N263SG

Part: BATTERY — NO TEST (ZONE 200) · airframe 53,878 hrs · 6,923 cycles

EMERGENCY LIGHTS INOP AT L1 DOOR AND R1 DOOR.(<P>REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY ASSY IAW AMM 33-51-04. OPS CHECK GOOD. REF AIPC 24-31-00-50D. (SN: 126523 PN: 2013-1A &AMP; SN: 105679 PN: 2013-1A)</P>)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 53,864 hrs · 6,922 cycles

FOUND DR I-R SLIDE EMERGENCY LIGHT ASSY (X323) FUCTION FAIL.(<P>1. REFERENCE AIPC 33-51-06-0J REV 88 AND IAW 33-51-00-715-001 REV 113. REPLACED DR I-R SLIDE EMERGENCY LIGHT ASSY (X323) AND PERFORMED EMERGENCY LIGHT OPERATIONAL TEST, THE RESULT WAS SATISFACTORY.</P>)

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 53,864 hrs · 6,922 cycles

FOUND ESCAPE PATH LIGHTING DETERIORATION OR MISSING IN SEVERAL CABIN AREA.(<P>1. REPLACED ESCAPE PATH LIGHTING IN SEVERAL CABIN AREAS (PN: SG8500, SG501, SG8503, SG8519) IAW DRAWING SG-B747 REV E. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.&NBSP;</P>)

Part: LIGHT — NO TEST (ZONE 200) · airframe 53,864 hrs · 6,922 cycles

FOUND ZONE E CREW REST EMERGENCY LIGHT ASSY (M6916) FUNCTION FAIL.(<P>1. REFERENCE AIPC 33-29-10-40B REV 88 AND IAW AMM 33-51-00-715-001 REV 113. REPLACED ZONE E CREW REST EMERGENCY LIGHT ASSY (M6916) AND PERFORM EMERGENCY LIGHT OPERATIONAL TEST, THE RESULT WAS SATISFACTORY.</P>)

Part: LATCH — WORN (ZONE 800) · airframe 53,864 hrs · 6,922 cycles

WEAR OUT - L1 DOOR LATCH FITTING AT FWD UPPER.(<P>1. REPAIR - CHAFING DAMAGE ON FITTING OF L1 DOOR SURROUND STRUCTURE FWD FRAME AT STA 434 IAW EGAT EI T2025A53M-720 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SPAR WEB — CORRODED (ZONE 100) · airframe 53,864 hrs · 6,922 cycles

CORROSION DAMAGE ON CENTER WINF REAR SPAR WEB LH SIDE NEAR JETTISON PUMP AT LBBL 90, STA 1240.(<P>1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 123. 2. PFM NDT INSP REFER TO JOB CARD ATTACHING SHEET NO: 0447498 &AMP; DATA SHEET NO: 10851928-1; 10851928-2; 10851928-3. 3. ACCOMPLISHED EI NO: T2025A57M-668 REV 1. 4. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: WIRE — CHAFED (ZONE 400) · airframe 53,864 hrs · 6,922 cycles

FOUND #3 ENG POWER FEEDER CABLE CHAFING. (W280-133-1/0).(<P>1. REPLACED #3 POWER FEEDER CABLE (W280-133-1/0) IAW AMM 24-11-01-004-055-001, 24-11-01-404-024-001 REV 113, WDM 24-21-31 REV 69 AND SWPM 20-30-13 REV 88. 2. PERFORMED GENERATOR DRIVE SYSTEM OPERATIONAL TEST IAW AMM 24-11-00-705-001 REV 113 AND TEST RESULT WAS SATISFACTORY.</P>)

Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 53,864 hrs · 6,922 cycles

FOUND U/D EMERGENCY LIGHT BATTERY CHARGER ASSY (M5051) FUNCTION.(<P>1. REPLACED U/D EMERGENCY LIGHT BATTERY CHARGER (M5051) IAW AMM 33-51-04-002-009-001 AND AMM 33-51-04-402-012-001 REV 113. 2. PERFOMED EMERGENCY LIGHT BATTERY CHARGER INSTALLATION TEST IAW AMM 33-51-04-402-012-001 REV 113 AND THE RESULT WAS SATISFACTORY.</P>)

Part: BEAM — CORRODED (ZONE 500) · airframe 53,864 hrs · 6,922 cycles

CORROSION - BEAM, L/H WING OUTBD L/E CAVITY LOWER PNL SUPPORT BEAM INNER FACE, AT OLES 1380 AND OLES 1413.(<P>1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV: 123. 2. PFM NDT INSP REFER TO JOB CARD ATTACHING SHEET NO: 0477877. 3. MEASURED REWORK AREA OLES 1380 DEPTH(X) = 0.001", LENGTH = 0.6", WIDTH = 0.5", OLES 14134 DEPTH(X) = 0.003" LENGTH = 0.7", WIDTH = 0.5". IT WAS ALLOWABLE IAW SRM 57-41-13-1A1, DETAIL V REV 123. 4. APPLY PROTECTIVE COATING AT REWORK AREA IAW SRM 51-20-01-0G-0, REV 123. 5. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: BATTERY — UNKNOWN (UNKNOWN) · airframe 53,275 hrs · 6,731 cycles

