N768QT

Part: VALVE — OPEN (ZONE 100) · airframe 88,811 hrs · 33,059 cycles

DURING CRUISE, WITH EQUIPMENT COOLING SWITCH IN STANBY, EICAS MESSAGE " FWD EQPT OVHT" DISPLAYED AND OVERHEAT LIGHT ILLUMINATING. IAW AMM TASK CARD 21-58-29-004-001 R & R DIFFERENTIAL PRESSURE SWITCH. R & R EQUIPMENT COOLING INDICATION CONTROL IAW AMM 21-58-24. TESTED OK. DURING APPROACH WITH EQUIPMENT COOLING SWITCH OVERRIDE, EICAS MESSAGE "FWD EQPT COOLING" DISPLAYED AND NO COOLING LIGHT ILLUMINATED. R & R EQUIPMENT COOLING LOW FLOW DETECTOR IAW AMM 21-58-17. OPS CHECKED OK. EICAS MESSAGE "FWD EQPT VALVE DISPLAYED EQUIPMENT COOLING VALVE LIGHT ILLUMINATED, STANBY SELECTED AND VALVE LIGHT REMAINS ILLUMINATED. R & R OVERBOARD EXHAUST VALVE IAW AMM 21-58-05, OPS TESTED SATISFACTORY.

Part: ELECTRONIC UNIT — MALFUNCTIONED (SLATS) · airframe 87,099 hrs · 32,420 cycles

AFTER ACFT ROTATION EICAS DISPLAYED L/E SLAT DISAGREE WITH THE FLAP LEVER IN 5. OVERWEIGHT LANDING, 1000KG LW 1293 KG NO HARD LANDING. HARD LANDING INSPECTION WAS PERFORMED IAW AAM 05-51-35 PAGE 201 TO 203 PHASE I OPTION A. NO DAMAGE FOUND. DURING BITE TEST TO PSEU, IT SHOWS FAULT CODE 010 CARD. PROXIMITY SW ELECTRONIC UNIT WAS R & R IAW AMM 32-09-4, PAGE 401-406. TEST OK IAW AMM32-09-04, PAGE 406. FLAP/SLAT ELECTRONIC UNIT WAS R & R AS TROUBLESHOOTING IAW AMM 27-51-01, PAGE 401 TO 406. BITE TEST OF THE FSEU IAW AMM 27-51-0, PAGE 550 TO 551 TEST OK. A VERIFICATION FLIGHT WAS PERFOMED TO CONFIRM C/A. NO DISCREPANCIES WERE NOTED.

Part: WARNING LIGHT — ILLUMINATED (SLATS)

DURING CLIMB, EICAS MESSAGE L/E SLAT ASSYM DISPLAYED L/E LIGHT ILLUMINATED WITH FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. AIR TURN BACK, AN OVERWEIGHT LANDING WAS NOT PERFORMED. ACFT IS DECLARED AOG. GROUND INSPECTION IS IN PROCESS. OPEN

Part: ROTARY ACTUATOR — CORRODED (NR 5 SLAT) · airframe 86,372 hrs · 32,150 cycles

DURING WALK AROUND ON ACFT, FOUND AT LT WING NR 5 SLAT HANGING DOWN FROM ONE SIDE. THE SLAT REMAINED SUPPORTED FROM ONE TRACK WHICH CAUSED HOLES OF SOME PANELS OF WING AND ANTI-ICE TUBES DEFLECTION. AFTER REMOVAL OF SLATS NR 4 AND NR 5 WAS FOUND GEARBOX ASSY (PN 256T2220-12) AND ROTARY ACTUATOR ASSY (PN 256T2120-5) WITH SIGNS OF HEAVY INTERNAL CORROSION. GEAR BOX AND ROTARY ACTUATOR WERE DISASSEMBLED TO LOOK INSIDE AND ALL GEARS WERE FOUND ATTACHED ONE TO ANOTHER BY CORROSION DUE TO GREASE ABSENCE. OTHER PARTS THAT WERE FOUND DAMAGED ARE: RT FIXED WING L/E WITH CRACKS, TAI DUCT WITH BENT, SLAT T/E AERODYNAMIC SEALS BROKEN.

