N453PA

Part: ELT — EXPIRED (ZONE 200) · airframe 94,737 hrs · 16,428 cycles

FWD M/D FIXED ELT BATTERY NEAR DUE DATE (03JUN25).(<P>1. REPLACED ELT TRANSMITTER IAW SWPM 20-60-06. 2. STEP A &AMP; B PERFORMED ELT INSTALLATION TEST IAW T/C NO: 23-024-00-03. THE RESULT WAS SATISFACTORY.</P>)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 94,737 hrs · 16,428 cycles

CORROSION - FOUND M/D FLOOR BEAMS TOP SURFACE CORROSION STA 1500 BETWEEN LBL 55 TO LBL 75.92.(<P>1. REMOVE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 103. 2. REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REV 103, W/S NO: 50169 AND EI NO: T2025A53M-489 REV 2. 3. INSTALL FASTENERS IAW SRM 51-40-02-0G-0 REV 103 AND DWG NO: 65B38075 SH 11 REV -. 4. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: BRACKET — CORRODED (ZONE 100) · corrosion level 2 · airframe 94,737 hrs · 16,428 cycles

CORROSION - BRACKET LOWER FUSELAGE WING-TO-BODY SUPPORT BRACKET STA 920 BL 0.(<P>1. REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 103. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV 103 AND DWG NO: 14240130 SHEET 1 REV A. 3. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 94,737 hrs · 16,428 cycles

CRACK - FOUND M/D FLOOR STRUCTURE TRACK SUBSTITUTE CRACK BETWEEN STA 980 TO STA 1000, LBL 75.92.(<P>1. ACCOMPLISHED W/S NO. 50160 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 94,737 hrs · 16,428 cycles

CORROSION - MFOUND M/D FLOOR BEAM CORROSION AT STA 2240 RBL 57 TO RBL 85.(<P>1. REMOVE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 103. 2. REPAIR DAMAGE AREA IAW SRM 53-00-51-2R-3 REV 103 W/S 50176 AND EI NO: T2025A53M-546 REV 1. 3. INSTALL FASTNERS IAW SRM 57-40-02-0G-0 REV 103 AND DWG NO: 65B38112 SH 13 REV - AND SH 14 REV -. 4. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 94,737 hrs · 16,428 cycles

CRACK - FOUND M/D SUBSTITUTE TRACK CRACK, BETWEEN STA 1480 TO STA 1500, RBL 75.(<P>1. ACCOMPLISHED W/S NO. 50172 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 94,737 hrs · 16,428 cycles

CRACK - FOUND M/D CGO COMPT SUB SEAT TRACK CRACK BETWEEN STA 660 TO STA 720, LBL 75.92, TTL 3 EA.(<P>1. ACCOMPLISHED W/S NO. 50182 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 94,737 hrs · 16,428 cycles

CRACK - FOUND M/D SUBSTITUTE TRACK CRACK, BETWEEN STA 1480 TO STA 1500, LBL 75.92.(<P>1. REMOVE AFFECTED FASTNERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 103. 2. REFER DAMAGE AREA IAW SRM 53-00-52-2R-13 REV 103 WORKSHEET NO: 50173. 3. INSTALL FASTENERS IAW SRM 51-40-02-0G-0 REV 103 AND DWG NO: 65B38251 SH 75 REV -, 144U0802, SH 3 REV: B. 4. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 94,737 hrs · 16,428 cycles

CRACK - FOUND M/D SUBSTITUTE TRACK CRACK, BETWEEN STA 1730, RBL 75.92.(<P>1. ACCOMPLISHED W/S NO: 50170 (SRM 53-00-52-2R-13 REV 103). 2. JOB COMPLETED AND CONDITION CHECK NORMAL.&NBSP;</P>)

Part: SPLICE ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 94,737 hrs · 16,428 cycles

CORROSION - FOUND SPLICE ANGLE CORROSION AT M/D COMPARTMENT BETWEEN STA 2280 TO STA 2300, RBL 68.(<P>1. REMOVE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 103. 2. INSTALLED NEW PART IAW SRM 51-40-02-0G-0 REV 103 AND DWG NO: 65B38694 SHEET 3 REV C. 3. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)

Part: ENGINE — VIBRATION (NR 1) · airframe 94,648 hrs · 16,412 cycles

ENG 1 VIB 4.0, N1 FAN, STEADY INCREASE THRU UPPER 20'S FLIGHT LEVEL.(<P>RAN ENG 1 PER 71-00-00-705-057-J00. NOTED 3.1 VIBRATION PEAK PER MCC ENGINEERING. OPS CHECK NORMAL.</P>)

Part: LINE — BROKEN (WATER SEPARATOR) · airframe 92,166 hrs · 15,926 cycles

ADVISORY MSG "SMOKE CREW REST " AROUND 800 TO 1000 FEET AFTER T.O., FOLLOWED BY FUMES ON THE FLIGHT DECK.(<P>R/R CREW REST AREA TRIM AIR MODULATING VLV, REAPIRED BROKEN WATER SEPERATOR LINE, AND REPLACED COALLESOR BAGS PER AMM 21-61-16. OPS CHK GOOD.</P>)

Part: UNKNOWN — FAULTED · airframe 91,370 hrs · 15,768 cycles

DURING TAKEOFF NOTICED UNCOMMANDED ROLLING, ALSO ON LANDING AIRCRAFT ROLLED UNCOMMANDED TO LEFT.(<P>ABNORMALITY PRESSURIZED HYD, &AMP; TRIM RUDDER TO NEUTRAL, RUDDER &AMP; RUDDER TRIM CONTROL SYS OPS CHECK NORMAL PER AMM 27-21-00 WITH FULL FLAP FULL UP, SPOILER OPS &AMP; IND CHECK NORMAL PER AMM 27-61-00. CHECKED ALL SPOILER DIFFERENTIAL SHEAR RIVETS AND MECHANISM, NO FAULT FOUND PER AMM 27-61-03. DID PHYSICAL DOUBLE CHECK OF SYS LOG ITEM, NO ABNORMALITY WAS FOUND. PERFORMED SPOILER ACTUATOR FUNCTION TEST PER AMM 27-61-00, TEST PASSED, BUT RH SPOILER MOVED FASTER THAN LH DURING DEPLOY. PERFORMED ADJUSTMENT OF SPOILER CONTROL SYS PER AMM 27-61-00. ALL RIGGING CHECK SATISFIED. T/E FLAPS EXTEND 20 DETENT, SPOILER OPS CHECK NORMAL PER AMM 27-61-00. AILERON OPS CHECK NORMAL PER AMM 27-11-00.</P>)

Part: WINGLET — NOT REPORTED (LEFT) · airframe 91,178 hrs · 15,729 cycles

LEFT WINGLET SCRAPED.(<P>TRANSFERED TO DMI 203268 IAW CDL 57-28-01 DUE DATE 18JUN24. PLACARD INSTALLED.&NBSP;</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LHW I/B FORE FLAP UPPER SURFACE 226" TO I/B EDGE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LHW O/B FORE FLAP O/B L/E FAIRING SKIN FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

COCKPIT - RH RUDDER PEDAL CAVITIES, THE I/B SIDE VERTICAL METAL PANEL CORNER FOUND CRACKED.(<P>COCKPIT - RH RUDDER PEDAL CAVITIES, RH PILOT FWD PANEL SUPPORT WEB P/N: 233U2320-212 CRACK AREA REPAIRED IAW RI-53-16279 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

FWD CARGO AFT ROW BALLMAT MID PANEL RH AFT CORNER CRK(<P>FWD CARGO COMPT AFT CTR BALLMAT PANEL P/N: 192511-3 CRACK AREA REPAIRED IAW RI-53-20-16283 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

1EA SURFACE CRACK FOUND ON LH STA 2231 STR 21L TO STR 22L REVEAL CRACK APPROX 2.375" IN LENGTH.(<P>STA 2231 STR 21L TO 22L, #5 DOOR REVEAL DOUBLER CRACK AREA REPAIRED IAW SRM 53-60-15-2R-3 REPAIR 3 FIG 203. NO FURTHER DEFECTS NOTED</P>)

Part: SHEAR TIE — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

STA 1000 FRONT SPAR SHEAR TIE CRACK FOUND RBL 33.99(<P>STA 1000 RBL 33.99 FRONT SPAR SHEAR TIE REPLACED AND INSTALLED IAW EO 4453C024 APRT 8 AND RI-53-43-16281 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

