N487MC

Part: SKIN — PUNCTURED (ZONE 500 FLAP) · airframe 101,884 hrs · 18,556 cycles

LEFT WING INBD AFT FLAP LE ENGINE LOWER SURFACE HAS A PUNCTURE. 36" OUTBD OF ACCORDION SEAL. REPAIRED SMALL PUNCTURE 1/2" ON LH INBD AFT FLAP LEADING EDGE 501/2" FROM ACCORDION SEAL AND 361/4" FROM TRAILING EDGE PER B747-400 SRM 51-70-07-0G-0 PG. 15 A. NO FURTHER DEFECTS NOTED.

Part: SKIN — DAMAGED (ZONE 500 FLAP) · airframe 101,884 hrs · 18,556 cycles

LT WING OTBD FORE FLAP OTBD END LOWER SURFACE L/E DAMAGED ABOUT 6 INCHES INBD OF OTBD EDGE(<P>PERMANENT COMPOSITE REPAIR MADE TO LH WING OTBD FORE FLAP LOWER SURFACE 9" FORM OTBD EDGE AND 19" FORM LOWER EDGE. SIZE AFTER REPAIR L 5" W 4" PER B747-400 SRM 51-70-07 PAR. 4C, E, F, G. NO FURTHER DEFECTS NOTED</P>)

Part: VALVE — FAULTED (NR 4) · airframe 101,653 hrs · 18,522 cycles

BLEED 4 CAUTION MSG ON CLIMB OUT. MSG 36229. REPLACED NR 4 PRVC AND CHECKED NORMAL PER AMM 36-11-20/401 &AMP; IPC 36-11-19-01</P>)

Part: AUDIO PANEL — ODOR (ZONE 200) · airframe 100,376 hrs · 18,326 cycles

STRONG SMELL OF BURNING WIRE IN COCKPIT DURING PREFLIGHT. PERFORMED SMOKE OR FUME IN CABIN INSPECTION IAW FIM 21-00TASK 810. FOUND F/O CONTROL AUDIO PANEL BAD WITH ODOR. R/R PANEL IAW AMM 23-51-11. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. HAPPENED ON GROUND.

Part: WEB — CRACKED (ZONE 500) · airframe 99,897 hrs · 18,249 cycles

LEFT WING T/E CAVITY SUPPORT RIB WEB AT NR 5 SPOILER INBD LWR WBL 432.65 FOUND CRACKED. LT WING T/E CAVITY SUPPORT RIB WEB (P/N: 6565B10865-26) AT NR 5 SPOILER INBD LWR WBL 432.65 REPLACED IAW RI-57-70-17735 REV. A. NO FURTHER DEFECTS NOTED.

Part: PACKING — LEAKING (PRESSURE SWITCH) · airframe 98,464 hrs · 18,017 cycles

ENG 2 OIL QTY DROPPED FROM 20Q TO 9Q, FOLLOWED BY A DROP FROM 8 TO 7 TO 6 ABOUT EVERY HALF HOUR. FOUND ENG #2 LOW PRESSURE WARNING SWITCH PACKING INSTALLED IN WRONG POSITION. INSTALLED NEW PACKING PER AMM 79-33-01 PERFORMED ENG #2 POWER PER AMM 71-00-00. AMM ENG INDICATIONS LEAK CHECK GOOD.

Part: WINDOW — LEAKING (ZONE 200) · airframe 97,867 hrs · 17,924 cycles

CLIMBING THROUGH 18,000' AND 6 PSI DIFFERENTIAL. A LOUD SQUEAL BEGAN FROM ONE OF THE CAPTAIN SIDE WINDOWS. DIFFICULT TO ASCERTAIN WHICH WINDOW BUT IT SEEMINGLY IS LOUDEST FROM THE L2 WINDOW. FUEL JETTISON ACCOMPLISHED AND RETURN TO ZAZ.(<P>WINDOW NO 2 LH REPLACED IAW AMM 56-11-02. CABIN PRESSURE LEAKAGE TEST PERFORMED IAW AMM 05-51--08/201. REPLACED RH WINDSHIELD WASHER NOZZLE CHECK VALVE IAW AMM 30-44-00. RH WINDSHIELD WASHER SOLENOID REPLACED IAW AMM 30-44-01.&NBSP;</P>)

Part: SMOKE DETECTOR — FAULTED · airframe 96,870 hrs · 17,771 cycles

DURING CRUISE FL310 EICAS CAUTION EQUIPMENT COOLING PERFORMED NNC, MESSAGE BLANKED, SMELLED ELECTRICAL BURNING, DIVERTED TO CTS.(<P>CMC REPORTED MX MSG 21422. R/R E/E COOLING SMOKE DET AND GND TEST PASSED. SET THE A/C TO AIR MODE AND KEPT THIS MODE FOR 3 HOURS AND NO EICAS MSG WAS OBSERVED PER AMM 21-58-00/801. PERFORMED GVI FOR WHOLE RH RISER DUCTS/ADJACENT WIRES AND NO DEFECTS FOUND. PERFORMED GVI FOR INSIDE OF P129, FOUND TERMINAL INSULATORS HAVE DISCOLORED ON TRANS (T187), ALSO TOO HOT. R/R TRANS (T187) PER WDM 33-35-24 P1. PER MCC REQEST, PERFORMED GVI E/E COOLING SUPPLY FAN / EXHAUST AND NO DEFECTS FOUND PER AMM 21-58-00-206-007.</P>)

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 500) · airframe 96,792 hrs · 17,758 cycles

LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: FRAME — CRACKED (ZONE 200) · airframe 96,792 hrs · 17,758 cycles

LEFT BS 2231 STR 16L FRAME FWD INNER CHORD 1EA FASTENER HOLE CRACK. FRAME FWD INNER CHORD REPAIRED AS PER SRM 53-60-15-2R-2 REPAIR 2 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED.

