N415MC

Part: ACTUATOR — FAULTED (ZONE 700) · airframe 90,825 hrs · 15,242 cycles

GEAR CONFIG WARNING ON TAKEOFF. R & R BODY L/H ACTUATOR AND OPS CHECK GOOD IAW AMM 32-53-11 & IPC 32-53-11-05A ITEM 65.

Part: VALVE — FAULTED (ZONE 400) · airframe 89,220 hrs · 15,003 cycles

ENG 4 T/R EICAS CAUTION MESSAGE(<P>REMOVED AND REPLACED #4 ENGINE DIRECTIONAL PILOT VALVE IAW AMM 78-34-01/401. OPS CHECK NORMAL. DMI 223578 CLOSED</P>)

Part: ENGINE — MAKING METAL (NR 4) · airframe 86,517 hrs · 14,595 cycles

CAUTION MESSAGE (EICAS) ENG 4 OIL FILTER IN FLIGHT. TIME 0910Z. FIRE HANDLE NOT PULLED. ENG SHUTDOWN.(<P>C/W OIL SYS CONTAMINATION EXAMINATION IAW AMM 79-00-00, FOUND EXTENSIVE CONTAMINATION LEADING TO ENGINE CHANGE REQUIRED. R/R FILTER IAW AMM 79-21-04. FOUND CONTAMINATION IN FILTER. R/R STARTER VALVE #4 IAW AMM 80-11-02. OPS CHECK GOOD. REF IPC 80-11-02-02B REV 86. C/W WO 129315 TASK CARD 71-099-02-01 FOR ENG R/R. NO FURTHER DEFECTS NOTED</P>)

Part: ROTOR — UNKNOWN (NR 3 ENGINE) · airframe 85,879 hrs · 14,502 cycles

ENG 3 CONTROL STS MSG. SUSPECT EEC FAILURE(<P>R/R #3 EEC &AMP; ROTOR OF CONTROL ALTERNATOR. OPS CHECK GOOD IAW AMM 73-21-08 &AMP; AMM 73-21-15. DMI 201757 CLOSED.</P>)

Part: SWITCH — UNKNOWN (UNKNOWN) · airframe 82,213 hrs · 13,918 cycles

ON TAKE-OFF, N1 ON #1 ENGINE ONLY PRODUCED 42% THRUST(<P>FOUND #1 THRUST REVERSER POSITION FEEDBACK SENSOR OUT OF ADJUSTMENT READING 28.0. ADJUSTED IAW B747-700 AMM 78-34-10. READING 0.0 NOW. DIRECTLY RELATED TO DMI 182884 ON LP 1777901 P1 PER MEL 78-31-01A CAT C. DMI REMAINS OPEN.</P> / <P>LP 1777919 P2: DUE TO REMAINING G/T AND FLT SCHEDULE, RE-DEACTIVATE T/R IAW AMM 78-31-01. BOTH SIDES SECURED CLOSED. DUE TO REMAINING G/T AND FLT SCHEDULE, RE-DEACTIVATE T/R IAW AMM 78-31-01. BOTH SIDES SECURED CLOSED. DMI 182884 REMAINS OPEN.</P> / <P>LP 1643743 M10: REMOVED AND REPLACED ENG T/R SWITCH PACK ASSY IAW AMM 76-11-03. #1 T/R OPS CHECK NORMAL REF AMM 78-31-00.

Part: STRAP — DISPLACED · airframe 78,714 hrs · 13,364 cycles

FLAPPING AND RUSHING AIR SOUND COMING FROM UPPER DECK SERVICE DOOR AT 10,500 FT(<P>FOUND DOOR STRAP INHIBITING DOOR SEAL, REMOVED DOOR STRAP, DOOR CLOSED PROPERLY.</P>)

Part: SKIN — DENTED · airframe 77,718 hrs · 13,211 cycles

RHW #18 VC-FLAP BALLNOSE SKIN LWR MID AREA FOUND DENT(<P>RHW #18 VC-FLAP BALLNOSE SKIN LWR MID OUT OF LIMITS DENT AREA EXTERNAL DOUBLER REPAIRED</P>)

Part: FLAP — DELAMINATED · airframe 77,718 hrs · 13,211 cycles

LHW O/B FORE FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)

Part: RIB — CRACKED · airframe 77,718 hrs · 13,211 cycles

RHW I/B MID FLAP O/B RIB AFT ANGLE (CLIP) FOUND CRACKED(<P>FABRICATE THE REPLACEMENT ANGLE (CLIP) FROM 70757651 BARD PLATE. AND REPLACED AND INSTALLED.</P>)

Part: DOUBLER — CRACKED · airframe 77,718 hrs · 13,211 cycles

M/D LH #5 DOOR FWD CUTOUT STA 2231 DOOR REVEAL DOUBLER BETWEEN STR 21L AND STR 22L FOUND CRACKED(<P>M/D LH #5 DOOR FWD CUTOUT STA 2231 DOOR REVEAL DOUBLER BETWEEN STR 21L AND STR 22L CRACK AREA EXTERNAL DOUBLERS REPAIRED.</P>)

Part: FRAME — CHAFED · airframe 77,718 hrs · 13,211 cycles

#1 ENG L/H CORE COWL INNER NO.4 FRAME MID AREA FOUND CHAFING DAMAGE(<P>#1 ENG LH CORE COWL INNER NO.4 FRAME MID CHAFING DAMAGE AREA EXTERNAL PATCH REPAIRED</P>)

Part: SHEAR TIE — CRACKED · airframe 77,718 hrs · 13,211 cycles

STA 1000 FRONT SPAR UPPER RBL 33.99" ATTACH SHEAR TIE FOUND CRACKED(<P>USING 69B14267U11 SHEAR TIP IN LIEU OF 69B14267U9 SHEAR TIE REPLACED AND INSTALLED</P>)

Part: FLAP — DELAMINATED · airframe 77,718 hrs · 13,211 cycles

LHW O/B MID FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)

Part: FLAP — DELAMINATED · airframe 77,718 hrs · 13,211 cycles

LHW I/B MID FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)

Part: BATTERY — FAILED · airframe 77,718 hrs · 13,211 cycles

EMERGENCY LIGHT TEST FOUND POWER SUPPLY BATT M5169 FAILED(<P>REPLACED POWER SUPPLY BATT M5169 IAW AMM 33-51-04 AND TEST PASS</P>)

Part: FLAP — DELAMINATED · airframe 77,718 hrs · 13,211 cycles

RHW I/B MID FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)

Part: ACCESS PANEL — ELONGATED · airframe 77,718 hrs · 13,211 cycles

#2 PYLON VALVE ACCESS PNL #462EL 1EA BOLT HOLE ELONGATED(<P>#2 PYLON VALVE ACCESS PNL #462EL 1EA ELONGATED BOLT HOLE AREA DOUBLER REPAIRED AS PER RI-54-50-15404 REV.A</P>)

Part: FLAP — DELAMINATED · airframe 77,718 hrs · 13,211 cycles

RHW O/B FORE FLAP L/E FOUND DELAMINATION(<P>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: BATTERY — FAILED · airframe 77,718 hrs · 13,211 cycles

