N176DN

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 138,280 hrs · 20,036 cycles

AIRCRAFT 0176, DURING SERVICE CHECK, FOUND EMERGENCY EXIT SIGN LENS MISSING AT 17G. CORRECTIVE ACTION: REPLACED EMERGENCY EXIT SIGN LENS PER B767 AMM 33-51. (LP 5053789)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 138,181 hrs · 20,015 cycles

SHIP 176 SEAT 27B HAS WHITE EMERGENCY EXIT LIGHT INOP. CORRECTIVE ACTION: REMOVED & REPLACED EMERGENCY ESCAPE PATH LIGHT ON SEAT 27B IAW B767-300 AMM 33-51. OPS CHK GOOD. (5053748)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 138,126 hrs · 20,000 cycles

SHIP 176 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:604. CORRECTIVE ACTION: RESECURED AS NECESSARY. OPS CHECKS NML. OK TO CONT IN SVC (0104325)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 137,856 hrs · 19,937 cycles

SHIP 176 2L DOOR SLIDE ARM LIGHT NOT EXTINGUISHING. CORRECTIVE ACTION: PERFORMED OPS CHECK ON 2L DOOR LIGHT ARM INDICATION PER B767-300 AMM 52-73. OPS CK GOOD, A/C OK FOR SVC. (5064168)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 137,472 hrs · 19,868 cycles

SHIP 176 DURING SVC CHK FOUND EMERGENCY LIGHTS AT SEATS 17GF, 18GF, 19GF, 20GF INOP. CORRECTIVE ACTION: C/W ERA 612680-14 SECTION 1 PERMANENT REPAIR. (4469338)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 137,403 hrs · 19,858 cycles

SHIP 176 F/A'S REPORT THAT SEVERAL PAX IN LAST ROW SMELLED FUMES DURING TAXI. FURTHERMORE SERVAL F/A'S REPORTED THAT DURING DEPLANING THEY SMELLED THE FUMES ALSO NEAR BOTH AFT LAVS AND IN THE CREW REST COMPARTMENT. CORRECTIVE ACTION: AS PER MCC REQUEST PEFORMED INSP FOR LAV/ GALLEY VENT FANS/ AFT CHILLERS/ LAV WATER HEATER/ LAV FIRE EXT/ LAV LIGHTS AND PSU / LAV SMOKE DET/ VACCUM GEN/ E&E COMP PER B767-300 AMM 05-51-56. PERFORMED ENG RUN WHILE ISOLATING PACKS TO VERFIY FUMES OR ODOR SOURCE PER B767-300 AMM 71-00. NO ODOR OR FUMES DETECTED AT THIS TIME. A/C OK FOR SVC. (4469336)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 137,387 hrs · 19,855 cycles

SHIP 176 FA REPORT BURNING SMELL N AFT LAV LEFT SIDE. CORRECTIVE ACTION: INSPECTED AFT LAV PER B767-300 AMM 26-13. OPS CHK NML. NO ODOR DETECTED. (4469334)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 137,220 hrs · 19,825 cycles

SHIP 176 L3 DOOR EXIT SIGN COVER NEEDS TO BE INSTALLED. CORRECTIVE ACTION: REATTACHED MID LH OVERHEAD EMERGENCY LIGHT LENSE. (4468736)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 137,131 hrs · 19,810 cycles

SHIP 1706 DOOR 1L WON'T ARM. CORRECTIVE ACTION: OPS GOOD DOOR 1L. CHKD OK PER B767 AMM 52-11. (4571474)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 136,770 hrs · 19,751 cycles

SHIP 0176 - ATB - RETURNING TO LAX DUE TO F/O ALTIMETER INOP. CORRECTIVE ACTION: REMOVED & REPLACED F/O ALTIMETER. (4926131)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 136,209 hrs · 19,657 cycles

PYLON INBD NACELLE STRUT DOOR MISSING. CORRECTIVE ACTION: INSTALLED RT ENG PANEL 446AL PER B767 AMM 54-53 OK FOR SVC. CDL & PLAC RMVD

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,786 hrs · 19,590 cycles

SHIP 176 L1 DOOR WOULD NOT ARM CAPT. CORRECTIVE ACTION: CYCLED L1 ENTRY DOOR ARM MECHANISM PER B767 AMM 52-11. OPS CHK GOOD. OK FOR SVC (4803164)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,786 hrs · 19,590 cycles

SHIP 176 MAIN CABIN DOOR WOULD NOT FULLY CLOSE AND ARM. CORRECTIVE ACTION: CYCLED 1L PAX DOOR & ARMED PER B767-300 AMM 52-11. OPS CKS GOOD AT THIS TIME. (4803152)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,690 hrs · 19,571 cycles

SHIP 176 DURING SVC, FOUND EMERGENCY LIGHT OVERHEAD PANEL ROW 16E MISSING. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT PANEL ON ROW 16E. PER B767-300 AMM 33- 51. CHECKS GOOD. A/C OK FOR SVC (4803118)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,525 hrs · 19,541 cycles

SHIP 176 AFTER GATE ARRIVAL DOOR 2R SLIDE LIGHT FLASHING AFTER DISARMING DOOR. CORRECTIVE ACTION: OPS CK OF 2R DOOR GOOD NO ISSUES FOUND W/ ARM/DISARM OR SLIDE LIGHT. OK FOR SVC. REF B767 AMM 33-51 AND 25-66 (4683940)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,503 hrs · 19,535 cycles

SHIP 176 ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS: 1L. CORRECTIVE ACTION: FOUND SLIDE/ARMED INDICATOR FLAG HITTING UPPER DOOR LINER PANEL. ADJUSTED SLIDE/ARMED INDICATOR FLAG AS PER B767 AMM 52-11-00/ 501. 1L DOOR NOW ARMS / DISARMS NORMALLY (2732943)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,497 hrs · 19,534 cycles

SHIP 176 ROW 16 CDE EMERGENCY LIGHT LENS COVER MISSING. CORRECTIVE ACTION: INSTALLED REPLACEMENT COVER PER B767-300 AMM 33-51. OPS NML. (4683916)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,476 hrs · 19,531 cycles

SHIP 176 L1 DOOR HARD TO ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR FITTINGS. CYCLED DOOR AND ARMING LEVER WITH NO ISSUES. REF B767AMM 25-66. (4683902)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,355 hrs · 19,509 cycles

SHIP 176 UNABLE TO ARM DOOR 1L. HANDLE CLOSE BUT FLAG WILL NOT SHOW. CORRECTIVE ACTION: NO TROUBLE FOUND. OPERATED DOOR ARMING SYSTEM AND DISARMING OF L1 DOOR OK PER B767 AMM 25-66 (4823924)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,172 hrs · 19,481 cycles

SHIP 176 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. CORRECTIVE ACTION: SECURED SAME ALL IS NRML (2687342)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,105 hrs · 19,468 cycles

SHIP 176 MAIN CABIN DOOR 1L, POSITION FAILS TO ARM PROPERLY. CORRECTIVE ACTION: ADJUSTED PAWL MECHANISM IAW B767 AMM 52-11. OPS CHECK GOOD. OK FOR SERVICE. (5118508)

Part: NONE — NONE · airframe 134,798 hrs · 19,416 cycles

SHIP 176 FA REPORTED 1L DOOR UNABLE TO ARM. CORRECTIVE ACTION: OPENED & CLOSED THE 1L DOOR AS PER B767-300 AMM 52-11. ARMED & VERIFIED DOOR ARMED. OPS CK GOOD. (9478966)

Part: DOOR — FOD (R1) · airframe 134,459 hrs · 19,350 cycles

FLT ATTENDANT UNABLE TO ARM 1R DOOR. FOUND FOD BLOCKING ARMING MECHANISM PERFORMED OPS CHECK OF 1R DOOR ALL OPS NML. REF B767-300 AMM 52-73.

Part: SWITCH — OUT OF POSITION (VMO/MMO) · airframe 134,270 hrs · 19,315 cycles

ATB DUE TO DUAL AIRSPEED LIMIT RESTRICTED. LANDED OVERWEIGHT. ALT VMO/MMO SWITCH WAS NOT IN CORRECT POSITION. REPOSITIONED SWITCH.

Part: GIRT BAR — FOD (L1 DOOR) · airframe 134,256 hrs · 19,313 cycles

PRIOR TO DEPARTURE CREW REPORTS L1 DOOR WONT ARM. FOUND DEBRIS IN GIRT BAR INSERT. REMOVED DEBRIS FROM DOOR. DOOR OK FOR SVC.

Part: LENS — DETACHED (EXIT SIGN) · airframe 134,193 hrs · 19,302 cycles

EMERGENCY EXIT ROW SIGN COVER FELL OFF. RESECURED EMERGENCY EXIT ROW SIGN COVER AS REQD. OK FOR SVC.

Part: LEVER — LOOSE (DOOR) · airframe 133,713 hrs · 19,209 cycles

SHIP 176 R WING SLIDE ADV MESSAGE ON DESCENT AND ARRIVAL. DURATION 1-2 MIN THEN EXTINCUISUES. CORRECTIVE ACTION: FOUND UNLOCK LEVER ON INTEGRATOR TO BE LOOSE & CAUSING TARGET TO MOVE AWAY FROM SENSOR S199.R/R INTEGRATOR PER B767-3 AMM 25-65 (9408278)

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 133,713 hrs · 19,209 cycles

SHIP 176 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:104. RE-ATTACHED EMERG EXIT SIGN COVER. OK FOR SVC.

