N742CK

Part: BATTERY PACK — WEAK (ZONE 200) · airframe 125,601 hrs · 25,802 cycles

CENTER EMERGENCY LIGHTS ON UPPER DECK DO NOT STAY ILLUMINATED.

Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 200) · airframe 124,853 hrs · 25,691 cycles

DOOR UPPER DECK FLIGHT LOCK CAUTION MESSAGE. PERFORMED FLIGHT LOCK ACTUATOR OPS TEST IAW AMM 52-23-00. OPS TESTED GOOD. NO DEFECTS NOTED.

Part: ACTUATOR — UNSERVICEABLE (ZONE 800) · airframe 124,860 hrs · 25,692 cycles

DOOR UPPER DECK FLIGHT LOCK CAUTION MESSAGE. TRANSFERRED TO DMI LIST NUMBER 100272910 IAW KA B747-400 MEL 52-23-3-2. CAT C. DUE 10-5-25. PLACARDS INSTALLED. : REFERENCE DMI 100272910. REMOVED AND REPLACED RIGHT HAND UPPER DECK DOOR LOCK ACTUATOR IAW KA B747-400 AMM 52-23-08. OPERATIONAL CHECK GOOD. THIS CLEARS DMI 100272910. PLACARDS REMOVED.

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 800) · airframe 124,850 hrs · 25,690 cycles

DOOR UPPER DECK FLIGHT LOCK CAUTION MESSAGE. PERFORMED FLIGHT LOCK ACTUATOR OPERATIONAL TEST IAW AMM 52-23-00. OPERATIONAL TEST GOOD. NO DEFECTS NOTED.

Part: STIFFENER — CRACKED (ZONE 600) · airframe 124,753 hrs · 25,673 cycles

AILERON CAVITY I/B STRUCTURE 20 IN. FWD OF HINGE POINT VERTICAL STIFFENER CRACKED AT LOWER EDGE

Part: WARNING MESSAGE — FALSE ACTIVATION (ZONE 800) · airframe 2,525 hrs · 1,090 cycles

DOOR UPPER DECK FLIGHT LOCK MESSAGE. PERFORMED ADJUSTMENT TEST OF UPPER DECK DOOR LOCK IAW AMM 52-23-00. NO DEFECTS NOTED. MESSAGE CLEARED.

Part: FIRE BOTTLE — UNSERVICEABLE (LOWER CARGO) · airframe 124,185 hrs · 25,560 cycles

FIRE CARGO FWD MSG. FAK & ALL SRCS MVD TO U/D XFER TO DMI 100259185 IAW MEL 26-23-1-2 CAT C DUE 08-06-2025 MX PROC C/W PLCDS INSTL. REF DMI 100259185 FOR DEACT FWD LWR LOBE SMOKE DET SYS. SYS DEACT, XFER TO DMI 100259186 IAW MEL 26-16-1-2-2B CAT C, MX PROC C/W. PLCDS INSTL. REF DMI #100259185 FIRE CARGO FWD–MOVED FAK ITEMS ONTO M/D. IAW WO 742049403 & DMI 100259185. RET FAK INTO ORIG POS, CLRS DMI 100259185 PLCDS REM. REF DMI 100259186– FWD LWR LOBE SMOKE DETECT DEACT FOR FIRE BOTTLES. REACT FWD LWR LOBE SMOKE DET SYS IAW AMM 26-16-01. CLRS DMI 100259186, PLCDS REM REF WO 742049404. ACCOMP DROP IN WP 742CK/L-280725. ACCOMP W/P 742CK/L-280725 DURING DROP IN 742049410,411,412,413,414,416. LWR CARGO FIRE BOTTLES REQ RPLCMNT. REM AND REP LWR CARGO FIRE BOTTLE F,E,D,C,B,A IAW AMM 26-23-01.OPS CHKS GOOD IAW AMM 26-23-01.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 124,104 hrs · 25,560 cycles

RIGHT UPPER DECK DOOR BATTERY "OK LIGHT" INOPERATIONAL. COMPLIED WITH PLACARD INSTALLED. RIGHT UPPER DECK DOOR BATTERY LIGHT. OPERATIONS CHECK GOOD IAW B747-400 AMM 51-23-14.