Part: ROTARY ACTUATOR — CORRODED (SLATS) · airframe 85,977 hrs · 32,012 cycles

DURING CLIMBING STAGE L/E SLAT ASSY APPEARS. AIR TURNBACK. GROUND INSP FINDINGS: DURING VISUAL INSP WAS FOUND SLAT NR 12 HANGING DOWN FROM ONE SIDE. THE SLAT REMAINS SUPPORTED FROM 1 TRACK WHICH CAUSED HOLES OF SOME PANELS OF WING AND ANTI-ICE TUBES DEFLECTION. AFTER REMOVAL OF SLAT WAS FOUND, GEARBOX ASSY (P/N 256T2220-12) AND ROTARY ACTUATOR ASSY (P/N 256T2120-5) WITH SIGNS OF HEAVY INTERNAL CORROSION. THE SHAFT BETWEEN THESE COMPONENTS WAS COMPLETELY SHEARED. GEAR BOX WAS DISASSEMBLED TO LOOK INSIDE AND ALL GEARS WERE FOUND ATTACHED ONE TO ANOTHER BY CORROSION DUE TO GREASE ABSENCE. OTHER PARTS THAT WERE FOUND DAMAGED ARE: RT FIXED WING L/E WITH A HOLE, TAI DUCT WITH BEND, SLAT T/E AERODYNAMIC SEAL BROKEN.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND AT FWD CARGO COMPARTMENT DOOR, INNER SKIN, AFT SIDE FLANGE HOLE BEND, REPAIR WAS ACCOMPLISHED UNDER EWO 767-52-022 AND SR 1-1665185720.

Part: CARGO TRACK — CORRODED (BS 1480-1605) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, MAIN DECK CARGO TRACKS RBL 33.00, STA 1480-1605 WAS FOUND WITH CORROSION, REPAIR ACCOMPLISHED IAW EWO 767-53-113 AND IAAC PARTS EO TAC-100824.

Part: SEAT TRACK — CORRODED (BS 478-588) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND CORROSION ON TRACKS RBL 11.00 BETWEEN STA 478-588. REPAIR ACCOMPLISHED IAW EWO 767-53-115 AND EO TAC-100823.

Part: KEELBEAM — CORRODED (BS 1070) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND KEELBEAM, BS 1070, LT MID SECTION CHORD HAS CORROSION, REPAIR WAS ACCOMPLISHED IAW EWO 767-53-106R1 AND SR 1-1657143102.

Part: CARGO TRACK — CORRODED (BS 1605.5) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND MAIN DECK CARGO TRACKS BETWEEN STA RBL 54.75 TO 1605.5 AND BETWEEN 1518-1605 HAS CORROSION.

Part: SPAR — DAMAGED (RT WING) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND RT WING FRONT SPAR BETWEEN RIB 32 TO 31 WITH A HOLE, REPAIR WAS ACCOMPLISHED IAW EWO 767-57-066 AND SR 1-1660377939.

Part: KEELBEAM — CORRODED (BS 1000-1010) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND KEELBEAM HORIZ WEB, BS 1000 TO BS 1010 HAS CORROSION, REPAIR WAS ACCOMPLISHED IAW EWO 767-53-108R1 AND SR 1-1660618916.

Part: RIB — CORRODED (RT WING TE FLAP) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND CORROSION ON RT INBD FLAP RIB ASSY AT HOLE (LODGING ON TORQUE TUBE) STA IFS 108.5 RIBS PN 113T2237-2/14, REPAIR ACCOMPLISHED IAW EWO 767-57-066 AND SR 1-1660377939.

Part: SEAT TRACK — CORRODED (BS 566-663) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND CORROSION ON TRACKS LBL 54.75 STA 566-663.45, REPAIR ACCOMPLISHED WITH EWO 767-53-0114 AND EO TAC-100824

Part: FRAME — BENT (RADOME) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND NOSE RADOME 7 O'CLOCK, 10 O'CLOCK, 12 O'CLOCK AND 1 O'CLOCK FRAME HAS BEND. REPAIR WAS ACCOMPLISHED IAW EWO 767-53-109 AND SR 1-1660613312.

