N1200K

Part: INDICATOR — INOPERATIVE (ZONE 800) · airframe 118,507 hrs · 17,216 cycles

SHIP 1200 R1 DOOR SLIDE LIGHT NOT COMING ON. SHOWS ARMED ON FA CONTROL PANEL. R & R SLIDE ARM LIGHT IAW AMM 52-73.

Part: OVEN — ODOR (ZONE 900) · airframe 118,507 hrs · 17,216 cycles

DIVERTED TO YYR DUE TO ELECTRICAL ODOR IN AFT GALLEY. GALLEY EQUIPMENT ISOLATED BY CREW AND ODOR DISSIPATED. REPLACED NUMBER 4 AND 5 OVENS FOR PRECAUTION. NO OTHER TROUBLE FOUND.

Part: GUARD — MISSING (LIGHT SWITCH) · airframe 116,852 hrs · 16,947 cycles

THE EMERGENCY LIGHTS SWITCH GUARD IS MISSING THE WIRE THAT PULLS THE SWITCH INTO ARMED POSITION WHEN THE GUARD IS CLOSED. MAINTENANCE REPLACED THE EMERGENCY LIGHTS SWITCH GAURD REF B767 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. THE A/C IS NOW OK FOR SERVICE. (LP #6660630)

Part: ALTIMETER — FAULTED (ZONE 200) · airframe 116,670 hrs · 16,905 cycles

SHIP 1200 -RVSM- ALT DISAGREE CAUTION CLIMBING THROUGH FL260. AT FL360 CAPTAIN 36250, FO 36000, STBY 36700. CAPTAIN AIRSPEED 280 KIAS, FO 270, STBY 270. CORRECTIVE ACTION: T/S PER B767 FIM TASK 34-12-00-815-804 ADC NO FAULT. DUE TO HISTORY REMOVED AND REPLACED CAPTS ADC PER B767 AMM 34-12 CHKD OK. (6369836)

Part: SWITCH — INOPERATIVE (ZONE 800) · airframe 116,408 hrs · 16,848 cycles

SHIP 1200 ENTRY DOOR ARM LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED 1L DOOR SLIDE ARMED INDIC SW. OPS CK NML. (5810248)

Part: SKIN — DAMAGED (ZONE 500 FLAP) · airframe 116,181 hrs · 16,796 cycles

SHIP 1200 L/H WING O/B FLAP UPPER SURFACE FOUND SWELL AT 46' TO I/B EDGE AND 26' TO AFT EDGE. CORRECTIVE ACTION: REPAIRED L/H WING O/B FLAP UPPER SURFACE SWELL AT 46'' TO I/B EDGE AND 26'' TO AFT EDGE AS PER B767-300 SRM 51-70-10 (0700510)

Part: INDICATOR — INOPERATIVE (ZONE 800) · airframe 115,979 hrs · 16,758 cycles

SHIP 1200 MAIN ENTRY/SERVICE DOOR ARMED INDICATORS INOP AT 1L LOCATION. CORRECTIVE ACTION: R/R L1 DOOR SLIDE-RAFT ARM LIGHT ASSY. PER B767 AMM 52-73, OPS CHK GOOD (0640231)

Part: ARMING LEVER — INOPERATIVE (L1 DOOR SLIDE) · airframe 114,425 hrs · 16,542 cycles

DOOR 1L SLIDE ARMED LIGHT NEXT TO DOOR HANDLE INOP. REPLACED SLIDE ARMED LIGHT ASSY.

Part: LAMP — INOPERATIVE (INDICATOR) · airframe 114,100 hrs · 16,494 cycles

AIRCRAFT 1200, ANNUNCIATOR LIGHT ON FLIGHT ATTENDANT PANEL AT 1L FOR DOOR 2R SLIDE IS INOP. CORRECTIVE ACTION: RELAMPED. (LP 0390425)

Part: BOTTLE — MECHANIC ERROR (RT OVRWG SLIDE) · airframe 113,453 hrs · 16,395 cycles

WHILE PERFORMING OVERWING SLIDE RE ARM PROCEDURE FOUND INFLATION TRIGGER CABLE NOT INSTALLED BEHIND TETAINER SPRING. NEED NEW INFLATION CYCLINDER FOR RT OVERWING SLIDE ASSY. R/R RH OFF WING SLIDE BOTTLE PER WC 2561-4723 (5321277)

Part: INDICATION SYS — FAULTED (L1 DOOR) · airframe 113,370 hrs · 16,383 cycles

SHIP 1200 FA DISARMED L1 DOOR 4 TIMES AND INDICATORS REMAINED INDICATING ARMED IN 3 SPOTS. CORRECTIVE ACTION: OPERATED L1 DOOR ARM/DISARM SEVERAL TIMES, NO TROUBLE FOUND. ARM /DISARM NORMAL AND SLIDE/ARM LIGHTS OPERATE NORMALLY. REF B767300 AMM 25-66. (5321253)

Part: SWITCH — LOOSE (DOOR INDICATOR) · airframe 113,204 hrs · 16,356 cycles

SHIP 1200 1L MAIN ENTRY/SERVICE DOOR ARMED INDICATORS. CORRECTIVE ACTION: FOUND ARMED LIGHT INDICATOR LIGHT SWITCH LOOSE AND TIGHTENED SAME OPS CHECK NML. PER B767-300 AMM 52-73. (0263840)

Part: LIGHT — MISSING (SEAT 36AB) · airframe 113,184 hrs · 16,353 cycles

AISLE EMERGENCY LIGHT MISSING SEAT 36 AB. CORRECTIVE ACTION: REPLACED ROW 36AB EMERGENCY LIGHT PER B767 AMM 33-51. OPS NORMAL . COMPLIED WITH ERA 600000-14TR REV C SEC 2.

Part: LIGHT — MISSING (SEAT 43AB) · airframe 113,184 hrs · 16,353 cycles

SHIP 1200 AISLE EMERGENCY LIGHT MISSING @ SEAT 43AB. CORRECTIVE ACTION: ACCOMPLISH ER/ A 600000-14TR (5851444)

Part: WIRE — NOT REQUIRED (EMERGENCY LIGHT) · airframe 113,173 hrs · 16,351 cycles

SHIP 1200 AISLE EMERGENCY LIGHTS INOP, 20FE TO 33GF. CORRECTIVE ACTION: PER B767 WDM 33-51-31 PG-4B SHEET 2, WIRE # W834-9019-20 COMING FROM SPLICE SP9027 DOES NOT EXIST PER THE CURRENT INTERIOR CONFIGURATION. DISCONNECTED & REMOVED WIRE W834-9019-20 TO CONFIGURE CIRCUIT CORRECTLY PER WDM. OPS CK (5851445)

Part: LIGHT — DAMAGED (L1 DOOR SLIDE) · airframe 113,041 hrs · 16,326 cycles

SHIP 1200 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 1L. CORRECTIVE ACTION: REMOVED AND REPLACED 1L DOOR SLIDE ALARM LIGHT ASSY PER B767-300 AMM 52-73. CHECKS GOOD. OK FOR SERVICE. (0233797)

Part: NONE — NONE (NONE) · airframe 112,698 hrs · 16,271 cycles

SHIP 1200 ERA 605516-14AD REV A, SECTION II. CORRECTIVE ACTION: ACCOMPLISH SECTION II WITHIN 5,085 TOTAL CYCLES FROM FEBRUARY 7, 2023 AND REPEAT NO LATER THAN EVERY 5,085 TOTAL CYCLES. (0182799)

