N464MC

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 100,901 hrs · 18,909 cycles

CLIMBING PAST FL 200, BURNING ODOR WAS SMELLED IN THE FLIGHT DECK ALONG WITH NOISE AND VIBRATION, ALSO REPORTED BY L2 DOOR AND ZONE C. SUSPECTED A PACK AS CAUSE. TURNED OFF PACKS 1 AT A TIME, COINCIDENTALLY RECYCLED PACK 3 AS POWER WAS REDUCED AT LEVEL OFF ALTITUDE. VIBRATIONS STOPPED AND THE BURNING ODOR CLEARED.(<P>TRANSFER TO MDDR 176871 AS PER&NBSP;MEL 21-51-01-01, CAT 'C'. PACK 3 DEACTIVATED. MCC INFORMED.&NBSP;</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 118,901 cycles

CABIN-STA 1660 LBL 40" FLOOR TRACK FOUND CORROSION(<P>CABIN-STA 1590-1770 LBL 40" FLOOR TRACK PN: 140U5617-19 RACK REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02</P>)

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 1846 RBL 35" FLOOR BEAM SPLITTER FOUND CORROSION.(<P>CABIN-STA 1846 RB 34"-40" FLOOR PANEL SPLITTER P/N: FSS1174A0507S100 FABRICATED AND REPLACED IAW ATLAS EO: 4453B792 REV. 0.</P>)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 780 LBL 116 FLOOR SUPPORT FOUND CORROSION(<P>CABIN-STA 780 LBL 116 FLOOR SUPPORT PLATE P/N" 140U5601-782 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02</P>)

Part: SKIN PANEL — DELAMINATED (LT WING) · airframe 100,863 hrs · 18,901 cycles

LHW - UPPER WING SURFACE MOST I/B T/E PANEL FOUND DELAMINATION.(<P>LH FIXED WING I/B T/E UPPER SKIN PANEL REPLACED IAW RI-57-50-13985 REV. A AND SB 747-57-2289.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 1740 LBL 11" FLOOR TRACK FOUND CORROSION(<P>CABIN-STA 1720 TO STA 1770 LBL 11" FLOOR TRACK REPAIRED IAW SRM 53-00-52 FIG 201</P>)

Part: LIGHT — INOPERATIVE (R5 DOOR) · airframe 100,863 hrs · 18,901 cycles

R5 DOOR SLIDE LT FOUND INOP.(<P>R5 DOOR SLIDE LIGHT LAMP REPLACED OPERATION CHECK NORMAL AMM 33-51-06.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,863 hrs · 18,901 cycles

UPPER DECK LAV 8U EMERGENCY LIGHT FOUND INOP.(<P>UPPER DECK LAV 8U EMERGENCY LT LAMP REPLACED AND LAMP TEST NORMAL IAW AMM 33-51-00.</P>)

Part: ACCESS PANEL — TORN (NR 4 PYLON) · airframe 100,863 hrs · 18,901 cycles

#4 PYLON ACCESS PNL #482BL INNER SURFACE CORNER FOUND TORN(<P>#4 PYLON ACCESS PNL #482BL INNER SURFACE TORN AREA PERFORMED METAL HOT BOND REPAIR AS PER RI #: RI-54-50-13970 REV A REV DATE 12MAR2020.</P>)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 940 RBL 75-97 FLOOR BEAM FOUND CORROSION(<P>CABIN-STA 940 RBL 60" TO RBL 124" FLOOR BEAM UPPER CHORD REPAIRED IAW SRM 53-20-51-2R-1 REPAIR 1</P>)

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 100,863 hrs · 18,901 cycles

RH MAIN ENTRY DOOR 5 CUTOUT AFT UPPER CORNER 1 EA FASTENER HOLE FOUND CRACK(<P>RH MAIN ENTRY DOOR 5 CUTOUT AFT UPPER CORNER CRACK AREA MODIFICATION PER SB 53A2839 AND EO" 4453A797 PART 6</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 100,863 hrs · 18,901 cycles

EMERGENCY LIGHT BATTERY PACK (M5057)CAPACITY TEST FAILED.(<P>EMERGENCY LIGHT BATTERY PACK (M5057) REPLACED. INSTALLATION TEST NORMAL AMM 33-51-12.</P>)

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 1630 LBL 11"-33" FLOOR BEAM SPLITTER FOUND CORROSION.(<P>CABIN-STA 1630 LBL 11"-33" FLOOR PANEL SPLITTER P/N: FSS1174A2117T100 FABRICATED AND REPLACED IAW ATLAS EO: 4453B792 REV. 0.</P>)

Part: LIGHT — INOPERATIVE (L4 DOOR) · airframe 100,863 hrs · 18,901 cycles

L4 DOOR SLIPE LT FOUND INOP.(<P>L4 DOOR SLIDE LT REPAIRED AND TEST NORMAL AS PER AMM 33-51-06.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 820-860 RBL 75" FLOOR TRACK FOUND CORROSION(<P>CABIN-STA 830-920 RBL 75" FLOOR TRACK REPAIRED IAW SRM 53-00-52-2R-5 REPAIR 5 FIG 201</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 1840 LBL 11" FLOOR TRACK FOUND CORROSION(<P>CABIN-STA 1820-1870 LBL 11" FLOOR TRACK REPAIRED IAW SRM 53-00-52 FIG 201</P>)

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

FUS-HINGE DOOR #191L ATT FRAME SEBERAL AREA FOUND CORROSION(<P>FUS-HINGE DOOR 191L ATTACHMENT FRAME DOUBLER P/N: 69B16975-8 DAMAGE AREA REPAIRED IAW RI-53-00-13982 REV A</P>)

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 100,863 hrs · 18,901 cycles

M/D-L1 ENTRY DR CTR SCUFF PLATE FOUND CRACK(<P>M/D-L1 ENTRY DR CTR SCUFF PLATE CRACK AREA REPAIRED AS PER RI-13-13964 REV A</P>)

Part: LIGHT — INOPERATIVE (L5 DOOR) · airframe 100,863 hrs · 18,901 cycles

L5 DOOR SLIDE LT FOUND INOP.(<P>DOOR L5 SLIDE LIGHT BULB REPLACED. OPERATIONAL CHECK NORMAL IAW AMM 33-51-06.</P>)

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 100,863 hrs · 18,901 cycles

BULK CARGO COMP LH STA 1920-2040 FLOOR PNL FOUND PUNCH MARK(<P>BULK CARGO COMP FLOOR PANEL PUNCTURE DAMAGE REPAIRED IAW RI-25-13941 REV A</P>)

Part: SKIN — BULGED (LT WING) · airframe 100,863 hrs · 18,901 cycles

LHW UPPER WING SURFACE L/E MOST O/B SIDE SAFETY LINE ATTACH POINT SURROUNDING AREA FOUND BULGE(<P>PERFORMED COMPOSITE HOT BOND REPAIR IAW RI-57-00-13972</P>)

Part: FRAME — CRACKED (FUSELAGE) · airframe 100,863 hrs · 18,901 cycles

FWD CARGO-STA 960 FRAME I/B CHORD FWD FLANGE FOUND CRACKED AT BL 0"(<P>FWD CARGO-STA 960 LWR LOBE FRAME INNER CHORD DAMAGED AREA (WL118" RBL18.5" TO RBL 18.5") REPAIRED IAW SRM 53-20-07-2R-11 REPAIR 11</P>)

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 100,863 hrs · 18,901 cycles

CABIN-ZONE C STA 1060 RBL98.58 TRACK FOUND CRACKED(<P>CABIN-STA 1060 RBL98.58 SEAT TRACK FLANGE CRACK AREA REPAIRED IAW RI-53-40-13968 REV A</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 940-950 RBL 75" FLOOR TRACK FOUND CORROSION(<P>CABIN-STA 920-980 RBL 75 FLOOR TRACK REPAIRED IAW SRM 53-00-52-2R-5 REPAIR 5 FIG 201</P>)

Part: LIGHT — INOPERATIVE (L3 DOOR) · airframe 100,863 hrs · 18,901 cycles

L3 DOOR SLIDE LT FOUND INOP.(<P>L3 DOOR SLIDE LT REPAIRED AND OP TEST NORMAL AS PER AMM 33-51-06.</P>)

Part: ANGLE — DAMAGED (VERTICAL STAB) · airframe 100,863 hrs · 18,901 cycles

VERT STAB-TIP FAIRING LWR WEB RH SIDE T ANGLE AND CHANNEL NUT FOUND DAMAGED(<P>VERTICAL FIN TIP RIB RH CHORD DAMAGED AREA REPAIRED IAW RI # RI-55-31-13974 REV A</P>)

Part: SKIN SPLICE — CORRODED (LT WING) · airframe 100,863 hrs · 18,901 cycles

LHW-L/E UPPER SKIN SPLICE SURFACE AT ILES 337-340 FOUND CORROSION(<P>LHW-ILES 337-340, L/E UPPER SKIN SPLICE AREA CORROSION REMOVED AND REPAIRED IAW SRM 57-20-01-1A-1 ALLOWABLE DAMAGED 1 FIG 101 DETAIL XI</P>)

Part: PANEL SUPPORT — CRACKED (COCKPIT) · airframe 100,863 hrs · 18,901 cycles

COCKPIT-CTR CONSOLE RHS FWD AREA FOUND CRACKED(<P>COCKPIT-RH PILOTS FWD PANEL SUPPORT WEB CRACK AREA REPAIRED IAW RI # RI-53-00-13945 REV A</P>)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 940 RBL 45 FLOOR BEAM FOUND CORROSION(<P>CABIN-STA 940 RBL 0 TO RBL 60 FLOOR BEAM UPPER CHORD REPAIRED IAW SRM 53-20-51-2R-1 REPAIR 1</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 904 RBL 41 FLOOR TRACK FOUND CORROSION(<P>CABIN-STA 880-940 RBL 41 FLOOR TRACK REPAIRED IAW SRM 53-00-52-2R-5 REPAIR 5 FIG 201</P>)

Part: SUPPORT ANGLE — CRACKED (NR 3 PYLON) · airframe 100,863 hrs · 18,901 cycles