Part: NOT REPORTED — OUT OF ADJUST (RT WING SLIDE) · airframe 133,713 hrs · 19,209 cycles

SHIP 176 INTERMITTENT R WING SLIDE EICAS MSG DURING APPROACH. R/R S219 PER SWPM CH 20 & ADJUSTED PER B767 AMM 52-71. ARMED OFF WING ESCAPE SYS . PERFORMED OP'S TEST. ALL CHKS GOOD (9408274)

Part: NONE — NONE · airframe 133,697 hrs · 19,206 cycles

SHIP 176 R. WING SLIDE, INTERMITANT INFLIGHTCORRECTIVE ACTION: T/S PER B767 FIM 52-71-00. PSEU HAD CARD FAULTS. R/R PSEU PER B767 AMM 32-09. OK FOR SVC. (9408264)

Part: DOOR LATCH — FAULT MESSAGE · airframe 133,614 hrs · 19,190 cycles

SHIP 176 R WING SLIDE EICAS MSG APPEARED INTERMITTENTLY, CORRECTIVE ACTION: T/S IAW B767 FIM 52-71-00-815-816. FOUND R OFFWING SLIDE COMPARTMENT DOOR LATCH 2 AND 3 DEFECTIVE. R/R #2 , #3 R OFF-WING SLIDE COMPARTMENT DOOR LATCH PER B767 AMM 25-65-09. PERFORM R OFF-WING SLIDE COMPARTMENT DOOR LATCH INSTALLATION TEST. OPS CHECK NORMAL IAW B767 AMM 25-65-09. RIGHT OFFWING SLIDE DOOR LATCH #2& #3 INSTALLED PER B767 AMM 25-65-09. OFF WINGS SLIDE REARMED PER B767 AMM 25-65-00 (2460287)

Part: NONE — NONE · airframe 133,413 hrs · 19,151 cycles

SHIP 176 DURING BOARDING, F/A FOUND EXIT LIGHT COVER @ SEAT 20A TO BE BROKEN. PLASTIC CLIP IS CRACKED. CORRECTIVE ACTION: RE-INSTALLED COVER AT 20A. OK FOR SVC. (8581424)

Part: NONE — NONE · airframe 133,320 hrs · 19,133 cycles

SHIP 176 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:17L. CORRECTIVE ACTION: RE-SECURED EMERGENCY EXIT SIGN COVER AT 17L. OK FOR SVC (2437978)

Part: NONE — NONE · airframe 133,261 hrs · 19,120 cycles

SHIP 176 "R WING SLIDE" EICAS MSG DISPLAYED INTERMITTENTY IN CRUISE. FA VERIFIED VISUALLY SLIDE NOT DEPLOYED PER QRH PROCEDURE, CORRECTIVE ACTION: PERFORMED SENSOR TARGET TEST PER B767 SSM 32-09-01. ON SENSOR #193 AND SENSOR #217 BOTH TARGETS NEST NEAR. NO CURRENT MESSAGES ON EICAS. NO HISTORY. (8580548)

Part: NONE — NONE · airframe 133,063 hrs · 19,080 cycles

SHIP 176 NO.10 SLAT ANTI-ICING DUCT I/B BRACKET FOUND CRACK. CORRECTIVE ACTION: REPAIRED THE CRACKED BRACKET AT NO.10 SLAT ANTI-ICING DUCT I/B AS PER PRI 601398-14 (2377880)

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

SHIP 176 CORROSION FOUND ON THE CABIN SEAT TRACK AT LBL57.4 INCH AFT OF STA 412, CORRECTIVE ACTION: THE DAMAGED SEAT TRACK REPLACED AS PER B767-300 SRM 51-40-02 (2377473)

Part: NONE — NONE · airframe 133,063 hrs · 19,080 cycles

SHIP 176 CORROSION FOUND ON THE WING CENTER SECTION UPPER SKIN UPR SURFACE AT STA 955 RBL 71,WHICH IS UNDER THE VENT TUBE PORT. CORRECTIVE ACTION: REPAIRED THE CORROSION ON THE WING CENTER SECTION UPPER SKIN UPR SURFACE AT STA 955 RBL 71 AS PER PRI 601144-14 (2377874)

Part: NONE — NONE · airframe 133,063 hrs · 19,080 cycles

SHIP 176 FOUND OUT CRACK ON NO.4 SLAT EXTERNAL SURFACE ADJACENT TO LOWER FWD TO AFT NO.1 RIVET HOLE 76 INCHES TO I/B EDGE. CORRECTIVE ACTION: REPAIRED THE CRACKED ON NO.4 SLAT EXTERNAL SURFACE ADJACENT TO LOWER FWD TO AFT NO.1 RIVET HOLE 76 INCHES TO I/B EDGE AS PER B767-300 SRM 57-43-01 (2377908)

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

SHIP 176 FOUND FWD CARGO DOOR CUTOUT SURROUND STRUCTURE INNER CHORD CORROSION AT STA478 - STA500. CORRECTIVE ACTION: CARRIED OUT THE REPAIR FOR THE INNER CHORD AND THE FAIL SAFE STRAP AT LWR SILL OF FWD CARGO DOOR SURROUNDING STRUCTURE AS PER PRI 601307-14 REV.0. (2375895)

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

SHIP 176 CORROSION FOUND ON THE CABIN FLOOR BEAM UPR CHORD AT STA1480, LBL50, CORRECTIVE ACTION: CARRIED OUT THE REPAIR TO THE FLOOR BEAM UPPER CHORD AS PER B767-300 SRM53-00-51 (2375801)

Part: NONE — NONE · airframe 133,063 hrs · 19,080 cycles

SHIP 176 CORROSION FOUND ON THE ATTACH ANGLE OF THE GAP AREA BETWEEN THE WING CENTER SECTION UPR SURFACE AND THE MAIN LANDING GEAR WHEEL WELL UPR SURFACE. CORRECTIVE ACTION: CORROSION REMOVED AND REPAIRED AS PER PRI 601203-14 (2374727)

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

SHIP 176 CORROSION FOUND ON THE CABIN FLOOR BEAM UPR CHORD AT STA1480, LBL50, CORRECTIVE ACTION: CARRIED OUT THE REPAIR TO THE FLOOR BEAM UPPER CHORD AS PER B767-300 SRM53-00-51 (2373588)

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

SHIP 176 SEAT TRACK- CORROSION FOUND ON THE SEAT TRACK AT RBL88, BETWEEN STA1197 AND STA1197+44, CORRECTIVE ACTION: THE DAMAGE SECTION OF SEAT TRACK CUT OUT AT STA 1197+11 AND REPAIRED AS PER B767-300 SRM 53-00-52 (2373470)

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

SHIP 176 CORROSION FOUND ON THE SEAT TRACK AT RBL88, 4 INCH FWD OF STA1439, CORRECTIVE ACTION: REPLACED THE SEAT TRACK AT STA 1439 RBL88.5 AS PER B767-300 SRM51-40-02 (2373570)

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

SHIP 176 CORROSION FOUND ON THE CABIN SEAT TRACK AT STA368, RBL88, CORRECTIVE ACTION: THE SEAT TRACK REPLACED AS PER B767-300 SRM51-40-02 (2373579)

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1197+88 S36R-S37R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.056". THE REMAINING THICKNESS IS 0.030". THE DEPTH OF CLEANUP IS 0.026">10%T. FOUND OUT OF LIMITS AS PER B767-300 SRM 53-00-07-1A-2 FIG101 RELEASE 119.00-06/01/22. THE NEW SHEAR TIE FABRICATED AS PER BOEING DWGING 140T2102 AND CONTROL NO 0270698948. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 RELEASE 119.00-06/01/22. LP 2371725

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1219 S38L-S39L REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.063". THE REMAINING THICKNESS IS 0.051". THE DEPTH OF CLEANUP IS 0.012">10%T. FOUND OUT OF LIMITS AS PER B767-300 SRM 53-00-07-1A-2 FIG101 RELEASE 119.00-06/01/22. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 RELEASE 119.00-06/01/22. LP 2371727

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1219 S35R-S36R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.063". THE REMAINING THICKNESS IS 0.052". THE DEPTH OF CLEANUP IS 0.011">10%T. FOUND OUT OF LIMITS AS PER B767-300 SRM 53-00-07-1A-2 FIG101 RELEASE 119.00-06/01/22. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 RELEASE 119.00-06/01/22. LP 2370529

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1197+132 S37R-S38R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.050". THE REMAINING THICKNESS IS 0.032". THE DEPTH OF CLEANUP IS 0.018">10%T. FOUND OUT OF LIMITS AS PER B767-300 SRM 53-00-07-1A-2 FIG101 RELEASE 119.00-06/01/22. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 RELEASE 119.00-06/01/22. LP 2370550

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1307 S38L-S39L REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.050". THE REMAINING THICKNESS IS 0.030". THE DEPTH OF CLEANUP IS 0.020">10%T. FOUND OUT OF LIMITS AS PER B767-300 SRM 53-00-07-1A-2 FIG101 RELEASE 119.00-06/01/22. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 RELEASE 119.00-06/01/22. LP 2370561

