N305UP

Part: HF COMM — MALFUNCTIONED (LEFT) · airframe 70,829 hrs · 24,427 cycles

*AIR TURN BACK* TRANSMISSION FROM ANY CREW POSITION ON LHF NOT POSSIBLE. LH HF OPS NML REF AMM 23-11-00.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 70,232 hrs · 24,152 cycles

CRACKED FLOORBEAM MID CHORD CRACK AT STA 246 NEAR LBL 40 (REPAIR) ACCOMPLISHED REPAIR I.A.W UPS EO NO: EO-91052-REQ1 REV1.

Part: DRAIN — DISCOVERED · airframe 70,232 hrs · 24,152 cycles

FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) ACCOMPLISHED SDR PER EO 82173-JIC001

Part: SUPPORT — CRACKED (ZONE 600 SLAT) · airframe 70,232 hrs · 24,152 cycles

**SUPPLEMENTAL SDR**FAULT - CRACK - BRACKET, R/H WING NO.7 SLAT LOWER DOOR. REMOVED DAMAGED PART IAW SRM 51-40-02 REV 89. PERFORMED CHROMIC ACID ANODIZE IAW EGAT WORK SHEET NO. 40586 STEP 7 & SPWPS-AN-004 REV 23 AND SPDS-AN REV 39 (REPLACE) REVIEWED TASK PER GMM-MTX 09.05.01.09.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 70,232 hrs · 24,152 cycles

CORROSION - INTERCOSTAL, BULK CARGO COMPARTMENT FLOOR BEAM SUPPORT INTERCOSTAL AT STA 1602 LBL 40 - LBL 54" (EVALUATE) REVIEWED TASK PER GMM-MTX 09.05.01.09.PERFORMED THE HEAT TREATMENT FROM 2024-O-071 BARE TO T62 CONDITION. I.A.W. WORK SHEET NO.:40598 STEP 3 AND SPWPS-HT-008 REV.32 AND SPDS-HT-005 REV.33 (REFER TO SHOP LOG NO:2024-239)

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 70,232 hrs · 24,152 cycles

BULK CARGO COMPARTMENT FLOOR SUPPORT AT 1602 RBL 54". REMOVED DAMAGED PART. FRABRICATED FLOOR SUPPORT IAW EGAT WORK SHEET NO. 40599 STEP 2.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 70,232 hrs · 24,152 cycles

BULK CARGO COMPARTMENT FLOOR SUPPORT INSTERCOSTAL AT STA 1602 RBL 10" ~ 15" (EVALUATE) CONDITION CHECK OK. REMOVED DAMAGED PART I.A.W. SRM 51-40-02-0G REV. 89. FABRICATED INTERCOSTAL I.A.W. EGAT WORK SHEET NO 40600 STEP 2.

Part: SUPPORT BRACKET — CORRODED (ZONE 200) · airframe 70,232 hrs · 24,152 cycles

CORROSION, PANEL 149BL FWD SIDE SUPPORT BRACKET, ACCOMPLISHED REPAIR PER EO-90997-REQ1 AND EGAT EI F2024A53M-1830, REV. 0.

Part: SKIN — CORRODED (ZONE 100) · airframe 70,232 hrs · 24,152 cycles

CORRODED SKIN, AFT CARGO COMPARTMENT LOWER LOBE SKIN AT STA 1197~STA 1197+22 S-35R TO S-36R. (REPAIR) I.A.W. EGAT EI NO.F2024A53M-1821 REV.2 SEQUENCE:C PAGE:1 OF 9 STEP:3.A.B, COMPLETED TO MACHINE THE BASE DOUBLER/FLAT FILLER THE THICKNESS FROM 0.125" TO 0.112"/0.250" TO 0.200". OPEN

Part: SKIN — CORRODED (ZONE 100) · airframe 70,241 hrs · 24,153 cycles

**SUPPLEMENTAL SDR**FAULT - CORROSION - SKIN, AFT CARGO COMPARTMENT LOWER LOBE SKIN AT STA 1197~STA 1197+22 S-35R TO S-36R.PERFORMED THE HEAT TREATMENT FROM 7075-O-100 BARE TO T62 CONDITION. I.A.W. EGAT EI NO.:F2024A53M-1821 SEQUENCE A PART A STEP 1.8) REV.0 AND SPWPS-HT-008 REV.32.PERFORMED NDT/ET FOR FASTENER HOLES I.A.W. 767 NTM PART6 51-00-16 REV:138. RESULT:NO CRACK WAS FOUND. (REPAIR)

Part: SKIN — CORRODED (ZONE 100) · airframe 70,232 hrs · 24,152 cycles

CORROSION - SKIN, AFT CARGO COMPARTMENT LOWER SKIN AT STA 1197+88~STA 1197+132 S-35R~S-36R.PERFORMED THE HEAT TREATMENT FROM 7075-O TO T62 CONDITION. I.A.W. EGAT EI NO.:F2024A53M-1838 SEQUENCE A PART A STEP 1.8) REV.0 AND SPWPS-HT-008 REV.32 AND SPDS-HT-005 REV.33 (REFER TO SHOP LOG NO:2024-241)

Part: STRINGER — CORRODED (ZONE 100) · airframe 70,232 hrs · 24,152 cycles

CORROSION - STRINGER, AFT CARGO COMPARTMENT LOWER SIDE SKIN AT STA 1197+66~STA 1197+88 S-34R. PERFORMED THE HEAT TREATMENT FROM 7075-O-080 CLAD TO T62 CONDITION. I.A.W. EGAT EI NO.:F2024A53M-1832 SEQUENCE A STEP 9 REV.0

Part: ANGLE — CRACKED (ZONE 100) · airframe 70,232 hrs · 24,152 cycles

FOUND BULK CARGO COMPARTMENT LEFT AREA ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89.INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 146T5650 SH. 5 REV. C.

Part: RIB — CRACKED (LT NR 3 SLAT) · airframe 70,232 hrs · 24,152 cycles

CRACKED RIB, L/H WING NO.3 SLAT OUTBD AUXILIARY TRACK FWD ARM AREA.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 114T4103 SH. 7 REV. B AND NO. 114T4103 SH. 8 REV. A.

Part: ANGLE — CRACKED (ZONE 100) · airframe 70,232 hrs · 24,152 cycles

FOUND BULK CARGO COMPARTMENT RIGHT AREA ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD.REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 89, INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 89. AND BOEING DWG NO. 146T5650 SH. 5 REV. C.

Part: FLOOR PANEL — DENTED (MAIN DECK) · airframe 70,232 hrs · 24,152 cycles

FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231DFF P/N: 143T5876-37.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3 CONDITION CHECK IS SATISFACTORY.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 70,232 hrs · 24,152 cycles

FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231CFF P/N: 143T5876-39.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9696-REQ001 REV 3. CONDITION CHECK IS SATISFACTORY.

Part: MASTER CAUTION — INOPERATIVE (ZONE 200) · airframe 70,250 hrs · 24,157 cycles

DFDR REPORT FAR #30 MASTER WARNING CAPT FAIL. (TROUBLESHOOTING/REPAIR) I.A.W AMM 33-13-00-902-045 REV 142 REPLACED MASTER WARNING SWITCH S507, AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 70,232 hrs · 24,152 cycles

FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231LFF P/N: 143T5876-51.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9696-REQ001 REV 3. CONDITION CHECK IS SATISFACTORY

Part: WARNING SYSTEM — FAILED (CAPTAIN'S MASTER) · airframe 70,232 hrs · 24,152 cycles

DFDR REPORT FAR #30 MASTER WARNING CAPT FAIL. (TROUBLESHOOTING/REPAIR) OK TO WORK.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 70,232 hrs · 24,152 cycles

FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 231EFF P/N: 143T5876-63.FLOOR PANEL SEALANT REMOVED AND OK TO INSTALL. FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9696-REQ001 REV 3. CONDITION CHECK IS SATISFACTORY.

