N852GT

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 54,380 hrs · 8,058 cycles

TE RUDDER DAMAGE.(<P>REPAIRED IAW SRM 51-70-05 AND EA 1955A028. NO FURTHER DEFECTS NOTED.</P>)

Part: RAM AIR TURB — ACTIVATED · airframe 53,427 hrs · 7,917 cycles

RAT BUTTON INADVERTANTLY DEPRESSED(<P>RAM AIR TURBINE DEPLOYED AND OPERATED NORMALLY. RESTOWED RAT AS PER AMM TASK 29-21-00-960-802, ALL FUNCTIONS NORMAL</P>)

Part: STRUCTURE — TORN (ZONE 500 FLAP) · airframe 52,385 hrs · 7,765 cycles

LHW #7 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SUPPORT CHANNEL — CRACKED (ZONE 500) · airframe 52,385 hrs · 7,765 cycles

LHW O/B REFUELING PNL FWD SUPPORT CHANNEL I/B AREA FOUND CRACKED.(<P>LHW O/B REFUELING PNL FWD SUPPORT CHANNEL I/B AREA REPAIRED IAW RI-57-00-17045 REV A . NO FURTHER DEFECTS NOTED.</P>)

Part: BEAM — CRACKED (ZONE 500) · airframe 52,385 hrs · 7,765 cycles

LHW L/E - ILES 567 D-BEAM WEB CRACKED.(<P><SPAN>LHW L/E - ILES 567 D-BEAM WEB REPAIRED IAW RI-57-41-17037 REV.A. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: PANEL — DAMAGED (ZONE 500 FLAP) · airframe 52,385 hrs · 7,765 cycles

LHW I/B MAIN FLAP MOST O/B SEAL PAN PANEL SCREW HOLE FOUND ELONGATED.(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER SRM 51-70-05 REPAIR 7. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,385 hrs · 7,765 cycles

M/D STA 1795-1815 LBL 11 SEAT TRACK CROWN AREA FOUND CORRODED.(<P>M/D STA 1795-1815 LBL 11" SEAT TRACK CORROSION CLEANED UP AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND MEASURED AFTER SMOOTHED OUT WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS REV.43 DATE 20JUN2024. NO FUTHER DEFECTS NOTED.</P>)

Part: SKIN — DAMAGED (ZONE 600) · airframe 52,385 hrs · 7,765 cycles

RHW - L/E ANTI-ICING DUCT SEPERATED AT NO.16 K/FLAP FWD L/E D-BEAM AREA AS MARKED.(<P>RHW L/E ANTI-ICING DUCT SEPERATED AT NO.16 K/FLAP FWD L/E D-BEAM SKIN PANEL CLOSE UP AS PER RI-57-41-17056 REV.A AND SRM 51-40-02 REV.43. NO FURTHER DEFECTS NOTED.</P>)

Part: CHANNEL — CRACKED (ZONE 300) · airframe 52,385 hrs · 7,765 cycles

R/H HORI. STAB. T/E U-CHANNEL FOUND CRACKED.(<P><SPAN>PERFORMED PERMANENT REPAIR AS PER HX RI NO:RI-55-10-17038 REV.A .NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRUCTURE — TORN (ZONE 600 FLAP) · airframe 52,385 hrs · 7,765 cycles

RHW #20 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRUCTURE — TORN (ZONE 500 FLAP) · airframe 52,385 hrs · 7,765 cycles

LHW #9 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRUCTURE — TORN (ZONE 500 FLAP) · airframe 52,385 hrs · 7,765 cycles

LHW #8 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: BEAM — CRACKED (ZONE 600) · airframe 52,385 hrs · 7,765 cycles

RHW L/E - ILES 567 D BEAM WEB CRACKED.(<P><SPAN>RHW L/E - ILES 567 D BEAM WEB REPAIRED IAW RI-57-41-17036 REV.A. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 100) · airframe 52,385 hrs · 7,765 cycles

AFT OF STA 2598 BULKHEAD, S-42R STRINGER FOUND CRACKED.(<P><SPAN>AFT OF STA 2598 BULKHEAD, S-42R STRINGER REPAIRED IAW RI-53-80-17040 REV.A. NO FURTHER DEFECTS FOUND.</SPAN></P>)

Part: STRUCTURE — TORN (ZONE 600 FLAP) · airframe 52,385 hrs · 7,765 cycles

RHW #18 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,385 hrs · 7,765 cycles

