N684UA

Part: LIGHT — BROKEN (ZONE 200) · airframe 77,443 hrs · 13,358 cycles

36D EMERGENCY PATH LIGHT ON SEAT BROKEN AND FOUND HANGING FROM SEAT. LIGHT HOUSING HAS BROKEN TABS SO UNABLE TO SECURE TO SEAT. TAPE FOUND ON SIDE WHICH FAILED TO RETAIN UNIT TO SEAT. NEW LIGHT ASSEMBLY INSTALLED AND EMERGENCY LIGHT SECURED INSIDE UNIT. TASK CARRIED OUT IAW CMM 25-23-52. EMERGENCY LIGHT OPS TEST CARRIED OUT IAW AMM 33-51-00/501.

Part: DISPLAY — FAULTED (FLIGHT DECK) · airframe 76,523 hrs · 13,242 cycles

EICAS UPPER DISPLAY BLANK AFTER TAKEOFF. NO AUTO. INTERMITTENT ON/OFF UPON ARIVAL FOUND UPPER EICAS DISPLAY FULLY OPS. PERFORMED EICAS OPS TEST REF 31-41-00-715-001 TEST PASS AS PRECAUTION. R & R UPPER DISPLAY CRT EFIS REF AMM 31-41-01/401. THE EICAS COMPUTER MANUAL SELECT SWITCH IS FULLY OPS WHEN LT OR RT COMPUTER IS SELECTED. WORKED IAW AMM REF 31-41-00/001.

Part: UNKNOWN — NOISE (ZONE 800) · airframe 75,935 hrs · 13,166 cycles

FA REPORTED HISSING SOUND AT L OVERWING EXIT 4000 FT ON DESCENT PERFORMED A LEAK TEST PER MM TASK 05-51-24-782-001. NO HISSING OR LEAK OBSERVED.

Part: INDICATOR — FAULTED (MACH SPEED) · airframe 75,823 hrs · 13,151 cycles

REJECT TO DUE TO A/S DISAGRE. CAP+STB 120KT/ FO 100 KT AND FLAG BRK TEMP 9 FOUND RIGHT HAND MAC AIRSPEED INDICATOR FLICKERING. REMOVED AND INSTALLED NEW MAC AIRSPEED INDICATOR REF AMM 34-13-02-404-003. FAULT NO LONGER REMAINS WITH NEW INDICATOR. FURTHER TROUBLESHOOTING TO FOLLOW THIS LOGPAGE. PARTS USED: 75-3111-9-0001,QTY :1 ROTABLE PARTS CHG:TT # 1419634 SN OFF 2206 PN OFF 75-3111-9-0001 INDICATOR, MACH OFF 75-3111-9-0001 2206 ON 75-3111-9-0001 4315 REF AMM 34-11-00-730-811 AND AMM 34-11-00-730-812, PERFORMED PITOT PERFORMANCE ACCURRACY TEST WITH NO DIFFERENTIAL. PERFORMED PITOT LEAK RATE CHECK WITH BOTH SYSTEMS WITHIN LIMITS. SUSPECT MASI FITTED TO CAPT POSITION AND FAULT FOLLOWED, CAPT MASI FITTED TO FO POSITION WITH NIL FAULT. SUSPECT MASI REPLACED AND CAPT SERVICEABLE MASI RE-FITTED IN CAPT POSITION. NO FAULTS ON LEFT AND RIGHT ADC OPS TESTS REF AMM 34-12-00-715-001. PITOT LEAK CHECK IMAGES ADDED FOR REF. REF LP 5316578 TROUBLESHOOTING FOR AIRCRAFT AOA SENSORS. AIRCRAFT HAS AOA SENSOR MODEL 0861FL INSTALLED IN BOTH CAPT / FO POSITIONS. FIM TASK 34-12 CARRIED OUT FOR BOTH AOA SENSORS. CAPTAINS AOA SENSOR MEASURED 50G UPWARDS AND 20G DOWNWARDS. FO AOA SENSOR MEASURED 20G UPWARDS AND 30G DOWNWARDS. PER FIM BOTH AOA SENSORS WELL WITHIN LIMITS.

