N302UP

Part: DOOR — MALFUNCTIONED (LIFE RAFT) · airframe 74,856 hrs · 25,686 cycles

COCKPIT LIFE RAFT STOWAGE COMPARTMENT DOOR WILL NOT STAY OPEN. DEFERRED PER SREO-52198.

Part: DOOR — INOPERATIVE (ZONE 200) · airframe 74,867 hrs · 25,693 cycles

COCKPIT LIFE RAFT STOWAGE COMPARTMENT DOOR WILL NOT STAY OPEN. FOUND BUSHING LOSE IN PFM BOX. INSTALLED SHOCK STRUT IN COCKPIT LIFE RAFT STOWAGE BOX COMPARTMENT DOOR AS PER B767 AMM 20-11-00 AND IPC 25-62-55. OPS CHECK NORMAL.

Part: LEVER — MALFUNCTIONED (ZONE 800) · airframe 74,309 hrs · 25,469 cycles

MAIN ENTRY DOOR - YELLOW PUSH TO, SECURE LEVER WILL NOT ENGAGE TO THE LOCK/SECURE POSITION WITH THE ENTRY DOOR CLOSED. PERFORMED ADJUSTMENT OPS CHECK OF ENTRY/SERVICE DOOR INTERLOCK PAWL. OPS CHECK GOOD AT THIS TIME REF AMM 52-11-26-710-801

Part: SKIN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - DENT, FUSELAGE EXTERNAL SKIN, STA 1654.5 ~ STA 1678, S-25R TO S-26R (EVALUATE) OK TO WORK

Part: FAIRING — CRACKED (LT WING TE FLAP) · airframe 71,120 hrs · 24,094 cycles

FAULT - CRACK FAIRING, LH WING NO.3 FLAP TRACK AFT FAIRING INBD LE (REPAIR) REVIEW COMPLETE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

CRACK FAIRING, LH WING NO.3 FLAP TRACK AFT FAIRING INBD LE (REPAIR) OK TO WORK. OPEN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT- FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-20 (REPAIR) OK TO WORK

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CRACK ANGLE, INTERNAL AFT INBOARD UPPER SLAT EDGE OF NO.1 PYLON AFT NACELLE STRUT FAIRING(REPLACE) OK TO WORK

Part: SKIN PANEL — CRACKED · airframe 71,097 hrs · 24,089 cycles

FAULT- CRACK - RIVET EDGE SKIN, NO.2 PYLON FWD TORQUE BOX ACCESS PANEL NO.442AL CUTOUT.(REPAIR) IAW AMM 78-31-01-404-026-H00, REV:141, STEP G. (28), PERF UPS EO B767-7830-52256 TASK CARD NO.: T3F18E003Q97J - OP CHK OF THE LH T REV, RESULT: NORMAL. IAW AMM 78-31-01-404-026-H00, REV:141, STEP G. (29) ~ (35) & AMM 78-31-00-725-005-H00, REV:141, PERF NO.2 ENG T REV OP TEST. RESULT: PASSED.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 71,120 hrs · 24,094 cycles

FAULT - CRACK PNL, RH WING LOWER OUTD MAIN FUEL PUMP ACCESS PNL(REPLACE) REVIEWED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-12 (REPAIR) OK TO WORK

Part: SKIN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

MAJOR REPAIR* FAULT- CRACK, FUSELAGE EXTERNAL SKIN, STA1654 STA1678 S-13AR (REPAIR) ACCOMPLISHED REPAIR I.A.W SRM 53-80-01-2R-7 REV.88 REVIEW COMPLETE

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 71,120 hrs · 24,094 cycles

FAULT - FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-12 (REPAIR) REVIEW COMPLETE

Part: ACCESS PANEL — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CRACK PNL, RH WING LOWER OUTD MAIN FUEL PUMP ACCESS PNL(REPLACE) OK TO WORK

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT- CRACK - RIVET EDGE SKIN, NO.2 PYLON FWD TORQUE BOX ACCESS PANEL NO.442AL CUTOUT.(REPAIR) OK TO WORK

Part: SKIN — DEBONDED (FUSELAGE) · airframe 71,120 hrs · 24,094 cycles

**SUPPLEMENTAL SDR**FAULT - DISBOND - SKIN, EXTERNAL LOWER SIDE SURFACE OF L/H AFTER WING TO BODY ACCESS PNL NO.197KL. (REPAIR) REVIEWED

Part: FLOOR PANEL — CRACKED (AFT CARGO BAY) · airframe 71,177 hrs · 24,106 cycles

FAULT- FOUND AFT CARGO FLOOR PANEL CRACK, P/N:453T1996-20 (REPAIR) CUT OUT THE DAMAGE AND CLEAN. MEASURE THE CUTOUT (LENGTH: 1.4", WIDTH: 0.3", AT AFTER EDGE AND 10" FROM LEFT HAND ON PANEL NO.453T1996-20). APPLY THE COMPOUND TO THE CUTOUT CURED AT 125°F FOR 3 HOURS AND BOND THE REPAIR PLIES WITH RESIN CURED AT 170°F FOR 2 HOURS WITH A MINIMUM VACUUM OF 20 IN/HG I.A.W. 767-300F SRM 53-00-50-2R-0 REV.88.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - DISBOND - SKIN, EXTERNAL LOWER SIDE SURFACE OF L/H AFTER WING TO BODY ACCESS PNL NO.197KL. (REPAIR) OK TO WORK

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CRACK FORMER, LH WING OUTBD FIXED LE NOSE BEAM OSS 437 (REPLACE) ASSIGNED EO-89074-REQ1 TO FAULT.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CRACK - WEB, INTERNAL AFTER LOWER SIDE OF NO.2 PYLON AFTER FAIRING PNL NO.447DB (REPLACE) OK TO WORK

Part: WEB — CRACKED (NR 2 NACELLE) · airframe 71,120 hrs · 24,094 cycles

**SUPPLEMENTAL SDR**FAULT - CRACK - WEB, INTERNAL AFTER LOWER SIDE OF NO.2 PYLON AFTER FAIRING PNL NO.447DB (REPLACE) REVIEW COMPLETE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CRACK - WEB MAIN EQUIPMENT CENTER AT STA 246 LBL 50" (REPLACE) 1.REMOVED DAMAGE PART I.A.W. SRM 51-40-02-0G REV.88

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT- CRACK SKIN PNL, LH WING NO.2 FLAP TRACK AFT FAIRING(REPAIR) REMOVED FITTING I.A.W SRM 51-40-02-0G REV.88

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CRACK FORMER, LH WING OUTBD FIXED LE NOSE BEAM OSS 441 (REPLACE) REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.88

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CRACK - CLIP NO.2 PYLON AFTER LOWER FAIRING AFTER INNER SIDE, LH FAIRING PNL SUPPORT BRACKET(REPLACE) OK TO WORK

Part: SPLICE — CRACKED (RT WING NOSE) · airframe 71,120 hrs · 24,094 cycles

FAULT - CRACK SPLICE, RH WING LE FIXED STRUCTURE NOSE AREA AT LES 691(REPLACE) REVIEW COMPLETE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CRACK SPLICE, RH WING LE FIXED STRUCTURE NOSE AREA AT LES 691(REPLACE) OK TO WORK

Part: BEAM — CRACKED (LT WING NOSE) · airframe 71,120 hrs · 24,094 cycles

**SUPPLEMENTAL SDR**FAULT - CRACK FORMER, LH WING OUTBD FIXED LE NOSE BEAM OSS 441 (REPLACE) REVIEW COMPLETE.

Part: ANGLE — CRACKED (NR 2 NACELLE) · airframe 71,120 hrs · 24,094 cycles

FAULT - CRACK - CLIP NO.2 PYLON AFTER LOWER FAIRING AFTER INNER SIDE, LH FAIRING PNL SUPPORT BRACKET(REPLACE) REVIEW COMPLETE