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1197+66 S37L-S38L REF TO CPCP 53-558-00. CORRECTIVE ACTION: ORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.050". THE REMAINING THICKNESS IS 0.033". THE DEPTH OF CLEANUP IS 0.017">10%T. FOUND OUT OF LIMITS AS PER B767-300 SRM 53-00-07-1A-2 FIG101 RELEASE 119.00-06/01/22. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 RELEASE 119.00-06/01/22. LP 2370543

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1175 S35R-S36R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.063". THE REMAINING THICKNESS IS 0.042". THE DEPTH OF CLEANUP IS 0.021">10%T. FOUND OUT OF LIMITS AS PER B767-300 SRM 53-00-07-1A-2 FIG101 RELEASE 119.00-06/01/22. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 RELEASE 119.00-06/01/22. LP 2370530

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1307 S37L-S38L REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.040". THE REMAINING THICKNESS IS 0.019". THE DEPTH OF CLEANUP IS 0.021">10%T. FOUND OUT OF LIMITS AS PER B767-300 SRM 53-00-07-1A-2 FIG101 RELEASE 119.00-06/01/22. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 RELEASE 119.00-06/01/22. LP 2370536

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1329 S38L-S39L REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.045". THE REMAINING THICKNESS IS 0.023". THE DEPTH OF CLEANUP IS 0.022">10%T. FOUND OUT OF LIMITS AS PER B767-300 SRM 53-00-07-1A-2 FIG101 RELEASE 119.00-06/01/22. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 RELEASE 119.00-06/01/22. LP 2370546

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1197+110 S37R-S38R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.050". THE REMAINING THICKNESS IS 0.032". THE DEPTH OF CLEANUP IS 0.018">10%T. FOUND OUT OF LIMITS AS PER B767-300 SRM 53-00-07-1A-2 FIG101 RELEASE 119.00-06/01/22. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 RELEASE 119.00-06/01/22. LP 2370508

Part: NONE — NONE · corrosion level 2 · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 173, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1285 S39L-S39R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.040". THE REMAINING THICKNESS IS 0.021". THE DEPTH OF CLEANUP IS 0.019">10%T. FOUND OUT OF LIMITS AS PER B767-300 SRM 53-00-07-1A-2 FIG101 RELEASE 119.00-06/01/22. THE SHEAR TIE REMOVED AND REPLACED AS PER B767-300 SRM 51-40-02 RELEASE 119.00-06/01/22. LP 2370523

Part: NONE — NONE · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, LH WING NO.3 SLAT UPPER SURFACE I/B AREA FOUND DELAMINATED. CORRECTIVED ACTION: LH WING NO.3 SLAT UPPER SURFACE I/B AREA REPAIRED AS PER B767-300 SRM 57-43-02-2R-1 & SRM 51-70-10-2R-4 FIG 202 & SRM 51-70-10-2R-0, RELEASE:119.00-06/01/22.RESULT: DISBOND SIZE: L X W =4.6 INCH X 3.6 INCH, AT I/B T/E EDGE UPPER CORNER OF LH WING NO.3 SLAT UPPER SURFACE HONEYCOMB CORE WAS DISBOND AT LOWER SURFACE SKIN WITHIN REPAIRABLE LIMIT. LOG 2369217

Part: NONE — NONE · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, LH WING NO.4 SLAT UPPER SURFACE AT 51" FROM I/B SIDE FOUND DELAMINATED . CORRECTIVE ACTION: LH WING NO.4 SLAT UPPER SURFACE AT 51" FROM I/B SIDE REPAIRED AS PER B767-300 SRM 57-43-02-2R-1 & SRM 51-70-10-2R-4 FIG 201 & SRM 51-70-10-2R-0 RELEASE:119.00- 06/01/22. RESULT:DISBOND SIZE: L X W = 9 INCH X 11 INCH AT 47" FROM I/B EDGE, 2" FROM UPPER EDGE FOUND THE HONEYCOMB CORE WAS DISBOND AT LOWER SURFACE SKIN WITHIN REPAIRABLE LIMIT. LP 2369273

Part: NONE — NONE · airframe 133,063 hrs · 19,080 cycles

AIRCRAFT 176, LH WING NO.6 SLAT UPPER SURFACE O/B AREA FOUND DELAMINATED. CORRECTIVE ACTION: H WING NO.6 SLAT UPPER SURFACE O/B AREA REPAIRED AS PER B767-300 SRM 57-43-02-2R-1 & SRM 51-70-10-2R-4 FIG 202 & SRM 51-70-10-2R-0 RELEASE: 119.00-06/01/22. RESULT: DISBOND SIZE: L X W =7.2" X 4.5" AT O/B T/E UPPER CORNER, FOUND THE HONEYCOMB CORE WAS DISBOND AT LOWER SURFACE SKIN WITH REPAIRABLE LIMIT. LOG 2369206

Part: NONE — NONE · airframe 133,064 hrs · 19,081 cycles

SHIP 176 DURING LAST C-CHECK (21NOV2018) AT STAG, ER/A 573161-14AD SECT. I REPAIR WAS ACCOMPLISHED ON A/C 176, IN THE RH WING LOWER SKIN AT STR L-9.5. FOLLOW ON ACTION IS REQUIRED FOR SECT. III INSPECTION, CORRECTIVE ACTION: ACCOMPLISH ER/A 573161-14AD REV. A SECTION III EXTERNAL HFEC INSPECTION AT AREA 'B' AND AREA 'C' PRIOR TO 6,000 CYCLES OR 18,000 FLIGHT HOURS AFTER SECTION I REPAIR (2350325)

Part: SEAL DEPRESSOR — DAMAGED · airframe 133,049 hrs · 19,078 cycles

SHIP 0176 -DIV/PRESS- TO MCI DURING MAINTENANCE REPOSITION FERRY DUE TO LOSS OF LT HPSOV AND "CABIN ALTITUDE WARNING" EICAS MESSAGE, INITIATED RAPID DECENT. CORRECTIVE ACTION: DEFERRED LT HPSOV PER MEL. REPAIRED AFT CARGO DOOR SEAL DEPRESSOR. (7054022)

Part: NONE — NONE · airframe 133,044 hrs · 19,076 cycles

SHIP 176 #2 ENGINE O/B NACELLE STRUT PRESSURE RELIEF DOOR IS MISSING. CORRECTIVE ACTION: REINSTALLED #2 ENGINE NACELLE STRUT PRESSURE RELIEF DOOR. OK FOR SERVICE. (7200848)

Part: CHILLER — LEAKING (GALLEY) · airframe 131,295 hrs · 18,777 cycles

PRIOR TO DISPATCH STRONG ACRID ODOR PRESENT IN FORWARD GALLEY AND COCKPIT AREA. INSPECTED FWD CARGO E/E COMPARTMENT FWD GALLEY AND COCKPIT NO DEFFECT FOUND. FOUND FWD GALLEY CHILLER FAULTY LEAKING AS THE SAME ODOR REPORTED. REPLACED CHILLER. SYSTEM OPERATION NORMAL.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 130,406 hrs · 18,662 cycles

SHIP 0176 - ATB - DUE TO AFTER T/O MCP ALTITUDE WINDOW FROZE AT 4000 FEET. ALT HOLD INOP. CREW COORDINATED WITH DISP, MCC FOR NON-EMERGENCY ATB TO FRA. CORRECTIVE ACTION: REPLACED AFDS MCP. C/W AFDS TEST 30 AND 40. A/C IS RTS.

Part: LIGHT — INOPERATIVE (R2 DOOR) · airframe 128,360 hrs · 18,400 cycles

SLIDE INDICATOR LIGHT INOPERATIVE. REPLACED SWITCH ASSEMBLY AT R2 DOOR. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 128,049 hrs · 18,362 cycles

EMERGENCY LIGHTS AT SEAT 38F ARE INOPERATIVE. REPLACED LIGHT ASSEMBLY AT 38F. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 127,517 hrs · 18,293 cycles

FOUND OUT O/B FLAP SKIN DELAMINATION AT TRAILING EDGE BETWEEN 13FT AND 14 FT TO HE FLAP I/B EDGE. REPAIRE PER SRM 57-53-01 (LP 0837599)

Part: SKIN — DAMAGED (WING) · airframe 127,517 hrs · 18,293 cycles

SKIN FOUND THE NO.66 HOLE DIAMETER :0.624" REPAIRED PER ERA 573161-14. (LP 0836480)

Part: SKIN — DENTED (LT WING SLAT) · airframe 127,517 hrs · 18,293 cycles

L/H WING NO.4 SLAT UPPER SURFACE FOUND A DENT LOCATED FORM O/B EDGE 11.5 INCH UPPER EDGE 8 INCH AND REPAIRED PER SRM 57-43-02. (LP 0836440)

Part: STRUCTURE — CORRODED (BS 955) · corrosion level 2 · airframe 127,517 hrs · 18,293 cycles

CORROSION LEVEL: 2 CABIN OVER CTR TANK STRUCTURE AT STA 955 RBL80 FOUND CORROSION REPARIED PER ERA 573135-14. (LP 0836663)