EMERGENCY LIGHT TEST FOUND POWER SUPPLY BATT M5170 FAILED(<P>REPLACED POWER SUPPLY BATT M5170 IAW AMM 33-51-04 AND TEST PASS</P>)

Part: SKIN — CRACKED · airframe 77,718 hrs · 13,211 cycles

#3 ENG RH CORE COWL EXHAUST LWR RIVETS HOLES FOUND CRACKED(<P>#3 ENG RH CORE COWL PRECOOLER LOWER SKIN CRACK AREA EXTERNAL DOUBLER REPAIRED</P>)

Part: ACCESS PANEL — ELONGATED · airframe 77,718 hrs · 13,211 cycles

#1 PYLON VALVE ACCESS PNL #452EL 1EA BOLT HOLE ELONGATED(<P>#1 PYLON VALVE ACCESS PNL #452EL 1EA ELONGATED BOLT HOLE AREA DOUBLER REPAIRED AS PER RI-54-50-15405 REV.A&NBSP;&NBSP;</P>)

Part: FLAP — DELAMINATED · airframe 77,718 hrs · 13,211 cycles

LHW O/B FORE FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)

Part: FLAP — DELAMINATED · airframe 77,718 hrs · 13,211 cycles

RHW O/B AFT FLAP AFT O/B CORNER FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5G</SPAN></P>)

Part: FLAP — DELAMINATED · airframe 77,718 hrs · 13,211 cycles

LHW O/B AFT FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)

Part: FLAP — DELAMINATED · airframe 77,718 hrs · 13,211 cycles

RHW O/B MID FLAP L/E FOUND DELAMINATION(<P>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: ACCESS PANEL — ELONGATED · airframe 77,718 hrs · 13,211 cycles

#3 PYLON VALVE ACCESS PNL #472EL 2EA BOLT HOLES ELONGATED(<P>#3 PYLON VALVE ACCESS PNL #472EL 2EA ELONGATED BOLT HOLES AREA DOUBLER REPAIRED AS PER RI-54-50-15403 REV.A</P>)

Part: FLAP — DELAMINATED · airframe 77,718 hrs · 13,211 cycles

RHW O/B FORE FLAP L/E FOUND DELAMINATION(<P><SPAN>PERFORMED REPAIR AS PER SRM 51-70-07 PAR.5A</SPAN></P>)

Part: NONE — NONE

ENG #1 WOULD NOT ACCELERATE OVER 50% N1 DURING TAKEOFF(<P>PERFORMED RIGGING OF ENG 1 RH TR FEED BACK ACTUATOR CDU. OPERATIONAL CHECK OKAY REF AMM 78-31-00/501 AND AMM 78-31-21/401. MSG CLEARED MCC NOTIFIEDL</P>)

Part: PDU — FAULTED (FLAP DRIVE) · airframe 74,372 hrs · 12,684 cycles

FLAPS DRIVE MSG(<P>REMOVED AND REPLACED R4 FLAP PDU. OPS OK IN BOTH MODE PER AMM 27-81-03.</P>)

Part: EICAS — WARNING MESSAGE (NR 4 ENGINE) · airframe 73,963 hrs · 12,617 cycles

ATB #4 ENGINE SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE, ENG 4 OIL PRESS EICAS MESSAGE. #4 OIL QTY 0 - OIL PRESS 4 WHILE WINDMILLING.(<P ><SPAN>REMOVED AND REPLACED STARTER AND SHAFT O-RING. LEAK &AMP; OPS CHECK OK. PER AMM 80-11-01/401.</SPAN></P>)

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 73,154 hrs · 12,485 cycles

COCKPIT DESCENT DEVICE "A" SEAL DAMAGE CABLE OVEREXTENDED. REMOVED AND REPLACED DESCENT DEVICE POSITION "A", IAW AMM 25-61-01. NO DISCREPANCIES NOTED.

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 73,154 hrs · 12,485 cycles

COCKPIT DESCENT DEVICE "B" SEAL DAMAGE CABLE OVEREXTENDED. REMOVED AND REPLACED DESCENT DEVICE POSITION "B", IAW AMM 25-61-05. NO DISCREPANCIES FOUND.

Part: ESCAPE REEL — DAMAGED (COCKPIT) · airframe 7,315,411 hrs · 12,485 cycles

COCKPIT DESCENT DEVICE "C" SEAL DAMAGE CABLE OVEREXTENDED. REMOVED AND REPLACED DESCENT DEVICE POSITION "C", IAW AMM 25-61-01, NO DISCREPANCIES FOUND.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 69,453 hrs · 11,922 cycles

WORN - TRACK, AFT CARGO COMPARTMENT SEAT TRACK WORN (STA 1780 LBL 45.5)(<P>REPAIRED DAMAGED AREA IAW SRM 53-00-52-2R-10 REV. 88. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SKIN — DEBONDED (RT AILERON) · airframe 69,453 hrs · 11,922 cycles

DISBOND - SKIN, OUTBD SIDE OF R/H WING INBD AILERON T/E SKIN, WBL 515.(<P>REMOVE THE DAMAGE MATERIAL AND CLEAN. MEASURE THE DAMAGED AREA (L = 2", W = 0.1", 1" FROM OUTBD EDGE AT AFT EDGE). BOND REPAIR PLIES WITH RESIN. CURE AT 150 DEGREES F FOR 180 MINUTES. KEEP A MINIMUM VACUUM PRESSURE AT 22 IN/HG, IAW B747-400F SRM 57-60-01-2R-1. REFER TO SRM 51-70-06-0G-0 REV. 88. CONDITION CHECK IS SATISFACTORY.</P>)

Part: WIRE — ERODED (NR 2 PYLON) · airframe 69,453 hrs · 11,922 cycles

FOUND WIRE W6054-205-206, 211-212-20 AND CLAMP EROSION IN NO. 2 PYLON FWD FAIRING.(<P>REPAIRED WIRE IAW WDM 24-11-12, 36-11-42 REV. 47, SWPM 20-30-12 REV. 73, AND TRANSFER TEST ITEM TO MCS 8007 FORM T2031 ITEM #1.&NBSP;</P>)

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,453 hrs · 11,922 cycles

FOUND EMERGENCY LIGHT POWER PACK M5168 TEST FAIL.(<P>IAW AMM 33-51-04-902-001-001 REPLACED BATTERY ASSY AND PERFORMED TEST. THE RESULT WAS SATISFACTORY.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,453 hrs · 11,922 cycles

CORROSION ON THE MAIN DECK SEAT TRACK AT STA 2175, RBL 11.33.(<P>REPAIR DAMAGED SEAT TRACK IAW SRM 53-00-52-2R-12 REPAIR 12 REV. 88 AND EI NO T2020-A53M-662 REV. 1 DWG NO 65338253 SH 53 REV. - , 65B3825, SH 54 REV. - . JOB COMPLETED AND CONDITION CHK NORMAL.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,453 hrs · 11,922 cycles