Part: SKIN PANEL — CRACKED (LT WING) · airframe 71,120 hrs · 24,094 cycles

FAULT- CRACK SKIN PNL, LH WING NO.2 FLAP TRACK AFT FAIRING(REPAIR) REVIEW COMPLETE

Part: BEAM — CRACKED (LT WING NOSE) · airframe 71,120 hrs · 24,094 cycles

**SUPPLEMENTAL SDR**FAULT - CRACK FORMER, LH WING OUTBD FIXED LE NOSE BEAM OSS 437 (REPLACE) REVIEW COMPLETE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CRACK - CHANNEL, NO.1 ENG PANEL NO.437DB TRIANGLE SUPPORT (REPAIR) OK TO WORK

Part: CHANNEL — CRACKED (NR 1 NACELLE) · airframe 71,120 hrs · 24,094 cycles

FAULT - CRACK - CHANNEL, NO.1 ENG PANEL NO.437DB TRIANGLE SUPPORT (REPAIR) REVIEW COMPLETE

Part: WEB — CRACKED (BS 246 LBL 50) · airframe 71,120 hrs · 24,094 cycles

FAULT - CRACK - WEB MAIN EQUIPMENT CENTER AT STA 246 LBL 50" (REPLACE) REVIEWED

Part: LEVER — DEFORMED (MAIN DOOR) · airframe 71,177 hrs · 24,106 cycles

FAULT - FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM (REPLACE) I.A.W AMM 20-11-00-910-802 REV.141 REPLACE HINGE ASSY. I.A.W AMM 52-12-02-404-025 REV.141 INSTALL DOORWAY LINING. I.A.W AMM 33-51-01-402-030 REV.141 PERFORM EXIT SIGN LAMP TEST WAS NORMAL. JOB COMPLETED AND CONDITION CHECK NORMAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CORROSION - FLOOR STRUCTURE BULK CARGO COMPARTMENT RIGHT AREA STA 1600 RBL 60(REPLACE) 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV. 88<BR>2. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV. 88 AND BOEING DWG NO:146T5650 SHEET 5 REV.C

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - FOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM (REPLACE) OK TO WORK

Part: ANGLE — CRACKED (HINGE FAIRING) · airframe 71,120 hrs · 24,094 cycles

FAULT - CRACK - ANGLE, NO. 1 ENG L/H AFT FAIRING DOOR HINGE BEAM ANGLE AT #4(REPLACE) REVIEW COMPLETE

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT- CORROSION - FLOOR STRUCTURE BULK CARGO COMPARTMENT LEFT AERA STA 1590 LBL60(REPLACE) 1. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV. 88<BR>2. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV. 88 AND BOEING DWG NO:146T5650 SHEET 5 REV.C

Part: HINGE — CRACKED (RT NACELLE DOOR) · airframe 71,177 hrs · 24,106 cycles

FAULT - CRACK - ANGLE, NO. 1 ENG R/H AFT FAIRING DOOR HINGE BEAM ANGLE AT #4.(REPLACE) I.A.W AMM 54-53-02-404-006 REV.141 INSTALLED HINGE BOLT FOR ACCESS NO.1 PYLON R/H FAIRING ACCESS DOOR NO.4 HINGE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CRACK - ANGLE, NO. 1 ENG R/H AFT FAIRING DOOR HINGE BEAM ANGLE AT #4.(REPLACE) I.A.W. AMM 54-53-02-004-002, REV.140, REMOVED NO.4 R/H HINGE BOLT OF NO.1 R/H FAIRING DOOR.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - CRACK - ANGLE, NO. 1 ENG L/H AFT FAIRING DOOR HINGE BEAM ANGLE AT #4(REPLACE) I.A.W. AMM 54-53-02-004-002, REV.140, REMOVED NO.4 L/H HINGE BOLT OF NO.1 L/H FAIRING DOOR.

Part: FILLER — CRACKED (CARGO BAY) · airframe 71,177 hrs · 24,106 cycles

FAULT - CRACK - FLOOR STRUCTURE BULK CARGO COMPARTMENT RIGHT AREA STA 1600 RBL 60(REPLACE) I.A.W AMM 25-59-01-404-019 REV.140 INSTALL SLOPING SIDEWALL , SIDEWALL AND BULKHEAD.

Part: FILLER — CRACKED (CARGO BAY) · airframe 71,177 hrs · 24,106 cycles

CRACK - FLOOR STRUCTURE BULK CARGO COMPARTMENT LEFT AERA STA 1590 LBL60(REPLACE) I.A.W AMM 25-59-01-404-019 REV.140 INSTALL SLOPING SIDEWALL , SIDEWALL AND BULKHEAD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,067 hrs · 24,079 cycles

*SDR FILED OPEN* FAULT - DENT, FUSELAGE EXTERNAL SKIN, STA 718, S-38R~S-39R. (EVALUATE) 1. MEASURED THE DENT ON FUSELAGE STA 718 S-38R~S-39R LENGTH=0.9" WIDTH(A)=0.9" DEPTH(Y)=0.009" AND A/Y = 100, FOUND TO BE IN LIMIT PER SRM 53-00-01-1A-1 FIGURE 101 DETAIL III REV.88<BR>2. SUBMITTED DETAILS TO ADM FOR TRACKING AND VISIBILITY DEFERRED AS INFO-DEFERRAL.

Part: SENSOR — WARNING MESSAGE (UNKNOWN) · airframe 70,978 hrs · 24,047 cycles

*** SUPPLEMENTAL SDR *** L PACK TEMP (EICAS C) **OII 1** ++ DMP REVERSED. AHM PICKED UP LH PACK TEMP SNSR FAILED TWICE. LH PACK TEMP CONTROL SENSOR R & R IAW AMM 21-51-08/401 REV 140. BITE AS PER FIM 21-51-00/101. NIL FAULTS. PACK OPS TESTED-NIL FAULTS/ LEAKS/EICAS MSG. PLACARD REMOVED. DI CLOSED

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,962 hrs · 24,041 cycles

L PACK TEMP (EICAS C) **OII 1** DMP REVERSED IAW MEL PROCEDURE FOR TROUBLESHOOTING. FOLLOWED FIM 21-51 TASK 877 REV NO:140 AND LH PACK TEMP CONT BITE TEST PERFORMED IAW FIM 21-51-00/101 FIG 103. LH PACK OPS CHECK ALSO GOOD. NO FAULT OBSERVED AND NO HISTORY FOUND IN MAINTENIX. DMP C/OUT AND MANUAL OVERRIDE ACTUATOR MOVED TO CLOSED POSITION. MEL STAYS OPEN.

Part: DOOR — CRACKED · airframe 70,916 hrs · 24,023 cycles

#1 ENG I/B REVERSER, UPPER BLOCKER DOOR CRACKED * OII 3 * (LINKED FAULT T3F18E003DYD0) INSTALLED THRUST REVERSER BLOCKER DOOR IAW AMM 78-31-14 AND CORRESPONDING DRAG LINK INSTALLED IAW AMM 78-31-15 OPERATIONAL CHECK SATIS DMP 78-31-1 REVERSED. CDL 78-31-3 CLEARED

Part: NONE — NONE (NONE) · airframe 70,390 hrs · 23,803 cycles

*SUPPLEMENTAL SDR* *ATB* SEVERE TURBULENCE FL350 C\W PARAGRAPH C STEPS #9 #10 #13 #14 OF LEFT WING AND STEPS #21 #22 #23 IAW MM 05-51-04-212-001. C/W SEVERE TURBULANCE INSPECTION SUB TASK 05-51-04-212-020 SECTION E CABIN INSPECTIONS NO CABIN DAMAGE FOUND AT THIS TIME. C\W PARAGRAPH C STEPS 3# 4# #5 #6 MM REF MM 05-51-04-212-001. C\W PARAGRAPH C STEPS 3# 4# #5 #6 MM REF MM 05-51-04-212-001. C/W PARAGRAPH C STEP 7 REF AMM 05-51-04-212-001

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,384 hrs · 23,800 cycles

*SDR FILED OPEN* *ATB* SEVERE TURBULENCE FL350 C\W PARAGRAPH C STEPS #9 #10 #13 #14 OF LEFT WING AND STEPS #21 #22 #23 IAW MM 05-51-04-212-001

Part: LIGHT — INOPERATIVE (UNKNOWN) · airframe 70,336 hrs · 23,783 cycles

EMERGENCY LIGHTS INOP FOUND ON PDC. R/R EMERGENCY BATT PACK IAW AMM 33-51-07. OPS CHECK SAT.