Part: LOCK — FAULTED (ZONE 800) · airframe 124,015 hrs · 25,545 cycles

DOOR UPPER DECK FLIGHT LOCK. TRANSFERRED TO DMI 100259089 IAW MEL 52-23-6-2 CATEGORY C DUE. PLACARDS INSTALLED MAINTENANCE PROCEDURES COMPLIED WITH. 100259106 - PERFORMED ADJUSTMENT TEST OF UPPER DECK FLIGHT LOCK IAW B747-400 AMM 52-23-00. NO DEFECTS NOTED.

Part: LOCK — FAULTED (ZONE 800) · airframe 124,005 hrs · 25,543 cycles

UPPER DECK FLIGHT LOCK. PERFORMED ADJUSTMENT TEST IAW AMM 52-23-00. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 2,235 hrs · 981 cycles

RIGHT HAND UPPER DECK GROUND MODE LIGHT INOPERATIVE. TRANSFERRED TO DMI 100259027 IAW MEL 52-23-4-2 CATEGORY C DUE DATE 07/15/25 PLACARDS INSTALLED (M) PROCEDURES COMPLIED WITH.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 2,235 hrs · 981 cycles

RIGHT UPPER DECK GROUND MODE LIGHT INOPERATIVE. COMPLIED WITH (M) PROCEDURES IAW MEL 52-23-4-2. CYCLED DOOR C/B ON P180 DOOR MODE LIGHT TEST OK IAW AMM 52-23-16. THIS CLEARS DMI 100259027.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 123,777 hrs · 25,500 cycles

L1 DOOR SILL EMERGENCY LIGHTS INOP

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 123,777 hrs · 25,500 cycles

AFT EMERGENCY LIGHT INOP

Part: AILERON — STUCK · airframe 23,436 hrs · 25,447 cycles

FAILS CONTROL CHECK RIGHT OUTBOARD AILERON REMAINS UP. REFERENCE LOGBOOK ENTRY 100231222/100231226 FOR AILERON CONTROL CABLE REPLACEMENT, AILERON ADJUSTMENT AND TEST. PERFORMED AILERON ADJUSTMENT TEST IAW B747-400 AMM 27-11-00 ALL CHECKS GOOD. 100231223- REFERENCE WORK ORDER 100231222: WHILE TROUBLESHOOTING THE RIGHT-HAND OUTBOARD AILERON STUCK IN THE UP POSITION, FOUND RIGHT HAND INBOARD AILERON EXTREMELY SLOW TO TRAVEL TO DOWN POSITION. PERFORMED AILERON TRIM CONTROL ADJUSTMENT AND TEST IAW AMM 27-11-00 ALL CHECKS GOOD. 100231225- PERFORM GENERAL VISUAL INSPECTION OF OUTBOARD RIGHT-HAND AILERON PER COMPANY REQUEST IN REFERENCE TO LOG PAGE 100231222. PERFORMED GENERAL VISUAL INSPECTION OF RIGHT-HAND OUTBOARD AILERON. NO DEFECTS NOTED AT THIS TIME IAW B747-400SF 51-00-00. 100231226- REFERENCE WORK ORDER 100231222: UPON FURTHER INVESTIGATION FOUND CONTROL CABLE AA10 FOR RIGHT HAND OUTBOARD AILERON TO BE BROKEN. REMOVED AND REPLACED RIGHT HAND OUTBOARD AILERON CONTROL CABLE AA10 IAW AMM 27-11-00 RIG AND OPS CHECK GOOD. 100231230- DUE TO THE REMOVAL AND REPLACEMENT OF AILERON CONTROL CABLES AA10/AB10 AIRCRAFT REQUIRES EVALUATION FLIGHT PER GMM 3.4.1. AIRCRAFT RELEASED FOR FUNCTIONAL EVALUATION FLIGHT ONLY.