CORROSION ON THE MAIN DECK SEAT TRACK AT STA 1795, LBL 11.33.(<P>REPAIR THE CORROSION AREA IAW SRM 53-00-52-2R-12 REV. 88 AND DWG 65B38253, SH49 REV. - AND SH50, REV. A AND EI NO T2020A53M-862 REV. 1. EI NO T2020A53M-862 REV. 1 ATTACHING NRC 4351302 (278). JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: WIRE — ERODED (NR 3 PYLON) · airframe 69,453 hrs · 11,922 cycles

FOUND WIRE: W6084-011-20, 007-20, 140-18, 015-20 AND CLAMP, EROSION IN NO 3 PYLON FWD FAIRING(<P>REPAIRED WIRE AND CLAMP IAW WDM 73-21-55, 73-21-35, 78-34-33 REV. 47, AND SWPM 20-30-12 REV. 73. TRANSFER TEST TO MCS 8007 FORM T2031 ITEM #2.</P>)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 69,453 hrs · 11,922 cycles

CORROSION ON THE MAIN DECK SEAT TRACK AT STA 1895 AND STA 1910, LBL 11.33.(<P>REPAIR THE CORROSION AREA IAW SRM 53-00-52-2R-12 REV. 88 AND DWG 65B38253 SH51 REV. 1 AND EI NO T2020A53M-862 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SEAT TRACK — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 69,453 hrs · 11,922 cycles

CORROSION ON THE MAIN DECK SEAT TRACK AT STA 2175 LBL 11.33.(<P>REPAIR DAMAGED SEAT TRACK IAW SRM 53-00-52-2R-12 REPAIR 12 REV. 88 AND EI NO T2020A53M-661 REV. 1 DWG NO 65B38253, SH 53 REV. - , 65B38253, SH 54 REV. - . JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 69,453 hrs · 11,922 cycles

WORN - TRACK, AFT CARGO COMPARTMENT SEAT TRACK WORN (STA 1680, LBL 24.75)(<P>REPAIRED DAMAGED AREA IAW SRM 53-00-52-2R-10 REV. 88. JOB COMPLETED AND CONDITION CHK NORMAL.</P>)

Part: SKIN — CORRODED (TE FLAP) · corrosion level 2 · airframe 69,453 hrs · 11,922 cycles

CORROSION - SKIN, LOWER SURFACE OF L/H WING OUTBD AFT FLAP BETWEEN WBL 515 AND WBL 619.(<P>IAW AMM 27-51-06-004-001 REV. 97 AND AMM 27-51-06-004-008 REV. 97, REPLACED L/H WING OUTBD AFT FLAP. TRANSFER TO J/C NO 27-051-04-15, ADJUST L/H WING OUTBD AFT FLAP. CONDITION CHECK NORMAL.</P>)

Part: STIFFENER — CORRODED (RT BLG WW) · corrosion level 2 · airframe 69,453 hrs · 11,922 cycles

FOUND CORROSION ON STIFFENER OF RH BODY LANDING GEAR WHEEL WELL, AT STA 1457.83, RBL 9, BETWEEN WL91 TO 116.(<P>ACCOMPLISHED EI NO T2020A53M-630 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 69,453 hrs · 11,922 cycles

FOUND CRACK DAMAGE ON WEB AND LOWER CHORD OF LH HST RIB AT HSBL 421.5.(<P>ACCOMPLISHED EI NO T2020A55M-751 REV. 1. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)

Part: SWITCH — STUCK (COCKPIT) · airframe 69,150 hrs · 11,878 cycles

SIMULTANEOUS FAILURE OF ALL THREE COMM RADIOS. "RADIO TRANSMIT" ON CONTINUOUSLY.(<P>FOUND&NBSP;FO'S&NBSP;YOKE SWITCH STUCK. CLEARED YOKE SWITCH. OPS CHECKED OK PER AMM 23-12-00.<BR /></P>)

Part: TRANSCEIVER — FAULTY (VHF COMM) · airframe 67,984 hrs · 11,693 cycles

L VHF INOP. REMOVED AND REPLACED LEFT VHF TRANSCEIVER PER AMM 23-11-05 (OFF; PN: 822-1047-002, SN: 8506), NO FAULTS AT THIS TIME. INSP ANTENNA'S, FOUND UPPER FWD AND UPPER AFT ANTENNA'S DAMAGED FROM LIGHTNING STRIKE. REPLACED FWD & AFT UPPER ANTENNA'S IAW AMM 23-12-03. ALSO PERFORMED LIGHTNING STRIKE CONDITIONAL INSP IAW AMM 05-51-13. OFF PART: (SN 22026, PN: DMC50-17)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,913 hrs · 11,508 cycles

M/D DOOR EMERGENCY LIGHT 2 EA FOUND INOP.(<P>M/D DOOR EMERGENCY LIGHT 2 EA REMOVED AND REPLACED. TESTED NORMAL IAW AMM 33-51-07.</P>)

Part: DOOR — DAMAGED (LT BLG) · airframe 66,657 hrs · 11,458 cycles

LEFT OUTBOARD BODY GEAR DOOR DAMAGED.&NBSP;(<P>REMOVED GEAR DOOR AND APPLIED CDL 32-14-02. AIRCRAFT FLOWN TO CVG TO REPLACE GEAR DOOR AND CLEAR CDL.&NBSP;</P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,244 hrs · 11,388 cycles

L1 DOOR SILL EMERGENCY LIGHTS L1853 AND L1854 INOP(<P>RELAMPED L1853 AND L1854 PER B747-400 AMM TASK 33-51-05-962-031. OPS CHECKED GOOD PER B747-400 SUB-TASK 33-51-05-712-029.</P>)

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 6,538,532 hrs · 11,243 cycles

UPPER DECK EXIT LIGHT AT THE RIGHT CREW DOOR WAS INOPERATIVE. REPLACED THE FUSE ON THE BATTERY POWER SUPPLY M5168. EMERGENCY LIGHTS OPS CHECKED GOOD IAW AMM 33-51-04-710-001.

Part: SKIN — DAMAGED (E/E DOOR) · airframe 62,699 hrs · 10,732 cycles

M/D E & E ACCESS DOOR SKIN FOUND CRACKED AND SEVERAL DENTS. REPAIRED IAW RI-57-44-12464, REV A.

Part: STEP — CRACKED (ACCESS LADDER) · airframe 62,699 hrs · 10,732 cycles

MID CREW ACCESS LADDER THREAD ASSY, NR 5 STEP FOUND CRACKED. REPAIRED IAW RI-25-50-12454, REV A.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 62,699 hrs · 10,732 cycles

RIGHT WING NR 22 FLAP BULLNOSE OTBD EDGE FOUND CRACKED. TRIMMED AND REPAIRED IAW RI-57-44-12466 REV A.

Part: CARGO TRACK — BROKEN (BS 1877-1880) · airframe 62,699 hrs · 10,732 cycles

AFT CARGO BS 1880, LBL25, CARGO TRACK FOUND BROKEN. THE CARGO TRACK WAS REPAIRED IAW RI-57-44-12473, REV A.

Part: FAIRING — DAMAGED (RT NACELLE) · airframe 62,699 hrs · 10,732 cycles

RIGHT CORE COWL EXTERNAL UPPER FAIRING AFT EDGE CRACKED AND DEFORMED. REPAIRED IAW EO 1971A176, REV O.