Part: LOCK — CRACKED (CARGO BAY) · airframe 69,868 hrs · 23,593 cycles

DOOR AREA CARGO LOCK #12 AT POS 2R IS CRACKED REMOVED AND REPLACED CARGO LOCK AT POS 2R #12 PER AMM 25-58-01.

Part: DOOR — NONE (L1) · airframe 69,073 hrs · 23,264 cycles

WHEN CLOSING CREW ENTRY DOOR THE CAPTURE LEVER IS EXTREMELY HARD TO PUSH OUTBOARD FROM INSIDE THE FIGHT DECK. PERFORMED OPERATIONAL TEST OF CRE WENTRY DOOR IAW AMM 52-12-00. OPS CHECKED GOOD

Part: MANIFOLD — FAULTED (LEFT ENGINE) · airframe 69,020 hrs · 23,243 cycles

INSPECTION TYPE:NA**ATB** L ENG OVHT EICAS MESSAGEFROM FLIGHT CREW CAPT SAID AFTER MESSAGE APPEARED REDUCED THROTTLE LEVEL MSG WENT AWAY. CH 7112742 FOUND LH ENG 14TH STAGE MANIFOILD LWR BALL JOPINT LOOSE & DAMAGED. REMOVED 14TH STAGE MANIFOLD R 0558904 12-08-22. REPLACED 8 N TO 14 STAGE MANIFOLD ASSY IAW AMM 35-11-01-404; IPC 35-11-01-03. OPERATED ENG NO MSG NOTED & LEAK CHKD OK

Part: THROTTLE — INOPERATIVE (POWERPLANT) · airframe 67,665 hrs · 22,721 cycles

INSPECTION TYPE:ETOP DURING T/O RIGHT ENG DID NOT ADVANCE BEYOND 96.6 N1 MANUAL TROTTLE MOVEMNT NO RESPONSE.ACCOMPLISHED FIM TASK 77-12-00-815-825-H01 REV 136 ALL ITEMS FROM BLOCK 1-3 C/W NIL FAULTS. REPLACED RH ENGINE HMU & LEAK TESTED. SATIS DURING WET MOTOR IAW AMM 79-21-14-401 REV 136.01

Part: NONE — NONE (CENTER WING TANK) · airframe 66,902 hrs · 22,465 cycles

INSPECTION TYPE:C14CRACK ON CENTER WING TANK STIFFENER ( P/N:111T2011-6) ON STA 785.9, RBL 55.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV 82.01, UPS EO B767-5740-58151-C AND UPS EO B767-5720-76672-A

Part: STIFFENER — NONE (CENTER WING TANK) · airframe 66,902 hrs · 22,465 cycles

INSPECTION TYPE:C14CRACK ON CENTER WING TANK STIFFENER(P/N:111T2008-11) ON STA 785.9, LBL 33.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.82.01, UPS EO B767-5740-58151 -C AND UPS EO B767-5720-76672-A

Part: FLOOR PANEL — NONE (UPPER SURFACE) · airframe 66,330 hrs · 22,218 cycles

INSPECTION TYPE:N/ADAMAGED FLOOR PANEL REQUIRES REPLACMENTFABRICATE NEW FLOOR PANEL PER EO B767-5320-9693-I

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 65,966 hrs · 22,097 cycles

INSPECTION TYPE:N/AEMERGENCY LIGHT FWD OF EMERGENCY ESCAP DESCENT DEVICES INOPRELAMPED LIGHT IAW AMM 33 51 11 002 001 OP CHECK GOOD

Part: PUMP — FAULTED (RT FUEL) · airframe 65,223 hrs · 21,834 cycles

INSPECTION TYPE:ETOP*** SUPPLEMENTAL ETOPS ***R FUEL PUMP EICAS MSG AND PUMP SW LIGHT ILLUMINATED IN FLT. COMPLETE QRH PROCEDURE AND PUMP SW OFF. ASSIGNED TO MEL 28-22-1. C/W DMP 28-22-1. PLACARD INSTALLED.REPLACED RT FWD MAIN FUEL PUMP, REVERSED DMP 28-22-1. REPLACED PUMP IAW AMM 28-22-03-404, OPS CK GOOD M7427894, CLEARED PLACARD REMOVED.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 64,793 hrs · 21,686 cycles

INSPECTION TYPE:N/AFLOOR PANEL AT POS 3/4 LEFT MULTIPLE AREAS OF DAMAGE. FABRICATED NEW FLOOR PANEL IAW SREO B767-5320-9693-I APP B

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,943 hrs · 21,007 cycles

INSPECTION TYPE:N/A FOUND EMERGENCY CEILING LIGHT NOT WORKING. REMOVED EMERGENCY CEILING LIGHT IAW AMM 33-51-11-002-008 REV 130.01. INSTALLED AND TESTED EMERGENCY CEILING LIGHT IAW AMM 33-51-11-402-014 REV 130.01. ACCOMPLISHED FUNCTIONAL TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00-725-247 REV 130.01. FOUND SATIS.

Part: CONNECTOR — CORRODED (FLAP TRANMITTER) · airframe 62,891 hrs · 20,986 cycles

INSPECTION TYPE: N/A, EMERGENCY DECLARED, LANDED W/O INCIDENT, FAA NOTIFIED. TE FLAP ASYM WHEN SELECTING FLAPS 5. LANDED WITH FLAPS 1 INDICATED. C/W FIM 27-51-00-815-811 AND FIM 27-51-00-815-819 NO FAULTS FOUND. DURING MAINTENANCE, FOUND LIGHT CORROSION ON CONNECTOR OF TRANSMITTER NR 4. CLEANED CONNECTOR AND OPS CHECK GOOD PER AMM 27-51-45-822-161.

Part: FLOOR PANEL — DAMAGED (MAIN DECK) · airframe 61,901 hrs · 20,659 cycles

INSPECTION TYPE:C13DAMAGE ON M/D CARGO FLOOR PANEL AT STA 287-STA412,RBL 11 - LBL11,PNL NO.222DFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B767-5320-9693-I

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 60,432 hrs · 20,017 cycles

INSPECTION TYPE:N/A BULK PIT FLOOR PANEL SUPPORT STRINGER STA 1440 LBL 36.91 HAS .5" CRACK TOP SECTION OF CHANNEL. REPAIRED IAW EO EO B767-5310-72036-A.

Part: UNKNOWN — MALFUNCTIONED (APU) · airframe 60,029 hrs · 19,861 cycles

INSPECTION TYPE:ETOP APU AIR INOP ON PUSHBACK. ISSUED DEFERRAL MEL 49-11-1-1 DMP ACCOMPLISHED BY CAPT. **ETOPS FILED OPEN**

Part: WARNING MESSAGE — FALSE ACTIVATION (RUDDER RATIO) · airframe 58,238 hrs · 19,175 cycles

AIR TURNBACK. RUDDER RATIO EICAS MESSAGE ENROUTE. PERFORMED FIM 27-09-00, FIG 106B, BLOCKS 1, 2, 3, 4, 5, & 6, CHECKED GOOD. PERFORMED A TEST OF THE RUDDER RATIO SYS IAW AMM 27-20-00. OPS CHECKED GOOD, NO FAULTS FOUND.

