N394DL

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,902 hrs · 16,976 cycles

SHIP 1521 -MISC/DE- AUTOBRAKE UNABLE TO ARM FOLLOWED BY AIR GOUND DISAGREE DURING APPROACH. ATC DECLARED EMERGENCY. CORRECTIVE ACTION: REPLACED PROX SWITCH ELECTRONIC UNIT. (5010070)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,874 hrs · 16,967 cycles

SHIP 1521 1L WOULD NOT ARM. CORRECTIVE ACTION: FOUND FOD ON 1L DOOR. REMOVED FOD, DOOR OPS CHK GOOD PER B767 AMM 52-11. OK FOR SVC. (5010048)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,862 hrs · 16,964 cycles

SHIP 1521 3R DOOR DIFFICULT TO ARM/DISARM LEVER REPORTED "STICKY". CORRECTIVE ACTION: NO FAULT FOUND AT THIS TIME. DOOR ESCAPE SYS CHK GOOD PER B767 AMM 25-66. (5010035)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,417 hrs · 16,867 cycles

SHIP 1521 DOOR 2 L ARM LIGHT NOT WORKING, CORRECTIVE ACTION: DOOR CONFIRMED AS CLOSE IAW PROCEEDURE B767-300-11-00 (4604791)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,417 hrs · 16,867 cycles

SHIP 1521 UPON LANDING RECEIVED LEFT DOOR INDICATION ON EICAS. F/A REPORT 2L SLIDE INDICATOR KEPT FLICKERING AND THEN WENT OUT. DOOR EICAS WENT AWAY AFTER A FEW SECONDS. R/R L2 DOOR SENSOR S221 REF B767 AMM 52-71, WDM 52-71 AND CMM 32-09-09 PG D32. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,207 hrs · 16,674 cycles

SHIP 1521 - DIV - TO AMS DUE TO LEFT HPSOV MESSAGE DURING CRUISE. CORRECTIVE ACTION: REPLACED PRV. HPSOV MEL APPLIED AND OPS CONTINUED. SUBSEQUENT ACTION TAKEN TO REPLACE THE LEFT HPSOV.(48786679)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,160 hrs · 16,664 cycles

SHIP 1521 2L LOWER EXIT DOOR LIGHT COVER MISSING, CORRECTIVE ACTION: R/R 2L LOWER EXIT DOOR LIGHT ASSY PER B767 AMM 33-51. OPS CHECK OK (4876641)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 106,728 hrs · 16,599 cycles

SHIP 1521 EMERGENCY BATTERY CHARGER M731 INOP. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY BATTERY PACK CHARGER M731 PER B767 AMM 33-51. OPS CHECKEED NORMAL. (5117196)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 106,447 hrs · 16,543 cycles

SHIP 1521 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS: 3R. CORRECTIVE ACTION: RECONNECTED CONNECTOR OPS CHK GOOD OK FOR SVC (2691980)

Part: NONE — NONE · airframe 106,009 hrs · 16,448 cycles

SHIP 1521 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS: 3L. CORRECTIVE ACTION: CAN NOT DUPLICATE. 3L SLIDE INDICATOR LIGHT OPS NORMAL. OK FOR SERVICE. (2623157)

Part: NONE — NONE · airframe 106,009 hrs · 16,448 cycles

SHIP 1521 L CTR ENT DOOR CAUTION MSG COME ON AT 1500 FT MOMENTARILY. FA SAID SLIDE LIGHT KEPT BLINKING. CORRECTIVE ACTION: PERFORMED DOOR OPERATION ARM/DISARM NO FAULT NOTED IAW B767 AMM 52-71 (4146679)

Part: INDICATOR — BURNED OUT (L2 DOOR SLIDE) · airframe 105,868 hrs · 16,420 cycles

SHIP 1521 2L DOOR SLIDE LIGHT INDICATOR BURNT OUT. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR 2L SLIDE ARM SWITCH PER B767 AMM 33-51 . OPS CK NML. OK FOR SVC (9355694)

Part: NONE — NONE (SLIDE INDICATOR) · airframe 105,791 hrs · 16,405 cycles

SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:603. UNABLE TO DUPLICATE, 2L SLIDE INDICATION NORMAL (2595420)

Part: SIGN — UNSECURE (CABIN) · airframe 105,791 hrs · 16,405 cycles

EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS: 3L. RESECURED EMERGENCY EXIT SIGN OPS CHK OK

Part: SIGN — DETACHED (CABIN) · airframe 105,723 hrs · 16,390 cycles

L3 DOOR EXIT SIGN FELL OFF. ATTACHED THE SIGN, CHECKED GOOD, OK FOR SERVICE.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 105,658 hrs · 16,379 cycles

SEAT 29AB AND SEAT 41AB ASILE EMERGENCY WHITE LIGHTS INOP. SEAT 29A&B RECONNECTED DISCONNECTED WIRE AT CONNECTOR. SEAT 41A &B REPLACED SEAT LIGHT ASSY PER B767 AMM 33-51. OK FOR SVC.

Part: TARGET — OUT OF ADJUST (AFT PAX DOOR) · airframe 105,324 hrs · 16,319 cycles

ON APPROACH IN DESCENT AT 4000 MSL, LT AFT ENTRY DOOR ADVISORY EICAS MESSAGE DISPLAYED INERMITTENTLY, L4 UNTIL APROX 1000 MSL, FA'S REPORTED SLIDE LIGHT ALSO FLASHED. PRESSURE WAS NORMAL. PSEU BITE CHECK SHOWS S204 TARGET. FOUND GAP AT S204 EXCESSIVE. ADJUSTED TARGET IAW AMM 52 71 TARGET TESTED OK, ORIG SUB DATE: 12/13/2022

Part: LIGHT — UNSECURE (L4 SLIDE) · airframe 105,324 hrs · 16,319 cycles

LEFT AFT ENTRY DOOR CAUTION ON FINAL APPEARED AND WENT AWAY TWICE. FOUND SLIDE LIGHT ASSY FOR L4 DOOR WAS LOOSE, SECURED THE SLIDE LIGHT ASSY. ARM/DISARM DOOR & OPS CK GOOD.