#3 PYLON AFT V-FAIRING I/B SIDE SUPPORT ANGLE FOUND CRACK(<P>#3 PYLON STRUT INBD SKATE ANGLE CRACK AREA (NEAR STA 456.36) REPAIRED IAW RI-54-56-13962 REV A</P>)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 936 RBL 116" L-SHAPE ANGLE FOUND CORROSION(<P>CABIN-STA 936 RBL 116" FLOOR SUPPORT CORROSION AREAS REPAIRED IAW RI-53-20-13969 REV A</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 1740-1744 RBL 40" FLOOR TRACK FOUND CORROSION(<P>CABIN-STA 1590-1770 RBL 40" FLOOR TRACK PN: 140U5617-20 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,863 hrs · 18,901 cycles

U/D L/H EMERGENCY EXIT DOOR AFT SLIDE LIGHT FOUND INOP.(<P>U/D L/H EMERGENCY EXIT DOOR AFT SLIDE LIGHT ASSY REPLACED. OPERATIONAL CHECK NORMAL IAW AMM 33-51-06.</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 100,863 hrs · 18,901 cycles

EMERGENCY LIGHT BATTERY PACK (M5058) CAPACITY TEST FAILED.(<P>EMERGENCY LIGHT BATTERY PACK (M5058) REPLACED. INSTALLATION TEST NORMAL AMM 33-51-00.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,863 hrs · 18,901 cycles

AFT CREW REST CEILING EMERGENCY LIGHT FOUND INOP.(<P>AFT CREW REST CEILING EMERGENCY LIGHT REPLACED. INSTALLATION TEST NORMAL IAW AMM 33-51-07.</P>)

Part: FRAME — CRACKED (FUSELAGE) · airframe 100,863 hrs · 18,901 cycles

FWD CARGO-STA 780 FRAME I/B CHORD AFT FLANGE FOUND CRACKED AT LBL 48".(<P>FWD CARGO-STA 780 LOWER LOBE FRAME INNER CHORD DAMAGED AREA (WL118" LBL35.5" TO LBL 75.5") REPAIRED IAW SRM 53-20-07-2R-11 REPAIR 11.</P>)

Part: BEAM — NOT REPORTED (RT MLG DOOR) · airframe 100,863 hrs · 18,901 cycles

RH BODY LANDING GEAR I/B SHOCK DOOR FWD SEAL RETAINER LOOSE(<P>RH BODY LANDING GEAR I/B SHOCK DOOR FWD SEAL RETAINER 65B10920-209 AND STRIP 69B14602-4 AND BEAM 65B11444-10 REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 100,863 hrs · 18,901 cycles

EMERGENCY LIGHT BATTERY PACK (M5059) CAPACITY TEST FAILED.(<P>EMERGENCY LIGHT BATTERY PACK (M5059) REPLACED OPERATIONAL CHECK NORMAL AMM 33-51-12.</P>)

Part: FAIRING — CRACKED (VERTICAL STAB) · airframe 100,863 hrs · 18,901 cycles

VERT STAB FIN FAIRING #321A RH AFT EDGE FOUND CHAFING(<P>VERT STABILIZER L/E DOOR SEAL FIN FAIRING #321A SKIN CRACK AREAS (STA 2280) REPAIRED IAW RI-55-35-13975 REV A</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 1730 RBL 11" FLOOR TRACK FOUND CORROSION(<P>CABIN-STA 1720 TO 1770 RBL 11" FLOOR TRACK REPAIRED IAW SRM 53-00-52 FIG 201</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 100,863 hrs · 18,901 cycles

EMERGENCY LIGHT BATTERY PACK (M7922) CAPACITY TEST FAILED.(<P>EMERGENCY LIGHT BATTERY PACK REPLACED (M7922). INSTALLATION TEST NORMAL AMM 33-51-00.</P>)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 960-975 RBL 15 FLOOR BEAM FOUND CORROSION(<P>CABIN-STA 940-980 RBL 15 FLOOR INTERCOSTAL REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02</P>)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 2348 RBL 32-36 FLOOR SUPPORT FOUND CORROSION(<P>CABIN-STA 2348 RBL 32-36 PN: 65B06642-4 FLOOR SUPPORT REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02</P>)

Part: FUSE — BLOWN (CABIN) · airframe 100,863 hrs · 18,901 cycles

U/D R/H EMERGENCY EXIT AFT SLIDE LIGHT FOUND INOP.(<P>U/D R/H EMERGENCY EXIT AFT SLIDE LT FUSE REPLACED AND LAMP TEST NORMAL IAW AMM 33-51-00.</P>)

Part: SKIN — BURNED (LT MLG DOOR) · airframe 100,863 hrs · 18,901 cycles

LH WING GEAR WHEEL O/B DOOR FOUND BURN MARKS, 3 LOCATIONS(<P>LH MLG WHEEL WELL SECONDARY DOOR OUTER SKIN 3 EACH BURN MARKS AREA REPAIRED IAW RI # RI-52-83-13959 REV A</P>)

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 100,863 hrs · 18,901 cycles

LH MAIN ENTRY DOOR 5 CUTOUT AFT UPPER CORNER 1 EA FASTENER HOLE FOUND CRACK(<P>LH MAIN ENTRY DOOR 5 CUTOUT AFT UPPER CORNER CRACK AREA MODIFICATION PER SB 53A2839 AND EO: 4453A797 PART 5</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 100,863 hrs · 18,901 cycles

EMERGENCY LIGHT BATTERY PACK (M7920) CAPACITY TEST FAILED.(<P>EMERGENCY LIGHT BATTERY PACK (M7920) REPLACED. INSTALLATION TEST NORMAL AMM 33-51-00.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 1770-1780 RBL 41" FLOOR TRACK FOUND CORROSION(<P>CABIN-STA 1770-1880 RBL 40" FLOOR TRACK PN 140U5617-22 FABRICATED PER BOEING PL 140U5617 AND DWG SHEET 1. TRACK REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02.</P>)

Part: SKIN SPLICE — CORRODED (LT WING) · airframe 100,863 hrs · 18,901 cycles

LHW-L/E UPPR SKIN SPLICE SURFACE AT ILES 327-328 FOUND CORROSION(<P>LHW-ILES 327-328, L/E UPPER SKIN SPLICE AREA CORROSION REMOVED AND REPAIRED IAW SRM 57-20-01-1A-1 ALLOWABLE DAMAGED 1 FIG 101 DETAIL XI</P>)

Part: PANEL SUPPORT — CRACKED (COCKPIT) · airframe 100,863 hrs · 18,901 cycles

COCKPIT - CTR CONSOLE LHS FWD AREA FOUND CRACK(<P>COCKPIT - LH PILOTS FWD PANEL SUPPORT WEB CRACK AREA REPAIRED IAW RI # RI-53-00-13945 REV A</P>)

Part: SUPPORT — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

LH HORIZONTAL STAB TE ELEV STA 131.9 (I/B ELEVATOR PCP O/B UPPER AREA) ACTUATOR REACTION SUPPORT 2 EA AREA FOUND CORROSION.(<P>LH HORIZONTAL STABILIZER FIXED T/E ACTUATOR SUPPORT CORROSION AREA REPAIRED IAW RI # RI-55-10-13973 REV A.</P>)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

M/D-STA 860-920 LBL 40 FLOOR SUPPORT FOUND CORROSION(<P>CABIN-STA 860-920 LBL FLOOR SUPPORT PLATE P/N: 69B17613-42 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02</P>)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 1765 CTR FLOOR BEAM INTERCOSTAL FOUND CORROSION.(<P>CABIN-STA 1760-1780 CTR O" FLOOR INTERCOSTAL P/N: 98FS818258-111 FABRICATED AND REPLACED IAW ATLAS EO: 4453B792 REV. 0.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 100,863 hrs · 18,901 cycles

CABIN-STA 1770-1780 LBL 41" FLOOR TRACK FOUND CORROSION(<P>CABIN-STA 1770-1880 LBL 40" FLOOR TRACK PN: 140U5617-21 FABRICATED PER BOEING PL 140U5617 AND DWG SHEET 1. TRACK REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02</P>)

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 100,863 hrs · 18,901 cycles

M/D- R1 ENTRY DR CTR SCUFF PLATE FOUND CRACK(<P>M/D-R1 ENTRY DR CTR SCUFF PLATE CRACKED AREA REPAIRED AS PER RI-13-10-13964 REV A</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 100,863 hrs · 18,901 cycles

EMERGENCY LIGHT BATTERY PACK (M7924) CAPACITY TEST FAILED.(<P>EMERGENCY LIGHT BATTERY PACK (M7924) REPLACED. INSTALLATION TEST NORMAL AMM 33-51-00.</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 100,863 hrs · 18,901 cycles

EMERGENCY LIGHT BATTERY PACK (M5056) CAPACITY TEST FAILED.(<P>EMERGENCY LIGHT BATTERY PACK (M5056) REPLACED. OPERATIONAL CHECK NORMAL AMM 33-51-00.</P>)

Part: SKIN SPLICE — CORRODED (LT WING) · airframe 100,863 hrs · 18,901 cycles

LHW-L/E UPPER SKIN SPLICE SURFACE AT ILES 345-348 FOUND CORROSION(<P>LHW-ILES 345-348, L/E UPPER SKIN SPLICE AREA CORROSION REMOVED AND REPAIRED IAW SRM 57-20-01-1A-1 ALLOWABLE DAMAGE 1 FIG 101 DETAIL XI</P>)

Part: OXYGEN BOTTLE — EMPTY (PORTABLE) · airframe 100,598 hrs · 18,846 cycles

PORTABLE O2 BOTTLE READS ZERO BESIDE F/A SEAT R2 DOOR.&NBSP;(<P>REMOVED AND REPLACED O2 BOTTLE,<SPAN>&NBSP;AND REGULATOR&NBSP;</SPAN><SPAN>(OFF PART: P/N&NBSP;</SPAN><SPAN>801160-3</SPAN><SPAN>, S/N&NBSP;</SPAN><SPAN>34579</SPAN><SPAN>),&NBSP;</SPAN><SPAN>PER B747 AMM 35-31-00-900-801 AT F/A SEAT R2 DOOR.</SPAN></P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,598 hrs · 18,846 cycles