Part: UNKNOWN — ODOR (CABIN) · airframe 75,823 hrs · 13,151 cycles

AFT FA NOTICED SLIGHT SMOKE SMELL ON T/O PRIOR TO REJECT REF AMM TASK 05-51-56-940-801-C1, SMOKE/ODOR EVENT QUESTIONNAIRE FORM WAS NOT COMPLETED BY CREW. SMOKE/ODOR WAS BRIEF AND DISAPATED QUICKLY. PERFORMED VISUAL INSPECTIONS AND OPS CHECKS OF AFT GALLEY EQUIPMENT (ALL OVENS, COFFEE MAKERS, WARMERS AND CHILLERS) WITH NO REOCCURANCE OR FINDINGS. PERFORMED APU AND BOTH AIR CONDITIONING PACK OPERATION WITH NO ODOR REOCCURANCE OR FINDINGS. REPLACEMENTS OF PARTS OR "BURN-OUT". DISPOSITION OF EVENT COMPLETED.

Part: CONTROLLER — FAULTY (A/C PACK TEMP) · airframe 75,127 hrs · 13,059 cycles

EXCESSIVE CABIN TEMP. UP TO 83F ALL ALTS. CLIM B AND CRUISE. RAN QRH NO HELP.PER CREW DEBRIEF A/C TEMPS WERE HIGHER THEN NORMAL ON GROUND, SUSPECTED TEMPS WOULD GO DOWN WHEN IN THE AIR. DURING CLB, CRZ AND HOLDING TEMPS ONLY GOT TO 75 DEGREES DURING BRIEF PERIOD WHEN QRH WAS FOLLOWED WITH OPENING OUTFLOW VALVE THEN TEMPS WENT BACK TO 80+ NO FURTHER INFO TO PROVIDE. UPON ARRIVAL TO A/C F/D FWD AND AFT CABIN TEMPS SHOW 78, 81 AND 80. ECS AUTO EVENT SNAPSHOT PERFORMED ZTCU AND CTC BITE PER FIM 21-61 TASK 902 WITH ZTCU FAULTING AFT ZONE TEMP SELECTOR DUE TO INOP LIGHT AND LEFT CTC FAULTING TEMP CONTROL VALVE, REMOVED AFT CABIN ZONE TEMPERATURE SENSOR REF B767 AMM 21-61-08-004-001-005. REPLACEMENT AND OPS CHECK REQUIRED. REINSTALLED PREVIUSLY REMOVED AFT CABIN ZONE TEMPERATURE SENSOR REF B767 AMM 21-61-08-404-017-005 OPS CHECK GOOD. PRRFORMED BITE CHECK OF RIGHT PACK TEMP CONTROLLER REF AMM 21-51-14, CONTROLLER FAILED. REMOVED & REPLACED REF AMM 21-51-14, OPS CHECKS GOOD.

Part: COVER — DETACHED (ZONE 800) · airframe 75,127 hrs · 13,059 cycles

DOOR 1L..SLIDE COVER FALLING OFF INSPECTED DOOR SLIDE BUSTLE AT L1 AN FOUND COVER COMPLETELY SECURE. INSPECTED R1 DOOR AS PRECAUTIONARY AND FOUND SAME RESULTS. SECURE.

Part: STRINGER — CORRODED (ZONE 100) · airframe 74,389 hrs · 12,963 cycles

BELOW FLOOR S39L FOUND CORROSION AT STA478-STA500 REF HX NR WO.4336897, ORGI BY V896820 FWD CARGO COMPT STR 39L BETWEEN STA478 AND STA500 REPAIRED AS PER ECRA 5300-03187 REV

Part: STRINGER — CORRODED (ZONE 100) · airframe 74,389 hrs · 12,963 cycles

FWD CARGO COMPT BELOW FLOOR S39R FND CORROSION AT STA 478 - STA 500 REFER HX NR WO4336886. FWD CGO COMPT STR 39R BETWEEN STA 478 AND STA 500 REPAIRED AS PER ECRA 5300-03187 REV.