Part: THRESHOLD — DIRTY · airframe 105,314 hrs · 16,317 cycles

SHIP 1521 ON APPROACH PASSING 4000' L AFT ENTRY EICAS MSG DISPLAYED. INTERM. DISPLAYED AND CLEARED THROUGH 1500', PRESR NORMAL THROUGHOUT. CORRECTIVE ACTION: CLEARED DEBRIS FROM DOOR THRESHOLD THEN CYCLE DOOR SEVERAL TIMES . CK OK PER B767 AMM CHAP 52-11. NO MSGS (9830992)

Part: LIGHT — INOPERATIVE (CONTROL PANEL) · airframe 104,939 hrs · 16,240 cycles

SHIP 1521 CREW PANEL UNRESPONSIVE / LOCATIONS:101. CORRECTIVE ACION: REMOVED LIGHT REF B767-300 AMM 52-73. OPS CHKS GOOD. (2489258)

Part: NONE — NONE · airframe 104,935 hrs · 16,239 cycles

SHIP 1521 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:101. CORRECTIVE ACTION: CYCLED SLIDE LIGHT SWITCH AT LOCATION 101, OP CHECK NORMAL. (2485661)

Part: NONE — NONE · airframe 104,618 hrs · 16,184 cycles

SHIP 1521 LEFT AFT ENTRY DOOR INDICATES OPEN WHEN DOOR IS CLOSED AND ARMED AFER A/C WAS DEPRESSURIZED, CORRECTIVE ACTION: CYCLED LT AFT DOOR SEVERAL TIMES W/ ECIAS MSG PER B767-300 AM 52 -11. COULD NOT DUPLICATE FAULT W/ DOOR CLOSED. A/C OK FOR SVC. (9618709)

Part: NONE — NONE · airframe 104,341 hrs · 16,143 cycles

SHIP 1521 ON TAXI IN L AFT ENTRY DOOR LIGHT EICAS AND DOOR DISCNETE LIGHT ILLUMINATED . WENT OUT AFTER APPROX 1 MINUTE. CORRECTIVE ACTION: COULD NOT REPRODUCE FAULT NO 30 DAY HISTORY. LEFT AFT ENTRY DOOR OPEN/CLOSE WARNING SYSTEM OPS NML PER B767-300 AMM 52-71. (9306100)

Part: NONE — NONE · airframe 104,077 hrs · 16,096 cycles

AIRCRAFT 1521, L/H I/B ELEVATOR UPPER SURFACE FOUND ONE HOLE. CORRECTIVE ACTION: L/H I/B ELEVATOR UPPER SURFACE REPAIRED AS PER B767-300 SRM 55-20-01-2R-1 & SRM 51-70-17 PARA.4B .FIG 024. (2332706)

Part: NONE — NONE · corrosion level 2 · airframe 104,077 hrs · 16,096 cycles

AIRCRAFT 1521, CORROSION FOUND ON THE GAP AREA BETWEEN THE LH SIDE WING CENTER SECTION REAR SPAR WEB AND THE SIDE FRAME BULKHEAD FITTING. CORECTIVE ACTION: THE REPAIR ACCOMPLISHED FOR THE SIDE FRAME FITTING AND THE REAR SPAR WEB AT STA955 LH WING CENTER SECTION AS PER PRI600432-14. (2333178)

Part: NONE — NONE · corrosion level 2 · airframe 104,077 hrs · 16,096 cycles

AIRCRAFT 1521, SEAT TRACK -CORROSION FOUND ON THE SEAT TRACK BETWEEM STA850 AND STA927, LBL88.5. CORRECTIVE ACTION: CARRIED OUT THE REPAIR FOR THE SRAT TRACK AS PER B767-300 SRM53-00-52-2R-3 FIG201. (2333134)

Part: NONE — NONE · airframe 104,077 hrs · 16,096 cycles

AIRCRAFT 1521, FOUND 01EA CRACK APPROX 0.350 INCH IN LENGTH ON RH NOSE WHEEL WELL BULKHEAD CHORD AS MARK, AND THE CRACK DO NOT EXTEND BELOW WL159. CORRECTIVE ACTION: REPAIRED THE CRACKED RH NOSE WHEEL WELL BULKHEAD CHORD AS PER B767-300 SRM 51-70-12-OG FIG1. (2331691)

Part: FITTING — CORRODED (NOT REPORTED) · airframe 110,062 hrs · 17,217 cycles

SHIP 1521 ER/A 600432-14 WAS ISSUED FOR WING CENTER SECTION NAD LH PICKLE FORK FITTING CORROSION REMOVAL. DTA/DTE IS REQUIRED. CORRECTIVE ACTION: REDEFFERED LOG TO QC, ESTABLISHED MONITOR INSP (2330679)

Part: NONE — NONE · airframe 104,004 hrs · 16,075 cycles

SHIP 1521 SLIDE INDICATOR LIGHT INOP OR DAMAGED, CORRECTIVE ACTION: ADJUSTED L1 DOOR ARM DISARM LEVER PER B767 AMM 52-11-02 CKS GOOD. (2018419)

Part: NONE — NONE · airframe 103,922 hrs · 16,057 cycles

SHIP 1521 SEAT 17F EEPL INOP . CORRECTIVE ACTION: REPLACED CONNECTOR ON SEAT PER AMM 767-300 33-51, OPS NML. (7989785)

Part: NONE — NONE · airframe 103,840 hrs · 16,042 cycles

SHIP 1521 COCKPIT EXIT SIGN DOES NOT ILLUMINATE WHEN EMERGENCY LIGHT TEST PERFORMED. CORRECTIVE ACTION: REPLACED POTABLE COCKPIT EMERGENCY EXIT SIGN. SYSTEM OPERATION IS NORMAL (LP 7989744)