EMERGENCY LIGHTS AT MID-CABIN GALLEY, LENS BROKEN AT FLOOR LEVEL ON BOTH R/H AND L/H SIDE.(<P>REMOVED AND REPLACED EMERGENCY PROXIMITY LIGHTS, 3 EA, AT MID CABIN GALLEY PER SWPM 20-30-12, PAGES 97-99, STEP G. OPS CHECK GOOD PER B747 AMM 33-51-12.</P>)

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 100,598 hrs · 18,846 cycles

EMERGENCY LIGHTS (CEILING) INOP AT REAR SECTION ON MAIN DECK.&NBSP;(<P>RELAMPED MAIN DECK REAR EMERGENCY CEILING LIGHTS AS NEEDED, AND OPS CHECK GOOD PER B747 AMM 33-51-07-962-001.&NBSP;</P>)

Part: LIGHT — MISSING (CABIN) · airframe 100,598 hrs · 18,846 cycles

SEAT 56C MISSING EMERGENCY TRACK LIGHT ASSY.(<P>TRANSFERRED TO MDDR 122269 IAW DDG 33-51-03-01-01, CAT 'C', DUE 28DEC19. PLACARD INSTALLED AND MCC NOTIFIED.&NBSP;</P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 100,598 hrs · 18,846 cycles

SEVERAL LAMPS BURNED OUT AT LATERAL EXIT SIGNS ON MAIN AND UPPER DECKS.&NBSP;(<P>RELAMPED&NBSP;UPPER AND MAIN DECK LATERAL EXIT SIGN LIGHTS, AND OPS CHECKED GOOD PER B747-400 AMM 33-51-02-962-001.</P>)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 100,598 hrs · 18,846 cycles

EMERGENCY TRACK LIGHTS INOP FROM ROW 1 THROUGH 6, UPPER DECK.&NBSP;(<P>REMOVED AND REPLACED M5055 EMERGENCY POWER SUPPLY FOR EMERGENCY TRACK LIGHTS, ROW 1 THROUGH 6, UPPER DECK, PER B747 AMM 33-51-04-402-012-00. OPS CHECK GOOD PER B747 AMM 33-51-04-712-015-001.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 98,768 hrs · 18,470 cycles

R3 AND R4 OVERHEAD EMERGENCY EXIT FLOOD LIGHT REQUIRES RE-LAMP.(<P>RE-LAMPED R3 AND R4 OVERHEAD FLOOD LIGHTS PER AMM TASK 33-51-07-962-001. OPS CHECK GOOD PER AMM TASK 33-51-00-715-105.</P>)

Part: LIGHT — INOPERATIVE (R4 DOOR) · airframe 98,768 hrs · 18,470 cycles

R4 DOOR SLIDE LIGHT INOP.(<P>REMOVED AND REPLACED R4 DOOR LIGHT ASSEMBLY PER AMM TASK 33-51-06-004-046. OPS CHECK GOOD PER AMM TASK 33-51-00-715-105.</P>)

Part: LIGHT — INOPERATIVE (R3 DOOR) · airframe 98,768 hrs · 18,470 cycles

R3 DOOR SLIDE LIGHT INOP.(<P>RE-LAMPED R3 DOOR SLIDE LIGHT PER AMM TASK 33-51-02-962-001. OPS CHECK GOOD PER AMM TASK 33-51-00-715-105.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 98,768 hrs · 18,470 cycles

G5 PATH LIGHT OTBD RT REQUIRES RELAMP.(<P>RE-LAMPED G5 PATH LIGHT CTR OTBD RT PER AMM TASK 33-51-12-962-002.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 98,768 hrs · 18,470 cycles

UPPER DECK SEAT ROW 10 AND 11 PATH LIGHTS REQUIRE RELAMP.&NBSP;(<P>RE-LAMPED UPPER DECK ROW 10 &AMP; 11 PATH LIGHTS PER AMM TASK 33-51-12-962-002. OPS CHECK GOOD PER AMM TASK 33-51-00-715-105.</P>)

Part: ACTUATOR — FAILED (NLG STEERING) · airframe 98,187 hrs · 18,352 cycles

LOW SPEED ABORTED TAKE OFF DUE TO "TAKE OFF CONFIG WARNING". SPEED WAS APPROXIMATELY 60 KNOTS.&NBSP;(<P>REMOVED AND REPLACED LEFT BODY GEAR OUTBOARD STEERING ACTUATOR. OPS CHECK GOOD AND NO MESSAGES PRESENT I.A.W. B747 AMM 32-53-11-404-010.&NBSP;</P><P><BR /></P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 98,000 hrs · 18,319 cycles

SEVERAL EMERGENCY LIGHTS INOPERATIVE(<P>RELAMPED R1, R5, L2, L4 DOOR SILL LIGHTS. REMOVED AND REPLACED M9058 BATTERY PACK FOR RT / LT CEILING EXIT SIGNS ROW 19. CORRECTED ROUTING OF SEATS 31, 32, 21 RT POWER CABLES.</P>)

Part: BATTERY — DISCHARGED (EVAC SLIDE) · airframe 97,281 hrs · 18,186 cycles

UPPER DECK RT BAT WING DOOR EMERG DOOR BATT LITE DOES NOT TEST. REPLACED BATTERY PACK NO HELP RETURNED ORIGINAL BATT PACK. UPPER DECK ESCAPE SLIDE BATTERY ASSY POWER SUPPLY REF AMM 52-23-14. OPS CHECK GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 97,259 hrs · 18,181 cycles

CABIN G8 GALLEY LT PARTITION FWD EMERGENCY LIGHT FOUND MISSING WHEN AIRCRAFT INPUT. G8 GALLEY LT PARTITION FWD EMERGENCY LIGHT INSTALLED AS PER AMM 33-51-12.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 97,259 hrs · 18,181 cycles

NLG WW RT AFT CORNER SKIN PANEL CRACKED AT STA 400. STA 400 NLG WW RT AFT CORNER SKIN PANEL CRACKED AREA REPAIRED IAW EO 4453A516 PART 4 AND RI-53-41-13071 REV A.

Part: LIGHT — MISSING (CABIN) · airframe 97,259 hrs · 18,181 cycles

CABIN SEAT 17ABC SEAT EMERGENCY LIGHT FOUND MISSING WHEN AIRCRAFT INPUT. CABIN SEAT 17ABC EMERGENCY LIGHT INSTALLED AS PER AMM 33-51-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 97,259 hrs · 18,181 cycles

CABIN C17 LT AFT EMERGENCY LIGHT FOUND DAMAGED. CABIN CC17 LT AFT EMERGENCY LIGHT REPLACED AS PER AMM 33-51-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 97,259 hrs · 18,181 cycles

CABIN CC12 RT FWD EMERGENCY LIGHT FOUND DAMAGED. CC12 RT FWD EMERGENCY LIGHT REPLACED AS PER AMM 33-51-12.

Part: FRAME — CRACKED (FUSELAGE) · airframe 97,259 hrs · 18,181 cycles

CABIN STA 2231 STR 25L 1EA FASTENER FOUND CRACKED AT FRAME STRAP LAYER. CABIN STA 2231 STR 25L, FRAME STRAP 1 EA FASTENER HOLE CRACK AREA REPAIRED IAW SRM 53-60-15-2R-2 REPAIR 2 THIS REPAIR IS A CATEGORY B REPAIR.

Part: LIGHT — DAMAGED (CABIN) · airframe 97,259 hrs · 18,181 cycles

M/D L2 DOOR PARTITION EMERGENCY LIGHT FOUND DAMAGED. M/D L2 DOOR PARTITION EMERGENCY LIGHT REPLACED AS PER AMM 33-51-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 97,259 hrs · 18,181 cycles

CABIN G8 GALLERY LT PARTITION AFT EMERGENCY LIGHT FOUND DAMAGED. G8 GALLEY LT PARTITION AFT EMERGENCY LIGHT REPLACED AS PER AMM 33-51-12.

Part: FRAME — CRACKED (FUSELAGE) · airframe 97,259 hrs · 18,181 cycles

CABIN STA 2231 STR 16R 1 EA FASTENER HOLE FOUND CRACK ON FRAME LAYER. CABIN STA 2231 STR 16R 1 EA FASTENER HOLE CRACK AREA OVERSIZE REPAIRED IAW EO 4453A569 PART 2 FIG 5.

Part: SUPPORT — DEFORMED (NR 4 PYLON) · airframe 97,259 hrs · 18,181 cycles

NR 4 PYLON FAIRING 482IL LOWER FRAME DEFORMED. NR 4 PYLON IB 284IL FAIRING LOWER SUPPORT DEFORMED AREAS REFORMED IAW RI-54-50-13072 REV A.

Part: SKIN — CRACKED (NR 4 PYLON) · airframe 97,259 hrs · 18,181 cycles

NR 4 PYLON I/B AFT STRUT SKIRT FAIRING L/E FOUND CRACKED. NR 4 PYLON I/B STRUT SKIRT BEAM SKIN CRACKED AREAS REPAIRED IAW RI-54-50-13075 REV A.

Part: LIGHT — DIM (EXIT SIGN) · airframe 97,259 hrs · 18,181 cycles

U/D LT EMERGENCY DR EXIT INDICATOR SIGN FOUND DIM. U/D LT EMERGENCY DR EXIT INDICATOR SIGN LAMP REPLACED AS PER AMM 33-51-12.

Part: EPSU — INOPERATIVE (CABIN) · airframe 97,259 hrs · 18,181 cycles

U/D AFT EMERGENCY LIGHT BATTERY OPERATION TEST FOUND INOP. U/D AFT EMER LIGHT EPSU REPLACED AND OPERATION TEST CARRIED OUT RESULT NORMAL IAW AMM 33-51-04.

Part: LIGHT — DIM (EXIT SIGN) · airframe 97,259 hrs · 18,181 cycles

M/D L4 DOOR EXIT INDICATOR SIGN FOUND DIM. M/D L4 DOOR EXIT INDICATOR SIGN LAMP REPLACED AS PER AMM 33-51-12.

Part: EPSU — INOPERATIVE (CABIN) · airframe 97,259 hrs · 18,181 cycles

L2 DOOR EMERGENCY LIGHT OPERATION TEST FAILED. L2 DOOR EMERGENCY LIGHT EPSU REPLACED IAW AMM 33-51-04 AND OPERATION TEST CARRIED OUT RESULT NORMAL IAW AMM 33-51-04.

