N780BA

Part: DOUBLER — NOT REPORTED (ZONE 200) · airframe 90,839 hrs · 17,060 cycles

FOUND EXISTING REPAIR DOUBLER AT FUSELAGE SKIN STA 2410, S-7L~S-8L.(<P>1. ACCOMPLISHED EL NO. T2024A53M-2850 REV.0. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 90,839 hrs · 17,060 cycles

CORROSION - FOUND ON GIRT BAR FITTING FWD SIDE AND AFT SIDE.(<P>1. REPLACED THE DAMAGED FITTING (PN: 65B14014-7; 65B14012-7) (SUB KIT NO: 015U0817-11) I.A.W EO NO. 4453A528 PART 1 STEP 4. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: STRUCTURE — MISMANUFACTURED · airframe 90,839 hrs · 17,060 cycles

DEVIATION DURING PERFORM NOSE W/W MODIFICATION FOUND CHORD (PIN: 65B07942U75, 65B07942U76 CONTOUR CAN NOT MATCH.(<P>1. ACCOMPLISH REPAIR AREA I.A.W. EL NO. T2024A53M-2524 REV.1</P> / <P>2. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)

Part: TRUNNION — CORRODED (ZONE 100) · corrosion level 2 · airframe 90,839 hrs · 17,060 cycles

CORROSION ON FITTING (PIN: 65B04474-5) OF LH MLG TRUNNION BACK-UP BETWEEN STA 1480 AND STA 1520. LBL 16.0.(<P>1. REMOVED DAMAGE FITTING IAW SRM 51-40-02-0G-0 REV.59. 2. FABRICATE FITTING IAW EL NO: T2024A53M-2718 REV.0. 3. INSTALL FABRICATE FITTING IAW SRM 51-40-02-0G-0 REV.59 AND DWG NO: 65B04271 SH4 REV.- &AMP; 65B15085 SH9 REV.K. 4. JOB COMPLETED AND CONDITION CHECK NORMAL. 5. ACCOMPLISHED EL NO. T2024A53M-2718 REV.1.</P>)

Part: SKIN — CORRODED (ZONE 500) · airframe 90,839 hrs · 17,060 cycles

CORROSION - SKIN, L/H WING L/E CAVITY FRONT SPAR LOWER SKIN, ILES 949.(<P>1. REMOVED THE EFFECTED FASTENERS IAW SRM 51-40-02-0G-0, REV.58. 2. BLENDED OUT THE DAMAGE AREA IAW SRM 57-20-01-1A-2, REV. 58. 3. PFM NDT INSP REFER TO JOB CARD ATTACHING NO. 0428990 &AMP; DATA SHEET NO.10247099-1. 4. MEASURED REWORKED AREA DEPTH 0.113", LENGTH 5", WIDTH 2.5", IT WAS ALLOWABLE IAW SRM 57-20-01-1A-2, CHART II, REV.59. 5. INSTALLED FASTENERS IAW. SRM 51-40-02-0G-0 REV. 59 &AMP; DWG NO. 65B10729, SH 3, REV.W. 6. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: DOUBLER — NOT REPORTED (ZONE 100) · airframe 90,839 hrs · 17,060 cycles

FOUND EXISTING REPAIR DOUBLER AT AFT CGO STA 1780 - 1800 STGR 49R.(<P>1. REMOVE EXISTING REPAIR PARTS I.A.W SRM 51-40-02-OG-O REV.59. 2. PERFORMED EL NO T2024A53M-2884, REV 0, SEQUENCE A. 3. ACCOMPLISHED EL NO. T2024A53M-2884 REV.1. 4.JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SKIN — CORRODED (ZONE 400) · corrosion level 2 · airframe 90,839 hrs · 17,060 cycles

CORROSION - FND #3 ENG LH CORE COWL SKIN CORROSION BETWEEN STA 222.5 AND STA 230.5.(<P>1. ACCOMPLISHED EL NO. T2024A71M-2536 REV.1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: FRAME — MISREPAIRED (ZONE 100) · airframe 90,839 hrs · 17,060 cycles

UNDOCUMENTED REPAIR ON FRAME WEB OF FWD CARGO COMPARTMENT AT STA 720, NEAR LBL 6.5 AND RBL 6.5.(<P>1. ACCOMPLISHED EL NO. T2024A53M-2904 REV.0. 2.JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: VALVE — FAULTED (PARKING BRAKE) · airframe 90,672 hrs · 17,033 cycles

REJECTED TAKE OFF FOR PARKING BRAKE SET MESSAGE(<P>FOUND CMC MSG 32893. R/R PARKING BRAKE VALVE PER AMM 32-44-08, CHECKED GOOD. PERFORMED HIGH ENERGY STOP INSPECTION PER AMM CHAPTER 05-51-10. NP MAINTENANCE ACTION REQUIRED. NO FURTHER DEFECTS NOTED.</P>)

Part: NONE — NONE · airframe 89,283 hrs · 16,795 cycles

CORROSION-SKIN, FWD CGO COMPARTMENT BILGE SURFACE STA 760~780, S-45L-S-47L.(<P>1) BLENDED OUT THE DAMAGE AREA I.A.W. SRM 51-10-02 REV. 52. 2) PFM NOT INSP REFER TO JOB CARD ATTACHING SHEET NO 0271927. 3) MEASURED REWORK AREA DEPTH= 0.01" LENGTH= 3.2" WIDTH=1.5" AT STA 772 S-46LUS-47L AND DEPTH=0.004" LENGTH=3" WIDTH=1.7" AT STA 762 S-45LUS-46L. IT WAS ALLOWABLE I.A.W SRM 53-00-01-1A-A TABLE I DETAIL II REV. 52 4) APPLY PROTECTIVE COATING AT REWORK AREA I.A.W SRM 51-20-01 REV. 52.5 JOB COMPLETED.</P>)

Part: NONE — NONE · corrosion level 2 · airframe 89,283 hrs · 16,795 cycles

FND UPPER GATE SURFACE CORROSION ON IL ENTRY DOOR STA 443~STA 485(<P>1) REMOVE THE DAMAGE PART I.A.W SRM 51-40-02. REV=52 2) INSTALL NEW PART I.A.W SRM 51-40-02, REV=53 AND DWG NO=65B01836 9H3, REV=T; 65B01836, 9H7 REV=N 3) JOB COMPLETED AND COND CHK NML</P>)