Part: NONE — NONE · airframe 103,794 hrs · 16,032 cycles

SHIP 1521 SLIDE INDICATOR LIGHT INOP OR DAMAGED LOCATIONS:607 CORRECTIVE ACTION: ADJUSTED LIGHT SOCKET. NOW OPS NORMAL. (1987054)

Part: NONE — NONE · airframe 103,794 hrs · 16,032 cycles

SHIP 1521 SLIDE INDICATOR LIGHT INOP OR DAMAGED LOCATIONS:607. CORRECTIVE ACTION: ADJUSTED LIGHT SOCKET. (1987051)

Part: PROBE — FAILED (TAT) · airframe 103,421 hrs · 15,948 cycles

SHIP 1521 EXCESSIVE WHITE PUFFS MIST/SMOKE FROM CAPTAINS SIDE PITOT TUBES OR TAT ON TAXI INTERMITTENT. CORRECTIVE ACTION: SUSPECT TAT PROBE FAILING INTERNALLY. REPLACED TAT PROBE. SYSTEM OPERATION IS NORMAL. (LP 8011264)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 102,344 hrs · 15,763 cycles

DURING SERVICE CHECK FOUND EMERGENCY PATH LIGHTS AT ROW 14-20 INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 101,815 hrs · 15,687 cycles

SEAT 15B EMERGENCY EXIT LIGHT INOP. REPLACED BULBS - NO HELP - 669526. T/S IAW B767 FIM 33-51. FOUND PUSHED BACK PIN INSIDE OF CONNECTOR PLUG. RESECURRED PIN, OPS CHECK GOOD. (LP1320703)

Part: TERMINAL — UNSECURE (EMERGENCY LIGHT) · airframe 101,070 hrs · 15,592 cycles

EMERGENCY LIGHTS FORWARD GALLEY ARE INOPERATIVE. FOUND WIRES ON GALLEY TERMINAL STRIP NOT SECURED AND SECURED. SYSTEM OPERATION IS NORMAL.

Part: QUICK DISCONNECT — DISCONNECTED (CABIN) · airframe 100,332 hrs · 15,500 cycles

BOTH RED AND WHITE EMERGENCY LIGHTS AT ROW 21 AB ARE INOPERATIVE. FOUND QUICK DISCONNECT DISCONNECTED. RECONNECTED. SYSTEM OPERATION IS NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 99,858 hrs · 15,439 cycles

EMERGENCY LIGHTS AT ROWS 13-20 RIGHT SIDE ARE INOPERATIVE. REPAIRED DAMAGED WIRE AT ROW 14R AND REPLACED BLOWN FUSE ON BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,182 hrs · 15,331 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT STA 1131- T0 1153 HAVE CORROSIOM BETWEEN STR 37-38 LT SIDE. REPAIRED. (LP 0975552)

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,182 hrs · 15,331 cycles

CORROSION LEVEL: 2 FWD CARGO AT STATION 764 BETWEEN STRINGERS S-37R AND S-38R. EVIDENCE OF CORROSION INSTALLED NEW ANGLE. (LP 0975479)

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,296 hrs · 15,347 cycles

FUSELAGE SKIN BS 654 PLUS 121-BS 676 S34L-S35L CORRODED. C/W ERA 575584-14. (LP 0976371)

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 102,520 hrs · 15,789 cycles

DURING AN H1 MAINTENANCE CHECK IN AAR-MIA, INSPECTION FOUND CORROSION ON UPPER SURFACE SKIN OF HORIZONTAL STABILIZER CENTER SECTION AT THE LEADING EDGE OF FRONT SPAR BETWEEN RBL 18 TO RBL 27, C/W ERA 575801-14. (LP 0975484)

Part: FRAME — CORRODED (FUSELAGE) · airframe 99,182 hrs · 15,331 cycles

CORROSION LEVEL: 1 FRAME CORRODED STA 1439, STR 17L-18L BLENDED SMOOTH AND REMOVED CORROSION PER ERA 575215-14.( LP 0975638)

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,182 hrs · 15,331 cycles

CORROSION LEVEL: 2 REWORK REPAIR AT AFT CARGO COMPARTMENT STA 1087-1109 STR 37L -38L INSTALLED REPAIR DOUBLER. C/W ERA 575939-14. (LP 0975490)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 FRAME CORRODED BS 1087, STR 18R-20R REPAIRED PER ERA 575218-14. (LP 0973894)

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT STA 1087 TO 1109 HAVE CORROSION BETWEEN STG 37L T0 38L. REPAIRED. (LP 0966779)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 AFT CARGO BETWEEN STA 1307 AND STA 1285 S39R CORRODED. INSTALLED NEW STRINGER. (LP 0966754)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 STRINGER 18R CORRODED AT STA 808. REPLACED STRINGER. (LP 0966564)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 AFT CARGO STA 1307 BETWEEN S39R AND S39L ANGLE CLIP CORRODED OUT OF LIMITS. REPLACED STRINGER. (LP 0966742)

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 AFT CARGO FLOOR STRUCTURE WEB CUT OUT HAS CORROSION UNDER NUT PLATES AT STA 1153 TO 1175, LBL 10 TO RBL 10.BLEND AND REMOVED CORROSION FROM STIFFENERS WITHIN LIMITS, FABRICATED STRAP, ALODINE PRIME AND TOP COAT AND INSTALLED AFT CARGO FLOOR STRUCTURE WEB CUT OUT @ STA 1153-1175 LBL 10-10R (LP 0965339)

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 CABIN PAX RT OVERWING EMERGENCY EXIT FWD FRAME LOWER CORNER CUTOUT WITH CORROSION. C/W ERA 575138-14. (LP 0965563)

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 AFT CARGO STA 1307 BETWEEN S39R AND S39L ANGLE CLIP CORRODED. REMOVED STRINGER SECTION FROM STA 1220-1307 STGR 39R FOUND CORROSION OUT OF LIMITS. INSTALLED NEW STRINGER. (LP 0965316)

