 742, STRINGER 34L. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: SPAR WEB — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON THE REAR SPAR WEB AT THE OUTBOARD END OF LEFT WING. BLENDED CORROSION IAW SRM 57-20-10 FIGURE 101 DETAIL III. REPAIRED IAW ENGINEERING DOCUMENT REA 47224REA11.

Part: SHEAR TIE — CORRODED (BS 1175) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO FLOOR AT BS 1175 STRINGER 37 - 38L CORRODED SHEAR TIE. BLENDED THE CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-51.

Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 742 SHEAR TIE BETWEEN STRINGERS 34L AND 35L CORRODED. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. AFT LOWER CARGO FLOOR AT STATION 1175 STRINGER 37L-38L CORRODED TEAR STRAP. STATION 1175 SHEAR TIE, TEAR STRAP CORRODED. BLENDED CORROSION LOST .016 FROM .5. .34 MATERIAL LEFT OVER. OUT OF LIMITS IN ACCORDANCE WITH SRM 53-00-51. NO CORROSION NOTED ON STRAP, ONLY SHEAR TIE.

Part: WEB — CORRODED (PYLON) · airframe 90,241 hrs · 43,067 cycles

WEB CRACKED ON FORWARD END OF NUMBER 2 PYLON WHERE ANTI-ICE DUCT ATTACH BRACKET ATTACHES AT PASS THRU AREA. REMOVED FORWARD SECTION OF ANTI-ICE DUCT AND WEB. REPLACED WEB IAW DRAWING 311T1510 AND SRM 51-40-02. REINSTALLED DUCT IAW AMM 20-11-00 PARAGRAPH B-2.

Part: STRINGER — CORRODED (BS 742) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO, BS 742 STRINGER 34L IS CORRODED. REMOVED DAMAGED PORTION OF STRINGER AND INSTALLED A REPAIR IAW SRM 53-00-03 REPAIR 2.

Part: ATTACH ANGLE — CORRODED (BS 785) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

PANEL ATTACH ANGLE AT BS 785.9 RBL 13 SPLIT ON EDGE. REMOVED AND REPLACED ATTACH ANGLE IAW SRM 51-40-05, 51-40-02. AIRCRAFT GROUNDED.

Part: WEB — CORRODED (BS 1455) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

UPPER CARGO BS 1461 LBL 65 WEB ON TOP OF FLOORBEAM CORRODED. BLENDED AREA IAW SRM 53-00-51. FOUND TO BE OUT OF LIMITS. FABRICATED A NEW PART IAW DRAWING 94339.

Part: TEE FITTING — CORRODED (BS 654) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO INTERNAL FRAME BS 654 FROM LBL 48 TO RBL 48 HAS CORROSION. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02.

Part: SKIN — CORRODED (BS 588-610) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON SKIN AT STRINGER 36 - 37R AND BS 588 - 610. REPAIRED IAW SRM 53-00-01, REPAIR 14 PAGE 201 STEPS 1-17.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. CORROSION ON SHEAR CLIP AT STRINGER 36R - 37R AT STATION 698. REMOVED AND REPLACED SHEAR TIE PER SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (BS 1726-1735) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION AROUND NUTPLATES ON APU INLET DOUBLER AT FORWARD END. CUT OUT DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW SRM 51-70-11.

Part: ANGLE — CORRODED (BS 1540) · airframe 90,241 hrs · 43,067 cycles

CORROSION AT BS 1540, CEILING TO AFT WALL ANGLES. . LEFT ANGLE IS OUT OF LIMITS. FABRICATED A NEW ANGLE AND INSTALLED IAW DRAWING 453T1616, SRM 51-40-02, AND 53-60-52.

Part: SHEAR TIE — CORRODED (BS 742) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FORWARD LOWER CARGO BS 742 SHEAR TIE BETWEEN STRINGERS 32L AND 33L CORRODED. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-40-02.

Part: STRINGER CLIP — CORRODED (BS 347) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

STRINGER CLIP AT BS 347 STRINGER 33L IS CORRODED BEYOND LIMITS. FABRICATED A NEW STRINGER CLIP IAW DRAWING 141T1225.