Part: FLOOR PANEL — DENTED (ZONE 200) · airframe 70,232 hrs · 24,152 cycles

FOUND MAIN DECK CARGO FLOOR PANEL DENT, PANEL NO: 251FFF P/N: 146T5869-17.FLOOR PANEL SEALANT REMOVE AND OK TO INSTALL CHECK OK.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. CONDITION CHECK IS SATISFACTORY.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,578 hrs · 23,571 cycles

*SDR FILED OPEN* CREW DOOR CLEAR PLASTIC COVER FOR LEVER LATCH STUCK IN THE OPEN POSITION DEFERRED AS PAR MEL 52-11-2 PLACARDS INSTALLED

Part: COVER — BROKEN (DOOR HINGE) · airframe 68,596 hrs · 23,577 cycles

*** SUPPLEMENTAL SDR *** CREW DOOR CLEAR PLASTIC COVER FOR LEVER LATCH STUCK IN THE OPEN POSITION R&R CREW DOOR CLEAR PLASTIC COVER HINGE PER IPC 52-11-02-10A ITEM 170 REMOVED PLACARD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,010 hrs · 23,342 cycles

MAIN ENTRY/SERVICE DOOR ARMING LEVER COVERS WON€™T STAY DOWN DEFERRED PER MEL 52-11-2. PLACED COVER IN PFM BOX. PLACARD INSTALLED. OPEN

Part: SERVICE DOOR — INOPERATIVE (UNKNOWN) · airframe 68,029 hrs · 23,347 cycles

*** SUPPLEMENTAL SDR *** MAIN ENTRY/SERVICE DOOR ARMING LEVER COVERS WON€™T STAY DOWN ++ REINSTALLED SECONDARY CAPTURE LEVER ACCESS DOOR/COVER, ADJUSTED, AND OPS CHECKS GOOD REF AMM 52-12-00 AND IPC 52-11-02-10A, PLACARDS REMOVED, NO DMP, OK FOR SERVICE

Part: RADAR — INOPERATIVE (CABIN) · airframe 65,888 hrs · 22,527 cycles

INSPECTION TYPE:N/A**ATB**WX FAULT MESSAGE WX INOP REQUIRING ATBFOUND WXR ANTENNA OPERATED INTERMITTANTLY R&R WXR ANTENNA DRIVE ASSY PER AMM 34-43-05 NO FAULTS NOTED ESR IPC 34-43-03-01A-015

Part: NONE — NONE (CABIN) · airframe 64,905 hrs · 22,130 cycles

INSPECTION TYPE:NA*SUPPLEMENTAL SDR*ON LANDING WAS GOING TO PREFORM A GO-AROUND FOR LANDING LONG. RH THROTTLE WAS FROZEN & GA. DIDN'T ENGAGE. PUT A/C ON GROUND. AUTO THROTTLE SERVO TEST 10 FAILS SERVO DEF ALT THROTTLE SERVO IAW 22-30-1-1 PLACARD INSTL R/H THROTTLE TESTS CHKS GOOD & ALSO ON ENGINE RUN OK AMM 76-11-01 VERIFIED THROTTLE BYPASSES SERVO MANUAL DMP C/W.REPLACED A/T SERVO MOTOR PER AMM 22-32-01 PB401. THIS CLEARS M772265. DMP 22-30-1-1 REVERSED. PLACARD REMOVED.

Part: NONE — NONE (CABIN) · airframe 64,293 hrs · 21,908 cycles

INSPECTION TYPE:N/AEMERGENCY EXIT LIGHT INOPREMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER B767 AMM 33 51 07 201 OPS TEST OK EFF SOURCE REF B767 IPC 33 51 07 32 020J

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 64,272 hrs · 21,900 cycles

ATB, EMERG DECLARED, AC LANDED WITHOUT INCIDENT, EICAS MESSAGE TE FLAP ASYM, TRAILING EDGE LIGHT. WE DID A GO AROUND WITH FLAPS 30 DEG HIGHEST SPEED SEEN 171 KNOTS. AFTER QRH CHECK LIST LANDED FLAPS WOUND NOT RETRACT AS COMMANDEDRESET TE FLAPS OPS CK OK 3 TIMES IAW AMM 27-51-00-705-508 NO HISTORY OK FOR SERVICE.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 63,001 hrs · 21,440 cycles

INSPECTION TYPE:N/APOS 2R - 41"AFT OF POS 1 AT RBL83.0 MAIN CARGO COMPARTMENT FLOOR PANEL REPAIRMANUFACTURED NEW FLOOR PANEL IAW UPS E.O. B767-5320-9693-I ON NRC 663360

Part: SLAT SYSTEM — MALFUNCTIONED · airframe 62,567 hrs · 21,276 cycles

INSPECTION TYPE:NA**ATB - EMERG DECLARED - NO EQUIP USED- LANDED W/OUT INCIDENT - AC TAKEN OOS** ON TAKEOFF LEADING EDGE DISAGREE SLATS STUCK BETWEEN 1-0 . ON RETURN TE DISAGREE GOING FLAPS 15-20. CK LIST ALTN SYSTEM MOVED FLAPS TO 20 FOR LANDING.PERF FSEU TEST IAW AMM 27-51-00-735-080, FIM 27-28-00-815-803 FIG 103 BLOCKS 1- 11. OK TO CONTINUE OPS NORM.

Part: TRANSMITTER — FAULTED (SLAT SYSTEM) · airframe 62,340 hrs · 21,182 cycles

INSPECTION TYPE: N/A DIVERSION EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. ON DEPARTURE FROM KBFI RECEIVED LEADING EDGE SLAT DISAGREE EICAS AND LEADING EDGE LT. FLAPS WERE SET FOR 0 BUT FLAP INDICATOR STOPPED AT 1. RAN CHECK LIST. LEADING EDGE ALTN OPERATION BROUGHT NEEDLE TO BETWEEN 0 AND 1. SLATS VISUALLY VERIFIED, REF FIM 27-51-00-815-809 TEST FAULTS M548 OUTBOARD LEADING EDGE SLATS NR 2 PDU XMTR FAULT 27-81006. REMOVED & REPLACED M548 PDU XMTR, IAW AMM 27-81-11-424-029, CHECKS GOOD. FAULT & STATUS CLEARED. RAN HYD & ELECT FLAP/SLAT SYSTEM MULTIPLE TIMES. CHECKS OK IPC 27-81-10-05-256K.

Part: ANGLE — CORRODED (COCKPIT FLOOR) · airframe 61,861 hrs · 21,005 cycles

INSPECTION TYPE: LDS FURTHER INSPECTION FOUND CORRODED EDGE ANGLE AT FS 212-237, LBL 62.5. CORRODED EDGE ANGLE REPLACED WITH MADE REPAIR PART, IAW BOEING DWG 141T5188 AND INSTALLED, IAW B767-300 SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (COCKPIT FLOOR) · airframe 61,861 hrs · 21,005 cycles

INSPECTION TYPE: LDS CORROSION FOUND ON SUPPORT ANGLE AT FS 212-FS 237, LBL 64.0 FLIGHT DECK FLOOR ANGLE. ANGLE REPLACED WITH MADE REPAIR PART, REF EO B767-5310-78064-A.

Part: LANDING GEAR — MALFUNCTIONED · airframe 61,835 hrs · 20,995 cycles

INSPECTION TYPE: NA ATB NO EMERGENCY DELARED. LANDED UNEVENTFUL. GEAR WOULD NOT COME UP ON DEPT. ACCOMPANIED BY VIBRATIONS. GEAR HANDLE WENT ONLY TO OFF POSITION. JACKED ACFT, PER AMM 078-11-01-201 & AMM 32-09-02-201, PERF FIM 32--30-00-815-804. AIR TO GND SYS 1 & 2 NORMAL. A/C GEAR CYCLED 3 TIMES, NO DEFECTS NOTED. A/C OK TO CONTINUE SERVICE. ALSO WDM 32-31-11 & 32-09-11.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,548 hrs · 20,915 cycles

INSPECTION TYPE:SWOCREW REST MODULE (STC ST02568SE) - EMERGENCY EXIT LIGHTED SIGNS: PRMRPL EMERGENCYLIGHT BATTERY PACK AND PERFORMED BATTERY PACK TEST, RESULT WAS SATISFACTORY ( PRM N076UP INSTALL ON N305UP)

Part: SKIN — CORRODED (LT WING) · airframe 61,548 hrs · 20,915 cycles

INSPECTION TYPE:C13CORROSION DAMAGE ON LT WING UPPER SKIN WS 404, REAR SPAR AREA. REPAIRED IAW SRM 57-20-01-1A-1 , REV.78.00.

