N409MC

BOEING 747-47UF None injury Part 121 — ATLAS AIR INC

ATA 2397

LEFT/RIGHT HF WILL NOT TRANSMIT. R & R RT & LT HF COUPLER PER AMM 23-11-03 & AIPC 23-11-03-05A. OPS CHK OK. L

ATA 5330

FUSELAGE STA 162, STR 23L-24L FOUND LIGHTNING STRIKE AS MARKED. FUSELAGE STA 162, STR 23L-24L LIGHTNING STRIKE REPAIRED AS PER B747-400F SRM 53-00-01 REPAIR 9 REV.103. NO FURTHER DEFECTS NOTED.

ATA 5347

MAIN DECK CARGO SEAT TRACK FOUND CORROSION BETWEEN STA 1580 AND STA 1600, RBL 11.33(<P>MAIN DECK CARGO SEAT TRACK REPAIRED AS PER EN #3096-25 REV.0 AND B747-400F SRM 53-00-52 REPAIR 12 REV.103. NO FURTHER DEFECTS NOTED.<!--ENDFRAGMENT--></P>)

ATA 5340

LH BLG INBOARD TRUNNION VERTICAL SUPPORT FITTING I/B AND O/B SIDE FACE FOUND GOUGE MARK. LH BLG INBOARD TRUNNION VERTICAL SUPPORT FITTING I/B AND O/B SIDE FACE MACHINED AS PER B747-400F SRM 53-40-90 REPAIR 1 REV. 103 AND FOUND WITHIN WORK LIMIT. FOR DETAILS REFER TO EO 4453C541_CS. NO FURTHER DEFECTS NOTED.

ATA 5330

FUSELAGE STA 154, STR 20R - 22R FOUND LIGHTNING STRIKE AS MARKED. FUSELAGE STA 154, STR 20R - 22R LIGHTNING STRIKE REPAIRED AS PER B747-400F SRM 53-00-01 REPAIR 9 REV.103. NO FURTHER DEFECTS NOTED.

ATA 5347

MAIN DECK CARGO SEAT TRACK, FOUND CORROSION BETWEEN STA 1000 AND STA 1020, LBL 11.33. MAIN DECK CARGO SEAT TRACK REPAIRED AS PER EN# 3071-25 REV.0. NO FURTHER DEFECTS NOTED.<!--ENDFRAGMENT--></P>)

ATA 5314

RH BODY GEAR W/W KEEL BEAM UPPER SURFACE AT STA 1472, 1444 AND 1425 FOUND SURFACE CORROSION AS MARKED.(<P><!--STARTFRAGMENT-->RH BODY GEAR W/W KEEL BEAM UPPER SURFACE AT STA 1472, 1444 AND 1425 SURFACE CORROSION REPAIRED PER&NBSP;<SPAN>EN# 3072-25 REV.0.</SPAN><SPAN> ACCOMPLISHED EN# 3072-25 REV.0. NO FURTHER DEFECTS NOTED.</SPAN></P>)

ATA 5314

LH BODY GEAR W/W KEEL BEAM UPPER SURFACE AT STA 1458, 1437 AND 1427 FOUND SURFACE CORROSION AS MARKED. LH BODY GEAR W/W KEEL BEAM UPPER SURFACE AT STA 1458, 1437 AND 1427 SURFACE CORROSION REPAIRED PER EN# 3072-25 REV.0. ACCOMPLISHED AS PER EN# 3072-25 REV.0. NO FURTHER DEFECTS NOTED.

ATA 5330

FUSELAGE STA 493, STR L27A - L28A FOUND LIGHTNING STRIKE AS MARKED. FUSELAGE STA 493, STR L27A - L28A LIGHTNING STRIKE REPAIRED AS PER B747-400F SRM 53-00-01 REPAIR 9 REV.103. NO FUTHER DEFECT NOTED.

ATA 5310

RH BODY GEAR W/W FIXED PANEL INNER SURFACE, JUST BELOW APU FIRE SHUT OFF MODULE. FOUND SURFACE CORROSION. RH BODY GEAR W/W FIXED PANEL INNER SURFACE JUST BELOW APU FIRE SHUT OFF MODULE SURFACE CORROSION FOUND OUT OF LIMITS AS PER B747-400F SRM 53-00-71-1A-1 REV. 103 AND FABRICATED NEW PANEL (65B10925-146) AS PER SMAL REQUEST NO: 271120012 AND BOEING DRAWING 65B10925 SHEET 17 REV.F. NO FURTHER DEFECTS NOTED.

ATA 5343

STA 1480 RH BLG INBOARD TRUNNION VERTICAL SUPPORT FITTING 65B10595-62 THE TOOL MARK BLENDOUT AND THE GROOVED HOLE DAMAGED. REQUEST FOR PERMANENT REPAIR INSTRUCTIONS.(<P>STA 1480 RH BLG INBOARD TRUNNION VERTICAL SUPPORT FITTING 65B10595-62 THE TOOL MARK BLENDOUT AND THE GROOVED HOLE REPAIRED AS PER EN #3077-25 REV.0. NO FURTHER DEFECTS NOTED.<!--ENDFRAGMENT--></P>)

ATA 5343

L/H BLG INBD TRUNNION CAP FITTING HAS PITTING CORROSION.(<P>REMOVED CORROSION AS PER SRM 53-40-90-2R-1. PERFORMED NDI AS PER NDTM 51-00-00-PART 6 &AMP; SOPM 20-20-02. REMOVED ADDITIONAL CORROSION AND PERFORMED NDI &AMP; DVI. APPLIED ALODINE, PRIMER, ENAMEL AND SEALANT AS PER BOEING SR TLS-TLS-24-0828-01C. EO 4453C541. NO FURTHER DEFECTS NOTED</P>)

ATA 5343

R/H BLG INBOARD TRUNNION SUPPORT BEAM TOOL MARK DAMAGED.(<P>REMOVED TOOL MARK AS PER SRM 51-20-01. PERFORMED NDI AS PER 747 NDTM 51-00-00-PART 6 PART 4. CLEANED THE HOLES AND APPLIED ALODINE &AMP; PRIMER AS PER SOPM 20-41-02, SRM 51-20-01, BOEING SR TLS-TLS-24-0838-03B AND EO 4453C542. NO FURTHER DEFECTS NOTED</P>)

ATA 5343

R/H BLG INBD TRUNNION CAP FITTING HAS PITTING CORROSION.(<P>REMOVED CORROSION AS PER SRM 53-40-90-2R-1. PERFORMED NDI AS PER NDTM 51-00-00-PART 6 &AMP; SOPM 20-20-02. REMOVED ADDITIONAL CORROSION AND PERFORMED NDI &AMP; DVI. APPLIED ALODINE, PRIMER, ENAMEL AND SEALANT AS PER BOEING SR TLS-TLS-24-0828-01C. EO 4453C541. NO FURTHER DEFECTS NOTED</P>)

ATA 2910

HYD QTY LOW 4  EICAS MESSAGE(<P>ITEM 1: FOUND ACCUMULATOR ISOLATION VALVE UPPER BLANK AND LOOSE, TIGHTENED 1 TURN IAW AMM 20-51-01 (FOR SOURCE SELECTOR 1 VALVE).&NBSP; ITEM 4: LEAK CHECK C/W AND FAILED. ITEM 7: FOUND O-RING ON TOP PLUG OF ACCUMULATOR VALVE DAMAGED, REPLACED AND LEAK CHECK GOOD.</P>)

ATA 5700

RIGHT WING FIXED TRAILING EDGE GROUND SPOILER AT STA 432.65 SUPPORT RIB STRUCTURE END CORRODED AND METAL PEELING(<P>REPLACED CHORD ON R/H WING STA. 432.65 RIB STRUCTURE IAW EO 4457A169. NO FURTHER DEFECTS NOTED.&NBSP;</P>)

ATA 5300

DEVIATION - FOUND STA 720 RH FRAME WITH TENSION AREA CONFIGURATION MISMATCH WITH THE PRODUCTION DRAWING(<P>1) PERFORM EI T2023A53M-718 REV 1. 2) ACCOMPLISH EI T2023A53M-718 REV 2 AND THIS EI ATTACHING WITH T/C 8122637. 3) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

ATA 3350

FOUND MANY EMERGENCY LIGHT TEST FAIL, EQUIPMENT #L1832, M4915, M4914, X325, X326, L5731, L5732, L5767, L5734 & L1854(<P>1) IAW AMM 33-51-04-902-001-001 REV 107, 33-51-04-002-009-001 REV 107 &AMP; 33-51-04-402-012-001 REV 107, REPLACED BATTERIES AND POWER SUPPLY AND PERFORMED INSTALLATION TEST, THE RESULT WAS GOOD. SN: 108875, 72047 &AMP; 49417. PN: 2013-1A &AMP; 2012-1</P>)

ATA 2300

FOUND ELT TEST FAIL, TRANSMITTER LED INDICATOR NOT BLANK DURING SELF-TEST AND TX MODE TEST(<P>1) IAW DWG AR320-0011-00 REV -, DWG ES-105-1 REV D &AMP; SWPM 20-10-12 REV 82 REPLACED ELT COAX CABLE AND CONDITION CHECK NORMAL. 3) CUSTOMER ISSUED EO 4423A157 FOR REPLACING THE NEW TYPE ELT AND PERFORMED CABLE TEST, W/O 8085707 CLOSE</P>)

ATA 5700

CORROSION - SKIN LH WLG W/W FWD BHD ADJACENT OVERRIDE / JETTISON PUMP CTR TANK - LH M224(<P>1) BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A57M-723 SEQUENCE A REV 0. 3) ACCOMPLISHED EI T2023A57M-723 REV 1. 4) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5300

DEVIATION - FOUND STA  720 LH FRAME WITH TENSION AREA CONFIGURATION  MISMATCH WITH THE PRODUCTION DRAWING(<P>1) PERFORM EI T2023A53M-969 REV 0. 2) ACCOMPLISH EI T2023A53M-969 REV 1. 3) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

ATA 5300

CRACK - PERFORM TENSION TIES AND FRAME INSPECTION FINDING ONE HOLE CRACK AT RHS STA 720 FOR FRAME AREA(<P>1) ACCOMPLISHED THE EI T2023A53M-718 REV 0. 2) ACCOMPLISH EI T2023A53M-718 REV 2. 3) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