Part: TEE FITTING — CRACKED (BS 287) · airframe 90,241 hrs · 43,067 cycles

CRACK FOUND BY HIGH FREQUENCY EDDY CURRENT IN VERTICAL TEE FITTING BS 287 RBL 25 WATER LINE 172. REPAIRED IAW SRM 51-70-12.

Part: INTERCOSTAL — CRACKED (BS 770) · airframe 90,241 hrs · 43,067 cycles

CARGO STATION 770 RBL 54 TO 77 INTERCOSTAL AND WEB CRACKED. REMOVED AND REPLACED THE INTERCOSTAL AND WEB IAW DRAWING 91046 AND SRM 51-40-02 PARAGRAPH 7D.

Part: SHEAR TIE — CORRODED (BS 566) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON SHEAR TIE AT BS 566 AND STRINGER 38 - 39L. FOUND TO BE BEYOND LIMITS. FABRICATED A REPLACEMENT SHEAR TIE AND INSTALLED IAW SRM 51-40-02 PARAGRAPH 4 AND 7.

Part: SHEAR TIE — CORRODED (BS 544) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE CORRODED AT STRINGER 36L AND BS 544 - 566. BLENDED SHEAR TIE AND FOUND TO BE OUT LIMITS IAW SRM 53-00-07. FABRICATED NEW SHEAR TIE IAW DRAWING 140T2102. HEAT TREATED 5602 AND 5946. ALODINE PRIMED TOPCOAT IAW SRM 51-20-01 AND AMM 51-20-00 PARAGRAHP 7. INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 544) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION AT SHEAR TIE STRINGER 36 - 37L, BS 544. REPLACED THE SHEAR TIE IAW AMM 51-40-02 PARAGRAPH 7, PAGE 103.

Part: SHEAR TIE — CORRODED (BS 566) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON SHEAR TIE AT STRINGER 37 - 38L, BS 566. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 53-00-07 PG 102.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. SHEAR CLIP IS CORRODED AT STRINGER 37L AND STATION 698. BLENDED SHEAR TIE AND FOUND TO BE OUT OF LIMITS IN ACCORDANCE WITH SRM 53-00-07 FIGURE 101. FABRICATED NEW SHEAR TIE IN ACCORDANCE WITH DRAWING 141T1200. 7075-0 .050" PO# 0074510. HEAT TREAT IN ACCORDANCE WITH S602 REVISION AF 25AVL-2001, 5946 REVISION AF 25 JULY 2001 PSD E-409 JULY 2012. ALODINE PRIME TOPCOAT IN ACCORDANCE WITH SRM 51-21-00. INSTALLED IN ACCORDANCE WITH SRM 51-40-02 PARAGRAPH 7.

Part: SPLICE PLATE — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT WING LEADING EDGE UPPER SPLICE PLATE HAS SPOTS OF CORROSION AT LWS 875. CUT AND REMOVED LEFT WING LEADING EDGE UPPER SPLICE PLATE AT LWS 754.2 TO 884.7 IAW SRM 51-40-02. INSTALLED A NEW UPPER SPICE PLATE IAW ENGINEERING DOCUMENT REA 47224REA04.

Part: SUPPORT ANGLE — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON LEFT WING TRAILING EDGE, WING BUTT LINE 183 , UPPER PANEL SUPPORT TEE COMMON TO AUXILIARY SPAR WEB. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. FABRICATED NEW SUPPORT TEE AND REPLACED IAW SRM 57-51-02, 51-40-02.

Part: ANGLE — CORRODED (BS 1500) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION AT BS 1500, LEFT CEILING TO SIDEWALL SUPPORT. REMOVED CORROSION AND FOUND TO BE OUT LIMITS. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-40-02, 53-60-51. AIRCRAFT GROUNDED.

Part: ANGLE — CORRODED (BS 1417) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION AT BS 1417 RIGHT CEILING TO SIDEWALL SUPPORT ANGLE. REMOVED CORROSION AND FOUND OUT OF LIMITS. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-40-02, 53-60-51. AIRCRAFT GROUNDED.

Part: SPLICE — CORRODED (LT WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT WING LEADING EDGE LOWER SPLICE PLATE IS CORRODED AT LWS 636. REMOVED AND REPLACED SECTION OF LOWER SPLICE FROM WING LWS 581 TO 694 IAW AMES ENGINEERING DOCUMENT REA 47224 REA 05.