Part: EPSU — INOPERATIVE (CABIN) · airframe 97,259 hrs · 18,181 cycles

L2 DOOR EMERGENCY LIGHT OPERATION TEST FAILED. L2 DOOR EMERGENCY LIGHT EPSU REPLACED IAW AMM 33-51-04 AND OPERATION TEST CARRY OUT RESULT NORMAL IAW AMM 33-51-04.

Part: LIGHT — MISSING (CABIN) · airframe 97,259 hrs · 18,181 cycles

G8 GALLEY LT PARTITION FWD EMER LT FOUND MISSING WHEN AIRCRAFT INPUT. G8 GALLEY LT PARTITION FWD EMER LT INSTALLED AS PER AMM 33-51-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 97,259 hrs · 18,181 cycles

M/D LT NR 2 DOOR PARTITION EMER LT FOUND DAMAGED. M/D LT NR 2 DOOR PARTITION EMER LT REPLACED AS PER AMM 33-51-12.

Part: LIGHT — DIM (EXIT SIGN) · airframe 97,259 hrs · 18,181 cycles

M/D LT D4 EXIT INDICATOR SIGN FOUND DIM. M/D L4 DOOR EXIT INDICATOR SIGN LAMP REPLACED AS PER AMM 33-51-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 97,259 hrs · 18,181 cycles

CABIN CC12 RT FWD EMER LT FOUND DAMAGED. CC12 RT FWD EMER LT REPLACED AS PER AMM 33-51-12.

Part: LIGHT — DIM (EXIT SIGN) · airframe 97,259 hrs · 18,181 cycles

U/D LT EMER DOOR EXIT INDICATOR SIGN FOUND DIM. U/D LT EMER DOOR EXIT INDICATOR SIGN LAMP REPLACED AS PER AMM 33-51-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 97,259 hrs · 18,181 cycles

CABIN G8 GALLEY LT PARTITION AFT EMERGENCY LIGHT FOUND DAMAGED. G8 GALLEY LT PARTITION AFT EMERGENCY LIGHT REPLACED AS PER AMM 33-51-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 97,259 hrs · 18,181 cycles

CABIN CC17 LT AFT EMER LT FOUND DAMAGED. CABIN CC17 LT AFT EMER LT REPLACED AS PER AMM 33-51-12.

Part: LIGHT — MISSING (CABIN) · airframe 97,259 hrs · 18,181 cycles

CABIN SEAT 17ABC SEAT EMERGENCY LIGHT FOUND MISSING WHEN AIRCRAFT INPUT. CABIN SEAT 17ABC EMERGENCY LIGHT INSTALLED AS PER AMM 33-51-12.

Part: FLAP — DAMAGED (LT WING) · airframe 97,114 hrs · 18,150 cycles

LT O/B MID FLAP O/B LE DAMAGED. REPAIRED DAMAGE OF LT O/B MID FLAP O/B LE PER SRM 51-53-01-2R-1 DETAIL IV AND SRM 51-70-07-05-0 PAR 5C.

Part: WIRE — DAMAGED (CABIN) · airframe 97,114 hrs · 18,155 cycles

SEAT 24ABC EMERG LIGHT INOP. REPAIRED WIRING OF 24ABC EMER LIGHT PER SWPM 20-30-12 PG'S 79-82. OP'S CHECK PASSED PER AMM 33-51-12-962-159.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 96,253 hrs · 17,969 cycles

EMERGENCY LIGHT TRACK COVER MISSING BETWEEN RT 5 TO LT 5. THE LIGHT TRACK COVER WAS REPLACED IAW AMM 25-27-08-008.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 96,253 hrs · 17,969 cycles

EMERGENCY LIGHT TRACK COVER MISSING BETWEEN RT 5 TO LT 5. THE LIGHT TRACK COVER WAS REPLACED IAW AMM 25-27-08-008.

Part: LIGHT — MISSING (SEAT 34C) · airframe 95,468 hrs · 17,800 cycles

SEAT 34C EMERGENCY LIGHT MISSING.

Part: PANEL — OUT OF ADJUST (LT WING) · airframe 95,444 hrs · 17,793 cycles

FIXED CLOSE OUT PANEL ON UPPER TRAILING EDGE OF THE LEFT WING OUTBOARD OF THE NR 5 SPOILER, BECAME SEPERATED DURING FLIGHT. NO DAMAGE TO PANEL NOTED. FOUND TO BE OUT OF ADJUSTMENT. ADJUSTED THE PANEL.

Part: LIGHT — LOOSE (UPPER CABIN) · airframe 95,362 hrs · 17,774 cycles

U/D FLOOR MOUNT EMERGENCY LIGHT AT L &AMP; R DOOR PADS LOOSE(<P>LOCATED AND RE SECURED LOOSE PADS AT U/D FLOOR MOUNTED EMERGENCY LIGHT AT EMERGENCY DOOR. PER AMM 20-30-01-802-001</P>)

Part: PAD — LOOSE (EMERGENCY LIGHT) · airframe 95,362 hrs · 17,774 cycles

U/D FLOOR MOUNT EMERGENCY LIGHT AT L &AMP; R DOOR PADS LOOSE.(<P>LOCATED AND RE SECURED LOOSE PADS AT U/D FLOOR MOUNTED EMERGENCY LIGHT AT EMERGENCY DOOR. PER AMM 20-30-01-802-001.</P>)

Part: VENT — CRACKED (BS 2090) · airframe 94,749 hrs · 17,650 cycles

DURING POST FLIGHT INSPECTION , FOUND A .750 INCH CRACK AT THE RT BS 2090 WASTE SYSTEM OVERBOARD VENT. REPAIRED IAW EO 4453B398.

Part: LIGHT — MISSING (CABIN) · airframe 94,449 hrs · 17,588 cycles

FLOOR EMERGENCY LIGHT MISSING ON UPPER DECK. REMOVED AND REPLACED THE LIGHT ASSY IAW 33-51-12, OPS CHECKED GOOD.

Part: SENSOR — OUT OF ADJUST (THRUST REVERSER) · airframe 94,405 hrs · 17,581 cycles

REJECTED TAKE OFF AT LOW SPEED DUE TO NO N1 ADVANCE ON NR 3 ENGINE. ADJUSTED THE FEEDBACK SENSOR FOR THE NR 3 ENGINE THRUST REVERSER, OPS CHECKED NORMAL IAW AMM 78-34-10-404.

Part: WARNING MESSAGE — ILLUMINATED (UPPER DECK DOOR) · airframe 93,631 hrs · 17,428 cycles

UPPER DECK DOOR LEAKK MESSAGE AFTER DEPARTURE. RETURNED TO DEPARTURE. VERIFIED LEFT DOOR WAS THE ISSUE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 93,524 hrs · 17,407 cycles

R1 DOOR EMERGENCY LIGHT FAILED A 15 MINUTE TEST. REPLACED THE BATTERY PACK AND PERFORMED A POWER SUPPLY TEST IAW AMM 33-51-04, NO DEFECT NOTED.

Part: STRUCTURE — CRACKED (LT WING) · airframe 93,524 hrs · 17,407 cycles

J8 JUNCTION BOX ON LT WING LANDING GEAR CRACKED. CLEANED, PREPPED, REPAIRED, & REFINISHED J8 JUNCTION BOX IAW SRM 51-20-06, 51-70-06, AND AMM 51-24-22.

Part: BRACKET — CRACKED (RT WING) · airframe 93,524 hrs · 17,407 cycles

RIGHT WING OTBD SIDE OF THE NR 7 FLAP TRACK REAR SPAR AREA BRACKET IS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-02.

Part: SPLICE — CRACKED (BS 2598 BULKHEAD) · airframe 93,524 hrs · 17,407 cycles

WHILE PERFORMING NDT OPEN HOLE INSPECTION ON THE BS 2598 BULKHEAD, RIGHT FWD INNER CHORD AND SPLICE FITTING, FOUND UPPER HOLE CRACKED IN SPLICE FITTING ONLY.

Part: ACTUATOR — CORRODED (MLG) · corrosion level 2 · airframe 93,524 hrs · 17,407 cycles

LEFT BODY GEAR ACTUATOR HAS CORROSION. REMOVED & REPLACED THE ACTUATOR IAW AMM TASK 32-33-01-004-001, & TASK 32-33-01-404-009. LEAK CHECKED, EXTENSION & RETRACTION TEST ACCOMPLISHED.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 93,524 hrs · 17,407 cycles

L3 DOOR EMERGENCY LIGHT FAILED A 15 MINUTE TEST. REPLACED THE BATTERY PACK AND PERFORMED A POWER SUPPLY TEST IAW AMM 33-51-04, NO DEFECTS NOTED.

Part: ANGLE — CORRODED (RT MLG WW) · corrosion level 2 · airframe 93,524 hrs · 17,407 cycles

ON REMOVAL OF APU FIRE CONTROL MODULE IN RT BODY GEAR WHEEL WELL FOR ROUTINE TASK CARD REPLACEMENT, LOWER AFT MOUNT FOUND TO HAVE EXFOLIATED CORROSION. REMOVED CORRODED ZEE ANGLE IAW SRM 51-40-02, FABRICATED A NEW ZEE ANGLE, FABRICATED A FILLER IAW SRM 53-40-12 FIG.1. INSTALLED THE FILLER & ANGLE IAW DRAWING 65B15069.

Part: STRUCTURE — DELAMINATED (THRUST REVERSER) · airframe 93,524 hrs · 17,407 cycles

NR 3 ENGINE OUTBD THRUST REVERSER HAS POSSIBLE DELAMINATED ON INNER UPPER AREA NRI 3162. REPAIRED THE THRUST REVERSER IAW EO 1978A138-CS.

Part: SPAR CAP — DAMAGED (LT WING) · airframe 93,524 hrs · 17,407 cycles

NR 2 PYLON UPPER WING AT & AROUND FRONT SPAR CAP UNDER PANEL 65B14963. OVERSIZED THE FASTENER HOLES IAW SRM 51-40-05, FIG 2, DETAIL 1, FIG 4, SHEET 1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 93,524 hrs · 17,407 cycles

L1 DOOR AREA EMERGENCY LIGHTS INOPERATIVE. REPLACED THE POWER SUPPLY BATTERY AND PERFORMED POWER SUPPLY TEST IAW AMM 33-51-04 ITEM E AND NO DEFECT NOTED.