RHW O/B FORE FLAP L/E FAIRING SKIN 127" TO I/B FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LH STA 720 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(<P>STA 720 LH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LH WLG I/B W/W DOOR AFT CLOSING RIB AND SKIN CHAFING(<P>LH WLG I/B W/W DOOR AFT CLOSING RIB AND SKIN CHAFING AREA REPAIRED IAW RI 52-82-16282 REV A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LHW T/E I/B FORE FLAP MOST O/B UPPER PANEL FOUND TWO DENTS(<P>PERFORMED REPAIR AT DENTS AREA PER SRM 51-70-10 REPAIR2 FIG203. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

RH STA 760 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(<P>STA 760 RH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LHW T/E I/B AFT FLAP UPPER O/B PANEL FOUND CHAFING(<P>PERFORMED REPAIR AT CHAFING AREA IAW SRM 51-70-10 REPAIR 2 FIG 203. NO FURTHER DEFECTS NOTED</P>)

Part: BATTERY PACK — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

MAIN DECK EMERGENCY LT FND INOP DURING OPS CHK(<P>EMERGENCY LT BATTERY PACK M5170 REPLACED AS PER AMM 33-51-04. OPS CHECK GOOD</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

FX STA 400 LH NOSE WW AFT CORNER SKIN CRACK(<P>FX STA 400 LH FUS SKIN - NWW AFT CORNER SKIN PANEL MOD ACCOMPLISHED IAW EO 4453A516 PART 3 AND RI-53-18-16306 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: LONGERON — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

STA 1480 RH LONGERON EXTENSION FTG FOUND CRACKED(<P>STA 1480 RH LONGERON EXTENSION FTG P/N: 65B15034U24 REPLACED AND INSTALLED IAW EO 4453A818 PART 4. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

RHW T/E O/B AFT FLAP O/B UPPER PANEL FOUND CHAFING(<P>PERFORMED REPAIR AT CHAFING AREA AS PER RI-57-50-16296 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LH BS 740 TENSION TIE FWD CHANNEL 2EA CRACK WERE FOUND ON THE FASTENER HOLE AT 12 O'CLOCK AND 6 O'CLOCK POSITION.(<P>STA 740 LH TENSION TIE CHANNEL REPAIRED IAW SRM 53-20-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 88,746 hrs · 15,255 cycles

M/D SCD AFT DR SILL O/B ASSY UPPER SKIN LWR SIDE FOUND CORROSION CRACK.(<P>M/D SCD AFT DOOR SILL O/B SILL ASSY CHANNEL CORROSION CRACK AREA REPAIRED IAW RI-25-50-16314 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

DAMAGE LOG D-4-15 - DENT BOTTOM OF BULK CARGO FRAME, STA 1992 WL175, L=3/4" X W=3/4" X D=1/32", PER SRM 53-00-01-1A-1 TABLE 1 DETAIL 3 ADL LIMIT.(<P>FX - STA 1992 STR 42R TO STR 43R SKIN DAMAGED AREA REPAIRED IAW RI-53-61-16293 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LH STA 760 TENSION TIE FWD CHANNEL 1EA CRACK FOUND.(<P>STA 760 LH TENSION TIE CHANNEL CRACK AREA REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LHW I/B FORE FLAP UPPER SURFACE 59" TO I/B EDGE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LHW I/B FORE FLAP UPPER SURFACE 145" TO I/B EDGE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

COCKPIT - LH RUDDER PEDAL CAVITIES, THE I/B SIDE VERTICAL METAL PANEL CORNER FOUND CRACKED.(<P>COCKPIT - LH RUDDER PEDAL CAVITIES, LH PILOT FWD PANEL SUPPORT WEB P/N: 233U2320-210 CRACK AREA REPAIRED IAW RI-53-16-16279 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LHW I/B FORE FLAP MID L/E FAIRING SKIN FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR 5A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

1EA THOUGHT THICKNESS CRACK FOUND ON LH BS2231 S16 STRAP (COUNT FROM O/B SECOND LAYER) RUNNING FWD AT 4 O/C POSITION (VIEW LOOKING O/B).(<P>M/D - STA 2231 STR 16L FRAME STRAP P/N: 65B01849-25 CRACK AREA REPAIRED IAW RI-53-60-16284 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

LHW I/B AILERON UPPER SURFACE AFT O/B CORNER FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA AS PER SRM 51-70-06 PAR 5G. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

AFT CARGO STA 1700 FLOOR BEAM MIDDLE AREA FOUND CHAFING.(<P>AFT CARGO STA 1700 FLOOR BEAM UPPER CHORD P/N: 65B07373-3 CHAFING AREA REPAIRED IAW RI-53-60-16278 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: SHEAR TIE — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

STA 1000 FRONT SPAR SHEAR TIE CRACK FOUND LBL 75.92(<P>STA 1000 LBL 75.92 FRONT SPAR SHEAR TIE REPLACED AND INSTALLED IAW EO 4453C024 PART 6 AND RI-53-43-16285 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

BODY FAIRING 191KL UPPER SUPPORT AND LOWER FLANGE FOUND CRACK(<P>BODY FAIRING 191KL UPPER SUPPORT AND LOWER FLANGE CRACK AREAS REPAIRED IAW RI-53-40-16280 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

EO 4453A516 PART 4, STA 400 RH WAS A REPAIR PREVIOUSLY INSTALLED IN THE MODIFICATION AREA.(<P>FX STA 400 RH FUS SKIN - NWW AFT CORNER SKIN PANEL MOD ACCOMPLISHED IAW EO 4453A516 PART 4 AND RI-53-18-16306 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: LONGERON — UNKNOWN (UNKNOWN) · airframe 88,746 hrs · 15,255 cycles

STA 1480 LH LONGERON EXTENSION FTG FOUND CRACKED(<P>STA 1480 LH LONGERON EXTENSION FTG P/N: 65B15034U23 REPLACED AND INSTALLED IAW EO 4453A818 PART 3. NO FURTHER DEFECTS NOTED</P>)

Part: NONE — NONE · corrosion level 3 · airframe 85,583 hrs · 14,728 cycles

FOUND PITTING IN STRUCTURE SURROUNDING #6 CARRIAGE SPINDLE BEARING(<P>R/R RH INBD MID FLAP IAW AMM 27-50-00</P>)

Part: NONE — NONE · airframe 83,960 hrs · 14,447 cycles

FUSELAGE SKIN (P/N 65B23673-4) - PUNCTURE DAMAGE AT STA 690, BETWEEN S-34R AND S-35R(<P STYLE="MARGIN: 0IN; MARGIN-BOTTOM: .0001PT;"><SPAN>THE DAMAGED SKIN PORTION WAS TRIMMED OUT, DETAIL VISUAL INSPECTION, SURFACE AND OPEN-HOLE HFEC INSPECTIONS WERE PERFORMED.</SPAN></P> / <P STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>TO CONFIRM NO ADDITIONAL DAMAGE AND CRACK-FREE CONDITION. AND, SERVICE BULLETIN 747-53A2563 INSPECTIONS WERE PERFORMED FOR SCRIBE LINES AT THE REPAIR LOCATION WITH NO FINDINGS. A REPAIR DOUBLER AND FILLER WERE INSTALLED ACROSS THE S-34R LAP SPLICE PER SERVICE REQUEST (SR) ID: 4-5398006572. ALL PROTECTIVE FINISHES WERE RESTORED PER 747 SRM AND SOPM REQUIREMENTS.</SPAN></P>)

Part: CONTROLLER — FAULTED (BLEED VALVE)

DURING CLIMB OUT #1, #2 &AMP; #4 BLEED VALVE OFF LIGHT ILLUMINATED WITH BLEED SWITCHES SELECTED ON, CYCLED VALVES WITH NO RESOLUTION.(<P ><SPAN>REMOVED AND REPLACED #3 BLEED PRV CONTROLLER IAW B747 AMM 36-11-19, REMOVED AND REPLACED #3 PRSOV IAW B747 AMM 36-11-04, REMOVED AND REPLACED #2 PRSOV IAW B747 AMM 36-11-01, FOUND #3 PRVC MUSCLE AIR LINE LEAKING, REPLACED PACKING IAW B747 AMM 36-11-19. OPS CHECK OF #2 AND #3 PRSOV GOOD IAW B747 AMM 36-11-04, OPS CHECK OF #3 PRVC GOOD IAW B747 AMM 36-11-20.</SPAN></P> / <P>&NBSP;</P>)