Part: BATTERY PACK — INOPERATIVE (ZONE 800) · airframe 122,911 hrs · 25,366 cycles

LH EMERGENCY SLIDE BOTTLE BATTERY INOP

Part: SLIDE — BINDING (ZONE 800) · airframe 121,162 hrs · 25,090 cycles

L EMERGENCY DOOR SLIDE HARD TO ARM.

Part: STRUCTURE — GROUND DAMAGE · airframe 120,528 hrs · 24,976 cycles

AIRCRAFT ROLLED FORWARD AFTER ENGINE START STRIKING VAN CAUSING DAMAGE AIRCRAFT RIGHT. AIRCRAFT DAMAGE INSPECTED, REPAIRED, AND LEAK CHECKED IAW E-52 #11533, DWG 52302402-1, 53302408-1 REV OR AND AMM 21-31-00 B747-400 REFERENCE M44 JOB CONTINUATION FORM FOR ADDITIONAL WORK ACCOMPLISHED. AIRCRAFT OK TO RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 120,272 hrs · 24,934 cycles

UPPER DECK LEFT HAND EMERGENCY DOOR LIGHT INOP.

Part: PRESSURE DECK — CRACKED (BS 1240 RBL 89) · airframe 119,349 hrs · 24,765 cycles

CANTED PRESSURE DECK STA 1240 RBL 89 COMPOSITE CLOSE OUT PANEL CRACKED

Part: PRESSURE DECK — CRACKED (BS 1240 RBL 80) · airframe 119,349 hrs · 24,765 cycles

CRACK ON CANTED PRESSURE WEB AT STA 1240 APPROXAMETLY RBL 80

Part: SKIN — CRACKED (ESCAPE HATCH) · airframe 119,349 hrs · 24,765 cycles

FLIGHT COMPARTMENT CREW OVERHEAD HATCH INNER SKIN HAS 1/2 INCH CRACK AT INNER HANDLE OPENING NEAR NUTPLATE LOCATION

Part: PRESSURE DECK — CRACKED (BS 1240 LBL 89) · airframe 119,349 hrs · 24,765 cycles

CANTED PRESSURE DECK STA 1240 LBL 89 COMPOSITE CLOSE OUT PANEL CRACKED

Part: FRAME — CRACKED (BS 1620) · airframe 119,349 hrs · 24,765 cycles

L/H AFT CARGO COMPARTMENT SLOPE SIDEWALL FRAME WEB AT STA 1620 AND APROX LBL47 CRACKED APPROX 7 INCHES FROM TOP CHORD.

Part: RIB — CRACKED (LT WING) · airframe 119,349 hrs · 24,765 cycles

OUTBOARD SEAL RIB ON L/H WING @ APPROXIMATELY WBL 470 FSSI 702 ABOVE #2 PYLON HAS CRACK @ ROD ATTACHMENT POINT.

Part: PRESSURE WEB — CRACKED (BS 1240 LBL80) · airframe 119,349 hrs · 24,765 cycles

CRACK ON CANTED PRESSURE WEB AT STA. 1240 APPROXAMETLY LBL 80

Part: BULKHEAD — CRACKED (BS 400) · airframe 119,349 hrs · 24,765 cycles

FWD E/E COMPARTMENT STA 400 BULKHEAD APPROXIMATELY S-43L HAS MARKED CRACK.

Part: WEB — CRACKED (HORIZONTAL STAB) · airframe 119,349 hrs · 24,765 cycles

L/H HORIZONTAL STAB CLOSEOUT RIB WEB CRACKED AT APPROX STAB STA 593.876

Part: BULKHEAD — CRACKED (BS 400) · airframe 119,349 hrs · 24,765 cycles

POSSIBLE CRACK AT STA 400 BULKHEAD CHORD APPROX WL 124 LBL 23

Part: FRAME — CRACKED (BS 1600 LBL 47) · airframe 119,349 hrs · 24,765 cycles

AFT CARGO PIT, SIDE WALL FRAME WEB CRACKED, 7" FROM TOP CHORD. STA 1600, LBL 47.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 119,349 hrs · 24,765 cycles