M/D - STA 1815-1835 LBL 11 SEAT TRACK CROWN AREA FOUND CORRODED.(<P><SPAN>M/D STA 1815-1835 LBL 11" SEAT TRACK CORROSION CLEANED UP AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND MEASURED AFTER SMOOTHED OUT WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS REV.43 DATE 20 JUN 2024. NO FURTHER DEFECT NOTED.</SPAN></P>)

Part: STRUCTURE — TORN (ZONE 600 FLAP) · airframe 52,385 hrs · 7,765 cycles

RHW #21 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,385 hrs · 7,765 cycles

M/D STA 1835-1852 LBL 11 SEAT TRACK CROWN AREA FOUND CORRODED.(<P><SPAN>M/D STA 1835-1852 LBL 11" SEAT TRACK CORROSION CLEANED UP AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01 AND MEASURED AFTER SMOOTHED OUT WITHIN SRM 53-00-52-1A-1 ALLOWABLE DAMAGE 1 FIG 101 LIMITS REV.43 20JUN2024. NO FURTHER DEFECT NOTED.

Part: SUPPORT RIB — BROKEN (ZONE 600) · airframe 52,385 hrs · 7,765 cycles

RHW #16 K/FLAP AREA FWD L/E D-BEAM INNER SUPPORT RIB BROKEN.(<P><SPAN>RH #16 K/FLAP AREA FWD L/E D-BEAM INNER SUPPORT RIB BROKEN FABRICATED IAW RI-57-00-17048 REV.A AND REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV.43. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRINGER — CRACKED (ZONE 200) · airframe 52,385 hrs · 7,765 cycles

AFT OF 2598 BULKHEAD, S-4R STRINGER CRACKED.(<P><SPAN>AFT OF 2598 BULKHEAD, S-4R STRINGER REPAIRED IAW RI-53-80-17041 REV.A. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: STRUCTURE — TORN (ZONE 600 FLAP) · airframe 52,385 hrs · 7,765 cycles

RHW #19 V/C FLAP LSA FOUND TORN.(<P><SPAN>PERFORMED REPAIR AT LSA TORN AREA IAW CMM 57-55-42 REPAIR 17-1. NO FURTHER DEFECTS NOTED.</SPAN></P>)

Part: CHANNEL — CRACKED (ZONE 300) · airframe 52,385 hrs · 7,765 cycles

L/H HORI. STAB. T/E U-CHANNEL FOUND CRACKED.(<P>PERFORMED PERMANENT REPAIR AS PER HX RI NO:RI-55-10-17039 REV.A .NO FURTHER DEFECTS NOTED.</P>)

Part: LAMP — INOPERATIVE · airframe 43,745 hrs · 6,506 cycles

DR #1 CEILING AFT EMER LT FOUND INOP(<P>DR #1 CEILING EMER LT REPLACED AND LAMP TEST PASS IAW AMM 33-51-07 REV 38 15MAR2022</P>)

Part: BATTERY PACK — INOPERATIVE · airframe 43,745 hrs · 6,506 cycles

EMER LT BATTERY PACK (M5170) FOUND STAY ON LESS THAN 15 MIN(EMER LT BATTERY PACK M5170 REPLACED & TESTED NORMAL AS PER AMM 33-51-04</P>)

Part: FLAP — PEELING · airframe 43,745 hrs · 6,506 cycles

LH W - #10 VC-FLAP SURFACE LSA FOUND PEELING OFF(REPAIR PERFORMED AS PER SRM 51-70-04 REPAIR7)

Part: FLAP — PEELING · airframe 43,745 hrs · 6,506 cycles

RH W - #18 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)

Part: WEB — CRACKED · airframe 43,745 hrs · 6,506 cycles

RH W L/E BEAM VERTICAL WEB FOUND CRACKED AT ILES 518 TO ILES 523(<P>RH W L/E NOSE BEAM VERTICAL WEB ILES 518 TO ILES 523 CRACK AREAS REPAIRED IWA RI-57-41-15746 REV A.&NBSP;</P>)

Part: FLAP — PEELING · airframe 43,745 hrs · 6,506 cycles

RH W #20 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)

Part: FLAP — PEELING · airframe 43,745 hrs · 6,506 cycles

RH W - #21 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)

Part: FLAP — PEELING · airframe 43,745 hrs · 6,506 cycles

LH W - #9 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)