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 96,792 hrs · 17,758 cycles

LEFT HORIZONTAL STAB OTBD TE AFT WEDGE FWD CHANNEL OTBD UPPER FLANGE, 1EA FASTENER HOLE CRACKED. WEDGE FWD CHANNEL REPLACED AS PER RI-55-10-6987 REV.A. NO FURTHER DEFECTS NOTED.

Part: TENSION TIE — CRACKED (ZONE 100) · airframe 96,792 hrs · 17,758 cycles

RH BS840 UPPER DECK TENSION TIE 1EA FASTENER HOLE CRACK AT AFT CHANNEL.(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DENTED (ZONE 200) · airframe 96,792 hrs · 17,758 cycles

FUSELAGE SECTION 41 DENT/NICK DAMAGE FOUND ON FUSELAGE SKIN (PN 65B12874) AT STA 284 APPROXIMATELY NEAR STR 10R(<P>DAMAGE AREA REPAIRED AS PER RI-53-10-16982 REV.A (CAT A). NO FURTHER DEFECTS NOTED.</P>)

Part: FRAME — CRACKED (ZONE 200) · airframe 96,792 hrs · 17,758 cycles

RIGHT BS880 UPPER DECK TENSION TIE ATTACHED TO FRAME FOUND 2EA FASTENER HOLES CRACK. FRAME REPAIRED AS PER EO 4453A301 R12 PART 6 STEP 9F AND SRM 53-20-07-2R-5 REPAIR 5 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED.

Part: SKIN — DELAMINATED (ZONE 500) · airframe 96,792 hrs · 17,758 cycles

LHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REAPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 500) · airframe 96,792 hrs · 17,758 cycles

LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 96,792 hrs · 17,758 cycles

CENTER FUSELAGE REAR WEB AT RBL 94" FND O/B BONDING ATT POINT CORROSION. CORROSION AREA REPAIRED AS PER RI NO: RI-57-10-17000 REV A. NO FURTHER DEFECTS NOTED.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: FRAME — CHAFED (NR 4 NACELLE) · airframe 96,792 hrs · 17,758 cycles

NUMBER 4 ENGINE RT CORE COWL FRAME NR 2 MID AREA FOUND CHAFING MARK, COUNT FROM FWD. FRAME REPAIRED IAW EA-1971A141 REV.0 DATE 01 JUL 24. NO FURTHER DEFECTS NOTED.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (ZONE 500) · airframe 96,792 hrs · 17,758 cycles

RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: TENSION TIE — CRACKED (ZONE 100) · airframe 96,792 hrs · 17,758 cycles

LH BS760 UPPER DECK TENSION TIE 1EA FASTENER HOLE CRACK FOUND AT AFT CHANNEL.(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 96,792 hrs · 17,758 cycles

LHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: FRAME — DAMAGED (ZONE 200) · airframe 96,792 hrs · 17,758 cycles

M/D LH STA 940 FRAME FASTENER HOLE BTN STR 8L-9L FOUND PREVIOUSLY FREEZE PLUG HOLE REPAIR.(<P>FRAME REPLACEMENT CARRIED OUT AS PER SRM 51-10-02, NEW FRAME HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW FRAME INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

RHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 96,792 hrs · 17,758 cycles

LHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — ERODED (RUDDER) · airframe 96,792 hrs · 17,758 cycles

LWR RUDDER LH FOUND EROSION(<P>PERFORMED REPAIR AT EROSION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 500) · airframe 96,792 hrs · 17,758 cycles

LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: FITTING — CRACKED (ZONE 200) · airframe 96,792 hrs · 17,758 cycles

ONE CRACK WAS FOUND AT INTERCOSTAL LUG FITTING APPROX 1 1/4" IN LENGTH ON RH STA 1000 RBL 11.33. INTERCOSTAL LUG FITTING REPLACED REFER ATLAS AIR EO 4453C024 REV 4 PART 7 STEP 3 CONDITION 11. NO FURTHER DEFECTS NOTED.

Part: RETAINER — DAMAGED (RUDDER DEFLECTOR) · airframe 96,792 hrs · 17,758 cycles

LWR RUDDER, RH LWR DEFLECTOR SEAL RETAINER RAIL BRACKETS FOUND DAMAGE(<P>FWD RETAINER REPLACED AS PER RI-53-51-16996 REV.A, AFT RETAINER REPLACED AS PER SRM 51-10-02, NEW RETAINER HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW RETAINER INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

LHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

RHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (ZONE 500) · airframe 96,792 hrs · 17,758 cycles

LHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: SUPPORT — CRACKED (LT WING) · airframe 96,792 hrs · 17,758 cycles

LHW LWR SURFACE REFUELING ACCESS DOORS FWD FIXED PNL FWD PNL SUPPORT FOUND CRACK. SUPPORT REPAIRED AS PER SRM 57-41-13-2R-3 REPAIR 13 FIG 201 (CATEGORY A). NO FURTHER DEFECTS NOTED.