ATA 5300

CORROSION - SKIN RH WLG NW FWD BHD ADJACENT OVERRIDE / JETTISON PUMP CTR TANK RH M225(<P>1) BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A57M-728 SEQUENCE A REV 0. 3) ACCOMPLISHED EI T2023A57M-728 REV 1. 4) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5300

CORROSION - INTERCOSTAL AFTER CGO COMPARTMENT LOWER AREA AT STA 1970 S-38R(<P>1) REMOVE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97. 2) INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 97 AND DWG 65B04652 SH 2 REV D, 146U1961 SH 156 REV C, 146U1961 SH 157 REV C. 3) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5200

FOUND EXISTING REPAIR DOUBLER ON FWD CGO DOOR FWD LWR CORNER(<P>1. REMOVE EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV 97. 2. REPAIR DAMAGE AREA IAW SRM 52-30-01-2R-2 DETAIL IV REV 97. 3. INSTALL FASTENERS IAW SRM 51-40-02-0G-0 REV 97. 4. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

ATA 5300

CRACK WAS FOUND ON STA 1000 FRONT SPAR BULKHEAD LBL 57.50 SHEAR TIE(<P>1) REMOVED THE DAMAGE PART IAW SRM 51-40-02-0G-0 REV 97. 2) INSTALL NEW PART IAW SRM 51-40-02-0G-0 REV 97 &AMP; EO 4453C24 PART 5 REV 3. 3) PERFORM EI T2023A53M-620 REV 0. 4) ACCOMPLISHED IAW EI T2023A53M-620 REV 1. 5) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5300

FOUND EXISTING REPAIR DOUBLER ON FUSELAGE SKIN AT STA 1920 TO STA 1940 BETWEEN S-31R TO S-34R(<P>1) REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-40-02-0G-0 REV 97. 2) PERFORM EI T2023A53M-724 SEQUENCE A REV 0. 3) PERFORMED EI T2023A53M-724 REV 1 SEQUENCE B. 4) ACCOMPLISHED IAW EI T2023A53M-724 REV 2. 5) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5300

FOUND EXISTING REPAIR DOUBLER ON FUSELAGE SKIN AT STA 1940 TO STA 1960 BETWEEN S-48R TO S-50R(<P>1) REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-40-02-0G-0 REV 97. 2) PERFORM EI T2023A53M-722 SEQUENCE A REV 0. 3) PERFORM EI T2023A53M-722 SEQUENCE B REV 1. 4) ACCOMPLISHED IAW EI T2023A53M-722 REV 2. 5) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5700

DELAMINATION - WEDGE ASSY, RH WING INBD AILERON T/E OUTBD SIDE AREA(<P>1) PERFORM REPAIR OF DELAMINATION DAMAGE FOUND ON RH WING INBD AILERON T/E OUTBD SIDE, PLEASE REFER TO THE JOB CARD ATTACHING SHEET FOR THE DETAILED REWORK INFORMATION. 2) CONDITION CHECK GOOD</P>)

ATA 5300

FOUND SLOT CUTOUT AREA CORROSION AT STA 2154 LBL 11.33 SEAT TRACK(<P>1) REMOVED THE AFFECTED FASTENERS IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M-782 REV 0. 3) REINSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 97 &AMP; DWG 65B28253, SHEET 55 REV A, SHEET 54 REV -, 65B38253, SHEET 53 REV -, SHEET 52 REV A. 4) ACCOMPLISHED EI T2023A53M-782 REV 1. 5) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5300

FOUND M/D FLOOR STRUCTURE CORROSION AT STA 2040 RBL 85(<P>1) REMOVED THE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M-754 REV 0. 3) REINSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 97 &AMP; DWG 6538102 SHEET 10 REV - , SHEET 11 REV A. 4) ACCOMPLISHED EI T2023A53M-754 REV 1. 5) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5300

FOUND FLOOR BEAM CORROSION AT STA 986 LBL 85(<P>1) REMOVED THE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M-798 REV 0. 3) REINSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 97 &AMP; DWG 65B28049, SHEET 13 REV A. 4) ACCOMPLISHED EI T2023A53M-798 REV 1. 5) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5300

CRACK DAMAGE ON STRAP OF STA 2231 AT S-16L(<P>1) REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV 97. 2) PERFORMED EI T2023A53M-746 REV 1 SEQUENCE B AND SEQUENCE A AND DWG 65B04-35 SH 13 REV D. 3) ACCOMPLISHED EI T2023A53M-746 REV 2. 4) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

ATA 5300

FOUND SEAT TRACK CORROSION AT STA 1015 & 1035 LBL 98.58(<P>1) REMOVED AFFECTED FASTENER TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M-799 REV 0. 3) REINSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 97 AND DWG 111U0805 SHEET 2 REV 3, SHEET 3 REV D, SHEET 4 REV G, 4) ACCOMPLISHED EI T2023A53M-799 REV 1. 5) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

ATA 5300

FOUND SEAT TRACK CORROSION AT STA 1095 - 1135 LBL 98.58(<P>1) REMOVED AFFECTED FASTNERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M-799 REV O (EI ATTACH W/O 8116606 (628)). 3) REINSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 97 &AMP; DWG 111U805 SHEET 2 REV E, SHEET 3 REV D, SHEET 4 REV G</P>)

ATA 5300

FOUND SEAT TRACK CORROSION AT STA 984 LBL 98.58(<P>1) REMOVED AFFECTED FASTENERS TO GET ACCES IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M &AMP; DWG 65B16004 SHEET 4 REV -, 65B16038 SHEET 1 REV D, 65B38250 SHEET 17 REV A, SHEET 4 REV -, SHEET 18 REV -, SHEET 19 REV -, SHEET 20 REV -. 4) ACCOMPLISHED T2023A53M-749 REV 1. 5) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5300

FOUND M/D FLOOR STRUCTURE CORROSION AT STA 2220 LBL 29(<P>1) REMOVED THE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M-748 REV 0. 3) REINSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 97 AND DWG 65B38111 SHEET 1 REV E, SHEET 7 REV B, SHEET 9 REV -,. 4) ACCOMPLISHED EI T2023A53M-748 REV 1. 5) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5200

FOUND EXISTING REPAIR DOUBLER ON THE AFT CGO DOOR AFT CORNER(<P>1) REMOVE EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV 97. 2) PERFORM EI T2023A52M-734 REV 1. 3) ACCOMPLISHED EI T2023A52M-734 REV 2. 4) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5300

FOUND M/D SEAT TRACK CORROSION AT STA 2220 RBL 33(<P>1) REMOVED THE AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 97. 2) ACCOMPLISHED EI T2023A53M-750 REV 0. 3) REINSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV 97 AND DWG 65B38251 SHEET 62 REV A, SHEET 33 REV -, SHEET 74 REV A. 4) ACCOMPLISHED EI T2023A53M-750 REV 1. 5) JOB COMPLETED AND CONDITION CHECK NORMAL</P>)

ATA 5230

FOUND EXISTING REPAIR DOUBLER ON NOSE CGO DOOR AT STA 180 BETWEEN S-45L AND BL 0(<P>1) REMOVE EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV 97. 2) PERFORM EI T2023A52M-752 REV 0, T2023A52M-730 REV 0 AND T2023A52M-740 REV 1. 3) ACCOMPLISHED EI T2023A52M-752 REV 1, T2023A52M-730 AND T2023A52M-740 REV 2. 4) CONDITION CHECK NORMAL AND JOB COMPLETED</P>)

ATA 3445

TCAS STATUS MESSAGE (REMOVED AND REPLACED TCAS COMPUTER AND TCAS LOWER ANTENNA IAW AMM 34-45-01 AND 34-45-02 BOTH OPS CHECKED& GOOD</P>)

ATA 7200

AFTER TAKEOFF RECEIVED A OVHT ENG 2 NAC EICAS MESSAGE FOLLOWED BY FIRE ENG 2 EICAS AND ALARMS(<P>INSPECTION FOUND 14TH STAGE HIGH PRESS MANIFOLD AT 3 O'CLOCK SEPARATED CAUSING HEAT DAMAGES TO NUMEROUS WIRES, HARNESS AND INSIDE OF RH TR COWL. REMOVED AND REPLACED ENGINE 2 IAW B747-400 AMM 71-00-00, 71-00-02</P> / <P>&NBSP;</P>)

ATA 5411

NO.2 ENG L/H CORE COWL NO.2 FRAME (COUNT FROM AFT) FOUND CHAFING BY HOLDING ROD.(<P>NO.2 ENG LH CORE COWL NO.2 FRAME CHAFED AREA REPAIRED AS PER SRM 54-45-02-2R-1 FIG 201.</P>)

ATA 5350

FX LH BODY FAIRING 191KL UPPER SUPPORT BEAM AT STA 1240 LWR EDGE FOUND CRACKED(<P>FX LH BODY FAIRING 191KL UPPER SUPPORT BEAM AT STA 1240 LWR EDGE REPAIRED AS PER RI NO: RI-53-00-14343 REV.A</P>)

ATA 5754

FOUND DENT AT NO.14 KRUEGER FLAP(<P>PERFORMED PERMANENT COMPOSITE REPAIR IAW&NBSP;<SPAN>SRM 51-70-07 PAR.5A</SPAN></P>)

ATA 5753

LHW I/B FORE FLAP MID LWR PNL MID AREA 1EA EXISTING REPAIR PATCH DISBOND AS MARK.(<P>PERFORMED PERMANENT METAL TO HOT BOND REPAIR AT LHW I/R FORE FLAP MID LWR PNL MID AREA DISBOND REPAIR PATCH AREA AS PER SRM 51-70-10 REPAIR 4 FIG 201 AND REFER TO HX PROCESS CARD SEQUENCE NO: XKE510283-01 FOR REPAIR DETAILS.</P>)

ATA 5753

LHW O/B MID FLAP L/E FAIRING FOUND DELAMINATED(<P>PERFORMED PERMANENT COMPOSITE HOT BOND REPAIR</P>)

ATA 5753

LHW O/B MID FLAP L/E FAIRING FOUND PUNCTURE(<P>PERFORMED PERMANENT COMPOSITE REPAIR</P>)

ATA 5347

M/D - STA 2180 TO 2200 RBL 11 BELOW SEAT TRACK SLOT HOLE FOUND CORROSION CRACK.(<P>M/D - STA 2150-2210 RBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12.</P>)

ATA 5347

M/D - STA 960 TO 980 RBL 11 BELOW SEAT TRACK SLOT HOLE FOUND CORROSION.(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 CHECKED WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.</P>)