Part: STRUCTURE — CORRODED (BS 955) · corrosion level 2 · airframe 127,517 hrs · 18,293 cycles

CORROSION LEVEL: 2 CABIN OVER CTR TANK STRUCTURE AT STA 955 LBL71FOUND CORROSION AND REPAIRED PER ERA 573135-14. (LP 0836656)

Part: SKIN — DENTED (CARGO DOOR) · airframe 127,517 hrs · 18,293 cycles

FOUND TWO DENTS IN FWD CONER ON AFT CARGO DOOR REPARIED PER ERA 560791-14 AND SRM 52-30-01. (LP 0836735)

Part: SKIN — CRACKED (WING) · airframe 127,517 hrs · 18,293 cycles

HFEC SURFACE INSPECTION FOUND 01 EA CRACK APPROX 0.080"IN LENGTH AT THE FWD DIRECTION OF THE MOST O/B HOLE AND REPAIRED. (LP 0836471)

Part: STRUCTURE — CORRODED (BS 955) · corrosion level 2 · airframe 127,517 hrs · 18,293 cycles

CORROSION LEVEL: 2 CABIN OVER CTR TANK STRUCTURE AT STA 955 LBL85 FOUND CORROSION REPARIED PER ERA 573135-14 (LP 0836668)

Part: SKIN — DENTED (CARGO DOOR) · airframe 127,517 hrs · 18,293 cycles

THE DENT ON BULK CARGO DOOR EXTERNAL SURFACE AT BETWEEN CENTER AND 4.35INCH FROM AFT EDGE REPAIRED ERA 573132-14 (LP 0835343)

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 127,248 hrs · 18,258 cycles

WHEN CHECKING EMERGENCY LIGHTS IN CABIN, FOUND LEFT AND RIGHT MID CABIN AFT POS ISLE EXIT SIGNS WILL NOT ILLUMINATE. MAINTENANCE REPLACED POWER SUPPLY. SYSTEM OPERATION IS NORMAL.

Part: MODULE — DEFECTIVE (L1 DOOR) · airframe 127,142 hrs · 18,244 cycles

FOUND DOOR L1 SLIDE ARM LIGHT STUCK AND WON'T BE ABLE TO TEST. MAINTENANCE REPLACED L1 DOOR ALARM SIGNAL MODULE. SYSTEM OPERATION IS NORMAL.

Part: FRAME — CRACKED (BS 1809 BULKHEAD) · airframe 125,093 hrs · 17,981 cycles

BS 1809.5 BULKHEAD OUTER FRAME CRACKED INDICATION C/W ERA 558073-14. (LP 0482557)

Part: UNKNOWN — SMOKE (CABIN) · airframe 124,140 hrs · 17,856 cycles

ON TAKEOFF ROLL, LIGHT HAZY BLUE SMOKE ENTERED THE CABIN. MOSTLY CENTERED IN ECONOMY COMFORT TO MID CABIN AREA. MID LAV SMOKE DETECTORS WERE SET OFF BY THE SMOKE, SMOKE WENT AWAY ON ITS OWN WITHOUT CREW INTERVENTION AFTER A COUPLE OF MINUTES F/A'S UNSURE WHERE SMOKE CAME FROM. LAVS & OVERHEAD BINS WERE SEARCHED WITHOUT ANY SIGNS OF SMOKE ORIGIN. INSPECTED GASPER FAN AND FOUND OK. INSPECTED GALLEY VENT FANS AND LAVS INCLUDING HOT WATER HEATERS. R & R RECIRC FAN FILTERS .

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 123,049 hrs · 17,719 cycles

SEAT EMERGENCY LIGHTS AT ROWS 32A/F INOPERATIVE. R & R BATTERY CHARGER M9010 IAW AMM 33-51.

Part: FRAME — CORRODED (BS 1809 BULKHEAD) · airframe 120,670 hrs · 17,404 cycles

FRAME HOLES ELONGATED AND CORRODED AT THE BS 1809.5 BULKHEAD. REPAIRED.

Part: LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 119,793 hrs · 17,289 cycles

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

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 118,950 hrs · 17,183 cycles

AFT CARGO AT BS 1197+66, BETWEEN STRINGERS 37 - 38R SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1241) · airframe 118,950 hrs · 17,183 cycles

AFT CARGO BAY AT BS 1241, BETWEEN STRINGERS 38 - 39R FOUND THE SHEAR TIE CORRODED.

Part: SHEAR TIE — CORRODED (BS 1219) · airframe 118,950 hrs · 17,183 cycles

AFT CARGO BAY AT BS 1219 BETWEEN STRINGERS 37 - 38L, FOUND THE SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 118,950 hrs · 17,183 cycles

AFT CARGO BAY AT BS 1197+132, BETWEEN STRINGERS 37 - 38L, FOUND THE SHEAR TIE CORRODED. REMOVED AND REPLACED THE SHEAR TIE.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 118,950 hrs · 17,183 cycles

LEFT WING INBD AFT FLAP PANEL 555 IS WORN OUT OF LIMITS AND REPLACED.

Part: FRAME — DAMAGED (BS 1809 BULKHEAD) · airframe 118,950 hrs · 17,183 cycles

DURING LFEC AND OPEN HOLE INSPECTION OF BS 1809.5 BULKHEAD FORWARD OUTER FRAME DAMAGED ON THE SPLICE FITTING. COMPLIED WITH ERA 551281-14.

Part: FLAP — DENTED (RT WING) · airframe 118,950 hrs · 17,183 cycles

FOUND DENT RIGHT WING I/B AFT FLAP. REPAIRED PER SRM 51-70-10.

Part: SKIN — DENTED (TE FLAP) · airframe 118,950 hrs · 17,183 cycles

FOUND DENT LEFT WING I/B AFT FLAP I/B UPPER SURFACE. REPAIRED PER SRM 51-70-10.

Part: SKIN — DENTED (TE FLAP) · airframe 118,950 hrs · 17,183 cycles

FOUND DENT LEFT WING I/B AFT FLAP I/B UPPER SURFACE. REPAIRED PER SRM 51-70-10.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 118,950 hrs · 17,183 cycles

FOUND A DENT ON THE RIGHT WING INBD AFT FLAP. REPAIRED IAW SRM 51-70-10.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 118,950 hrs · 17,183 cycles

NR 2 NACELLE STRUT SIDE SKIN PANEL AT FORWARD TORQUE BOX ACCESS HOLE CRACKED AND REPAIRED IAW ERA 271983-14.

Part: SKIN — CRACKED (NR 1 NACELLE) · airframe 118,950 hrs · 17,183 cycles

NR 1 NACELLE STRUT SIDE SKIN PANEL AT FORWARD TORQUE BOX ACCESS HOLE CRACKED. COMPLIED WITH EAR 360779-14.

Part: SEAT TRACK — CORRODED (BS 1538-1542) · corrosion level 2 · airframe 118,950 hrs · 17,183 cycles

SEAT TRACK BETWEEN BS 1538 - 1542, LBL 88 FOUND TO BE CORRODED AND OUT OF LIMITS. REMOVED AND REPLACED IAW SRM 51-40-02.

Part: SKIN — CORRODED (BS 1197) · corrosion level 2 · airframe 118,950 hrs · 17,183 cycles

CORROSION ON SKIN AT BS 1197+88 - 1197+110, STRINGERS 35-36R. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-00-01.

Part: SKIN — CORRODED (BS 1197) · airframe 118,950 hrs · 17,183 cycles

SKIN CORROSION AT BS 1197+22 - 1197+44, STRINGERS 36 - 37R. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-00-01.

Part: SHEAR TIE — CORRODED (BS 1307) · corrosion level 2 · airframe 118,950 hrs · 17,183 cycles

AFT CARGO AT BS 1307 BETWEEN STRINGERS 39L - 39R SHEAR TIE CORRODED. THE SHEAR TIE WAS REPLACED.

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 118,950 hrs · 17,183 cycles

AFT CARGO AT BS 1197+132, BETWEEN STIRNGERS 39L-39R FOUND THE SHEAR TIE CORRODED AND REPLACED.

Part: STRINGER — CORRODED (BS 698-720) · corrosion level 2 · airframe 118,950 hrs · 17,183 cycles

FWD CARGO BETWEEN BS 698 - 720, FOUND STRINGER 32R CORRODED AND OUT OF ALLOWABLE LIMITS. REPAIRED IAW SRM 53-00-03.

Part: STIFFENER — CORRODED (BS 1285) · corrosion level 2 · airframe 118,950 hrs · 17,183 cycles

CABIN INTERIOR STRUCTURE AT BS 1285 STRINGER 17L STIFFINER FOUND CORRODED AND REPLACED.

Part: STIFFENER — CORRODED (BS 1197) · airframe 118,950 hrs · 17,183 cycles

CABIN INTERIOR STRUCTURE BS 1197+132 AT STRINGER 17L STIFFINER FOUND CORRODED. REMOVED AND REPLACED.

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 118,950 hrs · 17,183 cycles

FLOORBEAM UPPER SURFACE FOUND CORRODED AT BS 1480, LBL 60. FOUND OUT OF LIMITS. REPAIRED IAW SRM 53-00-51.

