N312UP

Part: SPLICE — CORRODED (ZONE 100) · airframe 71,659 hrs · 24,354 cycles

FAULT - CORROSION - SPLICE TEE , LOWER WING - TO - BODY FAIRING PANEL #149AL INTERNAL FORWARD SURFACE.REMOVED DAMAGE SPLICE TEE I.A.W SRM 51-40-02-0G REV.92.INSTALL NEW SPLICE TEE I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG NO. 145T8629 SHEET 2 REV: A

Part: SKIN — DENTED (ZONE 600 SLAT 12) · airframe 71,636 hrs · 24,347 cycles

GOUGE-SKIN, R/H WING LEADING EDGE #12 SLAT UPPER EDGE AT MIDDLE SUPPORT ADJACENT AREA (AGING A/C NSPECTION) (REPAIR) PERFORMED NDT/ET FOR THE CUTOUT AREA I.A.W. 767 NTM PART6 51-00-19 REV.140 <BR>RESULT:NO CRACK WAS FOUND.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-38 PANEL NO.232BFF.I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145 REMOVED MAIN DECK CARGO HANDLING AND SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.I.A.W AMM 53-01-06-400-801 REV.145 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-89 PANEL NO.231KFF (REPAIR)I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-05-004-047 REV.145 REMOVED MAIN DECK CARGO HANDLING.I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL & SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.I.A.W AMM 53-01-06-400-801 REV.145INSTALLED MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-05-404-052 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-75 PANEL NO.231CFF (REPAIR)I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-05-004-047 REV.145 REMOVED MAIN DECK CARGO HANDLING. I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL & SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.I.A.W AMM 53-01-06-400-801 REV.145 INSTALLED MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-05-404-052 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-78 PANEL NO.231AFF.I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145 REMOVED MAIN DECK CARGO HANDLING AND SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.I.A.W AMM 53-01-06-400-801 REV.145 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE , P/N : 143T5876-77 PANEL NO. 231BFF.I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145 REMOVED MAIN DECK CARGO HANDLING.I.A.W AMM 53-01-06-000-801 REV.145 REMOVED MAIN DECK CARGO FLOOR PANEL AND SEALANT.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400-801 REV.145 INSTALLED MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-84 PANEL NO.232FFF.I.A.W AMM 25-57-02-004-029 REV.145 REMOVED BALL TRAY ASSY.I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400-801 REV.145 INSTALL MAIN DECK CARGO FLOOR PANEL AND BALL TRAY ASSY AND CONDITION CHECK NORMAL

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-76 PANEL NO.232AFF.I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145 REMOVED MAIN DECK CARGO HANDLING AND SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.I.A.W AMM 53-01-06-400-801 REV.145 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DAMAGE, P/N: 143T5876-72 PANEL NO.232CFF.I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145 REMOVED MAIN DECK CARGO HANDLING AND SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.I.A.W AMM 53-01-06-400-801 REV.145 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N : 143T5876-81 PANEL NO.231HFF (REPAIR)I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-05-004-047 REV.145 REMOVED MAIN DECK CARGO HANDLING. I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL & SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.I.A.W AMM 53-01-06-400-801 REV.145 INSTALLED MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-05-404-052 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-79 PANEL NO.231JFF (REPAIR)I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-05-004-047 REV.145 REMOVED MAIN DECK CARGO HANDLING. I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL & SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.I.A.W AMM 53-01-06-400-801 REV.145 INSTALLED MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-05-404-052 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-83 PANEL NO.231GFF (REPAIR)I.A.W AMM 25-57-02-004-029 REV.145 REMOVED BALL TRAY ASSY.I.A.W AMM 53-01-06-000-801 REV.145 REMOVED MAIN DECK CARGO FLOOR PANEL & SEALANT.FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.I.A.W AMM 53-01-06-400-801 REV.145 INSTALLED MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL

Part: FILLER — CORRODED (ZONE 100) · airframe 71,636 hrs · 24,347 cycles

FILLER WITH SURFACE CORROSION AT STA 1601 IN THE AREA AFT BULK CARGO COMPARTMENT.REMOVED DAMAGE FILLER I.A.W SRM 51-40-02-0G REV.92.PERFORMED CHROMIC ACID ANODIZE I.A.W. EGAT WORK SHEET NO.:50363 STEP 7 AND SPWPS-AN-004 REV.26 AND SPDS-AN-001 REV.41.FABRICATED FILLER (P/N: 146T5609-67) PER BOEING DRAWING 146T5609 SH 7 REV:"-", PL REV. "AA".INSTALLED FABRICATE FILLER I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG NO: 146T5650 SH 5 REV: C (REPLACE)

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-80 PANEL NO.232HFF.I.A.W AMM 25-57-02-004-029 REV.145 REMOVED BALL TRAY ASSY.I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4. I.A.W AMM 53-01-06-400-801 REV.145 INSTALL MAIN DECK CARGO FLOOR PANEL AND BALL TRAY ASSY AND CONDITION CHECK NORMAL

Part: FILLER — CORRODED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND THE FILLER WITH CORROSION DAMAGE AT STA 1599 LBL 60 IN CEILING AREA OF BULK CARGO.REMOVED DAMAGE FILLER I.A.W SRM 51-40-02-0G REV.92. PERFORMED CHROMIC ACID ANODIZE I.A.W. EGAT WORK SHEET NO.:50362 STEP 7 AND SPWPS-AN-004 REV.26 AND SPDS-AN-001 REV.41. FABRICATE FILLER (P/N: 146T5609-67) PER BOEING DRAWING 146T5609 SH 7 REV:"-", PL REV. "AA" AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 11.INSTALLED FABRICATE FILLER I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG NO: 146T5650 SH 5 REV: C.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE, P/N: 143T5876-10 PANEL NO.232EFF.I.A.W AMM 25-58-04-004-010 REV.145 REMOVED SIDE RESTRAINT ASSY.I.A.W AMM 53-01-06-000-801 REV.145 REMOVE MAIN DECK CARGO FLOOR PANEL AND SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.I.A.W AMM 53-01-06-400-801 REV.145 INSTALLED MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.I.A.W AMM 25-58-04-404-015 REV.145 INSTALLED SIDE RESTRAINT ASSY AND CONDITION CHECK NORMAL.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK FLOOR WITH DENT DAMAGE, P/N: 143T5876-90 PANEL NO.232JFF. I.A.W AMM 25-57-02-004-029, AMM 25-57-05-004-001 AND AMM 25-58-01-004-001 REV.145 REMOVED MAIN DECK CARGO HANDLING AND SEALANT.FABRICATED A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.4.I.A.W AMM 53-01-06-400-801 REV.145 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL.I.A.W AMM 25-57-02-404-016, AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 REV.145 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 71,636 hrs · 24,347 cycles

