N839MH

Part: SPAR WEB — NOT REPORTED (ZONE 400) · airframe 98,672 hrs · 17,256 cycles

FOUND EXISTING REPAIR AT LT PYLON STRUT FORWARD MID SPAR WEB AT NSTA 221.25. REPAIR DESCRIPTION DETAILED IN THE COMMENTS SECTION OF ER/A 585425-14. (1374601)

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 98,672 hrs · 17,256 cycles

FOUND CABIN FLOORBEAM LOWER SURFACE CRACK AT BS 1439 AND LBL25. CRACK AREA AT STA 1439 LBL25 REPAIRED AS PER PRI 630972-14 REV 0. (1374435)

Part: SPAR WEB — CRACKED (ZONE 400) · airframe 98,672 hrs · 17,256 cycles

DURING HCK AT STAG, A CRACK WAS NOTED ON THE NR 2 PYLON FWD UPPER SPAR WEB. REF TO ER/A 617658-14 FOR REPAIR. (1370726)

Part: WEB — CRACKED (ZONE 400) · airframe 98,672 hrs · 17,256 cycles

FOUND NR 1 PYLON UPPER WEB CRACKED AT OTBD SIDE OF PYLON TO WING INBD MID SPAR FITTING. REPAIRED AS PER PRI 630868-14 (1368270)

Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 98,672 hrs · 17,256 cycles

FUSELAGE SKIN BTW STA1395 AND STA1417, S35R TO S36R WHERE AFT DRAIN MAST INSTALLED FOUND CORROSION. THE DAMAGED SKIN REPAIRED AS PER PRI 631040-14 REV 0.COMAPRED AND COMPLIED WITH ER/A 631040-14 REV ORIGINAL. (1368590)

Part: SPAR WEB — CRACKED (ZONE 400) · airframe 98,672 hrs · 17,256 cycles

A CRACK WAS FOUND ON THE NR 1 PYLON AFT MID SPAR WEB. REPAIRED PER ER/A 74-630868. (1368070)

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 98,672 hrs · 17,256 cycles

CABIN SEAT TRACKS FOUND SURFACE CORROSION AT STA1208 TO STA1428,RBL88.5. REPAIRED AS PER PRI 630867-14 REV 0,COMPARED AND COMPLIED WITH ER/A 630867-14 (1364888)

Part: ACCESS PANEL — DELAMINATED (ZONE 600 FLAP) · airframe 98,672 hrs · 17,256 cycles

FOUND RT WING OTBD FLAP UPPER ACCESS PANEL 666MT, OTBD AREA DELAMINATED. DAMAGED AREA REPAIRED IAW SRM 57-53-01-2R-1, SRM 51-70-10-2R-4, FIG 201, & SRM 51-70-10. (1349215)

Part: ACCESS PANEL — DELAMINATED (ZONE 600 FLAP) · airframe 98,672 hrs · 17,256 cycles

FOUND RT WING OTBD FLAP UPPER ACCESS PANEL 666KT INBD AREA DELAMINATED. DAMAGED AREA REPAIRED IAW SRM 57-53-01-2R-1, SRM 51-70-10-2R-4 FIG201, & SRM 51-70-10 (1349207)

Part: SKIN — DELAMINATED (ZONE 600 SLAT) · airframe 98,672 hrs · 17,256 cycles

FOUND RT WING NR 12 SLAT UPPER SURFACE INBD AREA DELAMINATED. DAMAGED AREA REPAIRED IAW SRM 57-43-02-2R-1, SRM 51-70-10-2R-4, FIG 201, & SRM 51-70-10. (1349204)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 98,672 hrs · 17,256 cycles

FOUND BULK CARGO BAY SHEAR TIE CORRODED AT BS 1417, S38 - 39R. DAMAGED AREA REPAIRED IAW SRM 53-00-07. (1347719)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 98,672 hrs · 17,256 cycles

FOUND BULK CARGO BAY SHEAR TIE CORRODED AT BS 1417, S37R TO S38R. DAMAGED AREA REPAIRED IAW SRM 53-00-07 (1347712)

Part: SKIN — DAMAGED (ZONE 200) · airframe 98,672 hrs · 17,256 cycles

LEFT FUSELAGE SKIN AT BS 1730, WL 200 FOUND AN ABRASION. DAMAGED AREA REPAIRED IAW SRM 53-80-70. (1342749)

Part: SKIN — DAMAGED (ZONE 200) · airframe 98,672 hrs · 17,256 cycles

SECTION 48 AT BS 1735, WL 200 RT SKIN FOUND AN ABRASION. DAMAGED AREA REPAIRED IAW SRM 53-80-70. (1342752)

Part: SKIN — DAMAGED (ZONE 200) · airframe 98,672 hrs · 17,256 cycles

RT FUSELAGE SKIN AT BS 1730 WL 200 FOUND AN ABRASION. DAMAGED AREA REPAIRED IAW SRM 53-80-70 (1342733)

Part: SKIN — DAMAGED (ZONE 200) · airframe 98,672 hrs · 17,256 cycles

SECTION 48 AT BS 1735, WL 200 LT SKIN FOUND AN ABRASION. DAMAGED AREA REPAIRED IAW SRM 53-80-70. (1342740)

Part: SKIN — DAMAGED (ZONE 300) · airframe 98,672 hrs · 17,256 cycles

VERTICAL STABILIZER LT SKIN PANEL DAMAGED AT ABOUT BTW FSS170 AND FSS195. DAMAGED AREA REPAIRED PER B767-400 SRM 55-30-01-2R-1 AND SRM 51-70-10-2R-4 FIG 203 AND SRM 51-70-10 (1341308)

Part: SKIN — CRACKED (ZONE 200) · airframe 98,672 hrs · 17,256 cycles

TWO CRACKS FOUND ON THE RT FUSELAGE SKIN SECTION 48, BETWEEN BS 1629 & 1654.5 BELOW THE S14AR, ONE CRACK AT THE 13TH RIVET & ANOTHER ONE CRACK AT THE 17TH RIVET COUNTED FROM BS 1654.5 BELOW THE S14AR, BOTH CRACKS LENGTH WERE APPROXIMATELY 0.197 INCH. DAMAGED AREA REPAIRED IAW SRM 53-80-01. (1341150)

Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 98,672 hrs · 17,256 cycles

FOUND FWD CARGO BAY SHEAR TIE CORRODED AT THE BS 654+22 AND S39L TO S39R. DAMAGED AREA REPAIRED IAW SRM 53-00-07. (1340903)

Part: STIFFENER — CRACKED (ZONE 100) · airframe 98,672 hrs · 17,256 cycles

MFEC INSPECTION FOUND ONE CRACK AT NOSE WHEEL WELL RT VERTICAL STIFFENER BS 287, BL 25 AND WL 172. PEFORMED REPAIR ON NOSE WHEEL WELL RT VERTICAL STIFFENER AT BS 287, BL 25, AND WL 172 CRACKED AREA, REFER TO W/C 5312-01186-02B. (1334592)

Part: SIGN — INOPERATIVE (ZONE 200) · airframe 98,393 hrs · 17,215 cycles

EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS: 3R. C/W ERA 625342-14TR. (1253654)

Part: BATTERY — NO TEST (ZONE 200) · airframe 96,902 hrs · 16,995 cycles

SHIP 1815 LOWER EMERGENCY PATH LIGHTS ON RT SIDE ROWS 32-38 INOP. CORRECTIVE ACTION: SWAPPED WITH KNOWN GOOD BATTERY. FAULT FOLLOWED. R/R EMERGENCY BATTERY PACK (M732) PER B767-400 AMM 33-51. (7068480)

Part: COVER — BROKEN (ZONE 800 SLIDE) · airframe 96,686 hrs · 16,963 cycles

SHIP 1815 1L ENTRY DOOR SLIDE COWLING BROKEN. CORRECTIVE ACTION: R/R 1L ENTRY DOOR SLIDE IAW W/C 5200-4473. (7058494).

Part: PAWL — FAULTED (ZONE 800) · airframe 94,816 hrs · 16,694 cycles

SHIP 1815 DELAY FOLLOWUP SET UO TO CHECK THE 2R SERVICE DOOR FOR CORRECT OPERATION AND ARMING. BCN TOOK A DELAY - HAD DIFFICULTY CLOSING AND ARMING THE 2R DOOR. CORRECTIVE ACTION: R/R 2R DOOR PAWL REF B767-400 AMM 52-11, CLOSE + ARM 2R DOOR SEVERAL TIMES WITH NO DIFFICULTY. (0765697)

Part: GIRT BAR — FOD (ZONE 800) · airframe 94,556 hrs · 16,656 cycles

SHIP 1815 ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS:607. CORRECTIVE ACTION: FOUND BROKEN SCREW IN DOOR SILL GIRT BAR RECEPTICLE. OPS CHECK GOOD. (0737325)

Part: AOA — FAULTED (ZONE 100) · airframe 94,325 hrs · 16,620 cycles

SHIP 1815 -DIV- TO CDG. LOSS OF A/T, LNAV AND VNAV. V/S AND HDG SEL FUNCTIONAL. CORRECTIVE ACTION: C/W OVERWEIGHT LANDING INSP. REPLACED AOA SENSOR. PERFORMED TAT TEST. OK FOR SERVICE. (5789234)

Part: LIGHT SYS — INOPERATIVE (ROW 50-56 RH SID) · airframe 94,194 hrs · 16,601 cycles

SHIP 1815 EMERGENCY PATH LIGHTS INOP ROW 50-56 RH SIDE. CORRECTIVE ACTION: R/R BATTERY PACK M734. IAW B767 AMM 33-51. OPS CHK GOOD (6617949)

Part: SIGN — DETACHED (ZONE 200) · airframe 93,543 hrs · 16,513 cycles

SHIP 1815 DOOR 3R EXIT SIGN HAS FALLEN OUT OF PLACE. CORRECTIVE ACTION: RESECURED 3R EXIT SIGN AS REQUIRED PER B767-400 AMM 33-51 A/C OK FOR SVC (6394512)