Part: STRINGER CLIP — CORRODED (BS 1329) · corrosion level 2 · airframe 118,950 hrs · 17,183 cycles

CABIN INTERIOR STRUCTURE AT BS 1329 STRINGER CLIP 17L FOUND CORROSION. THE STRINGER CLIP WAS REMOVED AND REPLACED.

Part: STIFFENER — CORRODED (BS 1197) · corrosion level 2 · airframe 118,950 hrs · 17,183 cycles

CABIN INTERIOR STRUCTURE AT BS 1197+110 STRINGER 17L STIFFINER FOUND CORRODED. REMOVED AND REPLACED.

Part: FRAME — CRACKED (WW BULKHEAD) · airframe 118,950 hrs · 17,183 cycles

HFEC INSPECTION ON LHS NOSEWHEEL WELL BULKHEAD CHORD FOUND CRACKED AND REPAIRED.

Part: FRAME — CRACKED (BS 859) · airframe 118,950 hrs · 17,183 cycles

HFEC INSPECTION FOUND CRACKED BS 859.5 FRAME IN THE TRANSITION RADIUS AND REPAIRED.

Part: FRAME — CRACKED (BS 883) · airframe 118,950 hrs · 17,183 cycles

HFEC INSPECTION FOUND CRACKED BS 883.5 FRAME TRANSITION RADIUS AREA AND REPAIRED.

Part: SKIN — BURNED (FUSELAGE) · airframe 118,950 hrs · 17,183 cycles

STATION 685 BURN MARK ABOUT 2 FT ABOVE WINDOW PANE LINE BLENDED, TREATED AND PAINTED PER SRM 53-00-01 FIG 101.

Part: SKIN — BURNED (FUSELAGE) · airframe 118,950 hrs · 17,183 cycles

STATION 700 BURN MARK ABOUT 3 FT ABOVE WINDOW PANE BLENDED, TREATED AND PAINTED PER SRM 53-00-01 FIG 101.

Part: WINDOW FRAME — BURNED (FUSELAGE) · airframe 118,950 hrs · 17,183 cycles

BURN DAMAGE TO WINDOW FRAME 3 SPOTS BETWEEN STATION 615 AND 645 RT SIDE. INSPECTED DAMAGE AREA AND BLENDED AREAS AND TREATED PER SRM 56-20-02.

Part: FASTENER — BURNED (FUSELAGE) · airframe 118,950 hrs · 17,183 cycles

STATION 654 AND 650 SOME BURNED FASTENERS ABOUT 1 FOOT ABOVE WINDOWS BLENDED TREATED AND PAINTED PER 53-00-01 FIG 101.

Part: FASTENER — DAMAGED (FUSELAGE) · airframe 118,950 hrs · 17,183 cycles

GROUP OF FASTENERS DAMAGED ABOVE FWD CARGO DOOR STATION 500 BLENDED AND TREATED PER SRM 53-00-01 FIG 101 PAINTED.

Part: FASTENER — BURNED (FUSELAGE) · airframe 118,950 hrs · 17,183 cycles

6 BURNED FASTENERS STATION 654 JUST AFT OF PRODUCTION BREAK ABOUT 1 FOOT ABOVE THE WINDOW BLENDED TREATED AND PAINTED PER SRM 53-00-01 FIG 101.

Part: SKIN — CORRODED (FUSELAGE) · airframe 114,477 hrs · 16,600 cycles

FUSELAGE SKIN, STA 1582, S-24L TO S-25L CORRODED, 541071-14, LOG 2209980.

Part: SKIN — CRACKED (RT WING) · airframe 109,893 hrs · 16,042 cycles

DURING INSPECTION IAW WC 5713-2016, FOUND LOWER WING SKIN CRACKED ON RT WING JUST OTBD OF NR 12 SLAT CAN DRAIN HOLE AT FASTENER-LOCATION .150 IN LENGTH. REPAIRED IAW ERA 529920-14.

Part: SKIN — CRACKED (LT WING) · airframe 109,893 hrs · 16,042 cycles

DURING INSPECTION IAW WC 5713-2736, FOUND LOWER WING SKIN CRACKED ON LT WING JUST OTBD OF NR 1 SLAT CAN. REPAIRED IAW ERA 529921-14. DRAIN HOLE AT FASTENER - LOCATION .250 IN LENGTH.

Part: ACCESS PANEL — DAMAGED (KEEL BEAM) · airframe 105,186 hrs · 15,436 cycles

LOWER FUSELAGE KEELBEAM ACCESS PANEL 149AL, RT AFT ANCHOR NUT METAL STRIP DETACHED. REPAIRED IAW ERA 515565-14, REV.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 103,989 hrs · 15,281 cycles

EMERGENCY LIGHTS FROM ROW 32A LT AND RT ARE INOPERATIVE. REPLACED M9010 LIGHT CHARGER. SYS OPS IS NORMAL.

Part: SLIDE — UNWANTED DEPLOY (LT OVERWING) · airframe 102,420 hrs · 15,070 cycles

DUE TO LT OVERWING SLIDE DEPLOYMENT C/W, OP 7838 AD, OP 7838 AD COMPLIED WITH. REPLACED BATTERY, SLIDE CYLINDER, ESCAPE SLIDE DOOR OPEN ACTUATOR ON FWD AFT, LATCH OPEN ACTUATOR, AND SPOLIER OVER RIDE ACTUATOR.

Part: SUPPORT — UNKNOWN (TE FLAP) · airframe 99,529 hrs · 14,678 cycles

WING LT & RT INBD FLAP INBD AND OTBD SUPPORT CORROSION OR TOOLING DAMAGE 089397-14.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,512 hrs · 14,676 cycles

DURING DRC FOUND EMERGENCY LIGHT PATH LIGHT INOPERATIVE AT SEAT 37G. REPLACED LT ASSEMBLY ILLUMINATED CHECKED OK.

Part: FAILSAFE — CRACKED (BS 955) · airframe 98,867 hrs · 14,589 cycles

DURING ULTRASONIC INSPECTION, FOUND CRACK INDICATION ON FAILSAFE OF REAR SPAR SPAR BULKHEAD RT BS 955 AT 0800 POS LOOKING OUTBOARD. REPAIRED FAILSAFE IAW ERA 502640-14AD REV ORIG.

Part: FUSE — OPEN (CABIN) · airframe 97,420 hrs · 14,403 cycles

LEFT WING OUTSIDE EMERGENCY EXIT LIGHT INOP ON PDC PER SSM 33-51-01. FOUND FUSE 2 BLOWN ON M736 AND CONTACTS DIRTY ON LIGHT ASSY. REPLACED FUSE AND CLEANED CONTACTS. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: CHARGER — INOPERATIVE (CABIN) · airframe 96,879 hrs · 14,333 cycles

WHILE PERFORMING DRC MAINTENANCE FOUND OVERHEAD EMERGENCY LIGHTS AT 23GF THROUGH 28GF INOPERATIVE. THE BATTERY CHARGER FOR M732 BATTERY PACK WAS REPLACED. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 96,872 hrs · 14,332 cycles

DURING DRC FOUND OVERHEAD EMERGENCY LIGHTS AT 23GF-28GF INOP. MAINTENANCE REPLACE THE BATTERY CHARGER FORM M732 BATTERY PACK. SYSTEM OPERATION IS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: TIRE — BLOWN (RT MLG) · airframe 96,051 hrs · 14,212 cycles

FLIGHT RETURNED TO SFO DUE TO THE TOWER REPORTING A BLOWN TIRE ON THE RIGHT MAIN GEAR. EMERGENCY WAS DECLARED ON APPROACH. MAINTENANCE FOUND THE NR 3 TIRE BLOWN AND REPLACED THE NR 3 WHEEL AND TIRE ASSEMBLY. THE NR 3 WHEEL ANTI-SKID TRANSDUCER AND THE RIGHT MAIN GEAR WIRE HARNESS WERE REPLACED DUE TO IMPACT DAMAGE. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,437 hrs · 14,136 cycles

EMERGENCY PATH LIGHTS AT SEATS 37AB AND 37GF ARE INOPERATIVE. FORWARD TO MCO/PLAC PER 33-51-03A. BOS/457838

Part: TEE FITTING — DAMAGED (PYLON) · airframe 92,101 hrs · 13,707 cycles

DURING SIP-PYLON MOD, UPPER FITTING TEE CLIP REPLACEMENT PER SB 767-54-0080, TEE CLIPS P/N 112T7010-14/-16 FOUND SEM. ACCOMPLISHED REPAIR PER ERA 485500-14AD REV ORIG. (DL76L103183)

Part: FITTING — DAMAGED (FUSELAGE) · airframe 92,101 hrs · 13,707 cycles

CABIN RT STA 927 FRAME TO WING CTR SECTION FITTING REPLACED PER SRM 51-10-02. (DL76L103186)

Part: FITTING — DAMAGED (FUSELAGE) · airframe 92,101 hrs · 13,707 cycles

CABIN LT STA 927 FRAME TO WING CTR SECTION FITTING REPLACED PER SRM 51-10-02. (DL76L103185)

Part: TEE FITTING — DAMAGED (PYLON) · airframe 92,101 hrs · 13,707 cycles

DURING SIP PYLON MOD, UPPER FITTING TEE CLIP REPLACEMENT PER SB 767-54-0080, TEE CLIPS P/N 112T7010-13/-15 FOUND SEM. ACCOMPLISHED REPAIR PER ERA 485498-14AD. (DL76L103184)