ATA 5347

M/D - STA 1980 TO 2000 RBL 11 SEAT TRACK SLOT HOLE FOUND CORROSION.(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-10-01. CHECKED WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.</P>)

ATA 5347

M/D - STA 1480 TO 1500 LBL 33 SEAT TRACK R/H FLANGE FOUND CORROSION.(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 AND CHECKED WITHIN SRM 53-0-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.</P>)

ATA 5347

M/D - STA 1480 TO 1500 RBL 11 SEAT TRACK L/H FLANGE FOUND CORROSION.(<P>CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND 51-20-01 AND CHECKED WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.</P>)

ATA 5411

NO.2 ENG L/H CORE COWL AFT FRAME MID AND LOWER CLEARANCE HOLE FOUND 2EA CHAFING MARK.(<P>NO.2 ENG LH CORE COWL AFT FRAME MID AND LOWER CLEARANCE HOLE CHAFED AREA REPAIRED AS PER SRM 54-45-01-2R-10 REPAIR 10.</P>)

ATA 5411

NO.1 ENG L/H CORE COWL AFT FRAME FOUND TWO DAMAGE AS RED MARK.(<P>NO.1 ENG LH CORE COWL AFT FRAME DAMAGED AREA REPAIRED AS PER SRM 54-45-01-2R-10 REPAIR 10.</P>)

ATA 5347

M/D - STA 1620 TO 1650 LBL 11 SEAL TRACK SLOT HOLE FOUND ELONGATED.(<P>M/D - STA 1530-1670 LBL 11 SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201.</P>)

ATA 5347

M/D - STA 1480 TO 1500 RBL 33 SEAT TRACK L/H FLANGE FOUND CORROSION(<P>M/D - STA 1480-1550 RBL 33 CORROSION DAMAGED SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-6 REPAIR 6 FIG 201.</P>)

ATA 5347

M/D - STA 746 RBL 11 SEAT TRACK SLOT HOLE FOUND CORROSION CRACK.(<P>M/D - STA 690-753 RBL 11 CORROSION DAMAGED SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12</P>)

ATA 5320

M/D - STA 980 TO 1000 LBL 77 FLR SECTION R/H FLANGE FOUND CRACK(<P>M/D - STA 970-1000 LBL 77 FLOOR SECTION CRACKED AREA REPAIRED AS PER SRM 53-00-52-2R-13 REPAIR 13 FIG 201.</P>)

ATA 5320

M/D - STA 980 TO 1000 RBL 77 FLR SECTION FOUND CRACK.(<P>M/D - STA 970-1000 RBL 77 FLOOR SECTION CRACKED AREA REPAIRED AS PER SRM 53-00-52-2R-13 REPAIR 13 FIG 201.</P>)

ATA 5320

M/D - STA 1480 TO 1500 LBL TO RBL 11 BELOW FLR PNL COVER PLATE FOUND CORROSION.(<P>M/D - STA 1480 TO 1500 LBL 11 BELOW FLR PANEL SHEAR WEB REPAIRED AS PER RI-53-00-14354 REV A.</P>)

ATA 5347

M/D - STA 1180 TO 1200 LBL 11 SEAT TRACK CROWN FOUND CORROSION.(<P>M/D - STA 1180-1200 LBL 11 SEAT TRACK CROWN CORROSION REMOVED AND REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01 BLENDED OUT AREA DEPTH 0.015", WIDTH 0.7" LENGTH 2.5" WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS.</P>)

ATA 5330

AIRCRAFT DAMAGE LOG ITEM D19-001 - DENT 1.5" X 0.03" SMOOTH CRACK FREE W/I LIMITS PER SRM 53-00-01-1A STICKER INSTALLED #30369.(<P>DENT AREA REPAIRED AS PER RI-53-11-14364 REV A.</P>)

ATA 5310

FX - LH BODY FAIRING 191AEL SUPPORT FRAME AT STA 880 UPR END CRACKED AS MARK.(<P>FX - LH BODY FAIRING 191AEL SUPPORT FRAME AT STA 880 UPPER END CRACKED AREA REPAIRED AS PER SRM 53-00-71-2R-4 REPAIR 4</P>)

ATA 5340

FX - CENTER FUEL TANK BOTTOM ATT ANGLE AT STA 1240 LBL 103 FOUND CRACKED(<P>FX - CEMTER FUEL TANK BOTTOM ANGLE FABRICATED AS PER BOEING DWG 65B10750 PL INSTALLED AS PER RI-53-00-14366 REV A</P>)

ATA 5347

M/D - STA 907 LBL 11 SEAT TRACK SLOT HOLE FOUND CORROSION CRACK.(<P>M/D - STA 870-950 LBL11" SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-12 REPAIR 12 FIG 201</P>)

ATA 5310

M/D STAIRWAY NO.5 STEP FOUND CRACKED (COUNT FROM U/D)(<P>M/D STAIRWAY NO.5 STEP CRACK AREA REPAIRED AS PER RI NO: RI-25-50-14342 REV.A</P>)

ATA 2510

AIR TURN BACK (ATB) - F/O SEAT WILL NOT LOCK IN FWD OR AFT POSITION, OR ANY POSITION IN BETWEEN. EITHER WITH MANUAL LEVERS OR ELECTRICALLY. LP 674182 - REMOVED AND REPLACED F/O'S SEAT IAW AMM 25-11-01, OPS CHECK GOOD.

ATA 2510

M/D LADDER, UPPER SECTION - STEP NR 5 FOUND CRACKED.&NBSP;(<P>REPAIRED M/D CREW ACCESS LADDER TREAD, NR 5 STEP CRACK AREA IAW RI-25-50-13410 REV.A.&NBSP;</P>)

ATA 2550

MISSING PIECES ALONG THE EDGE OF AFT CENTER BALL MAT PANEL BETWEEN STA 1840 AND 1900 IN AFT CARGO COMPT.(<P>REPAIRED DAMAGE AREA WITH MISSING PIECES ALONG THE EDGE&NBSP;OF THE CENTER BALL MAT PANEL BETWEEN STA 1840 AND 1900 IAW RI-25-53-13416 REV.A.&NBSP;</P>)

ATA 5320

LT BS 720 U/DECK TENSION TIE AFT CHANNEL ONE HOLE FOUND CRACK AT 12 O/C APPROX 0.030(<P>TENSION TIE CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. TABLE 203</P>)

ATA 2550

LOWER SKIN FOUND CRACKED ON AFT CENTER BALL MAT PANEL BETWEEN STA 1840 AND 1900 IN THE AFT CARGO COMPT.(<P>REPAIRED THE LOWER SKIN CRACKED AREA ON THE AFT CENTER BALL MAT PANEL BETWEEN STA 1840 AND 1900 IAW RI 25-53-13416 REV.A.&NBSP;</P>)

ATA 2550

EDGE LIP FOUND CRACKED ON THE AFT CENTER BALL MAT PANEL BETWEEN STA 1840 AND 1900 IN AFT CARGO COMPT.(<P>REPAIRED AREA OF EDGE LIP CRACK ON AFT CENTER BALL MAT PANEL BETWEEN STA 1840 AND 1900 IAW RI-25-53-13416 REV.A.</P>)

ATA 5330

FOUND A CRACK ON FWD UPPER CORNER SKIN AND BEAR STRAP OF AFT CARGO DOOR CUTOUT.&NBSP;(<P>REPAIRED CRACK AREA OF AFT CARGO DOOR CUTOUT (UPPER CORNER) AND BEAR STRAP IAW SRM 53-60-01-2R-3 REPAIR 3 TYPE II REPAIR. THIS REPAIR IS A CATEGORY B REPAIR.&NBSP;</P>)

ATA 2520

M/D STA 1920-2020 HAS LT DADO PANEL CRACKED.(<P>REPAIRED M/D STA 1920-2020 LT DADO PANEL CRACK AREA IAW RI-25-21-13425 REV.A.&NBSP;</P>)

ATA 7110

NR 2 ENG RT CORE COWL HAS AN EXTERNAL SKIN CRACK WHICH WAS FOUND JUST BELOW THE EXHAUST GRILL AREA.(<P>REPAIRED NR 2 ENG RT CORE COWL EXTERNAL SKIN CRACK AREAS IAW CV19-02154 AND RI-54-45-13424.</P>)

ATA 5321

BULK CARGO - CENTER FLOOR PANEL AT 2080 RBL 20" PUNCTURED.&NBSP;(<P>REPAIRED DAMAGED FLOOR PANEL IN BULK CARGO COMPARTMENT, STA 2080 RBL 20" IAW RI-25-54-13405 REV.A.&NBSP;</P>)

ATA 2620

MAIN DECK WATER FIRE EXTINGUISHER HAS SIGN OF LEAKING. REMOVED AND REPLACED THE FIRE EXTINGUISHER IAW AMM 26-26-02.

ATA 5347

CORROSION ON THE MAIN DECK FLOOR SEAT TRACK NEAR BS 2200, LBL 89.67. REPAIR THE SEAT TRACK IAW EI T2017A53M-740, REV 1.

ATA 5315

CORROSION ON FLOORBEAM UPPER TEE AT BS 1500, LBL 86. REPAIRED THE FLOORBEAM IAW EI T2017A53M-755, REV 1.

ATA 5315

CORROSION ON THE MAIN DECK CARGO FLOORBEAM UPPER TEE AT BS 480 NEAR LBL 105 REPAIRD THE FLOORBEAM IAW EI T2017A53M-737, REV 1.

ATA 5315

CORROSION ON THE MAIN DECK CARGO FLOORBEAM UPPER TEE CAP AT BS 2280 BETWENN RBL 45 TO 70. REPAIRED IAW EI T2017A53M-798, REV 1.

ATA 5347

CORROSION ON THE MAIN DECK FLOOR SEAT TRACK NEAR BS 2265, LBL 33.69. REPAIR DAMAGED AREA IAW EI T2017A53M-741, REV 1.

ATA 5347

CORROSION ON THE MAIN DECK FLOOR SEAT TRACK BETWEEN BS 830 AND 925 RBL 11.33. REPAIRED THE SEAT TRACK IAW EI T2017A53M-726 REV 1.

ATA 5347

CORROSION ON THE MAIN DECK FLOOR SEAT TRACK BS 2015 AND 2138, RBL 11.33. REPAIR DAMAGED AREA IAW EI T2017A53M-730, REV 1.