Part: WEB — CRACKED (VERTICAL STAB) · airframe 91,540 hrs · 16,259 cycles

SHIP 1815 FOUND OUT VERTICAL STABILIZER LE WEB CRACKED AT FSS109. CORRECTIVE ACTION: THE CRACKED WEB AT VERTICAL STABILIZER L/E AT FSS109 REPAIRED AS PER PRI 617724-14 REV 0.COMPARED AND COMPLIED WITH ER/A 617724- 14 REV ORIGINAL. NO DEVIATION. (0328449)

Part: STRUCTURE — CRACKED (LT NACELLE) · airframe 91,540 hrs · 16,259 cycles

SHIP 1815 FOUND LH NACELLE STRUT FWD UPR SPAR CUTOUT CRACK AT NAC STA 230. CORRECTIVE ACTION: THE CRACK ON LH NACELLE STRUT FWD SPAR CUTOUT AT NAC STA 230 REPAIRED AS PER PRI 617659-14, COMPARED AND COMPLIED WITH ER/A 617659-14 (0326995)

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 91,540 hrs · 16,259 cycles

SHIP 1815 FOUND OUT LH VERTICAL STABILIZER SKIN DELAMINATION AT 60 INCHES TO LE AND 50 INCHES TO LOWER EDGE. CORRECTIVE ACTION: LH VERTICAL STABILIZER SKIN REPAIRED AT 60 INCHES TO LE AND 50 INCHES TO LOWER EDGE AS PER PRI 585586-14.REV.0.THE PRI 585586- 14.REV.0 COMPAIRED AND COMPLIANCE WITH ER/A 585586-14. (0326998)

Part: TUBE — LEAKING (HYD SYSTEM) · airframe 91,540 hrs · 16,259 cycles

SHIP 1815 FOUND RH NACELLE STRUT FWD UPR SPAR HYDRAULIC TUBE HOLE CUTOUT CRACK AT NAC STA 230. CORRECTIVE ACTION:RH NACELLE STRUT FWD UPR SPAR HYDRAULIC TUBE HOLE CUTOUT CRACK AREA AT NAC STA 230 REAPIRED AS PER PRI 617658-14 REV 0. COMPARED AND COMPLIED WITH ER/A 617658-14 (0322280)

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 91,540 hrs · 16,259 cycles

SHIP 1815 FOUND OUT RH VERTICAL STABILIZER SKIN DELAMINATION AT 30 INCHES TO LE AND 106 INCHES TO LOWER EDGE. CORRECTIVE ACTION: RH VERTICAL STABILIZER SKIN REPAIRED AT 30 INCHES TO LE AND 106 INCHES TO LOWER EDGE AS PER B767-400 SRM 51-70-10 (0321050)

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 91,540 hrs · 16,259 cycles

SHIP 1815 FOUND OUT RH VERTICAL STABILIZER SKIN DELAMINATION AT 28 INCHES TO LE AND 72 INCHES TO LOWER EDGE. CORRECTIVE ACTION: RH VERTICAL STABILIZER SKIN REPAIRED AT 28 INCHES TO LE AND 72 INCHES TO LOWER EDGE AS PER B767-400 SRM 51-70-10-2R-4. (0321057)

Part: SPAR — CRACKED (NR 1 NACELLE) · airframe 91,540 hrs · 16,259 cycles

SHIP 1815 DURING CCK AT STAG, A CRACK WAS FOUND ON THE #1 ENGINE PYLON UPPER SPAR WEB BETWEEN NSTA221.25 AND 237.5. A REPAIR WAS INSTALLED PER ER/A 617659-14 SECTION I. CORRECTIVE ACTION: ACCOMPLISH ER/A 617659-14 SECTION II REPEAT INSPECTIONS (0321418)

Part: GIRT BAR — FOD (R4 DOOR) · airframe 90,933 hrs · 16,182 cycles

SHIP 1815 DOOR 4R SLIDE LEVER STUCK IN MIDDLE POSITION. CORRECTIVE ACTION: DOOR 4R DEBRIS CLEANED FROM GIRT BAR TRACK , TESTED OK (5827026)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,675 hrs · 16,025 cycles

SHIP 1815 EMERGENCY LIGHT ACTIVATED WHEN YOU CLOSE THE GUARD AND THE SWITCH MOVES TO OFF.HAD TO LEAVE THE GUARD OPEN WITH THE SWITCH TO ARM POSITION. CORRECTIVE ACTION: GUARD ADJUSTED.OPERATIONAL TEST WITH THE CONTROL SWITCHES NOW OK IAW B764 AMM 33-51-00 (5062460)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 89,577 hrs · 16,012 cycles

SHIP 1815 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:1D. CORRECTIVE ACTION: ALL DELTA ONE TTL AND EMERGENCY LIGHTS CHECKED, ALL OPS OK. (0046150)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,922 hrs · 15,920 cycles

SHIP 1815 EMERGENCY EXIT SIGN AT THE 3 L DOOR IS LOOSE. TIME LIMITED REPAIR PERFORMED PER ER/A 612217-14 REV ORIGINAL.REPETITIVE INSPECTION RQD EVERY DAY WITH TERMINATING ACTION IN 10 DAYS.A/C OK FOR SERVICE. PREFORM PERMANENT REPAIR PER ERA 612217-14 REV ORIG.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,782 hrs · 15,901 cycles

SHIP 1815 CREW REST LLCR EMER LIGHTS FAIL TEST.CORRECTIVE ACTION: REPLACED LLCR EMER LIGHTS POWER SUPPLY AND BATTERY PER B767 AMM 33-51. OPS OK. (4570844)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,100 hrs · 15,811 cycles

SHIP 1815 - GEAR - ALTERNATE GEAR EXTEND SYSTEM USED TO LOWER LANDING GEAR AFTER MAIN GEAR DID NOT DISPLAY DOWN AND NOSE GEAR INDICATIONS NORMAL DURING INITIAL AND SECOND ATTEMPT. ALL GEAR DOWN AND LOCKED. CORRECTIVE ACTION: REPLACED MLG SELECTOR/BYPASS VALVE V652. (LP 4914038)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,082 hrs · 15,809 cycles

SHIP 1815 -ATB- TO JFK DUE TO BUMPING NOISES REPORTED FROM AFT CARGO AREA. CORRECTIVE ACTION: EMPTY AND UNSECURED CARGO CONTAINER FOUND IN AFT CARGO UPON ARRIVAL. C/W OVERWEIGHT LANDING INSPECTION. A/C RTS. (LP 4914030)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,896 hrs · 15,784 cycles

SHIP 1815 2R SLIDE ARMED LIGHT INOP. CORRECTIVE ACTION: FOUND LIGHT BODY LOOSE. ADJUSTED IN POS. OPS TEST OK AS PER B767 -400 AMM 52-73. (4929728)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,625 hrs · 15,751 cycles

SHIP 1815 HYDRAULIC SERVICING PANEL MISSING ON ARRIVAL W/ ADJACENT STRUCTURAL DAMAGE. CORRECTIVE ACTION: REPAIRED DAMAGED AREA PER B767 SRM 51-40. HYD SVC DOOR INSTALLED PER B767-400 AMM 52-49. (4676632)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,521 hrs · 15,735 cycles

AIRCRAFT 1815, LEFT AFT EXTERIOR EMERG LT INOP. CORRECTIVE ACTION: REPLACED LEFT AFT EXTERIOR EMERG LT PER B767-400 AMM 33-51-06. (LP 4539276)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,021 hrs · 15,662 cycles

SHIP 1815 R FWD WINDOW HEAT ARCING. TURNED OFF AND ARCING STOPPED. CORRECTIVE ACTION: R&R'D F/O WINDSHIELD AS PER B767-400 AMM 56-11-01-404-017. A/C OK FOR SVC. (9896812)

Part: NONE — NONE · airframe 86,486 hrs · 15,588 cycles

SHIP 1815 4R SLIDE INDICATOR LIGHT INOP OR DAMAGED. CORRECTIVE ACTION: REMOVED & REPLACED 4R SLIDE INDICATOR IAW B767-400 AMM 52-73 ALL OK FOR SVC PLACARD REMOVED (2666868)

Part: NONE — NONE · airframe 86,390 hrs · 15,575 cycles

SHIP 1815 4R DOOR ARMED PROPERLY BUT ARMED LIGHT NEVER ILLUMINATED. CORRECTIVE ACTION: ARMED 4R DOOR MULTIPLE TIMES PER B767 AMM 52-73. NO FAULTS INDICATED. OK FOR SVC (4147397)

Part: NONE — NONE · airframe 86,347 hrs · 15,569 cycles

SHIP 1815 ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS: 4R. CORRECTIVE ACTION: FOUND SPRING DISCONNECTED ON METERLOCK PANEL. RECONNECTED SPRING DOOR OPS NML PER B767 AMM 52-11 (2644787)

Part: NONE — NONE · airframe 86,335 hrs · 15,567 cycles

SHIP 1815 4R DOOR WOULD NOT ARM. CORRECTIVE ACTION: FOUND FOD IN GIRT BAR LOCK REMOVED FOD AS REQUIRED CYC DOOR ARM PER B767-400 AMM 52-11 OPS CHK NML. A/C OK FOR SVC (4147346)

Part: NONE — NONE · airframe 86,335 hrs · 15,567 cycles

SHIP 1815 R4 DOOR EXTERIOR EMERGENCY LIGHT INOP. CORRECTIVE ACTION: REPLACED FUSES IN BATTERY PACK FOR R4 DOOR NOW OPS NML REF B767- 400 AMM 33-51 (4147348)

Part: NONE — NONE · airframe 86,356 hrs · 15,570 cycles

SHIP 1815 4R DOOR HARD TO ARM. CORRECTIVE ACTION: REMOVED AND REPLACE 4R DOOR PAWL SPRING OPS CHECK GOOD REF B 767-4 AMM 52-11. (2639174)

Part: NONE — NONE · airframe 86,282 hrs · 15,559 cycles

SHIP 1815 4R WILL NOT ARM. CORRECTIVE ACTION: FOUND EXTERIOR HANDLE PARTIALLY OPEN. UNABLE TO ARM HANDLE. CYCLED HANDLE PER B767 AMM 52-11. OK FOR SVC. (4147326)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 86,115 hrs · 15,535 cycles

SHIP 1815 2 L AND 2 R EXIT DOORS HARD TO ARM. CORRECTIVE ACTION: BOTH TRACK CLEANED AND OPS CHECK C/O IAW B767-400 AMM 52-00 NOW FUNCTION NML (9934688)

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 86,055 hrs · 15,527 cycles

SHIP 1815 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 2L. CORRECTIVE ACTION: OPERATIONAL TEST OF SLIDE-RAFT ARMED WARNING SYSTEM ON DOOR 2L TESTS OK PER B767-400 AMM 52-73. (2610699)

Part: GIRT BAR — FOD (R4 DOOR) · airframe 85,840 hrs · 15,499 cycles

SHIP 1815 4R DOOR WILL NOT ARM. CORRECTIVE ACTION: CYCLED 4R DOOR FOUND DEBRIS ON GIRT BAR. CLEANED DEBRIS. ALL CHKS NML PER B767-400 AMM 52-11. OK FOR SVC. (9930992)

Part: TOILET — CLOGGED (LAVATORY) · airframe 85,713 hrs · 15,481 cycles

DIVERTED TO JFK DUE TO TWO LAVATORIES INOPERATIVE ENROUTE. MTC C/W OVERWEIGHT LANDING INSPECTION, REMOVED BUNDLE OF PAPER TOWELS FROM WASTE DUCT AND CLEARED MEL FOR INOPERATIVE VACUUM BLOWER.