FOUND MAIN DECK SEAT TRACK CRACK AT STA 522 LBL 88.I.A.W AMM 25-57-05-004-001 AND AMM 25-58-04-004-010 REV.145 REMOVED MAIN DECK CARGO HANDLING.I.A.W AMM 53-01-06-000-801 REV.145 REMOVED MAIN DECK CARGO FLOOR PANEL AND SEALANT.FABRICATED SEAT TRACK (P/N: 143T5242-1) PER BOEING DRAWING 143T5242 SH 1 AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 11.INSTALLED FABRICATED SEAT TRACK I.A.W SRM 51-40-02-0G, SRM 51-40-04-0G REV.92 AND BOEING DWG NO: 140T0510 SH 15 REV B SH 16 REV A.

Part: PAWL — BROKEN (ZONE 800) · airframe 71,255 hrs · 24,188 cycles

FWD LH ENTRY/SERVICE DOOR EXTERNAL HANDLE PAWL BROKEN. REMOVED AND REPLACED FWD LH ENTRY DOOR EXTERNAL HANDLE PAWL IAW 767 AMM 52-12-00. DOOR AND HANDLE TEST GOOD

Part: FLAP SYSTEM — FAULTED · airframe 69,450 hrs · 23,386 cycles

**EMERGENCY DECLARED**ON APPROACH WHEN FLAPS 20 SELECTED €Œ TE FLAP DISAGREE€? AOM PROCEDURE COMPLETED PERFORM FIM TASK 27-51 FAULT TREE 809.FAULT TE ON FSEU. FIM FAULT TREE , REPLACE FSEU . REPLACED FSEU REF 27-51-01-024-001, 27-51-01-404-130, OPS CK NML NO FAULTS. OK FOR SERVICE

Part: UNKNOWN — WARNING MESSAGE (RUDDER) · airframe 69,109 hrs · 23,234 cycles

*** DIVERSION *** RUDDER RATIO ON EICAS C/W FIM 27-21-804 AND FIM 27-09-814 NO FAULTS AND RUDDER RATIO CHANGER PASSES BITE TEST A/C OKAY TO CONTINUE

Part: INLET — CRACKED (UNKNOWN) · airframe 68,981 hrs · 23,174 cycles

#1 ENGINE INLET COWL HAS APPROXIMATELY 3.0 INCH CRACK AT 12:00 POSITION ON AFT PORTION OF BULLNOSE LIP. MARKED. REMOVED AND REPLACED LH ENGINE INLET DURING ENGINE CHANGE PER ENGINE CHANGE TASK CARD

Part: SLAT — CRACKED (UNKNOWN) · airframe 68,438 hrs · 22,937 cycles

RH WING #12 SLAT CLOSURE PANEL SPLIT AND NOT FAIRED TO LOWER WING SKIN. PANEL IS SPLIT APPROX. 2 INCHES OUTBOARD TO INBOARD. 10 CYCLE LIMIT, SM20/LMX4. FABRICATED NEW CLOSEOUT PANEL IAW DRAWING 7673655. INSTALLED CLOSEOUT PANEL IAW SRM 51-40-02. THIS CLEARS THE DEFERRAL.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 68,422 hrs · 22,930 cycles

*SDR FILED OPEN* RH WING #12 SLAT CLOSURE PANEL SPLIT AND NOT FAIRED TO LOWER WING SKIN. PANEL IS SPLIT APPROX. 2 INCHES OUTBOARD TO INBOARD.**10 CYCLE LIMIT***SM20/LMX4*** WILL REQUIRE S/M 20 HOURS TO REPAIR CLOSEOUT PANEL. LINE MX 4 HOURS TO DROP AND LOCK SLATS, HANGAR NOT NEEDED. REPAIR MATERIALS IN SDF.

Part: FITTING — BROKEN (UNKNOWN) · airframe 68,227 hrs · 22,849 cycles

FAULT - FOUND MAIN DECK CARGO RESTRAINT FLOOR ADAPTER FITTING BROKEN, LOC: STA 764 BL0, STA 764 LBL 47.5, STA 942 BL0, STA 1021 LBL 47.5, STA 1043 RBL 47.5, STA 1065 RBL 47.5. (REPLACE) 1.I.A.W AMM 20-11-00-910-802 REV.139.01 REPLACED FITTING AT STA 1021 LBL 47.5, STA 1043 RBL 47.5, STA 1065 RBL 47.5. 2.INSTALL MAIN DECK CARGO HANDLING AND FLOOR PANEL REFERENCE TASK CARD T3F18E0019LUQ. 3.JOB COMPLETED AND CONDITION CHECK NORMAL. 4.3.PART INFO ATTACHED. VERIFIED EO-87228 REVISED TO REV2 AND CLASS DEFINED AS MAJOR REPAIR.

Part: WARNING MESSAGE — FALSE ACTIVATION (AILERON SYS) · airframe 66,812 hrs · 22,287 cycles

INSPECTION TYPE:N/A**ATB** - AT ATLITUDE RECEIVED "AILERON LOCKOUT" MSG PERFORMED QRH RESULTED IN ATBR&R L AND R ADC PER TECH REQ. PER AMM 32-12-01. OPS CHECK GOOD. PERFORMED FIM 27-11-00-815-804 FOR AILERON LOCKOUT OPS CHECK GOOD IPC 34-12-01-50

Part: FAN — OUT OF BALANCE (LT ENGINE) · airframe 63,614 hrs · 21,162 cycles

ATB NO EMERG DCLD-NO EMERG EQUIP USED-LANDED UNEVENTFLY-AC OOS** DURING CL/OUT VIB ON LH ENG IND FAN 3.3 & INCREASED TO 4.0 AVER 3.5 3.7 @ CRZ VIB STEADY @ 1.9-2.0 DURING PWR REDUCT, INCRSD TO 3.5 REQ ATB TO MIA. PERF AVM BITE LH ENG, WGTS AVM BOX INCORR, PUT IN CORR WGTS MM 72 31 00 PERFOR VIB SURV FAN=3.1@72% MM71-00-00 D747231ACCOMPLISHED FAN TRIM BALANCE PER MM 72-31-00. ACCOMPLISHED VIBE SURVEY TEST NUMBER 6 PER MM 71-00-00, N1 FAN VIBES AT 0.8 UNITS.