ATA 5347

CORROSION ON THE MAIN DECK FLOOR SEAT TRACK BS 2170 LBL 11.33. REPAIR DAMAGED AREA IAW EI T2017A53M-729, REV 1.

ATA 5347

CORROSION ON THE MAIN DECK SEAT TRACK BETWEEN BS 2025 - 2070, NEAR BS 2170, LBL 11.33. REPAIR THE SEAT TRACK IAW EI T2017A53M-729, REV 1.

ATA 5320

FOUND A FLOOR SUPPORT CORRODED NEAR BS 2380, LBL 20. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 REV.79, DWG 65B38754 SH8 REV 1, AND SRM 51-40-02, REV 79.

ATA 5320

FOUND THE MAIN DECK CARGO FLOOR SUB TRACK DAMAGED BS 1483, RBL 75.92. REPAIRED THE DAMAGED AREA IAW SRM 53-00-52-2R-13, REV 79, AND DWG 65B38251, SH 62, REV A, SH 32, REV 0, SH 75, REV- , AND 14440802, SH 3, REV B2.

ATA 5320

CORRODED SUPPORT BRACKET LOWER FUSELAGE SUPPORT WING TO BODY FAIRING STRUCTURE BS 979, LBL 3. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G-0, REV 79. INSTALL A NEW BRACKET IAW SRM 51-40-02-OG-0, REV 79, AND DWG 65B06976, SH2, REV G.

ATA 5347

FOUND MAIN DECK SEAT TRACK CORRODED AT BS 1020 - 1135, RBL 11. REMOVE THE DAMAGED SEAT TRACK IAW SRM 51-40-02-0G-0 REV.79. INSTALL A NEW SEAT TRACK IAW SRM 51-40-02-0G-0, REV 79, AND DWG 111U0801, SHEET 2, REV D, SHEET 3, REV E, AND SHEET 4, REV J.

ATA 2497

FOUND THE NR 2 ENGINE POWER FEEDER CABLE HAS A SPLICE IN THE THRUST REVERSER COWLING AREA. REPLACED POWER FEEDER CABLE AND CONDITION CHECKED NORMAL IAW SWPM 20-30-13, 20-30-11, 20-10-11 REV 64, AND WDM 24-21-21, REV 41. PERFORMED GENERATOR DRIVE SYSTEM OPERATIONAL TEST AND THE RESULT WAS SATISFACTORY IAW AMM 24-11-00-705-001, REV 88.

ATA 5797

FOUND WIRES CHAFED AT THE NR 3 WING LEADING EDGE COVER. SPLICED THE WIRES AND PERFORMED CONTINUITY CHECK IAW SWPM 26-30-12, REV 64, WDM 73-21-83, 73-21-35, AND 26-11-34, REV 41. THE RESULT WAS SATISFACTORY. PERFORMED NR 3 ENGINE EEC SATISFACTORY TEST AND THE RESULT WAS SATISFACTORY IAW AMM 71-00-00-805-160-T00, REV.88. PERFORMED NR 3 ENGINE FIRE SYSTEM GROUND TEST AND THE RESULT WAS SATISFACTORY IAW AMM 26-11-00-745-047, REV 88.

ATA 2497

FOUND WIRE CHAFED AT THE NR 2 WIRE LEADING EDGE COVER. REPAIRED THE WIRE IAW SWPM 20-10-13, AND 20-30-12, REV 64. PERFORMED WIRING CHECK AND FOUND SATISFACTORY.

ATA 2830

STATUS MESSAGE FOR OVERRIDE JETTISON PUMP NR 3 FAILED. REPLACED THE PUMP IAW AMM 28-31-01-004-001-001, REV 88, AND AMM 28-31-01-404-018-001, REV 88, STEP 3A TO 3J11. OPS TESTED AND COND CHECK NORMAL.

ATA 5347

MAIN DECK CARGO TRACK CRACKED AT BS 980 - 1000, LBL 75. REPAIRED THE CARGO TRACK IAW SRM 53-00-52-2R-13, REV 79.

ATA 5347

CORROSION ON THE MAIN DECK SEAT TRACK BETWEEN BS 765 & 865, LBL 11.33. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R-12, REV 79, AND EI T2017A53M-725, REV 1.

ATA 5347

CORROSION ON THE MAIN DECK SEAT TRACK BETWEEN BS 645 - 745, LBL 11.33. REPAIRED THE SEAT TRACK IAW EI T2017A53M-723, REV 1, AND DWG 65B38252, SHEET 12, REV, SHEET 11, REV 2.

ATA 5315

CORROSION FOUND ON THE FLOORBEAM UPPER TEE AT BS 980 RBL 100. REPAIRED THE FLOORBEAM IAW EI T2017A53M-742, REV 1.

ATA 5315

CORROSION FOUND ON THE FLOORBEAM IN THE AFT CARGO BAY FWD UPPER SIDE BS 1580, LBL 75 - 98. REPAIRED THE FLOORBEAM IAW SRM 53-00-51, REPAIR 3, REV 79, AND DWG 65B38079, SHEET 9, REV.

ATA 5347

FOUND THE MAIN DECK FLOORBEAM CORRODED AT BS 2240, LBL 33. REPAIRED THE SEAT TRACK IAW SRM 53-00-51, REPAIR 3, REV 79, AND DWG 65B38112, SHEET 13, REV.

ATA 5347

CORROSION FOUND ON THE MAIN DECK SEAT TRACK BETWEEN BS 1784 AND 1942, LBL 11.33. REPAIRED THE SEAT TRACK IAW SRM 53-00-52-2R-12, REPAIR 12, DETAIL 1, REV 79, AND EI T2017A53M-692, REV 2.

ATA 5347

CORROSION FOUND ON THE MAIN DECK SEAT TRACK BS 1730, RBL 11.33. REPAIRED THE SEAT TRACK IAW EI T2017A53M-677, REV 2, AND SRM 53-00-52-2R-12, DETAIL III, REV 79.

ATA 5347

CORROSION FOUND ON THE MAIN DECK SEAT TRACK BS 1697, 1730, AND 1746, LBL 11.33. REPAIRED THE SEAT TRACK IAW EI T2017A53M-676, REV 2, AND SRM 53-00-52-2R-12, REPAIR 12, DETAIL III, REV 79.

ATA 5347

CORROSION FOUND ON THE MAIN DECK SEAT TRACK BETWEEN BS 1784 & 1942, LBL 11.33. REPAIRED IAW SRM 53-00-52-52-2R-12, REPAIR 12, DETAIL 1, REV 79 AND EI T2017A53M-692, REV 2.

ATA 5315

CORROSION ON THE FLOORBEAM UPPER TEE AT BS 1740, LBL 8. REPAIRED THE FLOORBEAM IAW EI T2017A53M-698, REV 2.

ATA 5313

FUSELAGE LT LONGERON EXTENSION FITTING AT BS 1480, STRINGER 32, CRACK FOUND ON FITTING APPROX 1/2" IN LENGTH. FUSELAGE LT LONGERON EXTENSION FITTING REPLACED IAW EO NR 4453A818 REV 11 PART 3.

ATA 5313

FUSELAGE RT LONGERON EXTENSION FITTING AT BS 1480, STRINGER 32, CRACKED. FOUND ON FITTING, APPROX 11/16" IN LENGTH. REPLACED IAW EO 4453A818 REV 11 PART 4.

ATA 5753

RIGHT WING INBD MID FLAP UPPER TE PANEL, REAR EDGE FOUND SEVERAL AREAS BULGED. RIGHT WING INBD MID FLAP REPLACEMENT.

ATA 3350

UPPER DECK AFT CEILING EMER LIGHTS DO NOT ILLUMINATE. BATTERY PACK REPLACED & OPERATION CHECK FOUND NORMAL IAW AMM 33-51-04 & 33-51-00.

ATA 3411

EICAS MSG, ATL DISAGREE AT FL 300, CAPTAINS 30000 & FIRST OFFICERS 30260, DESCENDED TO FL 280. FOUND THE FIRST OFFICERS PITOT STATIC PROBE, RT SIDE STATIC PORT PLUGGED WITH BIRD WASTE. R & R PITOT STATIC PROBE IAW AMM 34-11-01. FLUSHED SYS AS NECESSARY IAW AMM 34-11-00. R & R RT CADC IAW AMM0 34-12-01, CHECKED NORMAL. PERFORMED FULL RANGE LEAK CHECK IAW AMM 34-11-00, CHECKED NORMAL, CAPTAINS, FIRST OFFICERS & STBY ALT.

ATA 2120

STATUS MSG, EE CLNG, SUP FAN. ELECTRICAL SMOKE FUMES ASSOCIATED WITH THIS PROBLEM. TRANSFER TO MDDR 57392 IAW MEL 21-58-06 CAT C. CB R30 PULLED & COLLARD.

ATA 2710

AT FL 400, ACFT OSCILLATED ON ROLL & YAW. COMPLIED WITH QRH 9.1. REPLACED RT OTBD AILERON LOCKOUT ACTUATOR & FUNCTIONAL CHECKS GOOD IAW MM 27-11-16 & 27-11-00.

ATA 2597

REF ACTION PLAN 10367 FOR MDDR 52209, 19L1 & 19L2 PDU'S NOT TRANSITIONING WHEN SELECTED TO FWD OR AFT DRIVE POSITIONS. R & R MASTER CONTROL PANEL IAW MM 25-57-09 & PDU`S 19L1 & L2. OPERATIONS OK. HAD TO REMOVE NEW PANEL & REINSTALL ORIGINAL PANEL DUE TO ARCING & CHAFED WIRES BEHIND PANEL. MDDR 52209 REMAINS OPEN.

ATA 3350

MAIN DECK CEILING EMER LIGHTS INOPERATIVE. RE LAMPED, OPERATIONS CHECKED GOOD IAW AMM 33-51-07.

ATA 2550

PDU AT POS 12L SMOKE. REMOVED, DEACTIVATED & DEFERRED.

ATA 5755

ON WALK AROUND FOUND NR 8 SPOILER PANEL CRACKED & DELAMINATED. R & R SPOILER PANEL NR 8 IAW AMM 27-01-01.

ATA 5755

FOUND FIXED WING PANEL OTBD OF SPOILER NR 8 CRACKED. RIB AT RT WING STATION 620 R & R IAW SRM 51-40-02 REV 69, RIB REFITTED & SECURED.