Part: SKIN — CORRODED (BS 742 S33-34L) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND ON FUSELAGE EXTERIOR SKIN STA 742, STR 33L-34L AFTER BLENDING CORROSION OUT OF LIMITS, REPAIR WAS ACCOMPLISHED IAW EWO 767-53-110R1 AND SR 1-1664728418.

Part: LATCH — CORRODED (CARGO DOOR) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, WAS FOUND CORROSION ON LATCH FITTING PN 368-53-00-95345 (12 POSITION) MAIN CARGO DOOR, REPAIR ACCOMPLISHED IAW EWO 767-53-112 AND IAI DOC CS-23803-001.

Part: SKIN — CORRODED (WING) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND CORROSION ON LWR SKIN BETWEEN RIB 19, WS 668.2 AND RIB 23 WS 772.2 AFTER BLENDING REMAINING THICKNESS WAS FOUND OUT OF LIMITS, REPAIR WAS PERFORMED WITH EWO 767-57-070 AND SR 1-1664985960.

Part: SKIN — DENTED (CARGO DOOR) · airframe 82,903 hrs · 30,957 cycles

DURING SVC C4, FOUND 2 DENTS ON EXTERNAL SKIN FWD LARGE CARGO DOOR STA 533.60-542.4 BETWEEN INTERCOSTAL PLANE 3-4, REPAIR WAS ACCOMPLISHED IAW EWO 767-52-23R1 AND SR 1-1659397983.

Part: ENGINE — AUTO SHUTDOWN (RIGHT) · airframe 78,868 hrs · 29,558 cycles

DURING CRUISE LEVEL AT FL 360, 65 NM MILES SOUTH OF INTERSECTION, THE RT ENG OIL FILTER EICAS ANNUNCIATION DISPLAYED. ACCORDING TO CHECK LIST, REDUCED THRUST TO IDLE, THE ANNUNCIATION REMAIN DISPLAYED. FOLLOWING CHECK LIST, THE RT ENGINE WAS SHUTDOWN AFTER COOL DOWN PERIOD. ADVISED ATC, DUE TO ENGINE SHUTDOWN. WILL LAND AT ORIGINAL DESTINATION WITH NO OTHER INCONVENIENCE.

Part: SKIN — CORRODED (BS 448) · airframe 77,534 hrs · 29,072 cycles

DURING C3 CHECK FOUND CORROSION ON SKIN COMMON TO ATC ANTENNA, STA 448 STRINGER 39R/39L. REPAIR ACCOMPLISHED IAW EWO 767 53-088 AND BOEING SR 1-1249400131.

Part: SILL — CORRODED (BS 500-610) · airframe 77,534 hrs · 29,072 cycles

DURING C3 CHECK INSPECTION, FOUND FWD CARGO DOOR SURROUND STRUCTURE LOWER SILL BETWEEN STA 500 TO STA 610 LATCH FITTINGS WITH CORROSION. REPAIR ACCOMPLISHED IAW EWO 767 53-089 AND SR 1-1254161109.

Part: SKIN — CORRODED (LT WING) · airframe 77,534 hrs · 29,072 cycles

DURING C3 CHECK INSPECTION WAS FOUND CORROSION ON WING LOWER SKIN STA WS 694.2 WITH REAR SPAR, LT. REPAIR ACCOMPLISHED IAW EWO 767 57-053 AND BOEING SR 1-1251347105.

Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 77,534 hrs · 29,072 cycles

DURING C3 CHECK INSPECTION, FOUND RT WING OTBD T/E FLAP LWR SURFACE AT STA OTEF 119 AND BETWEEN STA OTEF 265.69 TO OTEF 371.88 HAS CORROSION. REPAIR ACCOMPLISHED IAW EWO 767 57-054 AND SR 1-1247041324.

Part: FRAME — CRACKED (NR 1 NACELLE) · airframe 77,534 hrs · 29,072 cycles

DURING C3 CHECK INSPECTION WAS FOUND A CRACK ON NR 1 ENGINE CORE COWL FRAME STA NAC 303.75. REPAIR ACCOMPLISHED IAW EWO 767 54-087 AND ROHR CV09-0810-03.