Part: SHEAR TIE — CORRODED (BS 588) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON SHEAR TIE AT STRINGER 36 - 37L AND BS 588. REPLACED THE SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 4.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. A SHEAR TIE MISSING PROTECTIVE COATING, POSSIBLE CORROSION, AT STATION 434, STRINGER 38L. INSTALLED SERVICEABLE SHEAR TIE AT STATION 434 STRINGER 38L IN ACCORDANCE WITH SRM 51-40-02 PARAGRAPH 4B.

Part: STRINGER CLIP — CORRODED (BS 1086) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON FORWARD SIDE OF STRINGER CLIP 36R AT BS 1086. FOUND TO BE OUT OF LIMITS. REPLACED STRINGER CLIP IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 566) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

SHEAR TIE CORRODED AT STRINGER 38 - 39R AND BS 566. INSTALLED A NEW SHEAR TIE IAW SRM 51-40-02 PARAGRAPH 7.

Part: KEELBEAM — CORRODED (BS 1004-1017) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT KEEL BEAM LOWER CHORD CORRODED ON UPPER AND LOWER SURFACES AT STATION 1013. BLENDED AREA IAW SRM 53-50-12. PERFORMED ULTRASONIC INSPECTION IAW NDTM PART 4. 51-00-10 PROCEDURE 2. HIGH FREQUENCY EDDY CURRENT IAW NDTM PART 6. 51-00-19. NO CORROSION INDICATION FOUND. REA 47224REA09 GENERATED AND COMPLIED WITH. ROTO PEENED BLENDED AREA IAW SRM 51-20-06. ALODINED, PRIMED AND TOP COATED IAW SRM 51-20-01. AIRCRAFT GROUNDED.

Part: KEELBEAM — CORRODED (BS 1006-1030) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT KEEL BEAM CORRODED AT BS 1025. BLENDED AREA IAW SRM 53-50-12. PERFORMED ULTRASONIC INSPECTION IAW NDTM PART 4. 51-00-10 PROCEDURE 2. HIGH FREQUENCY EDDY CURRENT IAW NDTM PART 6. 51-00-19. NO CORROSION INDICATION FOUND. REA 47224REA09 GENERATED AND COMPLIED WITH. ROTO PEENED BLENDED AREA IAW SRM 51-20-06. ALODINED, PRIMED AND TOP COATED IAW SRM 51-20-01. AIRCRAFT GROUNDED.

Part: KEELBEAM — CORRODED (BS 805-811) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON LOWER KEEL BEAM AT BS 808 RBL 9. BLENDED AREA IAW SRM 53-50-12. PERFORMED ULTRASONIC INSPECTION IAW NDTM PART 4 51-00-10 PARAGRAPH 2. HIGH FREQUENCY EDDY CURRENT SCAN IAW NDTM PART 6 51-00-19, NO CORROSION INDICATION FOUND IAW REA 47224REA09. GENERATED AND COMPLIED WITH. ROTO PEENED BLENDED AREA IAW SRM 51-20-06. ALODINED, PRIMED, AND TOP COATED IAW SRM 51-20-01.

Part: KEELBEAM — CORRODED · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION UNDER NUTPLATE ON KEEL BEAM AT BS 790 RBL 9. BLENDED AREA IAW SRM 53-50-12. PERFORMED ULTRASONIC INSPECTION IAW NDTM PART 4. 51-00-10 PROCEDURE 2. HIGH FREQUENCY EDDY CURRENT IAW SRM NDTM PART 6. 51-00-19. NO CORROSION INDICATION IAW REA 47224REA09 GENERATED AND COMPLIED WITH. ROTO PEENED BLENDED AREA IAW SRM 51-20-06. ALODINED, PRIMED, AND TOP COATED IAW SRM 51-20-01. FABRICATED AND INSTALLED NUT PLATE STRIP IAW SRM 53-50-12 REPAIR 2.