Part: STIFFENER — CRACKED (BS 785) · airframe 63,507 hrs · 21,118 cycles

INSPECTION TYPE:C13CRACK 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 REPAIR2 REV.80.01 AND UPS EO B767-5740-58151-C AND B767-5720-76672-A.

Part: SEAT TRACK — BROKEN (BS 467-511) · airframe 63,507 hrs · 21,118 cycles

INSPECTION TYPE:C13BROKEN ON SEAT TRACK ON MAIN DECK CGO COMPARTMENT BETWEEN STA 467.45-STA 511.45,LBL 88.5.REPAIR I.A.W BOEING SR:3-5033972797 AND UPS EO B767-5310-80467-A.

Part: SEAT TRACK — CORRODED (BS 310-654) · airframe 63,507 hrs · 21,118 cycles

INSPECTION TYPE:C13CORROSION ON SEAT TRACK ON MAIN DECK CGO COMPARTMENT BETWEEN STA 610 AND STA 654, RBL88.5.REPAIR I.A.W. BOEING SR:3-5034191698 AND UPS EO B767-5310-80449-A.

Part: STIFFENER — CRACKED (BS 785) · airframe 63,507 hrs · 21,118 cycles

INSPECTION TYPE:C13CRACK ON CENTER WING TANK STIFFENER (P/N:111T2005-8) ON STA 785.9,RBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.80.01 AND UPS EO B767-5740-58151-C.

Part: STIFFENER — CRACKED (BS 785) · airframe 63,507 hrs · 21,118 cycles

INSPECTION TYPE:C13CRACK ON CENTER WING TANK STIFFENER(P/N:111T2005-7) ON STA 785.9,LBL 11.REPAIR I.A.W 767-300F SRM 57-10-10-2R-2 REPAIR 2 REV.80.01 AND UPS EO B767-5740-58151-C.

Part: WARNING MESSAGE — ILLUMINATED (LT ENG FIRE LOOP) · airframe 60,289 hrs · 19,970 cycles

STATUS MESSAGE L ENG FIRE LP 1 APPEARED DURING CLIMB TO CRUISE ALTITUDE. DEFERRED IAW MEL 26-11-1-1

Part: PRESSURE DECK — CRACKED (BS 955-977) · airframe 58,786 hrs · 19,406 cycles

INSPECTION TYPE:C12 CRACK ON WEB (P/N:145T8755-27) OF WHEEL WELL PRESSURE DECK BETWEEN STA 955 - STA 977, LBL 11.06 - LBL 33.06.REPAIR I.AW BOEING SRID :4-4491904695 AND UPS EO B767-5310-72942-A

Part: STIFFENER — CRACKED (BS 287) · airframe 58,786 hrs · 19,406 cycles

INSPECTION TYPE:C12CRACK ON VERTICAL STIFFENER AT WHEEL WELL BULKHEAD AT STA 287, RBL 25.REPAIR I.A.W UPS EO B767-5310-20118-F AND 767-300F SRM 51-70-12 GENERAL ,FIGURE 1 , REV 74.00.

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 58,786 hrs · 19,406 cycles

INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA985 - STA 1087,RBL77 - RBL 88 , PNL NO.242VFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B767-5320-9693-I

Part: FLOOR PANEL — DAMAGED (MAIN DECK CARGO) · airframe 58,786 hrs · 19,406 cycles

INSPECTION TYPE:C12DAMAGE ON M/D CARGO FLOOR PANEL AT STA 731-STA834,RBL 11 - RBL 33, PNL NO.242AFF.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO.B767-5320-9693-I

Part: BUMPER — MISSING (CREW DOOR) · airframe 57,703 hrs · 18,987 cycles

CREW ENTRY DOOR INTERIOR HANDLE BUMPER MISSING & PANEL DAMAGED.

Part: SEAL — TORN (PAX DOOR) · airframe 57,125 hrs · 18,787 cycles

ENTERY DOOR INSIDE SEAL WAS TORN. REPLACED TRIM SEAL AS REQUIRED IAW AMM 20-00-00.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 55,973 hrs · 18,360 cycles

LEFT WING INBD AFT FLAP T/E WEDGE, LOWER SKIN DENTED. REPAIRED IAW EO B767-5750-67013-B.

Part: SEAL — MISSING (PAX DOOR) · airframe 54,370 hrs · 17,794 cycles

RUBBER SEAL ON FWD EDGE OF CREW DOOR MISSING. INSTALLED THE RUBBER SEAL IAW AMM 52-12-02.

Part: HANDLE — WORN (PAX DOOR) · airframe 54,367 hrs · 17,793 cycles

EXTERIOR CREW ENTRANCE DOOR HANDLE INTERNAL PANEL WORN. REMOVED AND REPLACED THE DOOR HANDLE IAW CMM 52-11-12, OPS CHECKED GOOD.

Part: SKIN — CRACKED (BS 1725.5) · airframe 53,953 hrs · 17,632 cycles

INSPECTION TYPE: C11, CRACK FOUND ON THE RT FUSELAGE SKIN AT BS 1725.5, STRINGER 7R. REPAIRED IAW EO B767-5330-24301-D, APPX. C AND SRM 53-80-01-2R-5, REPAIR 5, DETAIL III, REV 68.

Part: SKIN — CRACKED (LT WING) · airframe 53,953 hrs · 17,632 cycles

INSPECTION TYPE: C11, CRACK WAS FOUND ON THE LEADING EDGE SKIN OF THE LT WING NR 4 SLAT AT INBD TRACK AREA REPAIRED IAW SRM 57-43-01-2R-2, REPAIR 2, REV 68.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 53,804 hrs · 17,578 cycles

MAIN CABIN DOOR TAB (YELLOW) VERY STIFF. HARD TO CLOSE. LUBED MAIN CABIN DOOR IAW 52-12-00. OPS CK OK.