Part: SKIN — DELAMINATED (LT WING) · airframe 93,524 hrs · 17,407 cycles

LEFT WING LE UPPER SKIN ILES 630-662 HAS EDGE DELAMINATION AND CORNER CRACKED. AREA PREPPED AND CLEANED FOR REPAIR IAW SRM 51-70-06-OG-0. CLEANED THE SURFACE IAW AMM 51-21-02. APPLIED TOP COAT IAW AMM 51-24-11.

Part: PANEL — CRACKED (LT WING) · airframe 93,524 hrs · 17,407 cycles

LEFT WING UPPER SURFACE WS 863, FIXED LEADING EDGE PANEL HAS CRACK GOING FWD TO AFT OF PANEL. REPAIRED THE L/E PANEL IAW SRM 51-70-17-0G-0.

Part: KEELBEAM — CORRODED (BS 1460) · corrosion level 3 · airframe 93,524 hrs · 17,407 cycles

FOUND CORROSION BETWEEN FASTENERS ON KEEL BEAM LOWER FLANGE. BS 1460, RBL 9. REMOVED FASTENERS AT LWR KEEL BEAM CHORD TO REMOVE CORROSION BETWEEN FASTENERS HOLES IAW SRM 53-40-12-1A-1, PARA 3, STEP B. FOUND WITHIN LIMITS IAW 53-40-12, AND SRM 51-40-02.

Part: STRUCTURE — DAMAGED (APU DOOR) · airframe 93,524 hrs · 17,407 cycles

MULTIPLE DENTS IN APU DOORS AND EDGES AROUND DOORS ARE DAMAGED, FOUND OUT OF LIMITS IAW SRM 52-40-01-1A-5. DETAIL 111 FIG 101. FABRICATED A REPAIR IAW SRM 52-00-01-2R7. INSTALLED THE REPAIR IAW SRM 51-40-02.

Part: SKIN — DELAMINATED (RT WING) · airframe 93,524 hrs · 17,407 cycles

RIGHT WING FIXED LE UPPER SKIN HAS EDGE DELAMINATION AND DAMAGED FASTENER HOLES. AREA PREPPED AND CLEANED FOR REPAIR IAW SRM 51-70-06. CLEANED THE SURFACE IAW AMM 51-21-02. APPLIED TOP COAT IAW AMM 51-24-11.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 93,524 hrs · 17,407 cycles

EMERGENCY EXIT SIGN AFT OF R3 DOOR FAILED A 15 MINUTE TEST. REPLACED THE BATTERY PACK AND PERFORMED A POWER SUPPLY TEST IAW AMM 31-51-04. NO DEFECTS NOTED.

Part: SKIN — DELAMINATED (RT WING) · airframe 93,524 hrs · 17,407 cycles

RIGHT WING LE UPPER SKIN ILES 630-662 HAS EDGE DELAMINATION AND RIGHT CORNER CRACK. PREPPED AND CLEANED THE AREA AND APPLIED A REPAIR IAW SRM 51-70-06 AND APPLIED TOPCOAT IAW AMM 51-24-22-370-80L.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 93,524 hrs · 17,407 cycles

LEFT WING, INBOARD, TRAILING EDGE FLAP, AFT FLAP, OUTBOARD, NEAR TIP, HAS NICK AT FASTENER HOLD ON LEADING EDGE. APPLIED REPAIR TO LEFT WING, INBOARD TRAILING EDGE FLAP AFT FLAP OUTBOARD NEAR TIP IAW SRM 51-70-06 PARA 5.L. INSTALLED FASTENER IAW SRM 51-40-02 PARA 4B. RESTORED FINSIH IAW AMM 51-24-22-370-801 PARA 1A.

Part: ACTUATOR — CORRODED (MLG) · corrosion level 2 · airframe 93,524 hrs · 17,407 cycles

RIGHT BODY GEAR ACTUATOR HAS CORROSION. REMOVED & REPLACED THE R/H BODY GEAR ACTUATOR IAW AMM 32-33-01-00-001/ 32-33-01-404-009. CHECK OF THE EXTENSION & RETRACTION OF THE ACTUATOR AND LEAK CHECK ACCOMPLISHED.

Part: SKIN — DELAMINATED (LT WING) · airframe 93,524 hrs · 17,407 cycles

LEFT WING LE UPPER SKIN ILES 693-704 HAS EDGE DELAMINATION AND DAMAGED FASTENER HOLE. AREA PREPPED AND CLEANED FOR REPAIR IAW SRM 51-70-06-0G-0. CLEANED THE SURFACE IAW AMM 51-21-02. APPLIED TOP COAT IAW AMM 51-24-11.

Part: FITTING — CORRODED (WING) · corrosion level 2 · airframe 9,352,419 hrs · 17,407 cycles

ON ACCESSING FOR FRONT SPAR CORROSION, FOUND FITTING ON L/E RIB ATTACHMENT AT WS 1462 CORRODED AT BUSHING HOLE. FITTING REPLACED.

Part: SPAR — CORRODED (LT WING) · airframe 93,524 hrs · 17,407 cycles

CORROSION ON LT WING FRONT SPAR ON FSS 1440. REMOVED CORROSION.

Part: SPLICE — CRACKED (BS 2598 BULKHEAD) · airframe 93,524 hrs · 17,407 cycles

WHILE PERFORMING NDT OPEN HOLE INSPECTION ON THE BS 2598 BULKHEAD, RIGHT SPLICE FITTING AND FRAME SUPPORT FOUND UPPER HOLE CRACKED IN SPLICE FITTING ONLY . REMOVED AND REPLACED THE RT SPLICE FITTING IAW SRM 51-40-02.

Part: BEARING — CORRODED (TRUNNION) · corrosion level 2 · airframe 93,524 hrs · 17,407 cycles

RIGHT MLG TRUNNION AFT BEARING SLEEVE CORRODED. REMOVED & REPLACED THE BEARING SLEEVE IAW AMM 32-11-01, & AMM 32-11-01-404-205.

Part: FRAME SPLICE — CRACKED (BS 2598 BULKHEAD) · airframe 93,524 hrs · 17,407 cycles

WHILE PERFORMING NDT OPEN HOLE INSPECTION ON BS 2598 BULKHEAD, LEFT FWD INNER FRAME AND SPLICE FITTING, FOUND LOWER HOLE CRACKED IN SPLICE FITTING ONLY. REAMED TO .3235 IAW MESSAGE PMO-TLS-17-0015-51B.

Part: LIGHT — MALFUNCTIONED · airframe 93,406 hrs · 17,383 cycles

EMERGENCY LIGHTS AT L4 DOOR INTERMITTENTLY ILLUMINATING. CYCLED EMERGENCY LIGHTS, OPS CHECKED NORMAL IAW AMM 33-51-01.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 92,597 hrs · 17,219 cycles

UPPER DECK AFT LEFT EMERGENCY AISLE LIGHT INOPERATIVE. FOUND CABLE DISCONNECTED. RECONNECTED CABLE TO UPPER DECK AFT EMERGENCY LIGHT IAW AMM TASK 33-51-00-432-006 OPS CHECKED GOOD IAW TASK 33-57-00-715-105.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,597 hrs · 17,219 cycles

L1 AND R3 OVER DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMP IAW AMM TASK 33-51-07-962-028. OPS CHECKED GOOD IAW AMM TASK 33-51-00-715-105.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,597 hrs · 17,219 cycles

L5 DOOR SLIDE LIGHT AND UPPER DECK LT WING DOOR SLIDE LIGHT EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACKS AT L5 DOOR SLIDE LIGHT IAW AMM TASK 33-57-06-400-701, REPLACED THE LAMPS UPPER DECK GULL WING DOOR LT IAW AMM TASK 330-51-07-962-028, OPS CHECKS GOOD IAW AMM TASK 33-51-06-800-001 AND 33-51-00-215-105.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,597 hrs · 17,219 cycles

RIGHT OVERWING EMERGENCY LIGHTS AFT 2 AND 1ST FWD INOPERATIVE. REMOVED AND REPLACED THE BULBS IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,597 hrs · 17,219 cycles

L2, R2, L3, R3, R4, L5, R5 DOOR SILL EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMPS IAW AMM TASK 33-51-05-962-031, OPS CHECKED GOOD IAW AMM TASK 33-51-00-715-105.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,597 hrs · 17,219 cycles

EMERGENCY IGHTS INOPERATIVE. REPLACED THE LAMPS IAW AMM TASK 35-51-07-962-028. OPS CHECKED GOOD IAW AMM TASK 33-51-90-215-105.

Part: OVEN — SMOKE (GALLEY) · airframe 91,783 hrs · 17,061 cycles

OVEN 60-3 BEGAN SMOKING AND HAD STRONG ELECTRICAL BURNING ODOR. ITEM TRANSFERRED TO MDDR 67915 IAW DDG 25-20-01, GALLEY ITEM 6.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,816 hrs · 16,869 cycles

EMERGENCY EXIT LIGHTS L1, R2, L3, L4, R4 & INOPERATIVE DOOR SLIDE LIGHTS. R & R EMER DOOR SLIDE LIGHTS IAW TC 1336R AMM TASK 33-51-06-004-046 & TASK 33-51-06-404-049.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 90,816 hrs · 16,869 cycles

RIGHT INBD AFT FLAP MID FLAP AREA, HAS PUNCTURES IN LOWER SURFACE, STONE DAMAGE. PERMANENT COMPOSITE REPAIR IAW SRM 57-53-01-2-R1.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 90,733 hrs · 16,853 cycles

DURING POST FLIGHT INSPECTION, O2 MASKS DEPLOYED & STATUS MSG, OXYGEN ON DISPLAYED. STOWED & SECURED O2 MASKS IAW AMM 35-21-00.

