N465MC

Part: LIGHT — INOPERATIVE (CABIN) · airframe 101,718 hrs · 19,674 cycles

L2 DOOR AFT SILL EMERGENCY LIGHT NOT ILLUMINATED. REPLACED THE LIGHT AND TESTED NORMAL IAW AMM 33-51-05, REV 98.

Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

RIGHT WING INBD MID FLAP UPPER SKIN INBD SECTION CORRODED. THE FLAP UPPER SKIN CORROSION WAS REMOVED AND PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN SRM 57-53-01-1A-0 ALLOWABLE DAMAGE GENERAL LIMITS.

Part: SUPPORT — CORRODED (BS 1112) · airframe 101,718 hrs · 19,674 cycles

BODY FAIRING SUPPORT BS 1112.1, LBL 4, HAD SURFACE CORROSION. THE FAIRING SUPPORT CORROSION WAS REMOVED AND PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-71 ALLOWABLE DAMAGE 1 FIG 101, LIMITS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,718 hrs · 19,674 cycles

RIGHT OVERWING NR 1 AND 2 EMERGENCY LIGHTS FOUND NOT ILLUMINATING. THE LAMPS WERE REPLACED AND TESTED NORMAL IAW AMM 33-51-03.

Part: SKIN — DENTED (NR 2 SPOILER) · airframe 101,718 hrs · 19,674 cycles

LEFT WING NR 2 SPOILER UPPER SURFACE WAS FOUND WITH SEVERAL DENTS. THE NR 2SPOILER WAS REPLACED IAW AMM 27-61-02.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

RIGHT WING OTBD MID FLAP T/E UPPER MID AREA FOUND DELAMINATION. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: SKIN — DELAMINATED (LT WING) · airframe 101,718 hrs · 19,674 cycles

LHW I/B AFT UPPER SURFACE FIXED T/E UPPER PANEL, THE EXTERNAL SURFACE WAS FOUND DELAMINATED. PERFORMED COMPOSITE REPAIR IAW RI-57-50-14081, REV A.

Part: CHANNEL — CRACKED (BS 1200) · airframe 101,718 hrs · 19,674 cycles

BS 1200, RBL 40 - 50, RT TENSION TIE AFT CHANNEL WAS CRACKED AROUND FASTENER. THE TENSION TIE AFT CHANNEL WAS REPAIRED IAW RI-53-00-14084 REV A.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

RHW I/B FORE FLAP FOUND DELAMINATED AT THE INBD L/E SURFACE. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

RIGHT WING OTBD AFT FLAP UPPER SKIN T/E CTR SECTION FOUND DELAMINATED 84 INCHES FROM I/B EDGE. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: SUPPORT — CORRODED (BS 880) · airframe 101,718 hrs · 19,674 cycles

BODY FAIRING SUPPORT AT BS 880, LBL 60 TO RBL 55 HAD SURFACE CORROSION. THE CORROSION WAS REMOVED AND THE SUPPORT PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN LIMITS IAW SRM 53-00-71, ALLOWABLE DAMAGE 1, FIG 101.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

RIGHT WING INBD FORE FLAP UPPER SURFACE T/E FOUND DELAMINATION, 141 INCHES TO INBD. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

RIGHT WING OTBD MID FLAP L/E OTBD SECTION ONE LOCATION OF DELAMINATION, 9 INCHES FROM OTBD EDGE. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 101,718 hrs · 19,674 cycles

R2 DOOR EMERGENCY LIGHT BATTERY PACK (M7918) CAPACITY TEST FAILED. THE BATTERY PACK WAS REPLACED AND TESTED NORMAL IAW AMM 33-51-04.

Part: ATTACH FITTING — CRACKED (LT FLAP TRACK) · airframe 101,718 hrs · 19,674 cycles

ONE CRACK FOUND ON THE LEFT WING INBD FLAP TRACK NR 4 FWD ATTACH SUPPORT FITTING OTBD ANGLE. THE ATTACH FITTING WAS REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 101,718 hrs · 19,674 cycles

UPPER DECK DOOR, RT EMERGENCY SYSTEM FUNCTIONAL TEST FAILED. THE BATTERY PACK WAS REPLACED AND INSTALLATION TESTED NORMAL IAW AMM 52-23-14.

Part: ATTACH FITTING — CRACKED (RT FLAP TRACK) · airframe 101,718 hrs · 19,674 cycles

ONE CRACK FOUND ON THE RIGHT WING INBD FLAP TRACK NR 4 FWD ATTACH SUPPORT FITTING OTBD ANGLE. THE ATTACH FITTING WAS REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

RIGHT WING OTBD MID FLAP L/E INBD SECTION FOUND DELAMINATION, 112 INCHES FROM INBD EDGE. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 101,718 hrs · 19,674 cycles

RIGHT EMERGENCY LIGHT BATTERY PACK (M6378) CAPACITY TEST FAILED. THE BATTERY PACK WAS REPLACED AND TESTED NORMAL IAW AMM 33-51-04.

Part: WEB — CORRODED (BS 620-640) · airframe 101,718 hrs · 19,674 cycles

U/D STA 620-640 RT OTBD FLOOR WEB WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND THE WEB PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN LIMITS IAW SRM 53-00-51, ALLOWABLE DAMAGE, FIG 101.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 101,718 hrs · 19,674 cycles

L3 DOOR EMERGENCY LIGHT BATTERY PACK (M7919) CAPACITY TEST FAILED. THE BATTERY PACK WAS REPLACED AND TESTED NORMAL IAW AMM 33-51-04.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

RIGHT WING INBD FORE FLAP UPPER SURFACE T/E FOUND DELAMINATED 166 INCHES TO INBD. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: SKIN — CORRODED (BS 2090) · airframe 101,718 hrs · 19,674 cycles

AFT FUSELAGE RT WASTE SYSTEM OVERBOARD VENT SKIN FOUND CORRODED, BS 2090, STRINGERS 35R-36R, SURFACE CORROSION REMOVED AND PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1, FIG 101 LIMITS.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 101,718 hrs · 19,674 cycles

EMERGENCY LIGHT BATTERY PACK (M7050) CAPACITY TEST FAILED. THE BATTERY PACK WAS REPLACED AND TESTED NORMAL IAW AMM 33-51-04.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 101,718 hrs · 19,674 cycles

LEFT OVERWING NR 3 & 4 EMERGENCY LIGHTS FOUND NOT ILLUMINATED. LAMPS REPLACED AND LAMPS TESTED NORMAL IAW AMM 33-51-03.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

LEFT WING OTBD MID FLAP T/E UPPER SKIN FOUND DELAMINATED 112 INCHES TO INBD. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 101,718 hrs · 19,674 cycles

L5 DOOR EMERGENCY LIGHT BATTERY PACK (M7923) CAPACITY TEST FAILED. THE BATTERY PACK WAS REPLACED AND TESTED NORMAL IAW AMM 33-51-04.

Part: SUPPORT — CORRODED (BS 987) · airframe 101,718 hrs · 19,674 cycles

BODY FAIRING SUPPORT BS 987.35, BL 0 TO LBL 65 HAD SURFACE CORROSION. THE CORROSION WAS REMOVED AND THE SUPPORT PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN LIMITS IAW SRM 53-00-71, ALLOWABLE DAMAGE 1, FIG 101.

Part: SUPPORT — CORRODED (BS 1480) · corrosion level 2 · airframe 101,718 hrs · 19,674 cycles

LT BS 1480 BODY FAIRING SUPPORT FOUND CORRODED. THE FAIRING SUPPORT WAS REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: SUPPORT — CORRODED (BS 920) · airframe 101,718 hrs · 19,674 cycles

BODY FAIRING SUPPORT BS 920, LBL 1, HAD SURFACE CORROSION. THE BODY FAIRING SUPPORT SURFACE CORROSION WAS REMOVED AND PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN LIMITS IAW SRM 53-00-71 ALLOWABLE DAMAGE 1 FIG 101.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

LEFT WING OTBD FORE FLAP L/E INBD SURFACE FOUND DELAMINATED, 43" TO INBD. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: SUPPORT — CORRODED (BS 840) · airframe 101,718 hrs · 19,674 cycles

BODY FAIRING SUPPORT BS 840, LBL 14 HAD SURFACE CORROSION. THE BODY FAIRING SUPPORT CORROSION WAS REMOVED AND PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN LIMITS IAW SRM 53-00-71 ALLOWABLE DAMAGE 1 FIG 101.

Part: ATTACH ANGLE — CORRODED (BS 1480) · airframe 101,718 hrs · 19,674 cycles

BODY FAIRING 193BL FWD SUPPORT FRAME ATTACH ANGLE FOUND CORRODED. THE ATTACH ANGLE WAS REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02.</P><P><BR DATA-MCE-BOGUS="1" /></P>)

Part: LIGHT — NO TEST (CABIN) · airframe 101,718 hrs · 19,674 cycles

L2 DOOR EMERGENCY LIGHT TEST FAILED. THE EMERGENCY LIGHT WAS REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-06.