Part: NONE — NONE · airframe 89,283 hrs · 16,795 cycles

CORROSION-SKIN, FWD CGO COMPARTMENT BILGE SURFACE STA 740~760. S-46R~S-47R(<P>1) BLEND OUT THE DAMAGE AREA I.A.W SRM 51-10-02. REV=52 2) PFM NOT INSP REFER TO JOB CARD ATTACHING SHEET NO=0271928 3) MEASURED REWORK AREA DEPTH=0.005", LENGTH=2", WIDTH=2" IT WAS ALLOWABLE I.A.W SRM 53-00-01-1A-1, TABLE I, DETAIL II, REV=52 4) APPLY PROTECTIVE COATING AT REWORK AREA. I.A.W SRM 51-20-01, REV=52 5) JOB COMLETED.</P>)

Part: NONE — NONE · airframe 89,283 hrs · 16,795 cycles

FOUND L/H 1 DOOR EMERGENCY LIGHT INOP(<P>1) I.A.W AMM 33-51-06-000-801833-51-06-400-801 REV. 105 REPLACED DOOR SLIDE LIGHT BATTERY AND CONDITION CHECK NORMAL. 2) I.A.W AMM 33-51-00-115-001 REV. 105 PERFORMED OPERATIONAL TEST AND THE RESULT WAS SATISFACTORY</P>)

Part: STRAP — NONE · corrosion level 2 · airframe 89,283 hrs · 16,795 cycles

CORROSION-STRAP, LH WING INBD FIXED LE CAVITY LOWER SKIN PNL SPLICE, ILES 380(<P>1) REMOVE DAMAGE PARTS I.A.W SRM 51-40-02, REV=52 2) FABRICATE PARTS I.A.W SRM 51-40-02, REV=52 2) FABRICATE PARTS I.A.W EI=T2022P57M-3119, REV=0. 3) INSTALL FABRICATE PARTS I.A.W SRM 51-40-02, REV=52 AND DWG NO= 65B14598, SHEET=3. REV=D 4) CONDITION CHECK NORMAL AND JOB COMPLETE.</P>)

Part: NONE — NONE · airframe 89,283 hrs · 16,795 cycles

BROKEN DAMAGE WAS FOUND ON THE RH MAIN ENTRY DOOR NO. 1 FWD FRAME(<P>1) REMOVED THE AFFECTED FASTENERS I.A.W. SRM 51-40-02 REV.52 2) REPAIR DAMAGE AREA I.A.W SRM 52-10-02-2R-4 REV:52 AND EI NO T2022A52M-3052 REV:1 AND DWG NO 6501836, SH2 REV: AB 3) CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: ACTUATOR — FAILED (RT MLG) · airframe 86,976 hrs · 16,436 cycles

FOUND FUNCTION FAIL AT R/H WLG ALTERNATE ROTARY ACTUATOR.(<P>IAW AMM 32-36-01-004-001 REV. 97 AND AMM 32-36-01-404-009 REV. 97, REPLACED R/H WLG ALTERNATE ROTARY ACTUATOR. CONDITION CHECK NORMAL.</P>)

Part: SNUBBER — OUT OF LIMITS (PAX DOOR) · airframe 86,976 hrs · 16,436 cycles

FOUND M/D ENTRY DOOR SNUBBER IND P/N OUT OF LIMIT. LOCATION = L1.(<P>IAW AMM 52-11-10-004-001 REV. 97 AND AMM 52-11-10-404-005 REV. 97, REPLACED L1 ENTRY DOOR SNUBBER. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: FEEDER CABLE — CHAFED (NR 4 ENGINE) · airframe 86,976 hrs · 16,436 cycles

FOUND #4 ENG FEEDER CABLE (W282-143-110) CHAFING.(<P>IAW SWPM 20-10-11, 20-10-12, 20-30-13, 20-30-11 REV. 72 AND WDM 24-21-41 REV. 22, REPLACED ENG FEEDER CABLE. IAW AMM 24-11-00-705-001-001 REV. 97, PERFORMED GENERATOR DRIVE SYSTEM OPERATIONAL TEST AND THE RESULT WAS SATISFACTORY.</P>)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,976 hrs · 16,436 cycles

FOUND EMERGENCY BATTERY PACK (M14533) INOP.(<P>IAW AMM 33-51-04-902-001-001 REV. 97, REPLACED EMERGENCY BATTERY PACK AT M14533 AND CONDITION CHECK NORMAL. IAW AMM 33-51-04-902-001-001 REV. 97, PERFORMED POWER SUPPLY TEST AND THE RESULT WAS SATISFACTORY.</P>)

Part: STRINGER — CRACKED (BS 460) · airframe 86,976 hrs · 16,436 cycles

FOUND STRINGER CRACK AT R/H STA 460 S-10R UPPER DECK.(<P>REPAIRED CRACK AREA IAW EO NO. 4453A353 PART 2 REV. 0 AND EI NO. T2020A53M-477 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: LONGERON — CRACKED (FUSELAGE) · airframe 83,219 hrs · 15,893 cycles

CRACK ON NR 5, NR 9, NR 11 OF LT LONGERON EXTENSION FIG WHEN PFM SB 747-53A2390. RPL WITH NEW LONGERON EXTENTION FIG IAW EI T2018 A53M-5143 REV 1 AND EI T20177A07M-4573 REV1 AND DWG 65B15255 SHEET 2 REV B AND DWG 65B15254 SHEET 3 REV D AND SRM 51-40-04 REV 40. OPS CHECK NORMAL.

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION ON LT WING FIXED TE PANEL SUPPORT SPAR AT WRL 150. ACCOMPLISHED EI T2018A57M-4924 REV 1. JOB COMPLETED AND CONDITION CK NORMAL.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 83,219 hrs · 15,893 cycles

CRACK DAMAGE ON RT NR 7 HOLE WHEN PERFORMING SB 747-53A2390 AT STA 1480 LONGERON EXTENSION FIG. ACCOMPLISHED EI T2018A07M-4573 REV 0. O/S DAMAGE HOLE NR 7 TO 0.531" IAW EO 4453A874 REV 2. REMOVED & INSTALL LONGERON FIG FOR NDT INSP IAW SRM 51-40-02, 51-40-04 REV 40 AND DWG 65B15254 SH3 REV D, 65B15255 SH2 REV B. CRACK BE CLEARED REF JC ATTACHED TO SHEET NO 0158060. EI T2018A07M-4573 REV 0 ATTACH TO NRC 638. OPS CHECK GOOD.