Part: TENSION TIE — CRACKED (ZONE 100) · airframe 96,792 hrs · 17,758 cycles

RH BS760 UPR DECK TENSION TIE 1EA FASTENER HOLE CRACK FOUND AT AFT CHANNEL.(<P>TENSION TIE REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

LHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (ZONE 500) · airframe 96,792 hrs · 17,758 cycles

LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: ANGLE — CRACKED (LT WNG FUEL DOOR) · airframe 96,792 hrs · 17,758 cycles

LHW L/E REFUEL DOOR FWD ZEE FOUND CRACK.(<P>PERFORMED REPAIR AT CRAKCK AREA AS PER RI-57-00-16992 REV.A NO FURTHER DEFECTS NOTED</P>)

Part: FRAME — CRACKED (NR 2 NACELLE) · airframe 96,792 hrs · 17,758 cycles

#2 ENG L/H CORE COWL MOST AFT FRAME FOUND CRACK.(<P>FRAME CRACK AREA REPAIRED AS PER SRM 54-45-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED</P>)

Part: FAILSAFE — CRACKED (ZONE 200) · airframe 96,792 hrs · 17,758 cycles

RIGHT BS 880 UPPER DECK FRAME FAIL SAFE CHORD 1EA FASTENER HOLE CRACKED.FAIL SAFE CHORD REPAIRED AS PER EO 4453A301 R12 PART 6 STEP 9F AND SRM 53-20-07-2R-5 REPAIR 5 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED.

Part: BULKHEAD WEB — CRACKED (NLG WW) · airframe 96,792 hrs · 17,758 cycles

BS 260 NLG W/W FWD BULKHEAD WEB R/H LOWER CORNER ONE FASTENER HOLE CRACKED. WEB REPAIRED AS PER RI-53-15-16983 REV.A. NO FURTHER DEFECTS NOTED,

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

LHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: FRAME — CRACKED (NR 2 NACELLE) · airframe 96,792 hrs · 17,758 cycles

#2 ENG L/H CORE COWL #2 FRAME (COUNT FROM FWD) FOUND CHAFING MARK.(<P>#2 FRAME CHAFING MARK AREA REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG 201. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (ZONE 500) · airframe 96,792 hrs · 17,758 cycles

LHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DENTED (ZONE 300) · airframe 96,792 hrs · 17,758 cycles

R/H I/B ELEVATOR FOUND DENT(<P>PERFORMED REPAIR AT DENT AREA PER SRM 51-70-06 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 500) · airframe 96,792 hrs · 17,758 cycles

LHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

LHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: STRUCTURE — CHAFED (RUDDER) · airframe 96,792 hrs · 17,758 cycles

LWR RUDDER L/H LWR CHORD FOUND CHAFING(<P>LWR CHORD CHAFING AREA REPAIRED AS PER RI-55-40-17002 REV.B. NO FURTHER DEFECTS NOTED.

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 96,792 hrs · 17,758 cycles

LHW I/B FORE FLAP FOUND DELAMINATION. PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.

Part: FAIRING — CRACKED (LT AILERON) · airframe 96,792 hrs · 17,758 cycles

LHW O/B AILERON O/B LWR L/E FAIRING FOUND CRACK(<P>L/E SKIN LOCAL FABRICATED AS PER BOEING DWG: 65B02108 AND PL AND NEW SKIN HOLES TRANSFERRED AS PER SRM 51-40-05 AND NEW SKIN INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

RHW O/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: FRAME — CRACKED (ZONE 100) · airframe 96,792 hrs · 17,758 cycles

APU COMPARTMENT RT STA 2685 WL 325 FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1 FIG 201 (CAT A). NO FURTHER DEFECTS NOTED.

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 96,792 hrs · 17,758 cycles

LHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

RHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: FITTING — CORRODED (RT WING) · airframe 96,792 hrs · 17,758 cycles

RHW LWR WING L/E COMPOSITE PANEL FOUND BULGED AT OLES 1390(<P>FITTING REPLACED AND INSTALLED AS PER RI-57-21-16994 REV.A. NO FURTHER DEFECTS NOTED</P>)

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 96,792 hrs · 17,758 cycles

STA 1780-1800 LBL 99" SEAT TRACK FOUND CRACKED. SEAT TRACK REPAIRED AS PER SRM 53-00-52-2R-6 REPAIR 6 FIG 201. NO FURTHER DEFECTS NOTED.

Part: WEB — CHAFED (RUDDER) · airframe 96,792 hrs · 17,758 cycles

LWR RUDDER LWR WEB AFT FOUND CHAFING MARK. WEB CHAFING MARK AREA REPAIRED AS PER RI NO: RI-55-40-17002 REV.B. NO FURTHER DEFECTS NOTED.

Part: SKIN — DELAMINATED (ZONE 500) · airframe 96,792 hrs · 17,758 cycles

LHW I/B MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: FRAME — CRACKED (ZONE 200) · airframe 96,792 hrs · 17,758 cycles

RIGHT BS 840 UPR DECK TENSION TIE ATT FRAME FOUND 4EA FASTENER HOLES CRACK. FRAME REPAIRED AS PER EO 4453A301 R12 PART 6 STEP 7F AND SRM 53-20-07-2R-3 REPAIR 3 FIG 201 (CAT B). NO FURTHER DEFECTS NOTED.

Part: SKIN — DELAMINATED (ZONE 600) · airframe 96,792 hrs · 17,758 cycles

RHW O/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: SKIN — DELAMINATED (LT TE FLAP) · airframe 96,792 hrs · 17,758 cycles

LHW I/B FORE FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DELAMINATED (ZONE 500) · airframe 96,792 hrs · 17,758 cycles

LHW OB MID FLAP FOUND DELAMINATION(<P>PERFORMED REPAIR AT DELAMINATION AREA PER SRM 51-70-07 PAR 5.A (1). NO FURTHER DEFECTS NOTED</P>)

Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 96,792 hrs · 17,758 cycles

CENTER FUSELAGE REAR WEB AT LBL 94" FND 2EA BONDING ATT POINTS CORROSION. CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, CHECKED WITHIN SRM 57-10-10-1A-2 ALLOWABLE DAMAGE 2 FIG 101, DETAIL V LIMITS ORG: 0.815, L:2" X L:1" X D:0.065". NO FURTHER DEFECTS NOTED>)