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 CORROSION AT BULK CARGO COMPART STA 1560 BETWEEN STG 39L TO 39R. REPLACED ANGLE AT BULK CARGO. (LP 0965569)

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 CREASE BEAM WEB CORRODED BS 1274, STR 20L REMOVED CHANNEL TRUSS CORRODED OUT OF LIMITS AND INSTALLED NEW TRUSS. (LP 0959520)

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 AFT CARGO FLOORBEAM CORRODED STA 1175, RBL 12. INSTALLED REPAIRED ANGLE. (LP 0962345)

Part: CREASE BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 CREASE BEAM OUTER CORD UPPER SURFACE CORRODED BS 1197+99, STR 20L BLENDED AND REMOVED CORROSION, INSTALLED REPAIR ANGLE ON DISCREPANT AREA (LP 0958255)

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

AFT CARGO COMPARTMENT STA 1197 +110 AREA B/W STG35L TO 35R HAS EVIDENCE OF CORROSION. REPLACED SHEAR TIE. (LP 0958032)

Part: SHEAR TIE — CORRODED (BS 1175) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 AFT CARGO STA 1175 BRACKET BETWEEN S37R AND 37L CORRODED. REPLACED SHEAR TIES. (LP0958050)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT STA 1197+88 STG 36L TO 37R HAVE EVIDENCE OF CORROSION. REPLACED SHEAR TIE. (LP 0961263)

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2ANGLE CORRODED BETWEEN STRINGER AND SKIN STA 1351, STRINGER 17R . INSTALLED NEW SHEAR TIE. (LP 0959748)

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 CLIP CORRODED BETWEEN FRAME AND STRINGER 1395 STR 16L. INSTALLED NEW CLIP. (LP 0962311)

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 CORROSION IN PAX CABIN ON BRACKET AT STA 1043 S-18L. INSTALLED NEW BRACKET/CLIP. (LP 0962326)

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 SEAT TRACK CORRODED AT RBL88, STA 1080, 1065 AND 966 OUT OF LIMITS. REPLACED SEAT TRACK. (LP 0958199)

Part: FRAME — CORRODED (BS 1197) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL 2 - CORROSION ON FRAME 1197+88 BETWEEN S-18R AND S-20R. REPAIRED PER ER/A 575228-14. (LP 0940842)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 FRAME CORRODED BS 1351, STR 18L-19L. REMOVED CORROSION FOUND OUT OF LIMITS, REPAIRED PER SRM 53-00-07. (LP 0958186)

Part: FRAME — CORRODED (BS 1131) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 FRAME CORRODED BS 1131,STR 16L-17L. BLENDED AND REMOVED CORROSION. ALODINE AND PRIMED, LOCATED DRILLED AND DEBURRED REPAIR ANGLE, INSTALLED. (LP 0958107)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 FRAME CORRODED BS 1241, STR 19R-20R. INSTALLED NEW ANGLE. (LP 0959486)

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,175 hrs · 15,328 cycles

CORROSION LEVEL: 2 FRAME CORRODED BS 1417, STR 18R. INSTALLED NEW ANGLE PER SRM 53-00-07. (LP 0959476)

Part: CYLINDER — DISCHARGED (LT SPOILER) · airframe 99,034 hrs · 15,308 cycles

LEFT SPOILER OVERRIDE ACTUATOR DISCHARGED. REPLACED LT SPOILER ACTUATOR SQUIB AND INFLATION CYLINDER. (LP 5336613)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,040 hrs · 14,468 cycles

FOUND EMERGENCY LIGHT AT LAVATORY 1 RIGHT, RED ASSEMBLY BROKEN. REPLACED . SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 92,006 hrs · 14,313 cycles

SEAT 19GF EMERGENCY LIGHTS ARE INOPERATIVE. FOUND CONNECTOR DISCONNECTED ON SIDEWALL AND RECONNECTED. SYSTEM OPERATION IS NORMAL.

Part: FRAME — CORRODED (BS 955 BULKHEAD) · corrosion level 2 · airframe 90,768 hrs · 14,116 cycles

RIGHT MLG WW FWD BULKHEAD FRAME AT BS 955 RBL 80 - 88 FOUND CORRODED. REPAIRED IAW ER/A 551309-14.

Part: FRAME — CRACKED (NOT REPORTED) · airframe 90,768 hrs · 14,116 cycles

RIGHT SIDE FRAME INNER STRUCTURE CRACKED. REPAIRED IAW ERA 555728-14.

Part: FRAME — CRACKED (BS 903) · airframe 90,768 hrs · 14,116 cycles

HFEC INSPECTION FOUND ONE CRACK ON THE RT BS 903.5 FRAME INNER STRUCTURE SURFACE AND TRANSITION RADIUS. REPAIRED THE FRAME.

Part: FRAME — CRACKED (BS 859) · airframe 90,768 hrs · 14,116 cycles

HFEC INSPECTION, FOUND ONE CRACK AT BS 859.5 FRAME. REPAIRED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 85,283 hrs · 13,292 cycles

COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE DURING TEST. MAINTENANCE INSTALLED NEW BATTERIES AND NEW LIGHT ASSY. SYSTEM OPS IS NORMAL.

Part: SKIN — BENT (FUSELAGE) · airframe 81,948 hrs · 12,820 cycles

FUSELAGE SKIN IS BENT DOWN JUST AFT OF TAIL, SKID. REPAIRED IAW ERA 532413-14.

Part: WINGLET — NOT REPORTED (NOT REPORTED) · airframe 81,858 hrs · 12,809 cycles

WINGLET REPAIRED IAW AA 5724-01010 SECT 19, 20. / 

Part: SUPPORT STRAP — CORRODED (BS 1010) · airframe 81,859 hrs · 12,809 cycles

CORROSION ON KEEL BEAM PANEL SUPPORT STRAP AT BS 1010. R & R SUPPORT.