Part: FLAP — PEELING · airframe 43,745 hrs · 6,506 cycles

LH W - #7 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)

Part: FLAP — PEELING · airframe 43,745 hrs · 6,506 cycles

LHW - #8 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)

Part: BATTERY PACK — INOPERATIVE · airframe 43,745 hrs · 6,506 cycles

EMER LT BATTERY PACK (M5168) FOUND STAY ON LESS 15 MIN(EMER LT BATTERY PACK (M5168) REPLACED & TESTED NORMAL AS PER AMM 33-51-04</P>)

Part: FLAP — PEELING · airframe 43,745 hrs · 6,506 cycles

RH W - #19 VC-FLAP SURFACE LSA FOUND PEELED OFF(REPAIR PERFORMED AS PER CMM 57-55-42 REPAIR17-1)

Part: FRAME — CRACKED · airframe 43,745 hrs · 6,506 cycles

APU - APU COMPT STA 2664 L/H WL 310 FRAME FOUND CRACKED.(<P>APU - APU COMPT STA 2664 L/H WL 305-310 FRAME CRACK AREA REPAIRED IAW RI-53-00-15765 REV.A</P>)

Part: BATTERY PACK — INOPERATIVE · airframe 43,745 hrs · 6,506 cycles

EMER LT BATTERY PACK (M5169) FOUND STAY ON LESS THAN 15MIN(EMER LT BATTERY PACK M5169 REPLACED &TESTED NORMAL IAW AMM 33-51-04</P>)

Part: WEB — CRACKED · airframe 43,745 hrs · 6,506 cycles

LH W L/E BEAM VERTICAL WEB FOUND CRACKED AT ILES 456 TO ILES 470(<P>LH W L/E NOSE BEAM VERTICAL WEB ILES 456 TO ILES 470 CRACK AREAS REPAIRED IAW RI-57-41-15747 REV.A</P>)

Part: SKIN — DELAMINATED · airframe 43,745 hrs · 6,506 cycles

LH W - O/B T/E FLAP AFT EDGE AREA FOUND DELAMINATION ON UPPER SKIN(REPAIR PERFORMED AS PER SRM 51-70-04 REPAIR1)

Part: SWITCH — NONE · airframe 42,149 hrs

DURING T/O ROLL: EICAS MSG "FUEL PRESS ENG 2"(<P ><SPAN>&NBSP;</SPAN><SPAN>REMOVED AND REPLACED #2 FWD BOOST PUMP PRESSURE SWITCH, S65, IAW B747 AMM 28-42-01, OPS CHECK AND LEAK CHECK GOOD. REMOVED AND REPLACED #2 ENG FUEL FILTER AND STRAINER REPLACEMENT IAW B747 AMM&NBSP; 73-11-02, LEAK CHECK GOOD.&NBSP; &NBSP;PERFORMED HIGH POWER ENGINE RUN&NBSP; IAW B747 AMM 71-00-00, NO DEFECTS NOTED. PERFORMED HIGH ENERGY STOP INSPECTION IAW B747 AMM 05-51-10, NO DEFECTS NOTED.&NBSP;</SPAN></P>)

Part: PUMP — NONE · airframe 42,110 hrs

RTO DUE TO EICAS MSG FUEL PRESS ENG 2 AND FUEL PUMP 2 FWD(<P ><SPAN>PERFORMED HIGH ENERGY STOP INSPECTION PER AMM 05-51-10-202-001, NO DEFECTS NOTED.</SPAN></P> / <P >&NBSP;</P> / <P ><SPAN>REMOVED AND REPLACED #2 MAIN FWD BOOST PUMP PER AMM 28-22-03-400-801. #2 ENG RUN PERFORMED PER AMM 71-00-00, LEAK CHECK GOOD. NO DEFECTS NOTED.</SPAN></P> / <P>&NBSP;</P>)

Part: ACTUATOR — FAULTED (RUDDER) · airframe 41,577 hrs · 6,168 cycles

"RUDDER RATIO SNGL" EICAS MESSAGE. PERFORMED WIRING CHECK OF WIRING BETWEEN RUDDER RATIO ACTUATOR AND YSM PER IFIM TASK 27-21-00-810-844 AND WDM 27-21-31. NO FAULTS NOTED. RUDDER RATIO ACTUATOR REPLACED IAW B747 AMM 27-21-12/401, OPS CHECK GOOD. RUDDER RATIO L & R GROUND TEST GOOD IAW B747 AMM 27-21-00-720-810.