Part: SEAT TRACK — CORRODED (BS 1750-1800) · airframe 81,183 hrs · 13,915 cycles

M/D STA 1780 - 1800 LBL 99 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1750 - 1800 LBL 99 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-6.</P>)

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 81,183 hrs · 13,915 cycles

RH O/B AFT FLAP L/E FAIRING FOUND PUNCTURE(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.A</P>)

Part: SKIN — CRACKED (MAIN DOOR AREA) · airframe 81,183 hrs · 13,915 cycles

M/D SCD AFT DOOR SILL O/B PANEL UPPER SKIN FOUND CRACK.(<P>M/D SCD AFT DOOR SILL O/B PANEL UPPER SKIN REPAIRED AS PER&NBSP;<SPAN>EO 4425A500, SRM 51-70-13 AND COMPONENT SB AND CMM.</SPAN></P>)

Part: SEAT TRACK — CORRODED (BS 2230-2300) · airframe 81,183 hrs · 13,915 cycles

M/D STA 2260 LH LBL 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 2230 - 2300 LBL 33 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-6.</P>)

Part: SUPPORT — CRACKED (HORIZONTAL STAB) · airframe 81,183 hrs · 13,915 cycles

LH H/STAB TIP FAIRING SUPPORT UPPER CHORD AFT END FOUND CRACK(<P>LH H/STAB TIP FAIRING SUPPORT UPPER CHORD REPAIRED AS PER SRM 55-10-09-2R-13.</P>)

Part: SEAT TRACK — CORRODED (BS 1400-1460) · airframe 81,183 hrs · 13,915 cycles

M/D STA 1400 - 1460 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1400 - 1460 RBL 11 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52-1A1 FIG 101.</P>)

Part: SKIN — DELAMINATED (LT WING AILERON) · airframe 81,183 hrs · 13,915 cycles

LHW I/B AILERON O/B AFT EDGE FOUND DELAMINATION(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-06 PARA 5.G</P>)

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 81,183 hrs · 13,915 cycles

RHW O/B FORE FLAP L/E FAIRING MID AREA FOUND DELAM(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.A</P>)

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 81,183 hrs · 13,915 cycles

LHW I/B FORE FLAP O/B UPPER EDGE FOUND DELAMINATION(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.G</P>)

Part: SEAT TRACK — CORRODED (BS 980) · airframe 81,183 hrs · 13,915 cycles

M/D STA 980 RBL 11 - 33 SEAT TRACK FOUND CORROSION.(<P>M/D STA 980 RBL 11 -&NBSP; 33 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52-1A1 FIG 101.</P>)

Part: SEAT TRACK — CORRODED (BS 1080) · airframe 81,183 hrs · 13,915 cycles

M/D STA 1080 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1080 RBL 11 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52-1A1 FIG 101.</P>)

Part: LINK — DAMAGED (RT WING TE FLAP) · airframe 81,183 hrs · 13,915 cycles

RHW O/B T/E MID FLAP T/E #8 SUPPORT LINK UPR MOUNT BOLT HOLE ELONGATED (COUNT FROM O/B)(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.K</P>)

Part: SEAT TRACK — CORRODED (BS 1020) · airframe 81,183 hrs · 13,915 cycles

M/D STA 1020 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1020 LBL 11 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52-1A1 FIG 101.</P>)

Part: NONE — NONE · airframe 81,183 hrs · 13,915 cycles

NLG L/R FWD CORNER DOUBLER MOD FOUND L/R TOTAL 8EA FASTENER AND 8 WASHER INTERTERING INSTALLATION. NLG L/R FWD CORNER DOUBLER AND 8EA RIVETS AND 8EA WASHER INSTALLED AS PER RI 53-10-14631 REV A.

Part: RETAINER — CRACKED (HORIZONTAL STAB) · airframe 81,183 hrs · 13,915 cycles

LH HORI STAB T/E FAIRING RETAINER FOUND CRACK(<P>REPLACE RETAINER AS PER RI-55-10-14639</P>)

Part: TENSION TIE — CRACKED (BS 720) · airframe 81,183 hrs · 13,915 cycles

M/D STA 720 R/H TENSION TIE CHANNEL FOUND CRACK.(<P>M/D STA 720 RH TENSION TIE CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1</P>)

Part: FRAME — CRACKED (APU BAY) · airframe 81,183 hrs · 13,915 cycles

APU COMPT RH STA 2701 WL 314 FRAME FOUND CRACK.(<P>APU COMPT RH STA 2701 WL 314 FRAME REPAIRED AS PER SRM 53-80-07-2R-1</P>)

Part: DOUBLER — DETACHED (BS 1940) · airframe 81,183 hrs · 13,915 cycles

M/D STA 1940 LH DADO PANEL DOUBLER FOUND DETACH.(<P>M/D STA 1940 L/H DADO PANEL DOUBLER REPLACED AS PER SRM 51-10-02 AND 51-40-02.</P>)

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 81,183 hrs · 13,915 cycles

LH HORI STAB TIP FAIRING INTERIOR RIB FOUND CRACKED (TOTAL 9EA RIB RACK)(<P>LH HORI STAB TIP FAIRING INTERIOR RIB (5 LOCATIONS) RIB WAS REPLACED AND INSTALLED AS PER SRM 51-10-02, SRM 51-40-02 REV 91, 20 FEB 2021 AND (4 LOCATIONS) RIB WAS REPAIRED AS PER SRM 55-10-09-2R-12 REPAIR 12 REV 91, 20 FEB 2021</P>)

Part: SKIN — CRACKED (BS 1840-1920) · airframe 81,183 hrs · 13,915 cycles

M/D STA 1840 - 1920 RBL 77 - 99 CASTER PANEL SKIN FWD CORNER FOUND CRACK.(<P>M/D STA 1840 - 1920 RBL 77 - 99 CASTER PANEL SKIN FWD CORNER REPAIRED AS PER EO 4425A500, SRM 51-70-13 AND COMPONENT SB AND CMM.

Part: SEAT TRACK — CORRODED (BS 980) · airframe 81,183 hrs · 13,915 cycles

M/D STA 980 RBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 980 RBL 11 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52-1A1 FIG 101.</P>)

Part: DOOR FRAME — CRACKED (NLG WW) · airframe 81,183 hrs · 13,915 cycles

RH WLG I/B W/W DOOR AT O/B FWD CORNER FRAME CRACK.(<P>R/H WLG I/B W/W DOOR AT O/B FWD CORNER FRAME REPAIRED AS PER RI-52-80-14638 REV A</P>)

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 81,183 hrs · 13,915 cycles

LHW I/B FORE FLAP UPPER SURFACE O/B AREA FOUND DELAMINATED(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.A</P>)

Part: DOOR FRAME — CRACKED (RT WING MLGWW) · airframe 81,183 hrs · 13,915 cycles

RH WLG I/B W/W DOOR AT O/B FWD CORNER FRAME CRACK.(<P>L/H WLG I/B W/W DOOR AT O/B FWD CORNER FRAME REPAIRED AS PER RI-52-80-14637 REV A</P>)

Part: FLOORBEAM — CORRODED (BS 980) · airframe 81,183 hrs · 13,915 cycles

M/D STA 980 LBL 11 - 33 FLOOR BEAM LOWER FOUND CORROSION.(<P>M/D STA 980 LBL 11 - 33 FLOOR BEAM LOWER CORROSION AREA REWORKED AS PER SRM 53-00-52-1A1 FIG 101.</P>)

Part: SKIN — CRACKED (BS 1780-1840) · airframe 81,183 hrs · 13,915 cycles

M/D STA 1780 - 1840 RBL 55 - 77 CASTER PANEL SKIN FWD CORNER FOUND CRACK. M/D STA 1780 - 1840 RBL 55 - 77 CASTER PNL SKIN FWD CORNER REPAIRED AS PEREO 4425A500, SRM 51-70-13 AND COMPONENT SB AND CMM.