ATA 5753

RT INBD AFT FLAP UPPER SKIN FWD EDGE HAS GOUGES ON 3 REPAIR TRIPLERS & 2 ADDITIONAL LOCATIONS. REMOVED EXISTING REPAIRS AT 3 LOCATIONS & REPAIRED ALL DAMAGES IAW SRM 51-70-10-2R-2 REPAIR 2.

ATA 3230

REF SDR UIEA2014022400080. AT FL 320, SPEED .834 EICAS MESSAGE, GEAR DOOR, RUMBLE WAS FELT. QRH 14.16 COMPLIED WITH. GEAR HANDLE PLACED IN UP POSITION. REPLACED SAFETY VLV IAW AMM 32-33-29-404-006.

ATA 3232

AT FL320 SPEED .834 EICAS MESSAGE, GEAR DOOR, & RUMBLE WAS FELT. QRH 14.16 COMPLIED WITH. GEAR HANDLE PLACED IN UP POSITION. RT BODY GEAR DOOR ACTUATOR REPLACED IAW AMM 32-33-27-404-006.

ATA 2120

DURING REVERSE THRUST ON LANDING, SMOKE IN CREW REST AREA, ADVISORY EICAS MESSAGE APPEARED WITH VISIBLE SMOKE & ODOR IN CREW REST AREA. COMPLIED WITH CONDITIONAL INSPECTION IAW AMM 05-51-56, TASK 05-51-56-200-801, SMOKE OR FUMES IN CABIN. NO DEFECTS NOTED.

ATA 5320

MAIN DECK STATION 1200 RBL 105'' BELOW FLOOR INTERCOSTAL FOUND CRACKED. INTERCOSTAL REPLACED IAW R1-53-41-10434.

ATA 5315

MAIN DECK BS 2240, RBL 55-58 FLOOR BEAM FOUND CORROSION. FLOOR BEAM UPPER CHORD REPAIR CARRIED OUT IAW SRM 53-00-51 REPAIR 3.

ATA 5320

MAIN DECK STATION 1180 RBL 100 INCHES BELOW FLOOR INTERCOSTAL FOUND CRACKED. INTERCOSTAL REPLACED IAW R1-53-41-10436.

ATA 5320

MAIN DECK STATION 1180 LBL 100 INCHES BELOW FLOOR INTERCOSTAL FOUND CRACKED. INTERCOSTAL REPLACED IAW R1-53-41-10436.

ATA 5330

FX BS 980, STRINGER 38L SKIN, ONE EACH FASTENER HOLE FOUND CRACKED. SKIN REPAIRED CARRIED OUT IAW SRM 53-20-01 REPAIR 2.

ATA 5330

FX BS 980, STRINGER 38R SKIN, ONE EACH FASTENER HOLE FOUND CRACKED AT 6 O`CLOCK POSITION. SKIN REPAIRED CARRIED OUT IAW SRM 53-20-01 REPAIR 2.

ATA 5753

LEFT W OTBD FORE FLAP FRONT SPAR LOWER FLANGE ONE EACH FASTENER HOLE FOUND ELONGATED APPROXIMATELY 128 INCHES FROM ON BOARD & EDGE. REPAIRED CARRIED OUT IAW R1-57-58-10433.

ATA 5320

MAIN DECK STATION 1220 LBL 100 INCHES BELOW FLOOR INTERCOSTAL FOUND CRACK. REPAIRED CARRIED OUT IAW SRM 53-40-51 REPAIR 5.

ATA 5753

LEFT OTBD FORE FLAP UPPER SURFACE OF L/E HAS BIRD STRIKE DAMAGE. TAP TEST SHOWS DAMAGE TO BE WITHIN AN AREA OF 18" LONG BY 8" WIDE. APPLIED TIME LIMITED REPAIR IAW EO 4457A472, PART 1.

ATA 2612

FIRE WARNING BELL SOUNDS CONTINUOUSLY WITH RED MASTER BUT NO ASSOCIATED FIRE SYS RED LIGHT. FOUND A-3 CARD, MASTER MON A FAULTING. CARD REPLACED AND OPERATES NORMAL IAW MM.

ATA 5347

FOUND DAMAGE TO THE MAIN DECK SEAT TRACK BETWEEN BS 1509 AND 1521 RBL 11.33. DAMAGE FOUND TO BE BEYOND THE SRM 53-00-52, FIG 101, PERMANENT REPAIR ACCOMPLISHED IAW SRM 53-00-52, REPAIR 12.

ATA 5347

DAMAGE TO THE MAIN DECK SEAT TRACK WAS FOUND CRACKED, MEASURING 11.5" LONG. DAMAGE FOUND TO BE BEYOND THE SRM 53-00-52, FIG 101, ALLOWABLE DAMAGE 1 -SEAT TRACKS LIMITS. PERFORMED A TIME LIMITED REPAIR IAW EO 4453A829.

ATA 5347

DURING WALK-AROUND INSPECTION, DAMAGE TO THE MAIN DECK BS 1509 - 1521, LBL 11.33 - SEAT TRACK, CRACKED & DAMAGED, CRACK MEASURING 11.5 INCHES LONG. DAMAGE FOUND TO BE BEYOND THE SRM 53-00-52, FIG 101, ALLOWABLE DAMAGE 1 SEAT TRACKS LIMITS. PERFORMED A TIME LIMITED REPAIR IAW PART 1 WORK INSTRUCTIONS.

ATA 5320

DAMAGE TO MAIN DECK TO UPPER DECK STOWABLE CREW LADDER HAND RAIL SUPPORT STIFFENER. ACCOMPLISHED TIME LIMITED REPAIR.

ATA 7160

AFTER TAKEOFF AT AROUND 1000 FT AGL, LARGE BIRD STRIKE ON NR 4 ENGINE NACELLE L/E. FOUND NOSE COWL L/E 2 O'CLOCK POSITION DEFORMED. PERFORM NR 4 ENGINE BOROSCOPE INSPECTION ON HPC STAGE 1 AND 12. BIRDSTRIKE CONDITIONAL INSPECTION CARRIED OUT IAW AMM 05-51-14-202-001. REPLACED NR 4 ENGINE NOSE COWL IAW AMM 71-11-01. BOROSCOPE INSPECTION CARRIED OUT ON HPC STAGE 1 AND 12, IAW AMM 72-00-00-206-001. NO DAMAGE NOTED.

ATA 3520

EICAS-SUPERNUMERARY OXYGEN ON. MASKS DROPPED- NORM PRESSURE. CABIN ALT 5300'.

ATA 5751

INBD AILERON SUPPORT TRUSS WAS DAMAGED BEYOND REPAIR. FABRICATED TRUSS IAW DWG REQUIREMENTS.

ATA 5320

DURING C3 CHECK INSPECTION IAW EO 4453A301, REV C, CRACK WAS FOUND AT BS 760 RT TENSION TIE, AFT CHANNEL. DAMAGED TENSION TIE WAS REPAIRED IAW WORK STEP 6 OF PART 2 OF EO 4453A301 REV. C.

ATA 5320

DURING C3 CHECK, INSPECTION OF DATUM ACFT IAW EO 4453A301, REV C, CRACKS WERE FOUND AT 2 EA FASTENER HOLES AT BS 760 LT TENSION TIE, FWD CHANNEL.; THE SUBJECT DAMAGES WERE DOCUMENTED ON NRC GSP 501281. THE DAMAGED TENSION TIE WAS REPAIRED IAW WORK STEP 6 OF PART 1 OF EO 4453A301 REV C.

ATA 5320

LT BS720 TENSION TIE FWD CHANNEL 6 EA FASTENER HOLE FOUND CRACKED; 0.125", 0.060", 0.030, 0.030, 0.040, 0.040. TENSION TIE FWD CHANNEL REPAIRED IAW SRM 53-20-30, REPAIR 1, FIG 201.

ATA 5320

RIGHT BS 760 TENSION TIE AFT CHANNEL 1 EA FASTENER HOLE FOUND CRACKED. TENSION TIE AFT CHANNEL REPAIRED IAW SRM 53-20-30. REPAIR FIG 201.

ATA 5320

LEFT BS 760 TENSION TIE FWD CHANNEL 2 EA FASTENER HOLE FOUND CRACKED. TENSION TIE FWD CHANNEL REPAIRED IAW SRM 53-20-30, REPAIR 1, FIG 201.

ATA 5720

DURING EO 4457A391, PART 2, MX REPORTED DAMAGE TO THE RT INBD FIXED T/E WB135 - WBL155 SEAL RETAINER AND SEAL (REF FIG 1). PERFORMED A TIME LIMITED REPAIR.

ATA 5753

DURING MX WALKAROUND, FOUND DAMAGE TO THE RT INBD MID FLAP L/E WB132 - WBL139 PUNCTURED, MEASURING 2.5 IN. X 2.5 IN., 7.0 IN. TOTAL DAMAGE LENGTH.

ATA 5753

RT WING INBD MID FLAP HAS A HOLE- L/E INBD CORNER. IAW EO 4457A391 PART 1 TIME LIMITED REPAIR ACCOMPLISHED.

ATA 5321

DURING A-CHECK INSPECTION, MX REPORTED DAMAGE FOUND TO MAIN DECK - FLOORBOARD PANEL BS 1700 - 2020, LBL 99 AND OTBD GOUGE/DELAMINATION DAMAGE (PART 1 -TIME LIMITED REPAIR SCHEDULE PRIOR TO FURTHER FLIGHT; THIS EO DOCUMENTS THAT A TIME LIMITED REPAIR WAS ACCOMPLISHED AT PVG ON 25OCT11. REPEAT INSPECTION: SCHEDULE REPEAT INSP AT EVERY 1 FC (ONE FLIGHT CYCLE) AFTER PART 1 AND UNTIL PART 3 IS ACCOMPLISHED. PERMANENT REPAIR: SCHEDULE PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 1,000 FH (FLIGHT HOURS) AFTER PART 1.)

ATA 5753

FLIGHT CREW ADVISED MX UPON ARRIVAL, THEY NOTICED DAMAGE TO THE LT OTBD MID FLAP TRAILING EDGE.

ATA 5300

DURING LOADING OPERATIONS, ENGINE PALLET CAUSED DAMAGE TO FLOORBOARD PANELS BS1500 - BS1625, LBL 85.65 GOUGES/PUNCTURE DAMAGE (REF FIG 1). THE HOLE IS APPROX 30 INCHES LONG BY 2.5 IN. WIDE.