Part: SUPPORT STRAP — CORRODED (BS 950) · corrosion level 2 · airframe 81,859 hrs · 12,809 cycles

CORROSION ON PANEL SUPPORT STRAP AT BS 950 KEEL BEAM. R & R SUPPORT IAW SRM 53-50-12.

Part: FLOORBEAM — CORRODED (BS 654) · corrosion level 2 · airframe 77,487 hrs · 12,209 cycles

BS 654+66, RBL 22, FLOORBEAM FOUND CORRODED. FLOORBEAM UPPER FLANGE REPAIRED FROM LBL 47 TO RBL 33 IAW SRM 53-00-51.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 76,371 hrs · 12,067 cycles

EMERGENCY LIGHTS AT ROW 21-31 FG INOPERATIVE. MX REPLACED FUSE AT THE BATTERY PACK9. OPS CHECKED OK.

Part: LIGHT — UNSECURE (COCKPIT) · airframe 74,800 hrs · 11,880 cycles

PILOT REPORTED COCKPIT EXIT LIGHT UNSECURE. SECURED COCKPIT EXIT LIGHT. SYS OPS IS NORMAL.

Part: TERMINAL — DISCONNECTED (EMERGENCY LIGHT) · airframe 73,358 hrs · 11,694 cycles

EMERGENCY RED R1 LIGHT IS INOPERATIVE. MX RETERMINATED AND SECURED TERMINALS. SYS OPERATION IS NORMAL.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 73,358 hrs · 11,694 cycles

EMERGENCY DOOR LIGHTS AFT LT AND RT ARE INOPERATIVE. MX REPLACED A BROKEN FUSE. SYSTEM OPERATION IS NORMAL.

Part: FAILSAFE — CRACKED (BS 955) · airframe 73,330 hrs · 11,690 cycles

CRACK INDICATION FOUND ON LT BS 955, REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP. REPAIRED CARRIED OUT IAW ERA 509690-14AD, REV ORG.

Part: FAILSAFE — CRACKED (BS 955) · airframe 73,330 hrs · 11,690 cycles

CRACK INDICATION FOUND ON RT BS 955. REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP. REPAIRED CARRIED OUT IAW ERA 509691-14AD REV ORG.

Part: FAIRING — DAMAGED (THRUST REVERSER) · airframe 73,330 hrs · 11,690 cycles

NR 2 ENGINE INBD THRUST REVERSER AIRSTREAM T/E UPPER FAIRING DAMAGED. REPAIRED IAW CMM 78-32-00, REPAIR 007, PAGE 603.

Part: FITTING — MISMANUFACTURED (PYLON) · airframe 73,330 hrs · 11,690 cycles

DURING ACCOMPLISHMENT OF PYLON MODIFICATION, FOUND 2 EA HOLES ON SIDE-LOAD FITTING HAVING SHORT EDGE MARGIN. SHORT EDGE MARGIN CONDITION FOUND TO BE ACCEPTABLE AND TO REMAIN AS IS IAW ERA 570077-14AD, REV 0, STEP 2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 72,143 hrs · 11,547 cycles

SKIN BULGED AFT OF AFT LAV SERVICE PANEL BOTTOM CENTER FUSELAGE. COMPLIED WITH PERMANENT REPAIR PER ERA 506773-14 REV ORIG REF NRC 007.

Part: SPAR — CRACKED (NR 1 NACELLE) · airframe 69,479 hrs · 11,227 cycles

DURING PSV, FOUND TWO CRACKS EMANATING FROM THE NR 1 PYLON UPPER FWD SPAR WEB AT THE FWD I/B AND THE AFT O/B CORNERS OF THE GENERATOR FEEDER CABLE CUTOUT. REPAIRED IAW ERA 500275-14 REV "O" BY ACCOMPLISHING EO 1-7498-3 REV A ME-07.

Part: WIRE — BROKEN (CABIN) · airframe 68,620 hrs · 11,126 cycles

EMERGENCY LIGHTS AT SEAT 23GF ARE INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AND REPAIRED. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHT) · airframe 64,103 hrs · 10,604 cycles

EMERGENCY LIGHT AT SEATS 22GF ARE INOPERATIVE. MX FOUND WIRE BROKEN AT CONNECTOR AND RE-TERMINATED. SYS OPERATION IS NORMAL.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHT) · airframe 63,815 hrs · 10,571 cycles

EMERGENCY EGRESS AISLE LIGHTING IS INOPERATIVE AT ROW 34. MX RECONNECTED THE HARNESS AND SYS NOW CHECKS OK.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 63,551 hrs · 10,541 cycles

EMERGENCY LIGHTS CTR BULKHEAD, ROW 20 ARE INOPERATIVE. MX REPLACED A BROKEN WIRE ON THE RT SIDE OF THE BULKHEAD. SYS OPS IS NORMAL.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 62,759 hrs · 10,451 cycles

FOUND DURING PSV13 THE INBD SIDE SKIN OF THE NR2 ENG PYLON WAS FOUND CRACKED AT THE OVAL CUTOUT AT APPROX NAC STA 235 AND RAN FROM THE UPPER AFT CORNER APPROX 2.5 IN AND TERMINATES AT A FASTENER. REPAIRED IAW ERA 486275-14 REV ORIG.

Part: ENGINE — MALFUNCTIONED (APU) · airframe 62,563 hrs · 10,427 cycles

APU FAILED 3 COLD SOAK START ATTEMPTS. COLD SOAK START WAS SUCCESSFUL ON SUBSEQUENT FLIGHT.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 61,189 hrs · 10,271 cycles

EMERGENCY PATH LIGHTS AT SEAT 32AB AND 35AB ARE INOPERATIVE. MAINTENANCE RE-PINNED CONNECTOR. SYSTEM OPERATION IS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 59,416 hrs · 10,063 cycles

RED EMERGENCY EXIT LIGHT INOP AT DR 2R RT SIDE OF GALLEY 407. FOUND BROKEN WIRE UNDER CARPET EDGE AT GALLEY SIDEWALL. SPLICED WIRE - OPS NORMAL.