Part: DUCT — CRACKED (THRUST REVERSER) · airframe 58,184 hrs · 19,155 cycles

CRACK INSIDE NR 2 ENGINE INBD THRUST REVERSER C-DUCT, 6 OCLOCK. REPLACED FAIRING SPLICE PLATE IAW M-7830-45403-B, AND SRM 51-40-02.

Part: KEELBEAM — CORRODED (BS 918) · airframe 57,725 hrs · 18,992 cycles

INSPECTION TYPE: C12, CORROSION ON THE KEELBEAM SPLICE TEE LOWER SURFACE AT BS 918 , LBL 9 TO RBL 9. REPAIRED IAW SRM 51-40-02-0G AND DWG 145T8629.

Part: SKIN — CORRODED (RT WING) · airframe 57,725 hrs · 18,992 cycles

INSPECTION TYPE: C12, CORROSION ON THE RT WING TRAILING EDGE UPPER SKIN WS 730. REPAIR IAW SRM 57-20-01-1A-1.

Part: FLOORBEAM — CORRODED (BS 632) · airframe 57,725 hrs · 18,992 cycles

INSPECTION TYPE: C12, CORROSION ON MAIN DECK FLOORBEAM UPPER TEE LOWER SURFACE AT BS 632 , LBL 75. REPAIRED IAW EO B767-5310-67110-A

Part: ACCESS DOOR — CRACKED (POS 32) · airframe 56,197 hrs · 18,441 cycles

MCD POS 32 ACCESS DOOR TO LOWER DECK IS CRACKED, BOTTOM SIDE. INSTALLED A SERVICEABLE ACCESS DOOR IAW AMM 52-48-00-01-01-80A.

Part: UNKNOWN — MALFUNCTIONED (HF COMM) · airframe 55,495 hrs · 18,191 cycles

INSPECTION TYPE:ETOP, BOTH NR 1 & NR 2 HF RADIO CANNOT TRANSMIT, BOTH RADIO OPS CHECKED OK ON GROUND, BUT INFLIGHT WOULD NOT TRANSMIT. DIVERTED TO RJBB DUE TO NOT MEETING MINIMUM COMM REQUIREMENT FOR RNP AIRSPACE. T/S PER FIM23-11-00 FIG103. REPLACED RELAY K178 PER MM 32-09-02-201, L & R HF COUPLER PER MM 23-11-01-401, L & R HF TRANSCEIVER PER MM 23-11-03-401, L & R HF CONT PANEL PER MM 23-11-02-401. L & R HF SYSTEM TEST OK PER MM 23-11-00-501.

Part: STIFFENER — CRACKED · airframe 55,102 hrs · 18,048 cycles

INSPECTION TYPE: SPV, STIFFENER AT RBL 33 CRACKED. REPAIRED IAW SRM 57-10-10-2R PROCEDURE 2.

Part: STIFFENER — CRACKED (CENTER WING) · airframe 55,102 hrs · 18,048 cycles

INSPECTION TYPE: SPV, STIFFENER AT LBL 11 CRACKED. REPAIRED IAW SRM 57-10-10-2R PROCEDURE 2.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,102 hrs · 18,048 cycles

INSPECTION TYPE: SPV, STIFFENER AT LBL 55 CRACKED. REPAIRED IAW SRM 57-10-10-2R PROCEDURE 2.

Part: ESCAPE ROPE — UNSECURE (CREW ENTRY DOOR) · airframe 53,516 hrs · 17,486 cycles

CREW ENTRY DOOR ESCAPE ROPE UNPACKED. REPACKED IAW MM 25-61-04-402-013.

Part: STRAP — CRACKED (BS 1725) · airframe 53,259 hrs · 17,388 cycles

INSPECTION TYPE: C11, CRACK INDICATION WAS FOUND ON FASTENER HOLE OF THE BULKHEAD OUTER CHORD STRAP AT BS 1725.5. DURING REPAIR PROCESS OF THE BULKHEAD OUTER CHORD STRAP, CRACK BE FOUND ON FUSELAGE SKIN PN:148T3121-2. REPAIR BULKHEAD OUTER CHORD STRAP AND SKIN IAW SRM 53-80-01, REPAIR 5, DETAIL III, REV 64.

Part: SKIN — CRACKED (BS 1550) · airframe 53,259 hrs · 17,388 cycles

INSPECTION TYPE:C, 113.5" LONG CRACK WAS FOUND ON THE STR 20L AT BS 1550. REPAIR IAW SR 4-3105998863 WITH 8100-9 FORM DATE:14/JAN/2016 AND EO:B767-5310-59525-A.

Part: A/C PACK — ODOR · airframe 53,193 hrs · 17,364 cycles

STRONG MILDEW ODOR FROM PACKS DURING FLIGHT. PERFORMED OPS TEST OF PNEU AIR SUPPLY/DISTIBUTION SYS AND PACK TEMP CONTROL SYS IAW MM 36-11-00 AND 21-61-00, OPS NORMAL.

Part: A/C PACK — CONTAMINATED (RIGHT) · airframe 53,193 hrs · 17,364 cycles

NOTED ODOR WHEN BOTH PACKS WERE ON. TURNED RT PACK OFF AND ODOR WENT AWAY, TURNED RT PACK ON AND LEFT PACK OFF, ODOR RETURNED. PERFORMED REMOVAL OF CONTAMINATION FROM A/C SYSTEM IAW MM 21-00-21-102-030. PACK OPS CHECKED NORMAL. NO ODOR NOTED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT SIGN BESIDE DOOR FLOOR LIGHTS INOPERATIVE. R & R EMERGENCY EXIT SIGN BESIDE CREW ENTERY DOOR IAW 33-51-01.

Part: FLOOR PANEL — CRACKED (MAIN DECK CARGO) · airframe 48,926 hrs · 15,796 cycles

DURING C10 INSPECTION, FOUND A CRACK ON MAIN DECK CARGO FLOOR PANEL 241DFF BETWEEN BS 731.11 - 834, LBL 54.75 - 77.50. FABRICATE REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.

Part: FLOOR PANEL — CRACKED (MAIN DECK CARGO) · airframe 48,926 hrs · 15,796 cycles

DURING C10 INSPECTION, FOUND A CRACK ON MAIN DECK CARGO FLOOR PANEL 241KFF BETWEEN BS 850.9 - 933, LBL 74.75 - 88.5. FABRICATE REPLACEMENT FLOOR PANEL IAW EO 5320-9693-H.

Part: FLOOR PANEL — CRACKED (MAIN DECK CARGO) · airframe 48,926 hrs · 15,796 cycles

DURING C10 INSPECTION, FOUND A CRACK ON MAIN DECK CARGO FLOOR PANEL 242BFF BETWEEN BS 731.11 - 834, RBL 33, RBL 54.75. FABRICATE REPLACEMENT FLOOR PANEL IAW EO -5320-9693-H.

Part: FLOOR PANEL — CRACKED (MAIN DECK CARGO) · airframe 48,926 hrs · 15,796 cycles

DURING C10 INSPECTION, FOUND A CRACK ON MAIN DECK CARGO FLOOR PANEL 242UFF BETWEEN BS 972 - 1114.82, RBL 54.75 - 77.50. FABRICATE REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-H.

Part: WEDGE — DEBONDED (LT WING TE FLAP) · airframe 48,926 hrs · 15,796 cycles

DURING C10 INSPECTION, DISBOND ON THE LT WING OTBD FLAP T/E WEDGE LOWER SKIN AT OTEF STA 159. REPAIR IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-17, GENERAL REV:58.01.