Part: STICKER — CRACKED (ZONE 100) · airframe 74,389 hrs · 12,963 cycles

EA 5310-07143 REV E OP 002, 1EA CRACK FOUND ON SUBSURFACE OF RH NOSE WHEEL WELL VERTICAL STIFFENER ON STA 287 BETWEEN WL 118 TO 159 APPROX. 1.125" IN LENGTH AS MARKED. DETAIL REFER ATTACHED REPORT, RH NOSE WHEEL WELL VERTICAL STIFFENER STA 287 BTW WL 118 - 159 P ERMANENT REPAIRED AS PER EA 5310-07143 REV E OP 004.

Part: LENS — MISSING (ZONE 200) · airframe 74,377 hrs · 12,962 cycles

2X EMERGENCY LIGHT LENS COVER MISSING AT DOOR 1L 2X EMERGENCY LIGHT LENS COVERED INSTALLED IAW AMM TASK 33-51-10-962-172. OPS TEST GOOD. SDR RAISED AS PER GMM.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 74,377 hrs · 12,962 cycles

R/H SIDE EXTERIOR EMERGENCY LIGHT NOT WORKING EXTERIOR EMERGENCY LIGHT BLUB REPLACED IAW AMM 33-51-00. OPS TEST CARRIED OUT. ALL SATIS. SDR RAISED AS PER GMM.

Part: STATOR — BROKEN (BRAKE ASSY) · airframe 72,807 hrs · 12,752 cycles

ON LANDING SMOKE AND FLAMES OBSERVED ON RIGHT MAIN GEAR REPORT BY ANOTH A/C #7 BRAKE FOUND DAMAGED REF PICS, NO DAMAGE FOUND TO WHEEL AXEL OR NEIGHBOURING COMPONENTS. NO OVERTEMP WARNING INDICATION IN FLIGHTDECK. REMOVAL AND INSTALLATION OF MLG WHEEL I.A.W AMM TASK 32-45-01-004-001/ AMM TASK 32-45-01-404-027. REMOVAL AND ADD EMP:U401301,U347460,U366261 INSTALLATION OF MLG BRAKE I.A.W AMM TASK 32-41-08-004-001/ AMM TASK 32-41-08-404-017.PARTS USED: 76-3245-9-9001,QTY :1 76-3243-9-0002,QTY :1 PARTS USED: 76-3245-9-9001,QTY :1 76-3243-9-0002,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1563840 SN OFF 5395 TT # 1896642 SN OFF 0176 BRAKE, MLG, CAR OFF 76-3243-9-0002 5395 ON 76-3243-9-0002 2476 WHEEL, TIRE, AS OFF 76-3245-9-9001 0176 ON 76-3245-9-9001 8524 IDT INSPECTION CARRIED OUT PER GMM 09-10-05 TO BRAKE ROD PIN, END CAP, WASHER AND BOLT INSTALLATION PER AMM 32-41-08 AND OK TO CONTINUE.

Part: HOSE — MISINSTALLED (HYD SYSTEM) · airframe 71,422 hrs · 12,573 cycles

MAIN (LEFT, RIGHT, AND CENTER) HYDRAULIC SYSTEMS HYD QTY (01=L, 02=R) DECREASED TO _. QTY STABLE WITH EDP DEPRESSURIZED AND ACMP OFF 01 45 MINS AFTER TAKEOFF L HYD QTY EICAS MSG. L QTY WAS .45 DECRSN G .01/MIN W/ PUMPS ON. UPDATED FOR SDR AWARNESS PURPOSES. RUDDER RATIO CHANGER LEFT SYSTEM HYDRAULIC HOSE LEAK. RECTIFIED AS PER LP 7278092 LEFT SYSTEM NOW SATIS. LEAK FOUND AT LOOSE CONNECTION ON HYDRAULIC BLOCK CONNECTIONS FOR RUDDER RATIO CHANGER ACTUATOR HOSES. ALSO ORIENTATION OF PIPEWORK IS INCORRECT AND BADLY ASSEMBLED WITH STRAPS. HOSE CONNECTIONS TO BLOCK SHOULD BE HORIZONTAL NOT VERTICAL, PREVENTING STRESS ON PIPEWORK WHEN IN OPERATION. LEFT HYDRAULIC SYSTEM LEVEL BEFORE WORK BEGAN WAS AT . 30 . LEFT SYSTEM SERVICED TO FULL FOR LEAK CHECK PURPOSES. LOOSE UNION REMOVED AND REFITTED WITH NEW PACKING AS PER AMM 22-21-02-414-016. LEAK CHECK CARRIED OUT AS PER SUBTASK 22-21-02-864-048, NO LEAKS PRESENT. OPERATIONAL TEST OF THE YAW DAMPER SYSTEM CARRIED OUT AS PER AMM 22-21-00-715-001-001. SYSTEM TEST SATIS. RRCA HYDRAULIC HOSE STRAPS INSTALLED AS PER TASK 27-21-15-422-024. FIG 204. FIN ACCESS PANEL 311AZ INSTALLED AND STAB BAY CLOSED.