CRACK ON L/H HORIZONTAL STAB CLOSURE RIB UPPER CHORD AT APPROX STAB STA 593.876

Part: BULKHEAD WEB — CRACKED (BS 400) · airframe 119,349 hrs · 24,765 cycles

POSSIBLE CRACK AT STA. 400 BULK HEAD WEB LBL 40 AT WL 124

Part: STIFFENER — CRACKED (AFT CARGO DOOR) · airframe 119,349 hrs · 24,765 cycles

AFT CARGO DOOR, FWD DOOR SIDE LIFT LINK MOUNT STIFFNER HAS A CRACK.

Part: SEAT TRACK — CORRODED (BS 660-700 LBL20) · corrosion level 2 · airframe 119,349 hrs · 24,765 cycles

CORRODED UPPER DECK SEAT TRACK BETWEEN STA 660-700 LBL 20

Part: FITTING — CRACKED (LT FLAP GUIDE) · airframe 119,349 hrs · 24,765 cycles

O/B GUIDE ROLLER FITTING CRACKED ON L/H I/B FLAP.

Part: STIFFENER — CRACKED (FWD CARGO DOOR) · airframe 119,349 hrs · 24,765 cycles

FWD CARGO DOOR, FWD DOORSIDE LIFT LINK MOUNT STIFFNER HAS CRACK.

Part: CREASE BEAM — CRACKED (BS 1241-1264 S5R) · airframe 119,349 hrs · 24,765 cycles

FUSELAGE MAIN DECK CREASE BEAM WEB HAS A CRACK BETWEEN STA 1241 TO STA 1264.8 AND APPROX S-5R

Part: CREASE BEAM — CRACKED (BS 1241 S7L) · airframe 119,349 hrs · 24,765 cycles

FUSELAGE MAIN DECK CREASE BEAM WEB HAS A CRACK STA 1241 AND APPROX S-7L

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 118,537 hrs · 24,645 cycles

FIRE MAIN DOOR FORWARD EICAS MESSAGE APPEARED MOMENTARILY IN CRUISE. NO FIRE WAS DETECTED BY FLIGHT CREW. PERFORMED FIRE TEST GROUND TEST IAW B747-400 AMM 26-00-00. TEST PASS, NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (UNKNOWN) · airframe 117,171 hrs · 24,454 cycles

R/H UPPER DECK DOOR EMERGENCY LIGHTS INOP

Part: STIFFENER — DAMAGED · airframe 116,308 hrs · 24,332 cycles

FIXED TRAILING EDGE BEAM WBL 429 STIFFENER DAMAGED

Part: WEB — DAMAGED · airframe 116,308 hrs · 24,332 cycles

FIXED TRAILING EDGE BEAM WBL 429 WEB DAMAGED

Part: BATTERY PACK — INOPERATIVE · airframe 115,336 hrs · 24,193 cycles

LH UD EMERGENCY POWER SYS BATTERY PACK BAD

Part: BATTERY PACK — INOPERATIVE · airframe 115,336 hrs · 24,193 cycles

RH UPPER DECK SLIDE EMERGENCY POWER SYSTEM BATTERY PACK DOESN'T LIGHT BATTERY OK LIGHT

Part: LIGHT — INOPERATIVE · airframe 115,336 hrs · 24,193 cycles

THE L/H UPPER DECK EMERGENCY EXIT DOOR EXIT SIGN IS INOP

Part: LIGHT — INOPERATIVE · airframe 115,336 hrs · 24,193 cycles

THE UPPER DECK AFT AISLE EMERGENCY EXIT SIGN IS INOP

Part: LOCK — OUT OF POSITION (COCKPIT DOOR) · airframe 113,652 hrs · 23,951 cycles

DOOR UPPER DECK FLIGHT LOCK. CLEANED SWITCH CONTACT ON RIGHT UPPER DECK EMERGENCY HATCH AND RESEATED DOOR IN ACCORDANCE WITH BOEING 747 AMM 52-23-00 OPERATIONS CHECK GOOD MESSAGE CLEARED