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 92,101 hrs · 13,707 cycles

NR 2 PYLON I/B SIDE MID SPAR FITTING HOLES COMMON TO STRUT HORZ CHORD FOUND FIVE FASTENER HOLES CRACKED AT WEB AND REPAIR ACCOMPLISHED PER ERA 485491-14AD REV ORIG. (DL76L103081)

Part: SPAR — DAMAGED (NR 1 PYLON) · airframe 92,101 hrs · 13,707 cycles

NR 1 PYLON MID SPAR WEB O/B WEB TEN HOLES LARGER THAN SB CALL OUT AND REPAIR ACCOMPLISHED PER ERA 485492-14AD REV ORIG (DL76L103080)

Part: SKIN — PUNCTURED (TE FLAP) · airframe 92,101 hrs · 13,707 cycles

RT WING I/B MAIN FLAP UPPER SURFACE PUNCTURED AND REPAIRED PER SRM 57-53-01 REPAIR 1 AND SRM 51-70-17 FIG 1. (DL76L103031)

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 92,101 hrs · 13,707 cycles

LT WING I/B MAIN FLAP LEADING EDGE O/B END FAIRING FOUND DELAMINATED. COMPOSITE HOT BOND PREPREG REPAIR CARRIED OUT AT DELAMINATED AREA AS PER SRM 57-53-01 AND SRM 51-70-5 FIG 5. (DL76L103032)

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 92,101 hrs · 13,707 cycles

RT WING O/B FLAP T/E WEDGE UPPER SURFACE DELAMINATED AND REPAIRED PER SRM 57-53-01 REPAIR 1 AND SRM 51-70-07 FIG 9. (DL76L103030)

Part: FRAME — CRACKED (FUSELAGE) · airframe 92,101 hrs · 13,707 cycles

CABIN RT STA 903 BETWEEN S20R AND S21R FRAME INNER CHORD CRACK REPAIR ACCOMPLISHED AS PER ERA 485487-14AD REV ORIG. (DL76L103019)

Part: FRAME — CRACKED (FUSELAGE) · airframe 92,101 hrs · 13,707 cycles

CABIN LT STA 903 BETWEEN S20L AND S21L FRAME INNER CHORD CRACK. REPAIR ACCOMPLISHED AS PER ERA 485486-14AD REV ORIG. (DL76L103018)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 92,101 hrs · 13,707 cycles

FUSELAGE STA 434 BETWEEN S36R AND S39L SKIN PERMANENT REPAIR ACCOMPLISHED AS PER ER/A 485497-14AD. (DL76L103197)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,957 hrs · 13,688 cycles

EMERGENCY LIGHT AT SEAT 17B IS INOPERATIVE. MX REPLACED THE LIGHT ASSY. SYS OPS IS NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 90,263 hrs · 13,478 cycles

EMERGENCY PATH LIGHTING AT 20AB AND 24AB ARE INOP. MX REPINED CONNECTORS AT 20AB AND 24AB.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 89,307 hrs · 13,360 cycles

ENERGENCY LIGHT SIGNS INOP 1L AND 1R. REPLACED CHARGER PER AMM CK GOOD

Part: SKIN — DENTED (BS 430 S37R) · airframe 88,728 hrs · 13,278 cycles

FOUND AT PSV 12/24/09 DENT IN FUSELAGE SKIN AT STA 430 STR 37R, REPAIRED IAW ERA 478789-14 REF NRC 200.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 88,702 hrs · 13,273 cycles

DURING TAXI OUT MX IN PROGRESS, T/S PERFORMED - RAIL LOCKOUT ACT/ FSEU FAULT ON SAM. PSEU SHOW TARGET 294. FSEU SHOW FLAP POS TRANSMITTER 8 MSG 27-51014. F/S ELEC INTERMITTENT. RESET FAULTS. RETRACT AND EXTEND FLAP/SLAT SEVERAL TIMES. NO FAULTS NOTED. OPS NORMAL ON GND.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZ STAB) · airframe 88,137 hrs · 13,189 cycles

RTO - UNSCHEDULED STAB TRIM AT 80 KNOTS. T/S PER FIM 27-09-00-101 FIG 106A REPLACED BOTH SAMS. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: TRANSCEIVER — MALFUNCTIONED (WEATHER RADAR) · airframe 87,349 hrs · 13,090 cycles

WXR FAIL WITH R/T FAULT SHORTLY AFTER DEPARTURE. AIR TURNBACK TO ATL FOR MTC. REPLACED WXR R/T CHECKS GOOD. OVERWEIGHT LANDING INSP C/W, NEW PDC C/W.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 87,078 hrs · 13,056 cycles

AFT RT LAV WALL EMERGENCY LIGHT INOP. RECONNECTED WIRES AND ALSO REPLACED BATTERY AT M734. OPS CK GOOD. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: LINE — LEAKING (NR 1 ENG OIL) · airframe 86,742 hrs · 13,012 cycles

LEFT ENGINE OIL QTY DROPPING, PRESS AND TEMP GOOD DIVERTED TO LHR. LANDING UNEVENTFUL, ENGINE NOT SHUTDOWN. FOUND OIL PUMP LINE LEAKING IN THE FLEX PORTION. NOT A 'B' NUT LEAK REF IPC 79-21-05-05 NR 36. FOUND LEAK ON MAIN OIL SUPPLY TUBE BETWEEN OIL FILTER AND OIL PUMP-LEAKING FROM FLEXIBLE SECTION. SUPPLY TUBE REMOVED. REFITTED NEW SUPPLY TUBE SERVICED OIL TO FULL. LEAK CHECKED ENGINE, OK NO LEAKS.

Part: VALVE — MALFUNCTIONED (APU) · airframe 86,602 hrs · 12,994 cycles

ON PUSH BACK APU QUIT RETURNED TO GATE APU AUTO SHUTDOWN. IAW QRH SWITCH OFF TO ON. FAULT LIGHT EXTINGUISHED. APU STARTED NORMALLY. ECB BITE SHOWS NO FAULTS. APU STARTED TWICE SUCCESSFULLY AND RUNNING WITH LOADS NORMALLY. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: SKIN — GOUGED (FS 1417) · airframe 86,480 hrs · 12,980 cycles

FUSELAGE SKIN FS 1417 BULKHEAD CARGO DOOR OPENING LWR FWD CORNER EDGE IAW ERA 468529-14 C/W ERA 468529-14.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 84,687 hrs · 12,744 cycles

RTB DUE TO CABIN AUTO PRESS CONTROLLER INOP. PROBLEM OCCURRED AFTER AC WAS DEICED. PERFORMED BIT ON AUTO1 AND AUTO2 CABIN PRESS CONTROL UNIT BOTH FAULTED. CONTROLLER PERFORMED, VERIFY NO FAULTS. RESET BOTH CONTROLLERS, NO FAULTS, NO MSGS, NO HISTORY ON AUTO PRESS. AC OK FOR SERVICE.

Part: CONNECTOR — LOOSE (TRIM MODULE) · airframe 84,263 hrs · 12,692 cycles

RTB - ON TAXI OUT RUDDER TRIM INOP. NO MEL RELIEF, MTC RESEATED CONNECTOR ON RUDDER TRIM MODULE SYSTEM. OPS CK OK.

Part: BLEED VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 83,026 hrs · 12,539 cycles

DURING CLIMB-OUT HAD LEFT HPSOV EICAS MESSAGE WOULD NOT CLEAR FOLLOWED QRH PROCEDURES LEFT BLEED NOW SECURED. DIVERTING TO ATL FOR REPAIRS.

Part: SKIN — GOUGED (FUSELAGE) · airframe 82,154 hrs · 12,438 cycles

DURING PSV, MTC FOUND A GOUGE ALONG THE FUESLAGE SKIN FORWARD EDGE OF THE BULK CARGO DOOR CUTOUT AT FS 1417 AND S-30L. DAMAGE REMOVAL RESULTED IN A ROUTOUT APPROX 0.225 INCH WIDE BY 1.2 INCH LONG. THE UNDERLYING STRUCTURE WAS NOT DAMAGED OR CUT OUT. BOEING APPROVED A PERMANENT REPAIR FOR 12 MONTHS PENDING A DAMAGE TOLERANCE ANALYSIS.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 82,154 hrs · 12,438 cycles

CRACKS AT PASSTHROUGHS IN NR 2 PYLON UPPER SPAR WEB. CRACKS WERE CUT OUT AND DOUBLERS INSTALLED.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 81,913 hrs · 12,411 cycles

WHILE ACCOMPLISHING OPN 5281AD MTC, FOUND THE CLOSE OUT ANGLE CRACKED. CLOSE OUT ANGLE WAS REPLACED. MTC ALSO FOUND THEY NEEDED AN ADDITIONAL WASHER UNDER THE HEAD OF THE FASTENER FOR PROPER GRIPPING. THIS WAS AUTHORIZED. ADDITIONAL INSPECTIONS WERE ACCOMPLISHED PER 01-074944-12AD.