Part: STRUT — CORRODED (RT WING LE) · airframe 61,548 hrs · 20,915 cycles

INSPECTION TYPE:C13CORROSION DAMAGE ON STRUT OF RT WING FIXED LEADING EDGE AIR LOAD RIB INSTL AT OSS 456.975. REPAIRED IAW SRID 4-4861175324, AND EO B767-5720-77608-A.

Part: GENERATOR — INOPERATIVE (APU) · airframe 61,447 hrs · 20,877 cycles

INSPECTION TYPE:N/A**ATB**- **EMERGENCY DECLARED**AFTER TAKEOFF WE LOST L&R UTILITY BUSSES. SHORTLY THERE AFTER, THE "APU GEN OFF" EICAS MESSAGE ILLUMINATED. WE DECLARED AN EMERG AS WE WERE DOWN TO 1 ELECTRICAL SOURCE. RETURNED TO DSMT/S APU GENERATOR SYS. PER FIM TASK 24-20-00-815-801 & 24-20-00-810-805. TRACED TO APU GCU. R&R'D APU GCU IAW AMM 24-22-02. RAN & OPS CK'D GOOD.

Part: SKIN — DELAMINATED (FAN COWL) · airframe 61,025 hrs · 20,708 cycles

INSPECTION TYPE:ETOPDELAMINATION ON #2 ENG R/H FAN COWL AT 2 O'CLOCK POSITION. DELAM APPROX 3" LONG BY 2" WIDE RUNNING PARALLEL TO THE ENGINE AXIS. PEELED UP AND THICKNESS 1/64". C/W WITH E.O. B767-7110-76630-A AND ITEM PLACED ON DEFERRAL WITH INSPECTION DUE IN 30 DAYS.

Part: SKIN — DENTED (CARGO DOOR) · airframe 60,049 hrs · 20,364 cycles

FWD EDGE OF DOOR SKIN DENTED ABOVE #4 DOOR BEAM. 2.6" X 2.8" X .026. APPLIED A DOUBLER REPAIR IAW EO B767-5230-74126.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 59,675 hrs · 20,205 cycles

INSPECTION TYPE:N/A**SUPPLEMENTAL SDR** RIGHT WING NUMBER 11 SLAT TRAILING EDGE WEDGE UPPERSKIN OUTBOARD EDGE CRACK DAMAGE. REPAIRED IAW EO B767-57-50-74-3038-BREMOVED R/H WING #11 SLAT THROUGH STEP E(21). C/W REMAINING STEPS OF REMOVAL. GVI OF AIRFRAME AND HARDWARE, OK TO INSTALL. REINSTALLED #11 SLAT. OPS CHECK GOOD.

Part: CONTROL MODULE — FAULTY (HORIZ STAB) · airframe 58,331 hrs · 19,705 cycles

INSPECTION TYPE:NA**ATB** VIBRATION UNDER BOTH PILOTS FEET, ACCOMPANIED BY A HUMMING SOUND EVERY TIME CONTROL WHEEL TRIM SWITCHES WERE ACTIVATED IN FLIGHT IN EITHER DIRECTION. ISSUE WAS NOT PRESENT DURING AUTOPILOT TRIM OPERATIONS. COULD FEEL VIBRATION IN BOTH CONTR. PERFORMED VISUAL AND AUDIO INSPECTION OF VERTICAL STAB COMPONENTS IN JACKSCREW COMPARTMENT WHILE EXCERCISING VERT STAB SWITCHES NORMAL & ALTERNATE. NO VIBRATION OR UNUSUAL NOISES FOUND. RT (NEXT WORD ILLEGIBLE-LOOKS LIKE "SAM") SHOWED STCM FAULT BALL. R&R'D RT STCM PER MM 27-41-05-024 & 27-41-05-424.

Part: ADC — MALFUNCTIONED (RIGHT) · airframe 58,151 hrs · 19,622 cycles

DIVERSION - AT FL 300 IAS DISAGREE EICAS MSG L A/S 308 RT A/S 927 AND DECREASING STANBY A/S AT 240 RUDDER RATIO AILERON LOCKOUT EICAS MESSAGES FOLLOWED STALL WARNING ACTIVATION 5 OR 6 TIMES A FEW MINUTES LATER L/R EEC MODE EICAS MESSAGESPERFORMED PITOT STATIC LEAK CHECK IAW 34-11-00 NO FAUILTS FOUND INSPECTED PITOT DRAINS ALL ARE CLEAR REPLACED RH ADC IAW 34-12-01 OPS CHECK GOOD A/C OK FOR SERVICE ESR: 34-12-01-01A

Part: BLEED AIR SYS — MALFUNCTIONED (APU) · airframe 58,032 hrs · 19,588 cycles

INSPECTION TYPE:ETOP AFTER LDG, STARTED APU NO BLEED PRESSURE. DEFERRED PER MEL 49-11-1-1, DMP 49-11-1-1 C/W. **ETOPS FILED OPEN**

Part: STAY — MISSING (L1 DOOR) · airframe 57,422 hrs · 19,379 cycles

WALL CONTAINING FLIGHT DECK DOOR MADE SEVERAL LOUD KNOCKS DURING CLIMB AS PRESSURIZATION INCREASED. DID NOT OCCUR DURING DECENT AS PRESURIZATION DECREASED. FOUND MISSING CATCH ON PRESURE RELIEF DOOR AT THE RIGID BARRIER SECTION 41. INSTALLED THE STAY IAW DRAWING 141T0619, DOOR FUNCTION RESTORED.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 57,093 hrs · 19,244 cycles

CORROSION FOUND ON THE ANGLE ON THE AFT CARGO FLOOR STRUCTURE NEAR BS 1339. INSTALL A NEW PART IAW SRM 51-40-02-0G, REV 72, AND EO B767-5310-69701-A.

Part: CHANNEL — CORRODED (RT WING) · airframe 57,093 hrs · 19,244 cycles

CORROSION FOUND ON THE CHANNEL OF THE RT WING INBD T/E CAVITY, AFT HYD TUBE SUPPORT AT WBL 139. INSTALL A NEW PART IAW SRM 51-40-02-0G, REV 72.

Part: STIFFENER — CRACKED (BS 785.9) · airframe 57,093 hrs · 19,244 cycles

A CRACK WAS FOUND ON THE FRONT SPAR STIFFENER, UPPER SIDE AT BS 785.9, RBL 11. REPAIR IAW SRM 57-10-10-2R-2, REPAIR 2, REV 72, AND EO B767-5740-58151-A.

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 57,093 hrs · 19,244 cycles

DAMAGE WAS FOUND ON THE M/D CARGO FLOOR PANEL 241WFF BETWEEN BS 972 & 1112, LBL 11 - RBL 11, FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.

Part: STIFFENER — CRACKED (BS 785.9) · airframe 57,093 hrs · 19,244 cycles

A CRACK WAS ON THE FRONT SPAR STIFFENER, UPPER SIDE AT BS 785.9, LBL 11. REPAIRED IAW SRM 57-10-10-2R-2, REPAIR 2, REV 72, AND EO B767-5740-58151-A.

Part: STIFFENER — CRACKED (BS 785.9) · airframe 57,093 hrs · 19,244 cycles

A CRACK FOUND ON THE FRONT SPAR STIFFENER, UPPER SIDE AT BS 785.9, RBL 33. REPAIRED IAW SRM 57-10-10-2R2, REPAIR 2, REV 72, AND EO B767-5740-58151-A.

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 57,093 hrs · 19,244 cycles

DAMAGE WAS FOUND ON THE M/D CARGO FLOOR PANEL 231GFFF BETWEEN BS 533 - 654 PLUS 22 INCHES, FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.

Part: PAWL — WORN (L1 DOOR) · airframe 55,447 hrs · 18,607 cycles

CREW ENTRANCE DOOR EXT HANDLE U BRACKET WORN MARKED REQ 211953A. REMOVED AND REPLACE CREW EXTRACT DOOR EXT HANDLE PAWL REF MM 20-11-00 EFF 52-12-25-02.

Part: HOUR METER — INOPERATIVE (APU) · airframe 55,215 hrs · 18,528 cycles

PU HOUR METER INOPERATIVE. REPLACED THE HOUR METER IAW AMM 49-72-01-404-030.