Part: FAIRING — MISSING (TE FLAP) · airframe 36,696 hrs · 5,414 cycles

THE NR 2 TRAILING EDGE FLAP FAIRING MISSING. A/C DISPATCHED IAW CDL 27-51-02, MDDR 140129.

Part: FAIRING — MISSING (NR 2 FLAP TRACK)

ON 27 DECEMBER 2020, WHEN POLAR N852GT LANDED AT PVG (PUDONG AIRPORT) SHANGHAI, THE NR 2 FLAP TRACKING FAIRING WAS FOUND MISSING DURING WALK AROUND CHECK. THE OPERATOR WAS NOTIFIED. AFTER THAT, THE AIRCRAFT OPERATION CONTROL CENTER OF THE AIRPORT TOLD OPERATOR THAT THE MISSING PART WAS FOUND OUTSIDE THE END OF THE RUNWAY. FOLLOWED POLAR MCC'S INSTRUCTION, WE REMOVED REMAINING PARTS, CHECKED RELATED AREA AND NO FURTHER DAMAGE WAS FOUND. WE PERFORMED FLAP SYSTEM OPERATION CHECK, ALL NORMAL AND ITEM DEFERRED PER CDL.

Part: TRANSDUCER — MALFUNCTIONED (NLG STEERING) · airframe 36,096 hrs · 5,320 cycles

REJECTED TAKE OFF "CONFIG GEAR CENTER". PERFORMED A/P 18105 NOSE/WHEEL STEERING ADJUSTMENT, PER AMM 21-51-00-835-001 AND BGS ADJUSTMENT, PER AMM/32-53-00-705-001. BITE CHECK FAILED-STEERING TRANSDUCER VALUE ERRATIC. R & R BGS/INPUT TRANSDUCER, PER AMM 32-53-01. OPERATIONS CHECKED NORMAL. TOWED A/C AROUND, PER AMM 09-11-00 AND 32-53-00. OPERATIONS CHECKS NORMAL.

Part: SENSOR — FALSE INDICATION (BG TILT) · airframe 35,852 hrs · 5,284 cycles

UPON POWER UP CONFIG GEAR CENTER MESSAGE AND GEAR MONITOR STATUS MESSAGE. REMOVED AND REPLACED BODY GEAR TRUCK TILT SENSOR EQUIP 56R, IAW AMM 32-61-21.

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 35,738 hrs · 5,267 cycles

BTB. DURING INITIAL TAKEOFF ROLL (25 KTS). EICAS WARNING CONFIG GEAR CENTER ACTIVATED. ABORTED T/O AND WARNING CEASED IMMEDIATELY. WE ATTEMPTED TAKEOFF AGAIN. WARNING REPEATED PLACED ON DMI, MEL REF 32-53-01, MDDR NR 135599.

Part: STATUS MESSAGE — FALSE ACTIVATION (BDY GEAR STEER) · airframe 35,517 hrs · 5,229 cycles

BODY GEAR STEERING STATUS MESSAGE. PERFORMED GROUND TEST, PER AMM 32-53-11. PASSED MESSAGE CLEARED. A/C OK FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (MLG CONFIG) · airframe 35,517 hrs · 5,229 cycles

LOW SPEED REJECTED TAKE OFF DUE TO WARNING ALERT CONFIG GEAR CTR EICAS MESSAGE. DEFERRED BODY GEAR STEERING, PER MEL 32-53-01 DDG. C/W MDDR 135044.

Part: WARNING MESSAGE — ILLUMINATED (NLG STEERING) · airframe 35,065 hrs · 5,161 cycles

CONFIG GEAR CTR WARNING MESSAGE(DEFERRED BODY GEAR STEERING IAW MEL 32-53-01, MDDR;133277, CAT 'C').

Part: FLAP — INFLT SEPARATION (LE) · airframe 35,051 hrs · 5,159 cycles

FLAPS DRIVE DISPLAYED WHEN FLAP 1 SELECTED. STATUS MESSAGE FLAP SYSTEM MONITOR. WALKAROUND FOUND #6 LE VC FLAP PANEL MISSING #1 INBD T/R DAMAGE. INSPECTION OF ADJACENT ARE FOUND DAMAGED AT ILES 1100 LE PANEL.(INSTALLED MISSING #6 LE FLAP PANEL / IAW B747 AMM 27-81-02, REPAIRED #1 ENGINE INBD T/R IAW B747;SRM 57-41-01 AND / 51-70-04;REPAIRED LE PANEL AT ILES 1100 IAW B747 SRM 54-30-01-2R-9 / REPAIR 9 AND 51-70-04.