Part: ATTACH FITTING — CRACKED (RT FLAP TRACK) · airframe 101,718 hrs · 19,674 cycles

ONE CRACK FOUND ON THE RIGHT WING INBD FLAP TRACK NR 4, FWD ATTACH SUPPORT FITTING INBD ANGLE. REPLACED AND INSTALLED A NEW ATTACH FITTING IAW SRM 51-10-02 AND SRM 51-40-02.

Part: CHANNEL — CRACKED (BS 1200) · airframe 101,718 hrs · 19,674 cycles

BS 1200, RBL 40-50, RT TENSION TIE FWD CHANNEL FOUND CRACKED AROUND FASTENER. THE TENSION TIE FWD CHANNEL WAS REPAIRED IAW RI-53-00-14084, REV A.

Part: STRIP — TORN (RT WING AILERON) · airframe 101,718 hrs · 19,674 cycles

RIGHT WING OTBD AILERON T/E LOWER SURFACE CONDUCTING STRIP INBD AREA FOUND TORN. CONDUCTING STRIP REPLACED IAW RI-57-00-14085, REV A.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

RIGHT WING OTBD MID FLAP L/E INBD SECTION FOUND DELAMINATED, 54 INCHES FROM INBD EDGE. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

LEFT WING OTBD FORE FLAP L/E, INBD SURFACE FOUND DELAMINATED 98 INCHES TO I/B. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: SUPPORT — CORRODED (BS 987.35) · airframe 101,718 hrs · 19,674 cycles

BODY FAIRING SUPPORT, BS 987.35, BL 0 - RBL 55 HAD SURFACE CORROSIONG. THE SUPPORT CORROSION WAS REMOVED AND PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN LIMITS IAW SRM 53-00-71, ALLOWABLE DAMAGE 1, FIG 101.

Part: STRINGER SPLICE — DAMAGED (BS 600-620) · airframe 101,718 hrs · 19,674 cycles

BS 600 - 620, STRINGER 15R AND 17R, STRINGER SPLICE DAMAGED. THE STRINGER SPLICE WAS REPLACED AND REPAIRED IAW RI-53-00-14101 REV A. MAJOR REPAIR.

Part: SUPPORT — CORRODED (BS 1040) · airframe 101,718 hrs · 19,674 cycles

BODY FAIRING SUPPORT STA 1040 LBL 7 TO RBL 7 HAD SURFACE CORROSION. THE CORROSION WAS REMOVED AND THE SUPPORT PROTECTED IAW SRM 51-10-02, AND SRM 51-20-01. CHECKED WITHIN LIMITS IAW SRM 53-00-71, ALLOWABLE DAMAGE 1, FIG 101.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 101,718 hrs · 19,674 cycles

LEFT WING OTBD MID FLAP T/E UPPER SKIN FOUND DELAMINATED 156 INCHES TO INBD. PERFORMED A REPAIR IAW SRM 51-70-07, PAR 5A, REV 108.

Part: PANEL — CORRODED (BS 987-1060) · corrosion level 2 · airframe 101,718 hrs · 19,674 cycles

KEEL BEAM PANEL 191GG FWD AREA FOUND CORRODED. THE KEEL BEAM PANEL WS REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: STRIP — TORN (RT WING AILERON) · airframe 101,718 hrs · 19,674 cycles

RHW OTBD AILERON T/E LOWER SURFACE CONDUCTING STRIP OTBD AREA WAS FOUND TORN. REMOVED AND REBONDED THE CONDUCTING STRIP IAW RI-57-00-14085, REV A.

Part: LIFE VEST — MISSING (CABIN) · airframe 101,504 hrs · 19,637 cycles

MAIN CABIN R-3 FA SEAT MISSING 2 EACH LIFE VESTS.(<P>INSTALLED MAIN PASSENGER CABIN R-3 FA SEAT LIFE VEST (PN&NBSP;<SPAN>RSS-301CT)&NBSP;</SPAN><SPAN>AS PER B747-400 AMM 25-60-00.</SPAN></P>)

Part: SMOKE GOGGLES — DAMAGED (COCKPIT) · airframe 101,504 hrs · 19,637 cycles

COCKPIT 1ST AND 2ND OBS SMOKE GOGGLE DAMAGED.(<P>REMOVED AND REPLACED COCKPIT 1ST AND 2ND OBS SMOKE GOGGLES PER B747-400 AMM 25-13-00.</P>)

Part: BATTERY — DISCHARGED (CABIN) · airframe 101,504 hrs · 19,637 cycles

UPPER DECK EXIT EMERGENCY LIGHTS FOUND SEVERAL INOP.(<P>T/S W/D 33-51-23; REPAIRED U/D EMERGENCY LIGHT WIRING L3661, L3662 AND COVER LENS INSTALLED. OPS CHECK OK. REMOVED AND REPLACED M7038 BATTERY CARTRIDGE PER AMM 33-51-04 (OFF PART: PN&NBSP;<SPAN>9008-3-5A</SPAN><SPAN>, SN 141558</SPAN><SPAN>). REMOVED AND REPLACED M7040 BATTERY CARTRIDGE PER AMM 33-51-04. REMOVED AND REPLACED POWER SUPPLY FUSE (7050) PER AMM 33-51-04/900. EMERGENCY LIGHTS OPS TEST OK AMM 33-51-00/715.</SPAN></P>)

Part: SLIDE — PARTIAL DEPLOY (L4 DOOR) · airframe 101,461 hrs · 19,630 cycles

PASSENGER DOOR 4L SLIDE ASSY PARTIALLY DEPLOYED.(<P>REMOVED DOOR 4L SLIDE ASSY AND SECURED WITH STRAPS. DOOR BOTTLE SAFETY PIN IS INSTALLED. REMOVED SLIDE FROM A/C AND ROUTED TO ANC STORES. TRANSFER TO DMI 125431 PER DDG 52-11-01. PLACARD INSTALLED, CAT 'A'.<BR /></P><P>LP 1179003: REMOVED AND REPLACED L4 SLIDE IAW AMM 25-65-01. THIS CLEARS DMI 125431.</P>)

Part: GENERATOR — FAILED (APU) · airframe 101,206 hrs · 19,586 cycles

ON ENGINE START, ENGINES 1 AND 4, APU QUIT WORKING. SMELL OF ELECTRICAL BURNING AT L5 REPORTED BY FA. POWER WOULD NOT HOLD WITH GPU.(<P>TRANSFERRED TO MDDR 124399 IAW MEL 49-11-01, CAT 'C', DUE 17FEB20. GVI OF APU COMPARTMENT C/W. GEN OF APU CAUSED SMELL PER AMM 49-00-00.</P>)

Part: LIGHT — MISSING (CABIN) · airframe 100,815 hrs · 19,504 cycles

1" STRIP OF ESCAPE PATH LIGHTING AT DOOR R2 MISSING.(<P>REPLACED EMERGENCY LIGHT ASSEMBLIES AND SECURED FLOOR COVERING IAW AMM 33-51-12.&NBSP;</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,588 hrs · 19,456 cycles

MULTIPLE CABIN EMERGENCY FLOOR LIGHTS INOP.&NBSP;(<P>RELAMPED MULTIPLE CABIN EMERGENCY FLOOR LIGHTS. REMOVED AND REPLACED 1 EA LIGHT ASSY IAW&NBSP;AMM 33-51-12-962-002/162.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,588 hrs · 19,456 cycles

MULTIPLE DOOR SILL EMERGENCY LIGHTS INOP.&NBSP;(<P>RELAMPED MULTIPLE EMERGENCY DOOR SILL LIGHT ASSY PER B747-400 AMM&NBSP;33-51-05-962-031, OPS CHECK GOOD.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 100,588 hrs · 19,456 cycles

MULTIPLE CABIN SEAT EMERGENCY LIGHTS INOP.&NBSP;(<P>RELAMPED MULTIPLE CABIN SEAT EMERGENCY LIGHTS, OPERATIONAL CHECK GOOD IAW&NBSP;AMM 33-51-12-962-002.</P>)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 99,610 hrs · 19,267 cycles

RT EXTERNAL OVERWING EMERGENCY LIGHTS HAVE 1 EA LAMPS INOP.&NBSP;(<P>RELAMPED RT EXTERNAL OVERWING EMERGENCY LIGHTS PER AMM 33-51-03-962-001. OPS CHECKED GOOD PER AMM 33-51-03-962-001.</P>)

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 99,610 hrs · 19,267 cycles

IN-SEAT EMERGENCY LIGHT INOP, SEAT 45H.&NBSP;(<P>RESEATED EMERGENCY LIGHT SEAT CONNECTOR AT SEAT 45H PER BSWPM 20-61-28, PAGES 17-19, STEP 4. OPS CHECK GOOD PER AMM 33-51-00-715-001.</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 99,610 hrs · 19,267 cycles

LT UPPER DECK GULL WING DOOR EMERGENCY EXIT SIGN INOP&NBSP;(<P>REMOVED AND REPLACED LT GULL WING DOOR EMERGENCY EXIT SIGN BATTERY PACK AND OPERATIONAL CHECK GOOD</P>)