EMERGENCY EXIT SIGN ROW 11 INOP, TOP DECK OF THE STAIRS EXIT SIGN INOP, MD LH SIDE OF ENTRY DOOR EXIT SIGN INOP, TOP DECK ROW 15 EXIT SIGN INOP, RH MID GALLEY AND CEILING EXIT SIGN INOP, RH SIDE CEILING AND SERVICE DOOR OVER WING EXIT SIGN INOP(<P>ALL LOCATIONS LISTED HAD EMERGENCY EXIT LIGHT BATTERIES REPLACED IAW AMM 33-51-04. REF NR 30,31,32,33,34,37 UNDER W/O 113819</P>)

Part: BATTERY — INOPERATIVE (ELT) · airframe 53,193 hrs · 6,701 cycles

MAIN DECK FIXED EMERGENCY LOCATOR TRANSMITTER BATTERY DUE FOR SHOP VISIT P/N 1096801-1(<P>REPLACED ELT FXED BATTERY &AMP; OPS CHECK ELT SYS OK PER AMM 23-24-01.</P>)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,767 hrs · 6,514 cycles

FORWARD UPPER DECK EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M5932 IAW AMM TASK 33-51-04-902-001-001, OPERATIONAL TEST GOOD.

Part: SENSING ELEMENT — FAULTY (FIRE WARNING) · airframe 52,356 hrs · 6,412 cycles

FOUND EICAS MSG "FIRE WHEEL WELL" DISPLAYED.&NBSP;(<P>PERFORMED WIRING CHECK IAW FIM 26-17 TASK 807 REV.95 AND FOUND SENSING ELEMENT M691A, M692A, M692B, M691B, M694A, M694B RESISTANCE LOW. REPLACED SENSING ELEMENT IAW AMM 26-17-02-004-001,&NBSP; 26-17-02-404-012 REV. 95 AND WDM 26-17-11 REV.44. PERFORMED OPERATIONAL TEST IAW AMM 26-17-00-705-001 REV. 93 AND THE RESULT WAS SATISFACTORY.&NBSP;</P>)

Part: FLIGHT RECORDER — INTERMITTENT (COCKPIT) · airframe 52,356 hrs · 6,412 cycles

FAULT HISTORY, FLIGHT RECORDER FAIL INTERMITTENT.&NBSP;(<P>PERFORMED A WIRE CHECK, NO WIRING PROBLEM WAS FOUND IAW FIM 31-31 TASK 810 REV.95 AND WDM 31-31-11 REV. 44. REPLACED DIGITAL FLIGHT DATA RECORDER, CONDITION CHECK IS NORMAL IAW AMM 31-31-01-404-004 REV. 95. PERFORMED GROUND TEST OF FLIGHT RECORDER IAW AMM 31-31-00-745-090 REV.95, THE RESULT WAS SATISFACTORY.&NBSP;</P>)

Part: SKIN PANEL — DAMAGED (TE FLAP) · airframe 52,356 hrs · 6,412 cycles

RT OUTBOARD MID FLAP, TOP PANEL, 687JT DAMAGE 4" X 6".(<P>PERFORMED RT OUTBOARD MID FLAP TOP PANEL, 687JT REPAIR IAW EI NO. T2019A57M-1898 REV.1. CHECK CONDITION WAS SATISFACTORY.&NBSP;</P>)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,356 hrs · 6,412 cycles

CORROSION FOUND ON FUSELAGE BETWEEN SKIN AND STRINGER AT STA 1720 ~ 1741, S-43R.(<P>REPAIRED CORROSION AREA IAW SRM 53-00-01, REPAIR 1 FIG 201, DETAIL I, REV 105 AND DWG 65B04133 SH2 REV G. JOB COMPLETED AND CONDITION CHECK SATISFIED.&NBSP;</P>)

Part: FEEDER CABLE — DAMAGED (NR 1 IDG) · airframe 52,356 hrs · 6,412 cycles

FOUND NR 1 ENG 2 IDG POWER FEEDER CABLE INSULATION DAMAGE.&NBSP;(<P>REMOVED NR 1 ENG IDG CABLE IAW AMM 54-51-01-004-001 REV. 95. REPAIRED W274-111 AND W 274-112 CABLE IAW SWPM 20-30-11 AND 20-30-13 REV. 70. INSTALLED IDG CABLE IAW AMM 54-51-01-404-046 REV. 95. PERFORMED THE GENERATOR DRIVE SYSTEM OPERATIONAL TEST IAW AMM 24-11-00-705-001 REV.95, RESULT WAS SATISFACTORY.&NBSP;</P>)