Part: SUPPORT — CORRODED (LT WING TE FLAP) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT WING TRAILING EDGE PANEL SUPPORT HAS CORROSION AND IS LOOSE. AIRCRAFT GROUNDED. REMOVED AND REPLACED THE PANEL SUPPORT IAW SRM 51-40-02 PARAGRAPH 7D AND 9B.

Part: PIVOT — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

HORIZONTAL STAB RIGHT PIVOT PIN HINGE FITTING INBOARD AND OUTBOARD BUSHINGS ARE CORRODED. REPAIRED THE FITTINGS IAW ENGINEERING DOCUMENT 47224REA08. ACFT GROUNDED.

Part: PIVOT — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

HORIZONTAL STAB LEFT PIVOT PIN HINGE FITTING INBOARD AND OUTBOARD BUSHINGS ARE CORRODED. REMOVED AND REINSTALLED THE PIVOT FITTING AFTER REWORK WAS COMPLETED IAW SRM 51-40-02 AND DWG 148T2740. ACFT GROUNDED.

Part: FLOOR SUPPORT — CORRODED (BS 1087) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION AROUND NUTPLATES ON THE LEFT SLOPING FLOOR SUPPORT AT FORWARD WALL BS 1087. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS FABRICATED A NEW FLOOR SUPPORT AND REPLACED IAW SRM 51-40-02, 53-00-53, AND DRAWING 453T1719. AIRCRAFT GROUNDED

Part: HINGE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

HORIZONTAL STAB RIGHT PIVOT PIN HINGE FITTING INBD AND OTBD BUSHINGS ARE CORRODED. REPAIRED THE FITTINGS IAW ED 47224REA08.

Part: HINGE — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

HORIZONTAL STAB LT PIVOT PIN HINGE FITTING INBD AND OTBD BUSHINGS ARE CORRODED. REMOVED AND REINSTALLED THE HORIZONTAL STAB PIVOT PIN FITTING IAW SRM 51-40-02 AND DRAWING 148T2740.

Part: ANGLE — CORRODED (BS 1540 FRAME) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

AFT LOWER CARGO BS 1540 STRINGER 31L FRAME ANGLE FORWARD OF OUTFLOW VALVE IS CORRODED. FOUND TO BE OUT OF LIMITS. FABRICATED A NEW FRAME ANGLE IAW DRAWING 146T50002. INSTALLED A NEW FRAME ANGLE IAW SRM 51-40-02 PARAGRAPH 7.

Part: SKIN PANEL — CORRODED (WING) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

FOUND CORROSION UNDER TRAILING EDGE SKIN PANEL AT WS 432 ON TOP OF WING. REMOVED CORROSION, REPAIRED AREA IAW REA 47224REA07. AIRCRAFT GROUNDED.

Part: BRACKET — CORRODED (AILERON) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

RIGHT OUTBOARD AILERON POSITION TRANSMITTER MOUNTING BRACKET HAS AREA OF CORROSION. FABRICATED AND INSTALLED MOUNTING BRACKET IAW DWG 251T1011 AND ENGINEERING DOCUMENT 47224FAB01.

Part: SKIN — CORRODED (BS 1582) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BS 1582 AT STRINGER 10R SKIN IS CORRODED. REPAIRED IAW SRM 53-00-1 REPAIR 1 AND ENGINEERING DOCUMENT REA 47224REA06, AIRCRAFT GROUNDED.

Part: SKIN — CORRODED (BS 1582) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

BS 1582, STRINGER 10R SKIN IS CORRODED. REPAIRED IAW SRM 53-00-01, REPAIR 1 AND ED 47224REA06.

Part: SIDEWALL SUPPORT — CORRODED (CARGO BAY) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

CORROSION ON AFT LOWER CARGO FORWARD WALL, CENTER AND CENTER RIGHT WALL SUPPORTS AND ANGLE BRACKET AT THE BOTTOM. FABRICATED NEW LOWER FORWARD LINE CLAMP IAW 272T4515 ASSEMBLY-7. . INSTALLED IAW SRM 51-40-02.

Part: DOUBLER — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 90,241 hrs · 43,067 cycles

LEFT STABILIZER TRAILING EDGE AT OUTBOARD END HAS DOUBLER CORRODED. FOUND OUT OF LIMITS. FABRICATED A NEW DOUBLER, AND REPLACED IAW SRM 55-10-13, 51-40-02, DWG 18371700.