Part: NONE — NONE (NONE) · airframe 112,740 hrs · 16,277 cycles

SHIP 1200 ERA 605516-14AD REV A. CORRECTIVE ACTION: AMOC APPROVAL TO AD 2021-10-19 IS REQUIRED AT OR PRIOR TO 50,000 TOTAL AIRFRAME FLIGHT CYCLES. (0182785)

Part: CONNECTOR — DISCONNECTED (L1 SLIDE LIGHT) · airframe 112,680 hrs · 16,266 cycles

SHIP 1200 1L DOOR SLIDE ARMED LIGHT INOP. CORRECTIVE ACTION: FOUND SLIDE ARMED INDICATOR LIGHT ASSY DETACHED FROM CONNECTION- REPLACED WITH NEW LIGHT ASSY OPS CHECK GOOD (0178815)

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 112,655 hrs · 16,261 cycles

SHIP 1200 1L DOOR SLIDE ARMED LIGHT INOP. CORRECTIVE ACTION: RR 1L SLIDE ARMED LIGHT ASSY PER B767 WDM 5273 CKS GOOD MEL/PLAC RMVD (4494705)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,496 hrs · 16,226 cycles

SHIP 1200 1L MAIN DOOR ARMED INDICATOR INOP. CORRECTIVE ACTION: REPLACED CONNECTOR BEHIND LIGHT, OP CHK GOOD IAW B767 AMM 52-73. (5527394)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,443 hrs · 16,216 cycles

SHIP 1200 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: UNABLE TO DUPLICATE - ALL SLIDE INDICATOR LIGHTS OP NML PER B767 -3 AMM 33-51 (0118757)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,306 hrs · 16,189 cycles

SHIP 1200 1L DOOR SLIDE LIGHT WILL NOT ILLUMINATE. CORRECTIVE ACTION: DOOR 1L SLIDE LIGHT ADJUSTED IAW AMM 33-51 B767-300 - FOUND WORKS OK (5527314)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,306 hrs · 16,189 cycles

SHIP 1200 L1 DOOR SLIDE ARM LIGHT INOP. CORRECTIVE ACTION: PERF GVI OF WIRING ON L1 DOOR SLIDE LIGHT ASSY & L1 DOOR ARMED LIGHT ASSY ON FAP. NO DAMAGE OR DEFECTS NOTED PER B767-300 AMM 20-60. (0097404)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,211 hrs · 16,172 cycles

SHIP 1200 DOOR 1L SLIDE LIGHT WILL NOT ILLUMINATE. CORRECTIVE ACTION: T/S AND FOUND LIGHT ASSEMBLY DAMAGED. VERIFIED 28VDC PRESENT AT 2 AND 1. GOOD GND AT 4 PER B767 WDM 52-73-11. R/R LIGHT ASSEMBLY M1326 PER B767 AMM 52-71. CKS OK. (5041769)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,121 hrs · 16,159 cycles

SHIP 1200 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:606. CORRECTIVE ACTION: CHECKED ON GROUND COULD NOT DUPLICAT FAULT. SLIDE INDICATOR LIGHT WORKS OK. (0070842)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,051 hrs · 16,147 cycles

SHIP 1200 L1 HAS A HISTORY OF SLIDE LIGHT INOP AT DOOR. CORRECTIVE ACTION: RMVD AND REPLACED L1 DOOR ARMING LIGHT MODULE PER B767 AMM CHAP 52-73. OPS CK GOOD. OK FOR SVC (0063408)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,883 hrs · 16,119 cycles

SHIP 1200 1L & 1R SLIDE LIGHT INOP. CORRECTIVE ACTION: MCC NOTIFIED FWD "DOORS" SLIDE ARMED LIGHTS TO MEL 52-11-01. ARM LIGHTS ON F/A PANEL OPS NORMAL. PLACARDS INSTALLED C/W "M" PROC. OK FOR SERVICE. (4365046)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 111,865 hrs · 16,115 cycles

SHIP 1200 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: FOUND LIGHT CONNECTOR HOUSING NOT ATTATCHED CORRECTLY, REATTATCHED HOUSING PER B767 AMM 52-11. (0036338)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,887 hrs · 15,822 cycles

AIRCRAFT 1200, AFT EMERGANCY LIGHT SIGNS AT 2R & 2L DOOR INOP. CORRECTIVE ACTION: REPLACED BATTERY PACK. (LP 4692722)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 109,500 hrs · 15,766 cycles

SHIP 1200 FLIGHT ATTENDANT PANEL AMBER. CORRECTIVE ACTION: BULB CHECKED FOR SECURITY AND FOUND GOOD. (5115666)

Part: NONE — NONE · airframe 108,703 hrs · 15,648 cycles

SHIP 1200 AT CREW REST, SMALL EXIT SIGN (RUNNING MAN) INOP. CORRECTIVE ACTION: R/R LIGHT ASSY OPS CHK NML PER B767-300 AMM 33-51. (9134331)

Part: NONE — NONE · airframe 108,656 hrs · 15,642 cycles

SHIP 1200 OVERHEAD EMERGENCY LIGHT IN CEILING ABOVE 5D INOP. CORRECTIVE ACTION: FWD TO MEL 33-51-01A. NO "M" PROCEDURES. MCO+PLACARD INSTALLED. (9881188)

Part: NONE — NONE · airframe 108,656 hrs · 15,642 cycles

SHIP 1200 EMERGENCY PATH LIGHT AT SEAT 54F INOP. CORRECTIVE ACTION: FWD TO MEL 33-51-03A. NO "M" PROC MCO & PLACARD INSTALLED (9881187)

Part: NONE — NONE · airframe 108,611 hrs · 15,634 cycles

SHIP 1200 DURING SVC CHK FOUND E-PATH LIGHTS 45G-54G INOP. CORRECTIVE ACTION: FOUND GROUND GD2544 UNSECURE. SECURED PER WDM 33-51-31. ALL E-LIGHTS NOW OPS NML. SYS OK FOR SVC. (9881172)

Part: UNKNOWN — UNKNOWN · airframe 108,538 hrs · 15,619 cycles

SHIP 1200 HFEC INSPECTION FOUND 01 EA CRACK ON STRINGER S-2R AT STA 717 BETWEEN TWO FASTENERS HOLE AND IT IS ABOUT 1 INCH LONG. CORRECTIVE ACTION: DAMAGE AREA REPAIRED PER PRI 605516-14 (2619863)

Part: UNKNOWN — UNKNOWN · airframe 108,538 hrs · 15,619 cycles

SHIP 1200 WHEN PERFORM AIRCRAFT ARRIVE INSPECTION,FOUND A HEAVY DENT WITH A PERVIOUSLY INVALID LOG NUMBER(LOG:6926914)ON THE FUSELAGE SKIN EXTERNAL SURFACE BETWEEN STA 1562 AND STA 1582, JUST ABOVE STR20L.RE-EVALUATE THE DENT REUIRED. CORRECTIVE ACTION: DAMAGE AREA REPAIRED PER PRI 605103-14 (2617949)

Part: UNKNOWN — UNKNOWN · airframe 108,538 hrs · 15,619 cycles

SHIP 1200 FOUND FUSELAGE FRAME WEB CORROSION AT STA 1109 AND S-4L LOWER,REFER TO CPCP TASK 53-692-00. CORRECTIVE ACTION: DAMAGE AREA REPAIRED PER 605150-14 (2617926)