Part: SKIN — CORRODED (NR 4 COWLING) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION WITH BROKEN ON NR 4 ENG LT CORE COWL SKIN BETWEEN ST 222.5 AND STA 230.5. REPAIRED CORE COWL SKIN IAW EI T2018A71M-4600 REV1 AND EI T2018A71M-4600 REV1 AND EI T2018O71M-5022 REV 0. JOB COMPLETED AND CONDITION CK NORMAL.

Part: STIFFENER — CORRODED (RT MLG WW) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION ANGLE RT SIDE WING L/G WHEEL WELL LONGERON BOX STRUCTURE ANGLE STA 1325, RBL 122 AND RBL 124 AREA. REMOVED CORROSION STIFFENER IAW ARM 51-40-02 REV 40. ACCOMPLISHED EI T2018P 53M-4453 REV 0. FABRICATED THE NEW PART. INSTALLED NEW PART IAW SRM 51-40-02 REV 40 AND DWG 65B15093 SHEET 3 REV H. JOB COMPLETED AND CONDITION CK NORMAL.

Part: STIFFENER — CORRODED (RT MLG WW) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION ANGLE RT SIDE WING L/G WHEEL WELL LONGERON BOX STRUCTURE ANGLE STA 1323, RBL 122 AND RBL 124 AREA. REMOVED CORROSION STIFFENER IAW SRM 51-40-02 REV 40. ACCOMPLISHED EI T2018P53M-4453 REV 0. FABRICATE THE NEW PART. INSTALLED NEW PART IAW SRM 51-40-02 REV 40 AND DWG 65B15096 SH3 REV H. OPS CHECK GOOD.

Part: SKIN PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION ON AFT OF LT WING SKIN PANEL NR 1 NEAR WS 586.62. ACCOMPLISHED EI NO T2018A57M-4809 REV 1. JOB COMPLETED CONDITION CK NORMAL.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION ON STRINGER PN 65B02777-63 AT STA 2658 S9L. ACCOMPLISHED EI T20-18A53M-4629 REV 0. CONDITION CK NORMAL, JOB COMPLETED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 83,219 hrs · 15,893 cycles

FOUND EMERGENCY LIGHT INOP AT L1 DOOR AND MD CEILING. IAW AMM 33-51-04-902-001-001 REV 93 R&R BATTERY PACK. IAW AMM 33-51-04-902-001-001 REV 93 PERFORMED EMERGENCY LIGHT TEST, OPS CK NORMAL.

Part: ACTUATOR — FAILED (RT WLG) · airframe 83,219 hrs · 15,893 cycles

THE RT WLG ALTERNATE EXTENSION SYSTEM TEST, RESULT ELECTRICAL ACTUATOR FUCTION FAIL. IAW AMM 32-36-01-004-001 REV 93 AND AMM 32-36-01-404-009 REV 93 REPLACED ACTUATOR. CONDITION CK NORMAL.

Part: SUPPORT BRACKET — CORRODED (LT WING) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION, PLATE LT T/E CAVITY UPPER HYD TUBES SUPPORT WBL 133. REMOVED THE DAMAGED PART IAW SRM 51-40-02 REV 40. INSTALL THE NEW PART IAW SRM 51-40-02 REV 40 AND 65B11525 SHEET 2 REV E. JOB COMPLETED AND CONDITION CK NORMAL.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION ON THE LT WING INTER SPAR LWR SKIN LOWER SURFACE AROUND SURGE TANK SUMP DRAIN. REPAIR DAMAGED AREA IAW EI T2018A57M-4720 REV1. OPS CHECK GOOD.

Part: FITTING — CORRODED (RT WLG DOOR) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION CLIP RT SIDE WING LG FAIRING DOOR 1 EA CLIP. R&R DAMAGED CLIP IAW SRM 51-40-02 REV 40AND DWG NO 65B11675 SHEET 2 REV G DWG 65B11675 SHEET 1 REV K. OPS CHECK GOOD.

Part: SUPPORT ANGLE — CORRODED (RAM AIR INLET) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION ANGLE NR 3 RAM AIR INLET DUCT SUPPORT ANGLE STA 900 AREA. REMOVED AND REPLACED DAMAGED PART IAW SRM 51-40-02 REV 40 DWG 65B09715 SH3 REV 9. OPS CHECK GOOD.

Part: DOUBLER — CORRODED (LT WING) · airframe 83,219 hrs · 15,893 cycles

CORROSION ON THE DOUBLER OF THE LT WING REAR SPAR FUEL PUMP CUTOUT AT WS 425. ACCOMPLISHED EI T2018A57M-4660 REV 1, OPS CHECK NORMAL.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION ON LT WING LEADING EDGE SKIN NEAR WBL 1240. REPAIRED DAMAGED AREA IAW EI T2018A57-M-4551 REV1. JOB COMPLETED AND CONDITION CK NORMAL.

Part: SUPPORT — CORRODED (LT WING) · corrosion level 2 · airframe 83,219 hrs · 15,893 cycles

CORROSION ON LT WING FIXED TE PANEL SUPPORT SPAR AT WBL 180. ACCOMPLISHED EI T2018A57M-4923 REV 1. JOB COMPLETED AND CONDITION CK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 81,400 hrs · 15,621 cycles

EMERGENCY LIGHTS INOPERATIVE AT R1 DOOR AND ALL LIGHTS RIGHT OF CENTER LIGHT. REMOVED AND REPLACED THE BATTERY PACK M10684 IAW MM 33-51-04-402-D12-001.

Part: STRAP — DAMAGED (SURVIVAL KIT) · airframe 80,423 hrs · 15,467 cycles

L1 DOOR SLIDE SURVIVAL KIT ATTACH STRAP DAMAGED. REMOVED AND REPLACED RESCUE KIT IAW AMM 25-69-01.

Part: RESERVOIR — DISCHARGED (L1 DOOR) · airframe 80,423 hrs · 15,467 cycles

L1 DOOR EMERGENCY POWER RESERVOIR DISCHARGED. REMOVED AND REPLACED POWER RESERVOIR IAW AMM 52-11-06-404-015.

Part: SLIDE — UNWANTED DEPLOY (L1 DOOR) · airframe 80,423 hrs · 15,467 cycles

L1 DOOR SLIDE DEPLOYED. REMOVED AND REPLACED THE SLIDE IAW AMM 25-69-01, STEP 1-6.

Part: WEB — CRACKED (BS 1890) · airframe 79,516 hrs · 15,330 cycles

WEB CRACKED, MAIN DECK CARGO FLOOR NEAR BS 1890, LBL 101. ACCOMPLISHED EI T2017A53M-484, REV1.