Part: PROBE — UNKNOWN (UNKNOWN) · airframe 94,831 hrs · 17,458 cycles

WHILE ON CLIMBOUT, "ALT DISAGREE" EICAS FLASHED MULTIPLE TIMES. TRIED CENTER ADC ON CAPT SIDE, MESSAGE CONTINUED TO INTERMITTENTLY OCCUR. EVENTUALLY RAN ALT DISAGREE (2 ADC'S REMAINING) CHECKLIST. ONCE THIS CHECKLIST WAS COMPLETED, DETERMINED THAT MOST LIKELY RH ADC FAILED AND L AND C ADC'S OKAY. RETURNED TO HKG WITHOUT MESSAGE RETURNING. ALSO DIFFERENCE BETWEEN ALTIMETERS WAS 300 FT LH TO RH, 200 FT CTR TO RH.(<P>FIM 34-12 TASK 864 AND 34-12 TASK 903 FOLLOWED. RH UPPER PITOT STATIC PROBE AND RH ADC REPLACED IAW AMM 34-11-01 AND 34-12-01. OPS TEST OF RH ADC AND RH UPPER PITOT STATIC PROBE HEAT TEST RESULT SATISFACTORY. LEAK CHECK OF PITOT STATIC SYSTEM, RESULT NORMAL. BOTH ALT AND AIRSPEED INDICATION ON L, R &AMP; CTR ADC CHECKED NORMAL. SN: 316987 &AMP; 97014873 / PN: 0856RE6 &AMP; 4040800-911</P>)

Part: FAN — INOPERATIVE · airframe 89,598 hrs · 16,597 cycles

EQUIP COOLING EICAS MSG DURING CRUISE. QRH DIRECTED EQUIP COOLING OVRD. OVRD STATUS MSG FOLLOWED BY EQUIP COOLING STATUS MSG(<P>REMOVED AND REPLACED E/E COOLING SUPPLY FAN PER AMM 21-58-01/401 AND EQUIP COOLING INBD EXHAUST VALVE PER AMM 21-58-23/401. REMOVED AND REPLACED EQUIP COOLING VALVE RELAY (R7447) PER WDM 21-58-23. C/W AP-22179 AND E/E COOLING SYS OPS TEST OK PER AMM 21-58-00/501.</P>)

Part: BUSHING — FAULT MESSAGE · airframe 89,559 hrs · 16,590 cycles

ELEC AC BUS 1 EICAS MESSAGE(NO MSG FOUND. REMOVED AND REPLACED #1 BCU IAW AMM 24-23-01/401. OPS CK GOOD.</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LH W I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W FRONT SPAR OLES 1389 STIFFENER FOUND CORROSION.(<P>LH W FRONT SPAR OLES 1389 STIFFENER FTG P/N: 65B15683-9 REPLACED AND INSTALLED IAW RI 57-21-15734 REV.A</P>)

Part: NONE — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W OLES 1597 FRONT SPAR STIFFENER FOUND CORROSION(<P>LH W OLES 1597 FRONT SPAR STIFFENER FTG P/N 112U5642-1 CORROSION AREA REPAIRED IAW RI-57-21-15730 REV.A</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W FRONT SPAR OLES 1606 UNDER STIFFENER SHIM FOUND CORROSION(<P>LH W FRONT SPAR OLES 1606 STIFFENER ATT SHIM REPLACED AND INSTALLED IAW SRM 51-20-08-0G-0</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

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

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LHW O/B FORE FLAP UPPER T/E MOST O/B AREA FOUND DELAM(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LH BS 820 TENSION TIE 3EA HOLE FOUND CRACK AT FRAME.(<P>STA 820 LH TENSION TIE AREA FRAME DOUBLER AND PARTICAL FRAME SEGMENT REPLACEMENT REPAIRED IAW SRM 53-20-07-2R-2 REPAIR 2.</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH BS 820 TENSION TIE 3EA HOLE FOUND CRACK AT FRAME.(<P>STA 820 RH TENSION TIE AREA FRAME DOUBLER AND PARTICAL FRAME SEGMENT REPLACEMENT REPAIRED IAW SRM 53-20-07-2R-2 REPAIR 2.</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LHW I/B FORE FLAP LWR O/B FLAP PNL FWD EDGE FOUND DELAMINATION(<P>PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR 4/FIG2 02</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LH BS 860 TENSION TIE AREA 1EA HOLE FOUND CRACK AT FRAME.(<P>STA 860 LH TENSION TIE AREA, STR 7L TO STR 12L, FRAME DOUBLER AND PARTICAL FRAME SEGMENT REPLACEMENT REPAIRED IAW SRM 53-20-07-2R-4 REPAIR 4.</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LH 840 TENSION TIE FWD CHANNEL 1EA HOLE CRACK RUNNING 6 O/C AND 12 O/C APPROX 0.040IN(<P>STA 840 LH TENSION TIE CHANNEL REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH W I/B FORE FLAP L/E FAIRING FOUND DELAMINATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LH BS 840 TENSION TIE 2EA HOLE FOUND CRACK AT FRAME(<P>STA 840 LH STR 7L TO STR 12L FRAME SEGMENT REPLACEMENT REPAIRED IAW SRM 53-20-07-2R-3 REPAIR 3.</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W FRONT SPAR OLES 1460 STIFFENER FOUND CORROSION(<P>LH W FRONT SPAR OLES 1460 STIFFENER PN 65B15687-9 REPLACED AND INSTALL IAW SRM 51-10-02 AND SRM 51-40-02</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W FRONT SPAR OLES 1553 STIFFENER FOUND CORROSION(<P>LH W FRONT SPAR OLES 1553 STIFFENER PN 112U5612-1 REPLACED AND INSTALL IAW SRM 51-10-02 AND SRM 51-40-02 AND SHIM REPLACED IAW SRM 51-20-08-0G-0</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH W I/B FORE FLAP LOWER SURFACE FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