Part: UNKNOWN — UNKNOWN · airframe 108,538 hrs · 15,619 cycles

SHIP 1200 THE LH MLG UPPER SKIN OF CABIN END FITTING CRACK AT STA 852. CORRECTIVE ACTION: DAMAGE AREA REPAIRED PER PRI 605518-14 (2616521)

Part: UNKNOWN — UNKNOWN · airframe 108,538 hrs · 15,619 cycles

SHIP 1200 THE CABIN FLOOR BEAM UPPER SURFACE CORROSION AT STA 347 AND RBL 11 TO 54.7;REF TO CPCP TASK 53-400-00. CORRECTIVE ACTION: DAMAGE AREA REPAIRED PER PRI 605190-14 (2616528)

Part: UNKNOWN — UNKNOWN · airframe 108,538 hrs · 15,619 cycles

SHIP 1200 FUSELAGE FRAME END FITTING CRACK AT RH STA 927. CORRECTIVE ACTION: DAMAGE AREA REPAIRED PER 605624-14 (2616511)

Part: NONE — NONE · corrosion level 2 · airframe 108,703 hrs · 15,648 cycles

SHIP 1200 THE CABIN CENTER SECTION UPPER SURFACE CORROSION AT BL 0 AND STA 955.1;REF TO CPCP TASK:53-494-00. CORRECTIVE ACTION: REPAIRED THE CORRODED OF THE CABIN CENTER SECTION UPPER SURFACE AT BL 0 AND STA 955.1 AS PER PRI 605104-14 REV 0 AND PRI 605104- 14 REV 1. (2616536)

Part: UNKNOWN — UNKNOWN · airframe 108,538 hrs · 15,619 cycles

SHIP 1200 FOUND LHW LE RIB CRACK AT LES563.10. CORRECTIVE ACTION: LHW LE RIB CRACK AT LES 563.10 REMOVED AND REPAIRED AS PER PRI 605192-14 REV 0. THE PRI 605192-14 REV.0 COMPARED AND COMPLIED WITH THE ERA605192-14 REV ORIGINAL. (2616981)

Part: UNKNOWN — UNKNOWN · airframe 108,538 hrs · 15,619 cycles

SHIP 1200 SEAT TRACK ALONG RBL 20 BETWEEN STA 720 AND 742 FOUND EXISTING OLD REPAIR AT STA720. CORRECTIVE ACTION: REPAIRED THE INTERFERENCE BETWEEN THE EXISTING FLOOR BEAM REPAIR AND SEAT TRACK P/N:38123SF009-003 AND WEB P/N:38123SF009-005 LOCATED AREA AS PER VA 97428MA REV E AND CARD NO:5311-01225-06. (2616871)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 WORN SIGN FOUND ON THE SECTION 48 LH SIDE H/STAB TO FUSELAGE LOWER CUTOUT FWD SIDE LOWER SEAL FAIRING SKIN AT STA 1725. CORRECTIVE ACTION: DAMAGED AREA REPAIRED THE WORN SKIN AS PER B767-300 SRM 53-80 (2615422)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 WORN SIGN FOUND ON THE SECTION 48 RH SIDE H/STAB TO FUSELAGE LOWER CUTOUT FWD SIDE LOWER SEAL FAIRING SKIN AT STA 1725. CORRECTIVE ACTION: DAMAGED AREA REPAIRED THE WORN SKIN AS PER B767-300 SRM 53-80 (2615416)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 FOUND RH WING NO.10 SLAT UPPER NOSE SKIN FROM INBOARD SIDE 40 IHCH 01EA FASTENER AROUND CUTOUT CRACK. CORRECTIVE ACTION: CARRIED OUT THE REPAIR AT RHW NO.10 SLAT UPR NOSE SKIN FROM I/B SIDE 40'' AREA AS PER B767-300 SRM 57-43 (2612329)

Part: NOT ENTERED — NOT ENTERED (NOT ENTERED) · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 ERA 605103-14 ISSUED FOR SKIN REPAIR AT STA 1562 - 1582, S20L. D TA DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED. CORRECTIVE ACTION: DTA DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED AT OR BEFORE 37499 TOTAL FLIGHT CYCLES. (2609943)

Part: NONE — NONE · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 DELAMITON FOUND ON THE RH SIDE VERTICAL STABILER EXTERNAL SKIN WHICH IS BETWEEN AUXLIARY SPAR AND FROM SPAR,THE DELAMINATED SKIN ABOUT L:7 INCH AND W:6 INCH AND ABOUT 9 INCH AWAY FROM THE AUX SPAR, 17 INCH BELOW THE FSS 39.25. CORRECTIVE ACTION: RH SIDE VERTICAL STABILER EXTERNAL SKIN WHICH IS BETWEEN AUXLIARY SPAR AND FROM SPAR, ABOUT 9 INCH AWAY FROM THE AUX SPAR , 17 INCH BELOW THE FSS 39.25 REPAIRED AS PER B767-300 SRM 55-30 (2606214)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1197+44, S-39L TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2600121)

Part: SHEAR TIE — CORRODED (BS 1263 S39L-R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1263, S-39L TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2600111)

Part: SHEAR TIE — CORRODED (BS 1540 S37-38R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 BULK CARGO SHEAR TIE AT STA 1540, S-38R TO S-37R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2600139)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38L) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1197+44, S-37L TO S-38L FOUND CORROSION, CORRECTIVE ACTION: REPARIED THE SHEAR TIE AS PER B767-300 SRM51-40 (2600148)

Part: SHEAR TIE — CORRODED (BS 1480 S38-39R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 BULK CARGO SHEAR TIE AT STA 1480, S-38R TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED THE SHEAR TIE AS PER B767-300 SRM51-40 (2600153)

Part: SHEAR TIE — CORRODED (BS 1219 S38-39R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1219, S-38R TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED THE SHEAR TIE AS PER B767-300 SRM51-40 (2600124)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1197+22, S-37R TO S-38R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599096)

Part: SHEAR TIE — CORRODED (BS 1540 S38-39R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 BULK CARGO SHEAR TIE AT STA 1540, S-38R TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599081)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1197, S-37R TO S-38R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2598995)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1197, S-39L TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599107)

Part: SHEAR TIE — CORRODED (BS 1285 S39L-R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1285, S-39L TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599009)

Part: SHEAR TIE — CORRODED (BS 1540 S38-39L) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 BULK CARGO SHEAR TIE AT STA 1540, S-38L TO S-39L FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599085)

Part: SHEAR TIE — CORRODED (BS 1307 S39L/R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1307, S-39L TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599027)

Part: SHEAR TIE — CORRODED (BS 1219 S37-38L) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1219, S-38L TO S-37L FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599015)

Part: SHEAR TIE — CORRODED (BS 1197 S35-36R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1197+132, S-36R TO S-35R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599104)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1197+88, S-39L TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599017)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1197+22, S-39L TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599060)

Part: SHEAR TIE — CORRODED (BS 1197 S35-36R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1197+44, S-36R TO S-35R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599094)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1197+110, S-39L TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2598998)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 108,534 hrs · 15,617 cycles

SHIP 1200 AFT CARGO SHEAR TIE AT STA 1197+66, S-39L TO S-39R FOUND CORROSION, CORRECTIVE ACTION: REPARIED DAMAGED AREA AS PER B767-300 SRM51-40 (2599045)

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 108,330 hrs · 15,571 cycles

SHIP 1200 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:101 CORECTIVE ACTION: REINSTALLED EXIT SIGN COVER AT DOOR 1L. (2527800)

Part: ACCESS PANEL — MISSING (RT NACELLE) · airframe 108,299 hrs · 15,564 cycles

SHIP 1200 RT PYLON OUTBD SIDE ROUND ACCESS PNL MISSING, INSTALLED NEW COVER RT PYLON CDL AND PLACARD REMOVED.