Part: BATTERY — FAILED (CABIN) · airframe 52,356 hrs · 6,412 cycles

RQST DISCONNECT ALL OF EMERGENCY LIGHT POWER PACK.&NBSP;(<P>REMOVED CABIN EMERGENCY LIGHT POWER PACK BATTERIES IAW AMM 33-51-04-902-001-001 REV.95 STEP D. INSTALLED CABIN EMERGENCY LIGHT POWER PACK BATTERIES IAW AMM 33-51-04-902-001-001 REV.95, PER STEP E PERFORMED TEST AND FOUND 3 BATTERIES FAIL. TESTED AND REPLACED BATTERIES AND THE RESULT WAS SATISFACTORY IAW AMM 33-51-04-902-001-001 REV. 95.</P><P><BR /></P><P>S/N OFF: TLS 23998, 96723</P>)

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,356 hrs · 6,412 cycles

FOUND EMERGENCY LIGHT BATTERY PACK DEEP CYCLE FAIL AT M7915, M7919, M7920, M7922, AND M7924.(<P>REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT M7915, M7919, M7920, M7922, AND M7924 IAW AMM 33-51-04-902-001-001 REV. 95. PERFORMED POWER SUPPLY TEST AND THE RESULT WAS SATISFACTORY IAW AMM 33-51-04-902-001-001 REV.95 STEP E.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>S/N(S) OFF: 35284, 90174, 106267, 102043</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,123 hrs · 6,336 cycles

RT UPPER DECK DOOR EMERGENCY BATTERY TEST FAILED. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-04.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,963 hrs · 6,301 cycles

LEFT OVERWING EMERGENCY LIGHTS INOPERATIVE, 2 PLACES. REPLACED THE LAMPS AND REPLACED THE FUSE ON POWER SUPPLY M7919 IAW AMM 33-51-03-962-001 AND 33-51-04-900-801. OPS CHECKED GOOD IAW AMM 33-51-03-712-019.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,196,326 hrs · 6,301 cycles

RIGHT AFT OVERWING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMPS AND REPLACED THE FUSE IN POWER SUPPLY M7920 IAW AMM 33-51-03-962-001 AND 33-51-04-900-801. OPS CHECKED GOOD IAW AMM 33-51-03-712-019.

Part: LEVER — NO TEST (ARM - DISARM) · airframe 51,058 hrs · 6,219 cycles

R3 DOOR FAILED MODE SELECTOR LEVER ARM & DISARM TEST. CLEANED AND LUBRICATED THE MODE SELECTOR LEVER MECHANISM IAW AMM 12-21-04-600-804. PERFORMED MODE SELECTOR LEVER TEST. TEST PASSED IAW AMM 52-11-07-705-086.

Part: BATTERY PACK — NO TEST (EMEGENCY LIGHTS) · airframe 51,058 hrs · 6,219 cycles

LEFT UPPER DECK EMERGENCY EXIT POWER SUPPLY BATTERY PACK FAILED A VOLTAGE CHECK. REMOVED AND REPLACED THE BATTERY PACK AND OPS CHECKED GOOD IAW AMM 52-23-14-001 AND AMM 52-23-14-404-005.

Part: LEVER — NO TEST (ARM - DISARM) · airframe 51,058 hrs · 6,219 cycles

L3 DOOR FAILED THE MODE SELECTOR LEVER ARM - DISARM TEST. CLEANED AND LUBRICATED THE MODE SELECTOR LEVER MECHANISM IAW AMM 12-21-04-600-804. PERFORMED MODE LEVER TEST. TEST PASSED IAW AMM 52-11-07-705-084.

Part: LINE — LEAKING (PAX OXYGEN) · airframe 51,058 hrs · 6,219 cycles

PASSENGER OXYGEN LINE IS LEAKING AND CRACKED IN THE RT FWD CARGO WALL. REMOVED AND REPLACED OXYGEN LINE IAW 20-11-05-054-022. LEAK CHECKED GOOD IAW AMM 35-00-00-702-079.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 51,058 hrs · 6,219 cycles

NR 1 ENGINE AFT MOUNT IS CORRODED THROUGH OUTER PLATING. ACCOMPLISHED A REPAIR IAW EA 747-7120-28-A6988 I/R, AND EO 1971A158.

Part: LEVER — NO TEST (L1 DOOR) · airframe 51,058 hrs · 6,219 cycles

L1 DOOR FAILED MODE SELECTOR LEVER ARM - DISARM TEST. CLEANED AND LUBRICATED THE MODE SELECTOR LEVER MECHANISM IAW AMM 12-21-04-600-804. PERFORMED MODE SLECTOR LEVER TEST. TEST PASSED IAW AMM 52-11-07-705-086.

Part: SKIN — CRACKED (LT WING) · airframe 51,058 hrs · 6,219 cycles

LEFT WING L/E UPPER SURFACE PANLE HAS A TWO FOOT CRACK JUST AFT OF THE NR 10 VARIABLE CAMBER FLAP FROM ILES 693 - 822. REMOVED THE SKIN AND HONEYCOMB CORE, FABRICATED AND INSTALLED A REPLACEMENT SKIN AND HONEYCOMB CORE IAW SRM 51-70-07, PARA 4.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,330 hrs · 6,136 cycles

ALL EMERGENCY LIGHTS IN ZONE C INOPERATIVE. REPLACED THE BATTERY ASSY IAW AMM 33-51-00, OPS CHECKED NORMAL.