Part: NONE — UNSERVICEABLE (LEFT) · airframe 113,574 hrs · 23,934 cycles

NO FRM FOUND. EMERGENCY LIGHTS ON ADVISORY FLASHES IN ARM POSITION. REFERENCE LOG PAGE 100010081 EMERGENCY LIGHTS ON ADVISORY FLASHES IN ARM POSITION. PER E50 22-110 AND B747-400 AMM 33-51-04 REMOVED POWER SUPPLY AND APPLIED ELECTRICAL CONNECTORS. REINSTALLED ALL REMOVED SIDEWALL AND CEILING PANELS PER AMM 25-21-02 AND AMM 25-22-03. SEE LOG PAGE 100010082 FOR CARRY OVER ITEM. APPROVED FOR CARRY OVER ITEM 100010082 PER AMM 35-51-04 AND KA E50 22-110. SEE LOG PAGE 100010098 ITEM 100010100. REFERENCE LOG PAGE 100010089: EMERGENCY BATTERY PACK REMOVED AND CAPPED AND STOWED DUE EMERGENCY LIGHTS INTERMITTENTLY COMING ON IN THE ARM POSITION. INSTALLED POWER SUPPLY IAW B747-400 AMM 33-51-04, ALL CHECKS GOOD. REFERENCE WORK ORDER #742026224 FOR ORIGINAL SIGNATURES AND WORK PERFORMED. REFERENCE CARRY OVER ITEM 100010082: EMERGENCY LIGHTING/FERRY FLIGHT. REFERENCE WORK ORDER #742026224 FOR INSTALLATION OF SERVICEABLE POWER SUPPLY AND OPERATIONS CHECK. THIS CLEARS CARRY OVER ITEM 100010082.

Part: NONE — UNSERVICEABLE (M7050) · airframe 113,543 hrs · 23,927 cycles

LEFT AFT UPPER DECK EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED M7050 BATTERY ASSEMBLY IAW B747-400 AMM 33-51-04. OPERATIONS CHECK GOOD.

Part: NONE — UNSERVICEABLE (R/H AFT) · airframe 113,543 hrs · 23,927 cycles

EMERGENCY LIGHTS DON'T AGREE WITH COMMANDED SWITCH POSITION. REMOVED AND REPLACED UPPER DECK RIGHT BACK EMERGENCY BATTERY SUPPLY ASSEMBLY IAW B747-400 AMM 33-51-04. ALL CHECKS GOOD.

Part: LIGHT — INOPERATIVE · airframe 112,670 hrs · 23,783 cycles

MULTIPLE UPPER DECK EMERGENCY LIGHTS INOP.

Part: RIB — CRACKED · airframe 111,822 hrs · 23,662 cycles

L/H WING L/E RIB AT STATION 1048 HAS CRACK AT FASTENER HOLE ON FWD LWR SIDE

Part: LIGHT — INOPERATIVE · airframe 111,822 hrs · 23,662 cycles

L/H UPPER DECK DOOR SQUIB TEST LIGHT INOP.

Part: RIB — CRACKED · airframe 111,822 hrs · 23,662 cycles

L/H WING L/E RIB AT STATION 974 HAS CRACK AT FASTENER HOLE ON FWD LWR SIDE

Part: LIGHT — INOPERATIVE · airframe 111,822 hrs · 23,662 cycles

L5604 EMERGENCY LIGHT STA 470 WON`T TURN ON

Part: STRINGER — CRACKED · airframe 111,822 hrs · 23,662 cycles

FOUND CRACK INDICTION WITH HFEC OPEN HOLE INSPECTION ON R/H UPPER HOLE OF STRINGER 11 STATION 2598.