Part: SKIN — NONE · airframe 107,853 hrs · 15,471 cycles

SHIP 1200 DURING LAST C-CHECK (02APR2019) AT ILN, ER/A 576744-14AD SECT. I REPAIR WAS ACCOMPLISHED ON A/C 1200 (13,289 TFC AND 96,028 TFH) IN THE LH WING SKIN AT STR L-6.5. FOLLOW NO ACTION IS REQUIRED FOR SECT. III INSPECTION. CORRECTIVE ACTION: ACCOMPLISH ER/A 576744-14AD REV. A SECTION III PRIOR TO 6,000 CYCLES OR 18,000 FLIGHT HOURS AFTER SECTION I REPAIR (02APR2019) , WHICHEVER OCCURS FIRST. (2457888)

Part: NONE — NONE · airframe 107,581 hrs · 15,429 cycles

SHIP 1200 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS: 1L, CORRECTIVE ACTION: LENS COVER REATTACHED (2419968)

Part: NONE — NONE · airframe 107,505 hrs · 15,417 cycles

SHIP 1200 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:602, CORRECTIVE ACTION: R-1 DOOR CKS NML (2414447)

Part: NONE — NONE · airframe 107,003 hrs · 15,330 cycles

SHIP 1200 ONE LEFT ENTRY DOOR WILL NOT ARM, CORRECTIVE ACTION: FOUND OUTSIDE HANDLE NOT STOWED REOPEN/CLOSE DOOR. DOOR OP CHKD OK PER B767 AMM 52-11 (9011752)

Part: SIGN — DAMAGED · airframe 106,001 hrs · 15,171 cycles

SHIP 1200 EXIT SIGN FACE MISSING AT CABIN LOCATION 801 AFT FACING SIDE. CORRECTIVE ACTION: INSTALLED EXIT SIGN AT CABIN LOCATION 801. (7990110)

Part: NONE — NONE · airframe 105,868 hrs · 15,146 cycles

" SUPPLMENTAL INFOMATION' SHIP 1200 #1 ENG OUTBOARD NACELLE STRUT ACCESS DOOR MISSING/ DAMAGED . CORRECITVE ACTION: FORWARD TO CDL 54-53-02 ACCESS DOOR PLACED IN FWD E&E M.C.O POUCH. INSTALLED NEW ACCESS DOOR PER B767 - 300 AMM 5453. AC OK FOR SVC (8717701)

Part: NONE — NONE · airframe 105,868 hrs · 15,146 cycles

'SUPPLMENTAL INFOMATION' SHIP 1200 ON ARRIVAL FOUND NACELLE STRUT ACCESS DOOS MISSING ON #1 ENGINE INBOARD SIDE. CORRECTIVE ACTION: FWD TO CDL 54-53-02. MCC CONTACTED. DISPATCH APPROVED. INSTALLED NEW ACCESS DOOR PER B767-300 AMM 54-53 AC OK FOR SVC. (8148037)

Part: NONE — NONE · airframe 105,298 hrs · 15,032 cycles

SHIP 1200 2R DOOR SLIDE ARM ISSUE. CORRECTIVE ACTION: OPS CHK #2R DOOR SLIDE PER AMM 52-73. ALL NORMAL. (8148006)

Part: NONE — NONE · airframe 105,140 hrs · 15,002 cycles

SHIP 1200 -ATB- DUE TO BEING AIRSPEED RESTRICTED AFTER TAKE OFF CORRECTIVE ACTION: FOUND ALTERNATE VMO/MMO SWITCH IN ALTERNATE POSITION. REPOSITIONED. A/C RTS. (8306828)

Part: NONE — NONE · airframe 104,459 hrs · 14,866 cycles

SHIP 1200 OVERHEAD EXIT SIGN MISSING AT SEAT ROW 13 LH SIDE. CORRECTIVE ACTION: INSTALLED EXIT SING LENS, CHECK GOOD PER B767 AMM 33-51 (2011775)

Part: NONE — NONE · airframe 104,459 hrs · 14,866 cycles

SHIP 1200 OVERHEAD EXIT SIGN MISSING AT SEAT ROW 13 LH SIDE. CORRECTIVE ACTION: INSTALLED EXIT SING LENS, CHECK GOOD PER B767 AMM 33-51 (8023976)

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 103,439 hrs · 14,654 cycles

SHIP 1200 EMERGENCY LIGHTS AT SEATS 19AB ARE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT SEAT BASE NEXT TO KICK PANEL. REPAIRED WIRE. SYSTEM OPERATION IS NORMAL.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 101,749 hrs · 14,265 cycles

MAINTENANCE FOUND ALL 24 BULBS BURNT OUT BETWEEN THE EXIT SIGNS AT CREW REST LADDER AND COMMON AREA AND REPLACED BULBS.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 99,960 hrs · 13,845 cycles

CREW REST LADDER AND COMMON AREA EMERGENCY EXIT SIGNS INOPERATIVE. FOUND ALL 24 BULBS BURNT OUT BETWEEN BOTH SIGNS AND RELAMPED.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 99,481 hrs · 13,767 cycles

SHIP 1200 - DIV - TO SEA DUE LEFT HYD QTY DROPPING. CORRECTIVE ACTION: LT ELEC PUMP PRESSURE FILTER DPI FOUND LEAKING. REPLACED DPI O RING PER B767 AMM 29-11-17. LP 6742890

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 96,028 hrs · 13,289 cycles

DENT ON RIGHT WING I/B AFT FLAP LOWER SURFACE APPROXIMATELY 36" O/B AND 6" I/B PF T/E FOUND TO BE OUT OF LIMITS. REPAIRED PER SRM 57-53-01. (LP 1015922)

Part: NONE — NONE (NONE) · airframe 108,534 hrs · 15,617 cycles

AD 2018-11-14 AMOC APPROVAL REQUIRES REPETITIVE INSPECTIONS EVERY 12000 CYCLES OR 32000 HOURS (WHICHEVER OCCURS FIRST) PER ERA 576744-14AD. ACCOMPLISHED REPETITIVE INSPECTION AS PER ER/A 576744-14AD REV B SECTION II . FOUND NO CRACK.

Part: MODULE — DEFECTIVE (EVAC SLIDE) · airframe 95,540 hrs · 13,221 cycles

SLIDE INDICATOR LIGHT IS INOPERATIVE. REPLACED ALARM SIGNAL MODULE. SYSTEM OPERATION IS NORMAL.

Part: MODULE — DEFECTIVE (R2 DOOR) · airframe 95,365 hrs · 13,197 cycles

R2 DOOR SLIDE INDICATION LIGHT LAMP INOPERATIVE. REPLACED ALARM SIGNAL MODULE AT DOOR. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 94,035 hrs · 13,013 cycles

EMERGENCY FLOOR LIGHTING AT 23B IS INOPERATIVE. MAINTENANCE RE-SECURED LIGHT. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 94,035 hrs · 13,013 cycles

EMERGENCY FLOOR LIGHTING INOPERATIVE AT SEAT 24B. RE-SECURED LIGHT. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — DETACHED (SEAT 19B) · airframe 93,669 hrs · 12,966 cycles

EMERGENCY LIGHTS ARE HANGING BY WIRE FROM SEAT WALL BY WIRING. SECURED LIGHT PANEL TO SEAT 19B. SYSTEM OPS NORMAL.