Part: SUPPORT — CRACKED (HYD LINE) · airframe 62,699 hrs · 10,732 cycles

PITOT HYRAULIC TUBING SUPPORT FOUND CRACKED. REPAIRED IAW RL-53-80-12462, REV A

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 55,855 hrs · 9,425 cycles

MAIN DECK CARGO 12 LOOP B STATUS MSG DISPLAYED. NO MSG CURRENTLY DISPLAYED. VISUAL & OPERATIONAL CHECKS PERFORMED IAW AMM TASK 26-14-00-735-067 SUB TASK 26-14-00-860-025 730-023 024 025 & 026.

Part: DOUBLER — DENTED (FUSELAGE) · airframe 55,597 hrs · 9,376 cycles

DENT LOG STATION 2598 TAIL STAND JACK PAD EXISTING REPAIR DOUBLER BLEND OUT 0.375" * 0.5" * 0.054". EXISTING REPAIR DOUBLER BLEND OUT, REPAIRED IAW RI-53-80-11288 REV A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,597 hrs · 9,376 cycles

STATION 1480 RT LONGERON EXTENSION FTG CRACKED, LENGTH 1/2" APPROX. REPAIRED IAW EO 4453A818 PART 4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,597 hrs · 9,376 cycles

STATION 1480 LT LONGERON EXT FTG FOUND CRACKED, LENGTH 5/8" APPROX. REPAIRED IAW EO 4453A818 PART 3.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 55,597 hrs · 9,376 cycles

RIGHT BS 720, UPPER DECK TENSION TIE, FWD CHANNEL FOUND CRACKED AT RADIUS 3/8" LONG. REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1.

Part: RIB — CRACKED (LT MLG DOOR) · airframe 55,597 hrs · 9,376 cycles

LEFT INBD FWD MLG WW DOOR, FWD CORNER FOUND CRACK. LT INBD FWD MLG PRIMARY DOOR, FWD CLOSING RIB REPAIRED IAW SRM 51-40-02 & MX RI-52-80-11287 REV A.

Part: DOOR — DENTED (LT BLG) · airframe 55,597 hrs · 9,376 cycles

LEFT BLG INBD SHOCK DOOR, INNER SURFACE FOUND DENT. REPAIRED IAW RI NR RI-52-83-11289 REV A.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 55,597 hrs · 9,376 cycles

LEFT BS 720 UPPER DECK TENSION TIE FWD CHANNEL, FOUND CRACKED AT RADIUS 3/8" LONG. REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 55,597 hrs · 9,376 cycles

MAIN DECK SIDE CARGO DOOR, AFT DOOR SILL FOUND CRACK. REPAIRED IAW RI-25-55-11284 REV A.

Part: DOOR — CRACKED (RT MLG) · airframe 55,597 hrs · 9,376 cycles

RIGHT INBD FWD MLG WW DOOR, FWD EDGE OTBD CORNER FOUND CRACK. REPAIRED IAW MX RI-52-85-11287 REV A.

Part: IDG — DISCONNECTED (NR 3) · airframe 53,169 hrs · 8,880 cycles

ON TAXI OUT EXPERIENCE EICAS MSG ELEC ISLN 3. PERFORMED QRH PROCEDURE, PROBLEM CLEARED THEN ON TAKEOFF EXPERIENCED PROBLEM AGAIN, DID LOW SPEED REJECTED TAKEOFF, ITEM TRANSFERRED TO MDDR 57619 IAW MEL 24-11-01A. NR 3 IDG DISCONNECTED NORM IAW DDG PROCEDURES PLACARDS INSTALLED DISPATCH NOTIFIED.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 50,660 hrs · 8,399 cycles

BLOCK TURN BACK, REJECTED TAKEOFF LOW SPEED. 2 SEC MAIN DECK FIRE INDICATION. PERFORMED CMC FIRE SYS GND TEST, TEST PASSED. NO STATUS MSGS DISPLAYED IAW AMM 26-14-00-745-021 ALSO PERFORM VISUAL INSPECTION OF ALL MAIN DECK CARGO.

Part: THRUST REVERSER — FAULTED (NR 3 ENGINE) · airframe 50,366 hrs · 8,343 cycles

ENG 3 WOULD NOT SPOOL UP WHEN SETTING TAKEOFF THRUST. TROUBLE SHOT FAULT TO ENG 3 THRUST REVERSER, ITEM TRANSFERRED TO MDDR CL2528 IAW MEL 78-34-01A. CAT C ITEM DUE DATE 26SEP14. PLACARD INSTALLED & MX ACTION COMPLIED WITH.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,700 hrs · 8,023 cycles

CRACK ON THE MAIN DECK CARGO SEAT TRACK BETWEEN STATION 980 & 1000, RBL 75.92. REPAIR SEAT TRACK IAW SRM 53-00-52-2R-13 REV 69.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,700 hrs · 8,023 cycles

CORROSION ANGLE, STATION 1449 KEEL BEAM LOWER SUPPORT. FABRICATE NEW PART IAW EI NO T2014P53B-762 REV 0. REPLACED NEW PART IAW SRM 51-40-02 REV 69.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 48,700 hrs · 8,023 cycles

CORROSION ANGLE, STATION 1287 KEEL BEAM LOWER SUPPORT. FABRICATE NEW PART IAW EI NO T2014P53B-758 REV 0. REPLACED NEW PART IAW SRM 51-40-02 REV 69.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,700 hrs · 8,023 cycles

CORROSION ANGLE, STATION 1427 KEEL BEAM LOWER SUPPORT. FABRICATE NEW PART IAW EI NO T2014P53B-762 REV 0. REPLACED NEW PART IAW SRM 51-40-02 REV 69.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 48,700 hrs · 8,023 cycles

CRACK ON THE MAIN DECK CARGO SEAT TRACK BETWEEN STATION 980 & 1000, RBL 75.92. REPAIR SEAT TRACK IAW SRM 53-00-52-2R-13 REV 69.

Part: PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 48,700 hrs · 8,023 cycles

CORROSION PLATE AT RT WING LE LOWER SIDE, OLES 1545.5. REPLACED DAMAGED PART IAW SRM 51-40-02-06-0 REV 68.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,700 hrs · 8,023 cycles

CORROSION ANGLE, STATION 1405 KEEL BEAM LOWER SUPPORT. FABRICATE NEW PART IAW EI NO T2014P53B-758 REV 0. REPLACED NEW PART IAW SRM 51-40-02 REV 69.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,700 hrs · 8,023 cycles

CORROSION ANGLE, STATION 1308 & STATION 1314, KEEL BEAM LOWER SUPPORT. TTL = 2 EACH, FABRICATE NEW PART IAW EI NO T2014P53B-758 REV 0. REPLACED NEW PART IAW SRM 51-40-02 REV 69.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,701 hrs · 7,622 cycles

TWO EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY M5170 L-1 EMERGENCY LIGHTS OPS NORMAL REF AMM 33-51-04.