Part: DOOR — CORRODED (FWD CARGO) · airframe 77,534 hrs · 29,072 cycles

DURING C3 CHECKS INSPECTION WAS FOUND A CORROSION ON FWD CARGO DOOR EXTERNAL REPAIR DOUBLER STA 606 - 617 INTERCOSTAL PLANE 7. REPAIR ACCOMPLISHED IAW EWO 767 52-018 AND BOEING SR 1-1249442665.

Part: FRAME — CRACKED (NR 2 NACELLE) · airframe 77,534 hrs · 29,072 cycles

DURING C3 CHECK INSPECTION WAS FOUND A CRACK ON NR 2 ENGINE CORE COWL FRAME STA NAC 303.75. REPAIR ACCOMPLISHED IAW EWO 54-054 AND CV09-0811-02.

Part: FRAME — CRACKED (NR 2 NACELLE) · airframe 77,534 hrs · 29,072 cycles

DURING C3 CHECK INSPECTION WAS FOUND A CRACK ON NR 2 ENGINE CORE COWL FRAME STA NAC 303.75. REPAIR ACCOMPLISHED IAW EWO 54-055 AND CV09-0833-04.

Part: SKIN — DENTED (BS 1307-1329) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=25 ON SKIN STA 1307-1329 STR 32-33 - LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-052 AND SRM 53-00-01 REPAIR 6. THIS REPAIR CONSTITUTES A MAJOR REPAIR.

Part: SPAR — DAMAGED (WING) · airframe 71,323 hrs · 26,829 cycles

DURING C CHECK INSPECTION (TASK CARD 57-650-00) WAS FOUND LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 864.92 873.13 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-028 AND SERVICE REQUEST 1-527347746. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: STRAP — CORRODED (BS 1351) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, SAFE FAIL STRAP P/N 146T8048-3. REMOVED, FABRICATED AND INSTALLED A NEW FAIL SAFE STRAP P/N 146T8048-3 IAW EWO 767-53-057 AND SERVICE REQUEST 1-557292575. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: SPAR — DAMAGED (LT WING) · airframe 713,213 hrs · 26,829 cycles

DURING C CHECK INSPECTION (TASK CARD 06-102-01-1) WAS FOUND A LOOSE MATERIAL ON SPLICE PLATE AT FRONT SPAR STA ISS 1009 - 1017 LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-027 AND SERVICE REQUEST 1-526643882. THIS REPAIR IS CONSIDERED A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: BEAM — CRACKED (WING LE) · airframe 71,323 hrs · 26,829 cycles

DURING C-CHECKS INSPECTION WAS FOUND A CRACK ON FIXED LEADING EDGE NOSE BEAM WEB STA OSS 644.58-694.55 - RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-025 AND SRM 57-41-13 REPAIR 1-2. THIS REPAIR CONSTITUTES A MAJOR REPAIR.

Part: SKIN — CORRODED (BS 582) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON PRESSURE SKIN STA 582 BETWEEN STRINGER 34-35 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-058 AND SERVICE REQUEST 1-526668594. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: SILL — CORRODED (BS 569) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, MAIN SILL, OUTER CHORD STA 569.65 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-056 AND SERVICE REQUEST 1-527218048. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: SILL — CORRODED (FUSELAGE) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, MAIN SILL, OUTER CHORD STA 632 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-059 AND SERVICE REQUEST 1-533874348. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: SKIN — DENTED (BS 676-698) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT OVER REPAIR DOUBLER AT SKIN STA 676-698 STRINGER 37-38 - RT. THE DOUBLER NEEDS TO BE REPLACE. DAMAGED AREA WAS REPAIRED IAW EWO 767 53-047 AND SRM 53-00-01 REPAIR 14. THIS REPAIR CONSTITUTES A MAJOR REPAIR.

Part: SKIN — WRINKLED (NR 2 SLAT) · airframe 71,323 hrs · 26,829 cycles

DURING (C) CHECKS INSPECTION WAS FOUND AN EXISTING REPAIR WRINKLED ON LEADING EDGE SLAT NR 2 UPPER SKIN. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-029 AND MFG SERVICE REQUEST 1-527377149. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: SKIN — DENTED (BS 1536 S36L) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=40 ON LAP SKIN STA 1536 STR 36 - LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-049 AND SRM 53-00-01 REPAIR 12. THIS REPAIR CONSTITUTES A MAJOR REPAIR.