Part: UNKNOWN — MALFUNCTIONED (NR 1 ENGINE) · airframe 91,446 hrs · 12,680 cycles

STARTING LEFT (1) ENG PUSH CREW OBSERVED SPARKS ABORTED ENG START TOWER OBSERVED SMOKE ENG STARTED NORMAL UNTIL GET STAGNATED THEN TUG CREW REPORTED OBSERVATIONS. DRY RUN ENG FOUND LEFT STARTER FAULTY AND REPLACED.

Part: CABLE — DISCONNECTED (CABIN) · airframe 90,190 hrs · 12,513 cycles

EMERGENCY EXIT LIGHTS AT SEAT 41FG ARE INOPERATIVE. RECONNECTED CABLE. SYSTEM OPERATION IS NORMAL.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 89,790 hrs · 12,463 cycles

EMERGENCY LIGHT AT SEAT 35G HAS WIRE PULLED OUT OF PLUG. REPINNED PLUG. SYSTEM CHECKS NORMAL.

Part: LIGHT — UNSECURE (CABIN) · airframe 89,307 hrs · 12,405 cycles

EMERGENCY FLOOR LIGHTING INOPERATIVE AT 38F. SECURED THE LIGHTING. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 87,652 hrs · 12,199 cycles

COCKPIT EMERGENCY EXIT SIGN IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. SYSTEM OPERATION IS NORMAL.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 87,568 hrs · 12,185 cycles

NR 1 PYLON FWD UPPER SPAR WEB HYD LINE CUTOUT FOUND CRACKED . REPAIRED ER ERA 55744-14. (LP 2965479)

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 87,568 hrs · 12,185 cycles

DURING HCK AT STAG, 2 CRACKS WERE FOUND ON THE FWD UPPER SPAR WEB ASSEMBLY ON THE NR 1 PYLON, STA 182-192. REPAIR PERFORMED PER SECTION 1 OF ER/A.

Part: FAILSAFE — CRACKED · airframe 87,568 hrs · 12,185 cycles

DURING INSPECION OF THE FAILSAFE STRAP A CRACK INDICATION WAS FOUND AT THE LOWEST FASTENER HOLE. THE FAILSAFE STRAP WAS REPAIRED.

Part: FAILSAFE — CRACKED (BS 955) · airframe 87,568 hrs · 12,185 cycles

DURING INSPECTION OF THE BS 955 FAILSAFE STRAP, A CRACK INDICATION WAS FOUND DURING THE OPEN HOLE INSPECTION, AT THE LOWEST OF THE THREE FASTENER HOLES. THE FAILSAFE STRAP WAS REPAIRED.

Part: FAILSAFE — CRACKED (BS 955) · airframe 87,568 hrs · 12,185 cycles

DURING REPAIR OF THE RT BS 955 FAILSAFE STRAP SURFACE, A HFEC INSPECION OF THE FAILSAFE, A CRACK INDICATION WAS FOUND. TEH FAILSAFE WAS REPAIRED.

Part: NOT REPORTED — CRACKED (WING) · airframe 87,568 hrs · 12,185 cycles

02EA FASTENER HOLE HAVE CRACK INDICATIONS DETECTED BY HFEC INSPECTION AFTER OVERSIZING TO 0.288 INCH. ACCOMPLISH 5724-01010 SECTION 18.

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 87,568 hrs · 12,185 cycles

AFT CARGO AT BS 1197, BETWEEN STRINGERS 37 - 38L FOUND THE SHEAR TIE CORRODED. THE SHEAR TIE WAS REMOVED AND REPLACED.

Part: STRINGER — CRACKED (WING) · airframe 87,568 hrs · 12,185 cycles

CRACK FOUND IN THE WING AND THE INTERNAL STRINGER HAS HOLES HAVE BEEN OVERSIZED. ACCOMPLISHED 5724-01010 SECTION 24.

Part: SHEAR TIE — CORRODED (BS 742) · airframe 87,568 hrs · 12,185 cycles

FWD CARGO AT BS 742 BETWEEN STRINGER 38 - 39R. FOUND A CORRODED SHEAR TIE. REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (NOT REPORTED) · airframe 87,568 hrs · 12,185 cycles

BETWEEN STRINGERS 35-36R, FOUND THE SHEAR TIE CORRODED. THE SHEAR TIE WAS REMOVED AND REPLACED.

Part: STIFFENER — CRACKED (RT WING) · airframe 87,568 hrs · 12,185 cycles

RT WING FRONT SPAR STIFFENER FOUND CRACK AT LES 821. REMOVED AND REPLACED PER SRM.

Part: SPAR — CHAFED (NR 2 PYLON) · airframe 87,568 hrs · 12,185 cycles

NR 2 PYLON FWD UPPER SPAR WEB FOUND CHAFING AT NAC STA 190 CHAFING. REPAIRED PER ERA 555743-14.

Part: SHEAR TIE — CORRODED (BS 1241) · airframe 87,568 hrs · 12,185 cycles

AFT CARGO AT BS 1241 BETWEEN STRINGERS 39L -39R, THE SHEAR TIE WAS FOUND CORRODED. R & R THE SHEAR TIE.

Part: FITTING — WORN (NR 1 PYLON) · airframe 87,568 hrs · 12,185 cycles

NR 1 PYLON AFT BULKHEAD FITTING O/B LOWER SURFACE FOUND WORN. DAMAGE REMOVED, MATERIAL THICKNESS OUT OF LIMITS. AREA REPAIRED PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 87,568 hrs · 12,185 cycles

HFEC SURFACE INSPECTION FOUND CRACK APPROXIMATELY 0.15 AS MARKED ON RT BS 859.5 RBL 89 BELOW WL 200 AT THE FRAME INNER CHORD TRANSITION RADIUS. REPAIRED AND ACCOMPLISHED AS PER W/C:5311-01195 09B.

Part: SKIN — CRACKED (LT WING) · airframe 86,459 hrs · 12,047 cycles

WING LT LOWER INSPAR SKIN STR L-6.5, RIB 31 CRACKS. CW PRI.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 78,744 hrs · 11,107 cycles

SERVICE CHECK CABIN EMERGENCY LIGHTS LT SIDE ROW 32-40 INOPERATIVE. MAINTENANCE REPLACED NR 3 FUSE ON BATTERY PACK LOCATED M9010.

Part: RELAY — DAMAGED (HEAT CONTROL) · airframe 67,687 hrs · 9,684 cycles

ABORTED TAKEOFF AT APPROX 100 KNOTS DUE TO CONTINUOUS FIRE BELL SOUNDING, NO OTHER FIRE INDICATIONS APPEARED. MX PEFORMED A SERIES OF TESTS, REPLACED DEFECTIVE R907, SMOKE DETECTOR CONTROL PANELS AND THE CARGO HEAT CONTROL RELAY. ACFT IS CONSIDERED AIRWORTHY AND IS READY FOR TEST FLIGHT.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 67,684 hrs · 9,683 cycles

MAIN DECK FLOORBEAM BS 287 BETWEEN RBL 18 AND RBL 21 UPPER TEE CORRODED. REPAIRED IAW SRM 53-00-51, FIG 201, REPAIR 1.