BULK CARGO STA 2160 CURTAIN FOUND TORN(<P>PERMANENT PATCH REPAIR CARRIED OUT AS PER RI-25-54-15702 REV.A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH BS 740 TENSION TIE 2EA HOLE FOUND CRACK AT FWD AND AFT CHANNEL.(<P>STA 740 RH TENSION TIE CHANNEL REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1.</P>)

Part: NONE — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W T/E MOST I/B FIXED PNL ATT 'T' CHORD FOUND CORROSION(<P>LH W WBL 235 T/E MOST I/B FIXED PNL ATT 'T' CHORD CORROSION AREA REPAIRED IAW RI-57-51-15719 REV.A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH WING SPOILER SUPPORT BEAM BTN WBL 235.2, #7 SPOILER I/B EDGE FOUND UPPER CHORD UPPER SURFACE CORROSION(<P>RH WING SPOILER SUPPORT BEAM BTN WBL 235.2 #7 SPOILER I/B EDGE UPPER CHORD UPPER SURFACE CORROSION AREA REPAIRED IAW SRM 57-41-09 ADL 1, FIG 101</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH HORI STAB UPPER SKIN AND UPPER REAR SPAR CHORD ZONE B INSP 1EA FASTENER HOLE FOUND CRACK.(<P>RH HORI STAB UPPER SKIN AND UPPER REAR SPAR CHORD ZONE B FASTENER HOLE REPAIRED IAW RI 55-00-15706 REV.A</P>)

Part: NONE — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W L/E CAVITY OLES 1322-1520 LWR FIXED PANELS SUPPORT BEAM FOUND CORROSION(<P>LH W OLES STA 1490 L/E PANEL SUPPORT BEAM P/N: 65B11862-29 CORROSION AREA REPAIRED IAW RI-57-41-15708 REV.A</P>)

Part: NONE — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W OLES 1484 FRONT SPAR STIFFENER FOUND CORROSION(<P>LH W OLES 1484 FRONT SPAR STIFFENER FTG P/N 65B15688-5 CORROSION AREA REPAIRED IAW RI-57-21-15729 REV.A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH W I/B FORE FLAP L/E FAIRING FOUND DELAMINATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

RH W FRONT SPAR OLES 1563 STIFFENER ATT SHIM FOUND CORROSION(<P>RH W FRONT SPAR OLES 1563 STIFFENER ATT SHIM REPLACED AND INSTALLED IAW SRM 51-20-08-0G-0</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

#1 SPOILER O/B EDGE FIBERGLASS STRIP FOUND DISBONDED(<P>BONDED NEW&NBSP;<SPAN>FIBERGLASS STRIP</SPAN></P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH W O/B MID FLAP I/B L/E PNL FOUND DENT(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

RH W FRONT SPAR OLES 1553 STIFFENER FOUND CORROSION.(<P>RH W FRONT SPAR OLES 1553 STIFFENER FTG P/N: 112U5612-2 REPLACED AND INSTALLED IAW RI 57-21-15736 REV.A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

NOSE WHEEL WELL STA 260 RH CORNER 1 EA HOLE CRACK FOUND(<P>NOSE WHEEL WELL STA 260 RH CORNER CANTED BULKHEAD OUTER CHORD CRACK AREA REPAIRED IAW RI-53-00-15696 REV.A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH W I/B FORE FLAP L/E FAIRING FOUND DELAMINATION(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

#12 K FLAP (EXT SURFACE) FOUND 1EA DENT(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5.A.</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W FRONT SPAR OLES 1381 STIFFENER FOUND CORROSION.(<P>LH W FRONT SPAR OLES 1381 STIFFENER ASSY P/N: 65B15682-5 REPLACED AND INSTALLED IAW RI 57-21-15726 REV.A</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

RH W FRONT SPAR OLES 1460 STIFFENER FOUND CORROSION.(<P>RH W FRONT SPAR OLES 1460 STIFFENER ASSY P/N: 65B15687-10 REPLACED AND INSTALLED IAW RI 57-21-15731 REV.A</P>)

Part: NONE — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

RH W OLES 1493 FRONT SPAR STIFFENER FOUND CORROSION(<P>RH W OLES 1493 FRONT SPAR STIFFENER FTG P/N 65B15689-10 CORROSION AREA REPAIRED IAW RI-57-21-15732 REV.A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LH BS 840 2EA HOLE FOUND CRACK RUNNING 12 O/C ON THE FAIL SAFE CHORD LAYER WITH APPROX 0.040" IN DEPTH(<P>STA 840 LH, STR 6L TO STR 12L, THE FAIL SAFE CHORD SEGMENT REPLACEMENT REPAIRED IAW SRM 53-20-07-2R-3 REPAIR 3 AND SRM 51-70-11 REV.95 20 FEB 2022</P>)

Part: DOUBLER — NONE · airframe 89,425 hrs · 16,564 cycles

LH BS900 TENSION TIE 1EA HOLE FOUND CRACK AT FRAME DOUBLER.(<P>STA 900 LH TENSION TIE AREA FRAME DOUBLER P/N: 65B09464-49 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02.</P>)