Part: SKIN — DENTED (BS 1417-1436) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C2) CHECK WERE FOUND SEVERAL DENTS ON FUSELAGE SKIN STA 1417-1436 STRINGER 33 -36-LT. DAMAGED AREAS WERE REPAIRED IAW EWO 767-53-055 AND SERVICE REQUEST 1-527218048. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: RIB — CHAFED (RT AILERON) · airframe 71,323 hrs · 26,829 cycles

DURING C-CHECK INSPECTION WAS FOUND A WEAR OUT OF LIMITS ON IB AILERON RT - OB CLOSURE RIB WEB.DAMAGED AREA WAS REPAIRED IAW EWO 767 57-026 AND SERVICE REQUEST 1-525478883. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: COWLING — DAMAGED (NACELLE) · airframe 71,323 hrs · 26,829 cycles

DURING C CHECK INSPECTION WAS FOUND CORE COWL P/N: 224-2301-513 S/N: 0130 WITH ELONGATED HOLE AT FRAME STA NAC 294 - CF6-80C2. DAMAGED AREA WAS REPAIRED IAW CV07-1781-01 AND EWO 767-54-020. THIS REPAIR CONSTITUTES A MAJOR REPAIR.

Part: SKIN — CHAFED (FUSELAGE) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C) CHECK WAS FOUND A WEAR ON RUB STRIPS SKIN STA 1725.50 STRINGER 22 - RT/LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-054 AND MFG SERVICE REQUEST 1-524791119. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: SKIN — DENTED (BS 1506 S31-32L) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT A/Y=20 ON FUSELAGE SKIN AT STA 1506, STR 31-32 -LT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-048 AND SRM 53-00-01 REPAIR 6. THIS REPAIR CONSTITUTES A MAJOR REPAIR.

Part: SILL — CORRODED (BS 610) · airframe 71,323 hrs · 26,829 cycles

FWD CARGO COMPARTMENT LOWER MAIN SILL, THE UPPER EXTERIOR EXTRUDED SECTION HAS CORROSION AT STA 610. REMOVED AND REPLACED MAIN SILL IN FWD CARGO COMPARTMENT UPPER EXTERIOR EXTRUDED SECTION STA 610 IAW SRM 51-40-02 PAGE 2-3 AND SRM 51-40-02 PAGE 4-7.

Part: FAIRING — CORRODED (HORIZONTAL STAB) · airframe 71,323 hrs · 26,829 cycles

DURING C CHECK INSPECTION WAS FOUND A CORROSION ON HORIZONTAL STABILIZER TIP LT NOSE IB - LT.DAMAGED AREA WAS REPAIRED IAW EWO 767-57-030 AND MFG SERVICE REQUEST 1-524791300. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: SKIN — DENTED (BS 212 S30R) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF C2 CHECK WAS FOUND A DENT ON LAP SKIN STA 212.5, STR 30-RT. DENT ON LIMITS IAW EWO 767-53-051 AND MFG SERVICE REQUEST 1-526586182. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: SKIN — CORRODED (BS 456 S31-32R) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C2) CHECK WAS FOUND CORROSION OVER REPAIR DOUBLER AT SKIN STA 456, STR 31-32 -RT. THE DOUBLER NEEDS TO BE REPLACED. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-046 AND SRM 53-00-01 REPAIR 14.THIS REPAIR CONSTITUTES A MAJOR REPAIR.

Part: SKIN — DENTED (BS 1339 S17L) · airframe 71,323 hrs · 26,829 cycles

DURING INSPECTION OF (C2) CHECK WAS FOUND A DENT ON LAP SKIN STA 1339 STR 17 - LT. DAMAGE ON LIMITS IAW EWO 767-53-05 AND BOEING SERVICE REQUEST 1-526586182. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.