Part: A/C PACK — FUMES (AC BAY) · airframe 90,101 hrs · 42,922 cycles

AIR CONDITIONING PACKS EMITTING FUMES INTO COCKPIT DURING CLIMB, CRUISE AND DESCENT.

Part: CIRCUIT BREAKER — POPPED (LANDING GEAR) · airframe 89,572 hrs · 42,199 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF.

Part: KEELBEAM — CORRODED (BS 955-1073) · airframe 86,691 hrs · 41,293 cycles

FUSELAGE AFT SECTION LOWER KEEL BEAM SHOWS CORROSION LBL 10 BS 955 - 1073.

Part: SKIN — DELAMINATED (HORIZONTAL STAB) · airframe 86,691 hrs · 41,293 cycles

RIGHT HORIZONTAL STABILIZER T/E PANEL DELAMINATED 40" STA 80.

Part: SKIN — DELAMINATED (HORIZONTAL STAB) · airframe 86,691 hrs · 41,293 cycles

RT HORIZONTAL STABILIZER T/E PANEL DELAMINATED 25" STA 120.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 86,691 hrs · 41,293 cycles

RT HORIZONTAL STABILIZER REAR SPAR UPPER SURFACE SKIN SHOWS CORROSION RBL 10 - 36 STA 127.465.

Part: FRAME — CORRODED (BS 1351) · airframe 86,691 hrs · 41,293 cycles

AFT CARGO BAY FRAME 46 INNER ANGLE SHOW CORROSION AT BS 1351 S32R.

Part: SKIN — CORRODED (BS 1406) · airframe 86,691 hrs · 41,293 cycles

AFT CARGO BAY SECTION 46 INNER SKIN LAP JOINT SHOWS CORROSION STA 1406, S-36R.

Part: KEELBEAM — CORRODED (BS 955-1073) · airframe 86,691 hrs · 41,293 cycles

FUSELAGE KEEL BEAM, AFT SECTION LOWER PART SHOWS CORROSION RBL 10, BS 955 - 1073.

Part: SKIN — DELAMINATED (HORIZONTAL STAB) · airframe 86,691 hrs · 41,293 cycles

LEFT HORIZONTAL STABILIZER T/E PANEL DELAMINATED STA 105

Part: STRINGER — CORRODED (BS 1400) · airframe 86,691 hrs · 41,293 cycles

AFT CARGO BAY SECTION 46 STRINGER SHOWS CORROSION BS 1400 S36R.

Part: BEAR STRAP — CORRODED (BS 1373) · airframe 86,691 hrs · 41,293 cycles

AFT CARGO BAY SECTION 46, DOUBLER, BEAR STRAP SHOWS CORROSION BS 1373 S33R.

Part: SKIN — CORRODED (BS 1582) · airframe 86,691 hrs · 41,293 cycles

FUSELAGE EXTERIOR UPPER HALF SKIN SHOWS CORROSION AT BS 1582.

Part: SKIN — CORRODED (BS 1351-1363) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPT INNER SKIN AND REPAIRING SHOWS CORROSION FROM STRINGER 38L TO STRINGER 38R FROM STA 1351 TO STA 1363, REF NR 0571.

Part: DUCT — CRACKED (COWL) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, NR 2 ENGINE CORE COWL RT- NR 428 FRAME VENT DUCT CRACKED 1, REF NR 0102.

Part: STRINGER — CORRODED (BS 1306) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT, STRINGER 34L SHOWS CORROSION AT STA 1306.

Part: SEAT TRACK — CORRODED (BS 1605) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, UPPER CARGO COMPARTMENT SEC 46 SEAT TRACK SHOWS CORROSION AT BS 1605, RBL 11.

Part: SEAT TRACK — CORRODED (BS 1605) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, UPPER CARGO COMPARTMENT SEC 46, SEAT TRACK SHOWS CORROSION AT BS 1605, LBL 33.

Part: STRINGER — CORRODED (BS 1362 S38R) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT. STRINGER 38R SHOWS CORROSION AT BS 1362.

Part: STRINGER — CORRODED (BS 1427 S37R) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, BULK CARGO COMPARTMENT. STRINGER 34R SHOWS CORROSION AT BS 1427.