Part: SEAT TRACK — CORRODED (BS 1300) · airframe 81,183 hrs · 13,915 cycles

M/D STA 1300 - 1320 LBL 11 SEAT TRACK FOUND CORROSION.(<P>M/D STA 1300 - 1320 LBL 11 SEAT TRACK CORROSION AREA REWORKED AS PER SRM 53-00-52-1A1 FIG 101.</P>)

Part: SKIN — CRACKED (NLG AREA) · airframe 81,183 hrs · 13,915 cycles

NLG LH FWD CORNER SKIN FOUND 1EA FASTENER HOLE CRACK.(<P>NLG LH FWD CORNER SKIN 1EA FASTENER INSTALLED AS PER RI 53-10-14631 REV A.</P>)

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 81,183 hrs · 13,915 cycles

RHW I/B AFT FLAP LOWER SURFACE T/E FOUND DELAM(<P>PERFORMED PERMANENT HOT BOND REPAIR AS PER SRM 51-70-07 PARA 5.A</P>)

Part: SEAT TRACK — CORRODED (BS 1160) · airframe 81,183 hrs · 13,915 cycles

M/D STA 1160 LH O/B FLOOR SUPPORT FOUND CRACK.(<P>M/D STA&NBSP;1160 LH&NBSP;<SPAN>O/B FLOOR SUPPORT</SPAN><SPAN>&NBSP;</SPAN><SPAN>REPAIRED AS PER SRM 53-20-30-2R-1</SPAN></P>)

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 73,517 hrs · 12,372 cycles

REPAIR- SHARP DENTS WITH CRACK ON RH SIDE SKIN PANEL BETWEEN STA 2690.85 AND 2701.51(<P>1. ACCOMPLISHED REPAIR AREA I.A.W. EI NO. T2019A53M-2495 REV. 1. </P><P>2. JOB COMPLETED AND COND CHK NORMAL.</P>)

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 73,517 hrs · 12,372 cycles

REPAIR- SKIN EDGE BENDING AND DENT ON FWD LOWER CORNERS OF BULK CARGO DOOR OUTER SKIN(<P>1. ACCOMPLISHED BULK CARGO DOOR REPAIR IAW EI NO. T2019A52M-2104 REV. 1 &AMP; SRM 52-00-01 REPAIR 8 REV. 85.</P><P>2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,517 hrs · 12,372 cycles

REPAIR- SKIN MODIFICATION PER SB 747-53A2487.(<P>1. REPAIR DAMAGED AREA IAW EI NO. T2019A53M-1979 REV. 2.&NBSP;2. JOB COMPLETED AND COND CHK NORMAL.</P>)

Part: DOUBLER — CORRODED (RT WING) · corrosion level 2 · airframe 73,517 hrs · 12,372 cycles

REPAIR- CORROSION ON RH WING REAR SPAR FUEL PUMP CUTOUT DOUBLER AT WS 400.(<P>1. RMV CORROSION DOUBLER IAW SRM 51-40-02-06-0 REV. 85</P><P>2. INSTALLED FAB DOUBLER IAW EI NO. T2019A57M-2275 REV.0 &AMP; DWG NO. 11201001 543 REV. F, 5421 REV. J &AMP; 65B11631 542 REV.J.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 73,517 hrs · 12,372 cycles

REPAIR - CORROSION ON THE MAIN DECK SEAT TRACK (P/N: 65B38272-2) AT RBL 11.33, STA 1765.(<P>1. ACCOMPLISHED DAMAGED SEAT TRACK REPAIR IAW EI NO. T2019A53M-2135 REV. 1 AND DWG NO. 65B38253 541 REV. AP; 65B38253 5447 REV. "-"; 65B38253 5448 REV. "-"; 65B38253 5449 REV. "-" AND 65B38253 5456 REV. "A" AND SRM 53-00-52 REPAIR 12 REV. 85.</P><P>2. COND CHECK NORMAL AND JOB COMPLETED.&NBSP;</P>)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 71,973 hrs · 12,097 cycles

ACRID ODOR IN THE COCKPIT. PERFORMED MM 05-51-561, AND FIM 21-00, TASK 810, FLIGHT DECK EQUIPMENT CHECKED, NO SMOKE NOTED.

Part: ACTUATOR — MALFUNCTIONED (TILT) · airframe 67,445 hrs · 11,307 cycles

MLG WOULD NOT RETRACT. REMOVED AND REPLACED RT BODY POSITION TILT ACTUATOR AND FUSE ASSY.

Part: EXTINGUISHER — LEAKING (UPPER DECK) · airframe 66,837 hrs · 11,205 cycles

UPPER DECK WATER FIRE EXTINGUISHER HAS SIGNS OF LEAKING. REMOVED AND REPLACED THE FIRE EXTINGUISHER IAW AMM 26-26-02, CHECKED OK.

Part: SUPPORT — DAMAGED (RT WING) · airframe 661,494 hrs · 11,084 cycles

RT WING T/E 681BB FIXED PANEL AND OTBD PANEL SUPPORT BEAM AT BOLT HOLE FOUND ELONGATED. THE SUPPORT WAS REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: PANEL — DAMAGED (RT WING) · airframe 661,494 hrs · 11,084 cycles

RT WING T/E 681BB FIXED PANEL MD AND OTBD PANEL SUPPORT BEAM AT BOLT HOLE FOUND ELONGATED. REPAIRED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: DOOR SILL — CRACKED (CARGO DOORWAY) · airframe 66,194 hrs · 11,584 cycles

CARGO DOOR SILL PANEL FOUND CRACKED. THE DOOR SILL PANEL WAS REPLACED IAW SRM 51-10-05 AND SRM 51-40-02.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 66,194 hrs · 11,084 cycles

BS 1820, LBL 33 - 55 CASTER PANEL TOP SKIN DAMAGED. THE CASTER PANEL SKIN WAS REPAIRED IAW EO 4425A500, REV 0.

Part: FLOOR PANEL — CRACKED (CAROG BAY) · airframe 66,194 hrs · 11,084 cycles

BS 1820, RBL 33 - 55 CASTER PANEL FOUND CRACKED. THE CASTER PANEL WAS REPAIRED IAW R1-25 -55 11887, REV A.

Part: DOOR SILL — CRACKED (CARGO DOORWAY) · airframe 66,194 hrs · 11,084 cycles

CARGO DOOR FWD STILL PANEL FOUND CRACKED, BS 1786 - 1850, LBL 99 - 128. THE DOOR SILL WAS REPAIRED IAW R1-25-55-11885, REV A.

Part: SUPPORT BRACKET — DAMAGED (LT WING) · airframe 66,194 hrs · 11,084 cycles

LT WING OTBD T/E LOWER FIXED PANEL 581HB INBD SUPPORT BRACKET FOUND WITH A HOLE ELONGATED. THE SUPPORT BRACKET WAS REPLACED IAW SRM 51-10-02, AND SRM 51-40-02.

Part: SKIN — CHAFED (NR 4 NACELLE) · airframe 66,194 hrs · 11,084 cycles

NR 4 ENGINE LT CORE COWL INNER FACE FWD & NR 2 CHANNEL REPAIR DOUBLER FOUND CHAFED. REPAIRED IAW SRM 54-45-022R-1, FIG 201.

Part: CHANNEL — CHAFED (NR 2 NACELLE) · airframe 66,194 hrs · 11,084 cycles

NR 2 ENGINE LEFT CORE COWL INNER NR 2 CHANNEL DOUBLER, UPPER AND LOWER FOUND CHAFED. THE CHANNEL WAS REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: CHANNEL — CHAFED (NR 3 NACELLE) · airframe 66,194 hrs · 11,084 cycles

NR 3 LT CORE COWL INNER FACE FWD NR 2 CHANNEL REPAIR DOUBLER FOUND CHAFED. REPAIRED IAW SRM 54-45-02-2R-1, REPAIR, FIG 201.

Part: FRAME — BROKEN (BS 899) · airframe 66,194 hrs · 11,084 cycles

NR 3 PACK RAM AIR INLET ASSY AFT CUTOUT FRAME FOUND BROKEN. REPLACED AND REPLACED IAW SRM 51-10-02, AND 51-40-02.

Part: SUPPORT BRACKET — DAMAGED (WING) · airframe 66,194 hrs · 11,084 cycles

LOWER OTBD T/E LOWER FIXED PANEL NR 581 HB I/B SUPPORT BRACKET FOUND HOLE ELONGATED. THE SUPPORT BRACKET WAS REPLACED IAW SRM 51-10-02 AND SRM 51-40-02.