Part: COOLING FAN — INOPERATIVE (FWD EQUIP)

AFTER TAKEOFF FWD EQUIPMENT COOLING EICAS MESSAGE APPEARED, RAN QRH AND MESSAGE REAPPEARED, ACFT LANDED. IAW QRH TROUBLESHOOTING FWD EQUIPMENT COOLING IAW FIM 21-58-00-815-831-001-004-133. ALL TEST NOW PASS OK. OK FOR SERVICE.

Part: FLOOR PANEL — CRACKED (MAIN CARGO DECK) · airframe 44,829 hrs · 14,241 cycles

INSPECTION TYPE: 9C MAIN CARGO DECK FLOOR PANEL FOUND CRACKED AT BS 1043 TO 1109, RBL 33 TO 55. MAIN CARGO DECK FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.

Part: WEDGE — DELAMINATED (LT WING TE FLAP) · airframe 44,829 hrs · 14,241 cycles

INSPECTION TYPE: 9C, LT WING OTBD T/E FLAP T/E WEDGE LOWER SURFACE AT MID AREA DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1), FIG 9, REV 52.

Part: FLOOR PANEL — CRACKED (MAIN CARGO DECK) · airframe 44,829 hrs · 14,241 cycles

INSPECTION TYPE: 9C, MAIN CARGO DECK FLOOR PANEL FOUND CRACK AND 9 FUNCTURES AT BS 973 TO 1048, LBL 33 TO 55. MAIN CARGO DECK FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — PUNCTURED (MAIN CARGO DECK) · airframe 44,829 hrs · 14,241 cycles

INSPECTION TYPE: 9C, MAIN CARGO DECK FLOOR PANEL FOUND 8 PUNCTURES AND 9 DENTS MARK AT BS 731 TO 830, LBL 11 TO RBL 11. MAIN CARGO DECK FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED IAW AMM 53-01-06.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

FLOOR PANEL, POS 4 AFT CENTER HAS 2 HOLES BETWEEN OTBD 1ST AND 2ND RESTRAINTS. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-6993-H.

Part: FLOOR PANEL — DAMAGED (CARGO DECK)

MCD POS NR 2 AFT CENTER FLOOR PANEL HAS 2 HOLES. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

FLOOR PANEL DAMAGE. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

FLOOR PANEL DAMAGED. FABRICATED NEW PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MCD POS 6 CENTER FWD HAS 3 HOLES. REPAIR IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MCD FLOOR PANEL NR 6 CENTER FWD HAS 3 HOLES. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED

FLOOR PANEL POS NR 9L, 3RD PANEL FROM LT HAS HOLE. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MCD FLOOR PANEL POS 6 FWD CENTER HAS HOLE. REPAIRED FLOOR PANEL IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MCD FLOOR PANEL POS 9 CENTER AFT END HAS HOLE. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (BS 654.110)

MCD FLOOR PANEL POS NR 5 CENTER HAS HOLE STA 654.110 7 INCHES RIGHT OF CENTER. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK POS 4 FWD CENTER OF PANEL HAS A HOLE. REPAIRED REF SRM 53-00-50-2R, REPAIR 1.

Part: FLOOR PANEL — DAMAGED (BS 654)

MAIN CARGO FLOOR PANEL DAMAGED AT STA 654+98. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (BS 654)

FLOOR PANEL DAMAGED STA 654+110. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (BS 1500)

MAIN CARGO DECK FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.

Part: FLOOR PANEL — DAMAGED (BS 1343)

MAIN CARGO DECK FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.

Part: FLOOR PANEL — DAMAGED (BS 654.98)

MCD POS 5 CTR FLOOR PANEL HAS HOLE STA 654.98 1 INCH RT OF CTR. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (BS 1460)

MAIN CARGO FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.

Part: FLOOR PANEL — DAMAGED (MAIN DECK)

MAIN CARGO DECK POSITION 4 AFT CENTER OF PANEL HAS A HOLE. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (BS 1300)

FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50.

Part: ESCAPE ROPE — OUT OF TRACK (MAIN ENTRY DOOR)

ROPE END HAD FALLEN OUT OF TRACK IN DOOR CUT OUT. STOWED ROPE END BACK IN TRACK IAW AMM 25-61-04-2.

Part: WEDGE — DENTED (LT TE FLAP)

LT HAND OTBD FLAP T/E WEDGE HAS DENT AND DEBONDED AT STA 254.69. REPAIRED IAW EO B767-5750-40481-B.

Part: CONNECTOR — BROKEN (SMOKE DETECTOR)

INSPECTION TYPE:ETOP DIVERSION - "CARGO DET AIR" EICAS MESSAGE. M438137. R & R SMOKE DETECTOR VACUUM SWITCH IAW AMM 26-16- 04-4. FOUND CONNECTOR BROKEN ON SWITCH.

Part: WEDGE — DAMAGED (RT AILERON)

RT OTBD AILERON T/E WEDGE LIGHTNING DAMAGE. REPAIRED IAW EO B767-5750-38137-B.

Part: SKIN — DAMAGED (RT AILERON)

RT OTBD AILERON HAS 4 OTHER AREAS OF LIGHTNING STRIKE DAMAGE ON UPPER SURFACE OF WEDGE MARKED. STARTED SANDING AREA, FWD LIMITS TO ENGR. FINISHED DAMAGE REMOVAL REF SRM 57-60-02-2R. STARTED NR 346819. REPAIR COMPLETE SEE NRC 346819 AND ECA 020462. THIS REPAIR IS CONSIDERED PERMANENT. THIS IS A MAJOR REPAIR.

Part: SHIM — UNKNOWN (BS 955 FAILSAFE) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C FUS REMOVE FASTENERS / PARTS IDENTIFIED IN EO B767-5350-17922-E APP C, FIG 6 AS NECESSARY TO INSTALL A PROTECTIVE SHIM FASTENER / PARTS. REMOVED AND REINSTALLED IAW EO B767-5350-17922-E APPENDIX C FIG 6 IN ORDER TO INSTALL A PROTECTIVE SHIM BETWEEN THE SKIN AND THE FAIL SAFE STRAP.

Part: SKIN — MISREPAIRED (BS 439-463) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, SURVEY SEQ NR 302-F1-02 FUSELAGE BETWEEN BS 439 TO BS 463 AND STR 23R-25R EXISTING REPAIR DOES NOT CORRELATED TO A SRM. SURVEY SEQ 302-F1-02 FX BTN BS436-463 & STR23R-25R SKIN REPAIRED IAW RS R53-00-36706, EO B767-5330-37489, ORG MATL IS 2024T3 MACHINED SKIN 0.063" THICKNESS AT TRIM OUT AREA. FINAL CUTOUT SIZE IS 5.7" X 2.75" REPAIR SIZE IS 203.375" X 16.55" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH 2024T3-0.090" AS A DOUBLER.

Part: WEDGE — CRACKED (TE FLAP) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C RT WING O/B TRAILING EDGE FLAP TRAILING EDGE WEDGE I/B AFT EDGE AREA CRACKED. COMPOSITE PREP REG LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5G FIG 14.

Part: FAILSAFE — CRACKED (BS 955) · airframe 40,306 hrs · 12,722 cycles

INSP TYPE:C FUS RT BS 955 BULKHEAD FITTING AREA CRACK AT FAIL SAFE STRAP APPROX .2500" & .3750" IN LENGTH. REFER NRC 50422 FOR DETAIL, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-E, APPENDIX D.

Part: BRACKET — CRACKED (LT WING) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, LT WING - L/E LES675 FIXED FAIRING SUPPORT WEB AFT FRONT SPAR BRACKET FOUND CRACKED. LT WING L/E LES675 FIXED FAIRING SUPPORT WEB AFT FRONT SPAR BRACKET, REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, FX - RT STA 955 BULKHEAD FITTING AREA CORROSION FOUND AT "T" FITTING HOLE AROUND THE HOLE BORE SURFACE. RT STA 955 BULKHEAD FITTING AREA "T" FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-E APPENDIX D, FIG 6.