Part: SKIN — CORRODED (RT WING LE) · corrosion level 2 · airframe 79,516 hrs · 15,330 cycles

RIGHT WING L/E UPPER SKIN FWD SIDE CORRODED. ACCOMPLISH EI 72017A57M-460, REV 2.

Part: SKIN — CORRODED (BS 1350) · airframe 79,516 hrs · 15,330 cycles

CORRODED SKIN AT BS 1350, RBL 9. ACCOMPLISHED EI T2017A53M-445, REV 2.

Part: CARGO TRACK — CRACKED · airframe 79,516 hrs · 15,330 cycles

CRACK ON THE OTBD FLANGES OF THE CARGO TRACK. ACCOMPLISHED EI T2017A53M-542, REV1.

Part: CARGO TRACK — CRACKED · airframe 79,516 hrs · 15,330 cycles

CRACK ON THE OTBD FLANGES OF THE CARGO TRACK. ACCOMPLISHED EI T2017A53M-543, REV1.

Part: MOTOR — NO TEST (RT MLG) · airframe 79,516 hrs · 15,330 cycles

THE RT MLG ALTERNATE EXTENTION MOTOR TEST FAILED IAW AMM 32-36-01-004-001 AND AMM 32-36-01-404-009 REV.88 STEPS A-F(3). REPLACED THEMOTOR. IAW AMM 32-36-01-404-009 REV.88 STEP F(4). OPS TESTED GOOD.

Part: STRUCTURE — CORRODED (LT WING) · airframe 79,516 hrs · 15,330 cycles

LEFT WING L/E TO FRONT SPAR CAVITY AT ILES 1071 CORRODED. REMOVED THE CORROSION AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-41-09-1A-1, FIGURE 101, DETAIL IV, REV 36.

Part: WEB — CRACKED (BS 1790) · airframe 79,516 hrs · 15,330 cycles

CRACK ON WEB OF MAIN DECK CARGO FLOOR NEAR BS 1790, LBL 101. ACCOMPLISHED EI T2017A53M-485, REV1 2.

Part: SKIN — CORRODED (RT WING LE) · airframe 79,516 hrs · 15,330 cycles

RT WING L/E UPPER SKIN WS 452 FWD SIDE CORRODED. REMOVE THE CORROSION AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-41-01-1A-0, FIGURE 101, DETAIL II, REV 36.

Part: KEELBEAM — CORRODED (BS 1287-1308) · airframe 79,516 hrs · 15,330 cycles

KEEL BEAM CORRODED AT BS 1283 - 1303, LBL 9. ACCOMPLISHED EI T2017A53M-483, REV 1.

Part: WEB — CORRODED (BS 1890) · airframe 79,516 hrs · 15,330 cycles

CRACK ON WEB OF MAIN DECK CARGO FLOOR NEAR BS 1890, RBL 101. ACCOMPLISHED EI T2017A53M-482, REV 1.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 79,516 hrs · 15,330 cycles

SKIN BETWEEN WS 219 AND 262 ON RT WING FIXED LE UPPER FWD SIDE CORRODED. ACCOMPLISHED EI T2017A57M-460, REV 2.

Part: SKIN — CORRODED (BS 1350) · airframe 79,516 hrs · 15,330 cycles

SKIN CORROED AT BS 1350, LBL 9. ACCOMPLISHED EI T2017A53M-445, REV 2.

Part: SKIN — CORRODED (RT WING) · airframe 79,516 hrs · 15,330 cycles

RT WING SKIN CORRODED, WS 476. REMOVED THE CORROSION AND IAW SRM 57-41-01-1A-0, FIG 101, DETAIL II, REV 36.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 79,516 hrs · 15,330 cycles

CORROSION ON SKIN WS 331, RT WING LE UPPER SURFACE FWD SIDE. ACCOMPLISHED EI T2017A57M-460, REV 2.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 79,516 hrs · 15,330 cycles

FOUND R1 DOOR EXIT EMERGENCY LIGHT LAMP BURNED OUT. REPLACED LAMPS AND CONDITION CHECK NORMAL. IAW AMM 33-51-00, REV 88.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 79,516 hrs · 15,330 cycles

SKIN RT WING L/E UPPER SURFACE FWD SIDE.. ACCOMPLISHED EI T2017A57M-460, REV 2.

Part: PANEL — CORRODED (NR 4 NACELLE) · corrosion level 2 · airframe 79,516 hrs · 15,330 cycles

FOUND THE NR 4 NACELLE PANEL CORRODED. ACCOMPLISHED EI Y2017A54M-490 REV 1.

Part: STRUCTURE — DAMAGED (NR 1 NACELLE) · airframe 79,539 hrs · 15,332 cycles

DURING INBOUND INSPECTION, FOUND NR 1 NACELLE DAMAGED. INSTALLED NACELLE STRUCTURE IAW AMM 71-11-01.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 78,751 hrs · 15,217 cycles

COCKPIT F/O EMERGENCY FLASHLIGHT INOPERATIVE AND CASE DAMAGED. R & R F/O EMERGENCY FLASHLIGHT AND HOLDER IAW AMM 25-60-00, OPS CHECK NORMAL.

Part: FMU — MALFUNCTIONED (NR 3 ENGINE) · airframe 79,810 hrs · 15,187 cycles

NR 3 ENGINE EXCEEDED LIMITS DURING TAKEOFF, 656 C FOR 2 MINUTES. R & RTHE FUEL METERING UNIT IAW 73-21-01. OPS CHECKED GOOD.

Part: MOTOR — OUT OF ADJUST (PARKING BRAKE) · airframe 78,450 hrs · 15,171 cycles

CONFIGURE BRAKE EICAS WARNING DURING TAKEOFF, OCCURRED DURING INITIAL THRUST APPLICATION AT APPROXIMATELY 25 KTS. LOW SPEED REJECT, NO RELATED CMC MESSAGE. IAW FIM TASK 32-44-805 SWAPPED PARK BRAKE VALVE CLOSE RELAY R7514 WITH SERVICEABLE UNIT- NO HELP. REMOVED PARK BRAKE VALVE MOTOR AND ADJUSTED IAW MM 32-44-08 AND SYSTEM CHECKS NORMAL IAW MM 32-44-00.