Part: FITTING — CRACKED (LT ELEVATOR) · airframe 45,791 hrs · 7,447 cycles

LEFT OTBD ELEVATOR MOST OTBD HINGE FITTING BS 406.8 OTBD SIDE CORNER CRACKED AT SIDE OF T/E BEAM AREA. FITTING REPLACED IAW R1-55-20-10168 REV A.

Part: CARGO TRACK — DAMAGED (BS 885) · airframe 63,316 hrs · 13,379 cycles

DURING C4/A3 CHECK, CHAFE WAS FOUND ON CARGO TRACK IN SECTION 42 AT BS 885, RBL 24.75 IN FWD CARGO BAY. CARGO TRACK WAS REPAIRED IAW SRM 53-00-52-2R-10, REPAIR 10.

Part: CARRIAGE — LACK OF LUBE (RT WING TE FLAP) · airframe 45,544 hrs · 7,398 cycles

RT WING OTBD FLAP, LUBE BOTH INBD AND OTBD MID FLAP CARRIAGES. (LUBED BOTH INBD AND OTBD CARRIAGES OF OTBD FLAP RT WING IAW AMM 12-21-20-643-001.)

Part: LEVER — DAMAGED (RT WING TE FLAP) · airframe 45,544 hrs · 7,398 cycles

RT WING OTBD FORE FLAP TRACK NR 12 ATTACH LEVER ASSY DAMAGED. REMOVED DAMAGED LEVER ASSY LOCATED AND INSTALLED NEW LEVER ASSY IAW COMPONENT MM 57-52-51.

Part: FLAP TRACK — DAMAGED (NR 12 FLAP) · airframe 45,544 hrs · 7,398 cycles

NR 12 FLAP TRACK DAMAGED RT OTBD MID FLAP. NEW TRACK INSTALLED WITH INSTALLATION OF SERVICE MID FLAP ASSY, REF ITEM NR 7 IAW AMM 27-51-04-401.

Part: FLAP — DAMAGED (TE FLAP) · airframe 45,544 hrs · 7,398 cycles

REMOVE RT OTBD MID FLAP DUE TO DAMAGE. REMOVED RT OTBD MID FLAP IAW AMM 27-51-04. INSTALLED SERVICEABLE RT OTBD MID FLAP IAW AMM 27-51-04. OPS CHECK NORMAL IAW MM 27-51-04.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 45,277 hrs · 7,349 cycles

DURING POST FLIGHT WALK-AROUND INSPECTION, PUNCTURE DAMAGE APPROX 4.5" BY 2.5" WAS FOUND ON THE LOWER SURFACE OF THE L/E OF THE RIGHT WING INBD AFT FLAP. PERFORMED A TIME LIMITED REPAIR.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 44,850 hrs · 7,263 cycles

EMERGENCY LIGHTS ON UPPER DECK INOPERATIVE AT BS 410, 587, 550. R & R EMERGENCY BATTERY POWER SUPPLY M 5170. OPS CHECKED OK IAW AMM 33-51-04.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 43,906 hrs · 7,089 cycles

RT WING - INBD T/E FWD FLAP FWD EDGE FOUND DELAMINATED, APPROX 60", TIME LIMITED REPAIRED ACCOMPLISHED IAW EO 4457A424, PART 1.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 43,906 hrs · 7,089 cycles

LT WING INBD T/E FWD FLAP DELAMINATED IN FWD EDGE AREA. TIME LIMITED REPAIRED ACCOMPLISHED IAW EO 4457A424 PART 1.

Part: CLAMP — LOOSE (COOLING DUCT) · airframe 43,609 hrs · 7,029 cycles

EQUIPMENT COOLING EICAS MESSAGE APPEARED ON CLIMB OUT. WENT AWAY IN OVERRIDE POSITION BUT RETURNED IN BOTH STANDBY AND NORMAL MODES DURING CRUISE. (INSPECTION OF MAIN DECK DISTRIBUTION DUCTS CARRIED OUT. FOUND MAIN DUCT CLAMPS LOOSE AND SEPARATED BETWEEN STA 800 AND STA 1250. RESECURED ALL CLAMPS AND DUCTS IAW AMM 21-23-02. ACCOMPLISHED EQUIPMENT COOLING GROUND TEST IAW AMM 21-58-00 AND TEST PASSED. )

Part: RADIO — INOPERATIVE (VHF) · airframe 43,076 hrs · 6,918 cycles

INOPERATIVE LEFT VHF AFTER 5 HOURS IN FLIGHT, STRONG ELECTRICAL ODOR COMING FROM RADIO PANEL. LT SIDE RADIO CONTROL PANEL, AUDIO CONTROL PANEL REMOVED FROM RACK, ALL CONNECTORS AND WIRING HARNESS INSPECTED, NO CHAFED WIRING FOUND AND NO WIRE DAMAGE FOUND. LEFT VHF, ACP AND ASSOCIATED RADIOS CHECKED NORMAL.

Part: SMOKE DETECTOR — FAULTED (MAIN DECK CARGO) · airframe 42,593 hrs · 6,828 cycles

FIRE MAIN DECK AFT AT 1:20 FROM AMS, VERIFIED PHYSICALLY THERE WAS NO FIRE. EICAS FOLLOWED STATUS MESSAGES MAIN DECK CARGO 12 LP A, INDICATING A FALSE WARNING. FOUND MAIN DECK CARGO SMOKE DETECTOR 12A AT FAULT, R & R RT SMOKE DETECTOR 12A IAW AMM 26-14-02, TESTED SATISFACTORY.

Part: FAIRING — DAMAGED (BS 1550) · airframe 41,646 hrs · 6,659 cycles

LT WING TO BODY FAIRING PANEL DAMAGE AT BS 1550. ACCOMPLISHED PART 1 OF EO 4453A671.

Part: DOOR — DAMAGED (NR 4 NACELLE) · airframe 41,396 hrs · 6,615 cycles

DURING MX WALKAROUND FOUND THE NR4 RT ENGINE CORE COWL DOOR SKIRT (MID) FAIRING BENT INWARD, CURLED AND CRACKED IN RADIUS OF BEND. THE LENGTH OF THE DAMAGE EXCEEDS THE SRM LIMITS. REPAIRED DAMAGED.

Part: DOOR — DAMAGED (NR 4 NACELLE) · airframe 41,396 hrs · 6,615 cycles

DURING WALKAROUND INSPECTION, MX FOUND THE NR 4 RT ENGINE CORE COWL DOOR SKIRT (MID) FAIRING BENT INWARD, CURLED AND CRACKED IN RADIUS OF BEND. THE LENGTH OF THE DAMAGE EXCEEDS THE SRM LIMITS. PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; DVI EVERY 5 FLIGHT CYCLES; AND PERMANENT REPAIR WITHIN 75 FLIGHT CYCLES AFTER PART 1.)