Part: ENGINE — FAILED (NR 4) · airframe 50,065 hrs · 6,117 cycles

AFTER TAKE OFF, AND DURING LANDING GEAR RETRACTION. A LIGHT AIRFRAME VIBRATION AND RIGHT YAW WAS OBSERVED. SHORTLY AFTER, NR 4 ENGINE N1 EXCEEDENCE WAS OBSERVED, PERFORMED PRECAUTIONARY NR 4 ENGINE SEVERE DAMAGE CHECKLIST. FOUND ENGINE AT FAULT, REMOVED AND REPLACED THE NR 4 ENGINE IAW AMM 71-00-00. OPS CHECKED SATISFACTORY.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,504 hrs · 6,073 cycles

R1 DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BULB.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,504 hrs · 6,073 cycles

L1 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE BULBS.

Part: LIGHT — INOPERATIVE (CREW REST) · airframe 49,504 hrs · 6,073 cycles

AFT CREW REST EMERGENCY LIGHT INOPERATIVE. REPLACED THE EMERGENCY LIGHT ASSEMBLY.

Part: FUSE — INOPERATIVE (COCKPIT) · airframe 49,504 hrs · 6,073 cycles

FLIGHT DECK EMERGENCY LIGHT INOPERATIVE. REPLACED THE FUSE IN M5932 POWER SUPPLY.

Part: BOLT — CORRODED (AILERON) · corrosion level 2 · airframe 48,655 hrs · 6,011 cycles

DURING PFM OTBD AILERON PCA REPLACE FOUND BOTH PISTON ROD BOLTS CORROSION. IAW AMM 27-11-13-002-001 REV 85 STEP F E. REMOVED THE OTBD AILERON PCA PISTON ROD BOLTS AT OTHER SIDE. IAW AMM 27-11-13-402-012 REV 85 STEP G INSTALLED OTBD AILERON PCA PISTON ROD BOLTS AT BOTH SIDES. CONDITION CHECKED SATISFACTORY.

Part: TUBE — BENT (PAX O2 MASK) · airframe 48,655 hrs · 6,011 cycles

FOUND PAX OXYGEN MASK TUBE BENT & DISCOLORED AT 39C, 41C, 2 EA, 42C, 38H, 37H, 36A, 37D, 38D, 39G, 2 EACH, 39D 2 EACH, 40G, 40E, 41E, 41F, CREW REST RT 2 EACH CREW REST LT UP, 37K, TTL 2 EACH. IAW AMM 35-21-32-002-032-001 REV 85, AMM 35-21-36-002-032-001 REV 85, AMM 35-21-31-002-058-001 REV 85 & AMM 35-21-32-402-037-001 REV 85, AMM 35-21-31-402-064-001 REV 85, AMM35-21-31-36-402-307-001 REV 85. REPLACED PAX OXYGEN MASK, 22 EACH.

Part: TUBE — BENT (PAX O2 MASK) · airframe 48,655 hrs · 6,011 cycles

FOUND PX OXYGEN MASK TUBE BENT & DISCOLORED AT 10A, 12C, 14C, 14A, INBD, 14A OTBD 14H, 2A, B546A, 224, 22E, 22D, 24H INBD, 22H, 22G, 22E, 22D OTBD, 22H, 26A, 27A, 22C INBD, 22D CTR TO TOTAL, 21 EACH IAW AMM 35-21-34-002-032-001 REV 85, AMM 35-21-33-002-32-001 REV 85, AMM 35-21-32-002-032-001 REV 85, AMM 35-21-31-002-032-001 REV 85, AMM 35-21-34-402-037-001 REV 85, AMM 35-21-33-402-037-001 REV 85, AMM 35-21-32-402-037-001 REV 85 & AMM 35-21-31-402-064-001 REV 85, REPLACED PAX OXYGEN MASK.

Part: LIFE VEST — BROKEN (CABIN) · airframe 48,655 hrs · 6,011 cycles

FOUND LIFE VEST BROKEN AT 34D, 40H, ZONE A CTR 2. IAW AMM 25-62-05-206-001 REV 85 REPLACE LIFE VEST AT 34D, 40H, ZONE A CTR 2.

Part: CHANNEL — CORRODED (LT WING) · airframe 48,655 hrs · 6,011 cycles

CORROSION LT WING LE CAVITY INSIDE, LOWER PANEL SURFACE, UPPER CHANNEL SURFACE CORROSION OLES 1420. BLEND OUT THE DAMAGED AREA LXDXW=1.1"X0.002"X0.8" WHICH WAS WITHIN ALLOWABLE LIMIT IAW 57-00-03-1A-1. ALLOWABLE DAMAGE 1 FIG T 101 DETAIL II REV 96. DETAIL DATA REF JC ATTACHING SHEET NR 050648. APPLY PROTECTIVE TREATMENT & PRIMER IAW SRM 57-20-01 REV 96 4. JOB COMPETED & CONDITION CHECKED NORMAL.