Part: FITTING — WORN (L1 DOOR) · airframe 34,415 hrs · 5,057 cycles

FOUND L1 ENTRY DOOR FWD UPPER ROLLER LATCH FITTING WORN. IAW AMM 52-11-01-700-801 REV 32, REPLACED L1 ENTRY DOOR FWD UPPER ROLLER LATCH FITTING. IAW AMM 52-11-01-700-801 REV 32 ADJUST LATCH AND LATCH FITTING AT L1 DOOR FWD UPPER ROLLER LATCH FITTING. CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,415 hrs · 5,057 cycles

CRACK DAMAGES ON THE STRINGER S-11R BETWEEN STA 880 AND STA 890. ACCOMPLISHED EI NO T2020A53M-1657 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,415 hrs · 5,057 cycles

CRACK DAMAGES ON THE STRINGER S-11L BETWEEN STA 840 AND STA 890. ACCOMPLISHED EI NO T2020A53M-1650 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,415 hrs · 5,057 cycles

CRACK DAMAGES ON THE STRINGER S-10L BETWEEN STA 860 AND STA 880. ACCOMPLISHED EI NO T2020A53M-1652 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: SKIN — GOUGED (FUSELAGE) · airframe 34,415 hrs · 5,057 cycles

GOUGE DAMAGE ON FUSELAGE SKIN OUTER SURFACE AT STA 481, BETWEEN S-45L AND S-46L. REPAIRED THE DAMAGED AREA IAW EI NR T2020A53M-1666 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,415 hrs · 5,057 cycles

CRACK DAMAGE ON THE STRINGER S-8R BETWEEN STA 940 AND STA 950. ACCOMPLISHED EI NO T2020A53M-1659 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,415 hrs · 5,057 cycles

CRACK DAMAGES ON THE STRINGER S-7R BETWEEN STA 880 AND STA 890 AND BETWEEN STA 940 AND STA 970. ACCOMPLISHED EI NO T2020A53M-1655 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,415 hrs · 5,057 cycles

CRACK DAMAGES ON THE STRINGER S-9L BETWEEN STA 870 AND STA 930. ACCOMPLISHED EI NO T2020A53M-1651 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,415 hrs · 5,057 cycles

CRACK DAMAGES ON THE STRINGER S-8L BETWEEN STA 950 AND STA 960. ACCOMPLISHED EI NO T2020A53M-1658 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 34,415 hrs · 5,057 cycles

CRACK DAMAGES ON LT SIDE HST TIP RIB AT HSBL 421.5. REPAIRED DAMAGED AREA IAW EI NO T2020A55M-1660 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,415 hrs · 5,057 cycles

CRACK DAMAGES ON THE STRINGER S-7L BETWEEN STA 910 AND STA 970. ACCOMPLISHED EI NO T2020A53M-1654 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRUCTURE — BROKEN (FUSELAGE) · airframe 34,415 hrs · 5,057 cycles

BROKEN DAMAGE ON FRAME UPPER CAP OF FWD CARGO FLOOR STRUCTURE, AT STA 980 RBL 10. REPAIRED THE DAMAGED AREA IAW EI NO T2020A53M-1668 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 34,415 hrs · 5,057 cycles

CRACK DAMAGES ON THE STRINGER S-12L BETWEEN STA 880 AND STA 890. ACCOMPLISHED EI NO T2020A53M-1653 REV 1. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,372 hrs · 5,051 cycles

DURING TAKEOFF ROLL APPROX AT 50 KNOTS WE GET A MASTER WARNING WITH A CONFIG GEAR EICAS MESSAGE. TAKE OFF DISCONTINUED. PERFORMED PSEU TEST PRI ALT GEAR SYSTEMS PASS. DEFERRED BODY GEAR STEERING IAW MEL 32-53-01. CAT C DDG COMPLIED WITH MDDR 128957.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 30,290 hrs · 4,427 cycles