Part: CHANNEL — CRACKED (NR 2 NACELLE) · airframe 66,194 hrs · 11,084 cycles

NR 2 ENG LEFT CORE COWL INNER FACE MOST AFT CHANNEL FOUND CRACKED AT MD AREA. REPAIRED IAW EO 1917A135, REV 0.

Part: SKIN — SCRATCHED (BS 1920) · airframe 66,194 hrs · 11,084 cycles

AFT CARGO DOOR AFT CUTOUT SKIN BS 1920, STRINGER 38R FOUND SCRATCHED. AFT CARGO DOOR AFT CUTOUT SKIN PANEL AND LOWER STRAP WERE REPAIRED IAW R1-53-00-11890, REV A.

Part: SKIN — CORRODED (RT WING TE FLAP) · corrosion level 2 · airframe 66,194 hrs · 11,084 cycles

RT WING OTBD MID FLAP UPPER THE FIXED PANEL FOUND CORRODED. REPAIRED IAW R1-57-50-11889, REV A.

Part: SKIN — DAMAGED (BS 1810) · airframe 66,194 hrs · 11,084 cycles

AFT CARGO DOOR FWD CUTOUT SKIN AT BS 1810, STRINGERS 38 - 39R FOUND EXTEDING BLEND OUT BEYOND THE SRM LIMITS. THE SKIN AND LOWER STRAP WERE REPAIRED IAW R1-53-61-11888, REV A.

Part: SKIN — DAMAGED (NR 3 NACELLE) · airframe 66,194 hrs · 11,084 cycles

NR 3 ENGINE RT CORE COWL OUTER FACE AFT UPPER CORNER CHAFED WITH A HOLE AT LOWER OF SPRING SOFT. REPAIRED IAW SRM 54-45-01-2R, REPAIR 7, FIG 202.

Part: DOOR — DAMAGED (CARGO BAY) · airframe 64,979 hrs · 10,862 cycles

MAIN DECK CARGO DOOR DAMAGE DURING GROUND OPERATIONS. REPAIRED IAW PART 1 OF EO 1952A185 REV 0.

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 64,961 hrs · 10,858 cycles

COCKPIT DESCENT DEVICE NR 1 CABLE OVER EXTENDED. REMOVED AND REPLACED COCKPIT DESCENT DEVICE IAW MM 25-61-01.

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 64,961 hrs · 10,858 cycles

COCKPIT DESCENT DEVICE NR 8 OVER EXTENDED. REMOVED AND REPLACED COCKPIT DESCENT DEVICE IAW MM 25-61-01.

Part: SWITCH — FAULTY (STABILIZER TRIM) · airframe 63,389 hrs · 10,583 cycles

EICAS MESSAGE; STABILIZER TRIM UNSCHEDULED. ASSOCIATED AUTOPILOT MESSAGE. QRH FOLLOWED, UNABLE REGAIN STABILIZER TRIM. R & R CAPTAIN AND F/O STABILIZER MANUAL TRIM CONTROL WHEEL SWITCHES. R & R STABILIZER TRIM CONTROL MODULE. OPS LEAK CHECK OK IAW AMM 27-41-04, MANUAL TRIM TEST FOUND STABILIZER TRIM GOES TO 11.6 UNIT THEN CANNOT GO TO NOSE DOWN DIRECTION. MANUAL TRIM CHECK OK. AUTO TRIM, ALTN TRIM TEST SATISFACTORY AMM 27-41-00. AUTOLAND TEST PASSED.

Part: MODULE — MALFUNCTIONED (AUTOPILOT SYS) · airframe 63,389 hrs · 10,583 cycles

STABILIZER TRIM UNSCHEDULED STATUS. SRM R & R, TESTED OK IAW AMM 27-41-01, LP691776M8. STABILIZER COMPARTMENT RELATED PARTS INSPECTED NORMAL. FCC L, C, R AND SRM L AND R RERACKED, STABILIZER TRIM GROUND TEST CUTOUT PASSED IAW AMM 22-11-00.

Part: RVDT — OUT OF RIG (NR 2 ENGINE) · airframe 61,128 hrs · 10,174 cycles

LOW SPEED RTO DUE TO NR 2 ENGINE FAILED TO SPOOL BEYOND 74 PERCENT N1. FOUND RVDT OUT OF RIG. RIGGED RVDT AS REQUIRED IAW AMM 78-34-10. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,345 hrs · 9,829 cycles

UPPER DECK EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK, OPS CHECKED GOOD IAW MM 33-51-00.

Part: INTERCOSTAL — CRACKED (BS 1180) · airframe 58,563 hrs · 9,676 cycles

DURING INSPECTION OF TRIM AIR DIFFUSER DUCT FOUND LT BS 1180 INTERCOSTAL WEB CRACKED, BS 1180 LT OTBD INTERCOSTAL WEB. REPAIRED SRM 53-40-51-2R-8, REPAIR 8 BETWEEN LBL 92 TO LBL 105 AREA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 56,744 hrs · 9,239 cycles

UPPER DECK CREW REST RT M5169 BATTERY PACK FOUND INOPERATIVE. BATTERY PACK M5169, REPLACED AND CHECK NORMAL IAW AMM 33-51-04.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,744 hrs · 9,239 cycles

MAIN DECK L1 DOOR EMERGENCY LIGHT L5735 FOUND INOPERATIVE DURING TESTING, LIGHT BULBS REPLACED AND TESTED FOUND NORMAL.

Part: TORQUE TUBE — SHEARED (TE FLAPS) · airframe 59,807 hrs · 9,944 cycles

FLAP DRIVE EICAS WITH OTBD T/E FLAPS SHOW ASSYMETRY AT 20 DEGREES, FOUND TORQUE TUBE COUPLING ON OTBD SIDE OF NR 2 FLAP TRANSMISSION SHEARED, REPLACED ASSOCIATED TORQUE TUBE AND TRANSMISSION.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 56,065 hrs · 9,080 cycles

FLAPS DRIVE EICAS WITH OTBD T/E FLAPS SHOW ASYMETRY AT 20 DEGREE. OPEN

Part: TRANSFORMER — FAILED (TE FLAPS) · airframe 56,065 hrs · 9,080 cycles

FLAPS DRIVE, R & R 1 OTBD T/E FLAP RVDT IAW AMM 27-58-01, OPS CHECK NORMAL.

Part: WINDOW — ARCED (COCKPIT) · airframe 54,393 hrs · 8,778 cycles

L3 WINDOW APPEARED TO BE ARCING ON LOWER FORWARD EDGE. CIRCUIT BREAKER E28 AND E30 PULLED IAW MAINTENANCE CONTROL. QRH REFERENCED. FOUND NO ARCING EVIDENCE IAW AMM 56-11-02. REPLACED WINDOW 3L ASSEMBLY IAW AMM 56-11-02. WINDOW HEAT AND CONDITION CHECKED SATISFACTORY.

Part: FRAME — CRACKED (L5 DOOR) · airframe 50,576 hrs · 8,183 cycles

CRACK ON L5 FOR FORWARD CENTER FRAME. REPAIR IAW EI NO. T2013A53B-977 REV O.

Part: WINGLET — DAMAGED (RT WING) · airframe 50,576 hrs · 8,183 cycles

LIGHTNING STRIKE ON RIGHT WINGLET T/E CASTING UPPER TIP. REPAIR IAW EI NO. T2013A57B-1047 REV O.

Part: BATTERY — DISCHARGED (CABIN) · airframe 50,576 hrs · 8,183 cycles

FOUND EMERGENCY LIGHT POWER, M5169 &AMP;M5170 BATTERY. REPLACED BATTERIES PER NRC 712.

Part: WINGLET — DAMAGED (LT WING) · airframe 50,576 hrs · 8,183 cycles

LIGHNTING STRIKE ON THE LEFT WINGLET T/E CASTING UPPER TIP. REPAIR IAW EI NO. T2013A57B991 REV O.