Part: LIGHT — INOPERATIVE (R5 DOOR) · airframe 99,610 hrs · 19,267 cycles

R-5 DOOR SLIDE LIGHT INOP.&NBSP;(<P>REMOVED AND REPLACED R-5 DOOR SLIDE LIGHT ASSY. OPS CHECKED PER AMM TASK 33-51-06-004-001 AND 33-51-06-404-007.</P>)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 99,610 hrs · 19,267 cycles

LT EXTERNAL OVERWING EMERGENCY LIGHTS HAVE 1 EA LAMPS INOP.&NBSP;(<P>RELAMPED LT EXTERNAL OVERWING EMERGENCY LIGHTS PER AMM 33-51-03-962-001. OPS CHECK PASSED PER AMM 33-51-03-962-001.</P>)

Part: PANEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,268 hrs · 19,194 cycles

KEELBEAM PNL # 191HH RH EDGE COROSSION IN SEVERAL PLACES.&NBSP;(<P>KEEL BEAM PNL #191HH (P/N: 65B10545-113 ASSY) CORROSION AREAS REPAIRED IAW RI-53-40-13560 REV. A.&NBSP;</P>)

Part: LIGHT — MISSING (CABIN) · airframe 99,268 hrs · 19,194 cycles

R2 DOOR RT GALLEY FLOOR EMER. LIGHT AND LENS MISSING. (<P>EMERGENCY LIGHT AND LENS REPLACED. OPS CHECK NORMAL IAW AMM 33-51-00.</P>)

Part: PANEL — DAMAGED (NR 4 PYLON) · airframe 99,268 hrs · 19,194 cycles

#4 PYLON 482EL 1 EA LOCK INDICATOR FOUND ELONGATED. (<P>#4 PYLON 482EL PNL P/N: 311U2060-124 FABRICATED AND REPLACED IAW RI-54-50-13561 REV. A.&NBSP;</P>)

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 99,268 hrs · 19,194 cycles

DOOR 4 GALLEY BOTH SIDE EXIT SIGN INOP. (<P>REMOVED AND REPLACED DOOR 4 GALLEY EXIT SIGN BATTERY PACK. OPERATIONAL TEST RESULT NORMAL AS PER AMM 33-51-00.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,268 hrs · 19,194 cycles

SEAT 16H FLOOR EMERGENCY LIGHT INOP. (<P>REMOVED AND REPLACED EMERGENCY LIGHT LAMP. OPS CHECK NORMAL IAW AMM 33-51-00.</P><P><BR /></P>)

Part: STIFFENER — CORRODED (RT BLG WW) · corrosion level 2 · airframe 99,268 hrs · 19,194 cycles

RT BLG WW KEEL BEEM ATT. APU FIRE SHUTOFF MODULE MOUNTED STIFFENER, INNER SURFACE CORROSION AT STA 1450.(<P>FX - STA 1450 RT 10" BLG WW KEEL BEAM ATT. APU FIRE SHUTOFF MODULE MOUNTED STIFFENER (P/N 69B40371-1) INNER SURFACE CORROSION AREAS REPAIRED IAW RI-53-00-13576 REV. A.&NBSP;</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,268 hrs · 19,194 cycles

DOOR 5 LAV. FWD FLOOR EMERGENCY LIGHT #2 AND #3 INOP. (COUNT FROM LT).(<P>EMERGENCY LIGHT REPLACED. OPERATIONAL CHECK NORMAL IAW AMM 33-51-00.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,268 hrs · 19,194 cycles

L3 DOOR CEILING EMERGENCY LIGHT INOP. (<P>REMOVED AND REPLACED LAMP. OPS CHECK NORMAL IAW AMM 33-51-00.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,268 hrs · 19,194 cycles

SEAT 7AC EMERGENCY LIGHT BULB MISSING. (<P>EMERGENCY LIGHT&NBSP;LAMP REPLACED. OPERATIONAL CHECK NORMAL IAW AMM 33-51-00.</P>)

Part: COWLING — CRACKED (NR 3 ENGINE) · airframe 99,268 hrs · 19,194 cycles

#3 ENGINE LT CORE COWL, INNER WALL AFT FRAME, FOUND CRACK AT 7:30 O' CLOCK POSITION. (<P>#3 ENG LT CORE COWL, INNER WALL AFT FRAME, CRACK AREAS REPAIRED IAW EO:1971A210 REV. 0.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,268 hrs · 19,194 cycles

SEAT 41HK EMERGENCY LT INOP.(<P>EMERGENCY LIGHT LAMP REPLACED. OPS CHK, TEST NORMAL IAW AMM 33-51-00.</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,268 hrs · 19,194 cycles

SEAT 26AC HAS EMERGENCY LIGHT INOP. (<P>REMOVED AND REPLACED EMERGENCY LIGHT BULB. OPS CHK, TESTS NORMAL IAW AMM 33-51-00.</P>)

Part: PANEL — DAMAGED (NR 1 PYLON) · airframe 99,268 hrs · 19,194 cycles

#1 PYLON 452EL 1 EA LOCK INDICATOR FOUND WORN.&NBSP; (<P>FABRICATED #1 PYLON 452EL PNL P/N: 311U2060-124 AND REPLACED IAW RI-54-50-13561 REV. A.&NBSP;</P>)

Part: DOUBLER — CRACKED (PAX DOOR) · airframe 99,268 hrs · 19,194 cycles

L1 PAX DOOR UPPER HINGE DOUBLER FOUND CRACK.&NBSP; (<P>CABIN DOOR 1, LT UPPER HINGE DOUBLER AND OUTER SKIN CRACK AREAS REPAIRED IAW RI-52-10-13555 REV. A.&NBSP;</P>)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,268 hrs · 19,194 cycles

DOOR 2R RT LAV. FLOOR EMERGENCY LT PIN BROKEN (COUNT FROM RT).(<P>EMERGENCY LIGHT REPLACED. OPERATIONAL CHECK NORMAL IAW AMM 33-51-00.</P>)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 99,268 hrs · 19,194 cycles

DOOR 5R EMERGENCY LT POWER PACK M7924 INOP. (<P>REMOVED AND REPLACED 5R DOOR POWER SUPPLY M7924. OPERATIONAL CHECK NORMAL IAW AMM 33-51-00.</P>)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 98,320 hrs · 18,986 cycles

UPPER DECK EMERGENCY LIGHT INOP AT APROX STA 400 CENTER ISLE(<P>REMOVED AND REPLACED POWER SUPPLY BATTERY IAW AMM 33-51-04. OPERATIONAL CHECKS GOOD.&NBSP;</P>)

Part: BRAKE — DELAMINATED (MLG) · airframe 97,313 hrs · 18,772 cycles

NR 8 BRAKE ASSEMBLY FOUND DE-LAMINATED AND NR 8 TIRE DAMAGED FROM BRAKE. REMOVED NR 8 BRAKE AND DEFERRED PER MEL 32-41-01C. NR 8 WHEEL ASSEMBLY REPLACED.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 97,179 hrs · 18,737 cycles

OVEN 9A-06 AFT GALLEY HISSED, SPARKED, AND SMOKED AT THE PLUG. OVEN 9A-06 DEFERRED AND ELECTRICALLY SAFE AS PER NEF PROG 25-20-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,098 hrs · 18,721 cycles

EMERGENCY LIGHT FLOOR LIGHTS FAILED OPS CHECK, LOCATION BETWEEN L2 AND R2 DOORS. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY L2 AND R2 DOORS PER AMM TASKS 33-51-12-022-020 AND 33-51-12-422-021.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 97,098 hrs · 18,721 cycles

3 EMERGENCY LIGHT FLOOR LIGHTS FAILED OPS CHECK, LOCATION BETWEEN L2 AND R2 DOORS. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY BETWEEN L2 AND R2 DOORS PER AMM TASKS 33-51-12-022-020 AND 33-51-12-422-021.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 96,178 hrs · 18,519 cycles

UPPER DECK EMERGENCY EXIT LIGHTS AT THE LT DOOR INOPERATIVE, AND ROW 7, FACING AFT CENTER AISLE, AND ROW 9 FACING FWD CENTER AISLE INOPERATIVE. REMOVED AND REPLACED THE BATTERY IAW AMM 33-51-04, OPS CHECKED GOOD.

Part: ENGINE — FAILED (NR 1) · airframe 96,127 hrs · 18,508 cycles

NR 1 ENGINE OIL QUANTITY FELL TO ZERO AND OIL PRESSURE DROPPED BELOW RED LINE. EICAS MESSAGE FOR THE NR 1 ENGINE OIL PRESSURE. ENGINE SHUTDOWN IN FLIGHT. REMOVE AND REPLACED THE NR 1 ENGINE.

Part: NOT REPORTED — MALFUNCTIONED (CABIN TEMP) · airframe 96,106 hrs · 18,505 cycles

ROW 30 EXTREME HEAT AT SIDEWALL. PRIOR TO EACH FLIGHT, REVIEW CMC FOR ADDITIONAL FAULTS RELATED TO ZONE TEMP.