ATA 3410

RIGHT CDU INOP, FROZEN ON POSITION REPORT (REPLACED RT CDU IAW MM 34-61-02, ALL OPERATES NORMAL ).

ATA 5230

EGAT FOUND DAMAGE ON EXISTING REPAIR OF AFT CARGO DOOR (P/N 65B04250-17, S/N 001244) OUTER SKIN AT FOWARD LOWER SIDE AND SEAL RETAINERS (P/N 65B04712-5) IN FEBRUARY 2011.(A PERMANENT REPAIR WAS ACCOMPLISHED PER NRC 346 AND EGAT EL NO. T2011A52B-332. BOEING APPROVED THE PERMANENT REPAIR PER SR 1-1804275601 AND PROVIDED A SECOND STAGE APPROVAL FOR A THRESHOLD INSPECTION PER FAA 8100-9 FORM DATED 28FEB2011.)

ATA 5330

DURING D2-CHECK, A DENT AND A GOUGE WERE FOUND ON RT FUSELAGE SKIN AT BS 2586, S-50R TO S-51R.THE DENT AND GOUGE WERE LOCATED CLOSE TO AN EXISTING EXTERNAL SKIN REPAIR AND THE DENT AND GOUGE WERE BEYOND THE ALLOWABLE LIMIT PER SRM 53-00-01 FIG.101. REPLACED THE EXISTING EXTERNAL SKIN REPAIR WITH AN EXTENDED EXTERNAL SKIN REPAIR PER SR 1-1805401625 WITH 8100-9 APPROVAL. THE REPAIR AND WAS APPROVED BY MANUFACTURER SR 1-1805401625 .

ATA 5330

DENT DAMAGE IN 65B23701-5 SKIN WAS DETECTED AT BS 529 BETWEEN S23L TO S24L. DEPTH OF DENT WAS .046 INCHES, WIDTH WAS 1.1 INCHES, & LENGTH WAS 1.9 INCHES AS RECORDED PER EGAT NRC 035. TO RESTORE THE TRIMMED OUT AREAS OF 65B23701-5 SKIN TO ITS ORIGINAL STRENGTH WILL REQUIRE THE INSTALLATION OF AN EXTERNAL REPAIR DOUBLER AND TWO FILLERS TO COMPENSATE FOR THE LOST OF MATERIAL AND STRENGTH. THE INSTALLATION OF THE EXTERNAL REPAIR DOUBLER IS A "CATEGORY B" PERMANENT REPAIR PER DEFINITION OF SRM 51-00-06.THE CATEGORY B REPAIR AT BS 529 BETWEEN S23L TO S24L CONSISTS OF A SMALL REPAIR FILLER, A LARGE REPAIR FILLER, AND A REPAIR EXTERNAL DOUBLER.

ATA 7830

MAJOR REPAIR. DURING WALK-AROUND INSP. MX FOUND THE NR 4 RT THRUST REVERSER TRANSLATING COWL WITH DELAMINATION DAMAGE TO THE OUTER SKIN, LOCATED APPROX AT THE 3 O'CLOCK POSITION (REF FIG 1 AND 2). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, DVI INSP AFTER EVERY 5 FLIGHT CYCLE UNTIL ACCOMPLISHMENT OF PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 1,000 FH (FLIGHT HOURS) AFTER PART 1.)

ATA 5753

FWD NR 1, NR 8 BOLT TOO SHORT REF EGAT EI NR T2011A27B-349, REV 00. REPLACED NEW BOLT.

ATA 5410

WORN ON NR 1 PYLON RT ACCESS DOOR ASSY. REPAIRED DAMAGE AREA IAW T2011A54B-34, REV 00.

ATA 2760

FWD LT WING SPOILER CTRL CABLE WS1A-3 BROKEN STAND. REPAIRED IAW AMM 27-61-00, REV 70 ADJUSTMENT / TEST.

ATA 2710

FWD LT AILERON CONTROL CABLE AS-3 WORN OUT. REPAIRED IAW AMM 27-11-00 REV 70. ADJUSTMENT TEST.

ATA 2710

FWD LT AILERON CONTROL CABLE AB-9 WORN OUT. (IAW AMM 27-11-00. ADJUSTMENT TEST.)

ATA 2760

FWD RT WING SPOILER CONTROL CABLE WSIA-6: BROKEN STRAND (IAW AMM 20-11-03. REV 70. ADJUSTMENT/TEST).

ATA 5230

DURING D-CHECK INSP OF DATUM ACFT, A SCRATCH AND DENT WERE REPORTED ON THE BULK CARGO DOOR (PN 65B01857-22, SN TLS11203) OUTER SKIN AT THE FWD LOWER CORNER. (THE DAMAGED AREA WAS REPAIRED IAW EGAT NRC 352 AND EGAT EI T2011A52B-363 BY TRIMMING OUT THE DAMAGE AND INSTALLING A REPAIR DOUBLER AND FILLER.)

ATA 5511

CRACKED RIB IN THE FIXED L/E NOSE CAVITY, LT HORIZONTAL STAB STA 510. REPAIRED DAMAGE AREA IAW EI T2011A55B-287 REV.00 AND REV 01.

ATA 5511

CRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 441. REPAIRED DAMAGE AREA IAW EI T2011A55B-289 REV 00 AND REV 01.

ATA 5511

CRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 450. REPAIRED DAMAGE AREA IAW EI T2011A55B-290 REV 00 AND REV 01.

ATA 5511

CRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 467. REPAIRED DAMAGE AREA IAW EI T2011A55B-292 REV 00 AND REV 01.

ATA 5511

CRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 493. REPAIRED DAMAGE AREA IAW EI T2011A55B-294 REV 00 AND REV 01.

ATA 5511

CRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 527. REPAIRED DAMAGE AREA IAW EI T2011A55B-298 REV 00 AND REV 01.

ATA 5511

CRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORZ STAB STA 518. REPAIRED DAMAGE AREA IAW EI T2011A55B-297 REV 00 AND REV 01.

ATA 5511

CRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 510. REPAIRED DAMAGE AREA IAW EI T2011A55B-296 REV 00 AND REV 01.

ATA 5511

CRACKED RIB IN THE FIXED L/E NOSE CAVITY, RT HORIZONTAL STAB STA 501. REPAIR DAMAGE AREA IAW EI NO T2011A55B-295 REV 00 AND REV 01.

ATA 5511

CRACKED RIB AND LOWER CLIP IN THE FIXED L/E NOSE CAVITY RT HORIZONTAL STAB STA 484. REPAIRED DAMAGE AREA IAW EI T2011A55B-293 REV 00 AND REV 01.

ATA 5511

CRACKED RIB AND LOWER CLIP IN THE FIXED L/E NOSE CAVITY RT HORIZONAL STAB STA 458. REPAIRED DAMAGE AREA IAW EI T2011A55B-291 REV 00 AND REV 01.

ATA 5511

CRACKED RIB IN THE FIXED L/E NOSE CAVITY, LT HORIZONTAL STAB STA 518. REPAIRED DAMAGE AREA IAW EI T2011A55B-291 REV 00 AND REV 01.

ATA 5511

CRACKED RIB IN THE FIXED L/E NOSE CAVITY, LT HORIZONTAL STAB STA 501. REPAIRED DAMAGE AREA IAW EI T2011A55B-286 REV 00 AND REV 01.

ATA 5511

CRACKED LOWER RIB AND CLIP IN THE FIXED L/E NOSE CAVITY HORIZONAL STAB 458. REPAIRED DAMAGE AREA IAW EI T2011A55B-285 REV 00 AND REV 01.

ATA 5511

CRACK - RIB AND LOWER CLIP HORIZONTAL STAB STA 450. FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI T2011A55B-284 REV 00 AND REV 01.

ATA 5511

CRACKED RIB AND LOWER CLIP HORIZONTAL STAB STA 441: FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI NO T2011A55B-283 REV 00 AND REV 01.

ATA 5511

CRACKED RIB AND LOWER CLIP HORIZONTAL STAB STA 407: FIXED L/E NOSE CAVITY. REPAIRED DAMAGE AREA IAW EI NO T2011A55B-303 REV 00 AND REV 01.

ATA 5511

CRACKED RIB AND LOWER CLIP STAB STA 399: LT HORIZONTAL STAB FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI NO T2011A55B-302 REV 00 AND REV 01.

ATA 5511

CRACKED RIB AND UPPER CLIP L/E STA 159: LT HORIZONTAL STAB FIXED L/E NOSE CAVITY. REPAIR DAMAGE AREA IAW EI NO T2011A55B-301 REV 00 AND REV 01.

ATA 5511

CRACK - RIB AND UPPER CLIP L/E STA 151: LT HORIZONTAL STAB FIXED L/E NOSE CAVITY. REPAIRED DAMAGE AREA IAW EI T2011A55B-300 REV 00 AND REV 01.

ATA 5511

CRACK - RIB AND UPPER CLIP L/E STA 145 LT HOR STAB FIXED L/E NOSE CAVITY. REPAIRED DAMAGE AREA IAW EI T2011A55B-299 REV 00 AND REV 01.

ATA 5330

FOUND WEAR ON FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FROM BS 2517 THROUGH 2628 LT SIDE. REMOVED DAMAGED AREA AND CHECKED REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.

ATA 5330

WEAR FOUND ON THE FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FORM BS 2280 THROUGH 2416 LT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.

ATA 5330

FOUND WEAR ON THE FUSELAGE SKIN AND VERTICAL F/N SEAL INTERFACE FROM BS 2517 THRU 2628 RT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA CORD IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.

ATA 5330

FWD WEAR ON THE FUSELAGE SKIN AND VERTICAL FIN SEAL INTERFACE FROM BS 2280 THROUGH 2416 RT SIDE. REMOVED DAMAGED AREA AND CHECK REWORKED AREA IS WITHIN ALLOWABLE LIMITS IAW SRM 53-00-01. FIGURE 101 DETAIL V. REV 58.

ATA 5320

THE SUPPORT AND SKIN PANEL OF LT: LWR FUSELAGE LONGERON BOX FAIRING SUPPORT STRUCTURE CRACKED, S35L. STA 1372. REPAIRED IAW SRM 51-70-07, REV 58 REPAIR DAMAGE AREA.

ATA 5320

THE SUPPORT AND SKIN PANEL OF RT LWR FUSELAGE LONGERON BOX FAIRING SUPPORT STRUCTURE CRACKED S35R, STA 1372 IAW SRM 51-70-07, REV 58 REPAIR DAMAGE AREA.