Part: WEDGE — DENTED (RT WING TE FLAP) · airframe 55,022 hrs · 18,463 cycles

RT WING INBD AFT FLAP T/E WEDGE LOWER SKIN DENTED. REPAIRED THE FLAP IAW B767-5750-64932-B

Part: DOOR SEAL — OBSTRUCTED (PAX DOOR) · airframe 54,909 hrs · 18,425 cycles

CREW ENTRY DOOR HAS AIR LEAK NOISE DURING CLIMB, UNTIL REACHING 18,000 FT. NOISE FROM LOWER LEFT CORNER OF DOOR. FOUND DEBRIS ON CREW ENTRY DOOR SEAL (LOWER AFT) REMOVED DEBRIS, SEAL GOOD OK FOR FLT

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,786 hrs · 18,379 cycles

COCKPIT LEFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS AND OPS CHECKED NORMAL IAW MM 33-51-00-715-227.

Part: VALVE — INOPERATIVE (EQUIPEMENT COOL) · airframe 54,668 hrs · 18,337 cycles

FWD EQUIPMENT VALVE EICAS DISPLAYED PLUS OR MINUS FOUR SECONDS IN CLIMB. REOCCURRED AT 34,000 CRUISE, EQUIPMENT COOLING SELECTOR TO STANBY IAW QRH. WARNING EXTINGUISHED. DURING TROUBLSHOOTING PERFORMED MANIFOLD INTERCONNECT VALVE TEST. STEP 2 H FAILED AFTER 45 SECONDS. MM 21-58-00-705-342-001-1.SUSPECTED K2193 RECHECKED SYSTEM, OK IAW 21-58-00-705-342-001.1 (F) SIMULATION OF ALTITUDE ABOVE 10,000 FT.

Part: TEE FITTING — CORRODED (FUSELAGE) · airframe 52,387 hrs · 17,563 cycles

INSPECTION TYPE: C11, CORROSION DAMAGE ON KEELBEAM SUPPORT STRUT SPLICE TEE AT STA 965. REPLACEMENT OF SPLICE TEE.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 52,387 hrs · 17,563 cycles

INSPECTION TYPE:C11, WORN DAMAGE WAS FOUND ON THE M/D SEAT TRACK AT STA 1197 66, RBL 77. REPAIR IAW SRM 53-00-52-2R-9, REPAIR 9, REV 66 AND EO B767-5310-61625-A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 52,387 hrs · 17,563 cycles

INSPECTION TYPE: C11, CRACK WAS FOUND ON THE STR 20R AT STA 1550. REPAIR IAW SRM 53-00-03-2R-5, REPAIR 5, REV 66.

Part: SKIN — DELAMINATED (RT NACELLE) · airframe 51,841 hrs · 17,356 cycles

RIGHT ENGINE COWL INBD SIDE LARGE ARE DELAMINATED 2 FOOT X 4 FOOT. DEFERRED CHIPPING AND MISSING PAINT ON NR 2 ENGINE INBD FAN COWL NO DELAMINATION FOUND IAW AMM 51-21-10-07. R & R RT ENG INBD FAN COWL IAW AMM 71-11-04/401.

Part: FLOOR SUPPORT — CRACKED (BS 1417-1500) · airframe 51,706 hrs · 17,309 cycles

AFT CARGO FLOOR SUPPORT AT BS 1417-1540, RBL 15.5 IS CRACKED. REPAIRED.

Part: FLOOR SUPPORT — CRACKED (BS 1417-1540) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE:PS1. AFT CARGO FLOOR SUPPORT BS 1417-1540, LBL 15.5 CRACKED. REPAIRED.

Part: FLOOR SUPPORT — CRACKED (BS 1417-1540) · airframe 51,706 hrs · 17,309 cycles

AFT CARGO FLOOR SUPPORT CRACKED. REPAIRED.

Part: DOUBLER — DAMAGED (BS 1417) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE:PS1, EXISTING REPAIR AT BS 1417 BETWEEN STR 35L AND 36L WILL INTERFERE WITH NEW SKIN INSTALLATION. REMOVED FASTENERS IAW EA 767-5361-27-A2211, STEP 4 PERFORMED ROTO PROBE INSPECTION IAW NTM 51-00-01. NO NOTED CRACK INDICATIONS NOTED, FABRICATED REPAIR PARTS IAW EA 767-5361-27-A2211, DRAFT 2, STEP 7, INSTALLED REPAIR PARTS IAW EA 767-5361-27-A2211, DRAFT 2.

Part: STRINGER — BENT (BS 1395-1582) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE:PS1, S39L, BS 1395 TO BS 1582 DAMAGED DURING TAIL STRIKE, ACFT WAS FERRIED. R & R STRINGER, PN 146T3003-201.

Part: STRINGER — BENT (BS 1307-1502) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE:PS1, R & R STR 38R BETWEEN BS 1307 TO 1502 DUE TO TAIL STRIKE. R & R STR EA 767-0700-27-A2001.

Part: STRINGER — BENT (BS 1307-1582) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE:PS1, R & R STR 39R BETWEEN BS 1307 TO 1582 DUE TO TAIL STRIKE. R & R STRINGER IAW EA 767-0700-27-A2201.

Part: STRINGER — DAMAGED (BS 1307-1595) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE:PS1,STRINGER AT 38L BETWEEN BS 1307 TO 1595 DAMAGED. R & R STRINGER AT 38L BETWEEN BS 1307 TO BS 1595 IAW SRM 51-40-02-05.

Part: STRINGER — BENT (BS 1395-1582) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE: STRINGER BS 1395 - 1582 DAMAGED DURING TAIL STRIKE. R & R STRINGER.

Part: FRAME — DAMAGED (BS 1480) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE:PS1, FRAME AT BS 1480 DAMAGED. FABRICATE NEW FRAME WEB OMITTING CHEM-MILLED POCKETS IAW E.O B767-5310-60316-A.

Part: FRAME — DAMAGED (BS 1502) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE:PS1, FRAME AT BS 1502, S38L- S38R DAMAGED. FABRICATED NEW FRAME WEB OMITTING CHEM-MILLED POCKETS IAW EO B767-5310-60317-A.

Part: FRAME — DAMAGED (BS 1461) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE:PS1, FRAME BS 1461.0. S38L-S38R DAMAGED. FABRICATED FRAME WEB WITHOUT CHEM-MILLED POCKETS IAW EO B767-5310-60315-A.

Part: FRAME — DAMAGED (BS 1518) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE:PS1, FRAME BS 1518.0 S38L-S38R DAMAGED. FABRICATED A NEW FRAME WEB OMITTING CHEM MILLED POCKETS IAW EO 767-5310-60318-A.

Part: SKIN — DAMAGED (BS 1307-1582) · airframe 51,706 hrs · 17,309 cycles

INSPECTION TYPE:PS1, SKIN SECTION BS 1307-1582 STR 37L-37R DAMAGED. R & R SKIN.

Part: SKID — DAMAGED (TAIL) · airframe 51,691 hrs · 17,304 cycles

DURING GEAR RETRACTION, TAILSKID LIGHT ILLUMINATED, TAILSKID EICAS MSG ILLUMINATED, TAILSKID LIGHT & EICAS EXTINGUISHED UPON GEAR EXTENSION. EVALUATING DAMAGE. R & R TAILSKID ASSY AND OPS CK OF INDICATION IAW AMM 32-71-06-402-001.

Part: RELAY — MALFUNCTIONED · airframe 51,403 hrs · 17,218 cycles

INSPECTION TYPE: E, TOP CONDUCTED AUTOLAND WITH APU NOT OPERATING. SHORTLY AFTER TOUCHDOWN THERE WERE NUMEROUS WARNING AND CAUTION MESSAGES. WHEEL WELL FIRE LT YAW DAMP, SPEED BRAKE AND SEVERAL OTHERS. UPON DISCONNECTING AUTOPILOT, ALL MESSAGES CLEARED. C/O T/S PERF BPCU BITE TEST IAW AMM 24-11-00-745-001. NO FAULTS. PERFORMED AUTOFLIGHT BITE TEST IAW AMM 22-00-02. C/O 30/40 TEST, ALL TEST PASSED. IAW TECH SUPPORT R & R THE MAIN BATTERY TRANSFER RELAY K106, MAIN BATTERY RELAY K104 AND STATIC INVERTER. R & R RELAY K106 IAW AMM 24-33-02-401.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,324 hrs · 17,196 cycles

EXTERIOR EMEGENCY LIGHT INOPERATIVE R & R BULB IAW MM 33-51-16-962-001. NO HELP FOUND BAD FROM STOCK BULB. R & R BULB IAW MM 33-51-16-962-001, OPS CK GOOD.