Part: INDICATOR — FAILED (AIRSPEED) · airframe 57,965 hrs · 9,881 cycles

STBY AIRSPEED INDICATOR FAILED. REMOVED AND REPLACED STANDBY AIRSPEED IND IAW AMM PERFORMED PITOT PUMP UP TEST PER AMM 34-13-00, LEAK CHECK GOOD. STANDBY AIRSPEED IND OPS CHECK GOOD, OK FOR SERVICE. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: SKIN — PUNCTURED (FS 1767 S28L) · airframe 56,468 hrs · 9,710 cycles

AFT FUSELAGE FS 1767 AT STR 28L SKIN PUNCTURED. REPAIRED PER ERA 475586-14 REV A.

Part: PUMP — MALFUNCTIONED (FUEL SYSTEM) · airframe 54,936 hrs · 9,539 cycles

LT CENTER FUEL PUMP LIGHT ILLUMINATED. LT FUEL OVRD PUMP C/B OPEN. T/S PER FIM. OPEN ACCESS PNL FOR PUMP. REMOVED CONNECTOR INSPECTED PINS AND SOCKET NO TROUBLE FOUND. INSPECTED HARNESS VISUALLY IN HOUSING AREA NO DEFECTS NOTED C/B RESET OPERATED PUMP 25 MIN NO TROUBLE FOUND. REINSTALLED PANEL.

Part: CONTROL VALVE — UNSERVICEABLE (RT PACK BAY) · airframe 54,885 hrs · 9,533 cycles

RT PACK WOULD NOT COME ON AFTER 2ND ENG START. CYCLED BLEEDS AND N-19 N-20 PER MTC NO IMPROVEMENT. REMOVED AND REPLACED FLOW CONTROL VALVE. OPS OK PER AMM.

Part: PUMP — INOPERATIVE (FUEL BOOST) · airframe 54,138 hrs · 9,450 cycles

CTR FUEL PUMPS DID NOT COME ON WHEN BOTH ENGS ON LINE FWD TO MCO/PLAC MEL 28-22-02A, RT CTR C/B PULLED AND COLLARED, LT CTR WORKS OK. ACFT RETURNED A SECOND TIME FOR INOP CTR BOOST PUMP. REPLACED RELAY K330. OPS CHECK GOOD.

Part: HEAT EXCHANGER — CRACKED (RIGHT) · airframe 53,372 hrs · 9,364 cycles

RT PACK INOP ON BOTH APU AND ENG BLEEDS. WORKED FINE ON APU AT GATE. FAILED WHEN SWITCHED TO ENG BLEED. AT GATE RT PACK CHECKED NORMAL WITH APU AIR. FOUND TWO INCH CRACK IN RT HEAT EXCHANGER REHEATER. REMOVED AND REPLACED REHEATER PER AMM. LEAK CHECK GOOD, MPN 194274-4.

Part: GCU — ODOR (RIGHT) · airframe 49,724 hrs · 8,953 cycles

JUST AFTER LEVELING OFF AT FL390 NOTICED A DISTINCT ELECTRICAL SMELL SHORTLY AFTER THE LEFT AND RIGHT UTILITY BUSS LIGHTS AND RT GEN DRIVE LIGHTS ILLUMINATED ON OVERHEAD PANEL WITH EICAS MESSAGES. NOTICED SLIGHT WHIFF OF SMOKE IN COCKPIT. FOLLOWED QRH PROCEDURES FIELD OFF LIGHT ON AUX PANEL ILLUMINATED SMOKE AND FUMES DISSIPATED SHORTLY THERE AFTER. REMOVED RT GCU FOUND BAD BURNED ODOR. OPENED NR 2 ENGINE AND INSP FEEDER CABLES FROM GEN TO PYLON DISCONNECT. NO VISUAL TROUBLE FOUND. REPLACED RT GEN CONTROL UNIT. REPLACED RT IDG PER AMM CHECKS GOOD.

Part: SKIN — NICKED (FS 1300 S26-36L) · airframe 49,287 hrs · 8,889 cycles

MINOR NICKS IN SKIN BLENDED IN STA 1219 - 1307/STR 26L - 36L.

Part: PUMP — INOPERATIVE (CTR FUEL TANK) · airframe 47,944 hrs · 8,736 cycles

RTB - RT CTR FUEL PUMP IS INOP. RESET C/B`S AND RAN ENGINE. PUMP OPS NORMAL.

Part: COMPRESSOR — UNSERVICEABLE (POTABLE WATER) · airframe 45,728 hrs · 8,477 cycles

BURNING ELECTRICAL SMELL IN AFT RT GALLEY DURING LEFT ENGINE START. NO SMOKE RETURNED TO GATE. LOCATED POTABLE WATER COMPRESSOR MOTOR BURNED INOP FWD TO MCO/PLAC PER MEL 38-10-01A PULLED AND COLLARD C/B ON P33 PANEL FOR COMPRESSOR NEEDS NEW COMPRESSOR. FOUND POTABLE WATER COMPRESSOR MOTOR AT FAULT REPLACED PER AMM. OPERATION LEAK CKS GOOD. REMOVED MCO AND PLACARD.

Part: WIRE — OPEN (CONTROL PANEL) · airframe 44,671 hrs · 8,341 cycles

TAT LIGHT NOT ON WHILE ON GROUND FWD TO MCO AND PLACARD AS PER MEL 30-31-02, T/S PER WDM. FOUND BAD WIRE AT PIN D-3 OF K644 L PROBE HT N2 P33 PANEL. RETERMINATED WIRE NOW ALL CHECKS GOOD. MCO AND P REMOVED.

Part: ISOLATION VALVE — MALFUNCTIONED (LEFT SYSTEM) · airframe 42,736 hrs · 8,103 cycles

LEFT ISOLATION VALVE STUCK IN DISAGREE. VALVE CYCLED MANUALLY AND DEFECT CLEARED. REMOVED AND REPLACED VALVE PER M/M, OPS CHECK GOOD .