Part: SEAL — BROKEN (DESCENT DEVICE) · airframe 40,954 hrs · 6,543 cycles

FOUND 5TH EMERGENCY DESCENT DEVICE SAFETY SEAL BROKEN. (REPLACED 5TH DESCENT DEVICE)

Part: SEAL — BROKEN (DESCENT DEVICE) · airframe 40,954 hrs · 6,543 cycles

FOUND 4TH DESCENT DEVICE SAFETY SEAL BROKEN. (REPLACED DESCENT DEVICE)

Part: SEAL — BROKEN (DESCENT DEVICE) · airframe 40,952 hrs · 6,542 cycles

FOUND 7TH DESCENT DEVICE SAFETY SEAL BROKEN. (REPLACED DESCENT DEVICE)

Part: SEAL — BROKEN (DESCENT DEVICE) · airframe 40,954 hrs · 6,543 cycles

FOUND SECOND DESCENT DEVICE SAFETY SEAL BROKEN. (REPLACED DESCENT DEVICE)

Part: SEAL — BROKEN (DESCENT DEVICE) · airframe 40,954 hrs · 6,543 cycles

FOUND 6TH DESCENT DEVICE SAFETY SEAL BROKEN. (REPLACED DESCENT DEVICE)

Part: HANDLE — DAMAGED (E/E DOOR) · airframe 40,559 hrs · 6,474 cycles

DURING WALKAROUND INSPECTION, MX REPORTED DAMAGE FOUND TO MAIN DECK TO FWD E/E COMPARTMENT ACCESS DOOR HANDLE. REPLACED THE DAMAGED DOOR HANDLE.

Part: SLEEVE — CRACKED (EXHAUST NOZZLE) · airframe 38,130 hrs · 6,063 cycles

DURING MX WALKAROUND, MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR 2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 8" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. (DISPOSITION IS TO STOP DRILL THE ENDS OF THE CRACK WITH A 0.098" DIAMETER HOLE, DVI EVERY 3 FLIGHT CYCLES; AND REMOVAL OF THE PART WITHIN 50 FC (FLIGHT CYCLES).)

Part: STIFFENER — DAMAGED (BS 260) · airframe 37,953 hrs · 6,033 cycles

DURING LOADING OPERATIONS AT ACC THROUGH THE NOSE CARGO DOOR, LOADER DROPPED CAUSING DAMAGE TO BS260, WL195.8 - CANTED BULKHEAD STIFFENERS (2 EA), CONSISTING IN EDGE CRACKS MEASURING 1.5 INCHES LONG (REF FIG 1). DAMAGE TO THE STIFFENERS EXCEEDS THE SRM 53-10-08-1A-2 ALLOWABLE DAMAGE LIMITS. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPETITIVE DVIS AT EVERY 1000 FH (FLIGHT HOURS) AND PERMANENT REPAIR PRIOR TO, OR AT THE NEXT C-CHECK AFTER PART 1 IAW THE SRM 53-00-50, REPAIR 1)

Part: SLEEVE — CRACKED (EXHAUST NOZZLE) · airframe 36,822 hrs · 5,854 cycles

DURING MX WALKAROUND OF MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, APPROX THE 2 O'CLOCK POSITION ON THE NR2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 2.25" LONG AND IS NEAR THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OF THE CRACK IS WITHIN LIMITS, BUT THE EDGE DISTANCE IS OUT OF LIMITS.(DISPOSITION IS TO STOP DRILL THE ENDS OF THE CRACKS WITH A 0.098" DIAMETER HOLE; DVI EVERY 3 FLIGHT CYCLES; AND REMOVAL OF THE PART WITHIN 50 FC (FLIGHT CYCLES).)

Part: SKIN — PUNCTURED (BS 2594 S42L) · airframe 36,460 hrs · 5,798 cycles

DURING JACKING OF ACFT, MX PUNCTURED AN EXISTING REPAIR DOUBLER THROUGH THE UNDERLYING SKIN, LOCATED AT SECTION 48, BS 2594 ABOVE STRINGER 42R TAIL JACK PAD AREA. PUNCTURE MEASURING 5.0 IN. LENGTH X 1.750 WIDTH. DISPOSITION WAS MADE TO PERFORM PERMANENT REPAIR BASED IN THE SRM 53-00-01 FIG 201, REPAIR 11 GUIDELINES. AFTER THE REPAIR DOUBLERS WERE REMOVED, AN ADDITIONAL CRACK WAS FOUND (REF. FIGURE 1 (SHEET 4 OF 6)). THE ORIGINAL DAMAGE/REPAIR FIRST OCCURRED IN 2003 AND A REPAIR WAS INSTALLED, THEN IN 2007, GROUND DAMAGE PUNCTURED THE REPAIR DOUBLERS SO THEY WERE REMOVED REPLACED THEM WITH AN IDENTICAL REPAIR AS THE FIRST REPAIR (REF TLS EO 4453A034 REV A). THE REPAIR ACCOMPLISHED IAW PART 1 OF THIS EO IAW SRM 53-00-01, FIG 201, REPAIR 11 IS A CATEGORY A PERMANENT REPAIR.

Part: COMPRESSOR — STALLED (NR 4 ENGINE) · airframe 35,474 hrs · 5,635 cycles

CLIMBING OUT OF APPROX 3500' NR 4 ENG EMITTED 2 LOUD COMPRESSOR STALLS WITH ASSOCIATED SURGES IN N1, N2 AND EGT. SHUTDOWN NR 4 ENG SHUTDOWN ENG AT APPROX 2210Z. DUE TO SIGNIFICANT COMPRESSOR STALL, ELECTED TO COMPLETE THE "SEVERE ENG DAMAGE CHECKLIST", SO FIRE ENG SWITCH PULLED AS WELL. OIL PRESS NORMAL. AFTER SHUTDOWN UNKNOWN EGT JETTISONED FUEL TO LAND BELOW MAX LANDING WEIGHT. (AFTER BOROSCOPE INSP DAMAGE FOUND AT 14TH STAGE COMPRESSOR BEYOND LIMITS. NR 4 ENG IAW POWERPLANT REMOVAL/INSTALLATION SHEET REV E2023 MAY 10.)

Part: STRUCTURE — CRACKED (RT WING TE FLAP) · airframe 34,727 hrs · 5,518 cycles

DURING A2 CHECK INSP DAMAGE WAS FOUND, RT WING INBD MID FLAPS CRACKED. PERMANENT REPAIRS ACCOMPLISHED IAW THE SRM 51-70-07 PAR 5A. THE REPAIRS ACCOMPLISHED IAW PART 1 ARE CATEGORY A AND WERE PERFORMED IAW SRM 51-70-07 PARA 5A.

Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 34,727 hrs · 5,518 cycles

RT WING INBD MID FLAP MOST OTBD T/E FOUND CRACKED (RT WING INBD MID FLAP MOST OTBD T/E LWR SURFACE COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A. DETAIL REF HX PROCESS CARD SEQ NT EAX 500294-1)

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 34,727 hrs · 5,518 cycles

LT WING INBD MID FLAP MOST OTBD T/E FOUND CRACKED. (LT WING INBD MID FLAP MOST OTBD T/E LWR SURFACE COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A. DETAIL REF HX PROCESS CARD SEQ NR EAX 500344-1).