Part: FIRE BOTTLE — SCRATCHED (LAVATORY) · airframe 48,655 hrs · 6,011 cycles

FOUND LAVATORY FIRE EXTINGUISHER SCRATCHED AT B545A, DC2, B546A, FC4, 4 EACH. REPLACE LAVATORY FIRE EXTINGUISHER AT B545A, DC2, B546A, FC4, 4 EACH IAW AMM 26-27-01-004-001-002 REV 85 & AMM 26-27-01-404-006-002 REV 85.

Part: TUBE — BENT (PAX O2 MASK) · airframe 48,655 hrs · 6,011 cycles

FOUND PAX OXYGEN MASK TUBE BENT & DISCOLORED AT CC1 INBD, CC1 OTBD, DC1,31A,34A, 34C,32K,43K,43HY & 35K TTL. 10 EA IAW AMM 35-21-32-002-032-001 REV 85 AMM 35-21-34-002-032-001 REV 85 & AMM 35-21-32-402-037-001 REV 85, 35-21-34-402-037-001 REV 85 REPLACE PAX OXYGEN MASK.

Part: CHANNEL — CORRODED (LT WING) · airframe 48,655 hrs · 6,011 cycles

CORROSION, LT WING LE CAVITY INSIDE, LOWER PANEL UPPER SURFACE, UPPER CHANNEL SURFACE CORROSION, OLES 1550. BLENDED OUT THE DAMAGE AREA L X W X D = 0.9" X 0.005", WHICH WAS ALLOWABLE LIMIT IAW SRM 57-00-03-1A-1. ALLOWABLE DAMAGE I FIG 101 DETAIL II REV 96 & 2. DETAIL DATE IAW TO JC ATTACHING SHEET NO 0050653 & 3. APPLY PROTECTIVE TREATMENT & PRIMER IAW SRM 51-20-01 REV 96 & 4. JOB COMPLETED & CONDITION CHECKED NORMAL.

Part: SLIDE — UNWANTED DEPLOY (L2 DOOR) · airframe 48,163 hrs · 5,974 cycles

DOOR L2 SLIDE INADVERTENTLY DEPLOYED. R & R L2 SLIDE IAW 25-65-16-404-022 & OK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 47,714 hrs · 5,941 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEAT 15AC, SEAT 11AC, L4 DOOR, ABOVE SEAT 41LT AISLE & AT TOP OF STAIRS TO UPPER DECK. REPLACED EMER LAMPS AT L4 DOOR, SEATS 11AC & 15AC IAW AMM 33-51-06. REPLACED EMER BATTERY AT M5932, M5933 & M5218 IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.

Part: OVEN — DIRTY (GALLEY) · airframe 46,491 hrs · 5,843 cycles

FIRST CLASS OVEN INOPERATIVE. DEBRIS IN BASE CAUSING SMOKE. REMOVED DEBRIS & CLEANED RESIDUE. OPERATIONS CHECKED GOOD IAW FIM 21-00 TASK 810. NO SMOKE OR SMELL NOTED. IAW AMM 05051056-200-801 SMOKE OR FUMES IN CABIN INSPECTION COMPLIED WITH.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 46,214 hrs · 5,823 cycles

2L EMER LIGHTS WILL NOT ILLUMINATE DURING TEST. R & R 2LDOOR EMER LIGHT BATTERY PACK IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 45,901 hrs · 5,799 cycles

ZONE A & B EMER LIGHT INOPERATIVE. R & R EMER POWER SUPPLY ASSEMBLY IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (DOOR) · airframe 45,317 hrs · 5,757 cycles

RIGHT UPPER DECK DOOR EMER POWER SYS BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK IAW AMM 52-23-14. OPERATIONAL CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,041 hrs · 5,737 cycles

R2 DOOR EMER LIGHT INOPERATIVE. R & R R2 DOOR SLIDE LIGHT ASSEMBLY IAW AMM 33-51-06. OPERATION NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,041 hrs · 5,737 cycles

L1 DOOR EMER LIGHT INOPERATIVE. R & R THE L1 DOOR SLIDE LIGHT ASSEMBLY IAW AMM 33-51-06. ALL OPERATIONS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 45,041 hrs · 5,737 cycles

FORWARD RT OVERWING EMER LIGHTS INOPERATIVE. REPLACED BATTERY CHARGER AT L3 DOOR IAW AMM 33-52-00. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 45,041 hrs · 5,737 cycles

R5 DOOR EMER LIGHT INOPERATIVE. R & R R5 DOOR SLIDE LIGHT ASSEMBLY IAW AMM 33-51-06. OPERATION NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 45,010 hrs · 5,734 cycles

L5 DOOR EMER EXIT LIGHTS WILL NOT ILLUMINATE. PERFORMED RING OUT OF EMER LIGHT IAW 33-51-62. FOUND EMER BATTERY TO BE INOPERATIVE. REPLACED BATTERY AT DOOR L5. OPERATIONS CHECKED OK IAW AMM 33-51-04.