Part: FLOORBEAM — CRACKED (BS 1439) · airframe 67,684 hrs · 9,683 cycles

MAIN DECK BS 1439, LBL 24 FLOORBEAM LOWER FLANGE CRACKED. REPAIRED IAW ERA 502730-14, REV ORIG.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,543 hrs · 9,537 cycles

EMERGENCY LIGHTS AT SEAT 6GF-20GF ARE INOPERATIVE. THE BATTERY PACK AND FUSE M9011 WERE REPLACED. SYSTEM OPS NORMAL.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,503 hrs · 9,532 cycles

DURING DRC, FOUND EMERGENCY PATH LIGHTS AT SEAT 6GF AND 16GF TO 20GF INOPERATIVE. THE FUSE WAS REPLACED ON BATTERY CHARGER M9011. OPS CHKS GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,305 hrs · 9,503 cycles

EMERGENCY LIGHTS OUT SEAT ROW 6AB-19AB. REPLACED FUSES ON. EMERGENCY BATTERY CHARGER OPS CHECKED OK.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,305 hrs · 9,503 cycles

EMERGENCY LIGHTS OUT ROW 19 FG. REPLACED SEAT HARNESS FOR EMERGENCY LIGHT ASSY. OPS CHECKED OK.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,305 hrs · 9,503 cycles

EMERGENCY LIGHTS OUT ROW 20FG-30FG. REPLACED FUSES ON EMERGENCY BATTERY PACK. OPS CHECKED OK.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,706 hrs · 9,425 cycles

RED EMERGENCY LIGHT AT L1 COAT CLOSET IS INOPERATIVE. MAINTENANCE REPLACED THE FUSE AT BATTERY PACK M9008. SYSTEM OPERATION IS NORMAL.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 65,141 hrs · 9,348 cycles

EMERGENCY LIGHTS AT ROW 30AB ARE INOPERATIVE. MAINTENACE FOUND WIRE HARNESS PULLED OUT AND SECURED. SYSTEM OPS NORMAL.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 64,842 hrs · 9,311 cycles

EMERGENCY LIGHTS AT SEAT 30AB ARE INOPERATIVE. MAINTENANCE REPAIRED CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: PROBE — DEFECTIVE (TAT) · airframe 64,523 hrs · 9,268 cycles

ON TAKEOFF BY CAPTAIN, NO VNAV, LNAV, OR A/T OR LEFT/CETER A/P AND AIR SPEED BUGS INOP. RIGHT A/P WORKED WITH LNAV BUTNO A/T. HAND FLYING A/C A/S DID NOT MATCH WITH POWER CALLED MTC AND DISPATCHED PULLED AND RESET SEVERAL CIRCUIT BREAKERS NO HELP. 20 MINUTES LATER IN CRUISE ALL SYSTEMS RETURNED EVEN LEFT AND CENTER F/D. REPLACED TAT PROBE. SYSTEM OPS NORMAL.

Part: SKIN — CHAFED (FUSELAGE) · airframe 61,096 hrs · 8,829 cycles

RT HORZ STAB CUTOUT LWR AND FWD SKIN CHAFED AND REPAIRED PER SRM 53-80-01 REPAIR 3 FIG 201.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 61,096 hrs · 8,829 cycles

RT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING FOUND DELAMINATED. COMPOSITE REPAIR CARRIED OUT AS PER SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-03 FIG 5.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 61,096 hrs · 8,829 cycles

LT WING I/B MAIN FLAP O/B LEADING EDGE FAIRING FOUND DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-03 FIG 5.

Part: FLAP — DELAMINATED (LT WING) · airframe 61,096 hrs · 8,829 cycles

ADF 008-ON WALK AROUND FOUND FOD ON LEFT WING O/B FLAP ASSY I/B SIDE. LEFT WING O/B FLAP I/B SIDE DELAMINATED AREA COMPOSITE REPAIR CARRIED OUT AS PER SRM 57-53-01, REPAIR 1, FIG 201 AND SRM 51-70-06 FIG 9.

Part: ACCESS PANEL — CRACKED (AILERON) · airframe 61,096 hrs · 8,829 cycles

RT WING I/B AILERON ACCESS PNL SURFACE CRACKED AS MARKED. COMPOSITE HOT BOND REPAIR CARRIED OUT AT CRACKED AREA AS PER SRM 57-60-01 REPAIR 1 AND SRM 51-70-05, PAR 5A(1).

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,096 hrs · 8,829 cycles

CABIN RT STA 903 BETWEEN STR 20R AND STR 21R FRAME INNER CHORD CRACK REPAIR ACCOMPLISHED AS PER ERA 489714-14AD REV ORIG.

Part: SKIN — DENTED (TE FLAP) · airframe 61,096 hrs · 8,829 cycles

LT WING I/B TRAILING EDGE AFT FLAP LOWER SURFACE FOUND DENT MARK. METAL HOT BOND REPAIR PERFORMED ON DENTED AREA AS PER SRM 57-53-01 REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201.

Part: STRAP — CRACKED (FUSELAGE) · airframe 61,096 hrs · 8,829 cycles

LT STA 955 REAR SPAR BULKHEAD FAIL SAFE STRAP FASTENER HOLE CRACK. REPAIR ACCOMPLISHED AS PER ERA 489715-14AD REV ORIG.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 60,013 hrs · 8,688 cycles

SEAT MOUNTED EMERGENCY PATH LIGHTS AT 19AB ARE INOPERATIVE. MX REPAIRED A BROKEN WIRE. SYS OPS IS NORMAL.

Part: ENGINE — FAILED (LEFT) · airframe 59,954 hrs · 8,680 cycles

APPROX 400 FT AGL AND 190 KIAS APPROX, A LOUD BANG FROM THE LT ENGINE. RPM ROLLED BACK TO NEAR ZERO. ENGINE LT SHUTDOWN IAW CHECK LIST. R & R NR1 ENG IAW TRANS 1T148AD. OPS AND LEAK CK OK. ACFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,275 hrs · 8,475 cycles

DURING "A" CHECK THE COCKPIT EMERGENCY LIGHT FAILED OPS CHECK. REMOVED AND REPLACED COCKPIT DOOR EMERGENCY LIGHT ASSY, OPS CHECK GOOD (DL76L101900).

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 58,267 hrs · 8,474 cycles

LIGHTNING STRIKE AT FS 1197+100 AT STR 30 REPAIRED PER SRM 53-00-01 REPAIR 1. SDR REQUIRED PER REQUIREMENTS TABLE. THIS IS A REWORKED REPAIR DUE TO FAA FINDING. THE ORG REPAIR WAS COMPLETED ON N/R 5 MAR15, 2010 AN SDR WAS NOT SUBMITTED AT THAT TIME (DL76L101896).

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 58,083 hrs · 8,451 cycles

DURING DRC FOUND EMERGENCY PATH LIGHTS AT 21B INOPERATIVE. MX SECURED LOOSE CONNECTOR. SYS OPS IS NORMAL.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,859 hrs · 8,422 cycles

ROWS 19 GF THRU 32 GF EMERGENCY LIGHTS INOP. REPLACED FUSE IN BATTERY PACK POWER SUPPLY.