Part: STARTER — FAILED (APU) · airframe 90,252 hrs · 16,757 cycles

APU FIRE DURING GND TIME. EMER PROCEDURE CARRIED OUT BY FLIGHT CREW, FIRE EXTINGUISHING BY APU BOTTLES. INSPECTION CARRIED OUT IAW AMM 49-11-00-206. RAM FORM COMPLETED & SENT TO MCC, FOUND STARTER MOTOR FAILURE. EO 4449A027 & 4453B170 REFERS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,844 hrs · 16,667 cycles

EMERGENCY LIGHTS THROUGHOUT CABIN REQUIRE REPLACEMENT. REPLACED EMER LIGHT BULBS THROUGHOUT CABIN IAW AMM 33-51-07. OPERATIONS CHECKED GOOD OF ALL EMER LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,844 hrs · 16,667 cycles

UPPER DECK FLOOR EMER LIGHTS AT STAIRCASE INOPERATIVE. RELAMPED AISLE LOCATOR EMER LIGHTS AT STAIRCASE IAW AMM 33-51-12. OPERATIONS CHECKED GOOD.

Part: LENS — OUT OF POSITION (CABIN) · airframe 89,092 hrs · 16,582 cycles

ALL OTBD SEATS IN A ZONE HAVE EPL LENSES POINTED IN WRONG DIRECTION. INSTALLED EPL LENS COVER FROM ZONE A IAW CMM 29-90-63.

Part: LEAD — BROKEN (EMERGENCY EXIT) · airframe 89,092 hrs · 16,582 cycles

UPPER DECK EMER EXIT DOORS BLUE INDICATING LIGHTS OUT. RE -SOLDERED BROKEN LEAD ON UPPER DECK EMER EXIT DOOR BLUE LIGHT IAW PM 20-84-19.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,092 hrs · 16,582 cycles

UPPER EMER LIGHT BETWEEN EMER DOORS INOPERATIVE. RE-ARMED EMER LIGHTS IAW AMM 33-51-00.

Part: THRESHOLD — CRACKED (FUSELAGE) · airframe 89,092 hrs · 16,582 cycles

GALLEY 7 FLOOR LIGHT THRESHOLD CRACKED AT AFT FASTENER. INSTALLED GALLEY 7 FLOOR LIGHT THRESHOLD AFTER WELD REPAIR IAW SRM 51-40-02.

Part: BRACKET — DEBONDED (EMERGENCY EXIT) · airframe 89,092 hrs · 16,582 cycles

UPPER DECK, LT EMER EXIT RESERVOIR ACCESS DOOR HAS A DIS-BONDED BRACKET THAT TRIPS ACCESS DOOR HARDWARE. RE-BONDED BRACKET AT UPPER DECK, LT EMER EXIT RESERVOIR ACCESS DOOR IAW PM 20-50-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,092 hrs · 16,582 cycles

EMERGENCY LIGHT AT SEAT 10 ABC INOPERATIVE. CHANGED EMER LIGHT SYS ON ACFT IAW AMM 33-51-00-865-066 STEP 6. CHECK EMER LIGHT AT 10 ABC GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,092 hrs · 16,582 cycles

R1, L1, L3 DOORS AFT EMER LIGHT IN EACH DOORWAY INOPERATIVE. CHANGED EMER LIGHT SYS ON AIRCRAFT IAW AMM 33-51-00-865-066 STEP 6. OPERATIONS CHECK OF EMER LIGHTS AT DOORWAY R2, L1, L3 DOORS GOOD.

Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 89,092 hrs · 16,582 cycles

GOUGE NEXT TO TAIL JACK PAD POINT. REPAIRED IAW SRM 53-80-01.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 89,092 hrs · 16,582 cycles

AFT CARGO DOOR INTERIOR SKIN BELOW AFT DEPRESSURIZATION DOOR, CORROSION AROUND 2 PANEL ATTACH HOLES. REPAIRED IAW SR 4-2982477340 MSG PMO-TLS-15-0016-3B. FORM 8100-9 RECEIVED FOR APPROVAL.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 89,092 hrs · 16,582 cycles

DENT AT FUSELAGE STATION 2040, RT SIDE AFT OF BULK CARGO DOOR. REPAIRED IAW SRM 53-00-01-2R-14.

Part: LENS — MISSING (CABIN) · airframe 89,092 hrs · 16,582 cycles

UPPER DECK STAIRWELL PATH LIGHTING IS MISSING LENS. INSTALLED NEW LENS PN 81000-22701 IAW AMM 33-51-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,092 hrs · 16,582 cycles

UPPER DECK EMER FLOOR LIGHT OF SEAT 7 ABC INOPERATIVE. REPLACED UPPER DECK EMER FLOOR LIGHT FWD OF SEAT 7 ABC IAW AMM 33-51-12. OPERATIONS CHECKED GOOD.

Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 89,092 hrs · 16,582 cycles

GOUGE JUST AFT OF L4 CUT OUT. REWORKED IAW SRM 53-00-01 DETAIL II. REPAIR & APPROVAL WITH FLASH RESTORED PROVIDED IN SR 3-3301200735 MSGS. FORM 8100-9 RECEIVED FOR CATEGORY A REPAIR WITH R1 INSPECTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,092 hrs · 16,582 cycles

EMERGENCY LIGHTS AT SEATS 19 ABC & 20 ABC INOPERATIVE. CHANGED EMER LIGHT SYS ON ACFT AMM 33-51-00-865-066 STEP 6. OPERATIONS CHECK OF EMER LIGHTS AT SEAT 19 ABC & 20 ABC GOOD.

Part: CONNECTOR — UNKNOWN (CABIN) · airframe 88,109 hrs · 16,391 cycles

EMERGENCY PATH LIGHT FROM SEATS 44 & 54 ON RT SIDE OF A/C ZONE E INOPERATIVE. FOUND CONNECTOR, REMOVED FROM UNDER SEAT WIRE JUNCTION. OPERATIONS CHECKED GOOD IAW AMM 33-51-00, WDM 33-51-63 & CONNECTOR D9813. OPERATIONS CHECKED IAW AMM 33-51-12. REPAIRED IAW SWPM 20-30-00.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 88,109 hrs · 16,391 cycles

EMERGENCY PATH LIGHT FROM SEATS 44 & 54 ON RT SIDE OF ACFT ZONE E INOPERATIVE. FOUND CONNECTOR REMOVED FROM UNDER SEAT WIRE JUNCTION. REPAIRED & SECURED. SYS OPERATES NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,130 hrs · 16,211 cycles

SEAT EMER LIGHTS ARE NOT WORKING AT 17H, 14C, 24C & 59C. REPLACED LAMPS & LAMP ASSEMBLIES IAW SWPM 20-30-12 & AMM 33-51-12. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (DOOR) · airframe 87,130 hrs · 16,211 cycles

DOOR MOUNTED EMER EXIT LIGHTS ARE OUT L1, L2 & L5. REPAIRED DOOR MOUNTED EMER EXIT LIGHTS IAW AMM 33-51-06.

Part: SCREW — LOOSE (WINDOW SENSOR) · airframe 86,590 hrs · 16,151 cycles

R2 WINDOW SENSOR ARCING ACROSS LEADS. TIGHTENED BOTH SCREWS ON SENSOR & APPLIED HEAT SINK COMPOUND & OK PER MM 30-41-06.

Part: SUPPORT — CRACKED (TE FLAP) · airframe 86,370 hrs · 16,127 cycles

NUMBER 1 TE FLAP CARRIAGE ASSEMBLY GENEVA TRACK IND SUPPORT ASSEMBLY IS CRACKED. REPLACED IAW AMM 20-51-01.

Part: CARRIAGE — DAMAGED (TE FLAP) · airframe 86,370 hrs · 16,127 cycles

NUMBER 5 FLAP CARRIAGE FWD BOGIE, BOTH FWD LOWER ROLLERS CRACKED, SPLIT & DAMAGED & OTBD ROLLER ARM BENT. R & R NR 5 FLAP CARRIAGE FWD BOGIE IAW AMM 27-51-43. NO DEFECTS NOTED IN FLAP TRACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,370 hrs · 16,127 cycles

EIGHT EMER CEILING LIGHTS ON MAIN DECK & UPPER DECK INOPERATIVE & FLOOR PATHWAY EMER & LIGHT A LAVATORY UPPER DECK ARE INOPERATIVE. RELAMPLED EMER CEILING LIGHTS ON MAIN DECK & UPPER DECK & FLOOR PATHWAY EMER LIGHT IAW AMM 33-51-12 & 33-51-07. OPERATIONS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 86,313 hrs · 16,119 cycles

UPPER DECK LT DOOR TEST LIGHT INOPERATIVE. REMOVED AND REPLACED BATTERY POWER PACK IAW AMM 52-23-14. OPS CHECK OK. MDDR 50463 CLEARED AND MCC NOTIFIED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 85,733 hrs · 16,011 cycles

LEFT UPPER DECK EMER EXIT GREEN BATTERY CHECK LIGHT DOES NOT ILLUMINATE DURING TEST. R & R LT UPPER DECK EMER BATTERY PACK IAW AMM 33-51-04, OPERATIONS CHECKED GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 85,616 hrs · 15,989 cycles

EMERGENCY FLASHLIGHT AT L2 DOOR JUMP SEAT INOPERATIVE. DEFERRED IAW DDG 25-63-04. CONFIRMED FLIGHT CREW HAS A READILY AVAILABLE EQUIVALENT FLASHLIGHT.

Part: SKIN — CHAFED (FUSELAGE) · airframe 85,369 hrs · 15,942 cycles

CHAFING SKIN, LT FUSELAGE SKIN CHAFING STATION 2610, WL 265 & NBSP. REPAIRED THE CHAFING AREA IAW SRM 53-00-01 REPAIR 6 FIG 201 REV 89 & NBSP.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 85,369 hrs · 15,942 cycles

CORROSION DOUBLER, LT SATCOM ANTENNA EXTERNAL DOUBLER CORROSION AT STATION 1680 BETWEEN STRINGER 11L & STRINGER 12L. REPLACED WITH NEW DOUBLER IAW SRM 51-40-02 REV 89.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 85,369 hrs · 15,942 cycles

CORROSION, THE SPLICE BRACKET FOR THE WING TO BODY FAIRING SUPPORT STRUCTURE FRAME, STATION 880, BL 0. REPLACE WITH NEW PART IAW SRM 51-40-02 REV 89.