Part: FAN — FAILED (EQUIPMENT BAY) · airframe 49,903 hrs · 8,079 cycles

PRIOR TO DEPARTURE FOUND BAD SMELL CAME OUT. TROUBLESHOOTING FOUND EQUIPMENT COOLING SUPPLY FAN HAVING INTERNAL FAILURE AND BAD SMELL COMING FROM FAN. FAN WAS REPLACED PER AMM 21-58-01/401.

Part: FAIRING — DAMAGED (LT MLG DOOR) · airframe 48,465 hrs · 7,831 cycles

LEFT&NBSP; HAND WING LANDING GEAR - SHOCK STRUT INBOARD DOOR FAIRING - TRAILING EDGE DAMAGE. DAMAGE FOUND TO BE BEYOND THE LIMITS OF SRM 52-80-02 FIGURE 101&NBSP; ALLOWABLE DAMAGE 4 AND PER SRM 51-70-02, FIGURE 101 ALLOWABLE DAMAGE GENERAL. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1&NBSP;OF EO 4452A161 FAA 8110-3 DATED 23OCT12.

Part: TRIM PANEL — TORN (MAIN CARGO BAY) · airframe 48,334 hrs · 7,809 cycles

THERE IS A 2.5 INCHES LONG TEAR TO THE MAIN DECK SIDE CARGO DOOR CUTOUT AREA & NBSP;AT BS 1920 SIDEWALL TRIM.

Part: SKIN — DAMAGED (BS 1810) · airframe 47,479 hrs · 7,680 cycles

SKIN DAMAGED AT AFT CARGO DOOR FWD LOWER EDGE BS 1810 BETWEEN S38-40R. DAMAGE AREA REPAIRED AS PER RS-NO R-53-60-37384.453PA.

Part: CHANNEL — CRACKED (BS 760) · airframe 47,479 hrs · 7,680 cycles

BS 760 RT TENSION TIE AREA, FOUND 1 CRACK AT FWD CHANNEL RUNNING 6 O/C APPROX 0.020 INCH, FWD CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201 AND EO NR 4453A745.

Part: CHANNEL — CRACKED (BS 760) · airframe 47,479 hrs · 7,680 cycles

BS 760 RT TENSION TIE AREA FOUND HOLE CRACK AT AFT CHANNEL RUNNING 10 O/C APPROX 0.020 INCH LENGTH. AFT CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201 AND EO NR 4453A746.

Part: OVEN — DISLODGED (GALLEY) · airframe 46,926 hrs · 7,604 cycles

THE UPPER DECK GALLEY OVEN FELL OUT DURING LANDING THEN THERE WAS A BURNING ODOR FOR SEVERAL MINUTES DURING TAXI IN. REMOVED OVEN UNIT AND CHECKED AREA. FOUND ELECTRIC RECEPTACLE DIRTY. CLEANED CONNECTOR PER SWPM 20-10-04. OVEN INSTALLED AND OPS WAS NORMAL PER AMM 25-35-00.

Part: RUB STRIP — DAMAGED (FUSELAGE) · airframe 44,984 hrs · 7,287 cycles

LIGHTNING STRIKE DAMAGE FOUND ON FUSELAGE SKIN RUB STRIP AT BS 1350-BS 1351 BETWEEN S26 &AMP; S27.&NBSP; (DAMAGE EXCEEDS THE LIMITS OF SRM 53-00-01, FIGURE 101, ALLOWABLE DAMAGE 1. A TIME LIMITED REPAIR WAS ACCOMPLISHED IAW EO 4453A663 FAA 8110-3 DATED 15 DEC 11 PART 1 AND SRM 51-10-02. THIS EO REQUIRES A DETAILED VISUAL INSPECTION OF THE REPAIRED AREA EVERY 5 FLIGHT CYCLES WITH A PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 1000 FLIGHT HOURS.)

Part: FAIRING — DAMAGED (RT WLG DOOR) · airframe 44,389 hrs · 7,194 cycles

THE LEFT & NBSP; AND RIGHT WING GEAR DOOR FAIRINGS & NBSP; HAVE DELAMINATION/DAMAGE, DAMAGE FOUND TO BE BEYOND THE SRM 52-80-02, FIGURE 101 ALLOWABLE DAMAGE 4 LIMITS PER SRM 51-70-02, FIGURE 101 ALLOWABLE DAMAGE. A TIME LIMITED REPAIR WAS ACOMPLISHED AS PER PART 1 OF EO 4452A133 AND FAA FORM 8110-3 DATED 30OCT11 WITH A REPEAT INSPECTION DUE AT EVERY 5 FLIGHT CYCLE INTERVAL UNTIL A PERMANENT REPAIR IS ACCOMPLISHED.

Part: FUEL FILTER — DIRTY (NR 1 ENGINE) · airframe 43,776 hrs · 7,080 cycles

ON DESCENT INTO PVG NR 1 ENGINE HAD FLAME-OUT AND AUTO RESTART WITH STATUS MESSAGES & NBSP;"IDLE DISAGREE" AND "ENGINE NR 1 CONTROL" (ACCOMPLISH FUEL SUMP OF NR 1 MAIN TANK AS PER AMM 12-11-10 WITH "O" WATER FOUND. REMOVED AND REPLACED ENGINE NR 1 FUEL FILTER AS PER AMM 73-11-03. CLEANED ALL C/P ON HMU PER AMM & NBSP; 73-21-14. NR 1 ENGINE RUN UP ACCOMPLISHED BY CREW AS PER AMM 71-00-00 WITH NO FAULT FOUND).

Part: PLATE — MISSING (CARGO BAY) · airframe 43,546 hrs · 7,032 cycles

MAIN DECK CARGO LT SIDE AT STA 1140 ORIFACE PLATE FOUND MISSING. ACCOMPLISHED EO 4421 AO78 PART 1 AS REQUIRED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,706 hrs · 6,594 cycles

L1 DOOR SILL EMERGENCY LIGHT ASSEMBLY HAS THE AFT BULB OUT. THE AFT BULB WAS REPLACED IAW AMM 33-51-05. LIGHT TEST WAS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,706 hrs · 6,594 cycles

EMERGENCY LIGHT LOCATED ON THE MAIN DECK, ZONE A, WAS FOUND TO BE INOPERATIVE. BOTH LAMPS IN THE ASSEMBLY WERE REPLACED IAW AMM 33-51-07 AND OPERATION WAS & NBSP; NORMAL THEREAFTER.

Part: FRAME — CRACKED (RT COWLING) · airframe 35,976 hrs · 5,896 cycles

NR 4 ENGINE RT CORE COWL HAS MOST AFT FRAME CRACKED. REMOVED AND REPLACED FRAME HAS PERMANENT REPAIR AS PER ENGINEERING ORDER 4471A061.

Part: SKIN — DELAMINATED (MIDFLAP) · airframe 35,976 hrs · 5,896 cycles

RT WING I/B MID-FLAP UPPER SURFACE O/B SECTION HAS ONE AREA OF DELAMINATION WITH PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A279.

Part: FAIRING — DELAMINATED (FOREFLAP) · airframe 35,976 hrs · 5,896 cycles

RIGHT I/B FORE FLAP L/E FAIRING HAS DELAMINATION AT SEVERAL AREAS AND PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A279.

Part: FLOOR SUPPORT — DEFORMED (FUSELAGE) · airframe 35,976 hrs · 5,896 cycles

BULK CARGO COMPT AT STA 2020 TO STA 2060 LBL 37 HAS DEFORMED FLOOR SUPPORT WITH PERMANENT REPAIR AS PER ENGINEERING ORDER 4453A407.

Part: SKIN — DENTED (TE FLAP) · airframe 35,976 hrs · 5,896 cycles

RIGHT WING OUTBOARD AFT FLAP LOWER SURFACE MID AREA HAS DENT MARK WITH PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A279.

Part: SKIN — DELAMINATED (AILERON) · airframe 35,976 hrs · 5,896 cycles

LEFT WING OUTBOARD AILERON LOWER SURFACE MID SECTION HAS 1 EA AREA OF DELAMINATION WITH PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A280.

Part: FASTENER — LOOSE (MIDFLAP) · airframe 35,976 hrs · 5,896 cycles

LEFT WING OUTBOARD MID FLAP T/E HAS NR 9 FINGER BRACKET AFT ATTACH MOUNT SCREW LOOSE AT MOST O/B END WITH PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A279.