Part: LEVER — LACK OF LUBE (PAX DOOR) · airframe 85,687 hrs · 15,473 cycles

ENTRY DOOR ARMING LEVER HARD TO OPERATE. LUBED AND OPERATED LEVER 6 TIMES OPS CHECK GOOD.

Part: DOOR — FOD (R4) · airframe 85,654 hrs · 15,469 cycles

DOOR 4R WILL NOT ARM. REMOVED DEBRIS AND ARMED /DISARMED DOOR SEVERAL TIMES - ALL OP CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 85,485 hrs · 15,447 cycles

DURING SERVICE CHECK, FOUND AFT LEFT EXIT SIGN INOPERATIVE. R & R THE BATTERY PACK IAW AMM 33-51. EXIT SIGN OPS NORMAL. OK FOR SVC.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 85,369 hrs · 15,429 cycles

SHIP 1815 EMERGENCY LIGHT CAUTION MSG PRIOR TO PUSH BACK. CORRECTIVE ACTION: T/S I.A.W B767-400 WDMCHP 33-51-11. MSG CLEARED. (9700372)

Part: NONE — NONE (PAX DOOR) · airframe 85,369 hrs · 15,429 cycles

ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS:608. NO TROUBLE FOUND. ARMED/DISARM NORMAL AND VERIFIED ARMING INDICATION NORMAL. CHKS OK. REF B767400 AMM 52-11.

Part: NONE — NONE · airframe 84,870 hrs · 15,346 cycles

SHIP 1815 ITEM NOT LISTED IN THE EFM / LOCATIONS:900, CORRECTIVE ACTION: NO PROBLEM FOUND OPS OK REF B767-400 AMM 25-29. (2433783)

Part: NONE — NONE · airframe 84,745 hrs · 15,327 cycles

SHIP 1815 ON TO NOTICED BURNING RUBBER ODOR. ODOR DISAPATED IN FLIGHT. ON DESCENT WHEN TAXI LR&RT TURNOFF LIGHTS WERE TURNED ON ODOR RETURNED. TURNED OFF TAXI LT+RT ODOR DISAPATED. WHEN RESELECTED ON NOTICED SMALL WISP OF SMOKE. SELECTED OFF FOR REMAINDER OF FLIGHT. CORRECTIVE ACTION: INSPECTED AND FOUND RT TURNOFF SWITCH TERMINAL BURNT. REMOVED AND REPLACED LIGHT PANEL PER B767-400 AMM 33-42. OPS CK GOOD. AS PRECAUTION REMOVED AND REPLACED ANTI-COLLISION LIGHT PNL PER B767-400 AMM 33-42.OPS CK GOOD. OK FOR SVC. (8971666)

Part: ROTARY ACTUATOR — INOPERATIVE · airframe 84,410 hrs · 15,273 cycles

SHIP 1815 2L ENTRY DOOR ASSIST INOP, CORRECTIVE ACTION: R/R 2L DOOR ROTARY ACTUATOR IAW B767 AMM 52-11. OPS CHECK GOOD. MEL AND PLACARD REMOVED. (9286787)

Part: NONE — NONE · airframe 84,179 hrs · 15,245 cycles

SHIP 1815 ON SVC CHECK FOUND EPL OUT FROM ROW 20-34 LH. CORRECTIVE ACTION: REMOVED/REPLACED BATTERY PACK AND CHARGER PER B767-400 AMM 33-51 . OPS CHECK GOOD. A/C OK FOR CONT SVC. (9286710)

Part: NONE — NONE · airframe 84,162 hrs · 15,243 cycles

SHIP 1815 LH AFT FUSELAGE EXTERIOR EMERGENCY LIGHT INOP, CORRECTIVE ACTION: INSP. LIGHT, NO TROUBLE FOUND. (9286706)

Part: BATTERY PACK — INOPERATIVE · airframe 83,916 hrs · 15,208 cycles

SHIP 1815 EMERGENCY LIGHTS ROW 20AB TO 32AB INOP. CORRECTIVE ACTION: R/R BATTERY PACK PER B767-400 AMM 33-51. OPS CK NORMAL (8918619)

Part: NONE — NONE · airframe 83,642 hrs · 15,174 cycles

SHIP 1815 FOUND EMER FLOOR LIGHT 20AB-32AB INOP. CORRECTIVE ACTION: R/R EMER LIGHT BATTERY PACK AT 31AB IAW B767 AMM 33-51. OPS CHECKS GOOD. (8647521)

Part: NONE — NONE · airframe 83,435 hrs · 15,125 cycles

SHIP 1815 4R DOOR WILL NOT ARM. CORRECTIVE ACTION: RESYNCED 4R DOOR ARMING NORMAL OK FOR SERVICE. (8791404)

Part: NONE — NONE · airframe 83,205 hrs · 15,080 cycles

SHIP 1815 F/A REPORTED EMERGENCY EXIT SIGN COVER BROKEN LOC 203. CORRECTIVE ACTION: SECURED LOC 203 EMERGENCY EXIT SIGN COVER PER B767 AMM 33-51 OK FOR SVC. (8853885)

Part: NONE — NONE · airframe 83,045 hrs · 15,047 cycles

SHIP 1815 4R DOOR WONT ARM, CORRECTIVE ACTION: CYCLED 4R DOOR. DOOR ARMS NORMAL PER B767 AMM 25-11. (8853836)

Part: NONE — NONE · airframe 83,045 hrs · 15,047 cycles

SHIP 1815 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:503, CORRECTIVE ACTION: PERFORMED OPS TEST OF DOOR 1L SLIDE ARMED IND REF B767-400 AMM 52-73 IND OPS CHK NORMAL (2112147)

Part: DOOR SILL — DIRTY (R2 DOOR) · airframe 82,860 hrs · 15,016 cycles

SHIP 1815 AT DEPT 2R DOOR WONT ARM, CORRECTIVE ACTION: CLEARED DEBRIS FROM 2R DOOR SILL. CYCLED DOOR. ARMS NORMAL PER B767 AMM 25-66 OK FOR SVC. (8304228)

Part: NONE — NONE · airframe 82,591 hrs · 14,960 cycles

SHIP 1815 PILOT SIDE EMERGENCY LIGHTS FLICKER ON AND OFF INFLIGHT AFT OF DOOR 3L , CORRECITIVE ACTION: REPLACED EMERGENCY ;IGHT BATTERY CHARGER AT ROW 42 A/B, REPLACED BATTERY PACK (AFT) M739 AT ROW 53 A/B AND 54 A/B WITH REF TO B 767-400 AMM 33-51. OPS CHK OKAY. (8246436)

Part: NONE — NONE · airframe 82,591 hrs · 14,960 cycles

SHIP 1815 FLOOR AND CEILING EMERGENCY LIGHTS FLASHING ON AND OFF REPEATERLY FROM LEFT SIDE OF AIRCRAFT FROM DOOR 3L TO BACK OF AIRCRAFT , CORRECITIVE ACTION: OP CHECKED UNABLE TO FAULT OPS NML A/C CONTINUE TO SERVICE B767 -400 AMM 33-50 (8246434)

Part: NONE — NONE · airframe 82,551 hrs · 14,951 cycles

SHIP 1815 FROM SEAT 52B THRU 4L LAV ILLUMINATEFOR A MINUTE THEN TURN OFF FOR NOE SECOND. CORRECTIVE ACTION: OPERATED EMERGENCY LIGHTS PER B767-400 AMM 33-51 MULTIPLE TIMES UNABLE TO DUPLICATE ANY FAULTS. (2056178)

Part: NONE — NONE · airframe 82,476 hrs · 14,936 cycles

SHIP 1815 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:501. CORRECTIVE ACTION: OPERATED EMERGENCY LIGHTS PER AMM 33-50. EMERGENCY FLOOR LIGHTING CKS NORMAL AT THIS TIME. (2051515)

Part: NONE — NONE · airframe 82,476 hrs · 14,936 cycles

SHIP 1815. EMERGENCY LIGHTING ON CAPT'S SIDE FROM DOOR 3L AFT TURN ON AND OFF INTERMITTENTLY DURING FLIGHT. CORRECTIVE ACTION: R/R PWR SUPPLY AS PER B767 -400 AMM 33-51. OPS CHECK GOOD. (8206692)

Part: NONE — NONE · airframe 82,476 hrs · 14,936 cycles

SHIP 1815 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:EME . CORRECITVE ACTION: EMERGENCY LIGHTS OPS CK GOOD PER 67-400 AMM33-51 NO DEFECTS NOTED (2049747)

Part: NONE — NONE · airframe 82,476 hrs · 14,936 cycles

SHIP 1815 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:AFT. CORRECITVE ACTION: EMERGENCY LIGHTS OPS CK GOOD PER 67-400 AMM 33-51 OK FOR SVC (2049743)

Part: NONE — NONE · airframe 82,425 hrs · 14,927 cycles

SHIP 1815 ENTRY DOOR 4R ARMING LEVER HARD TO OPERATE. CORRECTIVE ACTION: PERFORMED OP CHK PER B767-400 AMM 52-11. FAULT COULDNOT BE DUPLICATED. OK FOR SVC (2041800)