Part: STRUCTURE — GOUGED (LT MLG WW) · airframe 45,010 hrs · 5,734 cycles

LEFT WING GEAR WW 3/4 INCH GOUGE ON STRUCTURE JUST FWD ON LT BODY GEAR UPPER DRAG STRUT SPINDLE. REWORKED GOUGE, ACCOMPLISHED NOT INSPECTIONS & RESTORED FINISH IAW AMM 51-24-11.

Part: OXYGEN MASK — UNWANTED DEPLOY (COCKPIT) · airframe 44,952 hrs · 5,729 cycles

AT GATE, FIRST OFFICER DEPLOYED O2 MASKS. STOWED O2 MASKS IAW MM 35-40-02 & MM 35-21-31.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,842 hrs · 5,721 cycles

R4 EMER OVERHEAD DOOR MOUNTED LIGHT DID NOT TEST. R & R BOTH SETS OF BATTERY PACKS ON THE R4 DOOR MOUNTED EMER LIGHT ASSEMBLY. OPERATIONS CHECKED GOOD. CHARGE TEST OK IAW AMM 33-51-06-400-801.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,842 hrs · 5,721 cycles

L5 EMER OVERHEAD DOOR MOUNTED LIGHT DID NOT TEST. R & R BOTH SETS OF BATTERIES ON THE L5 DOOR MOUNTED EMER LIGHT. OPERATIONS CHECKED GOOD. CHARGING TEST OK IAW MM 33-51-06-400-801.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 44,842 hrs · 5,721 cycles

DOOR L3 EMER LIGHT BATTERY DEAD. REPLACED BATTERY, OPERATIONS CHECKED GOOD IAW AMM 33-50-00.

Part: LIGHT — UNSECURE (CABIN) · airframe 44,595 hrs · 5,703 cycles

EMERGENCY LIGHT STRIP FWD GALLEY AT CARTS 705 & 706 NEEDS TO BE GLUED DOWN. SECURED EMER LIGHT STRIP IAW MANUAL M39-13.

Part: BATTERY PACK — FAILED (CABIN) · airframe 43,435 hrs · 5,611 cycles

DURING ROUTINE MAINTENANCE THE LT UPPER DECK DOOR ESCAPE LIGHT BATTERY FAILED OPERATIONAL CHECK. REPLACED LT UPPER DECK ESCAPE LIGHT BATTERY PACK IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.

Part: WINDOW FRAME — DAMAGED (CABIN) · airframe 43,213 hrs · 5,595 cycles

PREPARING FOR DEPARTURE AT THE GATE, THE DATUM ACFT SUFFERED LIGHTNING STRIKE DAMAGE AT THE WINDOW FRAME BETWEEN STA 860 & STA 880, STR 19L TO STR 23L. DAMAGE IS REPORTED AS A MELTED WINDOW FRAME FLANGE APPROX 5" X 0.010". DAMAGE ON THE WINDOW PLUG IS DETERMINED TO BE LIMITED TO SURFACE FINISH DAMAGE. AFTER DAMAGE REMOVAL & FURTHER EVALUATION, THE BLENDED OUT AREA MEASURED APPROX 5" LONG X 0.015" WIDE. THE REMAINING THICKNESS MEASURED AT THE DEEPEST POINT IS 0.021". THICKNESS OF MATERIAL REMOVED ON THE OUTER SURFACE OF THE WINDOW FRAME FLANGE IS 0.050". REFER TO FIGURE 2, THE MATERIAL LOST FOR DAMAGE REMOVAL IS BEYOND THE 747-400 SRM 56-20-02 ALLOWABLE DAMAGE 1, DISPOSITION IS TO ACCOMPLISH A TIME LIMITED REPAIR IAW PART 1 OF EO 44546A019, IAW SRM 56-20-02 FIGURE 201 REPAIR 1 & PERMANENT REPAIR AS GIVEN IN PART 2 OF EO 4456A019.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 42,664 hrs · 5,552 cycles

AFTER TAKEOFF, HYDR QTY AND PRESSURE WENT TO ZERO ON SYS 4 FLAPS ASYMETRIC AND WOULD NOT RETRACT. FUEL JETTISONED AND RETURNED TO DEPARTURE. REPAIRED IAW AMM 12-00-00.

Part: SKIN — DENTED (BS 1780) · airframe 41,384 hrs · 5,457 cycles

LEFT SIDE FUSELAGE FS 1780, STRINGER 27L SKIN DENTED. INSTALLED REPAIR DOUBLER ON LT SIDE OF FUSELAGE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,384 hrs · 5,457 cycles

SEVERAL EMERGENCY LIGHTS OUT IN MAIN CABIN. REPLACED LAMP IAW AMM TASK 33-51-12-962-002.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,384 hrs · 5,457 cycles

ZONE 6 UPPER DECK RIGHT HAND EXIT DOOR EXIT IDENTIFIER SIGN GOES OUT AFTER 1 MINUTE. R & R BATTERIES IN POWER SUPPLY M5057. TESTED IAW CMM 25-60-03, REV 7, SEPT 2010.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,384 hrs · 5,457 cycles

L5 DOOR SLIDE LIGHT OUT. R & R TWO BATTERY PACKS. TESTED IAW CMM 33-50-14, REV 8.