Part: DOOR — DAMAGED (A/C BAY) · airframe 30,665 hrs · 4,903 cycles

DURING WALK AROUND INSP BEING PERFORMED; GROUND DAMAGE FOUND ON THE BS 1112.1, BS 1170 AIR CONDITIONING ACCESS DOOR 192 HR. THE DAMAGE PENETRATED THROUGH THE HONEYCOMB MATERIAL (REF FIG 1)(PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS. SCHEDULE PART 2 PRIOR TO THE ACCUMULATION OF 5FC IN ACC WITH THE SRM 51-70-19 FIG 1. TYPICAL TIME LIMITED REPAIR WITH A METAL OVERLAY ON COMPOSITE PANELS. INITIATE REPEAT DVI AT EVERY A-CHECK. A PERMANENT REPAIR IAW THE SRM 53-00-70 FIG 201, REPAIR 1, TABLE 1 WILL BE ACCOMPLISHED AT THE NEXT C-CHECK.)

Part: DOOR — DAMAGED (AIR CON BAY) · airframe 30,665 hrs · 4,903 cycles

EO 4453A264: GROUND DAMAGE FOUND ON THE BS 1112.1-1170 AIR CONDITIONING ACCESS DOOR 192 HR. THE DAMAGE PENETRATED THROUGH THE HONEYCOMB MATERIAL. (PERFORMED A TIME LIMITED REPAIR AS DESCIBED IN PART 1 WORK INSTRUCTIONS. SCHEDULE PART 2 PRIOR TO THE ACCUMULATION OF 5 FC IAW THE SRM 51-70-19 FIG 1. TYPICAL TIME REPAIR WITH A METAL OVERLAY ON COMPSITE PANELS. REPEAT DVI AT EVERY A-CHECK. )

Part: DOOR — DAMAGED (A/C BAY) · airframe 30,665 hrs · 4,903 cycles

GROUND DAMAGE FOUND ON THE BS 1112.1 - 1170 AIR CONDITIONING ACCESS DOOR 192HR. THE DAMAGE PENETRATED THROUGH THE HONEYCOMB MATERIAL (REF FIG 1.) "TIME LIMITED REPAIR IAW PART 1 WORK INSTRUCTIONS. SCHEDULE PART 2 PRIOR TO THE ACCUMULATION OF 5 CYCLES IN ACC WITH THE SRM 51-70-19. TYPICAL TIME LIMITED REPAIR WITH A METAL OVERLAY ON COMPOSITE PANELS INITIATE REPEAT DVIS EVERY A CHECK. A PERMANENT REPAIR IN ACC WITH SRM 53-00-70, FIG 201, REPAIR TABLE 1 WILL BE ACCOMPLISHED AT THE NEXT C-CHECK."

Part: ACM — FAILED (NR 3) · airframe 30,072 hrs · 4,803 cycles

AIR TURN BACK, AFTER TAKEOFF UNABLE TO MAINTAIN CABIN PRESSURE DURING CLIMB. NR 1 PACK ON MEL AND NR 3 PACK FAILED DURING CLIMB. NR 2 PACK WAS UNABLE TO MAINTAIN PRESSURE. REPLACED NR 3 ACM, PERFORMED OPS CHECK, ALL NORMAL.

Part: SUPPORT — DAMAGED · airframe 29,916 hrs · 4,778 cycles

THE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C CHECK INSPECTION BEING PERFORMED AT HKG; DAMAGE WAS FOUND TO THE LEFT I/B UPPER TRAILING EDGE FIXED PANEL O/B SUPPORT WEB (REFERENCE FIGURE 1). PERMANENT REPAIR PERFORMED IN ACCORDANCE WITH THE 747-400F SRM 51-70-13 FIGURE 201, REPAIR 1.

Part: SUPPORT — DAMAGED (TE FLAP) · airframe 29,916 hrs · 4,778 cycles

THE PURPOSE OF THIS EO IS TO RECORD A MAJOR REPAIR. DURING C CHECK INSPECTION BEING PERFORMED AT HKG; DAMAGE WAS FOUND TO THE RIGHT O/B MID FLAP NR 3 TRAILING EDGE PANEL SUPPORT (I/B OF NR 8 CARRIAGE) CONSISTING OF A SCREW HOLE ELONGATED (REFERENCE FIGURE 1). PERMANENT REPAIR PERFORMED IN ACCORDANCE WITH THE 747-400F SRM 51-70-15, FIGURE 5.

Part: CIRCUIT CARD — FAILED (FIRE WARNING)

MASTER CAUTION/ FIRE WARNING BELL ON GROUND. NO EICAS MESSAGE (NO OTHER LIGHTS OR WARNINGS). REPLACED A15 CARD AT THE M5206 MODULE. OPS CHECKED OK. (S)

Part: FIRE WARNING — FALSE ACTIVATION

REF: LOG PAGE 362049; TWICE DURING CRUISE, MOMENTARY ILLUMINATION OF MASTER WARNING LIGHTS WITH ASSOCIATED FIRE WARNING BELL. NO EICAS MESSAGE. ACCOMPLISHED CMC GROUND TEST FIRE PROTECTION SYSTEM. (TEST PASS) NO FAULTS IN CMC FAULT HISTORY, MM26-10-00. (K)

Part: SKIN — DAMAGED (BS 166 S46R) · airframe 24,491 hrs · 3,926 cycles

FOUND LIGHTNING STRIKE AT STATION 166 STRINGER 46R. REPAIRED AS PER SRM 53-00-01 FIGURE 201 REPAIR 1 AND AS PER BOEING MESSAGE 1-764547003-7 AND FAA FORM 8100-9.

Part: LUG — CHAFED (NR 1 PYLON) · airframe 24,491 hrs · 3,926 cycles

DURING SCHEDULED MAINTENANCE FOUND NR 1 PYLON WEAR DAMAGE ON THE LUG FACE OF THE UNDERWING MIDSPAR FITTINGS. THE DAMAGE WAS REMOVED FROM THE LUG SURFACES BY BLENDING SMOOTH. THE FITTINGS WERE CONFIRMED FREE OF CRACKS AND OTHER DAMAGE BY DETAIL VISUAL AND NDT INSPECTION. AS PER BOEING MESSAGE 1-760110158-5 AND FAA 8100-9.

Part: FITTING — CHAFED (NR 4 PYLON) · airframe 24,491 hrs · 3,926 cycles

DURING SCHEDULED MAINTENANCE, FOUND NR 4 PYLON WEAR DAMAGE ON THE LUG FACE OF THE UNDERWING MIDSPAR FITTINGS. THE DAMAGE WAS REMOVED FROM THE LUG SURFACES BY BLENDING SMOOTH. THE FITTINGS WERE CONFIRMED FREE OF CRACKS AND OTHER DAMAGE BY DETAIL VISUAL AND NDT INSPECTION. AS PER BOEING MESSAGE 1-760110158-5 AND FAA 8100-9.