Part: CABLE — JAMMED (THRUST REVERSER) · airframe 53,540 hrs · 17,497 cycles

NR 2 ENG LEFT REVERSER LATCH CABLE JAMMED. REPLACED LEFT REVERSER LATCH CABLE AND CAM IAW AMM 78-31-02.

Part: DOOR FRAME — CRACKED (CARGO DOOR) · airframe 52,588 hrs · 17,174 cycles

BULK CARGO DOOR HAS CRACK ON LOWER FRAME BETWEEN STA 1429 - 1448. REPAIRED IAW EO B767-5230-62183-B.

Part: BUMPER — CRACKED (CARGO DOOR) · airframe 52,556 hrs · 17,162 cycles

INSPECTION TYPE: N/A, BULK CARGO DOOR HAS A 1.5" CRACK AT THE LOWER FRAME BUMPER CONTACT POINT. STOP DRILLED CRACK, TREATED, PRIMED AND DEFERRED PER EO B767-5230-62183A.

Part: CONTAINER — DAMAGED (PILOT LIFE VEST) · airframe 51,719 hrs · 16,853 cycles

CREW LIFE VEST PILOT SEAT VACUUM PACKAGE UNSERVICEABLE. CREW LIFE VEST PILOT SEAT REPLACED IAW AMM 25-62-00, REV 118.01, DATED 05-04-16. PN OFF-ON: P01074-201C, SN OFF: 14081830040, S/N ON: 16010300020. EFF REF IPC: 25-64-55-05A, ITEM 010W REV 82.00 DATED 05-09-16.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 51,227 hrs · 16,698 cycles

NR 1 ENGINE, AFT ENGINE MOUNT SIGNS OF SURFACE CORROSION NR 1 ENGINE CLEAN & REMOVED CORROSION AFT ENGINE MOUNT IAW AMM 20-10-22.

Part: SHUTOFF VALVE — INOPERATIVE (RT DE ICE) · airframe 51,078 hrs · 16,640 cycles

DIVERSION, RT ENGINE HPSOV, ENGINE ANTI-ICE AVOID ICING LIGHT. REPLACED HPSOV IAW MM 36-11-07. LEAK TEST IAW MM 36-11-07-424-016-001, TEST GOOD.

Part: STIFFENER — CRACKED (BS 785) · airframe 50,099 hrs · 16,282 cycles

INSPECTION TYPE:C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, LBL 33. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 63 AND SREO: B767-5740-58151-A.

Part: STIFFENER — CRACKED (BS 785) · airframe 50,099 hrs · 16,282 cycles

INSPECTION TYPE:C10, CRACK ON CENTER WING FRONT SPAR STIFFENER UPPER SIDE AT BS 785.9, RBL 33. REPAIR IAW SRM 57-10-10, REPAIR 2, REV 63 AND REO:B767-5740-58151-A.

Part: STRINGER — CRACKED (BS 1552) · airframe 50,099 hrs · 16,282 cycles

INSPECTION TYPE: C10, CRACK, 6.6" WAS FOUND ON THE STR 20R AT BS 1552. REPAIR IAW SR:-3-3363130110 WITH FAA APPROVED 8100-9 FORM DATE: 04SEP2015 AND EO:B767-5310-58644-A.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 49,721 hrs · 16,153 cycles

EMERGENCY EXIT SIGN BY DOOR, BOTTOM LIGHTS INOPERATIVE. R & R EMERGENCY EXIT SIGN IAW MM 52-11-02-10A. OPS CHECKED IAW 52-11-02-10A, ITEM 075.

Part: STRUT — INOPERATIVE (DOOR HOLD OPEN) · airframe 49,411 hrs · 16,045 cycles

LIFE RAFT DOOR PNEU STRUT DOES NOT HOLD DOOR OPEN. R & R LIFE RAFT DOOR STRUT REF AMM 00-2.B. 2 OPS CHECKS GOOD.

Part: CONNECTOR — FAILED (NR 2 OIL XMITER)

NR 2 ENGINE OIL PRESSURE INDICATION INOPERATIVE, ALL OTHER INDICATIONS NORMAL . AIR TURN BACK. R & R OIL TRANSMITTER CONNECTOR SWPM 20-10-13 PARA 13.

Part: FLOOR PANEL — DAMAGED (CABIN)

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

Part: UNKNOWN — SMOKE (COCKPIT)

AFTER CLIMB AND LEVEL OFF, FAINT SMOKE ODOR DETECTED IN THE COCKPIT. SHUTDOWN LT PACK TO ISOLATE AND SMOKE BECAME VISIBLY GREATER AND MORE PUNGENT. LT PACK BACK ON WITH RT PACK ON, ODOR STILL EVIDENT. COMPLIED WITH FIM 21-00-21-810-802. RAN BOTH ENGINES AND PACKS. NO SMOKE OR FUMES PRESENT.

Part: ACTUATOR — INOPERATIVE (LT MLG)

WHEN GEAR DOWN SELECTED GEAR DISAGREE EICAS MSG APPEARED AND BEEPER SOUNDED. LIGHTS WERE MOMENTARY. REPLACED LT MLG ACTUATOR, CONFIRMED SLOW TO EXTEND.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 45,780 hrs · 14,583 cycles

INSPECTION TYPE:C09, FOUND BROKEN DAMAGE ON M/D CARGO FLOOR PANEL 232GFF AT BS 612, RBL 52.5-55. REPAIR IAW EO NO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 45,780 hrs · 14,583 cycles

INSPECTION TYPE:C09, FOUND BROKEN DAMAGE ON M/D CARGO FLOOR PANEL NR 242DFF AT BS 932-933, RBL 79-80. DIMENSIONS OF DENT: 1.25" X 1.0". REPAIR IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO) · airframe 45,780 hrs · 14,583 cycles

INSPECTION TYPE:C09, FOUND BROKEN DAMAGE ON M/D CARGO FLOOR PANEL 241AFF AT BS 825-828, RBL6-11. REPAIR IAW EO NO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL P7 HAS TWO HOLES IN CENTER. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK POS 7 HAS HOLE IN RT OTBD FLOOR PANEL. FABRICATED NEW FLOOR PANEL, REF EO B767-5320-9693-H.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL POS 8 HAS HOLE RT OTBD PANEL FWD END. REPAIRED IAW SRM 53-00-50-2R.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL HAS HOLE POS 10. REPAIRED IAW SRM 53-00-50-2R, PARA 4.C.