Part: CONTROL PANEL — UNKNOWN (AFT WASTE TANK) · airframe 41,881 hrs · 8,000 cycles

AFT WASTE TANK FAIL 4 OF 6 TOILETS FAILED TO FLUSH. PULLED AND RESET C/B R8 ON P11 OVERHEAD PANEL AND M1 ON THE P34 PNL. NO HELP. FOUND AFT TOILETS WASTE FULL, DUMPED SAME. ALL OPS OK. BITE CK OK. REPLACED AFT TANK WASTE TANK CONTROL BOX AND DUMPED ACETIC ACID IN ALL LAVS AS PRECAUTION SYS OPS OK. TANKS EMPTY.

Part: CDU — INOPERATIVE (COCKPIT) · airframe 40,010 hrs · 7,771 cycles

IR - RT CDU WENT BLANK EN ROUTE RESET WITH CB NO FIX. CDU LEFT NO FIX. CDU RT SELECT ON F/O SIDE GOT V TRACK FLAG. FOUND RT CDU COOLING SCREEN CLOGGED CAUSING O/HEAT. REPLACED RT FMS CDU PER MM. CKS OK.

Part: WINDOW — MALFUNCTIONED (COCKPIT) · airframe 39,706 hrs · 7,730 cycles

PILOTS WINDOW CAME OPEN ON T/O ROLL AFTER PASSING 80 KTS. PRIOR TO T/O HANDLE WAS VERIFIED IN LOCKED POSITION. ABORTED T/O ROLL AT 100 KTS. MTC VERIFIED OPERATION AND LOCKING MECHANISM WORKS OK. PERFORMED HIGH ENERGY STOP INSPECTION. ALL NORMAL.

Part: RELAY — INOPERATIVE (ESCAPE SLIDE) · airframe 39,567 hrs · 7,712 cycles

WHILE PERFORMING ETOPS PRE-DEPARTURE CHECK, NR 1 AND NR 2 LT AND RT OVERWING ESCAPE SLIDE SQUIB TEST LIGHTS WOULD NOT ILLUMINATE. REPLACED K-839 RELAY, SYSTEM TEST CHECKS OK.

Part: MODULE — MALFUNCTIONED (RUDDER) · airframe 38,762 hrs · 7,613 cycles

RUDDER RATIO LIGHT AND MSG CAME ON DURING TAXI OUT. UNABLE TO RESET, RETURNED TO GATE. FOUND LEFT RUDDER RATIO MODULE FAULTED. RESET SAME, PERFORMED RUDDER RATIO TEST, CHECKS GODD. OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 38,156 hrs · 7,537 cycles

ON SQUIB TEST FOUND LEFT SIDE AND RT SPOILER WILL NOT TEST. REPLACED BATTERIES M962 AND M961 OFF WING BATTERY PACKS. OPS CKD NORMAL.

Part: ENGINE — DAMAGED (NR 2) · airframe 35,914 hrs · 7,237 cycles

BORESCOPE NR 2 ENG BOOSTER (LPC) AND HPC PER AMM TASK 72-00-00-206-H00 DUE TO PARAMETER SHIFT ON ENG. TREND AND RECENT FAN BLADE REPLACEMENT FOR IMPACT. ENGINE FAILED BOROSCOPE INSPECTION. REPLACED ENGINE.

Part: WIRE HARNESS — CHAFED (FWD GALLEY) · airframe 35,655 hrs · 7,202 cycles

F/A RECEIVING SHOCKS WHEN CONTACTING METAL DOOR IN FWD GALLEY NEAR COFFEEMAKERS. REPAIRED CHAFED GALLEY POWER WIRES.

Part: BATTERY — DISCHARGED (ESCAPE SLIDE) · airframe 35,579 hrs · 7,194 cycles

P-61 SQUIB TEST PANEL WON`T TEST CORRECTLY. REPLACED TEST PANEL, 2 EMERGENCY BATTERIES (M961 &M962 ) & 1 CHARGER ASSY. OPS CHECKS GOOD.

Part: BOTTLE — DISCHARGED (L1 SLIDE) · airframe 33,319 hrs · 6,847 cycles

1L DOOR SLIDE BOTTLE READING 0 PSI. REMOVED AND REPLACED 1L DOOR SLIDE PER AMM 25-66-01.

Part: BATTERY — DISCHARGED (ESCAPE SLIDE) · airframe 30,904 hrs · 6,493 cycles

ON PDC FOUND LEFT SLIDE AND RIGHT SPOILER SQUIBS NOT TESTING IN COCKPIT. REPLACED BATTERY PACK AT 22G, CHECKS NORMAL.

Part: TUBE — LOOSE (NR 2 ENGINE) · airframe 28,864 hrs · 6,158 cycles

ON DEPARTURE, RIGHT ENGINE OIL PRESSURE AND QTY WENT TO ZERO. FOUND SHROUD B-NUT ON NBR 6 BEARING SCAV SUPPLY TUBE LOOSE - SECURED SAME - LIMITS FOR LOSS OF OIL PSI NOT EXCEEDED IAW PIREP AND MTC OBSERVANCE - C/W REQD INSPN IAW AMM 72-00-00- LK AND OPS CK GD ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: ENGINE — FAILED (NR 2) · airframe 28,846 hrs · 6,156 cycles

ON TAKEOFF ROLL, ABORTED AT 100 KTS DUE TO NR 2 ENG FAILURE. FLAMES REPORTED COMING FROM THE FRONT AND REAR OF THE ENG. ENG EXPERIENCED A COMPRESSOR STALL. ENGINE CHANGE IN WORK IN BOM.