Part: FLOOR SUPPORT — DEFORMED (FUSELAGE) · airframe 35,976 hrs · 5,896 cycles

BULK CARGO COMPT AT STATION 2000 LBL 37 HAS DEFORMED FLOOR SUPPORT WITH PERMANENT REPAIR AS PER ENGINEERING ORDER 4453A407.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 35,976 hrs · 5,896 cycles

LEFT WING OUTBOARD FORE FLAP INBOARD L/E FAIRING HAS DELAMINATION IN ONE AREA AND PERMANENT REPAIR WAS ACCOMPLISHED AS PER E/O 4457A279.

Part: FAIRING — ERODED (FOREFLAP) · airframe 35,976 hrs · 5,896 cycles

LT WING OUTBOARD FORE FLAP L/E FAIRING FOUND EROSION AND PERMANENT REPAIR ACCOMPLISHED AS PER ENGINEERING ORDER 4457A279.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 37,974 hrs · 6,191 cycles

MAIN DECK BS 1600 TO 1720 FLOOR PANEL DELAMINATED. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4453A366, WITH FAA 8110-3 DATED 29 MAY 2010. REPEAT DVI EVERY 25 FLIGHT CYCLES. PERMANENT REPAIR WITHIN 1000 FLIGHT HOURS.

Part: SLEEVE — DAMAGED (THRUST REVERSER) · airframe 37,151 hrs · 6,150 cycles

SUSPECT LIGHTNING STRIKE DAMAGE FOUND ON NR 2 ENGINE OUTBOARD REVERSER SLEEVE AT TRAILING EDGE AT THE 3 O'CLOCK POSITION. TEMPORARY REPAIR ACCOMPLISHED PER EO 4478A126 WITH CHAPTER 5 LIGHTNING STRIKE INSPECTION.

Part: SKIN — DAMAGED (NR 2 NACELLE) · airframe 36,268 hrs · 5,938 cycles

DURING DEICING OPERATIONS NR 2 ENGINE INLET COWL SUSTAINED DAMAGE CONSISTING OF SCRATCHES ON THE EXTERNAL SKIN AT APPROXIMATELY 10 O'CLOCK POSITION. DAMAGE IS OUT OF ALLOWABLE DAMAGE SRM 54-15-01 LIMITS. TIME LIMITED REPAIR ACCOMPLISHED PER ENGINEERING ORDER 4454A093 & FAA 8110-3 DATED 26 JAN 2010. DVI REQUIRED EVERY 5 FLIGHT CYCLES & PERMANENT REPAIR AT NEXT A CHECK.

Part: DEPRESSOR — DAMAGED (CARGO DOOR) · airframe 35,314 hrs · 5,799 cycles

DURING WALK AROUND FOUND DEPRESSOR SEAL DAMAGE ON MAIN DECK SIDE CARGO DOOR FWD SIDE APPROX 1.5 IN X 0.5 IN. TIME LIMITED REPAIR ACCOMPLISHED AS PER EO 4453A307. FAA 8110-3 ISSUED 12 NOV 09. DVI REQUIRED EVERY FLIGHT CYCLE WITH PERMANENT REPAIR TO BE ACCOMPLISHED AT NEXT A-CHECK.

Part: ACCESS DOOR — MISSING (NR 1 NACELLE) · airframe 36,099 hrs · 5,990 cycles

NR 1 RT OUTBOARD STRUT ACCESS DOOR 454DR WAS FOUND TO BE MISSING DURING WALK AROUND INSPECTION. EO 4454A072 WAS ISSUED WITH A TIME LIMITED REPAIR AND A PERMANENT REPAIR TO BE DONE PRIOR TO 25 FLIGHT CYCLES.

Part: DOOR — DAMAGED (LT MLG) · airframe 31,177 hrs · 5,181 cycles

DAMAGE TO LT WING LANDING GEAR DOOR. TIME LIMITED REPAIR AS PER EO 4452A056. REPEAT DVI'S AT EVERY FLIGHT CYCLE AND A PERMANENT REPAIR AT NEXT "A" CHECK."

Part: START VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 30,671 hrs · 5,101 cycles

NR 1 ENGINE START VALVE FAILED. DEFERRED ITEM PER DISPATCH DEVIATIONS GUIDE PROCEDURE ITEM 80-11-1 CAT C, ALLOWING TO DISPATCH THE ACFT WITH NR 1 ENGINE START VALVE INOP. MANUAL START REQUIRED.

Part: SKIN — DELAMINATED (MLG DOOR) · airframe 27,661 hrs · 4,642 cycles

RT WING LANDING GEAR STRUT DOOR SKIN DELAMINATED. ACCOMPLISHED INTERIM REPAIR PER MA NR A4 5280-03:00 PART 1.

Part: DOOR — DELAMINATED (RT MLG) · airframe 27,437 hrs · 4,606 cycles

RIGHT WING GEAR INBD STRUT DOOR HAS SKIN DELAMINATION. ACCOMPLISHED PART 1 OF THE TIME LIMITED REPAIR OF MA NR A45280-02:00. COI NR 453-031 WAS OPENED FOR A 5-CYCLE VISUAL INSPECTION.

Part: CARBON SEAL — LEAKING (NR 4 ENGINE) · airframe 27,421 hrs · 4,602 cycles

"ENG 4 OIL PRESSURE" ENG 4 SHUT DOWN DUE TO ZERO OIL QUANTITY/LOW PRESS AFTER SHUT DOWN OIL PRESS REMAINED 7PSI. SERVED ENG OIL WITH 25 QTS ACCOMPLISHED ENG MOTORING AND FOUND LEAK ON IDG DRAIN PORT. REPLACED NR 4 ENG IDG CARBON SEAL. ACCOMPLISHED ENG RUN AND NO LEAK FOUND AMM 24-11-01.

Part: ATTACH ANGLE — DAMAGED (CARGO DOOR) · airframe 25,781 hrs · 4,342 cycles

DAMAGE WAS FOUND ON THE MAIN DECK SIDE CARGO DOOR BS 1920 SEAL DEPRESSOR AND ATTACH ANGLE. CRACKS WERE FOUND ON SAID ITEMS AT APPROXIMATELY 24" FROM LOWER AFT CORNER. INTERIM REPAIR ACCOMPLISHED AS PER PART 1 OF MA A4 5300-09-00:00 FAA 8110-3.

Part: WARNING LIGHT — FALSE ACTIVATION (GENERATORS) · airframe 24,948 hrs · 4,208 cycles

ELECT GEN 1, ELECT GEN 2, ELECT GEN 3 MESSAGES AFTER ENGINE START. RETURNED TO BLOCKS. PERFORMED GROUND TEST PER MM 24-23-00. OPERATIONS NORMAL.

Part: CONTROL UNIT — UNKNOWN (TE FLAPS) · airframe 23,454 hrs · 3,960 cycles

MULTIPLE STATUS MESSAGES: "STAB AUTO TRIM," "RUDDER RATIO," "NO LAND 3," AND "FLAP CONTROL R." PERFORMED OPERATIONAL CHECKS ASSOCIATED WITH SPECIFIC MESSAGES AND RERACKED FLAP CONTROL UNIT PER MM 27-50-00.

Part: UNKNOWN — UNKNOWN (MLG) · airframe 22,216 hrs · 3,763 cycles

GEAR DOOR AND GEAR MONITOR STATUS MESSAGES SHOWN ON EICAS. CYCLED GEAR DOORS, MESSAGES CLEARED PER FIM 32-61-00.

Part: START VALVE — UNKNOWN (NR 2 ENGINE) · airframe 20,634 hrs · 3,537 cycles

AFTER PUSHBACK, NR 2 ENGINE WOULD NOT START AND -HP BLEED 2- STATUS MESSAGE DISPLAYED. RESET ASCTU O/B EXERCISED NR 2 ENGINE START VALVE, SUCCESSFUL ENGINE START ACCOMPLISHED. REPAIR ACCOMPLISHED PER 80-11-02.

Part: ENGINE — FOD (NR 3) · airframe 18,630 hrs · 3,224 cycles

APPROACHING V1 LOUD BANG WITH FLASH OBSERVED. REJECTED TAKEOFF AT 128KTS AT END OF RUNWAY NR 3, ENGINE EGT AT 800 DEG. PERFORMED HIGH-ENERGY STOP INSPECTION. PERFORMED BOROSCOPE INSPECTION, FOUND 11TH AND 12TH STAGE BLADES FOD'D. REMOVED AND REPLACED NR 3 ENGINE PER PAC-JCP71-00-001A AND 2A. ENGINE RUN AND LEAK CHECK NORMAL.