Part: FLOOR PANEL — DAMAGED (MAIN CARGO)

MAIN CARGO DECK FLOOR PANEL POS 10 HAS HOLE RT OTBD PANEL FWD END. REPAIRED IAW SRM 53-00-50-2R.

Part: FLAP SYSTEM — MALFUNCTIONED

ON APPROACH, T/E FLAP DISAGREE MESSAGE. RAN CHECKLIST. LANDED WITH FLAPS 27. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. T/E FLAP DISAGREE MESSAGE NO LONGER DISPLAYED. AFTER FIM TASK 27-51-00 FIG 114B C/O. FLAP FUNCTION CHECK C/O SATISFACTORY IAW AMM 27-51-00-5. FLAPS OPERATED NORMALLY.

Part: TRANSCEIVER — INOPERATIVE (WX RADAR)

WEATHER RADAR FAIL DISPLAYED ON BOTH LOWER CRT AND WX S/R. DISPLAYED ON STATUS MESSAGE ON CLIMB OUT AND CRUISE. RADAR ON WX MODE, AND RANGE MODE MORE THAN 40 WOULD GIVE WXR FAIL. REMOVED RADAR TRANSCEIVER AND REPLACED WITH KNOWN GOOD UNIT FROM AC 302UP (SERVICEABLE) IAW MM 34-43-01-401. OPS AND TEST GOOD IAW 34-43-00-5. OPERATED RADAR FOR 2.5 HR, NO FAULTS NOTED.

Part: CONTROL PANEL — INOPERATIVE (WX RADAR SYS)

WEATHER RADAR FAIL TRWS FORECAST ENROUTE. WEATHER RADAR FAILED ON HSI OK IN TEST. R & R WEATHER RADAR CONTROL PANEL IAW AMM 34-43-00-501.

Part: FAIRING — DELAMINATED (RT WING TE FLAP) · airframe 41,319 hrs · 13,091 cycles

INSPECTION TYPE:8C, RT WING INBD MAIN FLAP OTBD L/E FAIRING. FIBREGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG5, REV50, 121 DEGREE/CURE.

Part: FAIRING — DELAMINATED (LT WING TE FLAP) · airframe 41,319 hrs · 13,091 cycles

INSPECTION TYPE:8C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBREGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG5, REV50, 121 DEGREE/CURE.

Part: FAILSAFE — CRACKED (BS 955 BULKHEAD) · airframe 41,319 hrs · 13,091 cycles

INSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FTG WAS FOUND 1EA FASTENER HOLE CRACKED AT FAIL SAFE STRAP ON 4 & 10 O/C POSITION THROUGH THICKNESS. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-I, APPENDIX 'D' ORG MAT'L IS 2024T351-0750" MACHINED STRAP, CRACK ON 4 & 10 O/C POSITION THROUGH THICKNESS, FINAL CUTOUT SIZE IS 7.75" X 2" THIS REPAIR IS CLASSIFIED AS A MAJOR RPEAIR.

Part: TEE FITTING — CRACKED (BS 955 BULKHEAD) · airframe 41,319 hrs · 13,091 cycles

INSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FTG WAS FOUND 1EA FASTENER HOLE CRACKED AT TEE FITTING ON 9 O/C POSITION APPROX .1250" IN LENGTH. TEE FITTING REPLACED AND INSTALLED IAW EO B767-5350-17922-I, APPENDIX 'D', FIG 6, ORG MAT'L IS 7075-T73 DIE FORGING, CRACK ON 9 O/C POSITION APPROX .1250" IN LENGTH, THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: TEE FITTING — CRACKED (BS 955 BULKHEAD) · airframe 41,319 hrs · 13,091 cycles

INSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG WAS FOUND 1EA FASTENER HOLE CRACKED AT 'T' FTG ON 3 O/C POSITION APPROX .1250" IN LENGTH FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG AREA 'T' FITTING REPLACED AND INSTALLED IAW EO NR B767-5350-17922-I APPENDIX 'C' FIG 6, ORG MAT'L IS 7075-T73 DIE FORGING, CRACK ON 3 O/C POSITION APPROX .1250" IN LENGTH THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: FAILSAFE — CRACKED (BS 955 BULKHEAD) · airframe 41,319 hrs · 13,091 cycles

INSPECTION TYPE:C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG WAS FOUND 1EA FASTENER HOLE CRACKED AT FAIL STRAP ON 2 O/C POSITION THROUGH THICKNESS FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FTG FAIL SAFE STRAP REPLACED IAW EO NR B767-5350-17922-I, APP 'C' ORG MAT'L IS 2024T351-0750" MACHINED STRAP , CRACK ON 2 O/C POSITION THROUGH THICKNESS FINAL CUTOUT SIZE IS 7.75" X 2" THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: FAILSAFE — CRACKED (BS 955 BULKHEAD) · airframe 41,319 hrs · 13,091 cycles

INSPECTION TYPE: C, FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING FAIL SAFE STRAP AREA SUSPECT CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. FUSELAGE LT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP AT MOST LOWER FASTENER. R & R IAW EO NR B767-5350-17922-I, APPENDIX C, FIG 6 FOR FURTHER CONFIRMATION BY NDT INSPECTION, THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: FAILSAFE — CRACKED (BS 955 BULKHEAD) · airframe 41,319 hrs · 13,091 cycles

INSPECTION TYPE:C, FUSELAGE RT BS 955 REAR SPAR BULKHEAD FTG FAIL SAFE STRAP AREA SUSPECT CRACK FOUND, REMOVE FASTENER FOR NDT CONFIRMATION. FUSELAGE RT BS 955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP AT MOST LOWER FASTENER REMOVED AND REINSTALLED IAW EO B767-5350-17922-I, APPENDIX 'D', FIG 6 FOR FURTHER CONFIRMATION BY NDT INSP, THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 41,319 hrs · 13,091 cycles

INSPECTION TYPE:8C COCKPIT: EMERGENCY LIGHT BATTERY PACK CAPACITY TEST FAILED. COCKPIT EMERGENCY LIGHT BATTERY PACK REPLACED AND LIGHT OPS CHECKED NORMAL, REF AMM 33-51-07.