Part: NONE — NONE · airframe 111,822 hrs · 23,662 cycles

SUPPLEMENTAL INFORMATION: IN SECTION 3.(A) TOTAL CYCLES SHOULD BE 23662 NOT 23622

Part: LIGHT — INOPERATIVE · airframe 111,822 hrs · 23,662 cycles

"BATTERY OK" LIGHT SWITCH ON THE DOOR ANNUNCIATOR MODULE ABOVE RIGHT UPPER DECK EMERGENCY DOOR INOP.

Part: NONE — NONE · airframe 111,822 hrs · 23,662 cycles

SUPPLEMENTAL INFORMATION: IN SECTION 3.(A) TOTAL CYCLES SHOULD BE 23662 NOT 23622

Part: LIGHT — INOPERATIVE (UPPER DECK) · airframe 109,668 hrs · 23,294 cycles

RH UPPER DECK DOOR EMERGENCY LIGHT INOP

Part: SENSOR — FAILED (LOW FLOW) · airframe 105,512 hrs · 22,596 cycles

EQUIPMENT COOLING. REMOVED AND REPLACED FLIGHT DECK. LOW FLOW DETECTOR IAW B747-400 AMM CHAPTER 21-58-02. PERFORMED OPS CHECK IAW 21-58-00. OPS CHECK GOOD. PERFORMED EQUIPMENT COOLING TASK IAW CHAPTER 21-58-00-705-062. OPS CHECK GOOD. AIRCRAFT OK FOR CONTINUED SERVICE.

Part: FUSE PIN — CRACKED (LT MLG) · airframe 104,850 hrs · 22,463 cycles

LEFT WING, WING LANDING GEAR SUPPORT BEAM FUSE PIN HAS CRACK INDICATIONS. CONFIRMED BY HFEC INSPECTION.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 104,850 hrs · 22,463 cycles

CORROSION ON POTABLE WATER OVER FLOW VALVE DOUBLER.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 104,850 hrs · 22,463 cycles

UPPER DECK LT DOOR EMERGENCY BATTERY PACK OK, LIGHT INOPERATIVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 104,850 hrs · 22,463 cycles

RIGHT UPPER DECK DOOR EMERGENCY BATTERY OK, LIGHT INOPERATIVE.

Part: SUPPORT FITTING — CORRODED (RT WING MLG) · corrosion level 2 · airframe 104,850 hrs · 22,463 cycles

RIGHT WING LANDING GEAR SUPPORT BEAM END FITTING HAS CRACK/ CORROSION INDICATION ON AFT SIDE OF FITTING O/B END

Part: SUPPORT FITTING — CRACKED (LT WING MLG) · airframe 104,850 hrs · 22,463 cycles

L/H WING LANDING GEAR SUPPORT BEAM END FITTING HAS 2 INCH CRACK INDICATION AT APPROX 2 O'CLOCK POS. OF FWD HALF OF FITTING

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 104,850 hrs · 22,463 cycles

CORROSION ON POTABLE WATER OVERFLOW VALVE DOUBLER

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 104,850 hrs · 22,436 cycles

EVIDENCE OF CRACK ON L1 DOOR UPPER SILL CENTER SECTION

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 104,850 hrs · 22,436 cycles

AFT PIT DOOR BOTTOM ANGLE IS CORRODED IN MULTIPLE SPOTS

Part: SKIN — CRACKED (FUSELAGE) · airframe 104,850 hrs · 22,463 cycles

EVIDENCE OF CRACK AT FASTENER LOCATION AT L/H NWW CUTOUT AFT CORNER

Part: THRUST BEARING — CORRODED (NR 5 SLAT) · corrosion level 2 · airframe 104,228 hrs · 22,335 cycles

#5 FLAP THRUST BEARING BORE CORRODED

Part: ESCAPE HATCH — DEFECTIVE (COCKPIT) · airframe 102,240 hrs · 21,950 cycles

DURING HANDS ON EMERGENCY EQUIPMENT TRAINING, DISCOVERED THAT COCKPIT ESCAPE HATCH WILL NOT OPEN. REMOVED AND REPLACED CREW COMPARTMENT OVERHEAD HATCH IAW B747-400 M/M 52-21-01. CLEARANCES AND RIG HAVE NOT BEEN DISTURBED. OPS AND CHECKS PASS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,140 hrs · 21,439 cycles

UPPER DECK AND STAIRWELL EMERGENCY LIGHTS AT STA 350, 490, 500, AND 540 INOP.