Part: NONE — NONE · airframe 82,390 hrs · 14,920 cycles

SHIP 1815 OVERHEAD LITS IN CABIN ON CAPT SIDE FLICKER ON & OFF. EMERGENCY FLOOR LIGHTING FLICKERING THROUGHOUT CABIN. CORRECTIVE ACTION: REMOVED AND REAPPLIED POWER PER B767 AMM 24-22 RESEATED CONNECTORS ON LGITHING CONTROL PANELS PER B767 AMM 33-90 AND OPS CHECK OF EMERGENCY LIGHTS PER B767 AMM 33-51. (8206658)

Part: NONE — NONE · airframe 82,390 hrs · 14,920 cycles

SHIP 1815 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE, CORRECTIVE ACTION: ALL EMER LIGHTS OP CK NML @ THIS TIME. (2038365)

Part: NONE — NONE · airframe 82,369 hrs · 14,914 cycles

SHIP 1815 EMERG LIGHTS COME ON INTERMITTENTLY FROM ROW 38 BACK. CORRECTIVE ACTION: NO HISTORY PER ATL MCC ERIC. OPS CKS NML AT THIS TIME. OK TO CONT. IN SVC . (1815)

Part: NONE — NONE · airframe 82,335 hrs · 14,905 cycles

SHIP A/C 1815 37ABC EMERYENCY LIGHTS REMAIN ON OVER SEAT. CORRECTIVE ACTION: FOR IMFORMATION PURPOSE 37ABC OPS CHECK NORMAL. (8106384)

Part: NONE — NONE · airframe 82,317 hrs · 14,902 cycles

SHIP 1815 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED. CORRECTIVE ACTION: PERFORMED EMERGENCY LIGHT TEST REF B767 AMM 33-51 OPS CHK NORMAL. (2024278)

Part: NONE — NONE · airframe 82,249 hrs · 14,888 cycles

SHIP 1815 1R DOOR SLIDE ARMED LIGHT INOP AT FWD F/A PNL. CORRECTIVE ACTION: OP TEST OF 1R DOOR SLIDE ARMED LIGHT ON FWD ATTD PANEL GOOD B767 -400 AMM 33-21 AND 1R DOOR ARMS CORRECTLY PER 52-11. (2019767)

Part: NONE — NONE · airframe 82,360 hrs · 14,912 cycles

SHIP 1815 EMER LTS IN FLT ATTD REST COMPARTMENT WON'T TURN OFF, CORRECTIVE ACTION: AS PER ER/A 595661-14 REV OG SEC II PERMANENT REPAIR C/W. (8106361)

Part: NONE — NONE · airframe 82,221 hrs · 14,884 cycles

SHIP 1815 AT DEPARTURE 4R DOOR WILL NOT ARM. CORRECTIVE ACTION: CYCLED EXTERIOR DOOR HANDLE. CHECKS NORMAL. (8106340)

Part: NONE — NONE · airframe 82,147 hrs · 14,869 cycles

SHIP 1815 4R DOOR WONT ARM CORRECTIVE ACTION: CYCLED 4R DOOR ARMS NORMAL A/C OK FOR SVC NO TROUBLE FOUND (8106316)

Part: NONE — NONE · airframe 82,100 hrs · 14,857 cycles

SHIP 1815 LOWER CREW REST EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: FOUND LADDER EMR LTS INOP. R/R EMR BAT AND CHARGER . REF B767 AMM 33-51. OPS CK OK. (8097876)

Part: WIRE — LOOSE (ARM SWITCH) · airframe 79,676 hrs · 14,322 cycles

SHIP 1815 EMERGENCY ARM SWITCH LIGHTS INTERNAL SPRING WIRE LOOSE. MAINTENANCE FOUND EMERGENCY LIGHTS SWITCH GUARD OPERATES NORMAL. SYSTEM OPERATION IS NORMAL. (LP 7288015)

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,638 hrs · 14,315 cycles

SHIP 1815 EMERGENCY LIGHT R2 AFT DOOR INOPERATIVE. MAINTENANCE REPLACED THE PASSENGER EXIT SIGN ASSEMBLY. (LP 7595476)

Part: LIGHT — DETACHED (CABIN) · airframe 79,273 hrs · 14,255 cycles

EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR FELL OFF ON LANDING. MAINTENANCE REATTACHED LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: INDICATOR — INOPERATIVE (L1 DOOR SLIDE) · airframe 79,207 hrs · 14,241 cycles

L1 DOOR SLIDE ARM LIGHT ASSEMBLY INOPERATIVE. MAINTENANCE REPLACED ARM LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — NO TEST (CREW REST) · airframe 79,090 hrs · 14,212 cycles

LOWER LOBE CREW REST EMERGENCY LIGHTS NOT TESTING PROPERLY FORWARD TO MEL. CREW REST EMERGENCY LIGHTS OPERATION IS NORMAL. MCO/PLAC REMOVED.

Part: STRAP — CRACKED (FUSELAGE) · airframe 78,934 hrs · 14,163 cycles

DURING HFEC INSPECTION FOUND 01EA CRACK AS MARKED ON THE CUT LINE OF FAIL- SAFE STRAP. REPAIRED PER ERA 585589-14. (LP1540518)

Part: HINGE FITTING — CRACKED (TE FLAP) · airframe 78,934 hrs · 14,163 cycles

HFEC INSPECTION FOUND 01EA CRACK ON THE RH INBOARD TRAILING EDGE MAIN FLAP, OUTBOARD HINGE FITTING. REPAIRED PER ERA 585622-14 (LP1540392)

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 78,934 hrs · 14,163 cycles

DURING PERFORM W/C5312-01170-10A-02, FOUND A STIFFENER(145T8703-11) CRACK BETWEEN STA 955 AND 977 LBL80. C/W ERA 585589-14. (LP 1539145)

Part: STRAP — CRACKED (FUSELAGE) · airframe 78,934 hrs · 14,163 cycles

DURING PERFORM W/C 5312-01170-05 STEP 7 HFEC INSPECTION FOUND 01EA CRACK OF THE FAIL -SAFE STRAP. C/W ERA 585589-14. (LP 1539053)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 78,934 hrs · 14,163 cycles

AFTER FASTENER REMOVAL PER NRC 130-007, FOUND A HOLE INNER SURFACE MATERIAL MISSING ON SHIN AT STA 955. REPAIRED PER ERA 585589-14. (LP 1539151)

Part: SKIN — CRACKED (LE SLAT) · airframe 78,934 hrs · 14,163 cycles

LHW SLAT NO.4 UPPER SURFACE IB FOUND FASTENER HOLE CRACKED REPAIRED PER ERA 585805-14 (LP 1537647)

Part: STRUCTURE — DEBONDED (LE SLAT) · airframe 78,934 hrs · 14,163 cycles

LHW SLAT NO.1 I/B UPR EDGE FOUND DISBONDING. REPAIRED PER SRM 51-70-10. (LP 1534712)

Part: SKIN — DENTED (TE FLAP) · airframe 78,934 hrs · 14,163 cycles

RH WING OB FLAP LOWER SURFACE FOUND DENT 55" TO OB EDGE AND 15" FROM LE OF FLAP. REPLACED SRM 51-70-10. (LP 1534697)

Part: SKIN — DENTED (TE FLAP) · airframe 78,934 hrs · 14,163 cycles

LHW I/B FLAP LOWER FLAP LOWER SURFACE FOUND DENT AT 5.1 FT FROM I/B EDGE AND 1.4FT FROM AFT EDGE. REPAIRED PER SRM 51-70-10. (LP 1534706)

Part: SKIN — DENTED (TE FLAP) · airframe 78,934 hrs · 14,163 cycles

LHW O/B FLAP LOWER SURFACE I/B FOUND DENT. REPAIRED PER SRM 51-70-07 (LP 1534714)

Part: SKIN — CRACKED (TE FLAP) · airframe 78,934 hrs · 14,163 cycles

FOUND LOWER SKIN CRACK ON RH WING OB FLAP T/E. REPAIRED PER SRM 57-53-01. (LP 1532624)

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 78,934 hrs · 14,163 cycles

FOUND DELAMINATION ON LH LATERAL SURFACE OF VERTACAL STABILIZER FSS65-92,10" FROM FRONT SPAR. C/W ERA 585586-14. (LP 1532644)

Part: ACCESS DOOR — DENTED (NR 1 ENGINE) · airframe 78,934 hrs · 14,163 cycles

NO.1 ENG ACCESS DOOR 431AT UPR SURFACE FOUND DENT REPAIRED PER SRM 51-70-17. (LP 1532653)

Part: BEAM — CRACKED (LE SLAT) · airframe 78,934 hrs · 14,163 cycles

ENTR 00785334 W MTC TASK-RH WING SLAT NO.9 NOSE BEAM WEB CRACK AT OSS 650.30 LOG-PAGE UPDATED THE CRACKED AREA AT RH WING SLAT NO.9 NOSE BEAM WEB. OSS 650.30 REPAIRED AS PER PRI585846-14 REV.O. THE PRI 585846-14 REVO COMPARED AND COMPLIED WITH ERA 585846-14 REV.ORIGINAL ASSOCIATED ER/A 14-585846 ADDED FOR AC 1815 (1527399)

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 78,934 hrs · 14,163 cycles

MTC TASK-A CRACK FOUND ON VERTICAL STABILIZER AUXILIARY SPAR WEB AT LH FSS 65.75 LOG-PAGE UPDATED RII: Y W THE CRACKED AUXILIARY SPAR WEB REPAIRED AS PER PRI585644-14. REV.O THE PRI 585644-14 REV.O COMPARED AND COMPLIED WITH ERA585644-14 REV.ORIGINAL ASSOCIATED ER/A 14-585644 ADDED FOR AC 1815 (1526213)