Part: LANDING GEAR — FOD (RIGHT) · airframe 96,102 hrs · 18,503 cycles

FOUND FIRE EXTINGUISHER WEDGED IN THE RIGHT INBOARD LANDING GEAR TRUCK BETWEEN THE NR 9 AND 10 MAIN LANDING TIRES. THIS CAUSED THE EICAS WARNING CONFIG STAB ON TAKE OFF. THE FIRE EXTINGUISHER RUBBED THE INBOARD SIDE LINER OF EACH NR 9 AND 10 MLG TIRES. REMOVED THE FIRE EXTINGUISHER. PERFORMED CONDITIONAL INSPECTIONS IAW AMM 05-51-58, AND 05-51-25.&NBSP; REMOVED AND REPLACED BOTH MLG WHEEL ASSEMBLIES. ACFT RETURNED TO SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE SKIN) · corrosion level 2 · airframe 95,330 hrs · 18,351 cycles

SKIN DOUBLER AT FUSELAGE SEX 42 POTABLE WATER SERVICE PANEL 192FFR CORRODED. INTERNAL SKIN DOUBLER SURFACE AREA. REPLACED THE DOUBLER IAW SRM 51-40-02-0G-0, REV 101, DWG 65B04118, S42, REV P AND S44 REV H.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,330 hrs · 18,359 cycles

FWD CABIN EMERGENCY LIGHT CRACKED AT THE LAVATORY, REPLACED CABIN EMERGENCY LIGHT IAW SWPM 20-30-12, REV 66, CMM 25-33-41, 25-42-69, REV 2. AND CONDITION CHECK NORMAL. IAW AMM 33-51-12-962-162 REV90 STEP 6.C PERFORMED LAMP TEST AND THE RESULT WAS SATISFACTORY.</P>)

Part: STIFFENER — CORRODED (HORIZONAL STAB) · airframe 95,330 hrs · 18,359 cycles

STIFFENER CORRODED, STAB T/E INNER UPPER SURFACE, HSS 118.9 . REWORKED THE FITTING AREA AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 55-20-09-1A-1, DETAIL III, REV 101. OPS CHECKED GOOD.

Part: ANGLE — CORRODED (DUCT) · corrosion level 2 · airframe 95,330 hrs · 18,359 cycles

DUCT ASSY AT AIR CONDITIONING NR 2 RAM AIR INLET DUCT AREA CORRODED. REMOVED AND REPLACED THE CORRODED ANGLE IAW SRM 51-40-02, REV 101, AND DWG 65809716, SHEET 3, REV F. OPS CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 95,330 hrs · 18,359 cycles

FOUND MANY MAIN DECK AND UPPER DECK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY BATTERIES IAW AMM 33-51-06-000-801 AND 33-51-06-400-801, REV 91. REPLACED SLIDE LIGHT BATTERIES IAW AMM 33-51-06-400-801, REV 91. PERFORMED EMERGENCY LIGHT OPS TEST AND THE RESULT WAS SATISFACTORY.

Part: SKIN — CORRODED (LT WING) · airframe 95,330 hrs · 18,359 cycles

LEFT WING INSPAR UPPER SKIN UPPER SURFACE CORRODED. WBL 183 - WBL 210 FRONT SPAR - S27. REMOVED CORROSION IAW SRM 51-10-02, REV 101. WITHIN ALLOWABLE LIMITS IAW SRM 57-20-01-1A-1, FIG 1-1, DETAIL II, REV101.

Part: SKIN — CORRODED (RT WING) · airframe 95,330 hrs · 18,359 cycles

RT WING INSPAR UPPER SKIN UPPER SURFACE ACCESS REAR SPAR CORRODED, WS 528.2. REMOVED CORROSION IAW SRM 51-10-02 REV101. WITHIN ALLOWABLE LIMITS IAW SRM 57-20-01-1A-1, FIG 101, DETAIL II, REV 101.

Part: DUCT — CORRODED (A/C PACK) · corrosion level 2 · airframe 95,330 hrs · 18,359 cycles

DUCT ASSY AT AIR CONDITIONING NT 3 RAM AIR INLET DUCT AREA CORRODED. REMOVED AND REPLACED THE DAMAGED PARTS IAW SRM 51-40-02-0G-0, REV 101, AND DWG NO 65B09715, SHEET 3, REV G. OPS CHECKED NORMAL.

Part: SKIN — CORRODED (BS 2090) · airframe 95,330 hrs · 18,359 cycles

SKIN CORRODED, BS 2090 BETWEEN STRINGERS 35R AND 36R. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01-1A-1, TABLE I, FIGURE 101, DETAIL II, REV 101.

Part: RIVET — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 95,330 hrs · 18,759 cycles

RT HORIZONTAL STAB FIXED T/E RBL 372 - RBL 392 RIVET CORRODED. REMOVED THE RIVET IAW SRM 51-40-02, REV.1. INSTALLED A NEW RIVET IAW DWG 65B03710 SH2, REV J, AND SRM 51-40-02, REV 1. CHECKED NORMAL.

Part: STRAP — CORRODED (LT WING) · corrosion level 2 · airframe 95,330 hrs · 18,359 cycles

THE UPPER STRAP OF THE LT WING LEADING EDGE NEAR OLES 1525 CORRODED. REPAIRED THE AREA IAW EI T2017A57M-2362 REV 1. OPS CHECK NORMAL</P>)

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 95,330 hrs · 18,359 cycles

BULGE DAMAGE ON THE LT WING LEADING EDGE LOWER SKIN NEAR ILES 500. REPAIRED THE AREA IAW EI T2017A57M-2423, REV 3. CHECKED NORMAL.

Part: BULKHEAD WEB — CORRODED (BS 1241) · airframe 95,330 hrs · 18,359 cycles

SKIN BS 1241, RBL 93, WW BULKHEAD AFT FACE CORRODED. CORROSION REMOVED AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2, DETAIL V, REV 101, PERFORMED SURFACE NDT INSPECTION AND BONDING TEST AT REWORKED AREA IAW JOB CARD. REWORK AREA IAW SRM 51-20-01 REV101. CHECKED GOOD.

Part: BULKHEAD — CORRODED (BS 1253) · airframe 95,330 hrs · 18,359 cycles

MLG WW. FWD BULKHEAD, BS 1253, LBL91 CORRODED. CORROSION REMOVED AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2, DETAIL V, REV 101. PERFORMED SURFACE NDT INSPECTION AND BONDING TEST AT REWORKED AREA. CHECKED GOOD.

Part: STRUCTURE — CRACKED (BS 1480) · airframe 95,330 hrs · 18,359 cycles

CRACK ON RT WHEEL WELL HINGE BOX AT BS 1480. ACCOMPLISHED EI T2017A53M-2275, REV 1.

Part: SKIN — CORRODED (BS 2090) · airframe 95,330 hrs · 18,359 cycles

SKIN CORRODED AT BS 2090, BETWEEN STRINGERS 35L AND 36L. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01-1A-1, TABLE I, FIGURE 101, DETAIL II, REV 101. PERFORMED PROTECTIVE TREATMENT ON REWORKED AREA IAW SRM 51-20-01 REV 101.

Part: FLOORBEAM — CORRODED (BS 460) · corrosion level 2 · airframe 95,330 hrs · 18,359 cycles

CORROSION ON THE FLOORBEAM UPPER TEE AT BS 460, BETWEEN LBL 39 TO LBL 51. BLENDED AND REPAIRED THE AREA IAW EI T2017A53M-2357, REV 2.

Part: FUEL FILTER — MALFUNCTIONED · airframe 94,841 hrs · 18,262 cycles

AN IN-FLIGHT DIVERSION HAPPENED DUE TO BOTH AN ENGINE 3 FUEL FILTER EICAS STATUS MESSAGE, AND AN ENGINE 4 FUEL FILTER EICAS STATUS MESSAGE. THE FUEL FILTER ELEMENTS WERE REPLACED.

Part: PANEL — MISSING (NR 2 NACELLE) · airframe 94,233 hrs · 18,147 cycles

PANEL 461AL ON THE NR 2 PYLON OTBD DISCOVERED MISSING DURING WALK AROUND INSPECTION. INSTALLED A TEMPORARY PANEL IAW EO 4454A089.

Part: WARNING MESSAGE — FALSE ACTIVATION (CONFIGURATION) · airframe 93,757 hrs · 18,049 cycles

STAB CONFIGURATION EICAS MESSAGE DURING TAKEOFF ROLL. REJECTED TAKEOFF COMPLIED WITH FIM 31-51, TASK 807, RESET MAWEA CONFIGURATION WARNING CARD. PERFORMED TAKEOFF WARNING TEST, PASSED.