Part: BULKHEAD WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,140 hrs · 21,439 cycles

LEFT WHEEL BS 1241.01, LEFT HAND JETTISON FUEL PUMP HAS CORROSION ON WEB AT BONDING WIRE ATTACH POINT.

Part: STRAP — CRACKED (BS 2231) · airframe 98,200 hrs · 21,298 cycles

CRACK NOTED AT BS 2231 FRAME STRAP AT THE TOP AFT FASTENER HOLE BELOW STRINGER 25R. CRACK IS FROM THE HOLE TO THE AFT EDGE OF THE STRAP.

Part: STRINGER SPLICE — DENTED (FUSELAGE) · airframe 94,035 hrs · 20,581 cycles

E&E BAY BILGE AREA, BS 406.0, STRINGER 42R HAS DENT IN STRINGER SPLICE ON FREE FLANGE AND WEB AREA.

Part: SLIDE — DEPLOYED (CABIN) · airframe 93,537 hrs · 20,492 cycles

UPPER DECK, RT SIDE ESCAPE SLIDE DEPLOYED. REMOVED DEPLOYED SLIDE IAW MM 25-68-00, PG 201; SECURED SLIDE IN AFT BULK. INSTALLED RT UPPER DECK SLIDE ASSEMBLY IAW 25-68-01 UP T-STEP 13. SAFETY PINS WILL REMAIN INSTALLED IN BOTH RESERVOIRS. INSTALLED FORWARD STORED GAS RESERVOIR IAW AMM 25-68-02. INSTALLED AFT STORED GAS RESERVOIR IAW AMM 25-68-02. REMOVED AND REPLACED RT UPPER DECK EMERGENCY POWER RESERVOIR. ALL CHECKS GOOD IAW AMM 52-23-13.

Part: DOOR FRAME — CRACKED (BS 1265) · airframe 91,457 hrs · 20,182 cycles

L3 DOOR CUTOUT, INSIDE FWD UPPER EDGE AT BS 1265 BETWEEN STR 16 AND STR 17, CRACKED.

Part: BEAR STRAP — CRACKED (PAX DOOR) · airframe 91,457 hrs · 20,182 cycles

LEFT MED NR 5 UPPER AFT CORNER LOWER HOLE HAS A CRACK INDICATION.

Part: BEAR STRAP — CRACKED (PAX DOOR) · airframe 91,457 hrs · 20,182 cycles

RIGHT MED NR 5 UPPER AFT CORNER LOWER HOLE HAS A CRACK INDICATION.

Part: FRAME — CRACKED (BS 1620) · airframe 91,457 hrs · 20,182 cycles

AFT CARGO BAY BS 1620, FRAME IS CRACKED BETWEEN BS 39 AND 40 RT.

Part: SEAL — LEAKING (IDG) · airframe 90,348 hrs · 20,010 cycles

PRECAUTIONARY SHUTDOWN NR 4 ENGINE AT 0308Z, FL300 DUE TO LOSS OF OIL QTY, ENGINE WAS STABLE WITH 3 QUARTS OIL AT SHUTDOWN WITH NO OTHER EXCEEDANCES. WINDMILLED 189 MINUTES AT 12 PSI, WINDMILLED 9 MINUTES BELOW 10 PSI. ENGINE 4 WAS SHUTDOWN IAW QRH. PERFORMED ENGINE POST WINDMILLING INSPECTION IAW MM 72-00-00. CLEANED OIL FROM ENGINE. PERFORMED EXAMINATION FOR OIL LEAKAGE IAW MM 79-00-00. FOUND EXCESS OIL ACCUMULATING AROUND AND ON IDG QAD RING. SUSPECT BAD IDG SHAFT SEAL. R & R IDG SHAFT SEAL IAW AMM 24-11-01. OPS AND LEAK CHECK IS GOOD.