Part: FITTING — CRACKED (RT BS 955) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, FUS RT BS 955 REAR SPAR BULKHEAD FITTING AREA 1EA FASTENER HOLE FOUND CRACKED INDICATIONS RUNNING BOTH FWD & AFT FUSELAGE RT BS 955 REAR SPAR BULKHEAD FITTING AREA FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-E, APPENDIX D.

Part: FAILSAFE — CRACKED (LT BS 955) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C FUS LT B S955 BULKHEAD FITTING FAIL SAFE STRAP CRACK FOUND AT FWD SIDE THRU THICKNESS AT 9 O/C POSN AFT SDE CRACK AT 5 O/C POSITION (LOCKING INBD) APPROX 0.040" REF NRC 50425 FOR DETAIL. FUSELAGE LT BS955 REAR SPAR BULKHEAD FITTING AREA FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-E APPENDIX C.

Part: FITTING — CRACKED (BS 955) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C FX - LT STA 955 BULKHEAD TEE FITTING CRACK FOUND AT 7 O`CLOCK POSITION APPROX .0625" LONG. FX - LT STA 955 BULKHEAD TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-E APPENDIX C, FIG 6.

Part: FLOOR PANEL — PUNCTURED (CARGO DECK) · airframe 40,306 hrs · 12,722 cycles

INSP TYPE:C, MCD FLOOR PANEL FOUND PUNCTURED, DAMAGED AT STN 588 TO 654+22 RBL 77" TO RBL 88". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, RT WING L/E LES 160 FRONT SPAR UPPER SUPPORT ANGLE FOUND CRACKED CRACK LENGTH .3750". RT WING L/E LES 160 FRONT SPAR UPPER SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 46.

Part: FLOOR PANEL — MISREPAIRED (BS 654-690) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, MCD FLOOR PANEL FOUND DAMAGE AND INCORRECT REPAIR EXISTING AT STN 654+22 TO STN690 LBL33" TO LBL55". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: FITTING — CRACKED (BS 955 BULKHEAD) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C FUS LT BS955 REAR SPAR BULKHEAD FITTING AREA 1EA FASTENER HOLE FOUND CRACKED INDICATIONS RUNNING BOTH FWD & AFT FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING AREA FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-E, APPENDIX C.

Part: FLOOR PANEL — PUNCTURED (BS 975-1114) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, MCD FLOOR PANEL FOUND PUNCTURE DAMAGE AT STN975 TO 1114 LBL11" TO RBL11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: PANEL — CHIPPED (RT ELEVATOR) · airframe 40,306 hrs · 12,722 cycles

INSP TYPE:C EMP - RT INBD ELEVATOR T/E OTBD CORNER UPPER SURFACE CHIPPED COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW RS R55-20-36704, REV A AND EO B767-5520-37442-A.

Part: FLOOR PANEL — MISREPAIRED (BS 833-933) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, MCD FLOOR PANEL FOUND DAMAGE AND INCORRECT REPAIR EXISTING AT STN 833 TO STN933 LBL11" TO RBL11". FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.

Part: STIFFENER — CRACKED (WING CTR TANK) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, WING CTR SECTION FRONT SPAR VERTICAL STIFFENER FOUND CRACKED JUST AT STA785.9 RBL10.94" WING CTR SECTION FRONT SPAR VERT STIFFENER REPAIRED IAW RS R57-00-36703, EO B767-5710-37458 JUST AT STA785.9 RBL10.94" ORG MATL IS BAC1518-749-2024T3511, CRK LENGTH 3.25", CUT OFF LENGTH 19.5" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH BAC1518-749-2024T3511 AS REPLACEMENT SECTION. TOTAL REPAIR LENGTH 25.5"

Part: HINGE FITTING — CRACKED (LT WING TE FLAP) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, LT WING INBD MAIN FLAP INBD SUPPORT HINGE FITTING FLANGE FOUND CRACKED. LT WING INBD MAIN FLAP INBD SUPT HINGE FTG REPAIRED IAW SRM 57-53-02-2R1, FIG201, ORG MATL IS 7075T73 FORGING, CRACK LENGTH AT BOTH INBD & OTBD FLANGE ARE 1.5", DAMAGED CUTOUT SIZE ARE 1.5" X 0.75" (2 LOCATIONS) THIS IS CLASSIFIED AS A MAJOR REPAIR WITH AND 10134-2007-7075T6511 AS REPAIR ANGLE, REPAIR SIZE IS 2" X 4".

Part: HINGE FITTING — CRACKED (RT WING TE FLAP) · airframe 40,306 hrs · 12,722 cycles

RT WING - INBD MAIN FLAP INBD SUPPORT HINGE FITTING FLANGE FOUND CRACKED. RT WING INBD MAIN FLAP INBD SUPT HINGE FTG REPAIRED IAW SRM 57-53-02-2R1, FIG 201, ORG MATL IS 7075T73 FORGING, CRK LENGTH AT BOTH INBD & OTBD FLANGE ARE 1.5", DAMAGED CUTOUT SIZE ARE 1.5" X 0.75" (2 LOCATIONS) THIS IS CLASSIFIED AS A MAJOR REPAIR WITH AND 10134-2007-7075T6511 AS REPAIR ANGLE, REPAIR SIZE IS 2" X 4".

Part: RIB — CRACKED (RT WING) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, RT WING INBD AILERON INBD RIB FTG UPPER AFT FLANGE FOUND CRACKED. RT WING INBD AILERON INBD RIB FTG UPR AFT FLANGE REPAIRED IAW RS R57-00-36698 & EO B767-5740-37472-A, ORG MATL IS 7075T73FORGING, CRACK LENGTH IS 1.1", FINAL CUTOUT SIZE IS 1.7" X 0.8" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL BAC1505-100081-7075T6511 AS REPAIR CLIP, REPAIR SIZE IS 1.5" X 2".

Part: FLOORBEAM — CRACKED (BS 246) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, MAIN DECK STA 246 FLOORBEAM ATTACH CLIP FOUND CRACKED AT LBL 50" MAIN DECK STA 246 FLOORBEAM AT LBL50" ATT CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, LT WING NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT INBD NOSE SKIN AT OSS723.9 SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1" DAMAGED CUTOUT IS 8.8750" X 7.2500". THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH 7075T6-0.071" AS REPAIR DOUBLER, 7075T6-0.063" AS REPAIR PLATE. REPAIR SIZE IS 12.1250" X 10.5".

Part: SKIN — CRACKED (NR 10 SLAT) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, RT WING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT OTBD NOSE SKIN AT OSS792.5 SKIN REPAIRED IAW SRM 57-43-01-2R2 FIG 201, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1" DAMAGED CUTOUT IS 8.8750" X 7" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH 7075T6-0.071" AS REPAIR DOUBLER, 7075T6-0.063" AS REPAIR PLATE. REPAIR SIZE IS 12" X 10.1250".

Part: SKIN — CRACKED (NR 9 SLAT) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, JUST AT OSS 572.5, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.08" DAMAGED CUTOUT IS 8.875" X 7.25" THIS IS CLASSIFIED AS A MAJOR REPAIR WITH 7075T6-0.071" AS REPAIR DOUBLER AND 7075T6-0.063" AS REPAIR PLATE, REPAIR SIZE IS 12.125" X 10.25".

Part: RIB — CRACKED (LT WING) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:8C, LT WING - INBD AILERON INBD RIB FITTING UPPER AFT FLANGE FOUND CRACKED. LT WING INBD AILERON INBD RIB FITTING UPPER AFT FLANGE REPAIRED IAW HX RS NO R-57-00-36699 REV A & UPS EO NO. B767-5740-37473-A. ORG MAT'L IS 7075T73 FORGING, CRK LENGTH 1", FINAL CUTOUT SIZE 1.7"X0.8". CLASSIFIED AS A MAJOR REPAIR WITH MAT'L BAC1505-100081-7075T6511 AS REPAIR CLIP, REPAIR SIZE IS 1.46" X 2".