Part: FLOOR PANEL — DAMAGED (BS 764-873) · airframe 41,319 hrs · 13,091 cycles

INSPECTION TYPE:8C, FLOOR PANEL FOUND 10 PUNCTURES AND 6 DENTS MARKS AT STA 764 TO 873, LBL 77 TO 88. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-H AND INSTALLED AMM 53-01-01.

Part: CHARGER — INOPERATIVE (MAIN BATTERY)

AT CRUISE ALT (350) STATUS MSG, MAIN BATTERY CHARGER. T/S C/O, FOUND MAIN BATTERY CHARGER AT FAULT. R & R MAIN BATTERY CHARGER IAW AMM 24-31-02-4, REV 49.1 12/22/10. OPS CHECKED OK.

Part: FLOOR PANEL — DAMAGED (BS 610)

MCD POS 4 CTR FWD FLOOR PANEL REPAIR, STA 610 BL0 WL200. REPLACED FLOOR PANEL IAW EO B767-5320-09793-G.

Part: FLOOR PANEL — DAMAGED (BS 390)

REF D 427434, P2 LT AFT HAS INTERIM REPAIR TO HOLE 1.75 DIA. (STA 390, LBL 62) REPLACED FLOOR PANEL IAW EO B767-5320-09793-G.

Part: FLOOR PANEL — DAMAGED (BS 654)

REF D412069 MCD FLOOR PANEL 4L AFT AREA SECOND PANEL FROM OTBD (STA 654+ 110, LBL 65) HAS 3/4" HOLE. REPLACED FLOOR PANEL IAW EO B767-5320-09793-G.

Part: ACTUATOR — LEAKING (NR 8 SPOILER)

ATB - C HYD QTY DECREASED TO ZERO AND SYS PRESS LIGHT ILLUM. EICAS MSG C HYD SYS PRESS AND C HYD QTY DISPLAYED. FOUND NR 8 INBD SPOILER ACTUATOR LEAKING AT FILTER CASE. REPLACED O'RING IAW AMM 27-61-02-4. SERVICED C HYD SYS 12-12-01-3. LEAK CKD OK.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT MID AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT MID AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT O/B AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.

Part: HINGE FITTING — CRACKED (TE FLAP) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:N/A RIGHT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG FOUND CRACKED. INBOARD FLANGE CRACK LENGTH 1.5 INCH, OUTBOARD FLANGE CRACK LENGTH 0.875 INCH. RIGHT WING I/B MAIN FLAP I/B AFT FLAP HINGE FTG REPAIRED AS PER SRM 57-53-02 -2R1 FIG 201 REV 45. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL AND10134-2007 7075T6 AS REPAIR ANGLE REPAIR SIZE 2 X 4 INCHES ORG MATERIAL 7075T73 DIE FORGING, CUTOUT SIZE 0.75 X 1.5 INCH AT BOTH FLANGES.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C SURVEY SEQ 312-F1-07 FX BETWEEN BS 1197+72 TO BS 1197+88 AND STR 19L - 21L EXISTING REPAIR FASTENER HOLES 3EA DRILLED & INSTALLED AT MACHINED RADIUS AREA. FX BETWEEN BS 1197+72 - 1197+88 & STR 19L-21L, ORG MAT'L 202473-0.200IN MACHINED SKIN WITH REPAIR DOUBLER 202473-0.063IN & REPAIR SIZE 9 X 11.875 INCHES EXISTING REPAIR FASTENER HOLES 3EA AT MACHINED RADIUS AREA REWORKED & FASTENERS 3EA INSTALLED IAW HX RS R53-00-36436 REV A & REPEAT INSP REQUIRED REF EO B767-5330-35079-A.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION AT O/B AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.

Part: SLAT — DAMAGED (RT WING) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C RT WING NR 9 SLAT O/B EDGE FOUND DAMAGED. METAL HOT BOND REPAIR PERFORMED AS PER SRM 51-70-10 REPAIR 4 FIG 202 SHT 8 REV 45.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C SURVEY SEQ 312-F1-06 FX BETWEEN BS 442-463 AND STR 23R - 27R EXISTING REPAIR DOUBLER HAS MANY ABRASIVE SANDING LINES, DEEP COUNTERSUNK FOUND AT SEVERAL LOCATIONS. AT THE EDGE OF REPAIR DOUBLER, FX BETWEEN BS 442-463 & STR 23R-27R EXISTING CUTOUT 2.25" X 3.125" & 0.875" X 1.875" RESP OF ORG MACHINED SKIN 2024T3 AT CUTOUT 0.063". REPAIRED IAW HX RS R53-00-36433 REV A THIS CLASSIFIED A MAJOR CATEGORY B REPAIR WITH MATERIAL 2024T3-0071IN AS DOUBLER (REPAIR SIZE 14.5" X 23.375") REPEAT INSP REQUIRED REF EO B767-5330-35075-A FOR DETAIL.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1425 TO 1540 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: DOUBLER — DELAMINATED (TE FLAP) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP L/E AREA THE EXISTING REPAIR PATCH DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5C FIG 2 REV 45.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C RIGHT WING NR 9 SLAT O/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RIGHT WING NR 9 SLAT O/B AREA AT OSS 641.49 NOSE SKIN CUT 7.375 X 9 INCHES REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45, THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075T6-0071IN AS DOUBLER 7075T6-0063IN AS REPAIR PLATE. REPAIR SIZE 10.5 X 12 INCHES ORG SKIN MATERIAL 7075T6-063IN.