Part: STRUT — BROKEN (LIFE RAFT DOOR) · airframe 50,250 hrs · 16,805 cycles

LIFE RAFT GAS STRUT IS BROKEN. R & R LIFE RAFT DOOR GAS STRUT IAW MM INTRO 2B.

Part: NONE — NONE (NONE) · airframe 49,484 hrs · 16,532 cycles

CAPT EVAS WAS REMOVED FROM CONTAINER. WAS NOT DEPLOYED. R & R CAPT EVAS IAW AMM 25-69-00-401. PN OFF-ON: 107STC-267, SN OFF: 0009X06P, SN ON: 0008X09P. EFF REF IPC 25-60-00-90, ITEM 001.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 49,484 hrs · 16,532 cycles

HAD STRONG ACID SMELL WHEN JUMPSEATER TURNED ON 1ST OBSERVER'S OVERHEAD MAP LIGHT. LIGHT FLICKERED AND HAD STRONG, BURNING ODOR. SECURED AND SMELL WENT AWAY. R & R 1ST OBSERVERS OVERHEAD MAP LIGHT IAW AMM 33-14-00-401. EFF SOURCE, REF IPC 33-14-51-02A, ITEM 005.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

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

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

FLOOR PANEL CRACKED, VERY WEAK. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H & EO B767-5320-5385 4-B.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

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

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

HOLE IN MAIN CARGO DECK FLOOR PANEL. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

HOLE IN MAIN CARGO DECK FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

HOLE IN MAIN CARGO DECK FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

HOLE IN MAIN CARGO DECK FLOOR PANEL. FABRICATED NEW FLOOR PANEL IAW EO-B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

HOLE IN MAIN CARGO FLOOR PANEL, REPAIRED IAW SRM 53-00-50-2R.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 44,181 hrs · 14,499 cycles

INSPECTION TYPE:9C LT WING OTBD FLAP INBD L/E FAIRING DELAMINATED AT 55.5" FROM INBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PARA 5A(1), FIG 5, REV 52.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 44,181 hrs · 14,499 cycles

INSPECTION TYPE:9C, LT WING OTBD FLAP MID L/E FAIRING DELAMINATED AT 119.5" FROM INBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PARA 5A(1), FIG 5, REV 52.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 44,181 hrs · 14,499 cycles

INSPECTION TYPE:9C, RT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1), FIG 5, REV 52.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 44,181 hrs · 14,499 cycles

INSPECTION TYPE:9C, LT WING OTBD FLAP INBD L/E FAIRING DELAMINATED 28.5" FROM INBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PARA 5A (1) FIG. 5, REV 52.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 44,181 hrs · 14,499 cycles

INSPECTION TYPE: 9C, LT WING OTBD T/E FLAP MID L/E FAIRING DELAMINATED AT 119.5" FROM INBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM51-70-05, PARA 5A(1), FIG 5, REV 52.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 44,181 hrs · 14,499 cycles

INSPECTION TYPE: 9C, NR 2 PYLON LT STRUT SKIN CRACKED APPROX 1.5" LONG AT ACCESS PANEL NR 442AL CUTOUT. REPAIRED IAW HX RS R-54-51-37402 REV A & EO B767-5430-48154-A JUST AT ACCESS PANEL NR 442AL CUTOUT AFT UPR CORNER AREA, SKIN & DOUBLER ORIG MATL ARE CLAD 2024T3-0080",CRK LENGTH 1.5",A 0.1875" DIA STOP HOLE DRILLED, CLASSIFIED AS A MAJOR REPAIR WITH MATL AMS4911-0090IN AS REPAIR DOUBLER & AISI-301-0016INHH AS A NEW REPAIR RUBSTRIP, SIZE 12" X 10".

Part: WEDGE — DELAMINATED (RT WING TE FLAP) · airframe 44,181 hrs · 14,499 cycles

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

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 44,181 hrs · 14,499 cycles

INSPECTION TYPE: 9C, LT WING OTBD FLAP MID L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PARA 5A(1), FIG 5, REV 52.

Part: SKIN — CRACKED · airframe 44,181 hrs · 14,499 cycles

INSPECTION TYPE: 9C, EMP STA-1725, STR-7R SKIN FOUND CRACKED. REPAIRED IAW SRM 53-80-01-2R-5 REPAIR 5 FIG 201, REV 53 AT BS 1725.5, STR-7R AREA, SKIN CRACK LENGTH 2.2", CHORD STRAP CRACK LENGTH 0.25", FINAL CUTOUT SIZE 3" X 4.25" & CHORD STRAP 1" X 1". CLASSIFIED AS A MAJOR REPAIR REPAIR SIZE: 12"X11", THIS IS A CATEGORY B REPAIR, REPEAT INSP IS REQUIRED IAW SRM 53-80-01-2R5, REPAIR 5, FIG 201, TABLE III, REV 53.

Part: STIFFENER — CRACKED (NLW WW BULKHEAD) · airframe 44,181 hrs · 14,499 cycles

INSPECTION TYPE:9C, FUSELAGE RT STA 287, BL 25 NLG WW AFT BULKHEAD VERTICAL CHORD CRACK FOUND AT WL 173 APPROX .5" IN LENGTH. REPAIRED IAW SRM 51-70-12-0G, FIG 1, REV 52 JUST BTW WL 164 & WL 182, ORIG MATL: AND10140-4005-7075T6511, CRACK LENGTH: 0.75", FINAL CUTOUT SIZE: 1.1"X2.1",CLASSIFIED AS A MAJOR REPAIR, REPAIR SIZE: 17.75"X3", SUPPLEMENTAL DAMAGE TOLERANCE INSP ARE REQUIRED FOR THE REPAIRED CHORD IAW EO B767-5310-20118-F, APPX 'C'.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 44,181 hrs · 14,499 cycles

INSPECTION TYPE: 9C, LT WING OTBD FLAP INBD L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1), FIG 5, REV 52.

Part: FLOORBOARD — PUNCTURED (BS 540-654) · airframe 44,181 hrs · 14,499 cycles

INSPECTION TYPE:9C, MAIN CARGO 4L, BS 540-654+22, L33 TO L55, HAS PUNCTURED FLOORBOARD. FLOORBOARD FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.

Part: CONTROL PANEL — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS DO NOT COME ON WHEN SWITCH PLACED TO ON POSITION. TROUBLESHOT IAW FIM 33-51-00, FIG 103, SHEET 1. SWITCH BAD E031979. R & R EMERGENCY LIGHTS CONTROL PANEL IAW MM 33-51-08. OPS CHECK GOOD.

Part: SKIN — DAMAGED (BS 955) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD SIDE FITTING FAILSAFE STRAP SKIN ATTACH AREA DAMAGE FOUND AFT FAILSAFE STRAP CUTOFF. DAMAGE SMOOTHED OUT & REPROTECTED IAW R53-50-36849 & EO B767-5330-40064. BLEND OUT AREA A 0.75" X 2.75" X 0.025", AREA B 2" X 2.5" X 0.095" ORG THICKNESS 0.400". THIS REPAIR IS CLASSIFIED AS MINOR REPAIR. TIME LIMITED TO 15948 TOTAL FLIGHT CYCLES

Part: ATTACH FITTING — CRACKED (BS 955) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD ATTACH FITTING FOUND 1EA FASTENER HOLE CRACKED APPROX 0.020" RUNNING DOWN. AND FOUND 2 EA FASTENER HOLES SHORT EDGE MARGIN ARE 1.33" AND 1.664". ATTACH FITTING REPLACED IAW EO B767-5350-17922G APP C & REPAIRED IAW HX RS R53-50-36850, REV A & EO B767-5310-40095A. DUE 2 EA FASTENER HOLES SHORT EDGE MARGIN, IT IS CLASSIFIED A MAJOR REPAIR , REPAIR SIZE 5.25" X 5.25".