Part: TRANSMITTER — INOPERATIVE (OIL QTY) · airframe 71,358 hrs · 12,565 cycles

15 MIN AFTER TO OIL QTY 7 20 MIN AFTER TO OIL QTY 0. DEFERED DUE INDICATION FOUND AT FAULT. NO OIL LOSS RECORDED OR V ISUALLY FOUND. CREW REPORTED NO LOSS OF OIL PRESSURE OF LOW PRESSURE LIGHT. MEL 7931B APPROVED FOR ENG 2 OIL QTY INDICATION INOP. DEFERRAL APPLIED. SDR ADDED. *DM* PENDING T/S RESULTS, ADDING X-MITTER/SEAL, CONNECTOR/ BACKSHELL TO M & L. REMOVED AND REPLACED E2 OIL QUANTITY TRANSMITTER IAW 767 AMM 79-31-01-424-015-N00. OPS CHECKS GOOD. DDP AND MEL CLEARED. PLACARD REMOVED.

Part: CABLE — INTERMITTENT (EMERGENCY LIGHT) · airframe 71,190 hrs · 12,542 cycles

EMERGENCY LIGHTS OPERATIONAL CHECK {B767-33-3-7000} - EMERGENCY AISLE LIGHTS AT SEAT 32 DEF WORKS INTERMITENTLY, SEAT BACK MOVED FORWARD AND BACK, LIGHT FLICKERS ON/OFF. SUSPECT WIRING FAULT. IDT INSPECTION ITEM REQUIRED. CHECK FOUND CABLE INTERMITTENT. PARTS ORDERED. CHECKED EMERGENCY LIGHT OPERATION AND ALL FOUND NORMAL AT 32DEF. SUBJECT QUICK DISCONNECT WIRING REPLACED. OP CHK IAW AMM 33-51-00-710-801-C1 PARTS USED: 76-2334-3-0079,QTY :1 TEST RESULT SATIS WITH NIL FURTHER FINDING IDT INSPECTION CARRIED OUT. LP CLEARED TO BE CLOSED.

Part: FUEL CAP — MISSING (LH WING) · airframe 71,029 hrs · 12,520 cycles

LH FUEL RECEPTACLE CAP MISSING NIL STOCK LHR REQUEST MEL 2821J ADD FAULT: 2821 MEL COMPLIED WITH APPROVED REPLACED LH FUEL RECEPTACLE CAP IN REF WITH IPC 28-21-01-11 PARTS USED: 00-0584-3-0701,QTY :1

Part: TANK UNIT — INTERMITTENT (LH WING, #8) · airframe 70,927 hrs · 12,501 cycles

LEFT FUEL QUANTITY DROPPED FROM 36.5 TO 29.7 IN APPOX 30 SECS THEN RETURNED TO 35.6 ACCOMPLISHED IDT INSPECTION OF FUEL PROBE #8 INSTALLATION, VERIFIED CDCCL''S PER GMM 09-10-05 DUE TO HISTORY OF LEFT FUEL TANK DENSITOMETER AND TANK PROBE TU8 REPEAT HITS ON THE FQIS REPLACING BOTH. PARTS USED: 99-2841-9-0009,QTY :1 99-2841-9-9004,QTY :1 LEFT WING #8 TANK UNIT TRACKING INFO ROTABLE PARTS CHANGE WAS INDICATED - TT # 1277314 SN OFF 0446 DENSITOMETER TRACKING INFO ROTABLE PARTS CHANGE WAS INDICATED - TT # 1835526 SN OFF 5250 INSTALLED LEFT TANK UNIT 8 REF AMM 28-41-01-404-017-002 ADD EMP:U138004 UNIT, TANK, FQI OFF 99-2841-9-9004 0446 ON 99-2841-9-9004 4738 UNIT, TANK, FQI OFF 99-2841-9-9004 0446 ON 0000 DENSITOMETER, F OFF 99-2841-9-0009 5250 ON 99-2841-9-0009 8008 DENSITOMETER, F OFF 99-2841-9-0009 5250 ON 0000 INSTALLED DESITOMETER REF AMM 28-41-03-404-014-002. COMPLEATED FUEL QUANTITY INDICATING SYSTEM OPERATION TEST REF AMM28-41-00-715-001-002, TESTED GOOD. ADD EMP:U101111.