Part: SPAR — CRACKED (NR 2 NACELLE) · airframe 78,934 hrs · 14,163 cycles

ENTR 00785334 W AD/MTC TASK-THERE EXISTED INDICATIONS OF POSISIBLE CRACK AROUND THE LH INBD FASTENER HOLE OF THE #2 NACELLE AFT UPPER SPAR CHORD HORIZONTAL FLANGE AT NAC STA 285.5.(ALI SSI 54-50-I17A,54-590- 14). LOG-PAGE UPDATED RII: Y ENTR 00785334 W THE CRACKED AREA REPAIRED AS PER PRI 585517-14AD REV:O THE PRI 585517-14AD REV.O COMPARED AND COMPLIED WITH ERA 585517-14AD REV-ORIGINAL PLS ACCOMPLISH FLLOW-UP INSPECTION AS PER ERA 585517-14AD REV.ORIGINAL SEC.II AND LOG PAG#1516486. ASSOCIATED ER/A 14-585517 ADDED FOR AC 1815 (1526292)

Part: RIB — CRACKED (RT WING) · airframe 78,934 hrs · 14,163 cycles

MTC TASK-RH WING SLAT NO.9 RIB HOLE CRACK AT OSS 646.35 LOG-PAGE UPDATED THE CRACKED RIB AT R/H WING NO.9 SLAT. OSS646.35 REFER TO PRI 585806-14 REV.O REPAIRED THE PRI 585806-14 REV.O COMPARED AND COMPLIED WITH ERA 585806-14 REV.ORIGINAL ASSOCIATED ER/A 14-585806 ADDED FOR AC 1815 (1526202)

Part: SKIN — CRACKED (LE SLAT) · airframe 78,934 hrs · 14,163 cycles

MTC TASK-FOUND RH WING #9 SLAT I/B UPPER SURFACE LOWER HOLE CRACK THE CRACKED AREA AT RH WING #9 SLAT I/B UPPER SURFACE REPAIRED AS PER B767-400 SRM 57-43-01-2R-2 RELEASE59.00-12/19/19 LOG-PAGE UPDATED (1525126)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 78,934 hrs · 14,163 cycles

FOUND FWD CARGO SHEAR TIE CORRODEN AT STA500, S-36R TO S-37R.REFER TO CPCP TASK 53-460-00 THE NEW SHEAR TIE (P/N:149T2102Y272) FABRICATED AS PER BOEING DRAWING 149T2102 AND SERVICE REQUEST NUMBER 0270437243. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-400 SRM 51-40-02 (1522495)

Part: SPAR — CRACKED (NACELLE) · airframe 81,684 hrs · 14,773 cycles

DURING INSPECTION FOUND CRACK ON THE HORIZONTAL FLANGE OF THE AFT UPPER SPAR CHORD. C/W ERA 585517-14AD. (LP 1516486)

Part: DOUBLER — CRACKED (NR 1 PYLON) · airframe 78,934 hrs · 14,163 cycles

MTC TASK-NO.1 PYLON IB UPR DOUBLERS FOUND CRACK AT NSTA230 REPAIRED THE CRACK ON NO.1 PYLON IB UPR DOUBLERS AT NSTA230 AS PER PRI 585398-14 REV.0 THE PRI 585398-14 REV.0 COMPARED AND COMPLIED WITH ERA585398-14 REV.ORIGINAL PLS ACCOMPLISH SEC:II OF ERA 585398-14 REA 585398-14 REA.ORIGINAL FOR THRESHOLD INSPECTION REF.TO LOG#1508039 FOR DETAIL ASSOCIATED ER/A 14-585398 ADDED FOR AC 1815 (1512592)

Part: STRUCTURE — CRACKED (NR 2 NACELLE) · airframe 78,934 hrs · 14,163 cycles

AD/MTC TASK-FOUND ONE CRACK AT AFT HOLE OF HORIZONTAL FLANGE AT NSTA221.250 AT NO.2 NACELLE,THE CRACK IS IN THE 4 O'CLOCK AT OUTBOARD OF RH.(ALI SSI 54-50-I16F,54-594-28) HORIZONTAL FLANGE AT NSTA221.250 AT NO.2 NACELLE CRACKED AREA REPAIRED AND ACCOMPLISHED AS PER PRI 585292-14AD REV0 11FEB2020 AND PRI 585292-14AD REV1 15FEB2020 COMPARED WITH ERA 585292-14AD REV ORIGINAL 28FEB2020 AND FOUND IN COMPLIANCE.PLS ACCOMPLISH SEC II OF ERA 585292-14AD REV.ORIGINAL FOR INSPECTION REF.TO LOG # 1507933 FOR DETAIL ASSOCIATED ER/A 14-585292 ADDED FOR AC 1815 (1512604)

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 78,934 hrs · 14,163 cycles

MTC TASK-NO.1 PYLON FWD SPAR LOWER WIRE HARNESS CUTOUT FOUND CRACK AT NSTA 210.0 REPAIRED THE CRACK ON NO.1 PYLON FWD SPAR LOWER WIRE HARNESS CUTOUT AT NSTA210.0 AS PER PRI 585425-14 REV.0 THE PRI 585425-14 REV.0 COMPARED AND COMPLIED WITH ERA585425-14 REV.ORIGINAL ASSOCIATED ER/A 14-585425 ADDED FOR AC 1815 (1512578)

Part: STRUCTURE — CRACKED (NR 1 NACELLE) · airframe 78,934 hrs · 14,163 cycles

AD/MTC TASK-FOUND ONE CRACK AT AFT HOLE OF HORIZONTAL FLANGE AT NSTA221.250 AT NO.1 NACELLE,THE CRACK IS IN THE 5 O'CLOCK AT INBOARD OF LH.(ALI SSI 54-50-L16F,54-594-28) HORIZONTAL FLANGE AT NSTA221.250 AT NO.1 NACELLE CRACKED AREA REPAIRED AND ACCOMPLISHED AS PER PRI 585291-14AD REV0 11FEB2020 AND PRI 585291-14AD REV1 15FEB2020 COMPARED WITH ERA 585291-14AD REV ORIGINAL 29FEB2020 AND FOUND IN COMPLIANCE.PLS ACCOMPLISH SEC II OF ERA 585292-14AD REV.ORIGINAL FOR INSPECTION REF.TO LOG # 1509106 FOR DETAIL LOG-PAGE UPDATED (1512712)

Part: NONE — NONE · airframe 83,605 hrs · 15,157 cycles

SHIP 1815 ERA 585398-14 ISSUED FOR REPAIR TO #1 ENGINE PYLON FWD UPPER SPAR CHORD AT NAC STA 230. FOLLOW ON ACTCION IS REQUIRED. CORRECTIVE ACTION: REMOVED SEALANT AND CLEANED AREA FOR INSPECTION PER ERA 585398- 14 REV. ORIGINAL. ORIGINAL AND B767 NDT MANUAL PART 6 51-00-19. NO DEFECTS FOUND. (1508039)

Part: SEAT TRACK — CORRODED (BS 1483) · corrosion level 2 · airframe 78,934 hrs · 14,163 cycles

SEAT TRACK-CABIN SEAT TRACK FOUND CORROSION AT LBL 55 STA1483, REF TO CPCP TASK 53-646-00.THE CRROSION ON CABIN SEAT TRACK AT LBL55 STA1483 REMOVED AND MEASURED THE REWORKED AREA THE CLEANUP DEPTH IN BOTTOM OF TRACK AT STA1483 IS 0.075",THE MAX.ALLOWABLE CLEANUP DEPTH IS 0.030" AND FOUND EXCEED THE LIMIT AS PER B767-400 SRM 53-00-52 ALLOWABLE DAMAGE 1 RELEASE 59.00 DATE:19.DEC.19.THE SEAT TRACK P /N:146T5213-29 FABRICATED WITH MATERIAL BAC1520-2898(DA) AS PER BOEING DRAWING:146T5213-29 AND SMAL SERVICE REQUEST NO:270444015 .THE SEAT TRACK REMOVED AND REPLACED AS PER B767-400 SRM 51-40- 02 RELEASE 59. (1505335)

Part: SEAT TRACK — CORRODED (BS 1208-1428) · corrosion level 2 · airframe 78,934 hrs · 14,163 cycles

SEAT TRACK-CABIN SEAT TRACK FOUND CORROSION AT RBL 88.5 STA1208 TO STA1428.REF.TO CPCP TASK 53-646-00. THE SEAT TACK CORROSION AT RBL 88.5 STA1208 TO STA 1428 REMOVED AND MEASURED THE MAXIMUM CLEANUP DEPTH IN BOTTOM OF TRACK IS 0.041" AT STA 1251,THE ALLOWABLE MAX.0.03" AND FOUND OUT OF LIMIT AS PER B767-400 SRM53-00-52 ALLOWABLE DAMAGE 1 RELEASE 59.00 19.DEC.19.PERFORMED THE REPAIR AS PER PRI 585199-14 REV.0. THE PRI 585199-14 REV.0 COMPARED AND COMPLIED WITH ERA 585199-14 REV.ORIGINAL. ASSOCIATED ER/A 14-585199 ADDED FOR AC 1815 (1501402)

Part: SEAT TRACK — CORRODED (BS 368) · corrosion level 2 · airframe 78,934 hrs · 14,163 cycles

SEAT TRACK-CABIN SEAT TRACK FOUND CORROSION AT LBL 11,STA 368. REF. TO CPCP TASK 53-646-00 THE DVI CARRIED OUT THE CORROSION REMOVED AREA AND FOUND NO OTHER DEFECT AS PER B767-400 SRM 51-10-08 RELEASE 59.00 DATE:19. DEC.19.THE REWORKED AREA MEASURED THE CLEANUP DEPTH IN BOTTOM OF TRACK AT STA368 IS 0.072",THE MAX.ALLOWABLE CLEANUP DEPTH IS 0.030" AND FOUND EXCEED THE LIMIT AS PER B767-400 SRM53-00-52 ALLOWABLE DAMAGE 1 RELEASE 59.00 DATE:19.DEC.19.THE SEAT TRACK REMOVED AND REPLACED AS PER B767-400 SRM 51-40-02 RELEASE 59.00 (1501309)

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 78,934 hrs · 14,163 cycles

-FLOOR STRUCTURE FOUND CORROSION AT LBL 11 TO LBL 54.75, STA 1480.REF.TO CPCP TASK 53-644-00 THE DVI CARRIED OUT AND FOUND THE CORROSION PERFORATION AT LBL11 TO LBL54.75 STA 1480 AS PER B767-400 SRM 51-10-08 RELEASE 59.00 DATE:19.DEC.19.FLOOR STRUCTURE AT LBL 11 TO LBL 54.75 STA 1480 REPAIRED AS PER B767-400 SRM 53-00-51-2R-1 RELEASE 59.00 DATE:19 .DEC.19. LOG-PAGE UPDATED @ 19FEB20 0946 UTC (1496145)