Part: FAIRING — CORRODED (RT WING) · airframe 76,891 hrs · 14,922 cycles

CORROSION SURFACE, FOUND SURFACE RT WING INBD DOOR FAIRING UPPER WAS CORRODED. BLENDED OUT THE DAMAGE AREA & MEASURED REWORKED AREA L X W X D = 2X1.5X0.0044. ORIGINAL THICKNESS WAS 0.071 WHICH WAS WITHIN THE ALLOWABLE LIMIT IAW SRM 52-80-02, ALLOWABLE DAMAGE 4 FIG.101 III REV 32 DETAIL DATA IAW TO IC ATTACHING SHEET NR 0069557. APPLIED PROTECTIVE TREATMENT & FINISH IAW SRM 5-1-20 -02 REV 32. JOB COMPLETED & COND CHECKED NORMAL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 76,891 hrs · 14,922 cycles

CORROSION SKIN, RIGHT FUSELAGE UPPER EXTERNAL SURFACE AT STATION 560 - 580 & STRINGER 132R - 133R. REMOVE DAMAGE & MEASURE REWORK AREA EXISTING. REWORKED REMAINING THICKNESS, LENGTH=2.5" & WIDTH=0.5" & DEPTH=0.004" & EXISTING THICKNESS = 0.125", IT IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01-1A-1 ALLOWABLE DAMAGE REV 32 & SRM 53-20-01-01-1 IDENTIFICATION REV 32 & PERFORM AREA PROTECTIVE TREATMENT IAW SRM 51-20-01 REV 31. CONDITION CHECK NORMAL & JOB COMPLETED.

Part: FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 76,891 hrs · 14,922 cycles

CORROSION CLIP, LT WING LE TO FRONT SPAR, LOWER CLIP AT HOLES 1360. REMOVE DAMAGE PART IAW SRM 51-40-02-06-0 REV 32 & PART FABRICATION IAW EI NR T2015P57B-2567 SEQUENCE A REV 0 & 3. INSTALLED FABRICATE PART IAW SRM 51-40-02-06-0 REV 32 & JOB COMPLETED & COND CHK NML.</P></ROOT>)

Part: SUPPORT — CORRODED (RT WING) · airframe 76,891 hrs · 14,922 cycles

CORROSION BEAM, OLES 1341, RT WING LE COMPARTMENT LOWER SUPPORT. REMOVED DAMAGE & MEASURED REWORKED AREA, LENGTH 3.1 IN. WIDTH = 23.0IN. DEPTH =0.014; WITHIN THE ALLOWABLE DAMAGE IAW SRM 57-41-13, ALLOWABLE DAMAGE 1 REV 32 DETAIL DATA. PLEASE REFER TO JC ATTACHING SHEET NR 0069546. PERFORMED DAMAGED AREA PROTECTIVE TREATMENT IAW SRM 51-20-01 OR REV 32. CONDITION CHECKED NORMAL & JOB COMPLETED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 76,891 hrs · 14,922 cycles

REPAIR CORROSION ON THE WING INTER SPAR LOWER SKIN, PANEL NR 3, LOWER SIDE NEAR FSS 1305. BLENDED OUT THE DAMAGED AREA, MEASURED & REWORKED. THE DEEPEST THICKNESS WAS 0.216 INCHES, WHICH WAS NOT ALLOWABLE IAW SRM 57-20-01, ALLOWABLE DAMAGES FIG 101 CHART I REV 32. DETAIL DATA REF TO IC ATTACHING SHEET NR 0069558 & NRC DATA SHEET CONTROL NR 050079 & CONTACT PE TO DO FURTHER ACTIONS. PEM EI NR T2015 57B-2573 REV 1 JOB COMPLETED & CONDITION CHECKED NORMAL.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 76,891 hrs · 14,922 cycles

CORROSION FOUND RT WING UPPER SKIN UPPER SURFACE HAD CORROSION AFT OF REAR SPAR WS 582.2. REPAIR CORROSION IAW E I NR T2015 A 57B - 2603 REV 4&. CONDITION CHECKED NORMAL & JOB COMPLETED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 76,891 hrs · 14,922 cycles

CORROSION DAMAGE ON THE RT WING INTER SPAR LOWER SKIN UPPER SURFACE NEAR OLES 1308. REMOVED DAMAGED AREA IAW SRM 51-10-02 REV 32. REPAIR DAMAGED AREA IAW EI NR T2015 A 578 - 2597 REV 2. JOB COMPLETED & CONDITION CHECKED.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 76,891 hrs · 14,922 cycles

CORROSION, SKIN AT HST RT LOWER EXTERNAL SKIN, REAR SPAR STAB STATION 255. REMOVE DAMAGE & MEASURE REWORK AREA LENGTH=1" & WIDTH=0.5" & DEPTH=0.007" IS WITHIN ALLOWABLE LIMITS IAW SRM 55-10-01-1A-1. ALLOWABLE DAMAGE 1 REV 32 & FREE OF CORROSION, DETAIL DATA IAW JOB CARD ATTACHING SHEET NR 0069640. PFM REWORKED AREA PROTECTIVE TREATMENT IAW SRM 51-20-01 REV 32. CONDITION CHECKED NORMAL & JOB COMPLETED.

Part: SKIN — CORRODED (LT WING) · airframe 76,891 hrs · 14,922 cycles

CORROSION, SKIN, LT WING UPPER SKIN AT WBL 849. BLEND OUT THE DAMAGED AREA & MEASURED REWORK AREA LX WXD = 1.1" X 0.9" X 0.007" WHICH IS WITHIN ALLOWABLE LIMIT IAW SRM 57-20-01-1A-1 FIG 101 DETAIL II REV 32. DETAIL DATA REA TO J/C ATTACHING SHEET NO. 0069538 & APPLY PROTECTIVE TREATMENT IAW SRM 51-20-01 REV 32. &NBSP;4. JOB COMPLETED & CONDITIION * CHECK .

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 76,891 hrs · 14,922 cycles

CORROSION ON THE RT WING INTERIOR LOWER SKIN UPPER SURFACE NEAR OLES 1308. REMOVE DAMAGE AREA IAW SRM 51-10-02 REV 32. REPAIR DAMAGE AREA IAW EI NR T2015 A 578 - 2597 REV 2. JOB COMPLETED & CONDITION CHECKED NORMAL.