Part: SKIN — CORRODED (BS 785) · airframe 68,239 hrs · 12,135 cycles

CORROSION LOWER SURFACE RIGHT WING CENTER BS 785.9 BTW KEEL BEAM AND BL 62 AT LOWER FUSELAGE (4 EA). REFER TO AEROMAN NON ROUTINE 2023-239484 MEASURES ON REWORKED AREAS ARE: P1 L: 2.392 IN W: 0.996 IN P2 INCH IAW NDT MANUAL PART 4, 51-00-10. NOMINAL THICKNESS ON PERFORMED HFEC INSPECTION ON OPEN FASTENERS HOLES (8E/A) IAW LOG PAGE #4686251 AND INSTALLED DOT AS PER GMM 06-35-05 L: 2.509 IN W: 1.568 IN P3 L: 1.933 IN W: 1.131 IN P4 L: REWORKED AREAS ON LOWER SURFACE RIGHT WING CENTER BS 785.9 BTW 767 NDT PART 6 51-00-04 CRACK INDICATION NOT FOUND. 1.263 IN W: 1.124 IN. MINIMUM REMAINING THICKNESS ON REWORKED KEEL BEAM AND BL 62 AT LOWER FUSELAGE IS: 0.200 IN I.A.W DWG PERFORMED DVI ON REWORKED AREA AND NOT FOUND MORE CORROSION AREAS ARE P1= 0.161 IN, P2= 0.134 IN, P3= 0.164 IN AND P4= 0.174 #111T4018. PERFORMED EDDY CURRENT HFEC INSPECTION ON REWORKED IAW B767-300 SRM 51-10-08-0G-0, PERFORMED SCEPTRE ENTRY ACCOMPLISHED REPAIR ON LOWER SURFACE RIGHT WING CENTER BS 785.9 BTW KEEL BEAM AND BL 60 AT LOWER FUSELAGE I.A.W. EC/RA# 5720-03333 AND EA# 57-0183-23 R0 PART 1 AND PART 2 AND NO DEVIATIONS ARE ALLOWED WITHOUT PRIOR ENGINEERING APPROVAL. ADD EMP:V938997 REVIEWED AND CARRIED TO DMG.

Part: SKIN — UNKNOWN (AFT CARGO DR) · airframe 67,894 hrs · 12,088 cycles

EA5100-02345 REV E FOUND REINFORCINGT DOUBLER REPAIR ON AFT CARGO DOOR EXTERNAL SKIN AT 6OCLOCK FROM UPPER EDGE 13IN FROM AFT EDGE SIZE 13/12X9 REPAIR HAS A DEEP SCRATCH 3IN LONG REF AAR N/R 975221 REMOVED EXISTING DOUBLER AND REINSTALLED NEW DOUBLER ON AFT CARGO DOOR AS PER B737 SRM 52-00-01-2R-2 AND SRM 51-40-02-0G-0 MAT USED ID 2024-T3 0.080 CLAD NO EXTRA WEIGHT ADDED WORK ACCOMPLISHED BY V894534

Part: TIRE — FLAT (NR 2) · airframe 66,976 hrs · 11,960 cycles

DURING INCOMMING FOUND TIRE NR 2 FLAT ZERO PRESSURE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 65,785 hrs · 11,795 cycles