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 78,934 hrs · 14,163 cycles

MTC TASK-FLOOR STRUCTURE FOUND CORROSION AT RBL 30 TO RBL 40,STA 1480. REF. TO CPCP TASK 53-644-00. LOG-PAGE UPDATED FLOOR STRUCTURE CORRODED AREA BLEND OUT AND MEASURED:THE BLEND OUT SIZE:1.2"X0.5",THE ORIGINAL THICKNESS IS 0.090",THE REMAINING THICKNESS IS 0.051"<0.8T(0.072") ON THE RBL 40 FWD FLANGE OF UPPER SURFACE AND FOUND EXCEED THE LIMIT AS PER B767- 400 SRM 53-00-51-1A-1 RELEASE 59.00 DATE:19.DEC.19.FLOOR STRUCTURE AT RBL 30 TO RBL 40 REPAIRED AS PER B767-400 SRM 53-00 -51-2R-2 RELEASE 59.00 DATE:19.DEC.19. LOG-PAGE UPDATED (1496128)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 78,635 hrs · 14,126 cycles

EMER LIGHT RED AFT GALLEY INOP RELAMPED NO HELP REPLACED LIGHY ASSY OPS CK GOOD OK FOR SVC (6009673)

Part: TARGET — OUT OF POSITION (ENTRY DOOR) · airframe 77,746 hrs · 14,010 cycles

SHIP 1815 - ATO - AT 50 KTS DUE TO LEFT FORWARD ENTRY LIGHT ILLUMINATED ON TAKEOFF ROLL. CORRECTIVE ACTION: DEFERRED PER MEL 52-71-01, SHIMMED TARGET, RE-TORQUED LINK ASSEMBLY FORWARD OF SHIM AND PLATED ASSEMBLY. LP 6586278

Part: TIE ROD — NOT REPORTED (POTABLE WATER) · airframe 77,746 hrs · 14,010 cycles

SHIP 1815 - DIV - TO DEN DUE TO LOSS OF POTABLE WATER. CORRECTIVE ACTION: DEFERRED PER MEL 38-10-01B. REPLACED WATER TANK 2 FORWARD MOUNTING TIE RODS, BOTTOM HEATED HOSE, AIR COMP HOSE AS PER IPC 28-15-01-07. WATER TANK SECURED. REPLACED CHILLER TIE ROD. LP 6586248.

Part: ACTUATOR — BROKEN (RAM AIR DOOR) · airframe 76,601 hrs · 13,850 cycles

ON W/A FOUND LT PACK RAM AIR DOOR DEPARTED AIRCRAFT. DURING INSTALLATION TEST FOUND RAM AIR DOOR ACTUATOR BROKEN IN HALF REPLACED RAM AIR ACTUATOR. SYSTEM OPERATION IS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,235 hrs · 13,805 cycles

DOOR 1 LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED DOOR L1 EXTERIOR EMERGENCY LIGHT FILAMENT. SYSTEM OPERTION IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,235 hrs · 13,805 cycles

SEATS 22AG -27AB ARE INOPERATIVE. REPLACED BATTERY LIGHT CHARGER. SYSTEM OPERATION IS NORMAL.

Part: UNKNOWN — LEAKING (HYD SYSTEM) · airframe 74,456 hrs · 13,544 cycles

STRONG FUMES IN THE COCKPIT AFTER T/O ROTATION AND BEGINNING OF GEAR RETRACTION. DISPPATCHED QUICKLY. PACKS OFF TAKEOFF NO EVIDENCE OF FUEL LEAKAGE. FOUND LT WHEEL WELL WET FROM HYDRAULIC FLUID WIPPED AND RAN ALL HYDRAULIC PUMPS. NO LEAKS FOUND AT THIS TIME. AC OK FOR SERVICE. (LP 5264170)

Part: PANEL — CRACKED (NR 2 PYLON) · airframe 73,161 hrs · 13,362 cycles

NR 2 ENG PYLON IB PANEL 447 ELX WHICH IS LOCATED JUST FWD OF THE HYD BAY DOOR HAS A SMALL CRACK ON THE AFT END C/W ERA 571107-14.

Part: CONNECTOR — UNSECURE (ELEC RECEPTICLE) · airframe 71,448 hrs · 13,132 cycles

L4 LAVATORY, 110 ELECTRICAL RECEPTICAL LOOSE AND EMITTED SPARKS. THE 110 RECEPTACLE WAS REMOVED POWER FROM OUTLET. FOUND LOOSE CONNECTION ON BACK OF PLUG. SECURED THE CONNECTOR. CHECKED GOOD. OK FOR SERVICE.

Part: PROXIMITY SENSOR — MALFUNCTIONED (R1 DOOR) · airframe 71,364 hrs · 13,122 cycles

DURING CLIMB OUT, THE CABIN EMERGENCY LIGHTS CAME ON, ONLY ON THE RIGHT. CYCLED EMERGENCY LIGHT SWITCH. THE LIGHTS REMAINED ON FOR A COUPLE MINUTES THEN WENT OFF. CYCLED THE SWITCH. REPLACED R1 DOOR PROXIMITY SENSOR.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 71,106 hrs · 13,086 cycles

RIGHT INBD FLAP AFT UPPER SURFACE, 25 INCHES FROM INBD EDGE, 3 INCHES FROM TRAILING EDGE WEDGE, FOUND ONE DENT AND REPAIRED IAW SRM 51-70-10.

Part: RELAY — INOPERATIVE (R1 DOOR) · airframe 71,106 hrs · 13,086 cycles

AFTER PARKING AT GATE, THE R1 DOOR WOULD NOT OPEN ELECTRICALLY. OPENED MANUALLY. REMOVED AND REPLACED THE FWD ENTRY DOOR UP RELAY K380 IAW SWPM 20-81. TESTED IAW AMM 52-11. FOUND SATISFACTORY.

Part: UNKNOWN — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 71,106 hrs · 13,086 cycles

AFTER LANDING ON TAXI IN F/A'S REPORTED THAT THE EMERGENCY LIGHTS ON THE CAPT'S SIDE ONLY IN THE CABIN WOULD COME ON STEADY PERIODICALLY FOR SAY 1 MINUTE THEN GO OFF FOR HALF A MINUTE THEN CYCLE ON AGAIN. NO LIGHTS CYCLED ON THE F/O SIDE. THE EMERGENCY EXIT LIGHT SWITCH IN COCKPIT IN ARMED. PERFORMED EMERGENCY LIGHT CHECK /TEST IAW AMM 33-51. NO DEFECTS NOTED. COULD NOT DUPLICATE FAULT. NO 90 DAYS HIST. OK TO CONT IN SVC.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 70,907 hrs · 13,054 cycles

LAVATORY SMOKE DETECTOR WENT OFF. THE SMOKE DETECTOR TURNED OFF. SUSPECT THE SMOKE DETECTOR WAS TRIGGERED. ACFT OK FOR SERVICE.

Part: COMPUTER — MALFUNCTIONED (THRUST MANAGE) · airframe 70,011 hrs · 12,928 cycles

SHIP 1815 RETURNED TO ATL DUE TO LOSING THRUST MANAGEMENT, LNAV AND VNAV. CORRECTIVE ACTION: REPLACED THRUST MANAGEMENT COMPUTER. PERFORMED AFDS TEST 30 AND 40. TESTS GOOD. A/C RTS. (9986638).

Part: ADIRU — MALFUNCTIONED · airframe 70,070 hrs · 12,935 cycles

RETURNED DUE TO LOST FMS, ETA, AND FUEL COMPUTATORS. REPLACED THE CENTER AND RIGHT ADIRU AND RIGHT TAT PROBE. ALL TESTED GOOD. VERIFICATION FLIGHT GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 69,387 hrs · 12,846 cycles

CLIMBING THRU FL 250, LEFT FWD ENTRY DOOR EICAS MESSAGE CAME ON. PRESSURIZATION NORMAL. OP TESTED IAW AMM 52-11. DOOR WORKS NORMAL, ALSO OP TEST OF SLIDE ARMING IAW AMM 52-73.

Part: DOOR SEAL — OBSTRUCTED (R4 DOOR) · airframe 68,552 hrs · 12,740 cycles

4R DOOR SEAL MAKING AIR NOISE DURING DESCENT. ON CHECK FOUND 4R DOOR WITH FOD DEBRIS. RMVD AND CLEANED ALL FOD DEBRIS. ACCOMPLISHED OPS CHKD IAW AMM 52-11 OPS CHKD GOOD.

Part: ENGINE — MAKING METAL (NR 2) · airframe 68,552 hrs · 12,740 cycles

RT ENG OIL FILTER MESSAGE DISPLAYED, OIL QUANTITY AND PRESSURE GOOD, ALL OTHER INDICATIONS NORMAL. DIVERTED. MAINTENANCE FOUND METAL DEBRIS ON MCD AND IN OIL FILTER BOWL, ENGINE CHANGE IN PROGRESS. REMOVED AND REPLACED NUMBER 2 ENGINE.

Part: HANDLE — UNSECURE (L2 DOOR) · airframe 68,491 hrs · 12,731 cycles

L2 DOOR WOULD NOT ARM. INSPECTED THE DOOR ARMING. FOUND OUTSIDE HANDLE NOT CLOSED. CYCLE DOOR OPS CHECKED GOOD.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 67,176 hrs · 12,564 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED. REPLACED THE LENS.

Part: LIGHT — UNKNOWN (CABIN) · airframe 65,775 hrs · 12,384 cycles

EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. RELAMPED EMER FLOOR LIGHTING PER AMM 33-51.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 64,146 hrs · 12,167 cycles

EMERGENCY LIGHT AT SEATS 15-20 AB ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,732 hrs · 12,115 cycles

EMERGENCY LIGHTS AT SEAT 15 AB THROUGH 21 AB ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. SYSTEM OPS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,001 hrs · 11,901 cycles

CREW REST LADDER AND COMMON AREA EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED THE LAMPS BOTH SIGNS IAW MM 33-51.