Part: FIRE WARNING — FALSE ACTIVATION (APU BAY) · airframe 93,315 hrs · 17,958 cycles

APU FIRE INDICATION DURING ROLL OUT AFTER LANDING, PULLED APU FIRE HANDLE AND DISCHARGED FIRE BOTTLE. APU FIRE WARNING LIGHT WAS A FALSE INDICATION. LIGHT REMAINED ON ABOUT 10-12 MINUTES. CHECKED AND INSPECTED APU AND FIRE LOOPS AND FOUND ALL NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,014 hrs · 17,992 cycles

DURING INSPECTION, FOUND LUD POWER ASSIST BATTERY INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51-04, OPS OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,014 hrs · 17,692 cycles

EMERGENCY LIGHTS INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-51-04, OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 91,821 hrs · 17,653 cycles

CABIN EMERGENCY LIGHTS ARE INOPERATIVE. REPAIRED WIRING TO LIGHTS IAW 20-10-17. ALL CHECKED GOOD AT THIS TIME.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 91,736 hrs · 17,635 cycles

CREW PERFORMED LOW SPEED REJECTED T/O WHEN EICAS MSG FOR OVERRIDE JETT PUMP NR 3 FWD APPEARED. PLACED ON DMI.

Part: LENS — LOOSE (CABIN) · airframe 91,518 hrs · 17,591 cycles

EMERGENCY LIGHT COVER IN MID GALLEY LOOSE. SECURED LENS ASSY AT MID GALLEY, OPS NORMAL IAW AMM 33-50-00.

Part: A/C PACK — FAULTY (AC BAY) · airframe 91,369 hrs · 17,565 cycles

EICAS MSG PACK 3. NOTED STRONG FUMES IN COCKPIT. NR 3 PACK CONFIRMED FAULTY & PLACED ON DMI IAW DDG 21-51-01-01.

Part: WIRE — DAMAGED (CABIN) · airframe 91,233 hrs · 17,540 cycles

EMERGENCY EXIT LIGHT BETWEEN L2 & R2 DOOR INOPERATIVE & FLOOR LIGHTING AT L5 & R5. SPLICED EMER LIGHT WIRES, BETWEEN L2 & R2 DOORS, BETWEEN L5 & R5 DOORS IAW SWPM 20-30-12. OPERATIONS CHECKED GOOD IAW AMM 33-51-00.

Part: SKIN — DENTED (FUSELAGE) · airframe 91,058 hrs · 17,504 cycles

DENT AT FUSELAGE SKIN RT SIDE, ABOVE MAIN CABIN WINDOWS 4 & 5. DENT FOUND TO BE PRE-EXISTING, REWORK EXCEEDING ALLOWABLE LIMITS IAW SRM 53-00-01-2R-15 REPAIR 15. ACCOMPLISHED PERMANENT REPAIR CATEGORY B, THRESHOLD 1200 FC & INTERNAL 600 FC.

Part: LIFE RAFT — MISSING (R5 DOOR) · airframe 91,058 hrs · 17,504 cycles

R5 DOOR LIFE RAFT IS MISSING. INSTALLED R5 DOOR LIFE RAFT IN OVERHEAD BIN IAW AMM 25-62-02.

Part: SKIN — GOUGED (FUSELAGE) · airframe 91,058 hrs · 17,504 cycles

GOUGE IN FUSELAGE SKIN FWD OF AFT CARGO DOOR, STATION 1806, BELOW STRINGER 39R. BLENDED GOUGE & RESTORED FINISH IAW SRM 53-00-01 & 51-40-02.

Part: LIGHT — DAMAGED (CABIN) · airframe 91,058 hrs · 17,504 cycles

FORWARD MID GALLEY EMER PATH LIGHTING STRAP IN FRONT OF GALLEY 707 IS DAMAGED. REPAIR ACCOMPLISHED ON NR 00412 IAW SUPPLEMENTAL SHEET ITEM 2, PAO I-40 ATTACHED.

Part: GATE — CORRODED (L5 DOOR) · airframe 91,058 hrs · 17,504 cycles

CORROSION ON THE L5 DOOR LOWER GATE AROUND BOTH WEAR PADS. R & R L5 DOOR LOWER GATE IAW SRM 51-40-02.

Part: COVER — MISSING (CABIN) · airframe 91,058 hrs · 17,504 cycles

EMERGENCY FLOOR LIGHTING ABOVE STAIRWAY TO UPPER DECK HAS MISSING & WORN TRACK COVERS. INSTALLED MISSING TRACK COVERS ABOVE STAIRWAY TO UPPER DECK IAW AMM 33-51-12.

Part: SKIN — GOUGED (FUSELAGE) · airframe 91,058 hrs · 17,504 cycles

FUSELAGE SKIN STATION 552, BELOW STRINGER 37R, HAS DENT & GOUGE PREVIOUS DAMAGE, FOUND TO BE OUT OF LIMITS DURING DENT LOG REVIEW. ACCOMPLISHED PERMANENT CATEGORY B REPAIR IAW SRM 53-00-01 REPAIR 1. FAA FORM 8100-9 RECEIVED FOR INSPECTION THRESHOLD OF 6000 FC APPROVAL.</P>)

Part: COMPOUND — ERODED (L4 DOOR) · airframe 91,058 hrs · 17,504 cycles

L4 DOOR FAIRING COMPOUND ERODED AT LOWER FWD & LOWER AFT SURROUND CORNERS. RESTORED FAIRING COMPOUND AS REQUIRED AT LOWER FWD & AFT CORNER OF L4 DOOR.

Part: RIVET — SHEARED (R5 DOOR) · airframe 91,058 hrs · 17,504 cycles

R5 DOOR SURROUND EXTERIOR UPPER CORNER HAS 1 EA SHEARED RIVET. R & R RIVET, RESTORED LEVELING COMPOUND IAW SRM 51-40-02 & AMM 52-09-02.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 90,887 hrs · 17,470 cycles

MAIN CABIN & UPPER DECK, SEVERAL CABIN EMER LIGHTS INOPERATIVE. RESEATED CONNECTOR ON MAIN CABIN & UPPER DECK LIGHTS. OPERATIONS CHECKED IAW AMM 35-51-12.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 90,887 hrs · 17,470 cycles

MAIN CABIN & UPPER DECK, SEVERAL CABIN EMER LIGHTS INOPERATIVE. RESEATED CONNECTOR ON MAIN CABIN & UPPER DECK LIGHTS. OPERATIONS CHECKED IAW AMM 35-51-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,887 hrs · 17,470 cycles

MAIN CABIN FIRST RT SIDE FLOOR EMER LIGHTS INOPERATIVE. R & R MAIN CABIN FIRST CLASS RT SIDE FLOOR EMER LIGHTS IAW AMM 33-51-12. OPERATIONS OK IAW AMM 33-51-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,887 hrs · 17,470 cycles

MAIN CABIN FIRST CLASS, RT SIDE FLOOR EMER LIGHTS INOPERATIVE. R & R IAW AMM 33-51-12. OPERATIONS OK IAW AMM 33-51-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,924 hrs · 17,272 cycles

EMERGENCY LIGHTS AT SEATS 45 - 57 HJK & MAIN DECK ZONE A RT SEATS & FLOOR INOPERATIVE. REPAIRED EMER LIGHTS AS REQUIRED IAW AMM 33-51-12, 33-51-00 & SWPM 20-30-12.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 89,924 hrs · 17,272 cycles

DAMAGE FOUND TO FUSELAGE SKIN AT STATION 1925, AFT CARGO DOOR AREA, A =1.5", Y =1/16". VISUAL INSPECTION EVERY 250 FLIGHT CYCLES. REMOVED DAMAGE & REPAIRED IAW SRM 53-00-01-2R-1 REPAIR 1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,539 hrs · 17,198 cycles

EMERGENCY LIGHT AT UPPER DECK DOORS LT & RT INOPERATIVE. RELAMPED EACH OVERHEAD LIGHT IAW AMM 33-50-00. ALL EMER LIGHTS OPERATIONS OK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,096 hrs · 17,104 cycles

FLOOR PROX LIGHT 46H, 47H, 48H, 50H & 60H REPLACED IAW 33-51-12. 60H STILL INOPERATIVE. TRANSFERRED TO MEL 33-21-01-01-01C.

Part: SIGN — DETACHED (EMERGENCY EXIT) · airframe 88,279 hrs · 16,957 cycles

EXIT & LIFT HANDLE SIGN DETACHED ON RT UPPER DECK DOOR. REATTACHED EXIT & LIFT HANDLE ON RT UPPER DECK DOOR IAW SOPM 20-50-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,279 hrs · 16,957 cycles

EMERGENCY LIGHTS OUT AT SEAT 45H & NEAR WASTE CONTAINER 1-06 GALLEY 1. REPLACED LAMPS AT SEATS 45H & NEAR WASTE CONTAINER 1-06 GALLEY 1 IAW AMM 33-51-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,279 hrs · 16,957 cycles

EMERGENCY LIGHT INOPERATIVE, UPPER DECK AT EDGE OF STAIRS TWO EACH. REPLACED LAMPS AT UPPER DECK STAIR EDGE IAW AMM 33-51-12.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,279 hrs · 16,957 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 40C & 41C. REPLACED LAMPS AT SEAT 40C & 41C IAW AMM 33-51-12.

Part: LENS — MISSING (CABIN) · airframe 87,773 hrs · 16,851 cycles

FLOOR EMER LIGHT LENS MISSING IN ZONE A. REPLACED FLOOR EMER LIGHT LENS IAW AMM 33-51-12.