Part: PANEL — DELAMINATED (LE SLAT) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C LT WING NR 6 SLAT LOWER CLOSURE PANEL. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 45.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:N/A RIGHT WING NR 10 SLAT I/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RIGHT WING NR 10 SLAT I/B AREA AT OSS 724.6 NOSE SKIN CUT 7.125 X 9 INCH REPAIR AS PER SRM 57-43-01-2R2 FIG 201 REV 45, THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075T6-0071IN AS DOUBLER, 7075T6-0063IN AS REPAIR PLATE. REPAIR SIZE 10.25 X 12 INCHES ORG SKIN MATERIAL 7075T6.063IN.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C LT WING I/B MAIN FLAP I/B AFT FLAP SUPPORT FTG FLANGE FOUND CRACKED. INBOARD FLANGE CRACK LENGTH 1.5 INCH, OUTBOARD FLANGE CRACK LENGTH 0.625 INCH. LEFT WING I/B MAIN FLAP I/B AFT FLAP SUPPORT FTG REPAIRED AS PER SRM 57-53-02-2R1, FIG 201 REV 45. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL AND10134-2007 7075T6 AS REPAIR ANGLE REPAIR SIZE 2 X 4 INCHES ORG MATERIAL 7075T73 DIE FORGING, CUTOUT SIZE 0.75 X 1.5 INCH AT BOTH FLANGES.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C RIGHT WING NR 9 SLAT I/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. RIGHT WING NR 9 SLAT I/B AREA AT OSS 573.25 NOSE SKIN CUT 7.375 X 9 INCHES REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075T6-0071IN AS DOUBLER, 7075T6-0063IN AS REPAIR PLATE. REPAIR SIZE 10.625 X 12 INCHES ORG SKIN MATERIAL 7075T6.063IN.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C LEFT WING O/B TRAILING EDGE FLAP MID L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 45.

Part: SKIN — CRACKED (LE SLAT) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C LEFT WING NR 3 SLAT I/B NOSE SKIN RIVET HOLE FOUND CRACKED. CRACK LENGTH 0.125 INCH. LEFT WING NR 3 SLAT I/B AREA AT OSS 724.61 NOSE SKIN CUT 9 X 7.125 INCHES REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 45. THIS REPAIR CLASSIFIED AS MAJOR REPAIR WITH MATERIAL 7075T6-0071IN AS DOUBLER 7075T6-0063IN AS REPAIR PLATE. REPAIR SIZE 10.25 X 12 INCHES ORG SKIN MATERIAL 7075T6.063IN.

Part: SKIN — DAMAGED (E&E DOOR) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C SURVEY SEQ 312-F1-05 E&E DOOR RT FWD CORNER SKIN AT BETWEEN BS 305-311 AND STR 38R - 39R AREA SEM WAS FOUND AT SKIN CUTOUT. FX E&E DOOR EXTERIOR SKIN AT BETWEEN BS 305 TO BS 323.5 STR 38L-38R AREA REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.

Part: ANGLE — CRACKED (LT WING) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C LT WING - L/E LES 160 UPPER AREA FRONT SPAR ANGLE FOUND CRACKED. CRACK LENGTH 0.75 INCH. LT WING L/E LES 160 UPPER AREA FRONT SPAR ATTACH ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.

Part: DOUBLER — DELAMINATED (SPOILER) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C RT WING NR 8 SPOILER T/E LOWER SURFACE THE EXISTING REPAIR PATCH DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-04 PAR 5G FIG 9 REV 45.

Part: DOUBLER — DELAMINATED (LE SLAT) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C LT WING NR 3 SLAT LOWER CLOSURE PANEL THE EXISTING REPAIR PATCH DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 45.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C LT WING O/B TRAILING EDGE FLAP T/E WEDGE LOWER SURFACE THE EXISTING REPAIR PATCH DELAMINATED. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A (1) FIG 9 REV 45.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 540 TO 654+22 LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 283 TO 412, RBL 55 TO RBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:7C AFT CARGO COMPT STA 1087 FLOOR PANEL SUPPORT CLIP FOUND CRACK AT LBL 25. AFT CARGO COMPT STA 1087 FLOOR PANEL SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT LBL 25.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 283 TO 412 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 520 , RBL 77 TO RBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 930 TO 975, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1370 TO 1480 RBL 77 TO RBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 731 TO 833, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 540 LBL 33 TO LBL 55. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 545, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:7C AFT CARGO COMPT STA 1087 FLOOR PANEL SUPPORT CLIP FOUND CRACK AT RBL 25. AFT CARGO COMPT STA 1087 FLOOR PANEL SUPPORT CLIP REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-10-02 REV 45 JUST AT RBL 25.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1344 TO 1480 RBL 33 TO RBL 55. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 873 TO 933, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1344 TO 1480, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGE AT STA 654+22 TO 690, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 985 TO 1090, LBL 77 TO LBL 88. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 412 TO 540, LBL 11 TO RBL 11. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND DAMAGED AT STA 1197+22 TO 1207 LBL 55 TO LBL 77. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MCD FLOOR PANEL FOUND CRACKED AT STA 930 TO 975 LBL 11 TO LBL 33. FLOOR PANEL FABRICATED PER EO B767-5320-9693-F & INSTALLED PER AMM 53-01-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM CLIP AT LBL 50 FOUND CRACKED. CRACK LENGTH 1 INCH. MEC COMPT BS 246 FLOORBEAM AT LBL 50 ATT CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.

Part: FITTING — CRACKED (FUSELAGE) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM CLIP AT RBL 10 FOUND CRACK. CRACK LENGTH 1.5 INCH. MEC COMPT BS 246 FLOORBEAM AT RBL 10 ATTACHED CLIP REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.

Part: SKIN — NONE · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE: C, SURVEY SEQUENCE NR 312-F1-05 BS 305 -311, STR 38R - 39R E&E DOOR RT FWD CORNER SKIN EXISTING REPAIR PATCH WAS FOUND. SURVEY SEQ NR 312-F1-05 FX E&E DOOR EXTERIOR SKIN AT BETWEEN BS 305 TO BS 323.5 STR 38L - 38R AREA REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02 REV 45

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,143 hrs · 11,473 cycles

INSPECTION TYPE:C MEC COMPT STA 246 FLOORBEAM ANGLE AT LBL 25 FOUND CRACKED. CRACK LENGTH 0.5 INCH. MEC COMPT BS 246 FLOORBEAM AT LBL 25 ATTACHED ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REV 45.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A MCD FLOOR PANEL POS 10 CTR DAMAGED. REPAIRED PER EO B767-5320-34306-A.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A MCD FLOOR PANEL POS 7 CTR DAMAGED. REPAIRED PER EO B767-5320-34305-A.

Part: FLOOR PANEL — DAMAGED (CARGO BAY)

INSPECTION TYPE:N/A MCD POS 4 CTR FLOOR PANEL DAMAGED. REPAIRED PER EO B767-5320-34304-A.

Part: SKIN — DAMAGED (BS 456)

FUSELAGE SKIN DAMAGE AT BS 456 BETWEEN S25R AND S26R. REPAIRED IAW EO B767-5330-25673-F.