Part: SKIN — SCRATCHED (BS 2200 S22-23L) · airframe 24,491 hrs · 3,926 cycles

FOUND NICK ON FUSELAGE SKIN STATION 2200 STRINGER 22L-23L. REPAIRED AS PER SRM 53-00-01 REPAIR 1 DETAIL 3 FIGURE 201 AND 53-60-01 FIGURE 1 AND SRM 51-40-06 FIGURE 3

Part: FLOOR SUPPORT — CRACKED (BS 531-688) · airframe 24,491 hrs · 3,926 cycles

MAIN DECK CARGO COMPARTMENT FLOOR PANEL SUPPORT CRACKED AT STATION 531 AND 688 RBL 116. REPAIRED FLOOR PANEL SUPPORT AS PER BOEING DOCUMENT RDR 0691225-1 TO 5.

Part: SKIN — SCRATCHED (BS 1790 S38-39L) · airframe 24,491 hrs · 3,926 cycles

SCRATCH ON FUSELAGE SKIN AT STATION 1790 BETWEEN STRINGER 38L-39L. INSPECTED AS PER SRM 51-10-02. REPAIRED AS PER SRM 53-00-01 REPAIR 1 FIGURE 201.

Part: SKIN — CRACKED (LT WING) · airframe 23,147 hrs · 3,705 cycles

DURING LEFT WING LIGHT REPLACEMENT THE PLATFORM SUDDENLY LOWERED AND HIT THE LEADING EDGE SKIN. THE PLATFORM MOVEMENT CAUSED A 15 INCH VERTICAL CRACK. A TIME LIMITED REPAIR WAS ACCOMPLISHED AS PER XEO 57-101007 PART 1 AND SRM 57-41-01 REPAIR 4. PERMANENT REPAIR IS TO BE ACCOMPLISHED WITHIN 6 MONTH. NO ADDITIONAL DAMAGE FOUND.

Part: INTERCOSTAL — CRACKED (BS 1787-1795) · airframe 18,612 hrs · 3,001 cycles

A/C M415MC: PERFORMED INTERIM REPAIR TO MAIN DECK SIDE CARGO DOOR INTERCOSTAL CUT-OUT IAW XEO 52-102106, A/C OK FOR CONTINUED OPERATIONS FOR UP TO 6 FLIGHT CYCLES. INTERCOSTAL CUT-OUT WEB REPAIRED IAW SRM 51-70-13 REPAIR FIG 201.

Part: SEAT TRACK — CRACKED (BS 560) · airframe 18,006 hrs · 2,910 cycles

N415MC AT PIK FOR MSG-3, CHECK C-4 & A-4. AS PER N/ROUTINE 163 FWD CARGO SEAT TRACK AT BS 560 LBL 45.5 HAS 6 INCH CRACK AND N/ROUTINE 188 FWD CARGO SEAT TRACK AT BS 560, LBL 25 HAS TWO HOLES. NR 4453A083 WAS GENERATED. FOR N/ROUTINE 163 REPAIR ACCOMPLISHED AT FWD CARGO SEAT TRACK BS 560 LBL 45.5 AS PER 747-400 SRM 53-00-52 FIG 201, REPAIR NR 10. FOR N/ROUTINE NR 188, REPAIR ACCOMPLISHED AT FWD CARGO SEAT TRACK BS 560 LBL 25.0 AS PER 747-400, SRM 53-00-52, FIG 201, REPAIR NR 10.

Part: SHIM — MIGRATED (CARGO DOOR HINGE) · airframe 18,006 hrs · 2,910 cycles

N415MC AT PIK FOR MSG-3 CHECK C-4 & A-4. AS PER N/ROUTINES 168, 169 AND 210, AFT AND FWD CARGO DOORS HINGE SHIMS MIGRATED. XEO 53-082906 WAS GENERATED. REPAIR ACCOMPLISHED TO THE AFT & FWD CARGO DOOR HINGE SHIMS MIGRATION AS PER SRM 51-20-08 AND 50 PERCENT TORQUE CHECKED ON THE FASTENERS AS PER AMM 52-34-08. REPEAT INSPECTION ON EVERY 2A CHECK. PERMANENT REPAIR AT NEXT C-CHECK. MIGRATED SHIMS TO BE REPLACED WITH SOLID 7075-T6 SHIMS (REF IPC 52-34-08-05) AS PER SRM 51-20-08 PARA 5.

Part: SKIN — CORRODED (LT WING) · airframe 18,006 hrs · 2,910 cycles

N415MC AT PIK FOR MSG-3 CHECK C-4 & A-4. AS PER N/ROUTINE 105 LEFT WING UPPER SURFACE WS 752-779 FIVE BLENDED & RESURFACED AREAS ON THE OUTER AREA. FWD MOST DEPTH TO BE CHECKED. FWD BLEND OUT CHECKED BETWEEN WS 752 - WS 779. MAX DEPTH OF BLEND OUT = 0.017 AND IS WITHIN ALLOWABLE MAX DEPTH AFTER CLEANED UP = 0.067 AS PER SRM 57-20-01.

Part: FAN BLADE — LACK OF LUBE (NR 1 ENGINE) · airframe 18,006 hrs · 2,910 cycles

N415MC AT PIK FOR MSG-3, C-4&A-4 CHECK. AS PER N/ROUTINE 154, NR 1 ENGINE S/N 704-916 FAN BLADES REMOVED FOR LUBRICATION. IT WAS FOUND, FAN DISKS HAVE NO EVIDENCE OF LUBRICANT. INSPECTION PERFORMED IAW MM 72-31-00, 206 TABLE 601 NR 1 DOVETAILS ON FAN DISK HAVE COATING MISSING ON PRESSURE FACES. (CU-NI-INDIUM) ALSO PER ENGINE SHOP MANUAL SUBTASK 72-21-03, 220-054 SECTION-C FRETTING ON PRESSURE FACES. THIS REQUIRES INSPECTION BY ENGINE SHOP WITH APPROPRIATE TOOLING FOR DEEP DISK INSPECTION.

Part: LEVER — BROKEN (NR 4 ENGINE) · airframe 16,673 hrs · 2,702 cycles

SEVERE COMPRESSOR STALL ON ENGINE NR 4 WITH FULL CLIMB POWER AT 6000 FEET ON CLIMBOUT FROM DXB. ENGINE NR 4 ROLLED BACK TO IDLE, OVERTEMP EGT INDICATION. NR 4 ENGINE SHUT DOWN. FUEL JETTISON ACCOMPLISHED. UNEVENTFUL SMOOTH AUTO LAND RWY 30R AT 299.0 TONS. NR 4 ENGINE REMOVED AND REPLACED AS PER WORK CARD A717101GTI & AMM 71-00-00. ENGINE RUN CARRIED OUT. ENGINE USED 1000KG FUEL. ALL SATISFIED. FOUND 5TH STAGE LEVER ARM BROKEN.

Part: SKIN — BIRD STRIKE (RT LE FLAP)

RIGHT INBOARD FLAP FOREFLAP DAMAGE. BIRD STRIKE ON RIGHT WING L/E FLAPS. PERFORMED INSPECTION PER MM 5-51-14, FOUND RIGHT INBOARD FLAP FOREFLAP DAMAGED OUT OF SRM LIMITS. REMOVED FLAP AND REPAIRED IAW SRM 51-70-07 AND MM 57-52-31. INSTALLED FLAP AS EPR MM 27-51-02. (M)