Part: BATTERY — DISCHARGED (CABIN) · airframe 87,754 hrs · 16,844 cycles

EMERGENCY LIGHTS AT 5L INOPERATIVE. COMPLIED WITH EMER LIGHT SYS TEST. LIGHTS AT 5L OPERATIONS CHECK GOOD IAW AMM 33-51-00. R & R BATTERY ASSEMBLY M7923 5L DOOR OVERHEAD IAW AMM 33-51-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,754 hrs · 16,844 cycles

3L EMER LIGHT ON L3 DOOR INOPERATIVE. RELAMPED EMER LIGHT ON L3 DOOR. OPERATIONS NORMAL IAW AMM 33-50-01.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 87,687 hrs · 16,829 cycles

WHEN POWER WAS RETARDED FOR DESCENT SMOKE & FUMES ENTERED COCKPIT. STRONG TURBINE OIL SMELL. REF EO 1972556 PART 1 ACCOMPLISHED. OIL CONSUMPTION VERIFICATION & ENG BLEED DEACTIVATION.

Part: CONNECTOR — LOOSE (CABIN) · airframe 87,687 hrs · 16,829 cycles

REF MDDR 54771 PATH LIGHT AT L2 JUMP SEAT INOPERATIVE. SECURED LOOSE CONNECTOR AT LIGHT CAPSULE. OPERATIONS CHECKED GOOD IAW AMM 33-51-12. PLACARDS REMOVED MC NOTIFIED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 87,669 hrs · 16,824 cycles

WHEN POWER WAS RESTARTED FOR DESCENT SMOKE & FUMES ENTERED COCKPIT. STRONG TURBINE OIL SMELL. TROUBLESHOOTING IN WORK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,669 hrs · 16,824 cycles

EMERGENCY PATH LIGHTING BY L2 JUMP SEAT INOPERATIVE. DEFERRED IAW MDDR 54771 MEL 33-51-03 CAT C.

Part: STRAP — CRACKED (FUSELAGE) · airframe 87,325 hrs · 16,738 cycles

SECTION 46 FRAME BS 2231, CRACK DAMAGE FOUND ON FRAME STRAP BETWEEN STRINGER 25L & 26L DURING ACCOMPLISHMENT OF SB 747-53A2450 REV 7 AD 2013-17-08. ACCOMPLISHED REPAIR IAW 747-5360-28A5682 REV & IR & EO 4453B049 REV 0.

Part: OXYGEN MASK — DEPLOYED (CABIN) · airframe 86,329 hrs · 16,562 cycles

PASSENGER OXYGEN MASK DEPLOYED BY FLIGHT CREW ON GND. NO PAX ON BOARD. SECURED ALL PASSENGER OXYGEN & FLIGHT CREW MASKS THROUGHOUT CABIN IAW MM 35-21-31.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 86,164 hrs · 16,527 cycles

UPPER DECK AFT MOST EMER LIGHT AT STATION 945 FLICKERS. R & R AFT UPPER EMER LIGHT IAW AMM 33-51-07-002-009. OPERATIONS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 86,164 hrs · 16,527 cycles

EMERGENCY LIGHT LENS AT SEAT 60H IS MISSING. INSTALLED EMER LIGHT LENS AT SEAT 60H IAW AMM 33-51-02.

Part: LENS — MISSING (CABIN) · airframe 86,164 hrs · 16,527 cycles

SEAT 60H END BAY COVER MISSING ESCAPE PATH LIGHTING. INSTALLED PATH LIGHTING COVER AT 60H IAW AMM 33-51-12.

Part: LENS — MISSING (CABIN) · airframe 86,164 hrs · 16,527 cycles

SEAT 4C END BAY COVER MISSING ESCAPE PATH LIGHTING LENS. FOUND LIGHT LENS FOR END BAY COVER FOR SEAT4C. UNDER SEAT INSTALLED AS REQUIRED IAW AMM 33-51-12.

Part: LENS — MISSING (CABIN) · airframe 86,164 hrs · 16,527 cycles

EMERGENCY LIGHT LENS AT SEAT 47C IS MISSING. REPLACED EMER LIGHT LENS AT SEAT 47C IAW AMM 33-51-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 85,682 hrs · 16,438 cycles

HYD QTY LOW 4 EICAS, QRH COMPLIED WITH. COMPLIED WITH FIM 32-61 TASK 808, HYDIM 4 GND TEST PASSED, NO FAULTS NOTED. PRESSURIZED HYDS, CYCLED FLIGHT CONTROLS & PERFORMED LEAK CHECK, NO LEAKS FOUND & OPERATIONS CHECKED GOOD.

Part: SWITCH — STUCK (COCKPIT) · airframe 85,420 hrs · 16,383 cycles

DURING TRANSIT CHECK FOUND EMERGENCY LIGHT SWITCH STUCK IN ARMED POSITION ON OVERHEAD COCKPIT. R & R OVERHEAD EMERGENCY LIGHTING SWITCH IAW MM 33-50-00, POSITION CHECKED NORMAL.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 85,290 hrs · 16,358 cycles

EMERGENCY ESCAPE PATH FLOOR LIGHTING ADJACENT TO SEAT 45H IS INOPERATIVE. SECURED CONNECTOR TO EMERGENCY PATH LIGHT AT SEAT 45H. OPERATIONS CHECKED GOOD IAW AM 33-50-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 84,968 hrs · 16,284 cycles

EMERGENCY LIGHTING ON FLOOR AT R2 INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM 33-51-12. OPERATIONAL CHECKED OK IAW AMM 33-51-00.

Part: WIRE — DAMAGED (CABIN) · airframe 84,968 hrs · 16,284 cycles

UPPER DECK FLOOR EMERGENCY LIGHTING INOPERATIVE. REPAIRED WIRING IAW SWPM 20-30-12. OPERATIONAL CHECK OK IAW AMM 33-51-00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 615,561 hrs · 84,968 cycles

LEFT HAND FIRST CLASS EMERGENCY FLOOR LIGHTING INOPERATIVE. R & R LT HAND FIRST CLASS EMERGENCY FLOOR LIGHTING BATTERY ASSEMBLY IAW AMM 33-51-00. ALL OPERATIONAL CHECKS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 73,349 hrs · 13,951 cycles

EICAS MESSAGE, DOOR FWD CGO, ON DEPARTURE PASSING 4000 FEET. PERFORMED DOOR OPERATIONAL CHECK IAW AMM 52-34-00-705-001, ALL OPERATIONS NORMAL. WARNING SYS CHECKED IAW AMM 52-71-00-715-005, NO DEFECTS NOTED.

Part: LIGHT — DAMAGED (CABIN) · airframe 73,345 hrs · 13,950 cycles

FLOOR TRACK EMERGENCY LIGHT DAMAGED AT DOOR 2R. REPAIRED EMERGENCY LIGHT AT 2R DOOR IAW SWPM 20-30-12. SYS OPERATIONS CHECKED GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 84,248 hrs · 16,117 cycles

EMERGENCY FLOOR LIGHTS BY SEAT ROW 16AC IS TAPED DOWN. SECURED IAW AMM 33-51-12-422-021.

Part: LIGHT — LOOSE (CABIN) · airframe 84,248 hrs · 16,117 cycles

EMERGENCY; LIGHTS ON FLOOR BY SEAT ROW 12AC HAVE; TAPE HOLDING THEM DOWN. SECURED IAW AMM 33-51-12-422-021.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 84,248 hrs · 16,117 cycles

EMERGENCY LIGHTS FLOOR BY SEAT ROW 11ABC IS MISSING PARTS. INSTALLED EMERGENCY LIGHT END CAPS IAW AMM 25-27-05).

Part: LIGHT — LOOSE (CABIN) · airframe 84,248 hrs · 16,117 cycles

UPPER DECK BETWEEN LT AND RT WING DOORS, TWO EMERGENCY EXIT FLOOR LIGHTS ARE TAPED DOWN. SECURED IAW AMM 33-51-12-422-021.

Part: ACTUATOR — FAILED (OUTFLOW VALVE) · airframe 10,729 hrs · 2,131 cycles

EICAS CABIN ALTITUDE AUTO; EICAS OUTFLOW VALVE LIGHT. R & R OUTFLOW VALVE ICU, VALVE ACTUATOR, & DIODES.

Part: FRAME — CRACKED (BS 320) · airframe 83,268 hrs · 15,910 cycles

WHILE ACCOMPLISHING EO:4453A295, REV 6, FOUND CRACK ON LOWER FRAME WEB BS 320, LBL 28. WEB REPLACED IAW EO:4453A295, PART 2 WHICH IS RELATED TO SB747-53A2784. NOTE: EO COMPLIES WITH AD 2012-22-02.

Part: SKIN — DENTED (BS 140-160) · airframe 83,268 hrs · 15,910 cycles

EXTERNAL FUSELAGE, DENT IN SKIN ON RT SIDE OF FUSELAGE BETWEEN BSTA 140-160 & STR 24R-26R. ACCOMPLISHED PERMANENT REPAIR BY INSTALLING REINFORCING DOUBLER AND TRIMMING OUT DENT IAW EA 5300-28-A4695, REV ORIG & IAW EO.