Part: FLOORBEAM — CORRODED (BS 1528) · airframe 53,429 hrs · 10,811 cycles

AFT CABIN FLOORBEAM UPPER INNER TEE FITTING AT BS 1528 LBL 88 FOUND CORRODED. REPLACED TEE IAW ERA 525464-14.

Part: SERVO — INOPERATIVE (HYD SYSTEM) · airframe 49,616 hrs · 10,332 cycles

HYD QTY EICAS MESSAGE IN FLT, DECLARED EMERGENCY. R & R LT YAW DAMPER SERVO IAW AMM 22-21. CHECKED GOOD IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,337 hrs · 9,799 cycles

TEST OF EMERGENCY PATH LIGHTING SYSTEM SHOWED THAT THE PATH LIGHTS AT SEATS 15B THROUGH 20B WERE NOT ILLUMINATING. MAINTENANCE FOUND THAT THE BATTERY PACK WAS INOPERATIVE. REMOVED AND REPLACED BATTERY, OPS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 45,337 hrs · 9,799 cycles

SEVERAL EMERGENCY LIGHT IN COACH CLASS ARE INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AND CHARGER PER AMM 33-51. OPS CHECKED GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 44,615 hrs · 9,713 cycles

EMERGENCY LIGHTS AT SEAT 18, 19, 20, 21GF INOPERATIVE. MAINTENANCE FOUND CONNECTOR DISCONNECTED.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 42,108 hrs · 9,395 cycles

DURING PSV8, FOUND CORROSION ON THE CANTED PRESSURE BULKHEAD WEB AT STA 955 AND LBL 85. WEB REPLACED PER PRI 491470-14.

Part: BALLAST — DEFECTIVE (LAVATORY) · airframe 40,113 hrs · 9,139 cycles

THE FLIGHT CREW REPORTED AN ELECTRICAL SMELL COMING FROM BEHIND LAVATORY 217 MIRROR. MAINTENANCE INSPECTED COMPARTMENT BEHIND LAVATORY MIRROR. MAINTENANCE FOUND THE LIGHT BALLAST TO BE HOT. MAINTENANCE DISCONNECTED THE BALLAST AND SMELL DISAPPEARED. NO FURTHER DEFECTS WERE NOTED. MAINTENANCE REPLACED THE BALLAST. OPERATIONAL CHECK WAS NORMAL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 40,019 hrs · 9,127 cycles

MAINTENANCE FOUND IN SEAT EMERGENCY PATH LIGHTING ON ROWS 30AB THROUGH 37AB INOPERATIVE. MAINTENANCE FOUND CONNECTOR AT SEAT 30A DISCONNECTED AND RE-CONNECTED IT. ALL EMERGENCY PATH LIGHTING CHECKS NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 38,887 hrs · 8,971 cycles

M/D - STA 324 RBL 22 TO 55 FLOORBEAM UPPER CHORD FOUND CORRODED AND REPAIRED IAW SRM 53-00-51 FIG 201, REPAIR 1.

Part: LIGHT — INOPERATIVE (DOOR L2) · airframe 38,628 hrs · 8,942 cycles

EMERGENCY PATH LIGHTS AT GALLEY L2 DOOR ARE INOPERATIVE. MX REPLACED THE LIGHT ASSY. SYS OPS IS NORMAL.

Part: FAN — SEIZED (CABIN) · airframe 36,049 hrs · 8,632 cycles

STRONG ACRID ODOR ELEC SMELL AT CRUISE, THROUGHOUT CABIN, QRH FOR ELEC SMOKE AND FIRE PERFORMED. NOTE - WHEN UTIL BUSSES TURNED OFF THE SMELL DISSAPTED. FOUND RECIRC FAN INOP AND SEIZED. INSPECTED FAN AND NOTICED STRONG ELEX SMELL FROM FAN. CONF CALL MCC AFTER TROUBLESHOOTING WAS COMPLETED. FAN DEFERRED IAW MEL 21-25-01A.(DL764101609)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 34,467 hrs · 8,429 cycles

EMERGENCY LIGHTS INOP AT 38GF-40GF. FOUND CONNECTOR DISCONNECTED AT SEAT 40GF. CONNECTED PLUG EMER LIGHTS CK GD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 34,459 hrs · 8,428 cycles

EMERGENCY LIGHTS INOP AT 38GF-40GF. FOUND CONNECTOR DISCONNECTED AT SEAT 40GF. CONNECTED PLUG EMER LIGHTS CK GD. (FOUND DURING OVERNIGHT CHECK) CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: GCU — INOPERATIVE (NR 1 ENGINE) · airframe 30,361 hrs · 7,931 cycles

RTB DUE TO LT ENG HAD TO RESET L GEN CONT SWITCH TO PWR L ENG GEN. REPLACED L GCU.

Part: ENGINE — DAMAGED (NR 2) · airframe 29,335 hrs · 7,813 cycles

NR 2 ENGINE FAILED SCHEDULED BORO. REPLACED ENGINE.

Part: ENGINE — MAKING METAL (NR 1) · airframe 25,381 hrs · 7,348 cycles

RTO DUE TO NR 1 ENG STALLED. REPLACED NR 1 ENG. FOUND METAL IN TAILPIPE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 24,887 hrs · 7,279 cycles

FOUND SEAT 7AB EEPL CONNECTOR IS DAMAGED. REPLACED CONNECTOR AT SEAT 7AB, OPERATIONALLY CHECKS GOOD IN ACCORDANCE WITH B767-400 MM 33-51-00-715-200.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 24,887 hrs · 7,279 cycles

EMERGENCY LIGHTS INOP FROM 38A TO 41A, CABLE CONNECTOR AT SEAT 42A WAS LOOSE, RECONNECTED CABLE CONNECTOR AT SEAT 42A. PERFORMED GOOD OPS CK OF EMERGENCY LIGHTS FOR SEATS 38A-41A IAW DAL B767-400MM 33-51-00 AND 33-51-05.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 24,887 hrs · 7,279 cycles

EMERGENCY LIGHTS INOP AT SEATS 38FG THRU 44FG, REMOVED AND REPLACED ELECTRICAL CONNECTOR AT SEAT ROW 44FG IAW SWPM 20-10-13 AND OPS CHECKED GOOD IAW B767-400 MM 33-51-10.

Part: START VALVE — INOPERATIVE (NR 2 ENGINE) · airframe 24,839 hrs · 7,272 cycles

EICAS MSG RT STARTER CUTOUT ILLUMINATED IN FLIGHT. DUE TO QRH PROCEDURES AND ICING CONDITIONS IN ATL HAD TO DIVERT TO MIA FOR REPAIR. REMOVED AND REPLACED RT ENG START VALVE PER AMM. SPUN ENG AT GATE. START VALVE CKS GOOD.

Part: SKIN — DAMAGED (BS 1395-1439) · airframe 24,542 hrs · 7,235 cycles

FOUND DEBRIS STUCK FUSELAGE AT FS 1395-1439. INSTALLED SKIN REPAIR DOUBLER.

Part: FAN BLADE — BIRD INGESTION (NR 1 ENGINE) · airframe 24,516 hrs · 7,232 cycles

BIRD STRIKE DURING T/O OUT OF DKR, LT ENG VIBS WENT TO 5.0. ALL OTHER PARAMETER NORMAL. RETURNED TO DKR. MTC FOUND 5 FAN BLADES DAMAGE OUT LIMITS AND 1 OGV WITHIN LIMITS. SENDING PARTS ON FLT 34/02. WILL NEED UPDATE WHEN MTC COMPLETE MA KEY 5-0145. REMOVED AND REPLACED NR 1 ENG FAN BLADE ASSY PER M/M. PERFORM VIBE SURVEY, ALL CHKS GOOD PER M/M. P/N INSTALLED C1-1 FAN S 6101.

Part: WIRE HARNESS — CHAFED (AFT GALLEY) · airframe 23,427 hrs · 7,097 cycles

AFTER PUSHBACK, IN AFT GALLEY 2 FLT ATTENDANTS FELT A SHOCK WHEN TOUCHING A DOOR IN THE GALLEY. FOUND 1 WIRE CHAFED IN WIRE BUNDLE NEXT TO GALLEY DISCONNECT REPAIRED AND REWRAPPED AND REROUTED WIRE BUNDLE. WRAPPED WIRE BUNDLE. CKS GOOD.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 20,018 hrs · 6,606 cycles

RT ENGINE CONTROL ADVISORY AND STATUS MSG ON 20 MINUTES AFTER ENGINE START. REPLACED NR 2 ENG HMU PER M/M RAN ENG PER AMM CHKS GOOD

Part: IDG — MALFUNCTIONED (LT ENGINE) · airframe 19,883 hrs · 6,571 cycles

LEFT GEN OFF. RTB, FWD TO MCO PER MEL 24-00-01. FAULT CODE 24-35751. REPLACED LEFT IDG ENG RUN AND LK CK GOOD MCO AND PLACARD REMOVED.

Part: GIRT BAR — MISSING (R4 DOOR) · airframe 19,271 hrs · 6,438 cycles

4R GIRT BAR MISSING INSTALLED MPN 141T6102-10 OPS CHECKS GOOD MCO AND PLAC REMO ETOPS CATEGORY (E): PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: CONTROL PANEL — UNSERVICEABLE (COCKPIT) · airframe 18,802 hrs · 6,335 cycles

AFTER TAKEOFF AUTO THROTTLES DISCONNECTED LOSS OF VNAV/LNAV BITE FAULTED 31-0211 - 21-0211- 22-0211 REPLACED MCP SYSTEM, TESTS OK. ALSO REPLACED CENTER ADIRU SYSTEM, CKS GOOD.

Part: APU — SHUTDOWN · airframe 18,538 hrs · 6,282 cycles

APU AUTOSHUTDOWN NO ACEL. REPLACED APU.

Part: IDG — FAILED (LEFT) · airframe 18,209 hrs · 6,218 cycles

WHILE AT CRUISE ALT, LOST LEFT ENG GEN ACCOMPANIED WITH LEFT CSD DRIVE LIGHT. REPLACED IDG AND TESTED PER MM.