CENTER HYDRAULIC SYSTEM LOST ALL FLUID. EMERGENCY LANDING DECLARED. ADP PRESSURE/CASE DRAIN FILTER MODULE CASE DRAIN PIPE IS SHEARED CASE DRAIN PIPE (GREEN) AND CTR SYS PRESSURE PIPE (SILVER) ADP HYD FILTER MODULE CASE DRAIN AND PRESSURE ELEMENTS REPLACED PHOTOS OFF. ADJACENT PIPE (SILVER) ALSO DAMAGED. 3 PIPE SUPPORT BRACKETS REMOVED FOR REPLACEMENT PER IPC 29-11-17-04. UNIONS BLANKED. REF AMM 29-11-19-401. FOUND CASE DRAIN FILTER ELEMENT CRACKED AND P-CLIPS BROKEN ON WHEEL WELL BULKHEAD. CONTAMINATED WITH DEBRIS AND METALLIC OIL. PRESSURE FILTER ELEMENT CONTAMINATED WITH METALLIC OIL.

Part: STRINGER — CORRODED (FUSELAGE)

TEST, TEST, TEST - B767-53-3-7058 BULK CARGO STA 1540-STA 1562 S37L STRINGER FOUND CORRODED BULK CARGO COMPT STA 1540-1562 S37L STRINGER REPAIRED AS PER SRM53-00-03 REPAIR 2 AND REFER EC/RA 5310-07607 REV - AND ATTACH MAINTENANCE WORKSHEET FORM ITEM 1-42 ACCOMPLISHED RII INSPECTED OKAY BULK CARGO COMPT STA 1540-1562 S37L STRINGER REPAIRED AS PER SRM53-00-03 REPAIR 2 AND REFER EC/RA 5310-07607 REV - AND ATTACH MAINTENANCE WORKSHEET FORM ITEM 1-42 ACCOMPLISHED RII INSPECTED OKAY.

Part: ACCESS PANEL — MISSING (RT WING) · airframe 63,898 hrs · 11,539 cycles

INSPECTION ACCESS PANEL MISSING RT WING LEADING EDGE SLAT MECHANISM LUBRICATION ACCESS DOOR 621XB ITEM PLACED ON CDL MISSING PLACED ON CW CDL OK TO CONTINUE DISPATCH DESK:LEADING EDGE SLAT MECHANISM LUBRICATION ACCESS DOOR 621XB - CDL 57F UPDATE REPLACED MISSING PANEL 621XB

Part: SWITCH — NONE (P5 PILOT OVERHEA) · airframe 63,733 hrs · 11,512 cycles

SMOKE IN FLIGHT DECK CREW DEBRIEF: THE FLIGHT CREW STATED AT THE APPROXIMATE SAME SPOKE WITH TOMC AND WE WILL START THE AMM TASK 05-51-56-940-8 ACCOMPLISHED INITIAL INSPECTION OF FLT DECK AS PER AMM TIME THEY SWITHCED ON THE RUNWAY TURNOFF, BEACONS AND NAV LIGHTS 01-C1. 05-51-56-940-801-C1 STEP 1. C (1). NO DEFECTS NOTED. AS PER TOMC ON HE SAW A PUFF OF SMOKE COME FROM THE AREA OF THE SWITCHES. NEED TO CONTINUE AT STEP 1 C (2). THIS WAS ALSO FOLLOWED BY AN ELECTRICAL BURNING SMELL. INSPECTED M10056 ON THE P5 PILOT OVERHEAD PANEL. FOUND MELTED TERMINAL POST ON THE S2 RIGHT RWY TURN OFF LIGHT SWITCH. R&R S2 SWITCH PER WDM 33-42-21. OPS CHECK GOOD. ADD EMP:U353871 REF ABOVE UPDATE FOR ID OF THE SOURCE OF THE SMOKE. PER AMM 05-51-56 B(6.A) & SUB TASK 05-51-56-200-001-C4 NO FURTHER MX REQ''D AT THIS TIME.