REJECTED TAKEOFF DUE TO EICAS MSG "CONFIG GEAR CTR". SECOND TAKEOFF ATTEMPT OKAY. PLEASE NOTE PREVIOUS WRITE-UPS.(<P>NO EICAS MSG AND CMC PLF/EF MSG NOTED, BUT FOUND CMC MSG 32063 FROM FAULT HISTORY. ITEM DEFERRED PER MEL 32-53-01, CAT 'C', MDDR #113933. T/I: 0416 CC; INSTALLED PLACARD AND MCC NOTIFIED. COMPLIED WITH "M" PROCEDURE.</P>)

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 30,154 hrs · 4,408 cycles

WHEN SETTING T/O THRUST, ''CONFIG GEAR CTR'' WARNING. 2 ATTEMPTS TO DEPART, SAME RESULT. CHECKED AND FOUND CMC MSG 32066.

Part: SUPPORT — CRACKED (NR 3 PYLON) · airframe 25,265 hrs · 3,678 cycles

NR 3 PYLON CAVITY VAPOUR BARRIER, OTBD FWD SUPPORT CRACKED. REPAIRED IAW RI-57-41-12749, REV A. INTERIM REPAIR.

Part: BRACE — BROKEN (RT WING LE) · airframe 25,265 hrs · 3,678 cycles

RIGHT WING ILES 440, LEADING EDGE BRACE WAS BROKEN. FABRICATED AND REPLACED IAW RI-57-41-12740, REV A. INTERIM REPAIR.

Part: SUPPORT BEAM — CRACKED (RT WING) · airframe 25,265 hrs · 3,678 cycles

RIGHT WING FIXED LEADING EDGE AT ILES 434.51, THE LOWER SUPPORT BEAM WAS CRACKED. REPAIRED IAW RI-57-41-12740, REV A.

Part: RIB — CRACKED (RT WING LE) · airframe 25,265 hrs · 3,678 cycles

RIGHT WING, ILES 440, LEADING EDGE RIB WAS FOUND CRACKED. REPAIRED IAW RI-57-41-12740, REV A. INTERIM REPAIR.

Part: STRUCTURE — DAMAGED (BS 2484-2486) · airframe 25,265 hrs · 3,678 cycles

WHILE ACCOMPLISHED EO 4853A024 PART 1, STEP 4 FOUND A FASTENER HOLE OVERSIZED BS 2484 - 2486, REPAIRED IAW RI-53-00-12745, REV A.

Part: TOILET — INOPERATIVE (LAVATORY) · airframe 20,398 hrs · 2,924 cycles

CREW REPORTED TOILET WOULD NOT OPERATE IN FLIGHT. AIRCRAFT RETURNED TO DEPARTURE AND THE SYSTEM WAS RESET AND RESTORED IAW AMM 38-32-06.

Part: UNKNOWN — ODOR (LAVATORY) · airframe 17,544 hrs · 2,498 cycles

SMELL BURNING ODOR IN LAV, HAS AN ELECTRICAL ODOR TO IT. OPENED PANELS AND INSPECTED LAVATORY. NO ABNORMAL ODORS FOUND IAW AMM 38-00-00, AMM 05-51-56.

Part: PANEL — CRACKED (RT WING) · airframe 17,541 hrs · 2,497 cycles

RIGHT WING UPPER T/E PANEL FOUND CRACKED. REPAIRED IAW RI NO= RI-57-51-11481 REV A.

Part: ACCESS PANEL — DAMAGED (LT WING) · airframe 17,541 hrs · 2,497 cycles

NR 2 PYLON OTBD WING ACCESS PANEL 521AB AFT BRACKET FOUND CRACKED. REPAIRED IAW RI-57-41-11488 REV A.

Part: STRUCTURE — CRACKED (RT WING TE FLAP) · airframe 17,541 hrs · 2,497 cycles

RT WING NR 17 V/C FLAP BULLNOSE OTBD EDGE FOUND CRACKED. REPAIRED IAW SRM 51-70-04 REPAIR 5.

Part: SKIN — CRACKED (BS 2674-2698) · airframe 17,541 hrs · 2,497 cycles

APU COMPARTMENT BS 2674 - 2680, WL 305 SKIN FOUND CRACKED. REPAIRED IAW RI-53-87-11493 REV A.

Part: SUPPORT FRAME — CRACKED (BS 2696) · airframe 17,541 hrs · 2,497 cycles

APU COMPARTMENT BS 2696 WL 292 LOWER SUPPORT FRAME FOUND CRACKED. REPAIRED IAW RI-53-82-11487 REV A.