Part: FLOOR PANEL — DAMAGED (POS 14L)

FLOOR PANEL POS 14 DAMAGED. REPAIRED IAW EO B767-5320-33802-A.

Part: FLOOR PANEL — DAMAGED (FUSELAGE)

FLOOR PANEL POS 10 DAMAGED. REPAIRED IAW EO B767-5320-33803-A.

Part: STATIC INVERTER — MALFUNCTIONED (E&E BAY)

INSPECTION TYPE:ETOP DURING PS-CHECK, STARTING APU MECHANIC NOTICED SMOKE IN COCKPIT. FURTHER INVESTIGATION FOUND STATIC INVERTER IN E3 RACK CAUGHT FIRE. REMOVED STATIC INVERTER AND FIRE HAD BEEN EXTINGUISHED BY FIRE FIGHTER, NO DAMAGED ADJACENT COMPONENT.

Part: WINDOW — DELAMINATED (COCKPIT)

INSPECTION TYPE:N/A DIVERSION - R2 WINDOW HAS DELAMINATION APPROX 3 INCHES HIGH COVERING THE LOWER FORWARD HALF OF THE WINDOW. SLIGHT DISTORTION OF VIEW. DISCOVERED AFTER AIRBORNE. REVISED AND REPLACED R2 WINDOW ASSY AS REQ'D PER 50-11-02-40. OPS AND LEAK CHECK GOOD.

Part: POWER SUPPLY — DISCHARGED (COCKPIT)

INSPECTION TYPE:PS1 EMERGENCY LIGHTS ARE INOP WITH NO PWR. REMOVED AND REPLACED PWR SUPPLY UNIT IAW MM 33-51-07-2, SYSTEM OPS CHECKS NORMAL.

Part: LIFE RAFT — UNSERVICEABLE (COCKPIT)

INSPECTION TYPE:N/A DURING PS CHECK, FOUND LIFE RAFT UNSERVICEABLE. REMOVED AND REPLACED LIFE RAFT PER MM 25-62-00-0.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR)

INSPECTION TYPE:ETOP WEATHER RADAR WOULD NOT TEST. REMOVED AND REPLACED R/T UNIT. OPS TEST OK PER MM 34-43-01-4.

Part: INDICATOR — INOPERATIVE (STANDBY ATTITUDE)

INSPECTION TYPE:ETOP STAND BY ATTITUDE INDICATOR IS ABNORMAL IN ROLL MODE. GYRO FLAG RETRACTED. REMOVED AND REPLACED SAI PER AMM 34-24-01-2.

Part: ENGINE — INOPERATIVE (APU)

INSPECTION TYPE:ETOP APU WILL NOT START. T/S PER FIM 49-11-00 FIG 104. RESET APU ECU POWER, APU RUN UP OPS CHECK NORMAL.

Part: SKIN — DAMAGED (BS 434 S26R)

ON PRE-DEPARTURE, WALK AROUND FOUND SKIN DAMAGE ON SKIN SECTION 43, 5.3125" ABOVE SKIN LAP S26R 16.75" AFT OF STA 434.00. REMOVED DAMAGED EXISTING DOUBLER REF B767 SRM 51-40-02. CW EO B767- 5330-25673.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

MAIN ENTRY EMERGENCY LIGHT INOPERATIVE. REPLAMPED EMERGENCY LIGHT.

Part: ENGINE — FAILED (NR 2)

RT ENGINE FAILURE ON TAKE OFF. REPLACED NR 2 ENGINE, TESTED AND OPERATED NORMAL.

Part: CONTROL PANEL — DEFECTIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHT SWITCH INWARDS MISSING SWITCH DOES NOT ARM AUTO WHEN CLOSING GUARD. WORKS OK MANUALLY. REMOVED AND REPLACED EMERGENCY LIGHT PANEL ASSY. OPS CHECKS GOOD.

Part: LINE — FAILED (LT MLG BRAKE)

INSPECTION TYPE:N/A, TAXI IN - LT MLG BRAKE FIRE DUE TO FAILED BRAKE LINE. REF L/P 518977 ITEM 2 THRU L/P 518992 REMOVED AND REPLACED PARTS AS REQUIRED.

Part: BRAKE — BURNED (NR 3)

NR 3 MAIN BRAKE CAUGHT ON FIRE AFTER ARRIVAL. FOUND TO BE ONLY GREASE ON BRAKE BURNING. PUT OUT FIRE. REPLACED TIRE ASSY PRECAUTIONARY. PLACARDED NR 3 BRAKE INOP PER MEL.

Part: FIRE LIGHT — ILLUMINATED (NR 2 ENGINE)

FIRE PROTECTION SYS FAIL LIGHT ILLUM. EICAS MSG FIRE/OVHT SYS DISPLAYED. LP1 MOMENTARILY ON AND OFF FOR ABOUT 30-40 SECS, THEN ONLY LP2 OCCURRED AT TOP OF DESCENT. NR 2 ENG NR 2 LOOP PREVIOUSLY DEFERED. T/S NR 1 LOOP PER FIM 26-11-00, BITE CHECK GOOD. INSPECTED LOOPS AND ENG DUCTING NO DEFECTS NOTED WORK PERFORMED BY NON ETOPS QUALIFIED MECH. DEF NR C159742.

Part: STANDBY ATT IND — GROUNDED (INSTRUMENT PNL.)

INSPECTION TYPE-N/A ON TAKEOFF AT 40 KTS GPWS PULL UPLIGHT AND MASTER WARN LIGHT ILLUM. WARNING LTS COME ON/OFF MOVING STANDBY ATT IND CAGE KNOB. REPOSITION WIRES IN AREA OF SAI BEHIND WARN LTS. REPLACED SAI, UNABLE TO GET WARN LTS ON. SUSPECT CASE GROUND, SAI OP CK NORM PER MM34-24-00.

Part: EICAS SCREEN — SMOKING (COCKPIT)

UPPER EICAS SCREEN INTERMITTENT. BLANKS. ELECT. SMOKE SMELL IN COCKPIT IN FLIGHT ONLY. RESEATED UPPER EICAS SCREEN. NO DEFECTS NOTED. NO EVIDENCE OF SMOKING NOTED, NO DEFECTS NOTED. OK FOR SERVICE.