Part: SEAT TRACK — DAMAGED (BS 571) · airframe 41,050 hrs · 5,429 cycles

MX REPORTED DAMAGE TO THE LOWER LOBE, FWD CARGO COMPARTMENT BS 571, RBL 24.75, SEAT TRACK CRACKED AND DAMAGE. DAMAGE EXCEEDED SRM 53-00-52-1A-1 ALLOWABLE DAMAGE LIMITS. PERFORMED A TIME LIMITED REPAIR.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

SEAT 38 AREA LEFT CEILING EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK, OPS CHECK OK IAW MM 33-51-04.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

SEAT 36 AREA RT CEILING EMERGENCY LIGHTS INOP. R & R EMERGENCY POWER SUPPLY IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

SEAT 31 TO SEAT 35 RT AND LT EMERGENCY CEILING LIGHTS INOPERATIVE. REPAIRED EMERGENCY LIGHTS. OPS CHECKED OK IAW AMM 33-51-04)

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT)

MAIN DECK SEAT 31 AREA IN FRONT OF L2 EXIT SIGN INOPERATIVE. REPAIRED IAW AMM 33-51-04.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT)

UPPER DECK EMERGENCY DOOR RT EXIT SIGN INOPERATIVE. R & R PWR SUPPLY M7050. OPS CHECKED OK IAW AMM 33-51-04.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS)

MAIN DECK R5 DOOR EXIT SIGN INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM 33-51-06.004-046. OPS CHECKED NORMAL AMM 33-51-06-404-049.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

MAIN DECK R2 DOOR EXIT SIGN INOPERATIVE. RELAMPED MAIN DECK R-2 DOOR EXIT LIGHT. OPS CHECKED OK IAW MM 33-51-06-962-048.

Part: FAN — FAILED · airframe 5,313 hrs · 39,568 cycles

BURNING SMOKE ODOR NOTICED IN CABIN AREA FOR APP 10 MIN SHORTLY THEREAFTER, EICAS STATUS MESSAGE LWR LT RECIRCULATION FAN FAILED, CIRCUIT BREAKER FOR RECIRCULATION FAN TRIPPED AND ODOR DISSIPATED. QRH C/W CREW CONTINUED WITH FLIGHT. RECIRCULATION FAN LWR LT C/W CHAPTER 5 INSPECTION IAW AMM 05-51-56, NO FURTHER FINDINGS NOTED. IAH MX INSPECTER LOWER RECIRCULATION FAN, AND FOUND INOPERATIVE. RT LOWER RECIRCULATION FAN, AND OPS CHECKED NORMAL.

Part: CIRCUIT CARD — MALFUNCTIONED (FIRE DETECTION) · airframe 39,151 hrs · 5,276 cycles

NR 4 ENGINE FIRE WARNING MESSAGE. COMPLIED WITH QRH, AIR TURN BACK, IN-FLIGHT SHUTDOWN. MX CURRENTLY TROUBLESHOOTING CARDS. UPPER FWD LOOP & AMP AFT LWR REPLACED. MX TO REPLACE LWR FWD & AMP UPPER AFT. INSPECTED PER EO 4426A052. ACCOMPLISHED ENGINE BLEED CHECKS PER MM. ALL SYSTEMS OPERATE NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,893 hrs · 5,256 cycles

UPPER DECK RT EMERGENCY EXIT DOOR PUSH TO TEST LIGHT INOPERATIVE. R & R UPPER DECK RT EMERGENCY EXIT DOOR BATTERY PACK IAW AMM 33-51-04. OPS CHECKED OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 38,893 hrs · 5,256 cycles

MAIN PASSENGER CABIN R5 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R POWER SUPPLY BATTERY PACK M7924 WDM 33-51-61 IAW MM TASK 33-51-04. OPS CHECKED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (A/C PACK) · airframe 38,469 hrs · 5,223 cycles

PACK 1,2,3 ILLUMINATED DURING CRUISE ALL RESET WITH PACKS IN B MODE EICAS PACK 1,2,3 SIMULTANEOUSLY. PACKS NEVER TRIPPED OR CLOSED. RESET PACK 1,2,3 PERFORMED GROUND TEST ON ALL PTC A+B NO DEFECTS NOTED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,990 hrs · 5,185 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 21 LT SIDE AISLE, CEILING. RELAMPED EMERGENCY CEILING LIGHT LIGHT AISLE, ROW 21. REF AMM 33-51-07. OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,990 hrs · 5,185 cycles

EMERGENCY EXIT LIGHT INOPERATIVE AT R2 DOOR SIDE. TROUBLESHOT TO LIGHT ASSY. IPC 33-51-06-05 ITEM 5. R & R EMERGENCY LIGHT ASSY IAW MM 33-51-06. OPS CHECKED OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 37,990 hrs · 5,185 cycles

EMERGENCY EXIT LIGHT INOP AT OVERHEAD L1 DOOR. RELAMPED REF AMM 33-51-07, OPS CHECKED NORMAL.