Part: LENS — NONE (LH EXIT SLIDE LT) · airframe 63,529 hrs · 11,484 cycles

EXTERIOR EMERGENCY LIGHTING SYSTEM HAS BEEN DEFERRED IN COMPLIANCE WITH CDL CARD 335110 AND REF LOGPAGE 8107342 REPAIR TO BE CARRIED OUT WITHIN 1 FLT CYCLE. EXTERIOR EMERGENCY LIGHTING SYSTEM HAS BEEN DEFERRED IN INTERIM REPAIR CARRIED OUT PER ECRA 3351-01366 PART 1. LENS COMPLIANCE WITH CDL CARD 335110 REF LOGPAGE 8107342. REINSTALLED AND SEALED AS PRESCRIBED IN PART 1. PART 3 PERMENANT APPROVED 1 CYCLE DIP REF ECRA 3351-01366 TOTAL AIRCRAFT CYCLES TOMC-APPROVAL FROM SC1ELBYC COMMENT 11483 CURRENTLY MEL 3351B REJECT LIGHT WORKS JUST LENS CRACKED AND WILL BE DIP FOR 1 CYCLE LIGHT AFFECTED IS L645, LEFT SIDE OVERWING EXIT SLIDE FLOODLIGHT RECORDS UPDATE ASSY. IMAGES ATTACHED. REMOVED AND REPLACED LENS ASSEMBLY AS PER ECRA 3351-01366 REV A PART 1A. WILL REQUIRE AERODYNAMIC SEALANT. REFERENCE L/P 8111695 FOR AERODYNAMIC SEALANT DIP. THIS DIP CLOSED. T/A: 1 F/C..................LT

Part: SENSOR — FAULTED (SLAT SYSTEM) · airframe 61,342 hrs · 11,149 cycles

LE SLAT ASSYM EICAS ALERTED TWICE FLAP INDICATOR INDICATED BETWE EN 0 AND 1 ACCOMPLISHED FSEU BITE CHECK FAULT IMAGE UPDATED COULD NOT DUPLICATE FLAP ASYMMETRY DISCREP., PERFORMED PSEU BITE, FOUND S295, & CODE 10. VISUALLY INSPECTED LE SLAT NR 11 AND TRACKS FOR PHYSICAL COND. AND NORMAL OPS, NO DEFECTS NOTED. INSPECTED AND FOUND S295 GAP WITH SLAT RETRACTED AT .152, RESHIMMED SENSOR AND VERIFED SLAT EXT. AND RET. S295 GAP TO ADD EMP:U348911,U349639 UNIT, ASSY, PRO OFF 76-3260-9-0005 0886 ON 76-3260-9-0005 0941 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1089410 SN OFF 0886 FOR SERVICE. CYCLED LE AND TE DEVICES SEVERAL TIMES ALL CKS. GOOD. ACFT OK (CODE 10 ISSUE) REF. AMM 32-09-04. INSTALLATION TEST GOOD. SPEC. REF. FIM 27-81-00-814-809, & AMM 27-88-01. REPLACED PSEU ENTRY IN PREVIOUS SIGNOFF MADE IN ERROR. ITEM SHOULD HAVE READ CARD 10, NOT CORE 10.

Part: FLOAT VALVE — MISINSTALLED (LT WING TANK) · airframe 61,087 hrs · 11,108 cycles

SUPPORT TASK - L/H WING AUX TANK NGS FLOAT VALVE INCORRECT INSTALLED REFER NR LP 9131168. LHW AUX TANK NGS FLOAT VALVE AND COVER PLATE RELOCATED TO BTN STR U-13 AND U-14 IAW EC/RA NO.4721-01010. ATTACHED FORM 44-0008 ITEM 1 TO ITEM 36 ACCOMPLISHED AND EC/RA NO.4721-01010 ACCOMPLISHED. ADD EMP:V897896 IDT INSPECT IS OKAY. APPROVED BY HX 135865.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 60,844 hrs · 11,073 cycles

AUTO-THROTTLE EICAS MSG ON TAKEOFF LOW SPEED ABORT PERFORMED GROUND VISUAL FOR REJECTED TAKEOFF. PERFORMED MCDP GROUND TEST 2 AND TEST 30. TEST PASSED AS PER AMM 22-00-02. AIRCRAFT REMAINS FULL CAT CAPABILIY.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 58,054 hrs · 10,675 cycles

SUPPORT TASK - QC PICKUP SHEET AFT COMPARTMENT BS 1562 FRAME AFT SHEAR TIE CORRODED BETWEEN STR 39L-39R REFER NR LP 9132543 AFT COMPARTMENT STA 1562 BETWEEN S39L-S39R ATTACH FRAME SHEAR TIE REPLACED AND INSTALLED AS PER SRM51-10-02 AND SRM51-40-02 AND ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM1-14 ACCOMPLISHED SHEAR TIE P/N 146T1223-27 LOCAL FABRICATED AS REFER NRC LP9132913 WORKING DETAILS RII INSPECTED OKAY.