Part: STRINGER — DENTED (BS 140-160) · airframe 83,268 hrs · 15,910 cycles

DENT FOUND ON STRINGER 34R, 140-160, WHILE ACCCOMPLISHING REPAIR IAW STA-SA 747-5300-28-A4695 ON NRC A000442. REPAIRED IAW EA 747-5300-28-A4724.

Part: SLIDE — NO TEST (L3 DOOR) · airframe 83,268 hrs · 15,910 cycles

L3 DOOR OVERWING SLIDE FAILED TO DEPLOY SUCCESSFULLY DURING AN INADVERTENT DEPLOYMENT. (OUTSIDE SERVICE) REPACKED L3 DOOR SLIDE IAW CMM 25-65-05, REV 11. L3 DOOR SLIDE REINSTALLED IAW AMM 25-65-16-404-022.

Part: STRINGER — DENTED (BS 140-160) · airframe 83,268 hrs · 15,910 cycles

DENT FOUND ON STRINGER 31R, BS 140-160. WHILE ACCOMPLISHING REPAIR IAW STA-SA EA 747-5300-28-A4695 ON NRC A000442. REPACED STRINGER IAW 51-40-02 AND DWG 65B07656.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 82,944 hrs · 15,844 cycles

FLASHLIGHT NEXT TO L2 DOOR INOPERATIVE. FOUND BATTERY INOPERATIVE AND CRADLE BROKEN. OPEN

Part: SKIN — DAMAGED (FUSELAGE) · airframe 82,666 hrs · 15,788 cycles

DURING LIGHTNING STRIKE INSPECTION, MX FOUND HOLE DAMAGE (APROX. 0.455 IN. DIA) ON THE FUSELAGE SKIN AND RING FRAME AT BS 134.75, S-45L. THE DAMAGE ON THE FUSELAGE SKIN WAS TRIMMED OUT AND REPAIR BASED ON SRM 53-00-01, REPAIR 1. THE SKIN (PN: 65B07658- 1001) IS MADE FROM 0.056 IN THICK 2024-T3 AL CLAD IAW QQ-A-250/5. THE LT LOWER RING FRAME (PN: 65B01700-529) IS MADE OF 0.063" THICK 7075-0 AL CLAD IAW QQ-A-250/13 AND HEAT TREATED TO T6 AFTER FORMING. THE TIME LIMITED REPAIRS INSTALLED ON THE FUSELAGE SKIN AND LOWER LT RING FRAME AT BS 134.75 IAW PART 1 AND PART 2 OF THIS EO WILL BE REPLACED BY A PERMANENT REPAIR IAW PART 4 OF THIS EO AT THE NEXT C-CHECK.)

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 82,303 hrs · 15,702 cycles

RIGHT OVER WING FWD EMERGENCY LIGHT AFT BULB INOPERATIVE. REPAIRED RT OVERWING EMERGENCY LIGHT WIRE IAW SWPM 20-10-13. PERFORMED EMERGENCY LIGHT SYS OPS CHECK, OK IAW AMM 33-51-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 82,303 hrs · 15,702 cycles

MAIN DECK ROW 45, RT EMERGENCY LIGHT INOPERATIVE. REPAIRED ROW 45 RT EMERGENCY LIGHT WIRE AND OPS CHECKED OK IAW SWPM 20-10-13 AND AMM 33-51-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,303 hrs · 15,702 cycles

MAIN DECK R05 SLIDE LIGHT INOPERATIVE. LAMPED R5 SLIDE SLIGHT. OPS CHECKED NORMAL REF AMM 33-51-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,303 hrs · 15,702 cycles

MAIN DECK L1 AFT DOOR SILL THRESHOLD EMERGENCY LIGHT INOPERATIVE. "L1854", LAMPED EMERGENCY LIGHT. OPS CHECKED NORMAL REF AMM 33-51-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 82,303 hrs · 15,702 cycles

MAIN DECK ROWS 29-32 LT EMERGENCY LIGHT INOPERATIVE. REPAIRED LIGHT. EMERGENCY LIGHT WIRING IAW SWPM 20-10-13. EMERGENCY LIGHT SYS OPS CHECKED OK IAW AMM 33-51-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 82,303 hrs · 15,702 cycles

MAIN DECK ZONE A, EMERGENCY LIGHT INOPERATIVE. LT AND RT ROWS 12-16. REPAIRED WIRING IAW SPWM 20-10-13. EMERGENCY SYS LIGHT OPS CHECKED OK IAW AMM 33-51-00.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 82,303 hrs · 15,702 cycles

UPPER DECK L1 DOOR FWD EMERGENCY LIGHT INOPERATIVE. REPAIRED WIRE IAW SWPM 20-10-13. OPS CHECKED OK IAW AMM 33-51-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,303 hrs · 15,702 cycles

MAIN DECK R-4 FWD DOOR SILL THRESHOLD EMERGENCY LIGHT INOPERATIVE. LAMPED LIGHT. OPS CHECKED NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,303 hrs · 15,702 cycles

MAIN DECK L3 DOOR SILL THRESHOLD EMERGENCY LIGHT INOPERATIVE. LAMPED EMERGENCY LIGHT. OPS CHECKED NORMAL, REF AMM 33-51-00.

Part: OVEN — INOPERATIVE (GALLEY) · airframe 81,624 hrs · 15,570 cycles

OVEN AT GALLEY G-02 STOP WORKING, FOUND EVIDENCE OF SMOKE AND CIRCUIT BREAKER POPPED. CIRCUIT BREAKER PULLED AND COLLARED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,340 hrs · 15,509 cycles

MAIN DECK SEAT 55H EMERGENCY LIGHT INOPERATIVE, RELAMPED, OPS CHECKED OK IAW MM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,340 hrs · 15,509 cycles

MAIN PASSENGER CABIN FLOOR EMERGENCY LIGHT IN L2 ENTRY DOOR AREA INOPERATIVE. R & R LIGHT AT L2 DOOR IAW MM 33-51-00. OPS CHECKED OK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 81,340 hrs · 15,509 cycles

MAIN DECK AT FIRST CLASS SECTION, BETWEEN LT SEAT ROWS 12 AND 16, ALL FLOOR PROXIMITY LIGHTS ARE OUT. RESECURED CONNECTOR AT SEAT 12A. OPS CHECKED OK IAW MM 33-51-00.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 81,340 hrs · 15,509 cycles

MAIN DECK 2 FLOOR PROXIMITY LIGHTS OUT AFTER 16H SEAT. SECURED LOOSE CONNECTION AT LIGHT ASSY ON FLOOR AT 16H. OPS CHECKED OK IAW MM 33-51-00.

Part: LIGHT — BURNED OUT · airframe 81,340 hrs · 15,509 cycles

ONE EMERGENCY LIGHT OUT AT DOOR ENTRY AREA. NEED PN S417N509, LT ASSY. R & R LIGHT ASSY AT L1 DOOR IAW MM 33-51-00. OPS CHECKED OK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 81,340 hrs · 15,509 cycles

UPPER DECK, 2 FLOOR PROXIMITY LIGHTS OUT BETWEEN LT SEAT ROW 6 AND 7 IN FRONT OF EMERGENCY EXIT DOOR. SECURED LOOSE CONNECTION AT FLOOR LIGHT ASSY, OPS CHECK OK IAW MM 33-51-00/ SOP.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 81,340 hrs · 15,509 cycles

MAIN DECK SEAT 23C EMERGENCY LIGHT INOPERATIVE. SECURED LOOSE CONNECTOR AT LIGHT ASSY. OPS CHECKED OK IAW MM 33-51-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,340 hrs · 15,509 cycles

MAIN DECK, ONE EMERGENCY LIGHT OUT AT R1 DOOR ENTRY AREA. RELAMPED LIGHT. OPS CHECKED OK IAW MM 33-51-00.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 81,340 hrs · 15,509 cycles

MAIN DECK BESIDE 14K SEAT, 2 FLOOR PROXIMITY LIGHTS INOPERATIVE. REINSTALLED LIGHT ASSY CONNECTOR AT SEAT 14K. OPS CHECKED OK IAW MM 33-51-00.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 81,340 hrs · 15,509 cycles

EMERGENCY LIGHTS OUT AFTER LT SEAT ROW 11 AT STAIR AREA. SECURED LOOSE CONNECTOR AT FLOOR LIGHT ASSY, OPS CHECKED OK IAW MM 33-51-00.

Part: PANEL — INOPERATIVE (OXYGEN SYSTEM) · airframe 7,442 hrs · 1,448 cycles

WHILE ON GROUND, PRIOR TO DEPARTURE, CREW INADVERTENTLY DEPLOYED THE OXYGEN SYSTEM. MAINTENANCE SECURED ALL OXYGEN MASKS, RESET OXYGEN SYSTEM. UNABLE TO CLOSE SEATS 16DG & 60 DEG OXYGEN PANELS, PANELS SECURED AND SEATS BLOCKED ACCORDINGLY. OPEN

Part: LIGHT — MISSING (CABIN) · airframe 80,344 hrs · 15,308 cycles

EMERGENCY LIGHT MISSING FROM SEAT 17R. AISLE LOCATOR EMERGENCY LIGHT ASSY INSTALLED AT SEAT 17 RT; OPS CHECKED OK IAW AMM 33-51-12.