Part: NONE — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

RH W L/E OLES 1420 LWR FIXED PNL SUPPORT BEAM CORROSION(<P>RH W L/E OLES 1420 LWR FIXED PNL SUPPORT BEAM P/N 65B11862-30 CORROSION AREA REPAIRED IAW RI-57-41-15709 REV.A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LH W O/B AILERON LOWER FOUND DELAMINATE(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-06 PAR.5.A.</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH W UPPER FIXED T/E PANEL WBL 128.47 TO 263.94 FOUND COFFIN DOUBLER DELAMINATED(<P>BONDED NEW BOUBLER AND PERFORMED REPAIR AT DELAMINATED AREA</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH BS860 TENSION TIE AREA 1EA HOLE FOUND CRACK AT FRAME AND DOUBLER.(<P>STA 860 RH TENSION TIE AREA, STR 7R TO STR 12R, FRAME DOUBLER AND PARTICAL FRAME SEQMENT REPLACEMENT REPAIRED IAW SRM 53-20-07-2R-4 REPAIR 4.</P>)

Part: NONE — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

RH W T/E MOST I/B FIXED PNL ATT 'T' CHORD FOUND CORROSION(<P>RH W WBL 235 T/E MOST I/B FIXED PNL ATT 'T' CHORD CORROSION AREA REPAIRED IAW RI-57-51-15720 REV.A</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

RH W FRONT SPAR OLES 1484 STIFFENER FOUND CORROSION.(<P>RH W FRONT SPAR OLES 1484 STIFFENER FTG P/N: 65B15688-6 REPLACED AND INSTALLED IAW RI 57-21-15735 REV.A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH W O/B MID FLAP CENTER L/E FOUND DELAMINATED(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LHW I/B MID FLAP LOWER SURFACE FOUND CRACK(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5K</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W FRONT SPAR OLES 1451 STIFFENER FOUND CORROSION.(<P>LH W FRONT SPAR OLES 1451 STIFFENER ASSY P/N: 65B15686-9 REPLACED AND INSTALLED IAW RI 57-21-15728 REV.A</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W FRONT SPAR OLES 1579 UNDER STIFFENER SHIM FOUND CORROSION(<P>LH W FRONT SPAR OLES 1579 STIFFENER ATT SHIM REPLACED AND INSTALLED IAW SRM 51-20-08-0G-0</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W FRONT SPAR OLES 1420 STIFFENER FOUND CORROSION(<P>LH W FRONT SPAR OLES 1420 STIFFENER PN 65B15685-9 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LH W I/B AILERON O/B AFT CORNER FOUND DELAMINATE(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-06 PAR.5.A.</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

BS 940 LH TENSION TIE 1 EA HOLE FOUND CRACK AT FRAME(<P>STA 940 LH TENSION TIE AREA FRAME P/N: 142U7764-57 CRACK AREA FREEZE PLUG HOLE REPAIRED IAW RI-53-00-15700 REV.A</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W FRONT SPAR OLES 1493 STIFFENER FOUND CORROSION(<P>LH W FRONT SPAR OLES 1493 STIFFENER P/N 65B15689-9 REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RHW I/B FORE FLAP LWR O/B FLAP PNL FWD EDGE 3 LOCATIONS FOUND DELAMINATION(<P>PERFORMED METAL HOTBOND REPAIR AS PER SRM 51-70-10 REPAIR4 /FIG202</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

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

Part: NONE — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W OLES 1410 FRONT SPAR STIFFENER FOUND CORROSION(<P>LH W OLES 1410 FRONT SPAR STIFFENER FTG P/N 65B15684-5 CORROSION AREA REPAIRED IAW RI-57-21-15727 REV.A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

RH W I/B MID FLAP L/E FAIRING FOUND DENT(<P>PERFORMED COMPOSITE HOTBOND REPAIR AS PER SRM 51-70-07 PAR.5A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

LH BS 880 TENSION TIE 1EA HOLE FOUND CRACK AT FRAME(<P>STA 880 LH STR 7L TO STR 12L FRAME SEGMENT REPLACEMENT REPAIRED IAW SRM 53-20-07-2R-5 REPAIR 5.</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

M/D EMER LT - OVER DOOR L5735 FOUND DIM.(<P>M/D EMER LT - OVER DOOR L5735 LAMP REPLACED, LENS INSTALLED AND OPERATION TEST AND SYSTEM TEST CARRIED OUT RESULT 'NORMAL' IAW AMM 33-51-07 AND 33-51-00.</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

EMP - APU FIRE WALL FWD SIDE COUNT FROM BOTTOM #2 ATT STIFFENER RHS END FOUND CRACKED(<P>EMP - APU FIRE WALL FWD SIDE WL 276 R/H O/B END STIFFENER P/N: 65B02712-19 CRACK AREA REPAIRED IAW RI-53-00-15717 REV.A</P>)

Part: NONE — NONE · airframe 89,425 hrs · 16,564 cycles

M/D STA 860 LH TENSION TIE AFT CHANNEL FOUND CRACKED THRU BETWEEN HOLES(<P>M/D STA 860 LH TENSION TIE CHANNEL REPAIRED IAW SRM 53-20-30-2R-1 REPAIR 1.</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

RH W FRONT SPAR OLES 1533 STIFFENER FOUND CORROSION.(<P>RH W FRONT SPAR OLES 1533 STIFFENER ASSY P/N: 65B15691-2 REPLACED AND INSTALLED IAW RI 57-21-15733 REV.A</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LH W FRONT SPAR OLES 1350 STIFFENER FOUND CORROSION.(<P>LH W FRONT SPAR OLES 1350 STIFFENER ASSY P/N: 65B15681-9 REPLACED AND INSTALLED IAW RI 57-21-15725 REV.A</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

RH W FRONT SPAR OLES 1597 STIFFENER ATT SHIM FOUND CORROSION(<P>RH W FRONT SPAR OLES 1597 STIFFENER ATT SHIM REPLACED AND INSTALLED IAW SRM 51-20-08-0G-0</P>)

Part: STIFFENER — NONE · corrosion level 2 · airframe 89,425 hrs · 16,564 cycles

LHW FRONT SPAR OLES 1563 STIFFENER ATT SHIM FOUND CORROSION(<P>LHW FRONT SPAR OLES 1563 STIFFENER ATT SHIM REPLACED AND INSTALLED IAW SRM 51-20-08-0G-0</P>)

Part: DUCT — RUPTURED (PNEUMATIC SYSTEM) · airframe 83,734 hrs · 15,644 cycles

BLEED AIR DUCT C MSG. TROUBLESHOT AND FOUND CENTER BLEED DUCT RUPTURED. REMOVED AND REPLACED CENTER BLEED DUCT. OPS CHECK NORMAL.