Part: SKIN — CORRODED (LT HORIZ STAB) · airframe 76,891 hrs · 14,922 cycles

CORROSION SKIN, AT LT HORIZONTAL STAB LOWER EXTERNAL SKIN, REAR SPAR STAB STATION 230. REMOVE DAMAGE & MEASURE REWORK AREA LENGTH = 1.4" & WIDTH = 1" & DEPTH=0.008" IS WITH ALLOWABLE LIMITS IAW SRM 55-10-01-1A-1 ALLOWABLE DAMAGE REV 32 & FREE OF CORROSION DETAIL DATA, REF TO JOB CARD ATTACHING SHEET NR 0069642. PERFORM REWORKED AREA PROTECTIVE TREATMENT IAW SRM 51-20-01 REV 32 & 3. CONDITION CHECK NORMAL & JOB COMPLETED.

Part: ACTUATOR — FAILED (FUEL SYSTEM) · airframe 76,891 hrs · 14,922 cycles

NUMBER 2 ENG FUEL SOV ACTUATOR FUNCTION FAIL. IAW AMM 28-22-01-404-057 REV 85, REMOVED NR 2 ENG SOV ACTUATOR. IAW AMM 28-22-01-404-056 REV 85 STEP 3A TO E, INSTALLED NR 2 ENG SOV ACTUATOR & IAW AMM 28-22-00-705-108 REV 85, PERFORM NR 2 ENG SOV OPERATION TEST. RESULT WAS SATISFACTORY. CONDITION CHECKED NORMAL.

Part: STRINGER — CORRODED (RT WING) · corrosion level 2 · airframe 76,891 hrs · 14,922 cycles

CORROSION RT WING LE NR 26E, V/C FLAP UPPER STRINGER CORROSION. REPLACED DAMAGED PART WITH NEW PART IAW SRM 51-40-02-06-0 REV 32. JOB COMPLETED & CONDITION CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 76,891 hrs · 14,922 cycles

FOUND L1 DOOR EMER LIGHT INOPERATIVE. IAW CMM 33-50-14 REV 8 STEP 2 E, REPLACED BATTERY PACK ASSEMBLY OF EMER LIGHT AT L1 DOOR & CHECKED NORMAL. IAW AMM 33-51-00-715-001 REV 85, PERFORMED OPERATIONAL TEST OF L1 DOOR EMER LIGHT & THE RESULT WAS SATISFACTORY.

Part: SMOKE BARRIER — FAILED (COCKPIT) · airframe 76,891 hrs · 14,922 cycles

COCKPIT SMOKE SHUTTER FUNCTION FAIL. IAW AMM 25-64-05-002-049 & 25-64-03-402-052 REV 85 REPLACED SHUTTER COND CHECKED NORMAL. IAW AMM 25-64-05-202-047 REV 85, PERFORMED OPERATION CHECK RESULT WAS SATISFACTORY.

Part: BOTTLE — DEPLETED (L1 DOOR) · airframe 76,373 hrs · 14,843 cycles

L1 DOOR ASSIST RESERVOIR BOTTLE DEPLETED. R & R DOOR ASSIST RESERVOIR BOTTLE IAW AMM 52-11-06-404-015.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 76,373 hrs · 14,843 cycles

L1 DOOR SLIDE, UPON OPENING FROM OUTSIDE BECAME UN-BUSTLED, PRESS BOTTLE INTACT. REPLACED L1 DOOR SLIDE IAW AMM 25-69-01.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 73,620 hrs · 14,410 cycles

RTO, DETECTOR FIRE & OVHT 3. ITEM DEFERRED IAW DDG 26-11-02-01.

Part: WINDOW — POPPED (COCKPIT) · airframe 73,595 hrs · 14,405 cycles

WHILE CLIMBING THROUGH 10,000 FT HEARD POP ON LT SIDE. OBSERVED CREW OXYGEN DROPPED IN FLIGHT FROM 1680 TO 1600 PSI LANDING. R & R NR 1 WINDOW IAW MM 56-11-01, OPERATIONS CHECKED OK. PRESSURIZATION CHECK OF WINDOW IAW MM 21-32-01. ALSO PERFORMED OXYGEN PRESS & LEAK CHECK IAW MM 35-00-00 NO LEAKS NOTED.

Part: CHANNEL — CORRODED (RT MLG WW) · airframe 73,578 hrs · 14,401 cycles

CORROSION CHANNEL RT WING GEAR WW STATION 1246 RBL 98.64. REPLACED DAMAGE PART WITH FABRICATED PART IAW EI NO T2014P53-2236 REV 0 & IAW SRM 51-40-02-0G-0 REV 28.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,578 hrs · 14,401 cycles

FOUND EMER LIGHT BATTERY ASSEMBLY FUNCTION FAIL M7915 DRL 1 OVHD. REPLACED EMER LIGHT POWER SUPPLY & CONDITON CHECKD NORMAL & PERFORMED POWER SUPPLY TEST & THE RESULTS WAS SATISFACTORY IAW AMM 33-51-04.

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION BEAM, FWD SUPPORT BEAM OF RT WING LE CAVITY LOWER FIXED PNL ILES 705 & 805. IAW SRM 57-41-13-1A-1 DETAIL V REV 27 REMOVED CORROSION AREA & APPLY PROTECTIVE COATING IAW SRM 51-20-01-0G-0 REV 27.

Part: STRUCTURE — CORRODED (LT BLG WW) · airframe 73,578 hrs · 14,401 cycles

CORROSION LOWER CHORD, LT BODY GEAR WW LOWER CHORD CORROSION STATION 1350 BETWEEN LBL 34 & LBL 45. REPAIR DAMAGE AREA IAW EI NO T2014A53B-2249 REV 2 CONDITION CHECK SATISFIED.

Part: CARGO TRACK — WORN (CARGO BAY) · airframe 73,578 hrs

FOUND THE WEAR DAMAGED ON THE LT MD CARGO RAIL AT STATION 1430 TO 1489. ACCOMPLISHED EI NO T2014A53B-2299 REV 1. JOB COMPLETED & CONDITION CHECKED NORMAL.

Part: SKIN — DAMAGED (RT WING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

SKIN FWD FACE OF RT WING INBD FIXED LE LANDING LIGHTS CUT OUT TOTAL 2 AREA. REPLACED DAMAGE PARTS WITH NEW PARTS IAW SRM 51-40-02-0G-0 REV 27. JOB COMPLETED & CONDITION CHECKED SATISFIED.

Part: BULKHEAD — CORRODED (RT WLG WW) · airframe 73,578 hrs · 14,401 cycles

CORROSION CHORD RT WING GEAR WW BULKHEAD CHORD CORROSION STATION 1350 RBL 5. IAW SRM 51-40-02 REV 27 REPLACED DAMAGE PART WITH NEW PART.