Part: WING — DAMAGED (RIGHT) · airframe 36,110 hrs · 5,047 cycles

DURING TAXI IN, TOP AND RT WING WINGLET CAME IN CONTACT WITH PARKED ACFT (EO 4457A308 ISSUED. PART 1 TIME LIMITED REPAIR ACCOMPLISHED. PART 2 REPEAT INSPECTIONS TO BE ACCOMPLISHED. PART 3 PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO THE ACCUMULATION OF 10 FLIGHT CYCLES.)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,089 hrs · 5,045 cycles

R5 DOOR EMERGENCY LIGHT INOP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,589 hrs · 5,004 cycles

DURING WALK-AROUND INSP, MX FOUND DAMAGE TO THE BS 1980 CARGO DOOR CUTOUT - FWD LOWER CORNER FUSELAGE SKIN DENT/CRACK, REPAIRED IAW ALL APPROPRIATE SRMS.

Part: BOTTLE — FAILED (R1 DOOR) · airframe 35,406 hrs · 4,990 cycles

REPLACEMENT OF NR 1R DOOR ASSIST BOTTLE REQUIRED DUE TO BOTTLE DID NOT BLOW IN SLIDE DEPLOYMENT EXERCISE.

Part: BOTTLE — FAILED (R2 DOOR)

REPLACEMENT OF NR 2R DOOR ASSIST BOTTLE REQUIRED DUE BOTTLE DID NOT BLOW IN SLIDE DEPLOYMENT EXERCISE. DOOR NR 2R ASSIST BOTTLE REPLACED PER MM 52-11-06-404-015. RIG OPERATION OF DOOR ASSIST BOTTLE ALSO ACCOMPLISHED PER MM 52-11-06.

Part: CABLE — OUT OF POSITION (ENTRY DOOR) · airframe 35,406 hrs · 4,990 cycles

DURING EMERGENCY EVACUATION EXERCISE, NR 3L MED FAILED TO AUTO / DEPLOY. FOUND AUDIO/VISUAL ENTERTAINMENT SYSTEM CABLE LODGED IN THE THROTTLE LEVER OF DOOR ASSIST RESERVOIR. REPOSITIONED AND SECURED CABLE. REPLACED DOOR ASSIST RESERVOIR PER AMM 52-11-06-404-015. INSPECTED SURROUNDING AREA AND FOUND NO OTHER ABNORMALITIES.

Part: INTERCOSTAL — DAMAGED (BS 2000) · airframe 35,385 hrs · 4,988 cycles

THE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR ACCOMPLISHED DURING D CHECK. DURING INSPECTION OF DATUM ACFT, CRACK WAS FOUND ON THE INTERCOSTAL AT BS 2000, RBL 55. PERMANENT REPAIR WAS ACCOMPLISHED IAW SRM 51-70-11-0G-0, FIG 1. PERFORM A DETAIL VISUAL INSP OF THE INTERCOSTAL AT BS 2000 (RBL 55) IN BULK CARGO COMPARTMENT TO DETERMINE THE EXTENT OF THE DAMAGE. ACCOMPLISH REPAIR FOR THE BULK CARGO COMPARTMENT INTERCOSTAL AT BS 2000 (RBL 55). 400 SRM 51-70-11-0G-0, FIG 1, EO 4453A313.

Part: FLOOR SUPPORT — DAMAGED (BS 2020) · airframe 35,385 hrs · 4,988 cycles

THE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR ACCOMPLISHED DURING D-CHECK. DURING INSPECTION OF DATUM ACFT, CRACK WAS FOUND ON THE FLOOR SUPPORT AT BS 2020, BL 0- PERMANENT REPAIR WAS ACCOMPLISHED IAW SRM 53-60-53-2R-1 FIG 201.1 . PERFORM A DETAIL VISUAL INSP OF THE FLOOR SUPPORT AT BS 2020 (BL 0) BULK CARGO COMPARTMENT TO DETERMINE THE EXTENT OF THE DAMAGE. ACCOMPLISH REPAIR FOR THE BULK CARGO COMPARTMENT FLOOR SUPPORT AT BS 2020 (BL 0) SRM 53-60-53-2R-1, FIG 201.

Part: ACTUATOR — SEIZED (DOOR ASSIST) · airframe 35,385 hrs · 4,988 cycles

DURING SLIDE DEPLOYMENT THE UPPER DECK LT DOOR DID NOT DEPLOY IN AUTO MODE BUT DID DEPLOY IN THE MANUAL MODE. FOUND DOOR ASSIST ACTUATOR SEIZED. REPLACED ACTUATOR.