Part: GEARBOX — LEAKING (LT ENGINE) · airframe 68,784 hrs · 25,917 cycles

DURING CLIMB ON FLIGHT # 861 (MDE-SCL) LT ENGINE OIL QTY DECREASED TO ZERO AND OIL PRESS DECREASED FROM 64 TO 15 PSI. ENGINE WAS REDUCED TO IDLE AND OIL PRESS REMAINED IN 15 PSI. AIRCRAFT WAS RETURNED TO MDE AND LANDED IN NORMAL CONDITION. DURING MAINTENANCE INSPECTION IAW FIM 710500 FIG 119 WAS DISCOVERED ENGINE INTERNAL LEAK BY TRANSFER GEARBOX. LT ENGINE WAS REMOVED & REPLACED IAW BOEING TASK CARD 71-R05 "POWER PLANT REPLACE". OVERWEIGHT LANDING INSPECTION WAS PERFORMED IAW EWO 767-32-010 & AMM 05-51-35 PHASE I, OPTION A AND NONE STRUCTURAL DAMAGE WAS FOUND. MAIN WHEELS NR 1, 2, 5 & 6 WERE REPLACED IAW AMM 32-45-01 PAGE 401-405 DUE TO THERMAL FUSE PLUGS WERE FOUND MELTED & BRAKE TEMP LIGHT INSPECTION WAS PE

Part: SKIN — DENTED (FUSELAGE) · airframe 66,037 hrs · 25,015 cycles

TEMPORARY REPAIR HAD BEEN PERFORMED ON FUSELAGE SKIN AT STA 172.5 STRINGER 21 RT (REF: SDR TAMF20050007O). PERMANENT REPAIR WAS PERFORMED IAW EWO 767-53-003 PART III, EWO DRAWING 767 53-002 AND SERVICE REQUEST 1-134757238.

Part: BEAR STRAP — CORRODED (FUSELAGE) · airframe 66,037 hrs · 25,015 cycles

DURING INSPECTION ACCORDING TASK CARD S53-003-10 WAS FOUND CORROSION AT BEARSTRAP AT THE AFTER CARGO DOOR CONTROL PANEL CUTOUT LOCATION AT STA 1263 STRINGER 26 - RT. CORRODED AREA WAS REPAIRED IAW EWO 767-53-004 R1 PART I AND II AND MSG NR:1-157473174 AND 1-193842742.

Part: SPLICE PLATE — CRACKED (LT WING) · airframe 66,037 hrs · 25,015 cycles

DURING C-CHECK INSPECTION WAS FOUND A CRACK ON LOWER CHORD AT FRONT SPAR STA ISS 314.14 LEFT. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-011 AND BOEING SERVICE REQUEST: 1-195119496.

Part: SKIN — CORRODED (CENTER WING) · airframe 66,037 hrs · 25,015 cycles

DURING C-CHECK INSPECTION WAS FOUND A CORROSION ON CENTER WING SKIN STA 955 AND RBL 74.81. CORRODED AREA WAS BLENDED OUT IAW B767 SRM 51-11-00 PAGE 4-5, THICKNESS MEASUREMENT PERFORMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-010 AND BOEING SERVICE REQUEST: 1-195119692.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 66,037 hrs · 25,015 cycles

DURING INSPECTION CHECK FOUND A SCRATCH ON PRESSURE SKIN AT STA 1582 STRINGER 5-6R. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-013 AND BOEING SERVICE REQUEST 1-195909646.

Part: FLOOR SKIN — CORRODED (CARGO BAY) · airframe 66,037 hrs · 25,015 cycles

DURING (C) INSPECTION CHECK AFT CARGO COMPARTMENT RT FLOOR STRUCTURE PANEL SKIN HAVE CORROSION AND LOWER ATTACH ANGLE AFT IS CRACKED (UNDER BALL MAT RT). CORROSION ON FLOORBEAM UPPER CHORD ON STA 1285 BETWEEN LBL-RBL WAS FOUND. CRACKED ANGLE AND CORRODED AREA IN STA 1285 BETWEEN LBL-RBL WERE REPLACED IAW DRAWING 146T5000 AND SKIN PANEL IN AFT CARGO COMPARTMENT RT FLOOR STRUCTURE WAS REPLACED IAW DRAWING 451T2502.