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION BEAM, FWD SUPPORT BEAM OF RT WING LE CAVITY LOWER FIXED PNL ILES 939. IAW SRM 57-41-13-1A-1 DETAIL V REV 27 REMOVED CORROSION AREA & APPLY PROTECTIVE COATING IAW SRM 51-20-01-0G-0 REV 27.

Part: BULKHEAD — CORRODED (LT WLG WW) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION WEB, LT WING GEAR WW BULKHEAD SKIN CORROSION STATION 1241 NEAR OVERRIDE PUMP. REMOVED CORROSION & MEASURE REWORK AREA DEPTH 0.019, LENGTH 3.8 & WIDTH 1.2 WITHIN ALLOWABLE LIMIT IAW SRM 57-10-10-1A-2 REV 27.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION SKIN OF LT WING LE FRONT SPAR UPPER STATION WS 1621 NEAR PNL 531BB. REMOVED CORROSION IAW SRM 57-20-01-1A -1 FIG 101 REV 28 & APPLY REWORK AREA SURFACE PROTECTIVE COATING IAW SRM 51-20-01 REV 28.

Part: BEAM — CRACKED (FUSELAGE) · airframe 73,578 hrs · 14,401 cycles

CRACK BEAM ON STATION 360 STRINGER 3L. REPAIR DAMAGE AREA IAW EI NO T2014A53B-2300 REV 1.

Part: STRAP — CORRODED (RT WING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION STRAP UPPER SURFACE OF RT WING INBD LE UPPER FIXED PNL ILES 516. REPLACED DAMAGE PART WITH NEW PART IAW SRM 51-40-02 & SRM 51-40-04 REV 28. JOB COMPLETED & CONDITION CHECKED NORMAL.

Part: FRAME — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

FRAME FWD CARGO COMPARTMENT STATION 980 STRINGER 46L - 47L. REPAIRED THE DAMAGE AREA IAW EI NO T2014A53B-2063 REV 1. CONDITION CHECKED NORMAL & JOB COMPLETED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION ON LOWER SKIN UPPER SURFACE OF RT WING LE FRONT SPAR AT FSSI 640. REPAIR DAMAGE AREA IAW EI NO T2014A57B-2302 REV 5. CONDITION CHECKED NORMAL & JOB COMPLETED.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION SKIN AROUND FASTENER HEADS OF RT WING IN SPAR LOWER SKIN, LOWER SURFACE WS 950 - 955 TOTAL 2 AREA. REPAIR DAMAGE AREA IAW SRM 57-20-01 REPAIR 1 REV 28 CONDITION CHECKED NORMAL & JOB COMPLETED)

Part: FRAME — CORRODED (BODY FAIRING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION WAS FOUND ON WING TO BODY FAIRING FRAME OUTER CHORD FWD FLANGE AT STATION 987.5 RBL 35. REPAIR THE CORROSION IAW EI NO T2014A53B-2261 REV 2. JOB COMPLETED & CONDITION CHECKED NORMAL.

Part: SKIN — BROKEN (FAIRING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

BROKEN & CORROSION ON FAIRING SKIN OF RT FWD MAIN LG WW AT STATION 1254. REPAIR DAMAGE AREA IAW EI NO T2014A53B-2232 REV 1. JOB COMPLETED & CONDITION CHECKED NORMAL.

Part: PANEL — DEFORMED (NACELLE) · airframe 73,578 hrs · 14,401 cycles

DEFORM FND NR 4 RT & LT STRUT SKIRT FAIRING PANEL HAD DEFORM BETWEEN NAC STATION 288 TO 323. ACCOMPLISHED EI NO T2014A54B-2245 REV 1. CONDITION CHECKED NORMAL & JOB COMPLETED.

Part: ROLLER TRAY — MECHANIC ERROR (FUSELAGE) · airframe 73,578 hrs · 14,401 cycles

LLM FIG 59 MISS DRILL EXISTING HOLE TO ROLLER TRAY AT STATION 960 RBL 58. ACCOMPLISH EI NO T2014A25B-2117 REV 1. CONDITION CHECKED NORMAL & JOB COMPLETED.

Part: PLATE — CORRODED (FUSELAGE) · airframe 73,578 hrs · 14,401 cycles

CORROSION BRIDGE PLATE 65B06097-56 OF FWD CARGO FLOOR STRUCTURE AT STATION 660 BETWEEN LBL 7 & RBL 7. REPLACE WITH NEW FABRICATION PART IAW EI NO T2014P53B-1998 REV 0 & SRM 51-40-02 REV 27.

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION BEAM, FWD SUPPORT BEAM OF RT WING OTBD LE LWR FIXED PNL OLES 1385 & 1410. IAW SRM 57-41-13-1A-1 DETAIL V REV 27 REMOVED CORROSION AREA & APPLY PROTECTIVE COATING IAW SRM 51-20-01-0G-0, REV 27.

Part: SKIN — DAMAGED (RT WING) · airframe 73,578 hrs · 14,401 cycles

LIGHTNING STRIKE SKIN UPPER SURFACE OF RT WING IN SPAR UPPER SKIN WBL 1215 - WBL 1224. REPAIR DAMAGE AREA IAW EI NO T2014A57B-2235 REV 01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 73,578 hrs · 14,401 cycles

FOUND TWO EMER LIGHTS INOPERATIVE. EQUIPMENT NR L1382. REPLACED LAMPS IAW AMM 33-51-00-715-001 REV 80. PERFORMED EMER LIGHT OPERATIONAL TEST & THE RESULTS WERE SATISFACTORY.

Part: STIFFENER — CORRODED (RT WLG WW) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION STIFFENER RT WING GEAR WW STATION 1345 RBL 72. REPLACE THE DAMAGE PART WITH THE NEW PART IAW SRM 51-40-02-0G-0 REV 28. CONDITION CHECKED NORMAL & JOB COMPLETED.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 73,578 hrs · 14,401 cycles

STRINGER 38L CRACK ON STATION 500. REPAIRED CRACK IAW SRM 53-00-03. REPAIR 4 DETAIL II FIGURE 201 REV 28. CONDITION CHECKED NORMAL & JOB COMPLETED.