Part: SMOKE DETECTOR — FALSE ACTIVATION (MAIN DECK CARGO) · airframe 83,495 hrs · 15,602 cycles

EICAS MSG FIRE MN DK AFT NO SMOKE OR FLAMES. CREW FOLLOWED QRH AND DEPRESSURIZED AIRCRAFT WHICH CAUSED THE O2 MASK DEPLOYMENT. R & R MCD SMOKE DETECTORS 12A AND 12B IAW AMM 26-14-01. OFF PN 2156-756A SN 20590B. OPS CHECK GOOD. MX RESTOWED ALL O2 MASKS IAW AMM 35-21-06.

Part: SENSOR — MALFUNCTIONED (MLG) · airframe 82,127 hrs · 15,319 cycles

RH BODY GEAR FAILED TO EXTEND ON APPROACH WITH NORMAL OPERATION. CREW PERFORMED GO AROUND, CYCLED GEAR, WHEN IT FAILED TO EXTEND A SECOND TIME CREW PERFORM ALTERNATE EXTENSION PROCEDURES. CMC MSG 32718 AND 32678, PERFORMED FIM 32-61 TASK 888 AND TASK 868. REPLACED THE RT BODY GEAR PRIMARY DOOR SENSOR S409, AND ALTERNATE S427. CHECKED FOR CLEARANCE BETWEEN THE SENSOR AND THE TARGET ALL GOOD, CHECK SYSTEM FOR OPERATION, ALL OK. AFTER REPLACEMENT OF SENSOR S409 AND S427, OPERATIONAL TEST OF MAIN LDG / AND DOOR EXTENSION AND RETRACTION PERFORMED IAW AMM 32-32-00-350-801. FOUND SATISFACTORY DUE TO HISTORY AND MCC REQUEST.

Part: WASHER — TORN (NR 1 PYLON) · airframe 81,707 hrs · 15,231 cycles

NR 1 PYLON, BOTH LT AND RT UNDERWING MIDSPAR FITTING KARON WASHERS FOUND TORN. NR 1 PYLON BOTH LT AND RT UNDERWING MIDSPAR FITTING KARON WASHERS REPLACED AS PER HX RI NO RI-57-20-14099 REV A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D LT FLOORBEAM AT STA 800 LBL 85 FOUND CORRODED. M/D LT FLOORBEAM AT STA 800 LBL 85 REPAIRED IAW SRM 53-00-51 REPAIR 3 FIG 201.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D FLOORBEAM STA 620 LBL 90 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101.

Part: STRUCTURE — CORRODED (RT WLG WW) · airframe 81,707 hrs · 15,231 cycles

RT WLG WW CENTER TANK JETTISON PUMP BOLT HOLE FOUND CORROSION. CORROSION REMOVED IAW RI-57-12-14098 REV A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D STA 1000 LBL 77 SEAT TRACK JOIN FITTING FOUND CRACKED. M/D STA 1000 LBL 77 SEAT TRACK JOIN FITTING REPLACED IAW SRM 51-10-02 AND DWG 69B14267.

Part: STRUCTURE — CORRODED (LT WLG WW) · airframe 81,707 hrs · 15,231 cycles

LT WLG WW CENTER TANK JETTISON PUMP BOLT HOLE FOUND CORROSION. CORROSION REMOVED IAW RI-57-12-14097 REV A.

Part: SKIN — CRACKED (L1 DOOR) · airframe 81,707 hrs · 15,231 cycles

M/D L1 DOOR SKIN UPPER HINGE CUTOUT FOUND CRACKED. DOOR SKIN REPAIRED AS PER SRM 52-10-01 REPAIR 3.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D SEAT TRACK STA 640-660 LBL 90 I/B FLANGE FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

APU COMPT FWD BULKHEAD STA 2658 LT LOWER FOUND CRACKED. STA 2658 BULKHEAD REPAIRED IAW RI-53-83-14095 REV A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D STA 33.99 SEAT TRACK SUPPORT JOIN FITTING FOUND CRACKED. SEAT TRACK JOIN FITTING REPLACED IAW SRM 57-10-02 AND DWG 69B14267.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D LT FLOOR O/B SUPPORT ANGLE AT STA 1358 LBL 116 FOUND CRACKED. M/D LT FLOOR O/B SUPPORT ANGLE REPAIRED IAW RI-53-60-14100 REV A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D FLOOR BEAM STA 761 RBL 22 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D SEAT TRACK STA 1780-1800 LBL 99 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 FIG 101.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D LT SEAT TRACK AT STA 1872-1877 LBL 11 FOUND CRACKED. M/D LT SEAT TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 12.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 81,707 hrs · 15,231 cycles

RT HORIZ STAB 420 T/E O/B RIB VERTICAL STIFFENER FOUND CRACKED. VERTICAL STIFFENER REPLACED AS PER DWG 65B03651.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D LT SUBSTITUTE TRACK AT STA 2183 FOUND CRACKED. M/D LT SUBSTITUTE TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 13.