Part: LIGHT — DAMAGED (CABIN) · airframe 80,344 hrs · 15,308 cycles

UPPER DECK EMERGENCY PATH LIGHTING AT LT EXIT DOOR DAMAGED.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 80,344 hrs · 15,308 cycles

UPPER DECK E-PATH FLOOR LIGHTS AFT TO DOOR INOP. FOUND WIRES TO FLOOR LIGHT ASSY BROKEN BY SEAT 11A. R & R FLOOR AISLE LOCATOR 11A SEAT; OPS CHECKED OK IAW AMM 33-51-12.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 80,344 hrs · 15,308 cycles

LEFT AFT LAV FLOOR EMERGENCY LIGHT INOPERATIVE. RESECURED LOOSE CONNECTOR IAW SWPM 20-60-06, PERFORMED OPS CHECK IAW MM 33-50-00; OPS CHECKED NORMAL.

Part: LIGHT — BROKEN (CABIN) · airframe 80,344 hrs · 15,308 cycles

UPPER DECK LT DOOR AFT FLOOR LIGHT INOP. FOUND LIGHT ASSY DISCONNECTED AND BROKEN. INSTALLED U/D FLOOR LIGHT LT DOOR, OPS CHECKED OK IAW AMM 33-07-00)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 80,344 hrs · 15,308 cycles

"A" ZONE FLOOR E-PATH RT AND LT SIDE INOPERATIVE. LT SIDE AFT A ZONE FOUND OPEN WIRE FROM CONNECTOR DM 2915 PIN 14; TRACED WIRE BACK FROM EMERGENCY LIGHT ASSY TO SIDEWALL. REMOVED SIDEWALL AND TRACED WIRE BEHIND SIDEWALL TO CONNECTOR D23661A. FOUND CONNECTOR DISCONNECTED. RESECURED CONNECTOR. RESECURED MULTIPLE LOOSE CONNECTORS ON RT SIDE, EMERGENCY LIGHTS IAW SWFM 20-60-06. PERFORMED OPS CHECK IAW MM 33-50-00. OPS CHECKED OK.

Part: LIGHT — FAILED (CABIN) · airframe 79,401 hrs · 15,100 cycles

FOUND RIGHT NR 4 OVERWING EMERGENCY LIGHT LENS BROKEN AND GROUND STUD LOOSE. LIGHT ASSY REPLACED AND CHECKED NORMAL IAW AMM 33-51-03.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

SEAT 53HJK CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BULB REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-07.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

R4 DOOR MOUNTED EMERGENCY LIGHT FOUND INOPERATIVE. BULB REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,401 hrs · 15,100 cycles

LAVATORY CC17 SIDE EMERGENCY LIGHT FOUND INOPERATIVE. EMERGENCY LIGHT REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-12.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

L5 DOOR FLOOR EXIT SIGN, OVER DOOR EXIT SIGN, CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK RESEATED AND RECHARGED, OPS TESTED NORMAL IAW AMM 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

MAIN DECK SEAT 54HJK EMERGENCY LIGHT FOUND INOPERATIVE. BULB REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-12.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

SEAT 17HJR - 21HJR EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK FUSE REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

UPPER DECK STAIRWAY CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BULB REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-07.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

SEAT 14HK - 16HK, SEAT EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK FUSE REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-00.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

L1 DOOR MOUNTED EMERGENCY LIGHT FOUND INOPERATIVE.BULB REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-06.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 79,401 hrs · 15,100 cycles

SEAT 45HJK - 60HJK EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK FUSE REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-00.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

UPPER DECK EMERGENCY DOOR AFT EXIT SIGN FOUND INOPERATIVE. BATTERY PACK FUSE REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

R5 DOOR FLOOR EXIT SIGN, OVER DOOR EXIT SIGN, CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK RESEATED AND RECHARGED, OPS TESTED NORMAL IAW AMM 33-51-00.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 79,401 hrs · 15,100 cycles

UPPER DECK 11ABC - STAIRWAY FLOOR EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK FUSE REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

R2 DR FLOOR EXIT SIGN, OVER DOOR EXIT SIGN, CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK RESEATED AND RECHARGED, OPS TESTED NORMAL IAW AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

R3 DR FLOOR EXIT SIGN, OVER DOOR EXIT SIGN, CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK RESEATED AND RECHARGED, OPS TESTED NORMAL IAW AMM 33-51-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

R1 DOOR FLOOR EXIT SIGN, OVER DOOR EXIT SIGN, CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK RESEATED AND RECHARGED, OPS TESTED NORMAL IAW AMM 33-51-04.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

20HJK CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BULB REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-07.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 79,401 hrs · 15,100 cycles

DOOR 5, STORAGE 5 CEILING EMERGENCY LIGHT FOUND INOPERATIVE. BULB REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-07.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 79,401 hrs · 15,100 cycles

SEAT 47ABC - 60ABC EMERGENCY LIGHT FOUND INOPERATIVE. BATTERY PACK FUSE REPLACED AND OPS TESTED NORMAL IAW AMM 33-51-00.

Part: SKIN — DAMAGED (BS 2285) · airframe 76,225 hrs · 14,507 cycles

WHILE DOING INSPECTIONS IAW SB 747-53A2500/ AD 2006-05-02, FOUND CRACK ON SKIN (PN 65B7004-2) AND BEAR STRAP (PN: 65B38836-4) OF THE R5 MED CUTOUT AFT UPPER CORNER. THE CRACK LENGH IS APPROX 1.35". REFER TO FIG 1 FOR DETAILS OF THE FINDING. (THE CRACK WAS REMOVED BY TRIMMING OUT THE DAMAGES AREA OF THE SKIN AND BEAR STRAP AND HFEC INSP WAS ACCOMPLISHED TO ENSURE CRACK FREE CONDITION. REFER FIG 1 FOR THE REPAIR SCHEME.)

Part: SKIN — NONE · airframe 76,225 hrs · 14,507 cycles

THE PURPOSE OF THIS EO IS TO DOCUMENT SEVEN "DEVIATIONS" WHICH OCCURRED DURING THE MODIFICATION OF RT NOSE WHEEL AFT CORNER IAW THE REQUIREMENTS OF SB 747-53A2305 REV 2 "FUSELAGE - SKIN - NOSE WHEEL WELL AFT CORNER SKIN PANEL INSP AND MODIFICATION". SB 747-53A2305, REV 2 REQUIRES THAT OPERATORS PERFORM A DETAILED INSP FOR CRACKS AT BS 400 NEAR S-44R OF THE SKIN PANEL AND SKIN SPLICE PLATE IN THE AFT CORNERS OF THE NOSE WHEEL WELL BECAUSE OF REPORTS OF CRACKS IN THE AREA. THE PURPOSE OF THE INSP IS TO ENSURE THAT NO UNREPAIRED CRACKS EXIST IN THE AFT CORNER OF THE NOSE WHEEL WELL IN THE SKIN PANEL AND/OR THE SKIN SPLICE PLATE. (JAL COMPLETED THE REPAIR WITHOUT DEVIATIONS AND MFG APPROVED THE REPAIR AND PROVIDED AN AMOC FORM FAA 8100-9 FOR AD 2006-05-09, AD 2006-22-09, AND AD 2004-07-22 REV 1 WITH INITIAL INSP AND REPEAT INSPECTION REQUIREMENTS (SEE FIG 2).)

Part: SKIN — NONE · airframe 76,225 hrs · 14,507 cycles

THIS EO DOCUMENTS 4 "DEVIATIONS" WHICH OCCURRED DURING MODIFICATION OF LT NOSE WHEEL AFT CORNER IAW REQUIREMENTS OF SB 747-53A2305, REV 2 "FUSELAGE - SKIN - NOSE WHEEL WELL AFT CORNER SKIN PANEL INSPECTION AND MODIFICATION. SB 747-53A2305 REV 2 REQUIRES OPERATORS PERFORM A DETAILED INSPECTION FOR CRACKS AT BS 400 NEAR S-44L OF THE SKIN PANEL AND SKIN SPLICE PLATE IN AFT CORNERS OF THE NOSE WHEEL WELL BECAUSE OF REPORTS OF CRACKS IN THE AREA. (RT647 IS A GROUP 8 ACFT IAW SB 747-53A2305, REV 2 THEREFORE JAL PERFORMED THE REQUIRED DETAIL INSPECTION IAW FIG 5 OF THE SB. THERE WERE NO CRACKS DETECTED BY THE DETAIL INSPECTION AND IAW THE SB, JAL HAD THE OPTION OF CONTINUING OPERATIONS WITH REPEAT INSPECTION OR DOING THE ALTERNATE MODIFICATION AND POST-MODIFICATION INSPECTIONS GIVEN IN THE SB. JAL CHOSE TO DO THE ALTERNATE MODIFICATION DOUBLERS INSTALLATION TO MAKE SURE NO UNREPAIRED CRACKS OCCUR IN THE AFT CORNER OF THE NOSE WHEEL WELL.)