Part: SUPPORT BEAM — CORRODED (RT WING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION BEAM FWD SUPPORT BEAM OF RT WING LE CAVITY LOWER FIXED PNL ILES 817. IAW SRM 57-41-13-1A-1 DETAIL V REV 27 REMOVED CORROSION AREA & APPLY PROTECTIVE COATING IAW SRM 51-20-01-0G-0 REV 27.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 73,578 hrs · 14,401 cycles

CORROSION SKIN PLATE OF LT WING UPPER LE FIXED PNL UPPER SURFACE ILES 514. REPLACED DAMAGE PARTS WITH NEW PARTS IAW SRM 51-40-02-0G-0 REV 28 & SRM 51-40-04 REV 28. CONDITION CHECKED NORMAL & JOB COMPLETED.

Part: CIRCUIT BREAKER — DAMAGED · airframe 71,629 hrs · 14,041 cycles

DURING TAKEOFF, MULTIPLE EICAS MESSAGES APPEARED. DUMPED FUEL AND RETURNED TO DEPARTURE. (DURING TROUBLESHOOTING FOUND CIRCUIT BREAKER C3140 (BUS 3 PWR SUPPLY) POPPED. FURTHER INSPECTION REVEALED BREAKER ASSY DAMAGED. R & R CIRCUIT BREAKER IAW & NBSP; SWPM 20-00. OPS CHECK OF BUS 3 WAS NORMAL IAW AMM 24-23-01. EICAS MESSAGES CLEARED.

Part: CONTROL UNIT — INOPERATIVE (TE FLAPS) · airframe 6,320 hrs · 1,114 cycles

DURING APPROACH, FLAPS WOULD NOT GO TO 20 OR 25 AND TURN GREEN. FLAPS 30 SELECTED AND TRAVELED TO 30 AND WENT GREEN (LEFT FCU STATUS MSG. LEFT FCU REPLACED IAW AMM)

Part: FRAME — DAMAGED (BS 320) · airframe 70,835 hrs · 13,894 cycles

DURING THE D2/C2/A2 CHECK IAW EO 4453A295/ SB 747-53A2784 FOUND THE CROWN FRAME WEB AT BS 320 TO BE UNDERSIZED REQUIRING REPLACEMENT. WHILE ACCOMPLISHING THE WEB REPLACEMENT IAW PART 2 OF EO 4453A295, EGAT NOTICED SEVERAL DEVIATIONS FROM THE SB REQUIREMENTS. ACCOMPLISHED EI NR T2012A53B-2850 REV 00 AND REV 01. JOB COMPLETED AND CONDITION CHECKS NORMAL.

Part: FLOORBOARD — DAMAGED (MAIN DECK) · airframe 70,515 hrs · 13,833 cycles

DAMAGE FOUND TO SECTION 46 MAIN DECK - FLOORBOARD BS 2060 - LBL 5.0 TO RBL 5.0 GOUGED AND DELAMINATION DAMAGE. THE GOUGED AREA MEASURES APPROX 12.0 IN. X 5.0 IN. DAMAGE IS BEYOND THE SRM 53-00-50, FIG 101. ALLOWABLE DAMAGE 1 LIMITS, DUE TO ITS LOCATION: DAMAGE IS NOT PERMITTED WITHIN 3.0" OF THE FLOOR PANEL EDGE. PERFORMED A TIME LIMITED REPAIR IAW EO 4453A774.

Part: ACCESS PANEL — DAMAGED (VERTICAL STAB) · airframe 69,055 hrs · 13,576 cycles

LEFT VERTICAL STABILIZER 324GL ACCESS PANEL HAS ELONGATED HOLES.

Part: LINE — LOOSE (RUDDER ACTUATOR)

EICAS MESSAGE HYD QTY LOW 1. SERVICED HYD OPENED RUDDER ACTUATOR PANELS, INSPECTED AREA, OPERATED SYS 1. TIGHTENED LOOSE PRESSURE LINE ON UPPER RUDDER ACTUATOR. LEAK CHECK OK IAW MM 291100 ALL PANELS CLOSED

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 69,043 hrs · 13,574 cycles

FOUND CABIN EMERGENCY LIGHT BATTERY (M14523) LOW. REPLACED EMERGENCY LIGHT BATTERY IAW AMM33-51-04-902-001-001, REV 72 AND PERFORMED OPS TEST RESULT WAS SATISFACTORY.)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,043 hrs · 13,574 cycles

FOUND CABIN EMERGENCY LIGHT BATTERY (M14523) LOW IAW AMM 33-51-04-902-001-001, REV 72. REPLACED BATTERY AND PERFORMED OPS TEST. RESULT SATISFACTORY.

Part: SKIN — CORRODED (LT WING)

LT WING L/E LOWER SKIN AT FRONT SPAR EXFOLIATED STA OLES 1534. REMOVED CORROSION, CUT OUT DAMAGE, NDT AREA, FABBED AND INSTALLED REPAIR PER ECRA 780-57-020-2.

Part: SKIN — DAMAGED (BS 440 S40R) · airframe 63,048 hrs · 13,395 cycles

DAMAGE TO SKIN AND WEB NEEDS REPAIR AT BS 440, STR 40 RT. ACCOMPLISHED ECRA 780-53-019-1 PER SRM 53-00-01 DETAIL 3 AT STA. 420 STR 41R, WITHIN SRM LIMITS

Part: SKIN — DENTED (BS 2640)

FUSELAGE SKIN BS 2640 LBL 16, DENT OUT OF LIMITS. REMOVED DAMAGED AREA, NDT AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 400 LCF 53-30-01 PG 3 ITEM 7, 53-00-01 REPAIR 6PG 201-204 51-30-50, PG 5, 51-10-02 PG 6-7. (K)

Part: STRINGER — CRACKED (BS 480-499 S10L)

BS 480-499 STRINGER 10 LT STRINGER IS CRACKED. REPAIRED CRACKED STRINGER AT BS 480 & 500 IAW SB747-53A2484, FIG 18 AND 20. (K)

Part: STRINGER — CRACKED (BS 480 S10R)

BODY STATION 480, STRINGER 10 RT CRACKED. REPAIRED STRINGER IAW SB 747-63A2484, FIG 24. (K)

Part: SKIN — DENTED (BS 220-260)

(2) DENTS IN FUSELAGE SKIN BS 220-260, STRINGER 30 RT-32 RT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-00-01 PG 201-211, REPAIR 1 DETAIL, FIG 201. (K)

Part: SLIDE — LOW PRESSURE (ENTRY DOOR) · airframe 65,349 hrs · 12,935 cycles

LT ENTRY DOOR 31 ESCAPE SLIDE INFLATION BOTTLE PRESSURE IS "0" PSI. REMOVED AND REPLACED SLIDE PER B747 MM 25-69-00.