Part: FITTING — CORRODED (FUSELAGE) · airframe 58,054 hrs · 10,675 cycles

REF NR LP 9132453 - SUPPORT TASK - EA 5340-01478 REV E OP 007 AD 2012-09-04 LT SIDE STA 955 REAR SPAR BULKHEAD FAILSAFE STRAP "T" FITTING FOUND SURFACE CORROSION AROUND FASTENER HOLE LT SIDE STA 955 REAR SPARE BULKHEAD FAILSAFE STRAP "T" FTG P/N 145T1929119 REPLACED AS PER EA5340-01478 REV - OP007 STEP 12 AND STEP 13 TRANSFERED HOLE AND INSTALLED NEW FTG STEP 18 SUB STEP 8 ATTACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 6 ACCOMPLISHED.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 58,054 hrs · 10,675 cycles

REF NR LP 9131853 - B767-53-3-7058 BULK CARGO COMPT STA 1540 AND STA 1562 S37L ATTACH STRINGER CLIPS FOUND CORROSION BULK CARGO COMPT STA1540 AND STA1562 S37L STRINGER CLIPS REPLACED AND INSTALLED AS PER SRM 51-10-02 AND SRM 51-40-02 AND ATTACH MAINTENANCE WORKSHEET FORM 44-0008 ITEM 1-6 ACCOMPLISHED STA 1562 S37L STRINGER CLIP P/N 146T1069-43, LOCAL FABRICATED AS REFER NRC LP 9132328 WORKING DETAILS STA 1540 S37L STRINGER CLIP P/N 140T2101U27.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 58,054 hrs · 10,675 cycles

B767-53-3-7058 BULK CARGO STA 1540-STA 1562 S37L STRINGER FOUND CORRODED BULK CARGO COMPT STA 1540-1562 S37L STRINGER REPAIRED AS PER SRM53-00-03 REPAIR 2 AND REFER EC/RA 5310-07607 REV - AND ATTACH MAINTENANCE WORKSHEET FORM ITEM 1-42 ACCOMPLISHED RII INSPECTED OKAY BULK CARGO COMPT STA 1540-1562 S37L STRINGER REPAIRED AS PER SRM53-00-03 REPAIR 2 AND REFER EC/RA 5310-07607 REV - AND ATTACH MAINTENANCE WORKSHEET FORM ITEM 1-42 ACCOMPLISHED RII INSPECTED OKAY.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,054 hrs · 10,675 cycles

BULK CARGO STA 1540 STR 37L AREA INTERIOR SKIN FOUND CORROSION. REPAIRED IAW ECRA 5331-02373PART 1 ITERIM REPAIR AT NRC TJE518820 INSP 156019. REPAIR IS CONSIDERED PERMANENT AS LONG AS REINSPECTION REQUIREMENTS OF PART 2 ARE COMPLIED WITH. ACCOMPLISH THE INSPECTION PER ECRA 5331-02373 PART 2 ON OR BEFORE THE AIRCRAFT REACHES 37500FC. REPEAT INSPECTIONS AT INTERVALS NOT TO EXCEED 9000FC THEREAFTER. DURING 8C FOUND INTERIOR SKIN CORROSION AT STATION 1540 AT STRINGER 37L. PER ECRA 5331-02373 COMPLY WITH REPAIR PART 1. INITIATE DIP TO ACCOMPLISH INSPECTION PER PART 2 ON OR BEFORE AIRCRAFT REACHES 37500 FLT CYCLES AND REPEAT INSPECTIONS AT 9000 FLIGHT CYCLES THEREAFTER. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEWED RECORDS.