Part: FLOOR PANEL — DENTED (BS 540-654) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:8C, M/D STA 540 TO 654+22, RBL 11" TO LBL 11" FLR PNL FND 8 DENTS & 4 DAMAGE. FLOOR PANLE FABRICATE IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53 53-01-01.

Part: FLOOR PANEL — DENTED (BS 933-970) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:8C, M/D STA 933 TO 970, LBL 11 TO RBL 11 FLR PNL FND 12 DENT MARKS & UPPER SURFACE FIBERGLASS DELAMINATED (1" WIDTH & 37" LONG). FLR PNL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, LT WING OTBD FLAP LWR SURFACE INBD AFT PANEL INBD AREA FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 3, REV 48.

Part: WEDGE — PUNCTURED (RT WING TE FLAP) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, RT WING OTBD FLAP T/E WEDGE UPPER SURFACE PUNCTURE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 9, REV 48.

Part: FITTING — CRACKED (BS 955) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 7 O/C POSITION AT TEE FITTING APPROX .2500" IN LENGTH AND FOUND 1 EA FASTENER HOLE SHORT EDGE MARGIN IS 0.66". TEE FITTING REPLACED IAW EO B767-5350-17922G APP. D & REPAIRED IAW HX RS R53-50-36851 REV A & EO B767-5310-40062A DUE 1EA FASTENER HOLE SHORT EDGE MARGIN. IT IS CLASSIFIED A MAJOR REPAIR, REPAIR SIZE IS 5.25" X 5.25".

Part: FAILSAFE — CRACKED (BS 955) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 2 O/C POSITION AT FAIL SAFE STRAP APPROX .1250" IN LENGTH. FUSELAGE BS955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-G, APPENDIX C AT LT SIDE.

Part: WEDGE — PUNCTURED (RT WING TE FLAP) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, RT WING OTBD FLAP UPPER SURFACE T/E WEDGE PUNCH HOLE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1) FIG 9, REV 48.

Part: STIFFENER — CRACKED (BS 977) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, LT MLG W/W CANTED PRESSURE DECK AT BS 977 LATERAL "Z" STIFFENER FOUND CRACKED AT FASTENER HOLE AREA BETWEEN LBL 20 AND LBL 55. CRACK LENGTH ARE 1.625" AT LBL 32.94 AND 1.6" AT LBL 54.69. STIFFENER REPAIRED IAW HX RS NR R53-58-36842 REV A & EO B747-5330- 40061A JUST AT LBL 32.94 & LBL 54.69, FINAL CUTOUT SIZE 1.95" X 0.9" AT LBL32.94 & 1.9"X0.9" AT LBL54.69, THIS IS CLASSIFIED A MAJOR REPAIR, REPAIR SIZE ARE 9.375"X2.375" AT LBL 32.94 & 13" X 2.375" AT LBL 54.69

Part: FITTING — CRACKED (BS 955) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 4 O/C AND 10 O/C POSITION AT FAIL SAFE STRAP THROUGH THICKNESS & APPROX .12" IN LENGTH. FUSELAGE BS955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-G, APPENDIX D AT RTS.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG 5, REV 48.

Part: INTERCOSTAL — CRACKED (BS 1043) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, M/DECK STA 1043 LBL 11 TO RBL 11 INTERCOSTAL FOUND CRACKED. MAIN DECK STA 1043 LBL 11 TO RBL 11 FLOOR INTERCOSTAL REPLACED AFTER FABRICATED IAW HX RS R53-00-36841 AND EO B767-5320-40037, ORG MATL BAC1518-790-7075T6511. FABRICATE NEW INTERCOSTAL WITH MATL 7075T6511-2500INX6000IN BAR AS NEW REPLACEMENT.

Part: SKIN — CHAFED (NR 9 SLAT) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, RT WING NR9 SLAT UPPER WEDGE OTBD OF 30" FOUND DEEP CHAFING ON LWR SURFACE. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R. REPAIR 4, FIG 202, SHEET 8, REV 48.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, LT WING OTBD T/E FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-71-05, PAR 5A(1) FIG 5, REV 48.

Part: STIFFENER — CRACKED (STA 785.9) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, FWD CARGO COMPT WING CTR TANK FRONT SPAR ATT VERT STIFFENER FOUND CRACK AT STA785.9, LBL32.94. THIS REPAIR WITHIN 22" OF ANOTHER REPAIR AT LBL54.69" NRC EUW500292. FWD CGO COMPT WING CTR TANK FRONT SPAR STA785.9, LBL32.94 VERT STIFFENER REPAIRED IAW RS R57-00-368837 & EO B767-5710-39975, ORG MATL BAC1518-749-2024T3511, CRK LENGTH 3.5", CUTOFF LENGTH 16.5", THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATL BAC1518-749-2024T3511 AS REPLACEMENT SECTION, TOTAL REPAIR LENGTH IS 22.5"

Part: STIFFENER — CRACKED (STA 785.9) · airframe 39,376 hrs · 12,948 cycles

INSPECTION TYPE:C, FWD CARGO COMPT WING CTR TANK FRONT SPAR ATT VERT STIFFNER FOUND CRACK AT STA785.9 LBL54.69 THIS REPAIR IS DAMAGE WITHIN 22" OF ANOTHER REPAIR AT LBL32.94, NRC EUW500284. FWD CGO COMPT WING CTR TANK FRONT SPAR AT STA785.9, LBL54.69 VERT STIFFENER REPAIRED IAW RS R57-00-36838 & EO B767-5710-39976, ORG MATL BAC1518-749-2024T3511, CRK LENGTH 1", CUTOFF LENGTH 16.5" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR WITH MATL BAC1518-749-2024T3511 AS REPLACEMENT SECTION. TOTAL REPAIR LENGTH IS 22.5"

Part: PRESSURE SWITCH — INTERMITTENT (HYD SYSTEM)

INSPECTION TYPE:E, TOP CTR HYD LOW SYS PRESSURE LIGHT ILLUMINATED ATB. REPLACED CTR HYDR SYS LOW PRESSURE SWITCH.

Part: FLOOR PANEL — DAMAGED (CARGO DECK)

MAIN CARGO DECK FLOOR PANEL POSITION 2 RT HAS DAMAGE. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-50-2R.

Part: WINDOW — OUT OF ADJUST (COCKPIT)

F/O SLIDING WINDOW HANDLE REQUIRES EXCESSIVE FORCE TO OPERATE. ADJUSTED F/O SLIDING WINDOW IAW 56-11-02-5. OPS NORMAL. NOTE: WINDOW HEAT TERMINAL WAS NOT DISTURBED.

Part: BRACKET — INOPERATIVE (SLIDING WINDOW)

F/O WINDOW BRACKET BROKEN WHEN WINDOW WAS CLOSED. R & R F/O'S SLIDING WINDOW BEWTWEEN BRACKET IAW AMM 56-11-04-4. ALL SATISFACTORY.

Part: CRANK ASSY — BINDING (L2 WINDOW)

L2 WINDOW CRANK BINDING TOWARD CLOSE. ADJUSTED THE L2 WINDOW IAW MM 56-11-02-5. OPS GOOD.

Part: CONTROL CABLE — ICED

ON ARRIVAL, CREW REPORTED STAB TRIM NO MOVEMENT IN NORM OR ALT MODES. ON INVESTIGATION STAB BAY FOUND TO HAVE ICE FORMATION APPROX 10 INCHES DEEP IN BILGE AREA. ICE FORMATION HAD PREVENTED POSITION MODULES AND FOLLOW UP CABLES FROM MOVING. THIS RESULTED IN CABLES BECOMING BROKEN AND KINKED.

Part: SKIN PANEL — MISREPAIRED (HORIZ STAB) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.

Part: SKIN PANEL — MISREPAIRED (HORIZ STAB) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.

Part: SKIN PANEL — MISREPAIRED (HORIZ STAB) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL SURVEY SEQ 305-S1-12 TO 16 EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.

Part: SKIN PANEL — MISREPAIRED (HORIZ STAB) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C EMP - LT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH NON STANDARD REPAIR. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 203.

Part: SKIN PANEL — DEBONDED (RT HORIZ STAB) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C EMP - RT HORIZONTAL STAB UPPER L/E FIXED PANEL EXISTING REPAIR PATCH DISBOND. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 2 FIG 201.