Part: TURBINE BLADES — DAMAGED (NR 1 ENGINE) · airframe 17,850 hrs · 6,147 cycles

PERFORM BORO OF NR 1 ENG DUE TO PRIOR EGT EXCEEDENCE. FOUND DAMAGE T1 BLADES AND END CAPS MISSING. REPLACED NR 1 ENG.

Part: COUPLER — FAILED (RT HF COMM) · airframe 17,629 hrs · 6,100 cycles

UNABLE TO GET RIGHT HFTO CHANNELIZE OR COMMUNICATE ON ANY FREQ. REPLACED NR 2 HF RADIO COUPLER TRANSMIT AND RECEIVE NORMAL ON 8843.

Part: SWITCH — INOPERATIVE (RT HYD SYS) · airframe 16,369 hrs · 5,813 cycles

CENTER RIGHT HYD PUMP SWITCH INOP. REPLACED SWITCH PANEL.

Part: SENSOR — MALFUNCTIONED (SLAT SYSTEM) · airframe 15,679 hrs · 5,638 cycles

L/E ASYM MESSAGE DURING DESCENT BEFORE 250 KTS. FOLLOWED QRH PROCEDURES. HIGHEST BRAKE TEMP AT 6.0 NR 6 BRAKE. T/S PER FIM 27-81-00 FIG 107 PSEU FAULTS S295 TARGET FAR FAILURE WITH FAILURE LIGHT ON. REPLACED SENSOR S295 AND CHECKED PER MM.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 14,728 hrs · 5,401 cycles

FOUND EMERGENCY TRACK LIGHTS OUT BEHIND ROW 32CDE. FOUND CONNECTOR DISCONNECTED, RECONNECTED ALL, CHECKS NORMAL.

Part: LOCK — LOOSE (RUDDER PEDAL) · airframe 14,644 hrs · 5,379 cycles

DURING TAKEOFF NOTICED CAPTAINS RUDDER PEDALS SHIFT FORWARD ABOUT AN INCH, NORMAL T/O. INSPECTED PEDAL MECHANISIM AND TIGHTEND LOCK. PDEAL NOW LOCKS INTO DESIRED POSITION.

Part: SEAL — DAMAGED (SPOILER ACT) · airframe 14,566 hrs · 5,362 cycles

RT HYD QTY WAS .48 AND DROPPED TO .38. REPLACED O-RING ON SPOILER ACTUATOR.

Part: ACM — SEIZED (A/C BAY) · airframe 12,206 hrs · 4,663 cycles

UPON DESCENT AT APPROXIMATELY 27,000 FT, ADVISED BY THE CABIN CREW OF A SMOKEY HAZE IN THE CABIN, REPORTED TO SMELL ELECTRICAL. SMOKE AND FUMES PROCEDURES WERE APPLIED BUT SMOKE NEVER TOTALLY DISSIPATED. STATUS MSGS - LT PACK ACM AND FWD IFE COOLING. FOUND LEFT ACM SEIZED. REPLACED ACM AND RAN PACKS AND ENGINES. ALL CHECKS OK.

Part: PSEU — FAILED (E/E BAY) · airframe 9,976 hrs · 4,005 cycles

ON CLIMB OUT GEAR DISAGREE FOLLOWED BY GEAR NOT DOWN CAUTION AND WARNING. AIR RETURN TO LAS. REPLACED PSEU. ALL CHECKS GOOD.

Part: PSEU — MALFUNCTIONED (E1 RACK) · airframe 9,668 hrs · 3,891 cycles

IN CRUISE MASTER WARNING SOUNDED AND MASTER CAUTION ILLUMINATED WITH GEAR DISAGREE CAUTION AND INTRANSIT INDICATIONS FOR BOTH MAIN/NOSE GEAR NORMAL UP INDICATION. AIR/GROUND AND NOSE DISAGREE STATUS MSG. GEAR RETRACTION NORMAL AT T/O. NO ABNORMAL CONDITIONS DURING CLIMBOUT/CRUISE. NO VIBRATION NOTED AIR TURNBACK WAS RECOMMENDED TO LAX. REPLACED PSEU PER M/M AND CHECKS NORMAL. MSG CLEARED.

Part: WARNING LIGHT — ILLUMINATED (SLATS) · airframe 9,323 hrs · 3,771 cycles

CREW DECLARED AN EMERGENCY DUE TO L/E SLAT ASSYM ON APPROACH INTO CVG. T/S PER FIM 27-81-00. PSEU HAS NO SENSOR FAULTS, RAN PSEU PER FIM 32-09-03. NO FAULTS SHOWN, DUE TO HISTORY OF S301 SENSOR FAULT, CKD RESISTANCE OF S301 AND FOUND WITHIN LIMITS. MEGGED WIRE FROM S301 TO PROX BOX NO SHORTS TO GND OR BETWEEN. REPLACED PSEU PER M/M. RAN FLAPS/SLATS, NO PROBLEMS NOTED. C/W MSU INSTALLED GOLD PINS IN POS 7 AND 8 ON D4378J, NO RII REQUIRED PER TOPP 40-30-05.

Part: BOLT — SHEARED (LT MLG) · airframe 8,715 hrs · 3,549 cycles

FOUND ON TRANSIT CHECK LEFT MLG UPLOCK FITTING ATTACH BOLT SHEARED. CLEANED AND INSPECTED UPLOCK FITTING NO ADDITIONAL DAMAGE NOTED. REPLACED LEFT MLG UPLOCK FITTING BOLT.

Part: PSEU — FAULTY (L/E SLAT) · airframe 8,426 hrs · 3,438 cycles

DURING C/O FROM LAX, L/E SLAT ASYM MSG CAME ON INTERMITTENTLY THEN REMAINED ON, LEVEL OFF LIGHT EXTINGUISHED DURING LATER STAGES OF DESCENT ON RETURN TO LAX. FIX FSEU FAULTED LAST FLT L/E INBD ASYM MSG NR 27-81020 PSEU FAULTED NR 304 SW NR 8 INBD SLAT CHECKED PROX SW TO TARGET CLEARANCE PER MM, FOUND WITHIN LIMITS. CLEANED SWITCH AND TARGET REPLACED PSEU, OPS CHECK NORMAL.

Part: ACTUATOR — TRIPPED (T/E FLAP) · airframe 5,009 hrs · 2,028 cycles

T/E FLAP DISAGREE AFTER T/O RAISED WITH ALT SYSTEM. DUE TO SHORT RUNWAY IN OGG DIVERTED TO HNL. T/S PER FIM, FOUND NR 6 T/E FLAP ROTARY ACT TRIPPED. RESET SAME. CYCLED FLAPS NO OTHER FAULTS.

Part: ACTUATOR — TRIPPED (T/E FLAP) · airframe 4,527 hrs · 1,832 cycles

AFTER DEPARTING HNL, FLAPS LOCKED AT 6 DEGS AND EICAS MSG T/E FLAP DISAGREE APPEARED. C/W QRH PROCEDURE AND RAISED FLAPS USING ALTERNATE MODE BUT FLAPS WOULD NOT COME UP BEYOND 2 DEGS. INITIATED AIR TURNBACK TO HNL. LANDED OVERWEIGHT, MTC IN PROGRESS. NO FAULTS ON FSEU. CHECKING OVER TORQUE TRIP INDICATORS. NO HISTORY. FOUND T/E FLAP ROTARY ACTUATORS 2 - 3 - 4 AND 6 OVER TORQUE IND TRIPPED. RESET SAME, ALL OPS NORMAL.

Part: ACTUATOR — MALFUNCTIONED (L/E SLAT) · airframe 3,662 hrs · 1,469 cycles

RECEIVED ACARS FOR A FLAP DISAGREE ON CLIMBOUT FROM HNL, QRHB FOLLOWED AND WILL CONTINUE TO LAX. ON APPROACH IN LAX, FLAPS/SLATS EXTENDED, FLAPS OK BUT HAD NO INDICATION THAT THE LEADING EDGE HAD EXTENDED. CREW CALLED FAA FOR EMERGENCY EQUIPMENT. NORMAL LANDING. THE CAPTAIN TOLD MTC UPON ARRIVAL VISUAL INSPECTION SHOWS THE L/E WERE DOWN. MTC IN PROGRESS. LAX MTC T/S PER FIM AND FOUND THE NR 7 ROTARY ACT TRIPPED. RESET AND OPS OK. REPLACE ALTERNATE IN/BD SLAT DRIVE MOTOR PER M/M ALL. CHECKS GOOD.

Part: PSEU — FAULTY (E/E BAY) · airframe 3,412 hrs · 1,344 cycles

GEAR DISAGREE CAME ON AT CRUISE (FL 290) NOSE INDICATED UP, MAINS IN TRANSIT (INDICATED). SUSPECT SOFTWARE PROBLEM. PSEU BIT SHOWS CARD 005 AND TARGET 260 FAULTS. SWUNG GEAR SEVERAL TIMES WHILE OPERATING CABIN EQUIP TO TEST FOR EMI FAULTS, ALL CHECKS GOOD. REPLACED PSEU, CHECKED PA CABIN INTERPHONE AND CHIME, NO FAULTS OR MESSAGES, REPLACED S-260. ATTEMPTING TO INDUCE FAULT, RAN BOTH ENGINES WHILE OPERATING VARIOUS A/C SYS TO INCLUDE WINDOW HEAT, FLAPS, IFE, PA AT ALL STATIONS AND EXTERIOR LIGHTS. NO MSGS/S OF FAULTS NOTED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (L/E SLAT) · airframe 3,399 hrs · 1,334 cycles

LEADING EDGE SLAT ASYMMETRY MESSAGE ON SLAT RETRACTION OUT OF ATL. NUMBER 2 SLAT PROX SENSOR OUT OF ADJUSTMENT. ADJUSTED PER BOEING S/L 767-SL-27-83.

Part: CONNECTOR — LOOSE (CABIN) · airframe 2,642 hrs · 1,050 cycles

EGRESS LIGHTING AT SEATS 10AB, 26AB THRU 32AB INOP. TIGHTENED LOOSE CONNECTOR, OPS CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (COCKPIT) · airframe 134 hrs · 76 cycles

BOTH INBOARD NAV DISPLAYS AND BOTH EICAS DISPLAYS BLANKED ON ATL APPROACH. REPLACED DISPLAY COMPUTER.