Part: ACTUATOR — FAILED · airframe 17,459 hrs · 3,039 cycles

SIDE CARGO DOOR INOP ELECTRICALLY AND MANUALLY. PWR LIFT ACTUATIOR REPLACED IAW MM 52-32-02. OPS CHECK OK.

Part: ENGINE — MALFUNCTIONED (NR 3) · airframe 16,865 hrs · 2,940 cycles

NR 3 ENG THRUST LEVER WOULD NOT ADVANCE TO TAKEOFF POWER ON T/O ROLL. LOW SPEED ABORT PERFORMED. A/C RETURNED TO BLOCKS. VISUAL INSPECTION OF THROTTLE & PEDESTAL MECHANISM PERFORMED PER MM 76-11-03. NO DISCREPANCIES FOUND AUTOTHROTTLE. FULL POWER ENGINE GROUND RUN PERFORMED. FLIGHT CREW NOTED, OPS CHECK OF SYSTEM GOOD.

Part: WARNING SYSTEM — ACTIVATED (BRAKES) · airframe 14,486 hrs · 2,555 cycles

CREW REPORTED REJECTED TAKEOFF - CONFIGURE WARNING BETWEEN 60/70 KTS. CONSULTED BRAKE COOLING. NO ACTION REQUIRED. WALK AROUND VISUAL INSPECTION NORMAL PER MM 05-51-10. NO DEFECTS NOTED.

Part: COOLING FAN — FAULTY (CARGO BAY) · airframe 13,069 hrs · 2,321 cycles

AFTER BLOCK IN ON THE GROUND IN HKG, STRONG SMELL OF TOXIC FUMES WERE PRESENT IN THE COCKPIT AND UPPER DECK. THE FUMES HAD THE SMELL OF ELECTRIC WIRING OVERHEAT OR BURNING AND CAUSED EYE AND SINUS IRRITATION. THE FUMES PERSISTED AFTER VENTILATION. FOUND LEFT SIDE WALL FWD CARGO COMPT STA 550 DRIVEBAY NR 1 E/E COOLING FAN EMITTING AN ODOR. LOCKED OUT FAN AND DEFERRED PER 21-58-6.

Part: WARNING LIGHT — ILLUMINATED (START VALVE) · airframe 12,303 hrs · 2,196 cycles

ENGINE NR 3 (START VALVE) EICAS MESSAGE, QPH CHECK ACCOMPLISHED. TRANSFERRED TO DMI NR 33262 IAW MEL 80-11-01.

Part: PDU — MALFUNCTIONED (LE FLAPS) · airframe 12,096 hrs · 2,170 cycles

A/C RETURN TO BLOCK DUE TO EICAS MESSAGE FLAP PRIMARY, FLAP DRIVE FOLLOWED BY STATUS MESSAGE L/E MULTI DRIVE, FLAP SYSTEM MONITOR. REPLACED NR 2 RIGHT HAND LED PDU & TESTED ELECTRICALLY NORMAL.

Part: ACTUATOR — INOPERATIVE (OUTFLOW VALVE) · airframe 11,819 hrs · 2,120 cycles

STATUS MESSAGE (OUTFLOW VALVE RT SIDE) APPEARED DURING CRUISE, BOTH OUT FLOW VALVES WOULD NOT OPERATE IN AUTO. REMOVED AND REPLACED OUTFLOW VALVE ACTUATOR.

Part: CONTROL UNIT — INOPERATIVE (OUTFLOW VALVE) · airframe 11,819 hrs · 2,120 cycles

STATUS MESSAGE (OUTFLOW VALVE LT SIDE) APPEARED DURING CRUISE. BOTH OUTFLOW VALVES WOULD NOT OPERATE IN AUTO. REMOVED AND REPLACED LT SIDE ICU.

Part: RELAY — FAILED (AOA HEAT) · airframe 11,489 hrs · 2,061 cycles

EICAS MESSAGE ON ENGINE START L AOA HEAT & R AOA HEAT. RESET RELAYS R1423 & R1424, PERFORMED GROUND TEST PER MM 30-31-00 & ENGINE RUNUP PER 71-00-00, OPS CHECK NORMAL.

Part: WARNING LIGHT — ILLUMINATED (TRANSFER VALVE) · airframe 11,249 hrs · 2,017 cycles

LOWER FUEL INDICATION OF RESERVE TANK TRANSFER VALVE 2 AND 3 OPEN LIGHT ON. ITEM TRANFERED TO DMI NR 32738 IAW MEL NR 28-16-1.

Part: CDU — INOPERATIVE (COCKPIT) · airframe 10,651 hrs · 1,911 cycles

CAPTAINS FMC CDU INOPERATIVE. SWAPPED CAPTAINS CDU WITH CENTER CDU, CAPTAINS CDU OPERATIONAL CHECK OK, AS PER MM 34-61-00. CENTER CDU PLACED ON DEFERRAL PER MEL 34-62-2-1.

Part: TRANSMITTER — MALFUNCTIONED (NR 4 ENG OIL) · airframe 10,525 hrs · 1,884 cycles

NR 4 ENGINE OIL PRESSURE 155 PSI AT IDLE POWER, WITH POWER INCREASE OIL PRESSURE REMAINS HIGH. REMOVED AND REPLACE NR 4 ENGINE OIL TRANSMITTER IAW AMM 79-32-01. OPS CHECK & LEAK CHECK OK.

Part: CONNECTOR — DAMAGED (ENG OIL TEMP) · airframe 5,674 hrs · 986 cycles

NR 2 ENG OIL PRESSURE VARIED FROM 100-160 ON TAXI OUT. OPENED NR 2 ENG, CHECKED CONNECTION AT OIL PRESSURE TRANSMITTER AND FOUND PUSHED BACK PIN. RESEATED OPS CHECKED NORMAL ON ENG RUN.

Part: ACCESS PANEL — BROKEN (RT WING) · airframe 5,476 hrs · 951 cycles

GROUND DAMAGE TO RT WING TIP BETWEEN WS 155-25 & WBL 1243-75. TAIL JACK WAS DRAGGED UNDER WING TIP CAUSING DAMAGE TO HEADING EDGE, TRAILING EDGE A FUEL TANK EDGE A FUEL TANK ACCESS PANEL & UNDERSIDE OF WING. PERFORMED DYE PENETRANT CK, FOUND NO CRACKS MATERIAL TO BE WITHIN LIMITS AS PER B747 SRM 57-20-01. SPEED TAPED AREAS OF LEADING EDGE & TRAILING EDGE THAT WHERE DAMAGED AS PER POLAR GMM 3-17-01. PERMANENT REPAIR TO BE PERFORMED AT JFK. THE TAIL STAND WAS REMOVED FROM THE A/C & WHEN THE STAND WAS MOVING, IT WAS DRAGGED UNDER THE WING. CONTINUED OPEN ITEM 453-055 WAS CREATED TO ALLOW A/C OPS WITH DAMAGE, UNTIL A/C ARRIVED AT JFK - WHERE PERMANENT REAIRS WERE COMPLETED PER B747-400 SRM 57-51-01.

Part: DISPLAY — INOPERATIVE (VOR) · airframe 5,399 hrs · 936 cycles

CENTER AUTO PILOT ON THE ILS DIDN'T CAPTURE LOCALIZER / GLIDE SLOPE. FOUND CMC MESSAGE VOR - RIGHT DISPLAYED. GROUND TEST CARRIED OUT PER 34-51-00. NO FAULTS NOTED.

Part: BOLT — STRIPPED (ACTUATOR) · airframe 5,119 hrs · 887 cycles

LOWER FWD CARGO DOOR ACTUATOR HAD TWO SUPPORT CARGO DOOR ACTUATORS WITH INSUFFICIENT BOLT THREAD SHOWING AND THE OTHER TWO BOLTS HAD EXCESSIVE THREAD ENGAGEMENT AND BOTTOMED OUT, INDICATING THE ENTIRE ACTUATOR LOAD WAS CARRIED OUT BY ONLY TWO BOLTS. REPOSITIONED AND RE-TORQUE BOLTS IAW AMM 52-34-02.