ATA 7200

SHORTLY AFTER TAKEOFF NR1 ENGINE OIL FILTER ILLUMINATED. SHUTDOWN ENGINE. ON ARRIVAL FOUND EICAS SHOWN OIL QTY READING 1 FOR NR1 ENGINE. ON INSP FOUND OIL IN THE TAIL PIPE. CHECKED MAIN CHIP DETECTOR AND "B" SUMP FOUND HEAVY METAL DEPOSIT ON CHIP DETECTORS. TRANSFER GEAR BOX INLET SCREEN AND NOTED MONITOR DEPOSIT OF METAL. FIM 79-21-04/ 79-21-06/ 79-00-00. ENGINE R & R

ATA 3421

DURING TAKEOFF ROLL CAPT CDU BLANKED , THUS THE CAPTAIN LOSSING T/O SPEEDS(MX SWAPPED LT CDU TO CTR POSITION, LT IRU TO CTR AND SWAPPED LT FMC TO RT AND DEFERRED THE CTR CDU, CTR IRU AND THE RT FMC. ALL SYS OPS NORMAL.

ATA 8012

REJECTED TAKEOFF. LOW SPEED EICAS MESSAGE "STARTER CUTOUT 3". START VALVE FOUND FAULTY, ITEM DEFERRED IAW DDG IAW 80-11-01.

ATA 5347

THE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR. DURING WALK AROUND INSP, DAMAGE TO THE MAIN DECK BS1820, LBL 98.58. SEAT TRACK DAMAGE WAS FOUND, CRACK MEASURING 14.0 INCH LONG (REF, FIG 1). DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS. SCHEDULE REPEAT INSPECTIONS AT EVERY (5) FC AND PERMANENT REPAIR PRIOR TO THE ACCUMULATION OF 25 FC AFTER PART 1.

ATA 5753

DURING A2-CHECK INSP, MX FOUND THE RT WBL 515 - OTBD MID FLAP L/E & AMP; RT WING FIXED T/E WITH CRACK/DAMAGE. WBL 515 - L/E OF RT OTBD MID FLAP BROKEN . THE DIMENSION IS 0.787 & .787 ) WBL 515 RT WING FIXED T/E FAIRING PANEL BROKEN AT WBL 515.. (1)PERMANENT REPAIR ACCOMPLISHED IAW PART 1 IAW THE SRM 57-53-01 FIGURE 201, REPAIR 1 TABLE II (REF. FIG 1). 2) PERMANENT REPAIR ACCOMPLISHED BY REMOVING THE DAMAGE IAW PART 1 IAW THE SRM 57-53-01 FIG 101 (ALLOWABLE DAMAGE), SRM 51-10-02 & AMP; SRM 51-20-01 WITH MINOR DEVIATIONS (DAMAGE REMOVED EXCEEDS THE SRM 57-53-01 FIG 101 (ALLOWABLE DAMAGE)) REQUIRES DER APPROVAL (REF.FIG 2).

ATA 5753

DURING WALKAROUND, DAMAGE WAS FOUND TO THE TO THE LT WING T/E INBD MID FLAP OTBD T/E COVE RIB. THE REPAIR PER PART 1 OF THIS EO IS CATEGORY C AND REQUIRES REPETITIVE INSPECTION IAW PART 2 OF THIS EO AT 5 CYCLE INTERVALS AND REPLACEMENT AT THE NEXT A-CHECK AFTER 26MAY2010 IAW PART 3 OF THIS EO. PART 2 OF THIS EO REPETITIVELY INSPECTS THE PART 1 REPAIR TO ENSURE CONTINUED AIRWORTHINESS. PART 3 OF THIS EO ACCOMPLISHES THE INTERIM REPAIR AT THE NEXT A-CHECK AFTER 26 MAY 2010.

ATA 7810

DURING MX WALKAROUND, FOUND A DENT ON THE EXHAUST NOZZLE OUTER SLEEVE AT APPROX THE 6:00 POSITION ON THE NR1 ENGINE. THE DENT IS APPROX 2" LONG AND 0.05 INCHES WIDE AND IS APPROX 42 INCHES FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE DENT IS OUT OF LIMITS. DISPOSITION IS TO PERFORM A DYE PENETRANT INSP OF THE CRACK TO ENSURE NO CRACKS. DVI EVERY 5 FLIGHT CYCLES. REPLACEMENT OF THE NOZZLE AT THE NEXT "A" CHECK.

ATA 5712

A RIVET WAS MISSING AND WAS NOTED ON THE LT WING L/E RIB, OTBD LOF LANDING LIGHT. PERFORMED A TIME LIMITED REPAIR BY INSTALLING A BLIND FASTENER IN LIEU OF A SOLID RIVET. SCHEDULE REPEAT INSPECTIONS AT EVERY 25 FC AFTER PART 1 AND PERMANENT REPAIR PRIOR TO OR AT THE NEXT A CHECK AFTER PART 1.

ATA 5751

LT WING UPPER SURFACE OTBD, ALL OTBD AREA FOUND DELAMINATED. RT WING OTBD AIL UPPER SURFACE DELAMINATED AT SEVERAL LOCATION AS MARKED. LT WING UPPER SURFACE OTBD AILERON REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU 507013-1. RT WING -OTBD AILERON UPPER SURFACE REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU 504200-1. EO 4457A224RA, EO 4457A225RA.

ATA 5753

RT WING OTBD AFT FLAP L/E MID AREA FOUND DELAMINATED. RT WING - OTBD AFT FLAP REPAIRED IAW SRM 51-70-07 FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU506866-1. EO 4457A224RA, 4457A225RA.

ATA 5751

LT WING UPPER SURFACE OTBB AIL INBD AREA DELAMINATED AT SEVERAL LOCATIONS AS MARKED. RT WING - OTBD AILERON UPPER SURFACE REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NT: DJU 504200-1, EO 4457A224RA AND 4457A225RA.

ATA 5320

BULK CARGO FLOOR PANEL SUPPORT DEFORMED AT RBL 38" STA 2100. DAMAGED AREA TRIMMED OFF IAW SRM 51-70-11 FIG 1. INSP CARRIED OUT AND NO CRACK FOUND. EO 4453A320.

ATA 5320

BULK CARGO FLOOR PANEL SUPPORT DEFORMED AT RBL 38" AT STA 2080. DAMAGED AREA TRIMMED OFF IAW SRM 51-70-11 FIG 1. INSP CARRIED OUT AND NO CRACK FOUND. EO 4453A320.

ATA 5320

BULK CARGO - FLOOR PANEL SUPPORT DEFORMED AT RBL 38" STA 2060. DAMAGED AREA TRIMMED OFF IAW SRM 51-70-11 FIG 1. INSP CARRIED OUT AND NO CRACK FOUND. EO 4453A320.

ATA 5320

BULK CARGO - FLOOR PANEL SUPPORT DEFORMED AT RBL 7" STA 2020. DAMAGED AREA TRIMMED OFF IAW SRM 51-70-11 FIG 1. INSP CARRIED OUT AND NO CRACK FOUND. EO 4453A320.

ATA 5753

RT WING T/E INBD FORE FLAP L/E FOUND DELAMINATION AS MARKED. RT WING - INBD FORE FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU 504747-1. EO 4457A224RA, 4457A225RA.

ATA 5753

RT WING T/E OTBD AFT FLAP LWR SURFACE FOUND DENT AS MARKED. RT WING - OTBD AFT FLAP REPAIRED IAW SRM 51-70-10, REPAIR NR 4, FIG 201 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU505223. EO 4457A224RA, 4457A225RA.

ATA 5751

LEFT WING I/B AILERON O/B TRAILING EDGE CORNER FOUND DELAMINATION AS MARKED. LEFT WING - I/B AILERON REPAIRED AS PER SRM 51-70-06, FIG 9 AND REF HX PROCESS CARD, CONTROL SEQ MO: DJU 503673-1. EO 4457A224RA 4457A225RA.

ATA 5753

RT WING INBD AFT FLAP LWR SURFACE 1 LOCATION FOUND DELAMINATED AS MARKED. RT WING - INBD AFT FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU504176-1. EO 4457A224RA , 4457A225RA.

ATA 5753

LT WING T/E OTBD FORE FLAP L/E FOUND DELAMINATION AT SEVERAL LOCATION AS MARKED. LT WING -OTBD FORE FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ MO: DJU 503665-1. EO 4457A224RA, 4457A225RA.

ATA 5753

EO 4457A224RA, 4457A225RA: RT WING INBD MID FLAP UPPER SURFACE 2 LOCATION FOUND DELAMINATED AS MARKED. RT WING INBD MID FLAP LWR SURFACE OTBD AFT CORNER SCRATCH AS MARKED. RT WING - INBD MID FLAP REPAIRED IAW SRM 51-70-07, FIG 5 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU504168-1. RT WING - INBD MID FLAP REPAIRED IAW SRM 51-70-07, FIG 9 AND REF HX PROCESS CARD, CONTROL SEQ NR: DJU 504184-1.

ATA 5753

NR 7 FIX FLAP TRACK FAIRING L/E AREA ERODED. NR 7 FIX FAIRING RESIN REPAIRED IAW SRM 51-70-06, PARA 5.0, EO 4457A224RA, 4457A225RA.

ATA 5730

RT WING LOWER SURFACE HAS 2 AREAS WITH GOUGES ON SKIN EDGES STN 1551 & STN 1558. BOTH WITHIN SRM LIMITS. SRM 57-20-01-1A-1 DETAIL 1. GOUGE MARK SMOOTHED OUT IAW SRM 51-10-02. EO 4457A218, REV B.

ATA 7250

ESN 706103 - HPT STAGE 1 BLADES FOUND WITH UNDER PLATEFORM CORROSION AND CRACKS.STAGE 1 P/N 1538M90P12 (80EA).

ATA 7250

ESN 704892 - HPT STAGE 1 BLADES AND STAGE 2 BLADES FOUND WITH UNDER PLATEFORM CORROSION AND CRACKS. STAGE 1 P/N 1538M90P12 (80EA) STAGE 2 P/N 1881M52G05 (74EA).

ATA 5751

FOUND ON WALK AROUND RT OUTBD LOCATION LOWER SURFACE HAS TWO LOCATIONS WITH PREVIOUS REPAIRS NOT PAINTED. REPAIRED PER XEO 57-050807-2.