Part: SKIN — MISREPAIRED (SPOILER) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C RT WING NR 12 SPOILER UPPER SURFACE 1EA EXISTING REPAIR PATCH NON STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A FIG 10.

Part: SKIN — MISREPAIRED (SPOILER) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C RT WING NR 12 SPOILER UPPER SURFACE 1EA EXISTING REPAIR PATCH NON STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A FIG 10.

Part: SKIN — MISREPAIRED (SPOILER) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C RT WING NR 10 SPOILER T/E UPPER SURFACE EXISTING REPAIR PATCH NON STANDARD REPAIR. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A (1) FIG 10.

Part: SKIN — MISREPAIRED (NR 12 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C RT WING NR 12 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-53, -54. REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511228-1.

Part: SKIN — MISREPAIRED (NR 10 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C RT WING NR 10 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-38, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511178-1.

Part: SKIN — MISREPAIRED (NR 4 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C LT WING NR 4 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W3-31, -32, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511244-1.

Part: SKIN — MISREPAIRED (NR 4 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C LT WING NR 4 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W3-34, -35, LT WING NR 4 SLAT T/E WEDGE UPPER SKIN REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511251-1.

Part: SKIN — MISREPAIRED (NR 8 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR REF SURVEY SEQ NR 305-W4-18, -19, RT WING NR 8 SLAT T/E WEDGE UPPER SKIN REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511137-1.

Part: SKIN — MISREPAIRED (NR 12 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C RT WING NR 12 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-51,52 RHW NR12 SLAT T/E WEDGE UPPER SKIN REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511186-1.

Part: SKIN — MISREPAIRED (NR 8 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-16, -17. REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511129-1.

Part: SKIN — MISREPAIRED (NR 8 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-20,21. RT WING NR 8 SLAT T/E WEDGE UPPER SKIN REPAIRED IAW SRM 51-70-10 AND COMPONENT WORK PROCESS CARD NR BTF 511152-1.

Part: SKIN — MISREPAIRED (NR 12 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C RT WING NR 12 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-55, -56, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511194-1.

Part: SKIN — MISREPAIRED (NR 9 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C RT WING NR 9 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR REF SURVEY SEQ NR 305-W4-30, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511210-1.

Part: SKIN — MISREPAIRED (NR 4 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C LT WING NR 4 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ. 305-W3-26, LT WING NR 4 SLAT T/E WEDGE UPPER SKIN REPAIRED IAW SRM 51-70-10 AND COMPONENT WORK PROCESS CARD NR BTF511236-1.

Part: SKIN — MISREPAIRED (NR 7 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C RT WING NR 7 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-5, -6, -7, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511160-1.

Part: SKIN — MISREPAIRED (NR 8 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-23, -24, REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511145-1.

Part: SKIN — MISREPAIRED (NR 8 SLAT) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C RT WING NR 8 SLAT T/E WEDGE UPPER SKIN EXISTING DOUBLER FOUND NON STANDARD REPAIR. REF SURVEY SEQ NR 305-W4-13, 14. REPAIRED IAW SRM 51-70-10 AND HX COMPONENT WORK PROCESS CARD NR BTF511202-1.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C FX- BS 132.5-145.6 STR 38R - 39R AREA SKIN REPAIR ISN'T APPLICABLE TO THE AREA WITHIN 22 INCHES OF A DOOR CUTOUT AS PER SRM 53-00-01 2R 14 FIG 201 REF TO SURVEY SEQ 305-F1-01. THE SURVEY SEQ 305-F1-01 FUSELAGE BS 132.5 - 145.6 STR 38R- 39R AREA SKIN REPAIRED AS PER HX RS R53-11-36255 AND UPS EO B767-5330-31919-A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C SURVEY SEQ 305-F1-07 FUSELAGE BS 654+22 TO 654+44 STR 23R-25R SKIN REPAIR CAN'T DETERMINE THE REPAIR CONFIGURATION AS PER SRM DUE TO NO CUTOUT FOUND REFER SRM. SURVEY SEQ 305-F1-07 FUSELAGE BS 654+22 TO BS 654+44 BETWEEN STR 23R-25R SKIN REPAIRED AS PER SRM 53-00-01-2R1 FIG 201 UPS MPI P20224 ISSUED FOR SUBSEQUENT INSP AS PER SRM 53-00-01-2R1 FIG 201 SHT 9 TABLE V.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C THE REPAIR CONFIGURATION IS NOT FULFILLED WITH THE SRM AT THE AREA BS 1310.5-1329 STR 27R-28R AREA REF SURVEY SEQ 305-F1-08. THE SURVEY SEQ 305-F1-08 FUSELAGE BS 1310.5 - 1329 STR 27R - 28R AREA DOOR SKIN REPAIRED AS PER HX RS R52-34-36254 AND UPS EO B767-5231-31912-A.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C LT WING O/B FLAP L/E MID FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5.

Part: SKIN PANEL — DELAMINATED (TE FLAP) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C LT WING I/B MAIN FLAP AFT UPPER FIXED PANEL UPPER SURFACE DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAPA 5A (1) FIG 5.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C FX- BS 164-172 STR 39R AREA SKIN REPAIR ISN'T APPLICABLE TO THE AREA WITHIN 22 INCHES OF A DOOR CUTOUT AS PER SRM 53-00-01 2R 14 FIG 201 REF TO SURVEY SEQ 305-F1-03. THE SURVEY SEQ 305-F1-03 FUSELAGE BS 164-172 STR 39R AREA SKIN REPAIRED AS PER HX RS R53-11-36255 AND UPS EO B767-5330-31919-A.

Part: SKIN PANEL — DELAMINATED (VERTICAL STAB) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C EMP - VERTICAL STABILIZER PANEL 322CR DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A (1) FIG 9.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C FX MEC COMPT BS 246 RBL 10 MAIN DECK FLOOR SUPPORT BEAM ATTACH STIFFENER CRACK. MEC BS 246 RBL 10 FLOOR SUPPORT BEAM ATTACH STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C AFT OF BULK CARGO STA 1580 LBL 80 MAIN DECK SEAT TRACK ATTACH ANGLE CRACK. AFT OF BULK CARGO BS 1580 LBL 80 MAIN DECK SEAT TRACK ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.

Part: SKIN PANEL — DELAMINATED (TE FLAP) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C RT WING I/B MAIN FLAP T/E UPPER SURFACE DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PARA 5A (1) FIG 5.

Part: FITTING — CRACKED (LT WING TE FLAP) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C LT WING INBD MAIN FLAP INBD AFT FLAP SUPPORT FTG UPPR AREA FLANGE FOUND CRACKED. REPAIRED IAW SRM 57-53-02-2R1 FIG 201.

Part: SKIN — DELAMINATED (NR 5 SPOILER) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C LT WING NR 5 SPOILER LOWER SURFACE DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER HX RS R57-70-36252 REV B AND UPS EO B767-5750-31918-A.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C SURVEY SEQUENCE 305-F1-05 FX BS 444-458.5 STR 23R-24R EXISTING REPAIR DOUBLER TOP SURFACE PREVIOUS BLENDING FOUND WITH SLIGHTLY DENT. SURVEY SEQUENCE 305-F1-05 FUSELAGE BS 444-458.5 BETWEEN STR 23R-24R SKIN REPAIRED WITH ZERO TIMING AS PER SRM 53-00-01-2R14 FIG 201. UPS MPI P20223 ISSUED FOR SUBSEQUENT INSP AS PER SRM 53-00-01-2R14 FIG 201 SHT 9 TABLE V.

Part: PANEL — DEBONDED (VERTICAL STAB) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C EMP VERTICAL STABILIZER RT LOWER SURFACE PREVIOUS REPAIR AREA DEBOND. METAL HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-10 REPAIR 4.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C M/D STA 363 WL 200 RBL 71 FLOOR PANEL FOUND REPAIR PATCH. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R.

Part: BRACKET — CRACKED (RT WING) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C RT WING LES 675 L/E SUPPORT AFT UPPER FRONT SPAR BRACKET FOUND CRACKED. RT WING LES 675 L/E SUPPORT AFT UPPER FRONT SPAR BRACKET REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C M/D STA 410 WL 200 RBL 83 FLOOR PANEL FOUND REPAIR PATCH. FLOOR PANEL REPAIRED AS PER SRM 53-00-50-2R.