Part: PANEL — CRACKED (LT WING) · airframe 17,541 hrs · 2,497 cycles

LT WING UPPER T/E PANEL FOUND CRACKED. REPAIRED IAW RI NO= RI-57-51-11481 REV A.

Part: SWITCH — MALFUNCTIONED (THROTTLE) · airframe 11,759 hrs · 1,624 cycles

EXITING RUNWAY, ALL 4 THROTTLES ADVANCED TO FULL POWER, UNCOMMANDED, NO PREV HISTORY NOTED, MSG 22466, GO ARROUND SWITCHES CYCLED, AND FCC LCR GROUND TEST PASSED IAW MM 22-10-00, REF LOG PAGE 700573, ITEM 12, GO ARROUND SWITCH IS REPLACED AS PRECAUTIONARY.

Part: SKIN — DAMAGED (BS 360) · airframe 8,554 hrs · 1,177 cycles

LIGHTNING STRIKE ON RT SIDE AND FORWARD OF COCKPIT SKIN. DESCENDING THROUGH 19,500 FEET. LIGHTING STRIKE INSPECTION CARRIED OUT IAW AMM 05-51-13. FOUND BURN MARK AT FUSELAGE BS 360 BETWEEN STRINGERS 23 - 24R. FOUND WITHIN SRM 53-00-01 ALLOWABLE DAMAGE LIMITS. AREA BLENDED SRM 53-00-01, FIG 201, REPAIR 9.

Part: SKIN — DAMAGED (BS 320) · airframe 8,554 hrs · 1,177 cycles

LIGHTNING STRIKE ON RT SIDE AND FWD OF COCKPIT SKIN. DESCENDING THROUGH 19,500 FEET. FASTENER AT BS 320, STRINGER S25R FOUND DAMAGED. TEMPORARY REPAIR ACCOMPLISHED IAW SRM 53-00-01-2R-9, REPAIR 9, PARA 5.

Part: FAIRING — CRACKED (LT WING) · airframe 8,298 hrs · 1,141 cycles

LEFT WING NR 4 FIXED FAIRING PANEL NR 571AB INBD SUPPORT BEAM AFT & END FOUND CRACKED, SUPPORT BEAM REPAIR CARRIED OUT IAW RI-57-51-10611.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 776 hrs · 116 cycles

FIRE WHEEL WELL EICAS MESSAGE DISPLAYED IMMEDIATELY AFTER LIFT OFF. MESSAGE CLEARED BY ITSELF IN APPROX 10 SECONDS. LT THE GEAR DOWN AND ACCOMPLISHED NON NORMAL PROCEDURES EXCEPT GEAR RAISED AFTER APPROX 4 MINUTES. ALL INDICATIONS NORMAL INCLUDING VISUAL INSPECTION OF MAIN DECK. THE ONLY UNUSUAL ITEM NOTED WAS A BRAKE TEMP INDICATION IN BOTH THE RT WING AND BODY GEAR BRAKES OF .5 TO .8. ALL LT BRAKES WERE 0. FLIGHT CONTINUED TO DESTINATION. INSPECTED WHEELWELL AREA FOR DUCT LEAKS. INSPECTED OVERHEAT LOOPS, NO DEFECTS NOTED. PERFORMED CMC GROUND TEST IAW MM 26-1-00, TEST PASSED, RAN ALL 3 PACKS.

Part: NUT PLATE — DAMAGED (NR 3 PYLON) · airframe 76 hrs · 20 cycles

NR 3 PYLON T/E FAIRING HAS TWO NUTPLATES DAMAGED. PERFORM A TIME LIMITED REPAIR.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 61 hrs · 17 cycles

HYD QTY LOW 2 & HYD PRESSURE ENG 2 EICAS MESSAGES. ON INSPECTION IT WAS FOUND THAT THERE WAS HYD FLUID LEAKING FROM ENG 2 DRAIN MAST, FOR THE ENGINE DRIVEN HYD PUMP. NR 2 EDP REPLACED IAW AMM 29-11-05. DURING LEAK CHECK, A LEAK WAS ALSO FOUND AT THE RT INBD AILERON ACTUATOR PRESSURE LINE. TEMPORARY FLEX LINE INSTALLED IAW EO 4829A001 AND LEAK CHECK WAS GOOD.