ATA 2121

UPON ENTERING THE FLIGHT DECK A STRONG ELECTRICAL OR FIRE ODOR WAS EVIDENT. STATUS MESSAGE "EE CLNG SUP FAN" DISPLAYED. FOUND THE EQUIPMENT COOLING SUPPLY FAN FAILED. DEACTIVATED THE FAN IAW DDPG 21-58-6 AND PLACED THE FAN ON DMI M07-050.

ATA 2913

HYD QTY LOW NR 2 EICAS MSG QTY 0. FOUND HYD FLUID LEAKING FROM NR 2 EDP (FLUID STILL IN SYSTEM). REMOVED AND REPLACED NR 2 EDP PER MM 29-11-08, OPS, LEAK CHECK OK AND ALL INDICATION ON PRESSURE NORMAL. REMOVED AND REPLACED NR 2 CASE DRAIN FILTER PER MM 29-11-14 CHECKED OK PER MM 29-11-14.

ATA 5610

DURING C CHECK INSPECTION, FOUND FLIGHT DECK WINDOW NR 3R EXHIBITING WIDE SPREAD BORDER DELAMINATION AROUND ENTIRE WINDOW. OTHER DIFFICULTIES UNDETERMINABLE DUE TO EXTENT OF DELAMINATION AND RESTRICTED VISUAL IMPAIRMENTS IN BORDER AREA. WINDOW CHANGED PRECAUTIONARY.

ATA 5610

DURING C-CHECK INSPECTION, PROCESS FOUND FLIGHT DECK WINDOW NR 3L EXHIBITING SIGNS OF FAIL/SAFE INTERLAYER CRACKING IN RADIUS AREAS. GENERAL IN-SERVICE USE AND LOCALIZED DELAMINATION OF WINDOW ASSEMBLY MADE IT IMPOSSIBLE TO POSITIVELY DETERMINE EXISTENCE AND EXTENT OF CRACKING. WINDOW CHANGED PRECAUTIONARY.

ATA 5610

DURING C CHECK INSPECTION, FOUND NR 2R FLIGHT DECK WINDOW EXHIBITING SIGNS OF FAIL/SAFE INTERLAYER CRACKING IN RADIUS AREAS. POSITIVE CONFORMATION IS NOT POSSIBLE DUE TO GENERAL IN-SERVICE WEAR AND LOCALIZED BORDER DELAMINATION. WINDOW CHANGED PRECAUTIONARY.

ATA 5347

AFT CARGO COMPARTMENT SEAT TRACK CROWN AREA DAMAGED AT STA 1860 TO STA 1880 LBL 45. SEAT TRACK REPAIRED PER SRM 53-00-52 REPAIR NR 10, AND EO 4453A102.

ATA 5320

AFT CARGO SIDE RAIL CRACKED.

ATA 5320

AFT CARGO SIDE RAIL DAMAGED.

ATA 7261

NR 2 ENGINE SHUTDOWN IN FLIGHT OIL QUANTITY DECREASED TO (0), FOLLOWED SHORTLY BY EICAS MSG ENG 2 OIL PRESSURE. ENGINE WINDMILLING OIL PRESS 8-10PSI. FOUND LUBE AND PUMP MANIFOLD LINE CRACK SERVICED ENGINE OIL. RR LUBE AND PUMP MANIFOLD LINE, OPERATED NR 2 ENG IAW 72-00-00, POST WINDMILL INSP 3 MINUTES LEAK CHECKED GOOD. RR LINE IAW REF 79-21-03.

ATA 7931

NR 2 ENGINE OIL PRESSURE DROPPED AND STABILIZED BELOW 10 PSI AFTER LEVEL OFF, INFLIGHT SHUT DOWN. REMOVED AND REPLACED PRESSURE XMITTER. RUN ENGINE, OPS CHECKED NORMAL AS PER AMM 79-32-00.

ATA 3250

RTO: DUE TO T/O WARNING. BODY GEAR STEERING, RETURNED TO BLOCKS. PRESENT LEG FAULT SHOWS RIGHT BODY GEAR STEERING RIGHT. ACTUATOR EXTENSION UNCOMMANDED AS PREVIOUS MEL 32-53-1. CONFIRM BODY GEAR STEERING ACTUATORS DEACTIVATED AND LOCKED PER MEL 32-53-2. BODY GEAR STEERING INDICATION SYSTEM INOP. BODY GEAR STEERING SYSTEM ALSO DEACTIVATED INOP AS PER MEL 32-53-1 DMI M06-090 RAISED. BODY STEERING SYSTEM INOP AND BODY GEAR INDICATION INOP. BODY GEAR STEERING ACTUATORS TO BE CHECKED LOCKED EACH DEPARTURE.

ATA 7830

MINOR LIGHTNING STRIKE, EXIT TO NR 2 ENGINE LT TRANSLATING COWL CAUSING DELAMINATION TO CARBON FIBRE MEASURING 0.5 INCH AXIAL BY 2.5 NR CIRCUMFRENTIAL ON TRAILING EDGE AT 8 O/C POSITION AFT LOOKING FORWARD.

ATA 3210

DAILY CHECK, ON WALK AROUND, FOUND LT BODY GEAR JURY STRUT UPPER ATTACHMENT PIN FOUND MIGRATED. RETENTION BOLT AND UPPER CAP STILL WITH CONDUIT. LOWER CAP AND NUT FOUND IN ADJACENT STRUCTURE. ON WALKAROUND, FOUND RT BODY GEAR JURY STRUT UPPER ATTACHMENT RETENTION BOLT NUT LOOSE. NO COTTER PIN EVIDENT. ALL OTHER DETAILS AT LOCATION INTACT. UPPER ATTACH AREA INSPECTED. PIN, CAPS AND RETENTION BOLT INSTALLED AND SAFETIED IAW MM. NUT TIGHTENED AND SAFETIED IAW MM. (K)

ATA 7320

AFTER ROTATION UP TO 1000 FT, NR3 ENGINE N1 WOULD SURGE (ROLL BACK) BETWEEN 101.5 AND 98.0 N1. AT THRUST REDUCTION ALTITUDE, THE SURGE WOULD STOP. ALL PHASES OF FLIGHT WERE NORMAL. AFTER LANDING, DID A POWER RUN UP AND THE SAME AS ABOVE OCCURRED, NO EICAS OR STATUS MESSAGE DISPLAYED. SERVICEABLE HMU FITTED ENGINE GROUND RUN CARRIED OUT. HMU REPLACED IAW AMM. IAW TAKEOFF POWER, OPS NORMAL. (K)

ATA 3240

EICAS MESSAGE BRAKE TEMP AFTER LANDING ROLLOUT IN MEL, SMALL FIRE NOTICED ON NR 7 BRAKE AFTER AIRCRAFT WAS PARKED. IT WAS QUICKLY EXTINGUISHED WITH A DRY FIRE EXTINGUISHER AGENT. INSPECTION CARRIED OUT. MAX TEMP INDICATION 5, CMC MSG 32127. NO ITEMS NOTED. ALL BRAKE TEMPERATURES AT ZERO FOR DEPARTURE. MCC REQUESTED NR 7 BRAKE AND TIRE REPLACED. (K)

ATA 7261

SHORTLY AFTER TAKEOFF OIL QTY DROPPED TO ZERO. DURING CLIMB-OUT, OIL PRESSURE DROPPED EVENTUALLY TO SIX PSI. NR 4 ENGINE WAS SHUT DOWN AS OIL PRESSURE TO 10 PSI. OIL PRESSURE REMAINED AT 6 PSI, N1 AT 25 PERCENT AND N2 BETWEEN 17 AND 21 PERCENT FOR DURATION OF FLIGHT. TIGHTENED B-NUT ON OIL PRESSURE TRANSMITTER PERFORMED 'NO OIL PRESSURE' INSPECTON PER MM 72-00-00. ALSO PERFORMED POST WINDMILLING INSPECTION PER 72-00-00. REPLACED OIL FILTER PER 79-21-04. NO METAL NOTED ON CHIP DETECTORS AND FILTER. NO LEAKS NOTED ON ENGINE RUN UP. ALL INSPECTION SATISFACTORY. (M)

ATA 7530

DURING ACCOMPLISHMENT OF ENGINE CONDITION MONITORING ALERT ITEM NR 2004P093. ENGINE NR 1 VISUAL INSPECTION OF STG 5 ACTUATION HARDWEAR, FOUND ONE VSV LEVER ARM MISSING AT 11 OCLOCK POSITION AMM. REPLACED ENGINE NR 1 IAW WORK CARD NR A717101GT1 AND MM. PERFORMED OPS CHECK AND LEAD CHECK, ALL OK. (K)

ATA 2612

HKG/ICN - AFTER TAKEOFF CLIMBING THROUGH 13,000 FEET, HAD INDICATION OF MAIN DECK CARGO FIRE. NO EICAS, NO WARNING BELL, JUST OVERHEAD SWITCH. IT WAS RAINING VERY HARD AND HIGH MOISTURE CONTENT IN AIRCRAFT. DEEP CLEANED MAIN DECK CARGO FIRE SWITCH. PERFORMED CMC GROUND TEST PASS PER MM 26-16-00. (M)

ATA 7250

ON TAKEOFF ROTATION, ENGINE NR 3 HAD 2 COMPRESSOR STALLS. N1 ROLLED BACK AND RECOVERED, EGT REACHED 950 DEGREES CELSIUS. ON CLIMB-OUT AND CRUISE ENGINE OPERATED NORMAL. PERFORMED TEST 72-00-00-206-050-020. STALL INSPECTION, FOUND HPC STAGE 6, THREE BLADES 50 PERCENT MISSING. REMOVED AND REPLACED ENGINE IAW A717101GT1. ENGINE RUN UP AND LEAK CHECK, OPS NORMAL IAW B150201FT1 TEST 6 VIBES 2.1 AT N1 109.9. (M)

ATA 2410

REFJECTED TAKEOFF DUE TO ELECTRIC DRIVE NR 3 WARNING ON TAKEOFF ROLL. ABORT OCCURRED AT 70 KNOTS. TRANSFERRED TO DMI, IDG OIL SERVICED TOO FULL. THREE QUARTS ADDED. REMOVED AND REPLACED NR 3 IDG IAW MM. PERFORMED OPS TEST IAW MM. OPS TEST OK. ALL INDICATIONS NORMAL. STATUS MESSAGE CLEARED. NO LEAKS FOUND ON IDG.