Part: LIGHT — INOPERATIVE (CREW REST) · airframe 85,369 hrs · 15,942 cycles

PERFORMED EMERGENCY LIGHT TEST FOUND ZONE E CREW REST EMERGENCY LIGHT INOPERATIVE, M3158, STATION 2316. REPLACED M3158 EMERGENCY LIGHT ASSEMBLY & FUNCTION CHECKED NORMAL.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 85,369 hrs · 15,942 cycles

FOLLOWING EMERGENCY LIGHT BATTERY PACKS CAPACITY TEST OUT OF LIMITS POSITIONS STATION 675, 770, 450L, 450R, 810L, 810R, 1268R, 1265L, 1674L, 1674R, 2277L & 2277R. REPLACED BATTERY PACKS & FUNCTION CHECKED NORMAL.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 85,369 hrs · 15,942 cycles

FUSELAGE CTR SECTION BS 1265 FRAME INSPECTION & REPAIR AD 2000-02-10. REPAIRED WITH EO 4453A767 PART 7 REV 1.

Part: STRAP — BULGED (RT WING) · airframe 85,369 hrs · 15,942 cycles

BULGE SKIN UPPER SURFACE OF RT WING LE UPPER FIXED PANEL ILES 630.72. REPLACED WITH NEW STRAP IAW SRM 51-40-02 REV 89.

Part: SKIN — CORRODED (RT WING) · airframe 85,369 hrs · 15,942 cycles

BULGE SKIN, UPPER SURFACE OF RT WING LE UPPER FIXED PANEL, ILES 822.50. REPAIRED CORROSION AREA IAW EI NO T2014A57B-1401 REV 0.

Part: BRACKET — CORRODED (FUSELAGE) · airframe 85,369 hrs · 15,942 cycles

CORROSION, THE FWD & AFT SPLICE BRACKETS FOR THE WING TO BODY FAIRING SUPPORT STRUCTURE FRAME, STATION 920, BL 0 LOWER FUSELAGE. REPLACE WITH NEW PART IAW SRM 51-40-02 REV 89.

Part: BRACKET — CORRODED (RT WING) · airframe 85,369 hrs · 15,942 cycles

CORROSION BRACKET, RT WING GEAR SHOCK STRUT INBD DOOR FAIRING. REPLACED WITH NEW CLIP IAW SRM 51-40-02 REV 89.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,827 hrs · 15,814 cycles

MAIN CABIN SEATS 24ABC & 21HJK EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED LAMP AT SEAT 21HJK & LIGHT ASSEMBLY AT SEAT 24ABC & PERFORMED SATISFACTORY OPERATIONS CHECK IAW 747-400 AMM 33-51-12.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 83,654 hrs · 15,632 cycles

EMERGENCY FLOOR PATH LIGHTS AT 11C INOPERATIVE. NOTICED WIRING AT 11C BROKEN. RECTIFIED WIRING AND OPS NORMAL IAW AMM 20-62-00.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 83,311 hrs · 15,559 cycles

EMERGENCY EXIT LIGHT COVER 11C MISSING. INSTALLED 11C EMERGENCY EXIT LIGHT COVER, REF AMM 25-27-08, OPS NORMAL.

Part: BOTTLE — LOW PRESSURE (L3 DOOR SLIDE) · airframe 83,311 hrs · 15,559 cycles

L3 DOOR SLIDE HAS LOW PRESSURE. REMOVED & REPLACED ESCAPE SLIDE ON L3 DOOR IAW AMM 25-69-01. ALL OPS NORMAL.

Part: SKIN — DAMAGED (BS 2300) · airframe 83,056 hrs · 15,495 cycles

FUSELAGE SKIN AT BS 2300 AND S-22L HAS A DENT WITH ABRASION AT DENT CENTER. REMOVED DAMAGE AS REQUIRED AND REPAIRED IAW SRM 53-00-01.

Part: DOOR FRAME — CRACKED (BS 2231) · airframe 83,056 hrs · 15,495 cycles

CRACK IN R5 DOOR FRAME REVEAL BETWEEN S-21R AND S-22R. REPAIRED DAMAGE IAW SRM 53-60-15-2R, REPAIR 3.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 83,056 hrs · 15,495 cycles

DENTED AND DEBONDED AREA ON LOWER SKIN OF LT WING INBD AFT FLAP. REPAIRED DAMAGES BY REPLACEMENT OF PART IAW SRM 51-40-02 AND 51-10-02.

Part: FRAME — CRACKED (BS 2231) · airframe 83,056 hrs · 15,495 cycles

CRACK INDICATION NOTED ON LT AFT INNER CHORD OF FRAME AT BS 2231 S19L LOWER AFT HOLE LT SIDE. REPAIRED FRAME IAW SRM 53-60-15-2R-2.

Part: STRUCTURE — DAMAGED (MLG WW) · corrosion level 2 · airframe 83,056 hrs · 15,495 cycles

CORROSION AND TEAR AT NOSE WHEEL WELL. LT SIDE STA 323 AND WL 180. REMOVED DAMAGE AND REPAIRED IAW SRM 53-10-14, REPAIR 4 AND SR 1-2439001753.

Part: LIGHT — DAMAGED (CABIN) · airframe 83,056 hrs · 15,495 cycles

FWD CORNER OF LAV FC4 EMERGENCY PATH LIGHTING MISSING CORNER. INSTALLED EMERGENCY PATH LIGHTING CORNER AT FWD OF LAV FC4.

Part: BRACKET — CRACKED (EMERGENCY LIGHT) · airframe 83,056 hrs · 15,495 cycles

R2 DOOR TOP DOOR BUSSLE EMERGENCY LIGHT HOUSING BRACKET CRACKED. R & R BRACKET ON R-2 TOP DOOR.

Part: CHANNEL — CRACKED (BS 1120) · airframe 83,056 hrs · 15,495 cycles

CRACK INDICATION AT TENSION TIRE INTERSECTION WITH SLOPING WEB AND SHEAR WEB AT STA 1120 LT SIDE. REPLACED PREVIOUSLY INSTALLED REPAIR SECTION OF AFT TENSION TIE CHANNEL WITH NEW REPAIR SECTION IAW SRM 53-40-30-2R-1.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 83,056 hrs · 15,495 cycles

FLOOR PATH LIGHT CONDUIT COVER FWD OF LAV FC4 CRACKED, WILL NOT LOCK DOWN. R & R FLOOR PATH LIGHT TRACK CONDUIT COVER FWD OF LAV FC4 IAW AMM 33-51-12. NO OPS TEST DUE.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 82,919 hrs · 15,467 cycles

EMERGENCY LIGHT ON SEAT 17-C INOPERATIVE. REPAIRED WIRING BEHIND SEAT 17-C E-PATH LIGHT OPS CHECK OK. IAW REF MM 33-51-00. WIRING REPAIR REF SWPM 20-10-13.

Part: LIGHT — INOPERATIVE (SEAT 24C) · airframe 82,920 hrs · 15,467 cycles

EMERGENCY LIGHT ON SEAT 24C INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY SEAT 24C. OPS CHECK OK AMM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,920 hrs · 15,467 cycles

UPPER DECK EMERGENCY LIGHTS NEXT TO STAIR WELL INOPERATIVE. R & R LIGHT IAW AMM 33-51-01, PERFORMED TEST IAW 33-51-00-715-105. NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 82,920 hrs · 15,467 cycles

EMERGENCY LIGHT AT LAV FC-4 INOPERATIVE. RECHARGED EMERGENCY LIGHTS BATTERY PACKS. OPS CHECKED LAVATORY FC-4 E-PATH LIGHTS, FOUND OK IAW MM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,920 hrs · 15,467 cycles

UPPER DECK EMERGENCY LIGHT AT LT EMERGENCY EXIT DOOR INOPERATIVE. R & R LIGHT ASSY IAW 33-51-01. PERFORMED TEST IAW 33-51-00-715-105.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,920 hrs · 15,467 cycles

EMERGENCY LIGHT ON SEAT 38-C INOPERATIVE. REPLACED LAMP . OPS CHECKED OK. IAW MM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,001 hrs · 15,264 cycles

OVERHEAD EMERGENCY LIGHTING AT SEAT 26-HJK INOPERATIVE. OPEN

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,102 hrs · 15,047 cycles

UPPER DECK FLOOR LEFT EXIT DOOR EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT ASSY IAW MM 33-51-12.

Part: BULB — LOOSE (EMERGENCY LIGHT) · airframe 81,102 hrs · 15,047 cycles

RT DOOR SIDE EMERGENCY LIGHT INOPERATIVE. FOUND BULB LOOSE, SECURED, OPS CHECKED NORMAL IAW MM 33-51-00-501.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 81,102 hrs · 15,047 cycles

EMERGENCY LIGHT ROW 20 RT EXIT DOOR INOPERATIVE. SECURED CONNECTOR AT EMERGENCY ROW LIGHT NR 20. OPS CHECKED NORMAL IAW MM 33-51-00-501.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 81,102 hrs · 15,047 cycles

MAIN PASSENGER CABIN EMERGENCY LIGHTS SEAT ROW 28 TO 33 ON SIDE OF SEATS INOPERATIVE. FOUND CONNECTOR FOR EMERGENCY LIGHTS TRAPPED UNDER SEAT. REMOVED SEAT, INSTALLED CONNECTOR IAW MM 33-51-00. EMERGENCY LIGHTS CHECK NORMAL. REINSTALLED SEAT IAW MM 25-26-01. OPS CHECK NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,207 hrs · 14,844 cycles

UPPER DECK EMERGENCY LIGHTS AT SEATS 1C, 8C, 11C, INOPERATIVE. RELAMPED IAW AMM 33-51-12. OPS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,207 hrs · 14,844 cycles

MAIN DECK EMERGENCY LIGHTS INOPERATIVE FWD AND AFT. R & R POWER SUPPLY M7921. OPS NORMAL IAW AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,207 hrs · 14,844 cycles

MAIN DECK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-51-00.