Part: FIRE WARNING — FALSE ACTIVATION (AFT CARGO) · airframe 89,610 hrs · 19,897 cycles

ON FINAL, INTERMITTENT AFT CARGO FIRE WARNING, PERFORMED TROUBLESHOOTING IAW FIM 26-16, TASK 894. REMOVED, INSPECTED AND CLEANED AFOLTS CARDS YLPA033 AND YLPA034 AND PERFORMED OPS CHECK. ALL CHECKED GOOD, IAW AMM 26-10-01 AND 26-16-01.

Part: WARNING MESSAGE — ILLUMINATED (CARGO BAY) · airframe 89,498 hrs · 19,881 cycles

CREW RECEIVED FIRE CARGO AFT DETECTION MESSAGE ABOUT 1500 TO 1000. R & R AFT CARGO AFT BOTTLE IAW AMM 26-23-01.

Part: DOOR — UNKNOWN · airframe 88,566 hrs · 19,725 cycles

RIGHT UPPER DECK DOOR WILL NOT ARM. ACCOMPLISHED WITH TASK 52-11-B07, P203. REACTIVATION RT UPPER DECK FLOOR MOUNTED ESCAPE SLIDE IAW MM 25-68-01, P 410. OPS CHECKS PASS IAW MM 25-68-00. ACCOMPLISHED WITH INSPECTION AND CHECKS AT RT UPPER EMERGENCY DOOR IAW MM 52-23-00, P 601. NO DEFECTS NOTED. ACCOMPLISHED WITH CHECKS AT RT UPPER EMERGENCY DOOR TEST PASS IAW MM 52-23-00, P501.

Part: SLIDE — UNWANTED DEPLOY · airframe 87,468 hrs · 19,528 cycles

RIGHT UPPER DECK SLIDE BLOWN. R & R RT UPPER DECK DOOR SLIDE IAW MM 25-68-01. OPS AND CHECKED PASSED IAW MM 25-68-02.

Part: SEAT TRACK — CRACKED (BS 570) · airframe 86,920 hrs · 19,442 cycles

BS 570, RBL 45 END OF SEAT TRACK CRACKED AT ATTACH FLANGE.

Part: ACTUATOR — INOPERATIVE (FLIGHT LOCK) · airframe 85,713 hrs · 19,267 cycles

UPPER DECK DOOR FLIGHT LOCK DAMAGED. REMOVED AND REPLACED FLIGHT LOCK ACTUATOR IAW MM 52-23-08. OPS CHECKED GOOD.

Part: FLOORBEAM — CRACKED (BS 440) · airframe 83,998 hrs · 18,994 cycles

UPPER DECK FLOORBEAM UPPER TEE AT BS 440 HAS A CRACK INDICATION IN THE FLOOR PANEL ATT. FASTENER HOLE AT RBL 50 ON THE AFT SIDE.

Part: WEB — CRACKED (CARGO BAY) · airframe 83,998 hrs · 18,994 cycles

AFT CARGO BS 1660-1680 TORQUE BOX WEB CRACKED.

Part: FLOORBEAM — CRACKED (BS 340) · airframe 83,998 hrs · 18,994 cycles

BS 340, RBL 68 UPPER DECK FLOORBEAM HAS CRACK IN FASTENER HOLE COMMON TO FLOORBEAM UPPER TEE AND FRAME INNER CHORD.

Part: FRAME — CRACKED (BS 800) · airframe 83,998 hrs · 18,994 cycles

BS 800 FRAME AFT INNER CHORD HAS CRACK INDICATION S17R UPPER AFT FASTENER HOLE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 73,236 hrs · 17,225 cycles

DURING UNLOADING OF AIRCRAFT FUSELAGE RECEIVED DAMAGE TO FUSELAGE AT STATION 2020 TO 2060.

Part: SIGN — BROKEN (CABIN) · airframe 71,303 hrs · 16,907 cycles

UPPER DECK EMERGENCY EXIT SIGN AT STA 600 MID CEILING HAS A BROKEN STUD.