Part: FRAME — DAMAGED (FS 303) · airframe 57,625 hrs · 8,390 cycles

DURING ACCOMPLISHMENT OF EA 01-455913-03AD ME-01. FOUND THE FRAME MISDRILLED AT FS 303 AT OTBD FASTERENER COMMON TO PN 287N4648-72 BRACKET. THE SUBJECT HOLE HAS EDGE DAMAGE AND IS NEAR THE RADIUS AND 2 REMAINING HOLES HAVE A LOOSE FIT WHEN THEY SHOULD BE TRANSITION FIT. ERA 482740-14 WAS ISSUED TO MOVE THE BRACKET INBD 1 HOLE STEP UP THE TO EXISTING HOLES AND PLUG THE DAMAGED HOLE WITH A RIVET.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 55,929 hrs · 8,170 cycles

RTB DUE TO ADP FAILED ON TAXI OUT, FWD TO MCO IAW MEL 29-11-03. R & R CTR ADP IAW MM. R & R M1057 OVERSPEED CARD IN P50 CARD FI ALL OPS NML. MCO PLAC RMVD. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: COMPUTER — MALFUNCTIONED (AILERONS) · airframe 55,785 hrs · 8,151 cycles

RUDDER RATIO AND AILERON LOCKOUT EICAS MESSAGE AND LIGHT ON OVERHEAD. ALSO L.C. AND R AUTOPILOTS WOULD NOT ENGAGE. T/S FOUND FAULT BALL SHOWS ON BOTH SAM. RESET AND PERFORMED MCDP TEST 1/30/40/65. FAILED FCCR SAM. ALSO FAULT BALL SHOWS ON RT SAM. R & R RT SAM MM. PERFORMED MCDP TEST 1/30/40 AND 65. ALL PASS NO FAULT BALL SHOWS ON SAM. ALL CHECK OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: MODULE — MALFUNCTIONED (RUDDER) · airframe 55,785 hrs · 8,151 cycles

RUDDER RATIO AND AILERON LOCKOUT EICAS MESSAGE AND LIGHT ON OVERHEAD. ALSO L/C/ AND R AUTOPILOTS WOULD NOT ENGAGE. T/S FOUND FAULT BALL SHOWS ON BOTH SAM. RESET PERFORMED MCDP TEST 1/30/40/65. FAILED FCC R SAM. ALSO FAULT BALL SHOWS ON RT SAM. R & R RT SAM IAW MM. PERFORMED MCDP TEST 1/30/40 AND 65. ALL PASS NO FAULT BALL SHOWS ON SAM. ALL CHECK OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: START VALVE — FAILED (NR 2 ENG) · airframe 55,252 hrs · 8,083 cycles

RT ENG START VALVE WILL NOT OPEN. REMOVED AND REPLACED START VALVE IAW MM, CHECKS NORMAL.

Part: WINDOW — CRACKED (COCKPIT) · airframe 54,870 hrs · 8,034 cycles

AT 33000 FT AND 3HRS INTO FLIGHT RT FWD WINDOW HEAT COMPONENTS BEGAN TO GLOW AND ARC. OUTER WINDSCREEN PANEL THEN CRACKED AND RT FWD WINDOW HEAT WAS IN REMOVAL OF RT FWD COCKPIT WINDOW SCREENS. REMOVED AND INSTALLED WINDOW PER AMM 56-11-01-404. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: ENGINE — HUNG START (NR 2) · airframe 54,224 hrs · 7,953 cycles

RIGHT ENG HUNG AT 46 PERCENT, N2 THEN FINALLY ACCEL TO IDLE. EEC C1 FAULT STATUS MSG. SHUTDOWN ENG PER MCC REQUEST AND RESTARTED. ENG WOULD NOT START. ENG HUNG AT 36 PERCENT N2 LOW FF AND LOW EGT NOTED. RTB FOR MTC.

Part: LINE — LEAKING (NR 1 GENERATOR) · airframe 53,978 hrs · 7,923 cycles

LEFT ENGINE GENERATOR KICKED OFF WHILE TAXIING OUT. ON ARRIVAL FOUND LT GEN OIL EMPTY. FOUND LEAK ON MAIN SUPPLY LINE AND DRAIN FITTING. ADJ PER AMM. RAN ENG AND SERVICED IDG PER AMM. NOW ALL NORMAL. GEN COMES ONLINE. A/C OK FOR SERVICE.

Part: ENGINE — HUNG START (NR 2) · airframe 53,456 hrs · 7,862 cycles

RT ENG HUNG START AT 52 PERCENT N2, MAX EGT 487. STARTED ENGINE AT GATE. ALL INDICATIONS NORMAL.

Part: CONNECTOR — DISCONNECTED (TRIM VALVE) · airframe 52,414 hrs · 7,729 cycles

FWD TRIM AIR VALVE INOP. UNABLE TO FLIGHT CREW PLACARD PER MED 21-61-04A. RESEATED CONNECTOR FWD TRIM VALVE. OPS NORMAL.

Part: CONNECTOR — LOOSE (FWD TRIM AIR) · airframe 52,414 hrs · 7,729 cycles

FWD ZONE TEMP INOP. RESEATED CONNECTOR FWD TRIM VALVE. OPS NORMAL.

Part: UNKNOWN — UNKNOWN (APU) · airframe 44,440 hrs · 6,750 cycles

APU FAULT AND SHUTDOWN ON ENGINE START. BITE CHECK OF APU ECU SHOWS NO FAULTS, APU SHUTDOWN OCCURRED ON ENGINE START WITH AIR DEMAND. FWD APU PNEU TO MCO PER MEL49-11-01C. ECU SHOWS NO FAULTS. REPLACED SCV AS PREVENTIVE MEASURE PE M/M. MOTORED ENG 2 TIMES CKS OK MCO AND PLACARD REMOVED.

Part: INDICATOR — INOPERATIVE (VSI) · airframe 43,696 hrs · 6,657 cycles

CAPT VSI INOP ON TAXI-OUT APPROX 20 MIN INTO TAXI. REPLACED CAPTS VSI PER AMM. OPS CHK NML. PART ROBBED FROM A/C 173. MPN 066-50001-1001 S/N 10139 CAPT POS. AC RTB TWICE FOR SAME PROBLEM. FIRST IND REMOVED AND REPLACED WITH PREV SHOPHIST. 2ND IND SAME THING BUT DIFFERENT SHOP HIST. C/B WAS ALSO REMOVED AND REPLACED ON 1ST RTB DUE TO ELEC FUME REPORTED. CONNECTOR AND WIRING WERE CHECKED PRIOR TO 3RD IND. REPLACED C/B C586 AND REPLACED CAPT IVSI PER AMM. OPS CHK NML, NO FUMES PRESENT.

Part: INDICATOR — FAILED (COCKPIT) · airframe 43,696 hrs · 6,657 cycles

CAPT VSI INDICATOR FAILED ON TAXI OUT ELECTRICAL FUMES WERE PRESENT PULL CB SMELL DISSIPATED. REPLACED C/B C586 AND REPLACED CAPT VSI PER AMM OPS NML. NO FUMES PRESENT. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: ENGINE — OIL CONSUMPTION (NR 2) · airframe 42,623 hrs · 6,521 cycles

NR 2 ENGINE OIL CONSUMPTION BEYOND AMM LIMITS, PER FIM 71-08-00 PAGE 132 OPENED AND INSPECTED NR 4 BEARING COMPT 614338. NO LEAKAGE AT BEARING COVER. RETORQUED NR 4 BEARING SCAVENGE LINES. PERFORMED ENGINE RUN TEST 13. NO GOOD OIL PUDDLING FWD OF LPT LAST STAGE. REPLACED NR 2 ENGINE PER 1T149AD.