Part: ATTACH FITTING — DAMAGED (PYLON) · airframe 81,913 hrs · 12,411 cycles

NACELLES/PYLONS ATTACH FITTING - MIDSPAR FITTING REPAIR IAW EO 01-074944-12 ME02 C/W EO 01-074944-12 ME02. ME02 WAS NOT COMPLETED ME04 WAS COMPLETED ON 04/24/08.

Part: COLLAR — DAMAGED (TE FLAP) · airframe 80,884 hrs · 12,285 cycles

WING T/E - INBD FLAP - MAIN FLAP - COLLAR FITTING REPAIR IAW 01-073591-12 ME20 AND ME21, C/W 01-073591-12 ME20 AND ME21.

Part: TERMINAL — BROKEN (HPSOV) · airframe 80,524 hrs · 12,237 cycles

DURING CLIMB-OUT FROM JFK, THE LEFT ENGINE BLEED/BLEED LIGHT AND AURAL WARNING KEPT CYCLING. HAD THEM RESET C/B P11S11 FOR THE LEFT ENGINE BLEED CONTROL WHICH FIXED FOR A SHORT PERIOD AND THEN THE PROBLEM RETURNED. DUE TO PREV HISTORY, OPTED TO RETURN THE AIRCRAFT TO JFK AND SWAP EQUIP. FOUND NR 2 TERMINAL BROKEN OFF ON HPSOV VALVE AS PRECAUTION RE-TERMINATED ALL 3 TERMINALS ON VLV PER MM. RAN ENG, OPS NORMAL.

Part: LINE — LEAKING (ENGINE OIL SYS) · airframe 79,983 hrs · 12,170 cycles

NR 1 ENG LOOSING OIL QTY STEADY DROP DIVERTING TO LGW FOR REPAIRS. OPENED LT ENG FOUND OIL RETURN LINE LEAKING AT TUBE ASSY SCAVENGE PUMP TO OIL FILTER P/N 59T347 IPC 79-21-05-05 ITEM 36 543778. REPLACED TUBE ASSY RETURNED A/C TO NML, PERF ENG RUN/LEAK CHECK ALL OPS/IND NML. A/C OK FOR SVC.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 79,470 hrs · 12,107 cycles

STATUS MSG, FLAP/SLAT ELECTRIC DISPLAYED. REMOVED AND REPLACED FSEU PER MM. BITE CHK OK. RAN FLAPS ALL OK. POWER TRANSFERRED, ALL OK.

Part: HOUSING — CRACKED (AC GENERATOR) · airframe 78,256 hrs · 11,958 cycles

APU A/C GENERATOR HOUSING CRACKED, LEAKING OIL FROM 12 O`CLOCK POS. REPLACED APU A/C GEN PER MM, SYSTEM TEST OK PER MM MFG P/N727810B.

Part: COLLAR — DAMAGED (WING TE FLAP) · airframe 77,650 hrs · 11,878 cycles

WING T/E- INBD FLAP- MAIN FLAP - COLLAR FITTING REPAIR IAW 01-073591-12 ME12 LT AND ME13 RT , EO 01-073591-12 ME12 LT AND ME13 RT.

Part: LINK — DAMAGED (TE FLAP) · airframe 77,287 hrs · 11,831 cycles

T/E FLAP MECHANISM 3-10 LINKS REPLACEMENT IAW 01-076248-12 ME07 LT, ME08 LT, MD09 LT AND ME10 RT ME11 RT ME12 RT. C/W EO 01-076248-12 ME07 THRU ME12.

Part: CIRCUIT CARD — MALFUNCTIONED (NR 1 ENGINE) · airframe 77,057 hrs · 11,801 cycles

AFTER LEFT ENG START STATUS MESSAGE L ENG SPEED CARD. CHECKED L ENG SPEED CARD OK INT CHANGED L AND R SPEEDCARDS. MSG RE-APPEARED AFTER ENG RUN NOW RT SIDE. REMOVED AND REPLACED RT SPEEDCARD IAW MM 77-12-01.

Part: PITOT HEAD — UNSERVICEABLE (RT) · airframe 76,182 hrs · 11,689 cycles

AFTER START, F/O'S PITOT HEAT LIGHT FAILED TO EXTINGUISH. REPLACED F/O'S AUX PITOT PROBE PER M/M. LEAK CHECKED PER M/M SYSTEM CHECKS NORMALLY.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 75,500 hrs · 11,606 cycles

AFTER ENGINE START NR 2 ENG OIL QTY DROPPED TO 3-4 QTS QTY BELOW DISPATCH LIMITS. MTC IN WORK PERFORMED NR 2 ENGINE CHANGE IAW TRANSMITTAL 1T149.

Part: BLEED VALVE — MALFUNCTIONED (LT ENGINE) · airframe 73,022 hrs · 11,300 cycles

LT ENG PRV MSG IN FLT WITH ASSOCIATED BLEED LIGHT. REPLACED PRV CONTROLLER AND PRV PER MM ENGINE RUN, OPS GOOD.

Part: WIRE — SHORTED (RT ENGINE) · airframe 66,625 hrs · 10,466 cycles

DURING CRUISE FLIGHT RIGHT ENGINE GEN DROPPED OFF LINE. FOUND FIELD WIRE SHORTED AT CSD PLUG D10966. REPAIRED SAME.

Part: COMPUTER — MALFUNCTIONED (EICAS) · airframe 64,489 hrs · 10,154 cycles

ON POWER UP FOR TAKEOFF PROBE HEAT EICAS DISPLAYED ALONG WITH 2 OR 3 OTHER MSGS. NO OVERHEAD LIGHTS WERE NOTED. T/S PER FIM 30-31-00 FIG 108 SHEET 1, HOOKED UP PITOT/STATIC TESTER PUMPED A/S TO 60 KNTS, RAN ENGINES TO TAKEOFF PWR NTF. POWERED PIMUS WITH ENGS RUNNING, PERFORMED N2 SPEED CARD BITE CK FOR BOTH LEFT RIGHT ENGS NTF. ALL SYSTEM RETURNED TO NML. REPLACED LT & RT EICAS COMPUTERS, NEEDS TAXI CHECK. ALSO REPLACED BOTH N2 SPEED CARDS ROBBED FROM 189.

Part: CARBON SEAL — LEAKING (NR 2 ENGINE) · airframe 62,753 hrs · 9,906 cycles

MID CABIN SMOKE DETECTORS AND AFT CABIN SMOKE DETECTORS CAME ON SHORTLY AFTER T/O, NOTICED MUSTY ODOR AND AGAIN AT TOD IN PASSENGER CABIN. ATL MAINT ALSO FOUND OIL LEAK AT NR 2 ENG INLET. FOUND 100 CCS OIL IN NR 2 ENG INTAKE. SUSPECT FROM FRAME LE OIL CONSUMPTION HIGHER THAN NR 1 FOR LAST 30 DAYS. OPENED AND REMOVED NOSE COWL. REPLACED NR 1 AND 1.5 CARBON SEALS A SEATS ON NR 2 ENG PER DAJIC M522. RT NOSE COWL INSTALLED PER M/M. RAN ENG PER PFM, OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,276 hrs · 8,507 cycles

SEAT 2AB, 22AB, 29AB, 40AB 1 E-PATH LIGHT BULB. FWD TO MCO PER MEL 33-51-03.

Part: ENGINE — SURGES (NR 1) · airframe 53,596 hrs · 8,364 cycles

UPON ARRIVAL ATL LEFT ENG SURGE DET MTC MESSAGE FOUND. EDR SURGE REPORT CONFIRMED SURGE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 52,786 hrs · 8,239 cycles

LEFT SIDE CABIN EMERGENCY LIGHT MID CABIN INOP. REPLACED BATTERY PACK, OPS CHECK NORMAL.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 52,341 hrs · 8,170 cycles

EMERGENCY AISLE LIGHT POWER SUPPLY FOR ROWS 6 THROUGH 20 LT SIDE INOP. REPLACED POWER SUPPLY AT ROW 6 LT SIDE, OPS CHECKS OK.

Part: ENGINE — FAILED (#1 ENGINE) · airframe 50,464 hrs · 7,872 cycles

ACFT ATB DUE TO NBR 1 ENGINE FLUX. REPLACED FMU. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: LAVATORY — INOPERATIVE (CABIN) · airframe 49,976 hrs · 7,804 cycles

DIVERTED TO CCS DUE TO LAV SYSTEMS INOP. SERVICED LAVS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,603 hrs · 7,578 cycles

AT DEPARTURE AFT LEFT HAND EMERGENCY FLASHLIGHT INOP. REPLACED BATTERY PACK.

Part: ENGINE — STALLED (NR 2) · airframe 48,341 hrs · 7,539 cycles

RT ENG AUDIBLE STALL ON T/O AT MAD. ACFT ATB. ENG WAS NOT SHUTDOWN IN FLIGHT. ENGINE TO BE REPLACED AT MAD.

Part: DISPLAY — FAILED (COCKPIT) · airframe 46,930 hrs · 7,276 cycles

ELECTRICAL SMELL IN COCPIT. FOUND CO-PILOTS FMS CDU FAILED. REPLACED SAME.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 46,528 hrs · 7,212 cycles

FOUND SEAT EMERGENCY LIGHTS AT 6 A/B TO 11 A/B INOP. REPLACED FWD CCN LT PWR SUPPLY/BATTERY CHARGER. OPS OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 45,496 hrs · 7,043 cycles

LAYOVER CHECK, FOUND EMERGENCY LIGHTS AFT OF F/C FWD COACH CLASS INOP. REPLACED M730 PWR SUPPLY AND BATTERY EMERGENCY LIGHTS NOW CHECK NORMAL.