Part: SEAT TRACK — CORRODED (BS 1605) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, UPPER CARGO COMPARTMENT SEC 46, SEAT TRACK SHOWS CORROSION AT BS 1605, LBL 33.

Part: SEAT TRACK — CRACKED (BS 1439) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, UPPER CARGO COMPARTMENT SEC 46 SEAT TRACK CRACKED 4 AT BS 1439, RBL 83.

Part: SEAT TRACK — CORRODED (BS 1605) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, UPPER CARGO COMPARTMENT SEC 46.- SEAT TRACK SHOWS CORROSION AT BS 1605 BL 110.

Part: STRINGER — CORRODED (BS 1361 S39R) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT. STRINGER 39R SHOWS CORROSION AT BS 1361.

Part: STRINGER — CORRODED (BS 1575 S38R) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C CHECK INSPECTION, AFT BULK CARGO COMPARTMENT, STRINGER 38R SHOWS CORROSION AT BS 1575.

Part: STRINGER — CORRODED (BS 416 S34L) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT, STRINGER 34L, SHOWS CORROSION AT BS 416.

Part: STRINGER — CORRODED (BS 1362 S36L) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT. STRINGER 39L SHOWS CORROSION AT BS 1362.

Part: STRINGER — CORRODED (BS 415 S39R) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT. STRINGER 39R, SHOWS CORROSION AT BS 415.

Part: STRINGER — CORRODED (BS 783 S37R) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT. STRINGER 37R, SHOWS CORROSION AT BS 783.

Part: SKIN — CORRODED (BS 746) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT. SKIN SHOWS CORROSION AT BS 746, RBL 43 BETWEEN S-34R AND S-35R.

Part: STRINGER — CORRODED (BS 448 S38L) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPARTMENT, STRINGER 38L, SHOWS CORROSION AT BS 448.

Part: STRINGER — CORRODED (BS 1361 S36L) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT. STRINGER 36L SHOWS CORROSION AT BS 1361.

Part: FRAME — CORRODED (BS 1562) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, AFT BULK CARGO COMPARTMENT FRAME SHOWS CORROSION BS 1562 S38L TO 38R REF NR-0083.

Part: STRINGER — CORRODED (BS 1575) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, AFT CARGO COMPARTMENT BULK CARGO LOWER LOBE STRINGER 38L SHOWS CORROSION AT BS 1575.

Part: STRINGER — CORRODED (BS 1361 S37L) · airframe 82,198 hrs · 39,061 cycles

DURING ROUTINE C-CHECK INSPECTION, BILGE AFT CARGO COMPARTMENT. STRINGER 37L SHOWS CORROSION AT BS 1361.

Part: BEAM — WORN (ZONE 500) · airframe 51,425 hrs · 41,745 cycles

LEFT WING O/B FLAP I/B HINGE CARRIER BEAM (ATTACHED TO FLAP) -WHERE 3-10 LINK ATTACHS TO FLAP -O/B FLANGE I/B BUSHING LOOSE IN FLANGE. REPAIRED ON REA B653-59822-MR, ACFT WAS GROUNDED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,064 hrs · 38,037 cycles

DURING SERVICE CHECK FOUND CENTER GUIDE AT BS 1020 LOOSE IN FLOOR. MAINTENANCE FOUND 3 CRACKED INTERCOSTAL SUPPORT PYLONS FITTINGS PART NUMBERS 95453-201 (1EA) AND 95453-202 (2EA). THE PYLON FITTINGS AND FLOOR PANELS WERE REPLACED.

Part: SWITCH — OUT OF ADJUST (EMERGENCY EXIT) · airframe 76,210 hrs · 36,387 cycles

R EMERGENCY DOOR EICAS MSG ON CLIMBOUT WITH NORMAL PRESSURIZATION; LIGHT AND EICAS MSG WENT OUT AT CRUISE ALTITUDE FL320. FOUND OVERWING DOOR SWITCH OUT OF ADJUSTMENT. RE-ADJUSTED PER AMM 52-21-01-2.