Part: WIRE — DAMAGED (NR 2 ENGINE) · airframe 39,675 hrs · 6,163 cycles

ON TAKEOFF ROLL, RT ENG OIL FILTER STATUS MSG RTO AT 105KTS. FOUND WIRE W3510-26-18 INSULATION DAMAGED AND GROUNDING TO FRAME REPAIRED INSULATION PER BSWPM AND REPOSITION CLAMP 429845. REPLACED MAIN OIL FILTER, NO METAL FOUND INSP ALL CHI DETECTORS NMF. REPLACED DIFF PRESSURE SWITCH 966400 RAN ENG T/O PWR LEAK CHECK GOOD. NO MSG OK FOR SVC.

Part: STARTER — INOPERATIVE (NR 1 ENGINE) · airframe 39,648 hrs · 6,160 cycles

NO N1 OR N2 DURING LEFT ENGINE START. START VALVE LIGHT DID NOT CYCLE. REPLACED STARTER PER AMM. SPUN ENGINE TO 26 PERCENT. STARTER CKS GOOD.

Part: PUMP — MALFUNCTIONED (HYDRAULIC SYS) · airframe 39,125 hrs · 6,097 cycles

C1 HYD PUMP LOW PRESSURE LIGHT ON. REPLACED C1 PUMP, OPS AND LEAK CHKS OK PER M/M.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 38,883 hrs · 6,069 cycles

ON ETOPS DRC FOUND RT WING EMERGENCY LIGHT INOP, JUST FWD OF C2 DOOR. RELAMPED CK OK.

Part: INDICATOR — FAILED (COCKPIT) · airframe 38,756 hrs · 6,051 cycles

CAPT VSI OVERHEATED AND CAUSED SMOKE ODOR IN THE COCKPIT. REMOVED AND REPLACED LEFT VSI, ALL CHECK NORMAL.

Part: CARBON SEAL — DAMAGED (NR 1 ENGINE) · airframe 36,857 hrs · 5,820 cycles

CREW REPORTED SOMKE/SMELL DURING T/O AND AGAIN ON APPROACH INTO ATL. REPLACED FRONT CARBON SEAL ON NR 1 ENGINE.

Part: BOLT — SHEARED (LT MLG) · airframe 32,539 hrs · 5,240 cycles

MLG WHEEL TIE BOLT SHEARED. REPLACED WHEEL ASSY.

Part: ENGINE — FAULTY (NR 2) · airframe 31,306 hrs · 5,067 cycles

NR 2 ENGINE REPLACED DUE TO HIGH OIL CONSUMPTION.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 28,514 hrs · 4,679 cycles

EMERGENCY LIGHT ASSY M9009 INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER BASE. EMERGENCY LIGHT OPS CHECK NORMAL.

Part: COFFEEMAKER — UNSERVICEABLE (GALLEY) · airframe 28,158 hrs · 4,623 cycles

ELECTRIC BURNING ODOR NEAR LOCATION 409. FOUND HOTPLATE CONNECTION ON NR 2 COFFEEMAKER BROKEN. REPLACED COFFEEMAKER, OPS NORMAL.

Part: LIGHT — SHORTED (AFT GALLEY) · airframe 25,602 hrs · 4,244 cycles

ON TAKEOFF OVERHEAD AFT GALLEY LIGHT SHORTED, HAD AN AUDIBLE POP, PUFF OF SMOKE, AND SPARK FROM LIGHT. REMOVED POWER FROM THAT AREA OF GALLEY. NO FURTHER PROBLEMS. INSPECTED LIGHT AT LT SIDE OF AFT GALLEY. F/A REPORTED AREA. LIGHT AND COFFEEMAKERS FUNCTION NORMAL. FOUND NO SHORTED WIRES OR BURN MARKS OR SMELL. OK FOR SERVICE.

Part: APU — SMOKE (AFT) · airframe 24,957 hrs · 4,147 cycles

SMOKE IN CABIN WHEN APU STARTED AT GATE PRIOR TO PUSH BACK. SHUT DOWN APU SMOKE CEASED. FOUND OIL IN APU EXHAUST, APU CHANGE IN PROGRESS.

Part: ENGINE — BIRD STRIKE (RIGHT) · airframe 24,673 hrs · 4,105 cycles

BIRDSTRIKE RT ENGINE. HIGH VIBES DURING CLIMB UP TO 3.8 N1.DUMPED 33K POUNDS FUEL. OVERWEIGHT LANDING AT SINK RATE OF 100FPM. ENGINE SHUT DOWN AFTER LANDING. BLADE DAMAGE FOUND ON THREE BLADES. LPC AND HPC BOROSCOPE PERFORMED IAW M/M. NO DEFECTS NOTED. FULL SET OF FAN BLADES REPLACED IAW M/M. ENG. RUN AND VIBE SURVEY IAW M/M. ALL SATISFACTORY. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: ODOR — DETECTED (CABIN) · airframe 24,590 hrs · 4,090 cycles

FLIGHT ATTENDANT REPORTED A SLIGHT BURNING PLASTIC ODOR AROUND ROW 24 ON THE COPILOTS SIDE. IT WENT AWAY IN 2 MIN. NO OTHER INDICATIONS. INSPECTED ALL AREAS AND UNABLE TO DUPLICATE, INSPECTED ALL AREA AND UNABLE TO DUPLICATE. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: OVEN — FAULTY (GALLEY) · airframe 22,783 hrs · 3,762 cycles

INBOUND OVEN ON FIRST OFFICERS SIDE IN AFT GALLEY WAS ON FIRE AND FLAMES WAS SHOOTING OUT FROM GRILL ABOVE THE OVEN. FLT ATTENDANTS TURNED OFF OVEN AND FLAMES STOPPED. CIRCUIT BREAKERS WERE PULLED LATER. FOUND NR 4 OVEN POWER WIRES BURNED. REMOVED AND REPLACED NR 4 OVEN. CANNON PLUG OK, NO DAMAGE FOUND. CHECKED NEW OVEN, CHECKS OK. BURNED WIRES PART OF THE OVEN UNIT.

Part: ENGINE — STALLED (NR 1) · airframe 22,658 hrs · 3,737 cycles

NR 1 ENGINE 2 AUDIBLE COMPRESSOR STALLS ON T/O FROM DUB...ACFT RETURNED MTC IN PROGRESS. REPLACING NR 1 ENGINE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 17,313 hrs · 2,776 cycles

BATTERY CHARGER MID-LEFT CABIN INOP.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 14,873 hrs · 2,404 cycles

SEAT 25 FG EMERGENCY LIGHT INOP. REPLCED SEAT HARNESS AND BATTERY CHARGER M733

Part: FAN — FAILED (CARGO BAY) · airframe 12,362 hrs · 1,994 cycles

DURING TAXI-OUT, F/A CALLED COCKPIT AND SAID THERE WAS A BURNING ODOR CAPT SIDE BEHIND MID GALLEY NEAR CNTR LAVS. REPLACED LEFT RECIRC FAN.

Part: LIGHT — INOPERATIVE (SEAT 29)

SEAT 29F WHITE EMERGENCY LIGHT INOP. REPLACED WIRING HARNESS, SYSTEM CHECKS GOOD.

Part: ENGINE — FAILED (NR 2)

FOUND METAL ON NR 3 BEARING CHIP DETECTOR. REPLACED ENGINE.

Part: IDG — FAILED (NR 2 ENGINE)

RIGHT GEN DRIVE LIGHT CAME ON DURING CLIMBOUT. REPLACED RIGHT IDG, OPS CHECK NORMAL.