Part: SKIN PANEL — DELAMINATED (VERTICAL STAB) · airframe 66,037 hrs · 25,015 cycles

DURING C CHECK INSPECTION FOUND A DELAMINATION ON LT VERTICAL STABILIZER SKIN PANEL, STA FSS 170.259 - 195.390. DELAMINATED PANEL PN: 175T2001-3 WAS REMOVED IAW SRM 51-40-02 PAGE 1 AND SENT TO REPAIR. PANEL WAS REPAIRED AND INSTALLED IAW BOEING MESSAGE NUMBER 1-194272386.

Part: SKIN — CRACKED (LT NACELLE) · airframe 66,037 hrs · 25,015 cycles

DURING (C) CHECK INSPECTION WAS FOUND CRACK AT SKIN ENGINE 1 LT AT FRAME AT NAC STA 274 - CF6-80C2. DAMAGE WAS REPAIRED IAW EWO 767-54-004 AND MFG REFERENCE CV06-1004-01.

Part: DOUBLER — CORRODED (LT PYLON) · airframe 66,037 hrs · 25,015 cycles

DURING INSPECTION ON C CHECK FOUND CORROSION AT SKIN DOUBLER. CORRODED AREA WAS REPAIRED IAW EWO 767 54-001, BOEING SERVICE REQUEST 1-194658477 AND SRM 54-52-01 FIGURE 201.

Part: SKIN — CRACKED (LT PYLON) · airframe 66,037 hrs · 25,015 cycles

DURING C CHECK INSPECTION WAS FOUND CRACK AT SKIN, ENGINE 1 LT AT FRAME AT NAC STA 274. DAMAGE WAS REPAIRED IAW EWO 767 54-003 AND GOODRICH AEROSTRUCTURES REFERENCE CV06-0985-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,037 hrs · 25,015 cycles

DURING C-CHECK INSPECTION FOUND A CRACK AT VERTICAL CHORD AT STA 287 BL 25 LT. DAMAGED AREA WAS CLEANED AND REPAIR DOUBLERS WERE FABRICATED & INSTALLED IAW EWO 767 53-009, SRM 53-10-14 & SRM 51-70-12.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,037 hrs · 25,015 cycles

DURING C-CHECK INSPECTION FOUND A CRACK AT VERTICAL CHORD AT STA 287 BL 25 RT. DAMAGED AREA WAS CLEANED AND REPAIR DOUBLERS WERE FABRICATED & INSTALLED IAW EWO 767-53-010, SRM 53-10-14 & SRM 51-70-12.

Part: SKIN — DENTED (BS 172.5) · airframe 63,597 hrs · 24,202 cycles

DURING INSPECTION CHECK, FOUND THE AIRPLANE HIT AT FUSELAGE SKIN, STA 172.5 STRINGER 21 RT BY A CARGO LOADING EQUIPMENT.REPAIR DOUBLER AS TEMPORARY REPAIR WAS INSTALLED IAW EWO 767-53-002, MFG SERVICE REQUEST NR 1-134757238 AND SRM 53-00-01 FIGURE 201. PERMANENT REPAIR WILL BE PERFORMED IN NEXT (C) MAINTENANCE CHECK. (MAY, 2006).

Part: WIRE — CHAFED (SLATS) · airframe 63,105 hrs · 24,029 cycles

DURING TAKEOFF EICAS MSG L/E SLAT ASSYM DISPLAYED & LEADING EDGE LIGHT ILLUM WITH THE FLAP LEVER IN 1. BOTH FLAP POINTERS WERE CORRECT. THE AIRPLANE WAS RETURNED TO RNG FRM 27810500. WIRING W176-102-24 IN P-36 WAS REPAIRED IAW WDM 32-09-11 PAGE 1 SH 2. FIM 27-81-00 FIG 107 STEPS 1 TO 20A WAS PERFORMED WITH NORMAL RESULTS. SYSTEM OK. OVERWEIGHT LANDING INSPECTION (PHASE I, STEP A) WAS PERFORMED IAW AMM 05-51-35 PAGES 201 & 202; NO DAMAGES WERE FOUND.