Part: SMOKE DETECTOR — WILL NOT TEST (LAVATORY) · airframe 27,926 hrs · 5,981 cycles

ON L/O FOUND LT AFT LAV SMOKE DETECTOR WILL NOT TEST. REPLACED DETECTOR, CHECKS OK.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 27,203 hrs · 5,853 cycles

ON PDC FOUND LEFT OVERWING SLIDE SQUIB NOT ILLUMINATING WITH TEST SWITCH 1. RT SPOILER SQUIB LIGHT WILL NOT ILLUMINATE WITH TEST SWITCH 2. INSTALLED NEW BATTERY POWER SUPPLY AND BATTERY M962. ALL SQUIB TESTS NOW OK.

Part: CONTROL UNIT — MALFUNCTIONED (E/E BAY) · airframe 24,097 hrs · 5,339 cycles

IN CRUISE LOST LEFT SYMBOL GENERATOR FOLLOWED 5 MINS LATER BY RUDDER RATIO AND AILERON LOCKOUT EICAS MSGS AND LOSS OF ALL 3 AUTOPILOTS. FOUND LEFT SAM W/ FAULT BALL. WILL NOT RESET. CYCLED 1L AND 2LAC AND DC FLT CTL ELEC C/B'S. ALL FAULTS CLEARED. REPLACED 1L AND 2L CSEUS AS PRECAUTION. RERACKED LEFT SYMBOL GEN. ALL OPS OK. PERFORMED TEST 40 FOR A/P. CHECKS OK.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 23,034 hrs · 5,164 cycles

DURING CRUISE A BURNING ELECTRICAL SMELL IN FORWARD GALLEY FAULT TRACED TO NUMBER 1 COFFEEMAKER. REMOVED SAME, CB PULLED AND COLLARED NIS LGW FWD TO MCO AND PLACARD PER MEL. CB PULL FOR COFFEEMAKER 2 AS PRECAUTION.

Part: CDU — FAILED (COCKPIT) · airframe 20,593 hrs · 4,753 cycles

CAPTS FMC CDU WENT BLANK. REPLACED CDU. FMS OPS CHECKS OK.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 15,445 hrs · 3,923 cycles

THE FUSELAGE SKIN WAS TORN AND DENTED FROM CONTACT WITH GROUND EQUIPMENT AT STRINGER 23R BETWEEN FS 654+22 & FS 654+44. THE DAMAGED SECTION OF STRINGER WAS REMOVED AND SPLICED PER THE B767 SRM. THE DAMAGE TO THE SKIN WAS REMOVED WITH A 9.8 X 1.2 CUTOUT AND A 4.3 X 1.4 CUTOUT. BOTH CUTOUTS WERE REPAIRED WITH A SINGLE ALUMINUM DOUBLER/TRIPLER REPAIR PER ER/A 377520-14, REV A.

Part: OVEN — MALFUNCTIONED (GALLEY)

GALLEY MID CABIN CENTER OVEN OVERHEATS, TOP WILL NOT SHUT OFF. REPLACED OVEN, SYSTEM CHECKS NORMAL.

Part: AIR DIST — ODOR (CABIN)

ELECT ODOR IN FWD CAB AND AFTER CAPTS SIG GEN WENT OUT, OUTSIDE ELECTRICAL ACTIVITY WAS HIGH. AFTER SHUTTING OFF UTIL BUSSES THE ODOR WENT AWAY IMMEDIATELY. LATER INFLIGHT ALL GALLEY C/BS PULLED AND RT UTILITY BUS TURNED ON WITH RECIRC FANS OFF. NO FUMES REST OF FLT. COULD NOT DUPLICATE ELECT ODOR. BOTH UTIL BUSSES RESET ON EACH, RECIRC FAN OPERATED INDIVIDUALLY. ALL GALLEY C/BS RESET AND GALLEY EQUIP OPERATED FOR 1 HR. ELEC EQUIP BAY INSPECTED, C/BS CHECKED. ALL NORMAL, NO PREVIOUS HISTORY. PER ATL OCC, A/C TO BE MONITORED.

Part: FAN — FAILED (CABIN)

STRONG ELECTRICAL SMELL AROUND SEATS 35-37 F/G. FOUND AFT EQ EXHAUST FAN 1 EMITTING ELECTRICAL ODOR, REPLACED FAN.

Part: VALVE — LEAKING (RT WING)

ON TAXI OUT, FOUND FUEL LEAKING ON RT WING. FOUND SURGE BOX RELIEF VALVE LEAKING. RESEATED, LEAK CHECKS NORMAL.

Part: OVERHEAT LOOP — MALFUNCTIONED (NR 2 ENGINE)

AT FL330, LEFT ENGINE OVHT LIGHT ON PEDESTAL. RETARDED ENG TO IDLE, LIGHT REMAINED ON FOR APPROX 3 MINUTES. NO ASSOCIATED MASTER CAUTION OR EICAS MESSAGE. REPLACED OVHT DET LOOP M684 AND LOGIC TEST CARD. ALSO, CHECKED ALL CLAMPS ON ENGINE AND TIGHTENED SAME. SYSTEM CHECKS OK.

Part: LOGIC CARD — MALFUNCTIONED (NR 1 ENGINE)

LEFT ENGINE OVERHEAT LIGHT PASSING 10,000 FT, LIGHT EXTINGUISHED WHEN POWER REDUCED. INSPECTED OVERHEAT LOOP AT LEFT ENGINE, CHECKS OK. MOTORED ENGINE, INSPECTED FOR AIR LEAKS AT LOOP AREA, NO LEAKS. REPLACED LOGIC TEST CARD M10224. RAN ENGINE AT T/O POWER, SYSTEM NORMAL.

Part: TERMINAL — BROKEN (NR 1 ENGINE)

STATUS MSG LEFT ENGINE FIRE LOOP 1 AND FIRE LOOP 2 AND NO LEFT ENGINE FIRE TEST. FOUND TERMINALS BROKEN AT WIRES W5340-9001 AND 9002R ON LWR FWD LOOP. INSTALLED TEMPORARY TERMINAL AND MTC FERRIED A/C FOR PERM REPAIR.