Part: SKIN — CRACKED (NR 4 SLAT) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, LT WING NR 4 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR4 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, JUST AT OSS641.9, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.25" DAMAGED CUTOUT IS 8.875" X 7" THIS IS CLASSIFIED AS A MAJOR REPAIR WITH 7075T6-0.071" AS REPAIR DOUBLER, 7075T6-0.063" AS REPAIR PLATE REPAIR SIZE IS 12.125" X 10.125"

Part: SKIN — CRACKED (NR 10 SLAT) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT INBD NOSE SKIN AT OSS723.9 SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.2" DAMAGED CUTOUT IS 8.8750" X 7.1250". THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH 7075T6-0.071" AS REPAIR DOUBLER, 7075T6-0.063" AS REPAIR PLATE. REPAIR SIZE IS 12" X 10.1250".

Part: SKIN — CRACKED (NR 9 SLAT) · airframe 40,306 hrs · 12,722 cycles

INSP TYPE:C, RT WING NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT OTBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201. JUST AT OSS641.9, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.09" DAMAGED CUTOUT IS 8.875" X 7.125". THIS IS CLASSIFIED AS A MAJOR REPAIR WITH 7075T6-0.071" AS REPAIR DOUBLER, 7075T6-0.063" AS REPAIR PLATE. REPAIR SIZE IS 12" X 10.25"

Part: FLOORBEAM — CRACKED (BS 246) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, MAIN DECK STA 246 FLOORBEAM ATTACH ANGLE FOUND CRACKED AT LBL 25". MAIN DECK STA 246 FLOORBEAM AT LBL 25" ATTACH ANGLE REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02.

Part: SKIN — CRACKED (NR 3 SLAT) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, LT WING NR 3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT OTBD NOSE SKIN AT OSS792.5 SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, ORG MATL IS 7075T6-0.063", CRK LEGNTH IS 0.09". DAMAGED CUTOUT IS 8.875" X 7.125" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH 7075T6-0.071" AS REPAIR DOUBLER, 7075T6-0.063" AS REPAIR PLATE, REPAIR SIZE IS 12" X 10.1250".

Part: SKIN — CRACKED (NR 4 SLAT) · airframe 40,306 hrs · 12,722 cycles

INSPECTION TYPE:C, LT WING NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LTW NR4 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201 JUST AT OSS572.5, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.125" DAMAGED CUTOUT IS 8.875" X 7.125" THIS IS CLASSIFIED AS A MAJOR REPAIR WITH 7075T6-0.071" AS REPAIR DOUBLER, 7075T6-0.063" AS REPAIR PLATE, REPAIR SIZE IS 12" X 10.25"

Part: FUEL FILTER — WARNING LIGHT (RT ENGINE)

INSPECTION TYPE:ETOP ATB - RT ENG FUEL FILTER STATUS MESSAGE. REMOVED AND REPLACED RT ENGINE FUEL FILTER PER B767 73-11-02-4. LEAK CHECK GOOD GROUND RAN ENGINES 30 MINUTES. NO PROBLEMS FOUND. A/C OK FOR SERVICE. OLD FILTER APPEARED TO BE OK PER FIM 73-31-00.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A MCD FLOOR PANEL POS 5R DAMAGED. REPAIRED PER SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A MCD FLOOR PANEL POS 5R. REPAIRED PER SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A MCD FLOOR PANEL 5R DAMAGED. REPAIRED PER SRM 53-00-50-2R.

Part: ESCAPE ROPE — FRAYED (CABIN)

INSPECTION TYPE:N/A ESCAPE ROPE FALLS OUT OF STORAGE POUCH AND BINDING DOOR AS IT OPENS. REPLACED DESCENT ROPE AND CHANNEL COVER.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY)

INSPECTION TYPE:N/A MAIN DECK FLOOR PANEL AT STA 627 BL 0 DAMAGED 1 INCH HOLE IN TOP SKIN AT CENTER OF PANEL. DAMAGE 59 INCHES FROM AFT OF PANEL AND 3.5 INCHES FROM RT EDGE OF PANEL. REPAIR PER EO B767-5320-32392-A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY)

INSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL IN CENTER OF POSITION 3 HAS HOLE. TRANSFERRED TO NRC 323651. REMOVED DAMAGE REF EO B767-5320-32391A. DAMAGE REMOVAL VERIFIED. OK TO INSTALL REPAIR. POTTED CORE & CURED AS PER SRM 53-00-50-2R. INSTALLED REPAIR PLIES AND CURED PER SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY)

MAIN CARGO FLOOR PANEL IN CENTER POSITION 6/7 HAS 4 SMALL HOLES. TRANSFERRED TO NRC 353653. REMOVED DAMAGE REF EO B767-5320-32393-A. POTTED CORE & APPLIED REPAIR PLIES IAW EO B767-5320-32393 AND SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A FLOOR PANEL DAMAGED AT STA 671 BL 0, 14 INCHES FROM AFT EDGE OF PANEL 3 INCHES FROM RT SIDE OF PANEL PUNCTURE .75 INCH DIA. REPAIR PER EO B767-5320-32392-A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY)

INSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL HAS .75 INCH HOLE IN CENTER POSITION 4 (DEF387483). TRANSFERRED TO NRC 353652. REMOVED DAMAGE & INSTALLED REPAIR REF EO B767-5320-32392A.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY)

MAIN CARGO DECK FLOOR PANEL HAS .75 INCH HOLE IN CENTER OF POSITION 5, DEF 387484. TRANSFERRED TO NRC 363350. REMOVED DAMAGE & INSTALLED REPAIR PER EO B767-5320-32392A.

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

INSPECTION TYPE:ETOP RTO LT ENG COMPRESSOR STALLED. PULLED HARD LEFT AT 80 KTS. TOWER REPORTED FLAMES FROM LEFT ENGINE AFTER ABORT. A/C OOS. ***SDR FILED OPEN***

Part: WEB — CRACKED (LT WING) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:N/A LEFT WING LES 675 FWD OF REFUEL PANEL LOWER CHORD FOUND CRACK. LEFT WING FWD D-NOSE FAIRING SUPPORT WEB REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02, JUST BETWEEN OSS648 AND 694 REFER NRC50623 FOR WORKING DETAIL.

Part: WEB — CRACKED (LT WING) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:N/A LEFT WING LES 694 FWD D-NOSE FAIRING SUPPORT WEB LOWER AREA FOUND CRACKED. CRACK LENGTH 2.5 INCHES APPROX. LEFT WING FWD D-NOSE FAIRING SUPPORT WEB REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02, JUST BETWEEN OSS648 AND 694 AREA.

Part: STIFFENER — CRACKED (LT WING) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:N/A LEFT WING LES 665 FRONT SPAR STIFFENER UPPER AREA FOUND CRACK. CRACK LENGTH .5 INCH APPROX . LEFT WING LES 665 FRONT SPAR STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.

Part: STIFFENER — CRACKED (RT WING) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:N/A RIGHT WING LES 665 FRONT SPAR STIFFENER UPPER AREA FOUND CRACK. CRACK LENGTH .5 INCH APPROX. RIGHT WING LES 665 FRONT SPAR STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:N/A MEC STA 246 RBL 10 FLOORBEAM STIFFENER CRACK. CRACK LENGTH .375 INCH. MEC STA 246 RBL 10 FLOORBEAM ATTACHED STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.