Part: DEPRESSOR — CRACKED (NR 2) · airframe 81,707 hrs · 15,231 cycles

NR 2 ENG RT FIRE WALL SUPPORT DEPRESSOR FWD END FOUND CRACKED. DEPRESSOR REPLACED WITH NEW PART 311U2680-438 IAW DWG 311U2680.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 81,707 hrs · 15,231 cycles

LT WING O/B MID FLAP L/E FAIRING (587QT) FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 81,707 hrs · 15,231 cycles

RT WING I/B MID FLAP L/E FAIRING FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D FLOORBEAM STA 400 LBL 80 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101.

Part: FRAME — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

FX STA 880 BODY FRAME UPPER FOUND CRACKED. BODY FRAME REPAIRED IAW SRM 53-00-71 REPAIR 4 FIG 201.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D LT SUBSTITUTE TRACK SPLICE FOUND CRACKED. M/D LT SUBSTITUTE TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 13.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D RT SEAT TRACK AT STA 1635-1670 RBL 98 FOUND CRACKED. M/D RT SEAT TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 12 AND RI-53-65-14082 REV A.

Part: SHEAR WEB — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D RT FLOOR SHEAR WEB AT STA 472 RBL 88-94 FOUND CRACKED. M/D RT FLOOR SHEAR WEB REPLACED, REFER TO DWG 65B14804.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D LT FLOOR O/B SUPPORT ANGLE AT STA 1941 LBL 116 FOUND CRACKED. M/D LT FLOOR O/B SUPPORT ANGLE REPAIRED IAW RI-53-60-14092.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D FLOORBEAM 980 LBL 11- RBL 11 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 81,707 hrs · 15,231 cycles

M/D SIDE CARGO DOOR INNER SKIN STA 1790-1800 SPOT LIGHT FOUND CORROSION. CORROSION REMOVED IAW SRM 52-30-01 ALLOWABLE DAMAGE 1 FIG 101.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 81,707 hrs · 15,231 cycles

RT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.

Part: WASHER — UNKNOWN (NR PYLON) · airframe 81,707 hrs · 15,231 cycles

NR 4 PYLON, BOTH LT AND RT UNDERWING MIDSPAR FITTING KARON WASHERS FOUND TORN OR DETACHED. NR 4 PYLON BOTH LT AND RT UNDERWING MIDSPAR FITTING KARON WASHERS REPLACED AS PER HX RI NO RI-57-20-14099 REV A.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 81,707 hrs · 15,231 cycles

LT WING O/B MID FLAP L/E FAIRING FOUND DELAMINATION (FROM I/B 58"). PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 81,707 hrs · 15,231 cycles

LT WING O/B MID FLAP L/E FAIRING (587PT) FOUND DELAMINATION. PERFORMED PERMANENT REPAIR AS PER SRM 51-70-07 PAR 5A REV 88.

Part: SKIN — CORRODED (CARGO DOOR) · airframe 81,707 hrs · 15,231 cycles

M/D SIDE CARGO DOOR INNER SKIN STA 1860-1870 SPOT LIGHT FOUND CORROSION. CORROSION REMOVED IAW SRM 52-30-01 ALLOWABLE DAMAGE 1 FIG 101.

Part: FITTING — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D STA 1000 LBL 11.33" SEAT TRACK SUPPORT SPLICE JOIN FITTING FOUND CRACK. M/D STA 1000 LBL 11.33 SEAT TRACK JOIN FITTING REPLACED IAW SRM 51-10-02 AND DWG 69B14592.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D RT SUBSTITUTE TRACK SPLICE FOUND CRACKED. M/D RT SUBSTITUTE TRACK REPAIRED AS PER SRM 53-00-52 REPAIR 13.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 81,707 hrs · 15,231 cycles

M/D FLOORBEAM STA 520 LBL 78 FOUND CORROSION. CORROSION REMOVED IAW SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG 101.

Part: PITOT HEAD — INOPERATIVE (CAPTAIN'S) · airframe 79,974 hrs · 14,918 cycles

REJECTED T/O AT 70 KTS DUE TO NO AIRSPEED INDICATION ON CAPTAINS PFD.(<P>REMOVED AND REPLACED PITOT STATIC PROBE IAW AMM 34-11-01/401. PERFORMED CAPTAIN'S PITOT SYSTEM LEAK&NBSP;TEST IAW AMM 34-11-00-795-019, SYSTEM CHECKS OK. AIRCRAFT OK FOR SERVICE.&NBSP;<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 77,497 hrs · 14,469 cycles

AIRCRAFT PERFORMED AIR RETURN TO ICN DUE TO ENG 1 FUEL FILT MESSAGE.(<P>ONCE BACK IN BLOCKS, DEBRIEFED CREW AND DETERMINED ALL ENGINE PARAMETERS WERE NORMAL AND NO ERRATIC ENGINE CONDITIONS.&NBSP; ENGINE OPERATION WAS NORMAL.<BR /></P><P>MAINTENANCE INSPECTED AND REPLACED THE FUEL FILTER.&NBSP; NO DEFECTS FOUND.&NBSP; OPS AND LEAK CHECK GOOD.<BR DATA-MCE-BOGUS="1" /></P>)

Part: PDU — MALFUNCTIONED (LE FLAP) · airframe 76,392 hrs · 14,286 cycles

FLAPS PRIMARY AND FLAPS DRIVE EICAS DURING FLAP EXTENSION.(<P>FLIGHT CREW&NBSP;REPORTED THAT&NBSP;LEFT INBOARD LEADING EDGE FLAP&NBSP;GROUP DID NOT EXTEND.&NBSP; CMC INDICATED &NBSP;LEADING EDGE FLAP DRIVE PDU L4 FAULTED.&NBSP; REPLACED PDU L4 AND ALL OPS CHECKS SATISFACTORY.<BR /></P>)