Part: SKIN — CREASED (FS 654, S-26L)

FUSELAGE SKIN FS 654, STRINGER 25L-26L, CREASE REPAIR. THE FUSELAGE SKIN WAS FOUND WITH A DEEP CREASE JUST ABOVE THE STRINGER 26L LAP JOINT AT FS 654. THE DAMAGED AREA WAS CUTOUT WITH A 13 LONG BY 1.1 HIGH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 368729-14.

Part: WIRE — CHAFED (NR 1 ENGINE)

DURING INSPECTION OF PYLON WIRE HARNESS FOUND TOTAL OF 8 WIRES CHAFED. WIRES REPAIRED PER BOEING STD MANUAL CHAPTER 20.

Part: WIRE — CHAFED (NR 2 ENGINE)

DURING INSPECTION OF PYLON WIRE HARNESS FOUND 12 WIRES CHAFFED THROUGH INSULATION. REPAIRED WIRES PER BOEING STD MANUAL CHAPT. 20.

Part: RELEASE ROD — OUT OF ADJUST (L1 DOOR)

L-1 DOOR WOULD NOT OPEN FROM INSIDE AFTER CYCLING SLIDE ARMING LEVER. ADJUSTED OUTER ARM/DISARM ROLLER RELEASE ROD, OPS CHECKS NORMAL.

Part: POWER SUPPLY — INOP (LEFT)

ON CHECK, FOUND EMERGENCY LIGHTS OUT AT FLOOR LEVEL AT OVERWING EMERGENCY DOORS ON BOTH SIDES OF AIRCRAFT. REPLACED BATTERY PACK AND CHARGER AT LEFT HAND POSITION AFT OF OVERWING EMERGENCY DOOR. OPN CHECKS OK.

Part: SPAR WEB — CRACKED (NR 1 STRUT)

TWO CRACKS WERE FOUND ON 8/20/97 EMANATING FROM A DRAIN HOLE ON THE NR 1 ENGINE STRUT FWD UPPER SPAR WEB AT NAC STA 158. THE CRACKS WERE TRIMMED OUT ON A TIME-LIMITED BASIS. AT 11/98 OVERHAUL, A PERMANENT DOUBLER REPAIR WAS INSTALLED. CRACKS WERE DUE TO FATIGUE DAMAGE. REPAIRED PER ERA 362549-14.

Part: INSULATION — TORN (BS 1373)

THE APU PNEUMATIC DUCT INSULATION WAS FOUND CHAFED THRU BETWEEN FS 1373 AND FS 1439 BY THE FIRE EXTINGISHER DISCHARGE LINE, THE FIRE EXTINGUISHER DISCHARGE LINE INSULATION WAS FOUND DAMAGED. THE APU DUCT INSULATION (P/N 212T3008-7) AND FIRE EXTINGUISHER DISCHARGE LINE INSULATION (P/N R180FS) WAS REPLACED AND THE FIRE EXTINGUISHER DISCHARGE LINE WAS REPOSITIONED TO PROVIDE CLEARANCE TO MINIMIZE CHAFING.

Part: BATTERY — DISCHARGED (CABIN)

OUTSIDE EMERGENCY LIGHTS INOP. REPLACED BATTERY, SYSTEM OPS CHECK NORMAL.

Part: DRAG BRACE ACT — FAILED (RT MLG)

AFTER TAKEOFF DURING GEAR RETRACTION, HAD GEAR DISAGREE WARNING AND GEAR DOORS CAUTION ON EICAS. UPON LOWERING GEAR FOR APPROACH, INITIALLY HAD DOWN AND 3 GREEN INDICATIONS THEN WENT TO RT MAIN UNSAFE INDICATION (NO GREEN) AND RT SIDE BRACE EICAS CAUTION WITH AMBER GEAR LIGHT. FOUND BOTH DOWN AND LOCKED SENSORS WITH EXCESSIVE GAP. ADJUSTED PER MM AND IND NORMAL. FOUND RT SIDE BRACE LOCK ACT. PISTON ROD SEPARATED INTERNALLY FROM PISTON. REPLACED THE RT SIDE BRACE AND DRAG BRACE ACTUATORS AND GEAR OPS AND INDICATION NORMAL ON RETRACTION CHECK. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: SKIN — CRACKED (NR 2 ENG STRUT)

A 2 INCH CRACK WAS FOUND IN THE NR 2 ENGINE PYLON O/B STRUT SKIN. THE CRACK EMANATES FROM THE FWD TORQUE BOX ACCESS HOLE. THE CRACK WAS REPAIRED PER A BAC MOD DWG. REV E TO ER/A PROVIDES BAC DER FAA APPROVAL.

Part: SKIN — CRACKED (NR 1 PYLON)

A CRACK WAS FOUND IN THE NR 1 PYLON I/B STRUT SKIN EMANTING FROM THE TORQUE BOX ACCESS HOLE. THE CRACK WAS REPAIRED PER BAC MOD DWG 311T3401.

Part: COFFEE MAKER — SHORTED (AFT GALLEY)

AT FL 330, 2.5 HRS INTO FLIGHT RIGHT AC BUS AND RIGHT BUS TIE ILLUMINATED, ALONG WITH NUMEROUS ASSOCIATED EICAS MESSAGES. AFTER RESETTING RIGHT GENERATOR, THE RIGHT AC BUS WAS RESTORED BUT THE ISLN LIGHT REMAINED ON. SHORTLY AFTER THAT THE FLIGHT ATTENDANTS REPORTED SPARKS COMING FROM AFT GALLERY CONTROL PANEL ON RIGHT SIDE. FLIGHT ATTENDANTS REMOVED POWER FROM GALLEY AND FLIGHT CREW REMOVED POWER FROM UTILITY BUSSES. REPLACED COFFEE MAKER.

Part: VSV GUIDE — MISSING (NR 1 ENGINE)

DURING INSPECTION, FOUND NR 1 ENGINE VARIABLE STATOR VANES RING GUIDE BLOCKS MISSING IN SEVERAL LOCATION AND LOOSE IN OTHERS. REPLACED NR 1 ENG AND ROUTED TO SHOP.

Part: COFFEE MAKER — FAILED (AFT GALLEY)

APPROX ONE HOUR BEFORE DESCENT, F/A IN AFT GALLEY REPORTED SEEING SMOKE AND SMELLING ELECTRICAL WIRE BURNING. UTILITY BUSSES SWITCHES OFF. REPLACED NR 2 COFFEE MAKER DUE TO C/B POPPED. INSPECTED OVENS AND GALLEY WIRING OPERATION NORMAL.

Part: EEL POWER SUPPLY — INOP (CABIN)

EMERGENCY TRACK LIGHTS AFT CABIN LT SIDE INOP. REPLACED POWER SUPPLY M9010 AND REPOSITIONED TRACK, CHECKS OK.

Part: SKIN — CRACKED (NR 2 PYLON)

AT LETTER CHECK, FOUND 2 CRACKS IN NR 2 ENGINE PYLON O/B STRUT SKIN. REPAIRED PER DL ERA 2 71983-14.

Part: IDG — FAILED (NR 2 ENGINE)

DURING CRUISE, HAD RT GENERATOR DRIVE LIGHT. PER POM DISCONNECTED DRIVE, STARTED APU AND AFTER 20 MIN HAD APU LOW OIL STATUS MSG WITH AUTO SHUTDOWN, DIVERTED DUB. REPLACED NR 2 IDG, SERVICED APU WITH OIL AND RETURNED TO SERVICE.

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

NUMBER 1 ENGINE HAD 2 COMPRESSOR STALLS AT TOP OF CLIMB. LOST LEFT HYDRAULIC SYSTEM FLUID AND OIL QUANTITY WENT TO ZERO. ENGINE WAS SHUTDOWN, AIRCRAFT RETURNED FRA. FOUND TURBINE CASE COOLING TUBING BROKEN, HYDRAULIC PRESSURE LINE LEAKING AT HYDRAULIC PUMP, OIL PRESSURE LINE BROKEN, AND METAL IN TAILPIPE. ENGINE WAS REPLACED, ROUTED TO SHOP FOR REPAIRS.

Part: VALVE — FAULTY (LT PNEUMATIC SYS)

ON CLIMBOUT, HAD LEFT BLEED OVERHEAT LIGHT WITH EICAS MSG, RETURNED ATL. AIR SUPPLY BITE FAULTS FAN, AIR VALVE AND FAN AIR TEMP SENSOR. REPLACED FAN AIR VALVE AND FAN AIR TEMP SENSOR. AIR SUPPLY BITE CHECKS GOOD OPERATION NORMAL.

Part: SKIN — CRACKED (RT ELEVATOR)

RT OUTBD ELEVATOR LOWER SKIN WAS CRACKED AND DENTED AT ELEVATOR, STA 246 AND 25 INCH AFT OF LEADING EDGE. DAMAGE WAS REPAIRED PER SRM 51-70-17.