Part: ANGLE — CRACKED (RT WING) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:C RIGHT WING LES 679 FRONT SPAR SUPPORT ANGLE FOUND CRACK. CRACK LENGTH .375 INCH APPROX. RIGHT WING LES 679 FRONT SPAR SUPPORT ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.

Part: WEB — CRACKED (RT WING) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:N/A RIGHT WING LES664 FWD D-NOSE WEB FOUND CRACKED AT LWR AREA. CRACK LENGTH 2 TO 2.5 INCHES APPROX. RIGHT WING FWD D-NOSE SUPPORT WEB REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02, JUST BETWEEN OSS648 AND 694. REFER NRC50622 FOR WORKING DETAIL.

Part: WEB — CRACKED (RT WING) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:N/A RIGHT WING LES 679 FWD D-NOSE SUPPORT WEB FOUND CRACK AT LOWER AREA. CRACK LENGTH 2 INCHES TO 2.5 INCHES APPROX. RIGHT WING FWD D-NOSE SUPPORT WEB REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 JUST BETWEEN OSS648 AN 694 AREA.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:C BULK CARGO STA 1580 RBL 75 FLOOR PANEL SUPPORT BRACKET CRACKED. CRACK THROUGH 2 INCH APPROX. BULK CARGO STA 1580 RBL 75 FLOOR SUPPORT BRACKET ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:C AFT CARGO COMPT STA 1087 LBL 25" END WALL SUPPORT LOWER BRACKET CRACK. CRACK LENGTH .875 INCH APPROX. AFT CARGO COMPT STA 1087 LBL 25" LOWER SUPPORT BRACKET REPLACED PER SRM 51-10-02 AND INSTALLED PER SRM 51-40-02.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:C AFT CARGO COMPT STA 1087 RBL 25" END WALL SUPPORT LOWER BRACKET CRACK. CRACK LENGTH .75 INCH APPROX. AFT CARGO COMPT STA 1087 RBL 25" LOWER SUPPORT BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:C BULK CARGO STA 1580 LBL 75 FLOOR PANEL SUPPORT BRACKET CRACKED (1.375 INCH APPROX). BULK CARGO STA 1580 LBL 75 FLOOR SUPPORT BRACKET ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 35,111 hrs · 11,112 cycles

INSPECTION TYPE:N/A CUSTOMER REQUEST - CLARIFY PREVIOUS REPAIR AND C/OUT PERMANENT REPAIR ON FX SKIN BETWEEN BS 654+100 AND BS 654+121 AT STR 19L AS PER UPS EO B767-5330-28779-A AND BOEING MSG 1-781623252. FX STA 654+97 TO STA 654+131.5 BETWEEN STR 18L-20L AREA SKIN REPAIRED STA 654+110 AND STA 654+121 AT STR 19L TEAR STRAP REPAIRED AS PER RS R53-30-36014. 4EA SHEAR TIE AND 2EA TIE CLIP REPLACED AND INSTALLED AS PER RS R53-30-36014. THIS REPAIR WILL BE CLASSIFIED AS CAT B. REPEAT INSP IS REQUIRED AS PER UPS EO B767-5330-28779-B.

Part: PRESSURE SWITCH — MALFUNCTIONED (HYD SYSTEM)

LOST CENTER HYDRAULIC PRESSURE WHILE ENROUTE. FLIGHT CREW FOLLOWED AOM CHECKLIST AND CONTINUED TO OAK. DECLARED EMERGENCY. A/C TAXIED TO GATE UNDER OWN POWER. ACCOMPLISHED OPERATIONAL TEST OF CENTER HYDRAULIC SYSTEM PER B767 MM 29-11-00-5. NO FAULTS NOTED. CHANGED CENTER SYSTEM AND ADP PRESSURE SWITCHES PER B767 MM 29-31-01-4. EICAS MSG CLEARED.

Part: LINE — LEAKING (HYD SYSTEM)

AIR TURNBACK, LEFT HYDRAULIC QUANTITY LOSS. T/S & FOUND HYD LEAKING AT THE L/H ENG STRUT HYD. BAY. OPENED & IN- SPECTED, FOUND DIFF PRESS IND. ON PRESS & DRAIN CASE FILTER MODULE LEAKING. R/R D.P.I. AS PER AMM 29-11-17-4; LEAK CK'D SATIS.

Part: PANEL — CRACKED (LT WING)

INSPECTION TYPE:PFLT LT O/B WING PANEL CRACKED 18 INCH AND 24 INCH AT FLAP TRACK. ***MRR FILED AS OPEN***

Part: ATTACH FITTING — CRACKED (LT WING TE FLAP)

INSPECTION TYPE:PFLT LEFT WING, LEFT O/B FLAP, PANEL (WING) ABOVE O/B FITTING HAS AN 18 INCH CRACK THRU AND 24 INCH CRACK THRU THE PANEL. (SEE ITEM 1, PG 534960) MARKED THE UPPER SURFACE. REMOVED PANEL AND ACCOMPLISHED INTERIM REPAIR IAW B767-5750-13691A INSPECT EA W/E CK AND PERMANENT REPAIR AT NEXT C-CK.

Part: SHUTOFF VALVE — FLUCTUATES (LT ENGINE)

PILOTS REPORT, LT ENGINE DUCT PRESSURE FLUCTUATION. T/S PER FIM TO LT ENGINE HIGH-STAGE VALVE. REPLACED LEFT ENGINE HPSOV PER AHM 36-11-07 PAGE 401-109 ALL TEST NORMAL

Part: ENGINE — MALFUNCTIONED (RIGHT)

INSPECTION TYPE:N/A, PILOT REPORT, RIGHT ENGINE SHUTDOWN ON LANDING. REMOVED AND REPLACED ENGINE.

Part: ESCAPE ROPE — DAMAGED (CREW ENTRY DOOR)

INSPECTION TYPE-N/A, REF: D138876 EMERGENCY ESCAPE ROPE AND BAG AT CREW ENTRY DOOR DAMAGED. INSTALLED EMERGENCY ESCAPE ROPE AND BAG. THIS CLEARS D138876 PLACARD REMOVED.

Part: ROPE BAG — TORN (CREW ENTRY DOOR)

INSPECTION TYPE-N/A, EMERGENCY ESCAPE ROPE AND BAG DAMAGED. REMOVED ROPE AND BAG AND DEACTIVATED 1ST OBS AND SUPERNUMERARY SEATS. POSSIBILITY OF ROPE GETTING CAUGHT ON THE DOOR UPON OPENING OR CLOSING.

Part: GASKET — LEAKING (OIL PUMP MOUNT)

INSPECTION TYPE N/A, SIMULATED LOSS OF OIL QUANTITY IN RIGHT ENGINE, ENG OIL PRESS LIGHT ILLUM, ENG OIL PRESS ZERO, ENG OIL QUANTITY ZERO. FOUND GASKET LEAKING AT OIL PUMP MOUNTING GASKET. REMOVED AND REPLACED GASKET IAW MM 79-21-03, NO OIL LEAKS NOTED. SERVICED OIL TANK WITH 18 QUART OF OIL.

Part: SEAL — BLOWN (CARGO DOOR)

SIMULATED ETOPS WHILE AT YQX, A/C SUSTAINED RAPID DECOMPRESSION IN-FLIGHT AND DIVERTED TO YQX. MAINTENANCE FOUND MAIN CARGO DOOR SEAL BLOWN. REPLACED DOOR SEAL AND OPERATIONAL CHECK OF PRESSURIZATION SYSTEM NORMAL FOR BOTH SYS 1 AND SYS 2.

Part: FUEL PUMP — FAILED (RT ENGINE)

CREW REPORTED, RT ENGINE FLAMED-OUT AT TOP OF DESCENT. INFLIGHT START ATTEMPT UNSUCCESSFUL DUE TO NO FUEL FLOW. MAINTENANCE REMOVED AND REPLACED FUEL PUMP IAW MM 73-11-01.