Part: SEAT — DEFECTIVE (COCKPIT) · airframe 74,445 hrs · 35,597 cycles

CAPTAINS ELECTRICAL SEAT UNOP. FORE AND AFT, UP AND DOWN, SEAT LOCK RELEASED WHEN APPLYING BRAKES ALLOWING SEAT TO SLIDE AFT UNCONTROLLABLY. REPLACED CAPTAINS SEAT WITH SERVICEABLE UNIT. OPS CHECK OK. IAW B767 MM 25-11-02.

Part: HOLDER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,515 hrs · 35,008 cycles

MAIN ENTRY DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED MAIN ENTRY DOOR SLIDE EMERGENCY LAMP HOLDER IAW B767 MM 33-51-06.

Part: PIN — OUT OF POSITION (CONNECTOR) · airframe 72,231 hrs · 34,895 cycles

LT EMERGENCY "EXIT" PANEL LIGHT WOULD NOT TEST. TROUBLESHOT PER WD 33-51-13. RELOCATED PIN 13 IN CONNECTOR J9084 TO POSITION 9 PER REA B633-56326. EMERGENCY LIGHTS TEST GOOD IAW B767 MM 33-51-01.

Part: BEAM — CORRODED (CARGO DOOR) · airframe 72,160 hrs · 34,876 cycles

FORWARD LOWER CARGO DOOR BEAM WAS CORRODED AROUND FORWARD 3 NUT PLATES. REMOVED AND REPLACED BEAM IAW B767 SRM 51-40-1.

Part: ENGINE — DEFECTIVE (NR 2) · airframe 71,916 hrs · 34,765 cycles

RIGHT ENGINE SHUTDOWN IN FLIGHT DUE TO HIGH EGT AND HIGH ENGINE VIBRATION (METAL FOUND IN THE TAILPIPE). REMOVED AND REPLACED RIGHT ENGINE ON WO 600272604, REF JOB CARD 7010 FOR WORK ACCOMPLISHED IAW B767 MM.

Part: GCU — DEFECTIVE (LT ENGINE) · airframe 71,166 hrs · 34,372 cycles

SMOKE SMELL COMING FROM E&E COMPARTMENT. FOUND LEFT ENGINE GCU WITH STRONG BURNT SMELL AND NO GENERATOR PRESSURE LIGHT IN COCKPIT. SWAPPED LEFT GCP AND APU GCP AS TROUBLESHOOTING. NO SMOKE PRESENT. APU ELECTRICAL FUNCTION INOPERATIVE. REMOVED AND REPLACED APU GCU IAW B767 MM 24-22-02. OPS CHECKED GOOD.

Part: LINKAGE — OBSTRUCTED (RT ENG THROTTLE) · airframe 71,051 hrs · 34,311 cycles

CLIMBING THRU 33,000 FT, THE RT ENG N1 INCREASED APPROX 1 PERCENT ABOVE THE LT ENG N1. AUTO THROTTLES WERE ENGAGED. ATTEMPTED TO ALIGN THE N1'S WITH THE AUTO THROTTLES ENGAGED. THE RT ENG N1 DID NOT RESPOND TO THRUST LEVER MOVEMENT. THEN DISENGAGED THE AUTO THROTTLES AND RETARDED THE RT THRUST LEVER. THE RT ENG DID NOT RESPOND TO THRUST LEVER MOVEMENT. WITH THE RT THRUST LEVER HALFWAY TO IDLE, APPROX A 5 INCH SPLIT BETWEEN THRUST LEVERS, THE RT ENG INDICATIONS DID NOT CHANGE. AFTER 5 MINS THE RT BEGAN RESPONDING TO THRUST LEVER MOVEMENTS. IMMEDIATELY AFTER THE RT ENG BEGAN RESPONDING TO THE THRUST LEVER. TROUBLESHOT SYSTEM, FOUND PANEL TO PYLON TUNNEL LOOSE AND FASTENER FROM PANEL HAD DROPPED OFF ON TO

Part: DISPLAY — DEFECTIVE (COCKPIT) · airframe 70,564 hrs · 34,079 cycles

CAPTAIN'S CDU DISPLAY BLANK, ODOR OF ELECTRICAL SMOKE. RETURNED TO BLOCKS AT MIA. REMOVED AND REPLACED CDU IAW AMM 34-61-02.