Part: FLOORBEAM — CRACKED (BS 1087) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C, AFT CARGO COMPT BS 1087 RBL 26 INCHES BELOW FLOOR ANGLE SUPPORT FOUND CRACK. AFT CARGO COMPT BS 1087 RBL 26 INCHES BELOW FLOOR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C MEC BS246 LBL 40 FLOORBEAM FRONT FACE SUPPORT ANGLE FWD CRACK. MEC BS 246 LBL 40 FLOORBEAM FRONT FACE SUPPORT ANGLE REPAIRED AS PER SRM 53-10-51-2R4 FIG 201. REPEAT INSP IS REQUIRED AS PER SRM 53-10-51-2R4 FIG 201 SHT 2 TABLE II UPS MPI P20220 ISSUED FOR REPEAT INSP.

Part: ANGLE — CRACKED (BS 246) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C FX MEC COMPT BS 246 LBL 25 INCH FLOORBEAM FRONT FACE SUPPORT ANGLE FOUND CRACKED. REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.

Part: ANGLE — CRACKED (BS 246) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C FX MEC COMPT BS 246 LBL 50 INCH FLOORBEAM, AFT FACE ANGLE SUPPORT FWD CRACK. REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE:C FX MEC COMPT BS 246 LBL 50 FLOORBEAM AFT FACE INTERCOSTAL UPPER AREA FOUND CRACK. MEC COMPT BS 246 LBL 50 FLOORBEAM AFT FACE INTERCOSTAL UPPER AREA REPAIRED AS PER SRM 51-70-11-0G FIG 1.

Part: FLOORBEAM — CRACKED (BS 1087) · airframe 34,576 hrs · 11,493 cycles

INSPECTION TYPE: C AFT CARGO COMPT BS 1087 LBL 26 INBD BELOW FLOOR ANGLE SUPPORT FOUND CRACKED. AFT CARGO COMPT BS 1087 LBL 26 INCH BELOW FLOOR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02.

Part: PANEL — DAMAGED (L1 DOOR)

L1 DOOR SIDE BUMPER AND SIDE PANEL DAMAGED. REMOVED INTERIOR PANEL FOR CREW ENTRY DOOR HANDLE AND SENT TO SM. REPAIRED SIDEWALL PANEL REF 767 AMM 25 00 00 08.

Part: SIGN — UNKNOWN (CABIN)

EMERGENCY LIGHT ASSY REMOVED FROM CREW ENTRY DOOR HANDLE PANEL. REINSTALLED EMERGENCY EXIT SIGN AND OPS CHECK NORMAL.

Part: CAP — CRACKED (T/E FLAP)

INSPECTION TYPE:N/A RIGHT WING O/B FLAP LEADING EDGE CAP CRACKED.

Part: LIGHT — BROKEN (FWD ENTRY DOOR)

FWD ENTRY DOOR INTERIOR EMERGENCY LIGHT INOP. [SUP 5-16-07] MOUNT WILL NOT ALLOW LENS TO BE SECURED. LOWE LAMP BAR SWIVEL IS BROKEN. REPLACED EMERGENCY EXIT LIGHT ASSY PER B767 WDM 33-51-11. OPS CHECK GOOD PER B767 MM 33-51-01-2.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE:PS DURING PERIODIC SERVICE CHECK, FOUND EMERGENCY LIGHT L312 AT INOP. DETERMINED WIRES CRIMPED BETWEEN STRUCTURE AND LIGHT ASSY. LIGHT ASSY WAS ALSO UNSERVICEABLE. SHORTED PWR WIRE BLEW LOAD FUSE IN BATTERY PACK/CHARGER. REPLACED BATTERY PACK/CHARGER AND L312 LIGHT ASSY. REPAIR DAMAGED WIRING TO LIGHT. EMERGENCY LIGHT CHECKED NORMAL AFTER CORRECTIVE ACTION.

Part: CONNECTOR — LOOSE (LT ENGINE) · airframe 28,679 hrs · 9,662 cycles

INSPECTION TYPE:ETOP 2:20 HRS INTO FLT AT FL 410 EICAS LEFT ENGINE OIL PRESSURE 160, RIGHT ENGINE OIL PRESSURE 52, NO EICAS MSG & NO OIL LIGHT. TROUBLESHOOTING WITH TECH SUPPORT FOUND LOOSE CONNECTOR PLUG. REPLACED CONNECTOR ON L/P 667048/2. RAN ENGINES AND NO DEFECTS FOUND AFTER CONNECTOR CHANGE. A/C RETURNED TO SERVICE.

Part: SEAT TRACK — DAMAGED (COCKPIT)

SEAT TRACK DAMAGED AT POS 2R 3RD LOCK FOR -M- CONTAINERS. BLENDED SEAT TRACK PER SRM 53-00-52 DEFER FOR SEAT TRACK REPAIR DMI D-328864. REMOVED AND REPLACED POS 2R SEAT TRACK REF SRM 53-10-52-2R. THIS CLEARS THIS DEFERRAL.

Part: SMOKE GOGGLES — CRACKED (COCKPIT)

INSPECTION TYPE:N/A CAPTAIN'S SMOKE GOGGLES CRACKED. REPLACED CAPTAIN'S SMOKE GOGGLES

Part: APU — INOPERATIVE (APU BAY)

LT GEN DRIVE LIGHT IN FLIGHT. APU FAULTED TWICE IN FLIGHT, DID NOT START. CREW DIVERTED TO NEAREST SUITABLE AIRPORT (DNA). DECLARED EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. LT IDG DEFRD DMI 293462. PER FIM 24-11-00 REPLACED LH IDG & OPS CHECKED NORMAL AS PER MM 24-11-00-5. A/C OK FOR SERVICE CLEARD DMI 293462 AND REMOVED PLACARD.

Part: FIRE LOOP — INTERMITTENT (LT ENGINE)

INSPECTION TYPE:N/A, ON TAXI OUT RECEIVED EICAS STATUS MSG OF L ENG FIRE LP 2 INTERMITTENTLY WITH THROTTLE LEVER MOVEMENT. *S/D* CLEARED M208730. NR 2 FIRE WARNING TESTS OK. NO MSGS, 2 FLTS.

Part: FIRE LOOP — FALSE INDICATION (LT ENGINE)

INSPECTION TYPE:N/A, FIRE/OVHT SYS EICAS MSG ON DESCENT. RESET W/EICAS MSG OUT-TWO OCCURRANCES. PERFORMED ENG FIRE DETECTION SYS BITE PROCEDURE IAW 26 11 00 FIG 104. RESEATED AFOLTS CARDS M10224 & M10274 PER FIM MANUAL SYS TESTS GOOD. OK FOR CONTINUED SERVICE.

Part: SKIN — DENTED (BS 1295)

INSPECTION TYPE-SP, DENT ON FUSELAGE CROWN AT STA 1295 AND STR 7R IS OUT OF LIMITS. REPAIRED AREA IAW SRM 53-00-01 FIG 201.

Part: ENGINE — BIRD STRIKE (RIGHT)

INSPECTION TYPE:N/A, ON ROTATION AT SDF TO BWI: BIRDSTRIKE, NOTICED FOUL, BURNING ODOR THAT LASTED 30 TO 40 SECONDS. ALL ENGINE INDICATIONS NORMAL. INSPECTED LT AND RT INLET AND EXHAUST. CLEANED BIRD FOD FROM RT NOSE COWL, FAN AND COMPRESSOR STATOR VANES, NO DAMAGE NOTED. RAN PACKS, NO FOUL ODORS NOTED.

Part: ACTUATOR — FAILED (NR 4 SPOILER)

CENTER HYDRAULIC QUANTITY DECREASED OF 0.02 PERCENT. SYSTEM DEPRESSURIZED AND LANDED WITH ALTERNATE FLAPS AND GEAR WITH NO INCIDENT. REMOVED AND REPLACED O-RING ON FILTER CAP ON NR 4 SPOILER ACTUATOR ASSY. LEAK CHK GOOD.

Part: APU — FUEL LEAK (APU DRAIN MAST)

MAINTENANCE REPORTED FUEL RUNNING OUT OF THE DRAIN MAST APU RUNNING. PLACARD PER MEL 49-11-1.