Part: BATTERY — WEAK (EMERGENCY LIGHTS) · airframe 80,207 hrs · 14,844 cycles

MAIN DECK EMERGENCY LIGHTS BATTERY WEAK. R &R BATTERY ASSY M7918 OPS CHECKED NORMAL IAW AMM 33-51-04.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 80,207 hrs · 14,844 cycles

MAIN DECK EMERGENCY LIGHTS INOPERATIVE AT R4 DOOR. CHARGED BATTERY. CHECKED GOOD IAW MM 33-51-00-01.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,207 hrs · 14,844 cycles

MAIN DECK EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY M7921. OPS NORMAL IAW MM 33-51-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,207 hrs · 14,844 cycles

MAIN DECK EMERGENCY LIGHTS INOPERATIVE. R & R LAMPS, OPS CHECKED NORMAL REF AMM 33-51-00.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 80,207 hrs · 14,844 cycles

MAIN DECK EMERGECNCY LIGHTS BATTERY WEAK. R & R BATTERY POWER SUPPLY M7921 OPS CHECKED NORMAL IAW AMM 33-51-04.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,207 hrs · 14,844 cycles

MAIN DECK EMERGENCY LIGHTS. SEAT 17H INOPERATIVE. RELAMPED, GROUND CHECKED GOOD IAW 33-51-00-715-001.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,207 hrs · 14,844 cycles

MAIN DECK EMERGENCY LIGHTS AT L2 DOOR SILL INOPERATIVE. R & R LAMP, OPS CHECKED NORMAL REF AMM 33-51-05.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,207 hrs · 14,844 cycles

UPPER DECK EMERGENCY LIGHTS INOPERATIVE. RELAMPED AND GROUND CHECKED GOOD IAW 33-51-00-715-001.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,207 hrs · 14,844 cycles

UPPER DECK EMERGENCY LIGHTS INOPERATIVE. R & R LAMP. OPS NORMAL IAW AMM 33-51-07.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,207 hrs · 14,844 cycles

UPPER DECK EMERGENCY LIGHTS INOPERATIVE. ROWS 2, 7, &11. R & R LAMPS. OPS CHECKED NORMAL IAW AMM 33-51-07.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,207 hrs · 14,844 cycles

MAIN DECK EMERGENCY LIGHTS INOPERATVE. RELAMPED, OPS CHECKED GOOD IAW 33-51-00-715-001.

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHTS) · airframe 80,207 hrs · 14,844 cycles

MAIN DECK EMERGENCY LIGHTS INOPERATIVE, ROW 60. RELAMPED, GROUND CHECKED GOOD IAW 33-51-00-715-001.

Part: FAIRING — DAMAGED (RT WING) · airframe 79,319 hrs · 14,652 cycles

RT WING TIP -MID FAIRING MADE CONTACT WITH A LIGHT POLE CAUSING DAMAGE/PUNCTURE, MEASURING APPROX 4.0 X 5.0 INCHES WITH A 6.0 INCH SCRAPE FWD OF HOLE (REF. FIGURE 1). PERFORMED A TIME LIMITED REPAIR.

Part: RETAINER — DAMAGED (CABIN) · airframe 79,246 hrs · 14,640 cycles

UPPER DECK CART LIFT INBD LOWER RETAINER DAMAGE AND CORROSION. RETAINER ANGLE REPAIRED IAW EO NO 4425A251.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

RIGHT EMERGENCY DOOR FLOOR PROXIMITY EXIT SIGN INOPERATIVE. RELAMP AND OPS TEST RESULT NORMAL IAW AMM 33-51-07.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

CABIN 11 ABC SEAT FLOOR PROXIMITY EMERGENCY LIGHT INOPERATIVE. RELAMPED AND TEST NORMAL, REF AMM 33-51-12.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

U/D GALLEY 6 CEILING EMERGENCY LIGHT FOUND INOPERATIVE. RELAMPED AND OPS TEST RESULT NORMAL. IAW AMM 33-51-07.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

UPPER DECK, SEAT ROW 5 CEILING EMERGENCY LIGHT FOUND INOPERATIVE. RELAMPED AND OPS TEST RESULT NORMAL IAW AMM 33-51-07.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

ZONE E53 ABC - 66 ABC CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY CHARGER (M7928) FUSE REPLACED IAW AMM 33-51-00, 33-51-04.

Part: SKIN — MISREPAIRED (BS 741) · airframe 79,246 hrs · 14,640 cycles

DURING C-CHECK, FOUND A REPAIR AT BS741, S-26L - S-27L WAS MISINSTALLED. REPAIR WAS R & R WITH A NEW REPAIR IAW SR 1-1975939450, WHICH WAS APPROVED AS A CATEGORY B REPAIR BY MFG WITH 8100-9 DATED 15-SEP-2011.

Part: MODULE — FAILED (OXYGEN SYSTEM) · airframe 79,246 hrs · 14,640 cycles

DOOR NR 5 OVERHEAD CREW REST FWD UPPER BUNK OXYGEN MODULE DROP TEST FAILED. OXYGEN MODULE REPLACED AND DROP TESTED NORMAL IAW AMM 35-21-36 AND 35-21-00.

Part: FLOOR PANEL — CORRODED · airframe 79,246 hrs · 14,640 cycles

DURING THE PRESENT C4-CHECK, CORROSION WAS REPORTED ON UPPER DECK LIFT CAR ASSY, PN 747-9202-14 LOWER FLOOR PANEL ASSY SHOWN IN FIG 1. CORROSION AFFECTED LOWER PANEL ASSY PN 747-9262-1 BOTH UPPER AND LOWER SURFACE SHEET SIDES AND AFT EDGES AS SHOWN IN FIG 2. IN ADDITION, THE ATTACHING ANGLE PN 747-9152-1 WAS FOUND CORRODED AND CRACKED AT THE AFT END. (SINCE NO SPARE PART WAS FOUND, PROPOSED THE REPAIR SHOWN IN FIG 2 & AMP; 3.NOTE: THIS REPAIR IS CONSIDERED PERMANENT AND IS APPROVED BY DER IAW 8110-3 FORM IN FIGURE 4.)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

UPPER DECK SEAT ROW 2 CELING EMERGENCY LIGHT INOPERATIVE. RELAMPED AND TEST NORMAL IAW AMM 33-51-07.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

MAIN DECK STAIR LEFT NR 2 FLOOR PROXIMITY EMERGENCY LIGHT FOUND INOPERATIVE. RELAMPED AND OPS TEST RESULT NORMAL IAW AMM 33-51-12.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

LAVATORY BS2A CEILING EMERGENCY LIGHT FOUND INOPERATIVE. RELAMP AND TEST RESULT NORMAL AS PER AMM 33-51-07.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

1L DOOR CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AND CKS NORMAL IAW AMM 33-51-07.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

ZONE E 53HJK - 66HJK CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK (M7928) REPLACED AND OPS TEST C/O RESULT NORMAL IAW AMM 33-51-04.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

STAIRWAY CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AND TESTED NORMAL IAW AMM 33-51-07.

Part: LIGHT — INOPERATIVE (LAVATORY) · airframe 79,246 hrs · 14,640 cycles

LAVATORY B51A EMERGENCY LIGHT INOP. EMERGENCY LIGHT REPLACED AND TEST NORMAL IAW AMM 33-51-07.

Part: POWERPACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

ZONE A SEAT 12 AC -16 AC EMERGENCY LIGHT INOPERATIVE. POWER PACK REPLACED AND TESTED NORMAL IAW AMM 33-51-04.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,246 hrs · 14,640 cycles

ZONE B SEAT 17 ABC EMERGENCY LIGHT INOPERATIVE. POWER PACK FUSE REPLACED AND TEST NORMAL AS PER AMM 33-51-04.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

COCKPIT EMERGENCY LIGHT INOPERATIVE. RELAMPED AND TEST NORMAL IAW AMM 33-51-07.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,246 hrs · 14,640 cycles

UPPER DECK SEAT ROW 9 CEILING EXIT SIGN INOPERATIVE. POWER PACK FUSE REPLACED AND TEST NORMAL IAW AMM 33-51-02.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,246 hrs · 14,640 cycles

U/D 1ABC-6ABC SEAT EMERGENCY LIGHT INOPERATIVE. POWER PACK (M5055) REPLACED AND TEST NORMAL IAW AMM 33-51-04. 33-51-00.)

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

1L DOOR FLOOR PROXIMITY EXIT SIGN INOPERATIVE. POWER PACK FUSE REPLACED AND TEST NORMAL IAW 33-51-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,246 hrs · 14,640 cycles

U/D EMERGENCY DOOR FLOOR PROXIMITY LIGHT FWD INOPERATIVE. FLOOR PROXIMITY LIGHT FWD REPLACED AND TEST NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

UPPER DECK LEFT EMERGENCY DOOR OVER DOOR EXIT SIGN INOPERATIVE. BATTERY PACK REPLACED AND TESTED NORMAL IAW AMM 33-51-04.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

ROW 50 ABC CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AND TEST NORMAL REF AMM 33-51-07.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,246 hrs · 14,640 cycles

U/D SEAT ROW 4 O/H CEILING LIGHT EXIT SIGN INOP. POWER PACK FUSE REPLACED AND TEST NORMAL IAW AMM 33-51-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

1L DOOR EXIT SIGN INOPERATIVE. RELAMPED AND TESTED NORMAL IAW AMM 33-51-02.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,246 hrs · 14,640 cycles

UPPER DECK EMERGENCY EXIT OVERHEAD EMERGENCY LIGHT FOUND INOPERATIVE. POWER PACK FUSE REPLACED AND TEST NORMAL IAW AMM 33-51-02.

Part: SKIN PANEL — DENTED (FUSELAGE) · airframe 79,246 hrs · 14,640 cycles

DENT WAS FOUND ON SKIN PANEL AND WAS MEASURED 0.130 INCH DEEP AND 1" X 1". THE DAMAGED SKIN IS A BONDED SKIN PANEL WITH A TOTAL THICKNESS OF 0.028 INCH. DENT REPAIRED IAW SRM 53-00-01, REPAIR 1, FIGURE 201 WITH THE EXCEPTION THAT THE MINIMUM THICKNESS OF THE REPAIRED AREA IS 0.028" THICK.

Part: SKIN — DENTED (TAILCONE) · airframe 79,246 hrs · 14,640 cycles

TAIL CONE LT UPPER HALF EXT SKIN HAS A DENT MARK AT STA 2707 APPROX BWL 359.7. SKIN PATCH REPAIRED IAW R5-53-81-37225 REV A.

Part: SKIN — DENTED (BS 730-741) · airframe 79,246 hrs · 14,640 cycles

MULTIPLE DENTS AND GOUGES AT PRODUCTION SPLICE BEFORE SECTION 43 JUST BELOW BELT. SKIN REPAIRED AT BS 730- BS 741 S-23L TO S-25L IAW RS NO R53-20-37221 REV A.